Beechcraft Turbo-Baron 56TC, Shop Manual

Page 1: ...ES ATP is a registered trademark of Aircraft Technical Publishers All original authorship of ATP is protected under U S and foreign copyrights and is subject to written license agreements between ATP and its Subscribers ALL RIGHTS RESERVED NO PART OF THIS PUBLICATION MAY BE REPRODUCED STORED IN A RETRIEVAL SYSTEM OR TRANSMITTED IN ANY FORM BY ANY MEANS ELECTRONIC MECHANICAL PHOTOCOPYING RECORDING ...

Page 2: ...Revisions Record of Temporary Revisions List of Effective Pages Alphabetical Index 1 General Information Dimensions of Aircraft Power Plant Fuel System Miscellaneous Table of Torques Torque Wrenches Supplementary Publications 2 Ground Handling Servicing Ground Handling Ground Handling Servicing 3 Airframe Stations Diagram Fuselage and Empennage Skin Information Wing Skin Information Fuselage Acces...

Page 3: ... 14 Autopilot Beechcraft New Matic Autopilot 5 Landing Gear Brake System Brakes System Landing Gear System Brake System Troubleshooting 6 Power Plant Magnetos Turbo Charger System 7 Propeller 8 Fuel System 9 Pressurization Not Applicable TO Beech Turbo Barren 10 Heating Cooling System Heater Control System Heater Electrical System Heater Fuel System Air Conditioning System Optional Air Conditionin...

Page 4: ...Deicing System Goodrich Pitot and Static System Vacuum System Pressure System 12 Aircraft Finishes 13 Electrical System 14 Wiring Diagrams 15 Overhaul and Replacement Schedule Temporary Revision No 15 1 16 Periodic Inspections 50 Hour Inspection 100 Hour Inspection End of Index 10 03 2001 Copyright Aircraft Technical Publishers Page 3 of 3 BC 0431 MM ...

Page 5: ...IVIFGI IN RO ...

Page 6: ...TURBO B RON SHOP n LANUAL 56TC A56TC COPYRIGHT 0 BEECH 1995 P N 96 590003 5B PM 96 590003 5B5 Reissued September 1970 Revised August 1995 ...

Page 7: ...PUBLISHED 8Y COMMERCIAL PUBLICATIONS BEECH AIRCRAFT CORPORATION WICHITA i ANSAS g7201 U S A C eechcraft Ahl mbs GP hU I rB General Auiadan Manufadu en ...

Page 8: ...RECORD OF REV SIONS MFG RRI NO DESCRIPTION ISSUEDATE ATPRR DA INSERTED BY BS SEE L IST OF PA ES 8 95 03 09 98 ATP KS ...

Page 9: ...ev Rev Date Inserted By N No No Date Inserted By Date Inserted By ATP ss 03 09 98 XS When a revision is inserted the revision number the date the revision is inserted into the manual and the initials of the person s inserting the revision should be recorded on this page ...

Page 10: ...Of TEMPOW RY TEMP ATP REV INSERT DATE REV REMOVE RN NO DESCRIPTION ISSUE DATE DATE BY REMOVED INCOR BY 4 2 SEC 4 PG 4 18 11 15 93 03 09 98 9TP KS 4 3 SEX 4 PG 4 1 10 24 97 15 1 SE 15 PG 15 2 10 31 97 ...

Page 11: ...RECORD OF TEMPORARY REVISIONS REVISION CHAPTEW DATE INSERTED DATE REASON REMOVED NUMBER PAGE INSERTED BY REMOVED REMOVED BY AFFECTED 4 2 SM 4 4 18 03 09 98 ATP 4 3 4 4 1 15 1 15 15 2 NOTE Insert this Record of Temporary Revisions after the Record of Revisions page ...

Page 12: ... 8 and 1 8A 8 Sep 1970 4 5 8 Sep 1970 1 9 and 1 10 8 Sep 1970 4 6 thru 4 68 84 Jun 1985 2 1 thru 2 3 B Sep 1970 4 7 B Sep 1970 2 4 81 Dec 1976 4 8 and 4 6A 81 Dec 1976 NOTE A list of effective pages will be found in the front of each chapter 85 Basic publications are assigned a part number which appears on the title page with the date of the issue Subsequent revisions are iden tified by the additi...

Page 13: ...B Sep 1970 14 1 thnu 14 31 8 Sep 1970 5 7 thru 5 10A 8 2 Feb 1971 14 32 thru 14 35 B 1 Jan 1971 5 11 thru 5 12A B Sep 1970 14 36 thru 14 50 B Sep 1970 5 13 thru 5 14A B Sep 1970 14 50A and 81 Dec 1976 5 15 thru 5 21 B Sep 1970 14 51 6 1 thru 6 28 B Sep 1970 14 52 thru 14 54 8 Sep 1970 8 3 thru 6 6C B Sep 1970 14 55 8 3 Aug 1971 6 7 thru 6 13 B Sep 1970 14 56 thru 14 81 B Sep 1970 7 1 thru 7 3 B Se...

Page 14: ...NEOUS TABLE OF TORQUES TORQUE WRENCHES SUPPLEMENTARY PUBLICATIONS 2 GROUND HANDLING E SERVICING GROUND HANDLING SERVICING 3 AIRFRAME STATIONS DIAGRAM FUSELAGE fr EMPENNAGE SKIN INFORMATION WING SKIN INFORMATION FUSELAGE ACCESS OPENING WING ACCESS OPENINGS WING SEATS CABIN DOOR WINDOWS FIBERGLASS 4 FLIGHT CONTROLS F SURFACES AILERON SYSTEM ELEVATOR SYSTEM ...

Page 15: ...CONTROL SURFACES FLAPS H 14 AUTOPILOT BEECHCRAFT NEW MATIC AUTOPILOT 5 LANDING GEAR a BRAKE SYSTEM BRAKE SYSTEM LANDING GEAR SYSTEM BRAKE SYSTEM TROUBLESHOOTING 6 POWER PLANT POWER PLANT MAGNETOS TURBO CHARGER SYSTEM 7 PROPELLER1 8 FUEL SYSTEM 9 PRESSURIZATION 10 HEATING a COOLING SYSTEM HEATER CONTROL SYSTEM HEATER ELECTRICAL SYSTEM HEATER FUEL SYSTEM AIR CONDITIONING SYSTEM OPT ...

Page 16: ...TEM TRBLSHTING AIR COND 11 UTILITY SYSTEMS OXYGEN SYSTEM SURFACE DEICER SYSTEM ELECTRIC PROPELLER DEICING SYSTEM GOODRICH PITOT E STATIC SYSTEM VACUUM SYSTEM PRESSURE SYSTEM 12 AIRCRAFT FINISHES 13 ELECTRICAL SYSTEM 1 1 WIRING DIAGRAMS 15 OVERHAUL E REPLACE SCHEDULE 16 PERIODIC INSPECTIONS 50 HOUR INSPECTION 100 HOUR INSPECTION 4 t3 ...

Page 17: ...ALPHABETICAL INDEX ...

Page 18: ...or Removal and Installation 10 10 Overhaul Condenser Blower Removal 10 9 Removal andlns alla ion Ri ing the Ar Scoop and Ramp 10 9 Parking Brake Servicing Adjustment 3 1 the Frean System 107 Valve Overhaul Checking Compressor Oil Removing Wheel and Brake S X Level 1Q 8 illus 10 S Servicing Compressor Belt Tension 10 9 Wear Limits 5 1 Evaporator Air Filter Replacement 10 10 Breaker Point Adjustment...

Page 19: ...acement Guide 13 0A Control Column Single 4 1 Elevator Trim Tab Control Column Chain Riggin 4 l illus 4 2 LtZA Actuator Removal 4 68 Control System Turbocharger Actuator Installation 4 68 Controller Turbocharger Electric Trim Tab 4 60 illus 4 60 Variable Pressure 6 6A illus 6 5 Actuator R moval 4 60 Correspondence 1 1 Cable installation 4 60 Cowl Flap Actuator 6 1 Magnetic Clutch Installation 4 60...

Page 20: ...rter Front Seat Eiectrolyrz Xdjusrmenc Barterv 13 1 Insralladon 3 12J 3leMcor R moMi 3 12J Balancing Fuel Pump Heater kemovai ad Down Soring Loads L ia Insralladon 10 i Insrallaton 6 Fuel 8 1 mt s Removal 4 1 Adjustment of Tran mi ter Ri ng Boost PumD Recrric S 2B Elevator Skin Replacement Box Section Cell 8 6 lilus S j Elevator Tab Actuator iilus siSc Deiueling 8 1 Tab Actuator ssembiy Engine Dri...

Page 21: ...t 7 i iUus 7 1 Information General 1 3 Removal and installation I i Insoefdon Periodic 16 1 Grades L pproved Oil 2 i Installation and Initial Pun n Gtaoh Turjcs arger Periormance Turboc ar er 6 M CroLnd Handling LigXring 1 8 Xnchorine and Moorino 1 Interior Colors 126 External ower 2 3 Hoisting 2 IlillUS 2 7 lacking 2 1 J Lzveiing 2 i Tar ing Brak 1 1 Towino 1 1 Jac dng Ground R nning and Wsrm uD ...

Page 22: ...ion Chart ra Painting iluminum Lubrication Dia am ij Aodication 2 1 Surface Preparation 12 1 M Painting Ma ksium odicasion 3_ 5 Sla nesiun Painting ll j Paint Removal 12 5 Sun ace Preparation 12J Breaker Point Adjustment 6 18 P ailelino Drop off Check 6 1B Checks 13 8 IB mus 6 3B Pzridn o Brake Yam Lu dinl i r AdSuiunenr Maintenance and Repair H 14 1 2 Valve Overhaul Ciastet Cylinder Bralce Parior...

Page 23: ... 13 nectric Deicer 11 9 us 11 9 11 I Roton Locks Servicing 2 7 iilus 7 7 Boot kwalIation 11 13 us 11 i3 11 14 Rudder o Il lj ilIus 11 13 11 14 Balancing cr 16 iUus L 1 las allarion I Brush R Dlacsmanr 4 7 11 11 Rig ing I1 11 Tab Acmator Xssembty Rzsisranc Cheek T1 lj j Slip Ring Macirining ll 10A Tab Ri ging Timer Check 11 I1 TravelinInches Troubleshooting 7 7 Governor djusting 7 1 iilus 7 1 S Rem...

Page 24: ...letic autctr Insr arion j0 10 i Masletic Clusci Removal to O Soe ai Tools 1 iM eric Clutch Toroue SrlnS ads Elevator Stabiiiurion of Gnerlcor System aa ileron 13 7 Elevator 3 6 liluS eL StabBze Insrallation Horizontal udder 47 iilus 49 3 _17 Table of Thread Lubricants 2 9 Insralladan Vertical I Table oiforques 1 illus 1 3 Removal Horizontal 4 i3 Test Turbocha ner Critical 6 8 Removal Vertical 17_ ...

Page 25: ... Butterfly 6 7 Removal 3 16 Overhaul Facilides 6 7 Center Performance Graph 6 9 Installation 3 17 Rigging Throttle and Pressure Conrr ollet 66A Removal 3 17 Schematic illus 6 5 Cleaning Plastic 26 Troubleshooting 6 12 Forward Left Hand Variable Pressure Controlle 66X illus 6 5 Installation 3 16 Waste Gate Valve Adjustment 6 6C ilIus 6 6C Removal 3 15 Storm Installation 3 15 Removal 3 15 V Windshie...

Page 26: ...e entries for each subject Troubleshooting guides may be found at the close of each major systems discussion Serial effectivity is maintained throughout the manual to assure correct information for each airplane MODEL j6TC TG I through TG 83 MODEL Aj6TC TG 84 and after NOTICE WHEN A PROCEDURE APPLIES TO ONLY A CERTAIN SERIES OF THE AIRCRAFT MODEL THE AIRCRAFT SERIAL EFFECTIVITY WILL BE DESIGNATED ...

Page 27: ...I 15 94 _1 1 _ I 0 r 7 37 82 6 DMEDRL L 1 1 1 74 I tA I 3uc U 19 221 I I I iO i Fi ure 1 1 L imensions of Aircraft r 2 ...

Page 28: ...ained from non BEECHCRAFT approved sources or parts components or structural assemblies the service history of which is unknown or cannot be authenticated may have been subjected to unacceptable stresses or temperatures or have other hidden damage not discernible through routine visual or usual nondestructive testing techniques This may render the part component or structnral assembly even though ...

Page 29: ...e 13 0 quarts Gage reading 4 8 to 10 5 quarts usable see Item 2 Consumable One Engine at 2200 rpm Materials Chart 4 9 in Hg Two Engines at 2200 rpm Gage reading 5 0 to 5 2 in Hg Propeller Hartzell HC F3YR 2 C7479 2R With Autopilot Deice Brush Block Replacement One Engine at 2200 rpm Gage reading 8 0 in Hg Goodrich replace brushes when 15 32 inch maxi tvo Engines at 2200 rpm Gage reading 8 4 mum di...

Page 30: ... psig Pushrod to bell crank 30 60 in Ibs Main Gear Tires 6 50 Bellcrank to structure 50 100 in Ibs x 8 8 ply 80 5 psig Aft Fuselage Controls Nose Gear Tire 5 00 Pushrod to bell crank 30 60 in Ibs x 5 6 ply 47 t 50 psig Bell crank to structure 40 60 in Ibs Oil Filter 50 hours Rudder bell crank Oil Change 75 to 100 hourslor on linkage 50 70 in Ibs condition Wing Mounting Induction Air Filter Leading...

Page 31: ...dicular to an adapter must be added to the length of the flex or T handle imaginary line extending from the center of the bolt through wrench and a value calculated for that particular the spring scale attaching point combination The following is a typical example in finding a desired value To calculate the force in pounds scale reading required to obtain the specified torque divide the torque in ...

Page 32: ...000 1 1 8 12 5000 7000 3000 4200 15000 9000 1 1 4 12 9000 11000 5400 6600 25000 15000 NOTE The above values apply to Class 3 threads cadmium plated and nonlubricated TORQUING COARSE THREAD SERIES BOLTS LOADED IN SMEAR TORQUE LIMITS RECOMMENDED MAXIMUM ALLX WABLE INCH POUNDS TORQUE INCH POUNDS SIZE AN365 and AN310 AN364 and AN320 AN365 and AN310 AN364 and AN320 Nuts Nuts Nuts Nuts Column 1 Column 2...

Page 33: ... WING BOLT WRENCH or I j7 B FLAP TRAVEL GAGE TS1222 5 TS1171 1 UPPER AFI WING NUT TORQUE WRENCH ADAPTER 96 524000 810 2 50 590013 50 590014 LOWER FORWARD WING NUT TORQUE WRENCH ADAPTER 402 TS1222 3 LOWER FORWARD WING BOLT WRENCH TK1817 922 4 LOWER AFT WING BOLT WRENCH TS1171 2 LOWER AFT WING NUT TORQUE WRENCH ADAPTER 401 403 404 ADAPTERS FOR SERVICE JACK 932 7135 000001 96 524000 810 RUDDER TRAVEL...

Page 34: ...vco Lycoming Division Williamsport Pen nsylvania Parts Catalog PC 120 Avco Lycoming Division Williamsport Pennsylvania FUEL INJECTION Operation and Service Manual Form 15 338B Bendix Corporation South Bend Indiana PROPELLER Overhaul Instructions 117 for Hartzell Propeller Hartzell Propeller Inc Piqua Ohio tmer s Manual 115 for Hartzell HC FSYR 2 C 7479 2RPropeller Hartzell Propeller Inc Piqua Ohio...

Page 35: ...ce California 90505 B 5 Flight Control System Ground Xnd Flight Check Procedures Manual 3952 Brittain Industries Torrance California 90505 B 7 Flight Procedures Manual 3959 Brittain Industies Torrance California 90505 B 7 Maintenance iManual 3960 Brittain Industries Torrance California 90505 1 8A ...

Page 36: ...ction and Tesdng or Prooeller Deicer System Report 68 04 708 B F Goodrich Company ud on Ohio SURFACE DE1CER Maintenance Instructions PublicationNumber 63 200 B F Goodrich Company A on Ohio HEATER VENT BLOWER Overhaul Instructions for Vane l_dal Blower Md861H 1A with Motor iLI2916V Dynamic Air En ineering Inc Santa Xna California HEATER Maintenance Instructions for Janitrol F83A28 ilircraft Heater ...

Page 37: ...2 379A Operation Manual 130333B Adaptive Maintenance Manual 92 30103B Overhaul Instructions for BG274B2 CI C2 Computer 92 30105 Overhaul Instructions for CG136A1 Heading Selector 92 30106B Overhaul Instructions for IG11SA1 MG113A2 1LIG113A3 MG113A4 Actuator and SG28A1 SG28A3 Pressure Switch 92 30107A1 Overhaul Instructions for PC S1X1 Altitude Control 92 30229 Overhaul Instructions for GC205A3 GG2...

Page 38: ...ed to lift the aircraft off the The aircraft may be hoisted for maintenance or parts ground Each jack pad is identified and located on replacement as follows the under side of the fuselage One jack pad is lo cated on each lower wing to fuselage attachment a Install one 95 590017 hoisting sling adapter on fitting along the front spar The rear jack pad is lo each forward wing attach bolt cated under...

Page 39: ...MOVED INSTALL 95 590017 ADAPTER HERE WITH WING INSTALLED 95 590016 23 SPACER WING ATTACH BOLT SPAR CARRY 95 590017 ADAPTER THRU FITTING SPAF CARRY THRIT FITTING WING SPAR FITTING 9 5 59 0017 1 ADAPTER WING ATTACH BOLT VIEW B _J VIEW A Figure 2 1 Hoisting the Aircraft 2 2 ...

Page 40: ...ment The reservoir should be check ed regularly and filled to within 1 1 2 inches of the The aircraft is equipped with a relay and diodes that top and a visible fluid level maintained on the dip protect the aircraft electrical system against damage stick at all times by adding hydraulic fluid Item 13 from an external power source with reversed polarity Consumable Materials Chart Observe the follow...

Page 41: ...An optional 16 gallon fuel cell may be located in the ah section of the nacelle Both standard cells located in each wing are interconnected and 01L SYSTEM filled through a common opening in the upper wing surface The opening is covered by a Rush type cap The optional Th gines are equipped with a wet sump pressure type oil nacelle tank is filled through an opening on the nacelle and is system Each ...

Page 42: ...curs first check the electrolyte engine Torque retainer bolt to 30 to 35 foot pounds level and clean the battery and filler vent plugs c Safety retainer bolt b Any time the battery is subjected to more than 32 volts for as long as two minutes the battery must be completely serviced Clean the battery charge it INDUCTION AIR FILTER and adjust the electrolyte level The induction air filter should be ...

Page 43: ...sparks away or lukewarm never hot water and a mild nondeter when outlets are in use Open and close all Pent soap Any rubbing of the painted surface should oxygen valves slowly Make sure the oxygen be done gently and held to a minimum tb avoid crack shut off valve is in the closed position In ing the paint film spect the filler connection for cleanliness be fore attaching it to the filler valve Kee...

Page 44: ...ton to the clevis end of the barrel See Section 10 of this manual for servicing instruc f Refill the displaced fluid and replace the end tions seal scraper ring and internal snap ring SHIMMY DAMPENER g Fill the piston rod with fluid To check the fluid level in the shimmy dampener in k Reinstall the floating piston spring washer and sert a wire of appro imately 1 18 inch diameter cotter pin Spread ...

Page 45: ...gun fitting on one zerk of each blade and filling until the grease is visible Internal lighting of the instruments provides additional from the zerk on the opposite side of the blade illumination across each instrument A light tray mounted on the top side of the bezel of each instrument d Clean excess grease from the propeller and re holds two bulbs wired in parallel If the light bulbs install the...

Page 46: ...nt panel and secure in place with the attaching screws a Install the new light tray and secure in place with the two attaching screws c Secure the instrument panel in place b Install the instrument if removed in the instru 2 8A ...

Page 47: ...g Co Whippany N J Brake Deicer Anti Size Compound Federal Specification Armite Product Static and Pitot White Lead Base TT A 580 JAN A 669 Armite Laboratories Los Angeles Calif Oxygen Thread Compound MIL T 5542 No 15 Rector Well Anti Seize and Sealing Equipment Co Oxygen Systems Houston Texas D 217 Acheson Colloies Co Port Huron Michigan Key Abso Lute Type St Louis nlinois Oxygen High Ribbon Dope ...

Page 48: ...ining Co 600 Fifth Franklin Oil and Gas Avenue New York Co Bedford Ohio N Y Kendex 7038 Kendall 8 Lubricating Grease MIL G 7711 Regal AFB 2 Texaco Refining Co Brad General Purpose Inc 135 East 42nd ford Pa Street New York 17 N Y Aeroshell Grease t6 4 Lubricating Oil MIL 0 6081 Gunlite Turbojet Oil Shell Oil Co 50 West 1010 Gulf Oil Corp 50th Street New York Pittsburg Pa 20 N Y Aeroshell 3 1286 224...

Page 49: ...on Consultants New York N Y Inc Philadelphia Pa FED 3565 Standard Oil Co of California 32 Penetrating Oil Mouse Milk Worldwide Aircraft 225 Bush Street San Filters Corp 1685 Francisco 20 Calif Abram Ct San Leandro California 14 Oxygen System Leak MIL L 25567 94577 Testing Compound 33 Adhesive EC2216 Minnesota Mining Mfg Co 15 Solvent PD680 St Paul Minnesota 16 Lubricating Oil SAE 10 jj Corrosion P...

Page 50: ...teering mechanism 5 Mn C 7711 100 hrs DETAIL G DETAIL 1 Rudder trim tab actuator 1 MIL G 23827 AR i Heater iris valve 1 MIL M 7866 AR 2 Rudder trim tab hinge 1 MIL G 6711 100 hrs NOTES DETAIL H i Elevator trim tab actuator 1 MTL G 23827 AR Precaution should be taken when using MIL G 23827 and MIL G 7711 since these 2 Elevator trim tab hinge 1 MIL G 6 711 100 hrs greases contain chemicals harmful t...

Page 51: ...TAIL D DETAIL E DETAIL F i ra 71 DETAIL Q DETAIL G DETAIL H LUBRICATION DIAGR dk M 111 A BCD E F 3 DETAIL P T DETAIL I DETAIL J a P O N Valk M L K DETAIL O DETAIL N DETAIL M DETAIL L DETAIL K I B Figure 2 4 Lubrication Diagram 2 13 ...

Page 52: ...ry with air pressure Every 100 hrs Heater Fuel Strainers L H side of nose wheel well 1 Clean with solvent and blow dry with air pressure Eve ry 100 hrs Engine Oil Screens Lower rear of engine 2 Clean with solvent and blow dry with air pressure Every 50 hrs Suction Relief Valve Screens Forward of instrument panel 2 Clean with solvent and blow dry with air pressure Every 100 hrs Air Pump Inlet Filte...

Page 53: ... Co St Paul Minnesota 3 Permatex Sealer No 2 Permatex Co Inc Kansas City Kansas 4 Presstite Sealer No 576 Presstite Engineering Co St Louis Mo 5 Silastic Sealer No 140 Dow Coming Midland Michigan 6 EP711 Coast Proseal and Manufacturing Co Los Angeles California 7 EC 1615 Minnesota Mining and Manufacturing Co St Paul Minnesota ...

Page 54: ...i 9 875 i ML FRONT SPAR IsTAa WL 100 000 ML REAR SPAR i FOSELAGE STA 273 750 VERrICAL STABILIZER IL36 150 jll3 900 80 260 36 900 6 200 60 340 7 59 000 HORIZONTAL STABILIZER 66 000 1 11 55 500 70 3401 II 11 53 000 47 000 73 000 39 375 228 000 205 500 175 831 80 340 191 000 162 563 94 09 34 37536 030 148 875 83 547 35 301 103 641 1 109 305 i I 113 1721 i FS 58 125 jjj II i iii FRONT SPAR FS 82 9601 ...

Page 55: ...mation for making skin repairs INDEX NO MATERIAL DESCRIPTION 1 025 Clad 2024 13 2 032 Clad 2024 T3 3 020 Clad 6061 T6 4 020 Clad 2024 T3 S 020 Clad 2024 14 6 016 Clad a024 3 7 090 Royalite 8 032 Clad 2024 T4 9 020 3da Xl oy AZ31B H24 10 060 Clad 2024 T3 11 040 Xlum Xlloy 6061 T6 12 050 Xlum Allov 6061 T6 13 020 Alum llo 6061 T6 14 o 181Glass Cloth 4 or 3 ply to obtain 050 wall thick ness 3 2 ...

Page 56: ...12 t I I I U I I 1 Y 12 1 4 4 1 10 7 11 9 2 BOTTOM 2 9 CI a 2 11 II 12 C III 1 2 3 14 I i9 i 2 13 2 9 2 2 2 2 t 2 J a O a 7 I 4 a 11 7 14 3 15 4 8 8 2 1 1 1 i 2 2 1 2 1 4 8 2 Figure 3 2 Fuselage and Empennage Skin Plating 3 3 ...

Page 57: ...furnished as ge erzl inform ion for mak in skin reairs INDEX NO MATERIAL DESCRIPTION 025 Clad 202 T3 2 032 Clad 2026 3 3 020 Clad 5024 T3 020 um Uloy 202 T42 5 040 Clad 2026 T3 016 Clad 6061 T6 7 032 Clad 202a T1 8 016 Clad 202s T3 9 03 0 Clad 6061 T6 10 025 11um LUlov 6061 T5 11 No 181GlaEs Cio n 3 Ply 12 032 Xlufi Allov 6061 0 ...

Page 58: ... T n 3 5 6 3 k i 6 111 I k k 3 2 6 RIGHT WTNG TOP VIEW LEFT WING TOP VTEW 1 2 3 s 12 Ip 1 2 2 1 Ip 112 5 7 2 1 3 3 3 3 8 7 3 3 7 2 6 1 cf c 1 3 i RIGHT WMG BOTTOM VIEW i r I LETT WDI G BOTTOM VIEW Figure 3 3 Wing Skin Plating 3 5 ...

Page 59: ...es 11 Ringe bolts for nose wheel strut 1 Horizontal stabilizer mounting bolts 12 Rudder tab actuator 5 Heater ignition iris valve and blower assembly 13 Nose baggage door 6 Tailcone 14 Afl baggage compartment 7 Elevator bellcrank elevator down spring 15 Jack attach point and turnbuckles 16 Nose gear retract idler arm 8 Cable inspection 17 Rudder bellcrank 3 6 ...

Page 60: ...Zi ii2IO 1 i J ii c C aj 6 1 a Is s is 6 O C1I iI 1 ii 51 Fi ure 3 4 Fusela e Access Ooenings 3 7 ...

Page 61: ... dliary fuel cell transmitter Installed if nacel 23 Flap hinge 501t access le fuel cell is not installed 26 Xileron cable inspection 8 leron bellcrank 25 Xileron cable pulley 9 Nacelle fuel cell vent plumbing 26 Aileron tab actuator and pulley 10 Nacelle fuel cell filler neck 27 Wing tip access ii Nacelle fuel cell and vent line plumbing 28 Wing tip spar fitting 12 Nacelle fuel cell plumbing trans...

Page 62: ...14 2 1 4 ill Z r 1 7 8 8 7 9 10 11 12 20 10 13 9 11 10 12 LI FT ING IilGII T S ING UDPE R Ci_ n 21 30 31 2 22 30 21 31 29 j 29 33 71 28 27 33 C 32 25 4 26 23 24 25 32 23 20 13 14 13 I rt lr l WING I OW 11 I i L I F I W N I OWEII FiG e 3 5 Access Ol ciiii s 3 9 ...

Page 63: ...ib and the fuselage Figure 3 6 a Drain and purge all fuel cells WARNING b Remove the wing mounting bolt access plates from the The two air conditioner lines between the right top and bottom of the wing wing root rib and the fuselage are high pressure lines Before disconnecting the two lines loosen c Place the aircraft on a three point jack to prevent an the fitting just enough to bleed off the pre...

Page 64: ...ning reused See Chart 3 1 three nuts b Coat the fitting bolt bores and bearing faces bolts h Torque the nuts in the following order upper forward washers and nuts with MIL C 16173 Grade II corrosion upper aft lower forward and lower aft Figure 3 6A 3 6B preventive compound Item 34 Consumable Material 3 6C and 3 6D When a torque wrench adapter is used the Chart length of the adapter must be added t...

Page 65: ...6L WASHER MS20365 524CNUT NAS 1305 21 FUSELAGE SMEAR TlE SUPPORT 60 100012 BOLT WING SMEAR TIE SLIDE 60 100011 AN960D916L WASHER BUSHING TORQUE TO 100 TO 140 INCH POUNDS 56TC 31 22 O Figure 3 6 Leading Edge Attach Point Bolt Installation 3 12 83 ...

Page 66: ...ORES AND EXPOSED BOLT THREADS WITH MIL C 16173 GRADE 2 CORROSION PREVENTIVE COMPOUND CHECK WASHER FOR A SMOOTH CONTINUOUS OUTER RADIUS WASHERS MAY 88 USED AS REQUIRED BETWEEN THE NUT AND 95 110025 1 WASHER TO PROVIDE A PROPER BOLT GRIP ADJUSTMENT NOTE Concunent with the scheduled torque ched inspect the upper wing attach fittings to assure that the drain hdes are clear O REFER TO CHART 3 1 FOR THE...

Page 67: ...ED BOLT THREADS WITH MIL C 16173 GRADE 2 CORROSION PREVENTIVE COMPOUND CHECK WASHER FOR A SMOOTH CONTINUOUS OUTER RADIUS NAS143 10 WASHERS MAY BE USED AS REQUIRED BETWEEN THE NUT AND 95 110025 3 WASHER TO PROVIDE A PROPER BOLT GRIP ADJUSTMENT NOTE I REFER TO CHART 3 1 FOR THE WING BOLT WRENCHES AND TORQUE ADAPTERS USED Concunent with the scheduled torque WITH THIS WING BOLT AND NUT check inspect t...

Page 68: ... WING FITTING WET BOLT TORQUE 2880 TO 3000 INCH POUNDS COAT THE COMPLETE BOLT NUT WASHER WING FITTING BOLT BORES AND EXPOSED THREADS WITH MIL C 16173 GRADE 2 CORROSION PREVENTIVE COMPOUND CHECK WASHER FOR A SMOOTH CONTINUOUS OUTER RADIUS 56TC 31 35 Figure 3 6C Lower Forward Wing Bolt Installation 83 3 12C ...

Page 69: ...T TORQUE 2480 10 2600 INCH POUNDS COAT THE COMPLETE BOLT NUT WASHERS WING FITTING BOLT BORES AND EXPOSED BOLT THREADS WITH MiL C 16173 GRADE 2 CORROSION PREVENTIVE COMPOUND CHECK WASHER FOR A SMOOTH CONTINUOUS OUTER RADIUS MS20002 12 WASHERS MAY BE USED AS REQUIRED BETWEEN THE NUT AND 95 110025 1 WASHER TO PROVIDE A PROPER BOLT GRIP ADJUSTMENT 56TC 3 24 Figure 3 6D Lower Aft Wing Bolt Installation...

Page 70: ... 3 EB144 50 590014 LOWER AFT MS31150 12 TK1817 922 4 1213126 TS1171 2 02411CV WING SMEAR FITTING LOOSEN THIS NUT UNTIL THE BUSHING CAN BE DISENGAGED FROM THE HOLES IN THE WING SMEAR FITTING SCRIBE MARK BUSHING FUSELAGE SMEAR TIE SUPPORT BUSHING NOTE SCRIBE MARK THE MARK SCRIBED ON THE SIDE OF EACH BUSHING AT THE TIME DETAIL A OF MANUFACTURE MUST BE ALIGNED PRIOR TO RETORQUING LOOKING DOWN AT LEADI...

Page 71: ... Section 2 forjacking instructions Place WARNING a suitable cradle under each wing and a tail stand under the aft portion of the fuselage The wing bolts and nuts installed in all 56TC Turbo Barons must be removed and inspected If c Loosen the nuts on the lower wing attach bolts and the bolts and nuts prove to be free of all damage remove the bolts and nuts from the upper wing attach fittings they ...

Page 72: ...anical damage must be is not encountered and the wing has not shifted replaced replacement of the soft aluminum washers between the upper wing attach fittings is not e Using the magnetic particle inspection process described required in this chapter check each bolt for circumferential crack indications and each nut for longitudinal crack indications If WARNING the bolt and nut prove to be free of ...

Page 73: ... type equipment with either visible or fluorescent CAUTION magnetic particles suspended in a petroleum base vehicle normaiiy kerosene Since magnetic panicle indications are Ensure that the wing bolt wrenches do not best obtained when the discontinuity lies in a direction bottom out on the fittings when torquing the nut transverse to the magnetic field the following procedures are This could result...

Page 74: ...s positioned between the heads of the wet Inspection of the upper and lower spar caps should be horizontal equipment The magnetic particle suspension is accomplished in the following manner flowed on the nut and the appropriate current is applied through the central conductor to achieve adequate field a Examine the forward and aft sides of the spar cap where it strength Using the described procedu...

Page 75: ...DICATORS ARE ALL SHOWN IN ONE AREA AND ARE EXAGGERATED FOR CLARITY ANY ONE OR ANY COMBINATION OF THE INDICATORS ARE CAUSE FOR FURTHER INVESTIGATION 8OX SECTION SKIN CRACKS SPAR CAP RAISED AREAS s o O p o o LEADING EDGE SKIN THIS RIVET PATTERN WILL VARY N DIFFERENT IODELS PAINT BLISTER C9aiCOlB3023 C Figure 3 66 Outboard Wing Main Spar Cap Visual Inspection 3 1 2J 65 ...

Page 76: ...ion b Thoroughly clean the forward and aft frames and determination of any corrective action that may be required wehs of the front spar carry through structure in the areas shown in Figure 3 61 with Naphtha or equivalent cleaning agent 20 Consumable Materials Chart Sec WING FORWARD SPAR tion 2 CARRY THROUGH STRUCTURE INSPECTION WITHOUT REPAIR K17 c Perform a visual inspection of the cleaned areas...

Page 77: ...ust be stop drilled with a 30 drill bit at the through structure in the areas shown in Figure 3 61 crack ends The area must be repaired within the next with Naphtha or equivalent cleaning agent 20 Con 100 flight hours with the applicable kit in Chart 3 7 sumable Materials Chart Section 2 c A crack exceeding 4 0 inches in iength must be Perform a visual inspection of the cleaned areas repaired prio...

Page 78: ...racks perthe appropriate kitlisted in CRACKS Chart 3 7 if the limitations in the BEND RADIUS A combination of BEND RADIUS and WEB FACE CRACK and WEB FACE CRACK procedures are CRACKS are acceptable without repair However if exceeded there are any cracks in both the forward and the aft c Reinstall the carry through cover and the pilot s web face or in the bend radius on the same side of and copilot ...

Page 79: ...YPICAL LOCATIONS AROUND HUCKeOLTS eRACK O INSPECTION BETWEEN HUCKBOLTS LOCATIONS AREA AND ALONG THE RADIUS OF THE CARRY THROUGH WEB IN THE INSPEC TION AREAS O INSPECTION aa aIsI80o o 80ooooI AREA a II o i a a a O O Oo o O O O g a olS i Oo E QO O 8 o 8 o Q aa QQ 8 a I ba a I bb TYPICAL O gOOba a a a0a LOCATIONS a ab odea ObdddOd CRACK a AREAINSPECTION aa as BQ c9aiC0382037C FORWARD WEB Figure 3 61 ...

Page 80: ...ce b Remove the seat back support rod from the c Replace the seat stop on the aft end of the out board track mounting brackets and fold the seat back forward c Remove the attaching bolts and seat CENTER SEAT REMOVAL a Release the fore and aft adjustment lock and FIFTH AND SIXTH SEAT INSTALLATION move the seat forward against the stop a Postion the seat and secure in place with the b Remove the sea...

Page 81: ...er upholstery _oanel terminal to properly seal the door e Remove the phillips screws from each hinge If the door does not open freely the main door latch cover see Figure 3 7 may not be retracting enough This can be corrected by removing the upholstery panel below the door win f With the door open insert a screw driver between dow and shortening the length of the connecting tube the door stop and ...

Page 82: ...ter duct and secure in place a Clean the sealer from the canopy section where with the attaching screws the old windshield was removed usi toluol Item 22 Consumable Chart k Install the trim strips b Trim the tooling tabs from the windshield place i Install the glare shield and outside air temDer the windshield in position and mark the areas where ature gage material must be removed from the windsh...

Page 83: ...ition and cleco in place using the pilot holes provided d Place the window in position and cleco in place using the two pilot holes on the at t side of the window e Back drill the window frame using the e risting frame holes in the canopy section as a guide f Remove the window burr all holes and apply NOTE sealer Item i Sealing Charr to an area mately 1 2 inch wide on the canopy section where the ...

Page 84: ...g bottom of the specifications 1ML R 7575 and iLIIL P 015 window b Remove the royalite molding around the window c Remove the top bottom and forward retaining I NnRnlNcl angles by removing the attaching screws it Remove the window In oreoari resin never mix DDM Peroxide an Cobalt together as this will result in a AFT WINDOW INSTALLATION sDon aneous fire lways add one catalytic agent to the resin a...

Page 85: ...PORARY REVISIONS REVISION DATE DATE REASON PAGE NUMBER INSERTED REMOVED REMOVED NUMBER 4 1 Dec 11 92 Nov 15 93 Temporary 4 18 Revision 4 2 4 2 Nov 15 93 4 1 8 4 3 OC 24 9 4 1 NOTE Insert this Record of Tempora y Revisions after the Section 4 divider tab Page 1 Nov 15 93 ...

Page 86: ...Rayi heon Aircraft BEECH TURBO BARON 56TC AND 6TC SHOP MANUAL THIS PAGE INTENTIONALLY LEFT BLANK Page 1 of 2 Temporary Revision No 4 3 Oct 24 97 ...

Page 87: ...cal position and slide the control column arm off the housing CONTROL COLUMN ARM INSTALLATION a Position the control arm in a vertical position Refer to Figure 4 1 Ensure that the slot in the lower spracket is approximately parallel to the sides of the am and the tumbuckfes between the long and short chains are oppo site each other neat the access opening b The ailerons MUST be in the neutral posi...

Page 88: ...of the flao A honzontal ir lsaiignment of plus or minus 3ilS inch Is allowed between trailing edges of the alieron and wing tip With the bell crank RIGGING THE CONTROL COLUMN C 1AIN oarailel to the wing rib set the alleron In neutral by adjusting Figure J i the ienath of the push pull tube Loosen he locknuts on both ends and turn the tut e to shonen or lenathen a With the control wheel in the neut...

Page 89: ...2 I I r YELLOW MARK ON I SPROCKET AND CHAIN I I I I y II I I ___Ir TURNBUCKLE j ACCESS OPENING YELLOW MARK ON SPROCKET AND CHAIN SLOT IN SPROCKET 36 155 2 Figure 4 1 Control Column B1 4 2 ...

Page 90: ... ri 6 J 1 3 3 13 P I i s 1 Wheel 2 Control Arm E 2 3 Sprocket 4 Position Pin 5 Chain 6 Column Tube 7 Fitting 9 Inner ColumnC3 8 Column Link 10 Torque Knee 11 Fitti 12 Sprocket 13 Xiieron Column Stop Figure 4 1A Control Column ...

Page 91: ...ON TRIM TAB ACTUATOR ASSEMBLY position Figure 4 3 2 Center the chain on the sprocket and tighten the NOTE cable Rig cable tension and adjust travel as noted on the Aileron Cable Tension Temperature Charr Lubricate ail moving parts with Item Il Consumable Materials Chart f Check trim tab travel adjust cable stops and safety rurnbuckles a Screw the nut 5 onto the screw 8 NOTE b Install bearing 4 on ...

Page 92: ...G DOWN UI 30 e i LEFT WING DOWN 1 20 F S 68 00 1 Ai eron_ RIGHT WING DOWN Y cc J 10 A ran T SVRFACETRAVEL AIL RON 200 1 above 200 f bcla AILERON TAB 100 1D above 100 f 10 below W S 23 881 L 30 so so 60 70 so 90 ioo Iio DETAIL A FWD Temperature O F 30 W 5 45 20 1 W S 66 Y rl H 4 2 10 W S Wing S t a t i o n F S Fuselage Station W S 94 094 o 40 50 60 70 80 90 ioo Iio NOTE Rig autopilot cablet ofter c...

Page 93: ... cables and remove the elevator a Detach the tail cone disconnect the tail ELEVATOR SKIN REPLACEMENT navigation light wire and remove the tail cone Should an elevator become damaged to a point where skin b Remove the tail section access doors on the left replacement is required it is possible to replace one or both hand side of the aft fuselage skins however it should be undertaken only by an expe...

Page 94: ...s to be obrained locally b Insrail the elevator in the holding fixture n Install the tab actuator rod i airing s Upper s m c Remove the forward our board elevator tip cover O ly d Remove the elevator ab o Position the new skin on d e elevator structure and cleco in place NOTE p River the skin to the elevator spar and ribs Nork Use drill bits of the appropriate size when re ing from Be center out t...

Page 95: ...all screws and attaching hardware re moved during disassembly NOTE z Paint the elevator The clamping device should be tightened just enough to hold the bonded area together aa Balance the elevator by the procedure located elsewhere in this section v Use a suitable clamping device to hold the tail ing edge of the skins together for drilling and riveting bb Reinstali the elevator on the aircraft C C...

Page 96: ...ELEV UP 20 veto Tob DETAIL A ELEV DOWN Eo a E evo or Tab NOSE DOWN t 10 1 SURFACE TRAVEL BEV OR 30 1 Up 1SC rl Down NOSE UP ELEV TA6 10D i Up 230 115 DDrr ELEV UP cl 40 50 60 70 80 90 100 110 1 11 30 ELEV Temperature OF 31 10 C L VP 20 Autop F S 118 50 NOSE DOWN g lo F S 112 000 30 40 50 60 70 80 90 100 110 Temperature OF DETAIL B NOTE Rig outapilat cables aher central system cables are rigged Fi ...

Page 97: ...evator Up stop to obtain 300 f 1 UP NOTE travel Elevators must be removed from the airplane and d Rig cable tension as noted on the Elevator Cable checked for static balance after accomplishing Tension Temperature Chart adjusting the cable so that the the repair procedures described in ELEVATOR elevator bell crank Down stop comes into contact before the TRIM TAB HORN REPAIR control column is in th...

Page 98: ...nside diameter cerher use care not o scueeta cut all of he adhesive until the achesive has cured ccmp eleiy 24 hrs 5 Using 3 cieul rag damoened with methyl ethyl keytone nem 21 Consumable Materials Chart or equivalent cJ Remove the existing rod end from the tab oush rod clean the wle in the tao hom he area around the hcle and a Ssembly at he ao horn end and eoia it w Br a F FS PIN busning c6 dlCQ2...

Page 99: ...access panel near the leading edge of edge of the hon zontal stabilizer the horizontal stabilizer to gain access to the elevator trim tab h Install the access panel located near the trailing actuator sprocket edge of the horizontal stabilizer e Remove the elevator as outlined in Section 4 of this i Install the access panel on the left hand side of the Shop Manual under the heading ELEVATOR REMOVAL...

Page 100: ...screw 4 that rotate clockwise when adjusting bushing 10 screwed into the nut assembly 2 The trim tab actuator to be installed on the right hand horizon Clean all parts in Item 15 Consumable Materials Chart and tal stabilizer MUST have threads on the actuator inspect for cracks corrosion and distortion Replace screw 4 that rotate counterclockwise when bushings and any parts showing evidence of dete...

Page 101: ...r screw end of the housing a Disconnectthe actuatorwire harness at the discon nect splices c Using a spanner wrench install the adjusting b Place a wood or sheet metal shim between the bushing 10 cable drum and the cable guard so the cable will not unwind c Remove the fairlead mounted on the bulkhead aft of d install and secure the check nut 91 the actuator d Disconnect the actuator cable at the t...

Page 102: ...ue of the clutch is less than 30 inch clutch housing pounds burn in the clutch as follows e Remove the clutch from the clutch housing 1 Find a metal plate of sufficient thickness for rigidity and large enough to fit in a vise with the actuator MOTOR assembly attached Anchor the plate in a vise and drill three holes in the plate to match the actuator mounting holes Bolt CLUTCH HOUSING the actuator ...

Page 103: ...les provided in d Remove the pivot bolt attaching the rudder torque the pilots rudder pedals which will off set the left tube actuating arm to its mounting bracket Remove rudder pedal 38 to 45 inch aft of the right rudder the beilcrank push rod bolt and bonding cable pedal e Remove the rudder hinge bolts and remove the c Rig the rudder neutral with the pilots rudder ped rudder als pinned in the of...

Page 104: ...ust tab stops check travel and safety turnbuck les steel block 1 2 x 1 x 2 inches and two 3 8 x 2 1 8 inch long n g pins See figure 4 6 The rig pins are located parallel and NOTE forward on the block one on each side and welded The rig pins should be spaced as noted in the illustration After rigging the rudder tab system check the tab control and the surfacefor correct movement d Set rudder bell c...

Page 105: ...measurements given in the Table of Rudder and cal stabilizer Full the free ends of the material in firmly against Rudder Tab Travel are for a stwght line distance between the the skin contour to fair the rudder in the 00 position and mark position of the surface at 0 and its position at maximum the point on the tail cone corresponding to the bottom trailing deflection edge corner of the rudder 4 8...

Page 106: ...EFT TEMPERATURE CABLE TENSION GRAPH RUD LEFT 40 so RUD RIGHT __ 30 40 1 r i a a i c u mY puaa C DETAIL A I r sy I 1 Avt _i 20 H 4 30 Cob e_Minim _ILL i i RUD TAB RIGHT i 20 RUDDER PEDAL io c Rudde T e _ RIGGING HOLES 7ob 7 T i _ SURFACE TRAVEL _i _ to Rudd r I CL i 1 Right 33C 1 _OC or 12 55 mar to 1221 min RUD TAB LEFT 30 40 50 60 70 80 90 100 110 i L h 25E 1C 1C or 9 60 mar te 8 86 min FWD NOTE ...

Page 107: ...e and provide housing 16 and pull the back of the housing off of the smooth operation through its full travel sprocket assembly shaft 17 e Remove the roil pins 10 and remove the d Install actuator screw 3 in the housing 15 sprocket assembly 7 f Remove the bearings 8 and bushings 19 NOTE Clean all parts with Item 15 Consumable Materials Chart Check the end play between the screw 3 and and inspect f...

Page 108: ...eck Vut9 10Br 3 Actuator ScrewXI 3 Actuator Rod End I Retaining lut 5 Housing le k 6 Sprocket Assembly Housing 7 Sprocket Assembly 10 8 Bearing 9 Bushing 10 RollPin 90 1631 Figure d 9 Rudder Tab Actuator 4 10A ...

Page 109: ...9 1 i Elevator 2 Vertical Stabilizer 3 Rudder 4 Horizontal Stabilizer 5 Seal 6 Bonding Cable 7 Elevator Hinge 8 Bearing 9 StaticWick 10 Elevator Torque Arm b i 10 3 d O 6 6 I 8 I Figure4 lO Empennage ...

Page 110: ...Position the vertical stabilizer on the fuselage d Connect the elevator tab actuator rods and install the bolts at the forward and rear ars Install the elevator center hinge bracket on the bottom e Rerig the trim tabs of the rear spar Torque the bolts to 160 190 inch pounds f Replace access doors b CoMect the rotating beacon wires and the tail navigation light wires Ii new stabilizers P N 96 62000...

Page 111: ...e re quired amount of nose heaviness 0 2 inch oounds 50 give the total amount of tail heavy balance that must be comDensated for Use this formula to determine the amount of weight to add Y X B Y Distance in inches from hinge center line to center line oI the balancing weight ZC The unlnown weight to be added S The total amount needed to give tail heavy balance Using 3 inches as an euample of the d...

Page 112: ...3 7 STEEL TUBE WITH PIG LEAD JIC ZrlUST BE HORIZONTALLY LEVEL Fi ure 4 11 Balancing The Aileron 4 13 ...

Page 113: ...e in inches from hinge center Line to point where spindle sugoorts elevator W Scale reading of platform scale in pounds S Wej ht of spindle tin pounds used to support trailing edge of elevator Remove the elevator horn cover and add or remove solder to bring the ele Jator balance within required Limits Coat the weight with a corrosion preventative material such as zinc chromate oriner to insulate t...

Page 114: ...JIG IUST BE HORIZONTALLY LEVEL 2 I I 9 ii o I Balanci The Elevator 4 15 ...

Page 115: ...nge center Line to point where rhe spindle suooorts the rudder W Scale reading of platform scale in Dounds S Weight of spindle tin pounds used to uowrt trailing edge of rudder Remove the rudder horn weight and add or remove solder to bring the rudder balance within required limits Coat the weight vith a corrosion Dreventative material such as zinc chromate primer to insulate the dissimilar metals ...

Page 116: ...32 9 i62 V I all W JIG MUST BE HORIZONT LLY LEVEL Figure a 13 Balancing The Rudder ...

Page 117: ...ill go and rotate the retainer 900 e Keep inboard pressure on the retainer and tighten both retainer set screws f Secure the flap drive cable to the mounting support by tightening the nuts Tighten the inboard nut to ensure that there is sufficient clearance between the outboard edge of the retainer and the cable housing to allow the retainer to rotate without coming into contact with the cable hou...

Page 118: ...switches are mounted on a bracket and installed on the outboard side of u4e inboard flaD track NOTE in the left wing panel The limit s vitches one lor up two for the approach tone is a backup position and one for down travel control the cravel of e flaps After the flap is completely rigged adjust the by breaking the circuit to the flap motor at the ex rubber bumper flap do n installed on the flap ...

Page 119: ...taching bolts and c Remove the screws which secure the cover 8 and the ground wire secured to one of the bolts and re gasket 7 to the gear housing move the flap motor d X small set screw 11 must be removed to allow p Reinstall the nan motor by reversing the above the counter shat t 10 to be drawn out of the gearbox removal procedure FLAP MOTOR GEARBOX OVERHAUL Figure 1 15 a Cut and remove aU saiet...

Page 120: ...Shaft and Housi 3 FlapXctuator O Limit Switches 2 FWP TRANSMITTER X ID INDICATOR rl O B 2 Indicator1 Transmitter 3 Flapi ctuator 2 To adjust loosen mounti bolts and move fore and afl or rotate Sli ahtly FLt P LIMIT SPT TCHES GY i u i Down Limit Switches 2 Up Limit Switches 3 Approach Position Switches Fi oure 4_ 1 I Flap System d 19 ...

Page 121: ...eal Collar 1S ThrustWasher Oil teal Washer 16 Counter Shaft Be3rinS 3 rmature Shaft Washer 17 Searingc up i S o or Housing End Plate 18 rhrustniashe 7 Gear Housing Gasket 19 trorm Wheel Clear 8 Cover Plate 20 Flap Concrol Shait 19 9 Sleeve Bearing 21 Soacer 18 i 10 CounterShaft 82 Washer 11 SeeScrew 23 Shim asher 12 Washer 2a Retaining Pin Fioure 4 15 FlaZ L lotor Gearho r 6 20 ...

Page 122: ... placement brushes Fill the gearbox with lubricating in the housing grease Item 11 Consumable Materials Chart Pour Item 7 Consumable Materials Chart into the hssembly is accomplished by reversing the above piston until it is about two inches from being full procedure Slide a bearing on the screw Start the screw in the piston and slide the piston into the housing install the FLAP ACTUATOR OVERHAUL ...

Page 123: ...control valves through 3 pressure manifold Pressure in the mani d Rudder Control fold is regulated by variable pressure regulators located in e nacelle of each engine constant i Release the rudder pedal adjusting levers and pressure is maintained by the re ulators for the place all pedals in the aft position combined operation of the autooilot and deicer systems Control valves are installed betwee...

Page 124: ...ilter 7 FLight Controller 8 Positive Shut Off S alve 9 Operboard Vent 10 E ine Driven Vacuum Pump 11 Solenoid Vahre i 12 Pressure Regulator Valve 13 erticai Gvro 14 Directional Gpro 15 Suction Relie T alve 3 5 4 2 8 6 j 12 ii 5 io 1 7 3 115 Figure 4 17 H 14 Autopilot TE1 thro h TG 51 4 23 ...

Page 125: ...Regulator 3 Comnuter 10 Filter 4 Aileron Servo ii Dry Air Pump 5 Positive Shut off Valve 12 Filter 6 Pressure Manifold 13 Rudder Servo i Plight Controller 14 Adjustabie essure Re ulator 1 2 3 d 3 7 3 9 10 11 12 L i3 i 9 io 12 11 Figure 6 18 H ld Autopilot TG S2 through TG 84 4 24 ...

Page 126: ...39r lT N jTO P HEL VALVE rO ENGINE a id AUTOPILOT WITH DEICER ITC j2 THROUGH TC 134 COILIPUTERXUTOPILOT hILERON j LilVO iI29B20N C O ELEVATOR SEIIVO rX TOPILOT RELAY O PITCH T RIi I t Y hCTC XTOR Y 14 AUTOPILOT WITH DEICER TG 32 THROUGH TG 4 RUDDER SERVO FILTER AUTOPILOT ON OFF VALVE TO ENGINE DRIVEN PUIMP AUTOPILOT VALVE AUTOPILOT I G932A22N PRESSURE IIXNIFOLD TO INSTR JILIZMT PANEL TO ENGINE DRI...

Page 127: ... I I CONTROL REWY VENT H2X20 LEFT ENCL E R TDDER SERVO H23C20 I II30A20N FUSELAGE 1i 14 AUTOPILOT X FD DEICER SYSTEM R B DEICE CONTROL VALVE DEICE CIRCUIT 1 H 29A2 O N H23B20 PU MP DUMP V LVE t XCTUATORPZTCH TRI yI VENT ELECTRICAL CIRCUIT FOR PNEUMATIC INTERCONNECT ELEVATOR SERVO Normally open Dump Valve a is energized TER 4 i j closed when normally closed Positive Shut oCf Valve is energ ized to ...

Page 128: ...e Ditch servos 4 altitude hold sensing uators The systems are completely non tumbling unit works in conjunction with Ditch control to sustain Yaw roll and turn detection is made by a tilted ro a given altitude EVT turn coordinator electrical vacuum torquing combination mounted in the instrument pane A dam G 8d and after pened miniature aircraft serves as the instrument indication arm Iny deviation...

Page 129: ...COMMAND SIGNAL DIP COMPENSATION RUDDER SERVOS AIRCRAFT GYXO DETECTS ROLL YAW BATTERY Q t i IL RUDDER SERVO CONTROL VALVE AIRCRAFT MASTER SW PILOT DISPLAY 2 POSITION ACTOPILOT MASTER PNEUMATIC PITCH CONTROL VACUUM I I AIR SPEED ELEVATOR SERVOS ATTITUDE HOLD ELEVATOR SERVO CONTROL VALVE AIRCRAFT STATIC LINE Fi ure 4 21 BEECHCRAFT New Matic B 5 Autopilot System 4 28 ...

Page 130: ... I i h iclC rc 91KK I r IAI91C D I i 9 I g r ZES 919 j L n U e YICITE I 1 S TiH AL i I I ir CY rC WI jl Il f 5i SCP i HO Si SIV Lllhrl POWu A i I i U I N I i oiD vnLv i PE3 j I IWTIPC I Ill L SLSL i i sLncali f P C i IrDc T uiu ce 9L E rc i cului r Y i z Zh 1cY33 l3 15 3 I i c blCK o ol 7 i kl GNETIC 3 i IF L I uO OLY L3 j j Sch 5 2 Y J ru T77 u GZSuw 3 i i TWISTiD m j I J O c D Il IIII b ii OJ Y ...

Page 131: ... TP 3 YELLOW NAV CENTERING HDG GRADIENT VOR GAIN if adiusted recheck t II c I adjustment C r a FACTORY ADJUSTS i a INTERCEPT i o a o I MAN CENTERING Q OUADRATURE ADJUST set at 450 Figure 1 23 BEECHCRAFT New Mar ic B 3 and B 7 Heading Lock Navigation Coupler System Adjusuneni Poinrs 4 30 ...

Page 132: ...ircraft primary cables b Check security of attacfi or e ucessive friction in aileron ment binding etc and and or rudder cables pulleys adjust as outlined in Section oellcranks or loose servo cables 4 c Leak in servo or servo lines c Check for leaks d Obstruction in servo lines d Check for foreign matter e Faulty turn coordinator gpro e Replace turn coordinator 3 Autopilot sluggish a Low system pre...

Page 133: ...rn a Faulty magnetic heading a Replace magnetic heading to and hold magnetic headings sensor sensor b Faulty heading selector b ReDlace heading selector resolver resolver c Faulty controller amplifier c Replace controller amplifier 12 Magnetic headings con a Heading sensor misaligned in a Check for proper installation sistently high or low aircraft b Heading azimuth dial shifted b Tighten screw an...

Page 134: ...a Wrong nav input signals a Check wiring mode decays to 0 voltage b Defective switching console b Repair or replace console if installed c Dirty input signal C c Check indicators volts 23 Voltage output in M L N a Polarization pins reversed a Reverse pins See Figure CXP TRK and XPP mode but on heading sensor plug LL 22 none in HDG mode 24 Nav indicator needle a One of the components is a Check for...

Page 135: ...l not respond to a Primary pressure not a Adjust as outlined in airspeed changes set properly Section 11 b Pitot pressure inadequate b Check pitot plumbing c Decay rate improperly c Adjust as required adjusted 10 System will not respond a Defective pitch altitude a Replace pitch altitude to up command adjustment amplifier amplifier b No EVT potentiometer output b Replace turn coordinator 11 System...

Page 136: ...aced inoperative b Leak in altitude sy ste m b Che ck fo r le ak s c Altitude lim ite r im p rope rly c Adjust as recluired adjusted 16 Ai re raft de s c ends o r a Se rvo co ntro 1 v alv e not a Apply po s itiv e 6 O volts as ce nd s continually whe n phased co rr e ctly m as to blue lead and sy ste m engaged ve rify no se up re spon se 4 35 ...

Page 137: ...position and clog the compensating valve and cause the brakes to check the sarking brake valve to make sure it is in lock the off position Loosen he locknut and setscrew and take up the slack in the actuator wire Tighten the Use either gravity flow or pressure bleeding to bleed setscrew and lock nut down on the brake acruator wire brakes Using either method the parking brake lever Xiter the proper...

Page 138: ...A TG 1 THROUGH TG 76 BRAA E MASTER CYLINDER DETAIL B x I J i L I Y c x 9 r i clII i O i v i i L i L I PARKING BRAKE VALVE DETAIL D LINING TG 77 AND AFTER TORQUE PLATE INSULATOR oIsc l PRESSURE PLc TE u PISTON SHIM u CY7 INDERS BRAKE ASSEMBLY DETAIL C 56FC2 PS Fi ure 6 I Brake System 5 2 ...

Page 139: ...c o pilot s b r ake sy ste m is bled by c i os ing the valve on the p re s s u re pot and pu m ping t he c o pilot s b rake pedal to c h ange the s hu tt ie valve position This R E M O V I N G T H E W H E EL A N D B R A K E A S S E M B L Y c aus e s hyd rau iic flu id to be route d through the c o pilot s sys tem and this sy stem should i e bled as was the pilot s sy ste m a P lac e the ai rplane ...

Page 140: ...e dise assembly can be removed if NOTE desired by removing the six bolts which join the wheel halves If the torque plate has been removed it should be reinstalled so that the guide pin holes are positioned aft and are centered above and NOTE below the horizontal centerline of the axle The brake linings and cylinder assembly can be removed without removing the wheel by d Install the back plate inne...

Page 141: ...2 to nuts and re move the mas te r cv inde rs c ome free The return s p ring 13 c ill fall free of the cylinde r with the piston re m oved e If new master cylinders are to be installed note the positions of the maste r c y linde r deg ree elbow C le an all parts inith s o ive nt Ite m 1 5 C onsumable fittings Mate rials Chart Checl all parts for cr ac Ls cor r os i on distortion and Ne ar Re u lac...

Page 142: ...inp 4 Washer g LockWashers 5 Ball 10 0 Ring h Check the valve seat for wear and distortion Lr necessary replace the valve seat Figure 5 4 Parking Brake Valve i Reassemble the valve in reverse or the above procedure TG 77 and after Check the parking brake valve for leaks by placi o Figure 5 4 4 1300 Ibs pressure in the valve through he elbow 2 Remove the pressure and place it in She nozzle 8 a Disc...

Page 143: ...erential between the above procedure the pitoc and static systems will actuate the pressure switch in the gear down circuit With both the micro switch and pressure switch closed the current flow 1ANDING GEAR SYSTEM through the solenoid will cause the landing gear posi Figure 3 5 tion switch to drop into the DOWiu position thus completing the gear down circuit IANDING GEAR SAFETY SYSTEM OPTIONAL If...

Page 144: ...bber tubing over the tion pitot he ad inle makin c e rrain that the c o nne c ti on is airtight i Plac e the i arte ry nl jte r s witch ON Tile landing e ar c i re u it nlay i e eithe r IN i r OU T C rimp the e nd oi he tubing and r o ii it up unt ii i the ai r s pee i indic at o r reqiste rs YO m ph The landing c P ac e the landiny ge a r s ale tp s y s ts m s V ite h in g e 3 r M i i s iart retr...

Page 145: ...tire landing gear is our of rig the internal stop The down limit witchadjustment is accomplished by bending the switch actuator arm tab so that it just breaks She circuit NOTE g Extend and retract the gear two or three times Over tightening the nut on the bolt that con to assure that the switches are correctly set Check nec s the retract rod to the shock strut can the hand crank each time to insur...

Page 146: ...ck the adjustment of the If unable to obtain adequate spring tension safety jaritch Refer to the landing gear safety switch check for worn bushings in the retract in iiau e 5 3 while adjusting the switch Wear in the bushings has the effect of ening the entire linkage causing the rod end i Remove the safety switch actuator rod 1 from spring to compress and stack leaving nothing the upper torque ee ...

Page 147: ... Nur Switcf Arm A 4 LocMng Screw B 5 Adju S ting Sc r ea 1 E 6 Ac tuaror Rod End ii f D 2 jc I 4 L h I e i C I d C IIII i C PI llll i t i iii e r I tf _ c Y O O MAIN GEAR UP LOCK CH ECKING M AIN G AR DOWN IOCK TENSION NOSE GEAR D O O R ADJ U STMENT 1 Uplock Rolie r S AFETY SWITCH ADJ USTMENT 2 Uplock Block Issued Figure 5 5 Landing Gear SJrstem Februa ry 1971 5 9 ...

Page 148: ...p Ilare completed 16 Close the inboard landing gear doors 9 Xdjusr the actuating rod end 6 to nLjo Irith 17 Remove the aircraft from the jacks and he mounting hole in the upper torque knee Ins all inr la e the LH main gear shock strut as described in the actuating rod on the toraue la ee LL iDDiG GEXR NOTE The switch shaft should remain as adjusted i MAIN GEAR REMOVAL AND INSTALLATION step 6 while...

Page 149: ... move the snap ring 23 and slide the u ppe r bolts 2 S 0 to 800 inch nounds Ope rate the gear to be ar ing 2 4 down to free the r e taine r r i ng i 2 5 S lide c he c k fo r p ro pe r rigging of uploc k and doors the re m aining c o mpo ne nts off the strut piston MAIN LANDING GEAR DISASSEMBLY INSPE CTION AND PARTS REPLACEMENT Figure 5 6 a Deflate the shock strut and re move the air valve as s e m...

Page 150: ... Knee 9 Upper Torque Knee Roll Pin 10 Upper Torque Knee Bushings 11 11 Torque Knee Bushings 12 xle Bushing 13 Lower Torque Knee Roll Pin 14 Lower Torque Knee Bushings P n 15 Lower Torque Knee 16 Shock Strut Piston 15 17 Strut Retainer and Scraper Ring 6 18 Lower Strut Bearing 19 O Ri 1 20 Back up Ring 2 13 21 OU Ring 22 ReboundTube 23 Snap Ring 24 Upper Strut Bearing 25 RetainerRing 26 Bolt 27 Bol...

Page 151: ...stall a cotter pin h Rebound tube 22 j Install the landing gear in the main gear wheel Minimum Length 4 540 well Measure the gap between the landing gear as sembly hinge points and the spar structure If the i UDoer Strut Bearing measurement is between 016 and 031 insert a i j Iaximum ID 1 968 016 thrust washer at each attach point If the measure OD 2 156 ment is between 032 and 047 insert a 032 th...

Page 152: ...ove the bolt attaching the up lock roller and ing the bearings have be n subjected to frequent de the V brace drag leg center hinge point greasing with solvent under pressure lubrication of the bearing may be necessary d Remove the up lock roller bearing from the bolt To lubricate the uplock roller bearings e Hold a linger over one end of the up lock roller a Place the aircraft on jacks s laA ...

Page 153: ...the drag leg at its fitting on the nose assernbl check the small O ring of the valve gear brace assembly assembly then look for defects in the valve assembl d Remove the hinge bolts securing the nose aear c Replace scored bushings bearings and pins br ace assembly to the fuselage structure and lower the nose gear au av from the aircraft d Replace self locking nuts which have lost their locking abi...

Page 154: ...Bearing 2 4 Retaine r Ring 9 S pac e r 2 5 Upper Bearing 5 6 10 Upper Torque Knee 26 Snap Ring 11 Upper Torque Knee Roil Pin 27 Rebound Tube 28 Lc we r Bear ing 1 2 Uppe r To rque Knee Bushings 1 3 Lowe r T or que Knee 11 o t Ring 14 Lower Torque Knee Roll Pin 30 Backup Rings 2 1 5 Lowe r T or que Knee Bushing s 3 i Lowe r Strut Retainer iII 1 16 Torque Knee Bushing 3 2 Shock Strut Pi ston i I 20 ...

Page 155: ...de the uDDe the bearings Back off the nut and re sighten with bearing 25 over the lower flange of the ret i ner nngers to remove any end play Using a wrench ring 24 and secure with the snap ring 26 tighten the nut to the next available keying position and instdll a cotter pin c Install the orifice metering rod assembly 22 in the strut housing 19 Install the 0 ring 20 in n Install the landing gear ...

Page 156: ...oating piston 12 Maintain tension on the floating piston while e Remove the aft floating piston 10 with a 6 32 drivinSa OUt the piston retaining pin 13 screw and remove the 0 ring 11 g Release the floating piston slowly and push it out I Insert a long 6 32 screw into the hole at the 5 15 ...

Page 157: ... Piston 3 Barrel End 13 Piston Retaining Pin 4 0 Ring lLt 11011 Ring 5 Snap Ring 15 Compression Spring 6 Piston Rod 16 Piston 7 Washer 17 O Ring 8 Cotter Pin 18 Barrel End 9 Compression Spring 19 Scraper Ring 10 Floating Piston 20 0 Ring 56TC 209 2 21 Barrel Figure 5 a Shimmy Dampener 5 16 ...

Page 158: ... e m ov al When re i ns t al ling the no se ge sr ac t u at o r retracr arm D n t he c Place the dampene r piston 16 on the piston rod ac tuator make ce r ain that the inde u r lark on the and inse rt the retaining pin Replace the 1 O ring s arm c o inc ide s with the index mark on th e actu at o r 17 on the dam pene r piston shaft d Inse rt the piston rod assembly into the barrel j Make ce rtain ...

Page 159: ...OR WORM SECTOR 1 1 SCREW 3 12 ACTUATOR HAND CRANK I 9 13 SPACER 14 0 RING SEAL 15 SCREW 16 HAND CRANK SHAFT HOUSING 17 RETAINER NUT 8 20 BEARING19 WORM GEAR SHAFT 4 re HALF RING 22 SEAL YL 1 21 LOCK NUT 23 BEARING 24 BEARING 25 SEAL 26 BEARING 27 SNAP RING 2 28 ACTUATOR RETRACT ARM 9 29 BEARING 30 GREASE FILL PLUG 31 BALL CHECK A56TC 216 I 32 SECTOR GEAR STOP ASSEMBLY Fi vure 5 9 Landing Gear Actu...

Page 160: ...edure and check rigging Clean allparts in solvent Item 15 Consumable Materials Chart removing the grease and oil Check all bearings for cracks and wear Check the teeth NOSE WHEEL STEERING MECHANISM of the sector gear for cracks and wear Replace Figure 5 10 parts as necessary Replace all seals at reassembly Seal the upper and lower housing joints using Perfect Seal Sealing Compound Item 5 Sealing C...

Page 161: ...uts securely In senrice tire carcasses grow slightly due to shock loads in landing Normally this growth is balanced e Turn the nose vheel o the e utreme right _Dlace by tread wear so there is no increase in tire dia the tape on the forward end of the piston and repeat meter steps b c and d Beech L ircraft CorDoration cannot recommend the use or recapped tires The tires may pass the re WHEEL AND TI...

Page 162: ...ls a Tripped circuit breaker a Reset circuit breaker to e c end b Down limit switches open b Check down limit switch With thegear retracred the down limit switch should be closed c Opencircuit c Run a continuity check on the down limit switch 7 Landingeearwill a Bad electrical connections a Run a continuity check from not retract or extend circuit breaker to switch Insoect the dynamic brake relay ...

Page 163: ...l ap side s vill checkout e u e nd in to the cowl by 25 inche s minimum when open Lf he cowl flap does no t m e e t the minimum roauired e tension into the C3Wl adjust the ac ruato r to obtain Warm up the engine at 1000 to 1500 rpm this o sition 1 minimum oi 0 6 inch clearance is reauired betwe en he ac tua to r and th e ac uato r sucpo rt and between he a c u ate r rod end lug and IOT E he cowl r...

Page 164: ...l re move the ignition harness cap or dis sure to iden iiv each wire iEor las and easy reins tail connect the s pa rk plug leads tion f Place a win stand under the opposite winy anti a Remove the upper and lower co vl iSee cowliny sup port under r he tail re moval proc edure this se crion Position the ent ine hoist and attach o the three c Remove the propeller See propeller removal iifting eyes on...

Page 165: ...0 rpm The oil pressure adjustment screw is located approx inor3lal idle setting To adjust turn the idle speed imately 3 inches direct v below the oil filter housing adjusting screw at the throttle lever stop until the To adjust turn the adjusting screw clock vise to in desired rpm is reached o e When the idle setting has been stabilized move the cockpit mixture control lever with a smooch b is set...

Page 166: ...ing Breaker point clearances b Land the airplane and shut the engine down for the magnetos are 016 006 for the retard points and 016 003 for the conventional points If c Position the throttle levers on the mark pre the ooints are burned or worn excessively do not try viously made Raise or lower the micro switches to redress the contact surfaces Install a complete until the cams click the switches ...

Page 167: ...l the c Remove the inspection plug on the left maoneto mark on the starter ring gear aligns with the hole in and turn the drive coupling in the direction of normal the starter housing If the timingis correct the rotation until the first marked tooth is aligned in the timing light should go OUT center of the inspection hole Without allowing the gear to turn from this position assemble the gasket an...

Page 168: ...thin the controller is where it is compressed and delivered to the engine held closed by spring tension and vacuum As the in The turhocharger reacts to engine exhaust variation duction manifold pressure increases the force on the to meet engine demands As the engine power in aneroid bellows causes the metering valve to open creases the flow of exhaust also increases result The controller is by a c...

Page 169: ...LTERNATE AIR DOOR I i r r II t II I THROTTLE CONTROL THRCYTTLF t tt i I xr 2 ENGINE COMPRESSOR I I t L ITURBINE r I 1 TAIL PIPE I i 1 I I ENGINE LBL WASTEGXTE WASTEGATE ACTUATOR OVERBOARD c F 9 INDUCTION AIR EXHAUST i Figure 6 d Tu rb0charger Schematic 6 5 ...

Page 170: ...INSERT A 025 INCH FEELER GAGE HERE BETWEEN LINKAGE AND FULL THROTTLE STOP PIN I I s FUEL INJECTOR LINI AGE I i I ii p I L C Q HIGH 800ST STOP PIN 60 258 2 Figure 6 1A Adjusting Throttle and Pressure Controller Linkage 6 6 ...

Page 171: ...ature reaches a mmlmum or 1850F Xs soon as oil appears at the end of the oil inlet line attach the line to the turbocharger and allow the ro c Set the oroDeller control lever in the high rpm tatinS assembly o spin position Slowi and smoothly apply the throttle until dl in Hg manifold pressure or the full throttle Operate the engine at a load and listen for sounds of position is reached metallic co...

Page 172: ... has not reached 41 in Hg 4 Retighten the lo cknut on the adjustingr s c r ew i Slowly and smoothly shut down the engine 2 Loosen the lock nut on the adjusting s cr ew 3 Turn the adjusting sc rew c ounter clockwise to in crease the manifold pr e s sur e One full turn equals approldmately 1 in Hg manifold Do not exe ee d 4 i 5 in Hg manifold pr e s su r e pressure 4 Retighten the o cknut on the adj...

Page 173: ...de at which the outterny edge and bore waste gate buttefly just fully closes The adjustment must be made with full hydraulic or air pressure d Reinstall the pin washer and cotter pin Tighten applied to the inlet port of the waste gate actuator the loc lnut against the turnbuckle with 80 to 100 in The full open butterfly stop adjustment located on Ibs torque the center of the actuator cover may be ...

Page 174: ...g Rein stall the wastegate exhaust stack and co nne ct the valve linkage TIT INDICATOR CALIBRATION Figure 6 i APPROVED OVERHAUL FACILITIES CAUTION The folio wing facilitie s are p re se ntly app rov ed fo r Dam age to the tu rboc ha rge r turbine blade s providing complete 9 e rv i ce fo r the exhaust tu rbo ex c e s s iv e turbine coking and ex c e s s iv e oil cha rge r and co ntr ol s m anufac ...

Page 175: ...ead Lubricants turbocharge r p e rf o rm anc e Refe r to the Tu r bo char ge r P e rfo rm anc e G raph This graph indicates the mini f Re pe at the above p ro c e du re on the LH e ng ine mum a c c eptabl e c ritical al titude he ai r c raft can achieve while maintaining 41 9 inch Hg manifold p re s su re T o check he tu rbo c ha rge r pe rfo rm an c e A L C A L C A L I B 8 A T IO N V N IT against...

Page 176: ...uc o i c I r I 1 23000 w pr i 5 I i I r in u L ____ Y __ t 22000 O C i L L_ __ r C e 210 00 r c I 1 i II I i I if c Lffe ff C c i I LL 20000 r t f LL C fL L I I LC l IC 1 c_ i 1 i 19000 O 70 60 50 40 30 20 10 0 10 20 30 40 OUTSIDE AIR TEMPERATURE 0 60 601 11 Figure 6 a T urbo cha rge r Performance Graph 6 9 ...

Page 177: ...in induction system c Tighten ail connections re place any defective parts d Uneven cylinder compression d Check condition of piston rings and valve seats e Faulty ignition system e Check ignition system 3 Low Power and Uneven a 1Miyiure too rich indicated a Readjustment of fuel injector is Running by slug ish e aine red exhaust indicated name Extreme cases indi cated by black smoke at ex haust b ...

Page 178: ... pr e s sur e valve relief valve c Dirty oil str aine r s c Remove and clean oil str aine r s d High oil te mper atur e s d See High Oi 1 T e mper atur e s e Defective pressure gage e Replace gage f Stopp e in oil pu mp intake f C heck line for obstruction passage 7 High OilTem per ature a Insufficient oil supply a Fill sump with oil of recom mended grade b Low grade of oil b Drain and fill sump w...

Page 179: ...heck for leakage d Leak in engine intake or d Tighten loose connections or exhaust manifold replace manifold gaskets as neces sary e Rotating assembly bearing e Remove and send to the nearest ap seizure proved overhaul station for repair f Restriction in return lines f Remove and clean Lines from actuator to waste te controller g Waste gate controller out of g Have waste gate controller ad adjustm...

Page 180: ...fold c Actuator to by pass valve c Correct cause of binding linkage binding d Clogged breather d Check breather for restriction to air flow OTE Smoke would be normal if engine has idled for a prolonged period j High Deck Pressure a Controller metering valve a Replace controller Compressor Dis Charge not opening Pressure b Exhaust by pass valve b Shut off valve in return line sticking closed inoper...

Page 181: ...ing gear the g asket be twe e n the gove mo r and engine c Pu 11 the propeller carefully from the mounting d T o in st all the ove rno r rever se the di s as se m studs Sly procedure T o rque gove mo r mounting nuts to 150 in Ibs ADJU STING THE PROPELLER GOVERNOR Figure 7 1 Do not damage thr e ads on artac hme nt s tud s and be c ar eiu 1 not to damage spinner T he propeller gove rno r c an Se ad ...

Page 182: ... the detent and observe the To adjust the feathering action pullthe control back rpm setting If the rpm varies from the specified low through the detent and observe the wint at which the rpm setting of 2200 rpm che low rpm setd must rpm setting begins to fall off sharpip then bring the b adjusted The low rpm adjustment is made on the propeller back to low rpm The point at which pro detent rod whic...

Page 183: ... the disassem bly procedure MINOR PROPELLER BLADE REPAIR Fiqure 7 3 Minor nicks dents and gouges may be dressed out by approved line _oersonnel Blend any nicks or go ps OIL L SE into the leading edge with smooth curves and gener ous radii as shown in figure 7 3 Reanodize reworked f area by he chromic acid process only t PROPELLER ACCUMULATOR REMOVAL Figure 7 4 a Check the propeller control lever f...

Page 184: ...ick or if fuel is less than six lower right side of the engine inches below the filler opening b install a fuel pressure gage 0 30 psi range and The fuel system on aircraft serials TC 69 and after a T fitting on the pressure side of the pump consists of nacelle box inboard and outboard leading edge fuel cells This increases the total fuel capacity c 13rP the safety wire and loosen the lock nut on ...

Page 185: ...E LL FLUSH ISYPHONI3P EXii 11111r i 4 1 I1II LI NACE LLE FUEL CELL DRAIN TCEL CELL FUEL CELL FLOAT VAL E VENT LINE LIIII EXTERNALVE TT 0 II I Q PRESSURE RELIEF II OHEATED VALVE FLUSH VE jT d FUE L TRANSMITTER STRAINER DR4II I AND IIII VENT 8 FILLER THERMAL RELIEF VALVE IIIII1 IIIII I FUEL FLOW Iry CHECK VALVE I f I FUEL SELECTOR VALVE TRA_h SMITTER USED UTHEN ru ACELLE TANK IS OMITTED Figure 8 1 F...

Page 186: ... I I i CROSS FEED 11 11 111111 E VALVEI FLAPPER VALVE I BOX SECTION CE LL FLUSI I Llf FUEL TrE r TT r L FUEL CELL DRAIN O FUEL CELL DRAIN NACELLE CE LL SYPIION PRESSURE RELIEF BfiDAK VAL rE C ENT LINE 11 IFLUSH EXTERNAL VENTI VENT HEATED L FUEL T EAI ITSMITTER STRAINER DRAIN AND IIIVENT FILLER THERMAL RELIEF VALVE NORMAL FUEL FLOW IICcl CHECK 1 AL E I i FUEL SELECTOR VALVE Fig 8 1A Fuel System Sch...

Page 187: ...ge the fuel system for the appro priate wing a To check the resistance of the transmitter Dlace an ohmeter between the transmitter cover and the b iMake sure the electrical power to the boost terminal stud pump is off b Refer to the chart below to determine the c Remove the boost pump access cover on the desired resistance readings underside of the wing d Disconnect the electrical leads to the pum...

Page 188: ...rom the OO position and hold the mounting bracket firmly in this position f ssembly is accomplished by the reversal of the d I sert the control cable 5 through the over above procedure Lubricate the fuel line threads with travel port and rotate the cable LH thread to anti seize compound See Table of Thread Lubricants e page two threads in the selector valve gear before installation e Rotate the se...

Page 189: ...er Plate Removed I Stop Screw 6 Slider 2 Overtravel Tube 7 Cable Rousing When installing flared fittings and hoses make sure the threads are lubricated properly see Figure 8 4 3 Selector Valve Gearbox 8 Cross Feed Port with anti seize compound tin accordance with the Ta d Selector Gear 9 Over Travel Port BLE OF THREAD LUBRICANTS When previously installed fittings are removed they should be wiped 3...

Page 190: ... I nacelle cavitv through the access hole 1 NOTE Tape edge of access hole to protect cell 4 from damage during removal i Nacelle Fuel Cell Access and Transmitter g Installation is accomplished by reversing the 2 Forward Access Plate above Drocedure Use Permates No 2 Item 3 3 lacelle Filler Neck TG 1 thro h TG 68 Sealinp Chart between the skin and the adaoter nange when installing the filler neck T...

Page 191: ...L AND INSTALLATION Ifl BOTTOM VIEW i Access Plate and Transmitter 2 Fuel CellXccess and Transmitter 3 Fuel Boost Pump I Fuel Cell Access Plate under the removable r 7 aft nacelle section i I 0 __ J 5 Outboard Fuel Cell Access Figure 8 6 Leading Edge Fuel Cell Access Openings TOP VIEW a Drain and purXe the fuel ceil b Remove the fuel ceil access plate 2 and trans mitter c Remove inboard access cove...

Page 192: ... inch pounds g Installation is accomplished by reversing the UT TE above procedure Use permate e No 2 Itern 3 if the fuel cell is to be stored for a period of Sealing Chart between the skin and the adaoter 10 days or longer coat the inside o he cz ilange when installing the filler neck Toro e the filler neck bolts to 45 to 33 inch pounds an l safetv with Light engine oil to prevent cracking or wir...

Page 193: ... cell and install the remaining test plate 3 Iake up a phenolphthalein solution as fol FUEL CELL REPAIR lows add O grams phenolphthalein crystals to 1 2 gallon of ethylalcohol miu then add lj2 llon of water REP 4IR OF RUBBER FUE L CELLS COODYEAR I Inflate the cell with air to a pressure of 1 The followin items for field rPoairable injuries in psi mauimum side or outside are per nissable Damaged ce...

Page 194: ... quart can containing 272 grams of 23 62C heat if necessary to liquify To this add one Iaterials and Equipment needed for repair can of 2233C 185cc and stir until smooth a minimum of 9 minutes is required a Air Care Kit 2F1 2 31853 a Apply two evenly brushed coats of cement to the QUAI PTITY TOEdENCLXTTiRE GOODYEhR cell and patch surface Allow 30 minutes drying time P 4RT NO between the second coa...

Page 195: ...le With the CABIN AIR control push let duct The heater is cycled by a 180 F thermal ed in attach the control wire to the iris valve actu switch in the heater outlet duct When the mode ator arm The air valve switch is positioned on the switch is placed in e BLOWER position the vent underside of the radio shelf and may be adjusted by air blower on the heater intake is activated The moving the snritc...

Page 196: ...Air Intake Duct i _ 18 Iris Valve 19 Intake Blower Assembly i f 20 Heater Safety Switch II i01 O O 21 Ignition Assembly i S 0 0 22 Heater Duct Thermostat 23 Overheat ruse 24 Heater Resistor 25 Duct to Rear Seat Outlet 26 Pilot s Air Control 27 Go Pilot s Air Control 28 Canopy Fresh Air Vent 29 Cabin Heat Circuit Breaker 30 Cabin Temperature Sensor 31 Outside Air Temperature Sensor 32 Combustion Ai...

Page 197: ... head of the switch indicates the direction the a pail of oil Heat the oil slowly until the points close screw should be turned to increase the temperature setting One turn will change the temperature setti o If it is necessary the overheat thermostat may be ad approldmately 125 degrees Fahrenheit justed by an adjusting screw on the bottom of the 10 2A ...

Page 198: ... lodging there t3 during the cleaning d Ens FL1 the vibrator retaining ring t1 e Safety wire ihe retaining ring to one of the screw HEATER SPARK PLUG GAP in the vibrator support collar a Heater spark plug gap should be set from 0 312 to J 0 250 inches The gap is determined by measuring 1 2 3 llt1 the distance between the spark plug electrode and the ground electrode Thegap may be adjusted by addin...

Page 199: ...n is the reverse of the removal pro cedure When installing he heater position the sup e Remove the screws securing the blower intake port ring and gasket so that the heater exhaust ex duct the bulkhead tends to the left of perpendicular approdmately 8 f Remove the clamps and pull the flexible combust m Make certain the clamps securing the inlet and ion air hose from the blower exhaust duct outlet ...

Page 200: ...er in clean unleaded gasoline and dry vith compressed air f DiscoMecr Ehe i nition lead at spark plug and remove the plenum and blower assemblv See Bendix Electric Fuel P 1ITID rns alladon and Ser vice Instructions orm EM 2j6 and Supplement o g Remove the fuel inlet cover and disconnect the I for detailed coverageof d e heater fuel pump combustion fuel inlet line h Remove the screws securing the f...

Page 201: ...MP CAGE SUC TION ACCUMULATOR C OPVI PRE SSOR CYLINDER RESSURE 1ELIEF VALVE TG 74 AND Z1 AIR BLOWER FTER 000 CABIN HOT GAS AIR 000 t II BYPASS 000 VALVE II IIEQUALIZER I I I tl AIR LINE FILTER TEMPERATURE O REFERENCE LINEI II TO OVERHEAD V EXHAUST FAN VENT I 00 rj P SIGHT GLASS EX PA NSION EVAPORATOR j COND ENSE R VA LVE R H WHEEL WELL RECEIVER DRIER TO FORWARD DRAIN CONDENSATION DUCTS Figure 10 3 ...

Page 202: ...ethyl tion gear down the air scoor will ooen to the chloride will cause rapid deterioration of the alum ground position gear off the groun i the air scoop inum compressor components will open or lower to the aight position The con denser fan operates any time the air conditioning d When the system with R 12 avoid mode is selected smoking or working near an open flame R 12 Dass ing over an open fla...

Page 203: ...o the connections on the com pressor The abbreviation DISCH or the letter D 2 Xttach service gages to compressor service on the compressor cylinder head designates the dis valve ports charge service valve The word SUCTION or the letter S on the compressor cylinder head desig 3 With air conditioner operating slowly close the nates the suction service valve suction service valve until the suction pr...

Page 204: ...re 10 J when the air scoop moves down from the round may be fabricated from 1 8 diameter rod a non position ferrous material which is not subject to corrosion is preferred Xotches cut 1j8 apart will aid in visually detecting oil depth CONDENSER AND EXHAUST BLOWER REMOVAL AND INSTALLATION COMPRESSOR BELT TENSION ADJUSTMENT The condenser compartment is located aft of the right fter 36 to Id hours op...

Page 205: ...ndenser to its COMPRESSOR REMOVAL AND INSTALLATION mounting flange and lift he condenser out of the com partment Installation is accomplished by the re versal of the above proceriure a Remove the RH engine cowling to gain access to the air conditioner compressor EVAPORATOR AIR FILTER REPLACEMENT b Disconnect electrical leads to the magnetic clutch c Disconnect Freon lines at compressor service The...

Page 206: ...ing the compressor mrbocharger mount support to the engine g Installation is accomplished by reversal of the above procedure See compressor belt tension adjust ment d Remove the belt from the engine crankshaft pulley and slip it out between the compressor turbochargor COMPRESSOR BELT REMOVAL AND mount and the engine INStALLATION e installation is accomplished by reversal of the above procedure ter...

Page 207: ... a Defective ductssat a Connect continuity meter across automatically ductscac leads and operate control Xs the control is pulled out ductstat switch should close completing the circuit 3 Heater backfires inter a Loose connection in a Check electrical connections mittently control circuit of loose joni tion lead to spark plug b Jlli ure too rich b Maka checks in item l below 4 Fuel misture too ric...

Page 208: ...er not functioning b Repair c Leak in system c Leak test and recharge d Compressor reed valves d Repair or replace inoperative e Expansion valve stuc i open e Replace 3 Air conditioner will not a 1Misadjustment of heater a Replace operate in AUTO mode bur will control box function in the IMXN COOL mode b Ialfunction of control box b EZeola ce c lalfunccion of emperarure c Replace sensing elements ...

Page 209: ...vaporator case a Lowcharge a Add R t2 8 Chatter or knock in evaporator a Defective e pansion valve a Replace case 9 Belt Slipping a Loose a Adjust b Overcharge b Correct Freon level c Air in system c Evacuate and recharge 10 Excessive belt wear a Pulleys not in line a Align pulleys b Belt too tight b Adjust or replace c Pulley groove wrong size c Replace d d Replace 1 EJroken oeit a Check all caus...

Page 210: ...The filler valve To prevent overheating fill the oxygen purging operation consists of nothing more than con system slowly by adjusting the recharging rate with necting a recharging cart filler hose to the applicable the pressure regulating valve on the cart The oxygen oxygen filler valve and allowing oxygen to flow through cylinder should be filled to a pressure of 1850 50 the system and escape at...

Page 211: ...OXYGEN FILLER VALVE I i I OXYGENGAGE I PRESSURE OXYGEN 65 CUBIC FOOT OXYGEN CYLINDER SHUT OFF VALVE 114 CUBIC FOOT OXYGEN CYLINDER Fi ure 11 1 Oxygen System 11 2 ...

Page 212: ...rks away from the vicinity of the oxygen cylinder Hands g Place the new cylinder in the brackets and close clothing and tools should be clean Oil and the cylinder clamps grease will ignite upon contact with pure oxy gen under pressure h Tighten the bracket clamp wing nuts i Install the shelf support tube a Slowly close the oxygen supply cylinder valve j Carefully inspect the fittings on both the c...

Page 213: ...nts which creates a vacuum in the deicer supply lines Normally the engine driven vacuum pumps apply to hold down the boots vacuum to the deicer boots at alltimes except when the boots are being inflated When the deicer system Either an AUTOMATIC or MANUAL position may control switch is olaced in either the MANUAL or be selected by the Deicer Control Switch located on AUTOMATIC position the timer e...

Page 214: ...1 j L H WING DEICE PRESSURE GAGE SHUTTLE VALVEI ISHUTTLE VALVE ITERC I F C 1 FILTER VACUUM MANIFOLD VENT VENT t DEICER CONTROL VALVE OVERBOARD VACUUM PUMP VACUUM PUMP SYSTEM VACUUM SYSTEM PRESSURE Figure 11 2 Surface Deicer System Vacuum TG 1 through TG 51 11 4 ...

Page 215: ...TOR VALVE OVERBOARD R H WING L H WING TO AUTOPILOT TO THE DEICER PRESSURE GAGE PRESSURE MANIFOLD rVARIABLE PRESSURE REGULATOR FILTER OVERBOARD OVERBOARD ENGINE DRIVEN DRY AIR PUMP TO THE MSTRU1MENT PANEL FILTER Figure ll 2A Surface Deicer System Pressure TG 52 and after 11 5 ...

Page 216: ...cer switch If the pin is not ejected from the the valve poppet and internal lining of the control solenoid replace the control valve valve may become coated with a film substance caus ing the valve poppet to stick To determine if the Air Leakage Test valve poppet is sticking perform the checks out lined in System Checkout Control Valves If the a Cap the overboard port of the control valve in solen...

Page 217: ...ct with the skin should be avoided a Clean the deicer boot thoroughly with toluol or uncontaminated unleaded aviation oasoline After the acid cleaner has had one minute s contact wipe dry with a clean cloth Allow a minimum of one b Roughen the entire surface of the boot with fine hour dry time before applying cement At the end of sandpaper the dry time wipe the surface with a clean cloth and inspe...

Page 218: ...the deicer connection being d Apply a coat to both the stall strip and the area careful to handle the boot section without getting to which it will be bonded Allow to dry 10 to 15 finger marks on the adhesive Using a lint free cloth minutes then install the strip as described in the heavily moisten not dripping with toluol reacti illustration The cement will set in about 6 hours vate the surface o...

Page 219: ...s f Piping lines kinked blocked f Inspect lines and connections blow or not connected out lines g Leak in system g See System Checkout Air Leakage Test 2 Deicer boots in a Piping lines kinked partially a Inspect lines and connections blow nate too slowly either blocked or not connected se out lines or both engines operating curely at minimum cruise rpm for a period of b Leak in system b See System...

Page 220: ... and connections blocked or not connec blow out lines ted g Leak in system g See system checkout locate and repair 2 Deicer boots inflate too a Piping lines kinked a Inspect lines and connections slowly either or both partially blocked or blow out lines engines operating at not connected securely minimum cruise RPM for a period of eight b Leak in system b See system checkout locate and seconds rep...

Page 221: ... valve ports of the distributor valve and check valve operation with a gage If trouble is not found in the distributor valve inspect boots and lines for leaks or blockage 5 One or more boots inflate a Exhaust port of distri a Reroute exhaust line to low but do not denate readily butor valve not vented to pressure area with pressure gage at normal low pressure area reading and timer cycling b Vacuu...

Page 222: ...ch is to the outboard and inboard heating elements in the turned on the ammeter registers the amount of cur following sequence RH outboard RH inboard LH rent 14 to 18 amps passing through the system If outboard LH inboard Since each of these phases is the current rises beyond the switch limit an integral 30 seconds in duration the timer makes a complete circuit breaker will cut off the power to th...

Page 223: ... stripe 170 to 180 inch wide on th e brush block lnd brush guide Locate 1 7 16 as shown in figure 1l 6A The white stripes should MAX r be in line with the outer brush and will be used to align the brushes with the slip ring during reinstal lation h Remove the termindlplate brushes and springs from the brush block Figure 11 5 Determining Deicer Brush Wear t a Loosen both ends of the brush block mou...

Page 224: ...ude arcing caused by the rough surfaces of the new brushes the engine should be operated for When replacing brushes or brush retainer at least five hours before the deicer system is turned assemblies always install new brush springs on This does not apply to ground checks of the sys tem performed while the engine is not running i Check the amount of brush protrusion from the block If the brushes p...

Page 225: ...ammeter needle should deflect every 30 seconds the ground lead rather than the timer If ground con in response to the switching action of the timer Each nection is open the timer step switch nrill not change time this occurs the man in the cockpit must notify position the man inspecting the propeller deicer boots so that the latter can change the position of his hands to b After the ground and pow...

Page 226: ...Ciir loi SPACER LEAD STRAP RESTRAINER PROP DEICER 13 8 L CLAMp SLIP RING STARTER RING GEAR ASSEMBLY MOUNTING PLATE SUPPORT BRUSH BLOCK AND MOUNTING BRACKET BAFFLE II I SLIP RINGS Figure 11 8 Propeller Deice Instdllatian 11 12 ...

Page 227: ...nt to soften the adhesive BRUSH BLOCK RESISTANCE CHECK f Remove the remaining adhesive from the boot and To check for an open circuit a short or high re pfopeller blade with toluol or methyl ethyl ketone sistance in the brush block measure the resistance from the face of the brush to its terminal studs or PROPELLER DEICER BOOT INSTALLATION receptacle pin with a low range ohmmeter If this resistanc...

Page 228: ...one coat of cement to the unglazed surface of the deicer boot It is not necessary to cement more than 1 2 i Roll outwardly from the center line to the edges inch of the deicer lead strap Allow the cement o of the boot See Figure 11 12 If excess material at the edges tends to form puckers work them out dry smoothly and carefully g Position the deicer boot on the propeller start ing 2t1 16 inch from...

Page 229: ...ead strap to the ropeller blade retaining clamps i Stick either the center or one edge of the patch lightly in place on the boot then work the remain r Connect the lead terminals and install the clip der of the patch down carefully to avoid trapping air on the spinner bulkhead There must be no slack between the surfaces of the patch and boot between the terminal and the clip to assure enough j Rol...

Page 230: ...ing chart the in step a of the 50 hour inspection in Section 16 and dication entries should be read to locate that which the heat test described in this section to determine matches conditions of the particular system being which circuits are involved A reading of two thirds checked The numbered probable cause and re the normal amount of current is an indication that one marks then indicate the pr...

Page 231: ...fire rent rest of cycle wallconnector If zero over 2 min utes locate and fix open in wiring from timer to firewall b Open between firewall and b If voltage Og to firewall plug try deicer lead straps voltage at junction of deicer lead and slip ring lead If no voltage find and correct open in wifi o to brush block open within brush block or no contact brush to slip ring c No ground circuit one c If ...

Page 232: ...ds check with ohmeter from pin G of harness to ground If no circuit refer to wiring diagram to fix open circuit b Timer contacts are welded b Test timer as in paragraph on caused by short circuit in timer check If timer does not cycle system with voltage at pin B replace timer but be sure short causing original failure has been located and correct ed 8 Ammeter flicks between a Loose connection bet...

Page 233: ...hin less d Replace at least 8 inches from than 8 inches of radio equipment input wiring to radio equipment 10 Cycling sequence not cor a Crossed connections a Check system wiring against cir cuit for improper connect rect ions 11 Rapid brush wear or frequent a Brush block out of alignment a Check brush alignment as in step g of 100 hour inspection breakage b Slip ring nrobbles b Check slip ring al...

Page 234: ...tem right side of the nose e If a decline in the reading of the airspeed indica tor is observed check the pitot system plumbing for CLEANING THE STATIC AIR SYSTEM leaky hoses and loose connections Blow LOW pressure air through the lines from the disconnected line at the airspeed indicator to the static ports Cover each static port separately when blowing to insure that each line is clear Instrumen...

Page 235: ...SEMBLY b o o STATIC AIR BUTTON STATIC AIR BUTTON PITOTLINE 56TC OPTIONAL PITOT INSTALLATION STATIC AIR LINE PITOT MAST rPITOT MAST EMERGENCY STATIC AIR SOURCE D ___1 STATIC AIR BUITON c FC STATIC AIR BUTTON AS6TC 56 394 3 Figure 11 13 Pitot and Static System 11 20 ...

Page 236: ...h the vane up and forward Moving the vane Actuate Sooner O with the phillips head screws loosened moves the entire unit up or down inside the wing causing the switch to be closed earlier or later Retighten the1 O screws after making each adjustment NEVER TRY THE SWITCH BY BENDING THE I I As a rule of thumb moving the vane 1 4 inch will o change the time the stall warning actuates by about 5 Adjust...

Page 237: ...e or a Lines clogged Drain lines at Emer erratic in operation gency Static Drain Disconnect lines at instruments and blow out with low pressure air b Line leaks Check lines for loose ness at all connection points STALL WARNING SYSTEM 1 Warning system inoperative a Warning circuit breaker tripped If circuit breaker persists in tripping check for grounded circuit b Open circuit Check for continuity ...

Page 238: ...ould be set at 8 0 in Hg With both engines The screens should be cleaned every 100 hoursor running the gage reading should be 8 4 in Hg more frequently as required If it appears that the valves need adjustment especially to lower the vacu um the screens should be cleaned and the setting checked before readjusting the valve REMOVAL AND INSTALLATION OF THE VACUUM PUMP SUCTION RELIEF VALVE ADJUSTMENT...

Page 239: ...VACUUM GAGE VACUUM RELIEF VACUUM RELIEF VALVE VALVE CHECK VALVE CHECK VALVE FILTER GYRO DIRECTIONAL HORIZON GYRO VACUUM PUMP VACUUM PUMP Figure 11 15 Vacuum System TG lthrough TG 51 11 24 ...

Page 240: ...ours of Rotating the adjusting screw on top of the pres operation or sooner if conditions warrant The sure regulator cloclnvise increases pressure sealed tilter on the pressure side of the pressure and counterclockwise decreases pressure pump located in each nacelle air of the firewall should be replaced every 300 hours of operation or e Locate the gyro pressure regulator on the LH less if operati...

Page 241: ...YRO I I t V GYRO I I II I I OVERBOARD I I GYRO HORIZON GYRO HORIZON I t I II I I REGULATOR I j GIPO PRESSURE INDICATOR MANIFOLD c FILTER CHECK VALVES FILTER f TEST GAGE TEST GAGE PRESSURE REGULATOR PRESSURE REGULATOR PUMP PUMP 567C 603 6 FILTER FILTER Figure 11 16 Basic Pressure System 11 26 ...

Page 242: ... operating at 2300 rpm the difference between the pressures on the test gages at ADJUSTMENT the pressure regulators in the nacelles should not exceed 5 psi a Remove both inline filters from the system and check for obstruction by comparing the resistance to NOTE now with a new filter Use a dry low pressure air source ma imum of 10 psi to accomplish this test If the required pressures of the above ...

Page 243: ...YRO L I 1 II REGULATOR i I I DEICER PRESSURE GAGE TO DEICER SYSTEM CYRO PRESSURE INDICATOR MANIFOLD FILTER FILTER CHECK VALVES TE3T OACE TEST OP GE I II TWO STAGE PRESSURE REGULATOR I TWO STAGE PRESSURE REGULATOR O O L l L J PUMP PUMP 56TC 603 1 FILTER FILTER Figure 11 17 Basic Pressure System and Deicer 11 28 ...

Page 244: ...RO i j GVRO HORIZON L I I I I I I t II II I I H1ESTGA6E rr i GYRO PRESSURE INDICATOR AUTOPILOT c MANIFOLD I MASTER VALVE TURN FILTER I 1 COORDINATOR FILTER CHECK VALVES TEST GAGE TEST GAGE PRESSURE REGULATOR I I PRESSURE REGULATOR PUMP PUMP 67C 603 8 FILTER FILTER Figure 11 18 Basic Pressure Syst m and New Matic Autopilot 11 29 ...

Page 245: ...sure regulator for that engine to obtain a reading of pressure regulator located on the RH side of each 5 0 c 0 5 psi on the test gage in the turn coordin nacelle aft of the firewall ator supply line with the autopilot ON Nrrmdly a pressure of 6 5 psi on the testgage at the pressure b Install a test gage 0 10 psi in the turn coordin regulator is sufficient to obtain the 5 0 0 5 psi ator supply lin...

Page 246: ...I I ii II TODEICFR ii H SYSTEM TEST GAGE __li o GYRO PRESSURE It l H DEICER PRESSURE INDICATOR I I 1 I I I I I INDICATOR AUTOPILOT r i MANIFOLD MASTER FILTER FILTER r 1 VALVE TURN COORDINATOR CHECK VALVES 1 1 1 1 TEST GAGE TEST GAGE z TWO STAGE PRESSURE REGULATOR TWO STAGE PRESSURE REGULATOR OI lo __J PUMP PUMP 56TC 603 9 FILTER FILTER Figure 11 19 Basic Pressure System New Matic Autopilot and Dei...

Page 247: ...rs located on the RH side of each nac elle aft of 0 5 psi on the test gage in the turn coordinator the firewall supply line with the autopilot ON and the deicer OFF The pressure regulator is located in the nose b Install a test gage 0 10 psi in the autopilot baggage compartment or under the pilot s seat aft of supply line at the out side of the pres sure mani the main spar fold The pressure manifo...

Page 248: ... I i I I REGULATOR DIRECTION GYRO GYRO HORIZON i TO H 14 AUTOPILOT L I I I _ TEST GAGE GYRO PRESSURE INDICATOR MANIFOLD FILTER CHECK VALVES FILTER TEST GAGE TEST GAGE PRESSURE REGULATOR PRESSURE REGULATOR PUMP PUMP 567C 603 10 FILTER FILTER Figure 11 20 Basic Pressure Sgstem and H 14 Autopilot ...

Page 249: ... not exceed 5 psi 1 Loosen the check nut and rot ate the adjusting If the pressure system does not meet the require screw do c kwi s e to i n c re as e pressure or counter ments of the preceding inspection procedure the system should be adjusted as follows clockwise to decrease pressure to obtain a reading of 5 0 1 2 in Hg on the gyro pr es sure indi cater with both engines operating at 23 00 rpm ...

Page 250: ...TH DEICER ON I I I I RESTRICTOR AUTOPILOT VALVE WITH DEICER OFF TO H l DEICER PRESSURE AUTOPILOT I INDI C A TO R GYRO PRESSURE O INDICATOR MANIFOLD FILTER i CHICK Y LYES r FILTER TEST GAGE I 1 I I 1 7 TEST GAGE r II TW STPIOl PRESSUR REOVIPITOP i O TWO STAGE PRESSURE REGULATOR L l L J J PUMP PUMP 567C 603 11 FILTER FILTER Figure 11 21 Basic Pressure System Deicer and H 14 Autopilot 11 35 ...

Page 251: ...radio panel to provide access to the back side of the turn and slip 1 Loosen the check nut and rotate the adjusting indicator screw clockwise to increase pressure or counter clockwise to decrease pressure to obtain a reading b Remove the plug on the upper side of the orifice of 5 0 1 2 in Hg on the gyro pressure indicator and install a test gage 0 5 inches Hg with both engines operating at 2300 rp...

Page 252: ...cquer i Spray on two thin topcoats of finish paint thinner or methyl ethylketone to remove shop primer euposed sealer and other shop soils The following is a list of the Enamel paints available d Lightly roughen all scratches with a nylon pad for the BEECHCRAFT TURBO BARON to insure a satisfactory paint base e Reclean the roughened surface with solvents to insure removal of all hand prints dirt an...

Page 253: ...y of the paints used in this blowing the skin laps with compressed air Wet procedure will extend beyond the time nor masking should be replaced mally required Under no circumstances should the paint be applied at temperatures below 600F since the paint will not cure PRETREATMENT WASH PRIMER The aircraft maybe finished with pretreatment wash primer Epoxy primer and a topcoat of Epoxy enamel An acid...

Page 254: ...and scratches left by the coarse paper so Sunshine Yellow 118684 233 that the finish will be perfectly smooth Take care to avoid removing any more metal than is absolutely WHITE necessary e Wash the sanded area with a solvent such as Matterhorn White 118684 217 lacquer thinner or methyl ethyl ketone Change the wash cloths used for this purpose frequently so that ORANGE all of the sanding dirt will...

Page 255: ...er Because of their resistance to chemicals and solvents urethane paints and primers require a special paint NOTE stripper If a methane stripper is not available a good enamel stripper may be used Rembving the For the best results these directions must be finish with such a substitute will require several followed carefully for some manufacturers applications while working the stripper in with a s...

Page 256: ...to the bare metal This should produce Sunshine Yellow 118684 321 a satisfactory undercoat for the repair area PAINTING MAGNESIUM g After the urethane primer has cured for 24 hours sand the area under repair with medium fine sand PAINT REMOVAL FROM MAGNESNM SURFACES paper Sand the edge of the repair area until the indentation where the metal and old paint meet is gone a Mask around the edge of the ...

Page 257: ...the painted surface should be done gently and held to a minimum to avoid cracking the paint b One coat of intermediate vinyl paint film c One coat of finish viny paint After the paint cures a thorough waxing win protect painted and unpainted metal surfaces from a variety of highly corrosive elements Flush loose dirt away NOTE first with clear water then wash the airplane with a mild soap and water...

Page 258: ...e color scheme has been reduced by less than 15C o after the cor must be maintained rosion has been removed the area should be treated with a 50 solution of nitric acid in water h Interior of all fluid lines and then given a protective coating as described below i Chromium plated portions of the landing oear piston tubes IcnunontUTION j Rubber and rubber like surfaces Be careful to keep the 50 nit...

Page 259: ...running water work to minimize streaking Keep the surface wet or a cheesecloth pad wetted with clean water Never with the solution for 1 to 3 minutes so that a con use a high pressure hose rinse since the freshly tinuous film is obtained with neither a grayish appear formed chemical film will be removed or damaged ance nor a dark powdery non adherent coating All treated parts should be kept clean ...

Page 260: ... other foreign materials of the electrolyte then release it as the battery is which will contaminate a storage battery and recharged Ti e electrolyte level on any battery must shorten its Life be ad usted after a full charae and a two to four hour p rest on open circuit Check the electrolyte level of the batte r Nly charged in the following manner after each 100 hours of service or every 30 days w...

Page 261: ...alent Make sure that the tion with a sodium bicarbonate solution and vents are unobstructed rinse Even minute traces of acid can dam age a nickel cadmium battery f Dry the filler cap vent plug with a clean cloth or compressed air then reinstall the plugs on the bat tery BATTERY CLEANING For peak performance nickel cadmium batteries g If the inside of the battery container is damp or wet discharge ...

Page 262: ...rging is necessary the following constant below or more frequently if temperatures are a current method is recommended bove 1000F When the battery condition is checked it also serves to equalize the cell voltages a When a new or completelydischarged battery is being charged the single cell voltage will be 1 4 a Discharge the battery at 2 2 amperes until the volts at the beginning of the charge and...

Page 263: ...uce an adequate electrical connection wall so NEVER use homemade hardware for this purpose b Remove the two nuts from the battery hold down bar and remove the bar and Lid j Tighten the link screws to a torque of 48 to 60 c Remove the battery from its compartment and inch pounds 4 to 5 foot pounds clean in accordance with the cleaning procedure out lined in this section k Discharge the battery at a...

Page 264: ...justment at which the overvoltage relay trips and removes the alternator from the line Slowly adjust the voltage regulator to increase the bus voltage The overvoltage Both alternators are controlled by a single transis relay must trip at 32 I volt torized voltage regulator therefore paralleling of the alternators is not necessary The voltage reg Icnvn di ulators are located in the electrical equip...

Page 265: ...a test harness The test harness may be nator may result from accidental ground constructed from an MS3106 18 13 connector or ing equivalent with pins A F H and J jumpered and connected to the positive side of the variable power supply pin C connected to the negative side of the variable power supply and a 30 volt indicating light a Secure the alternator to the upper and lower connected between pin...

Page 266: ...moved 33 c 00 25 volts on aircraft TG 84 and after from the aircraft and completely serviced When the relay is determined defective it should be replaced with a new or exchange relay f Start the engines and advance the throttles as required to obtain desired voltage output OVERVOLTAGE RELAY CHECK g Turn off all switches and circuit breakers except the battery master switch and the alternator or ge...

Page 267: ...ration Excessive heat Preliminary Adjustment of Paralleling Rheostats build up may cause damage to these com ponents a Open the electrical components compartment ac cess cover on top of the LtI nacelle aft of the engine VOLTAGE ADJUSTMENT Minimum Load cowling b Connect the negative lead of a voltmeter to ter minal p on the LH voltage regulator base and the The voltage regulators are adjusted to pr...

Page 268: ... and generator temper equal outputs from the generators at heavy loads atures as outlined in Stabilization of Generator Sys tem a Check the accuracy of the loadmeters on the in c Check minimum load voltage and m udmum strument panel by alternately switching from one gen current paralleling at cruise engine rpm 2750 rpm erator to the other while a normal load is turned on If equal readings are obta...

Page 269: ... should not should be replaced if it has been worn to the indicator exceed 0 3 volts or if it is obvious that the brush will reach the min imum length before the next inspection time 2 The voltage loss from the battery ground terminal to the starter frame should not New brushes must be properly seated on the commu exceed 0 i volt tator surface before the generator is subjected to heavy loads to pr...

Page 270: ... I 1 12 R H Alternator Out Relav 33 Navigation Light Flasher i 1 13 tl Voltage Regulator Overvoltag e Relay 34 Starting Vibrator CJfl 14 2 Voltage Regulator Overvoltage Relay 35 Warning Horn Flasher i i 15 Inverter Fuel Flow Indicator 36 Landing Gear Warning Horn 1 16 L H Shunt and Loadmeter Fuse 37 Stall Warning Horn 17 R H Shunt and Loadmeter Fuse 38 Limiters 18 L H Generator Control Relay and F...

Page 271: ...p Light 1495 Reading Light 1495 Tab Position Indicator Light 1819R L G Visual Indicator Light Assembly 95 324006 75 Compass Light 327 Instrument Lights 327 Rotating Beacon A 7079B 24 Taxi Light Landing Gear 4626 Landing Gear Position Light 327 Ice Light A 7796A 24 Alternator Warning Light 2390A17 Generator Warning Light 2390812 Fuel Boost Warning Light 2390A20 Glareshield Instrument Lights 1829 No...

Page 272: ...lly trip the cfr light cult breaker in the power supply unit The most likely reasons for malfunctions of this unit are shorts POWER CABLE CHECKS in either the power cable or the lamp assembly shorts caused by contact of the transistor case with a a Check that the individual conductors of the power foreign object during operation of the unit moisture cable are soldered to the connector pins as foll...

Page 273: ... the case on its top remove the four approximately 900 volts If there is no reading bottom screws andlift away the bottom replace or repair the power pack assembly 2 Reverse the case remove the four top screws 3 The power pack assembly consists of a simple and lift away top assembly single transistor DC to DC converter The diodes resistors and transistor can be checked with an 3 Remove the circuit...

Page 274: ...n the lamp As the lamp ignites moved apply power to the input wire and measure the energy stored in the capacitor is discharged each pin of the three Jones pl gos through the lamp to produce a peak light intensity of over a million candle power When the capacitor Pin 1 the pin turned lengthwise Gnd voltage drops below 50 volts the lamp will go out Pin 2 center alternating lOV approximately and the...

Page 275: ... If the converter won t start when voltage is first 55 times per minute If the pulse is recorded on the applied a small current kick is noted and then no scope then the SCR is not triggering and should be current is drawn look for a poor solder feint in the replaced starting circuit R2 2 7K and R1 82 ohms The con verter map be started by applying about 2 volts to the c When no voltage is observed ...

Page 276: ... 0 16 Field ESrciter Printed Circuit Board 1 0 03 0 03 Heater System VentBlower 1 14 0 14 0 Vent Blower Relay 1 0 10 0 10 Combustion Blower 1 2 90 2 90 Fuel Pump 2 0 40 0 80 Solenoid theater fuel I 0 39 0 39 iManual or Auto Select Relay 1 0 09 0 09 Cabin Temperature Control Box 1 0 18 0 18 Ignitor 1 1 90 1 90 Lighting Edge Lights Circuit breaker and switch panel 7 0 04 0 28 Compass 1 0 04 0 04 Dom...

Page 277: ...ter L H 1 3 30 3 30 Stall Warning Switch Heater 1 1 60 1 60 CONTINUOUS LOAD OPTIONAL EQUIPMENT Air Conditioner Heater and Air Conditioner Control Relays 2 0 09 0 18 Condenser and Evaporator Blower Relay 1 0 50 0 50 Evaporator Blower 1 17 50 17 50 Condenser Blower 1 15 00 15 00 Nacelle Scoop Relay 1 0 09 0 09 lagnetic Clutch 1 0 20 0 20 Suction Throttling Solenoid 1 0 75 0 75 Hot Gas By Pass 1 0 75...

Page 278: ...ur Meter 1 0 05 0 05 INTERMITTENT LOAD STANDARD EQUIPMENT Lights Landing 2 8 90 17 80 T ud 1 6 00 6 00 Fuel Boost Out Annunciator 2 0 08 0 16 Stall Warning Horn 1 1 50 1 50 Fuel Boost Pump 2 14 0 14 0 Cowl Flap Actuator 2 1 2 1 2 Cigarette Lighter 1 7 5 7 5 Starter Relay 2 0 6 0 6 Starting Vibrator 1 2 00 2 00 Starter 1 275 00 275 00 Flap Motor 1 13 0 13 0 L G Warning Horn 1 1 5 1 5 L G Horn Flash...

Page 279: ...it Aircraft In Amps In Amps INTERMITTENT LOAD OPTIONAL EQUIPMENT Surface Deice Relay 1 0 09 0 09 Surface Deice Time Delay Relay 1 0 17 0 1 Surface Deice Valve 2 1 50 3 00 Magic Hand Switch 1 2 50 2 50 Nacelle Scoop Actuator I 1 20 1 20 13 15 ...

Page 280: ...nce varies greatly from 12 ohms repair alternator per Al ternator Service anual g Shorted or open diodes g Check resistance with ohmmeter from BAT terminal to alternator frame Note reading and reverse the ohmmeter leads One reading should be low and one high If both are low or high repair alternator per the Alternator Service Manual 2 Noisy Alternator a Loose worn or frayed a Replace drive belt b ...

Page 281: ... c Clean the jatter j and charge as required then adj us t the ele c tr o lyte level 6 Cell cases distorted a Excessive charge rate a Replace distorted cells 7 Unequal vo itages among cells a Cells unbalanced a Equaiiz e cell es 8 Foreign m a tte r within c ells a Impure or a c id e onta minat ed a Such c e ils will not no rmaily re wa te r spend to charging They will show up as unbalanced cells a...

Page 282: ...it c Test resis ance of field Check in generator defective armature field circuit connections Replace generator if defective d Brushes not contacting com d Clean brushes and holders with mutator a clean Lint free dry cloth Re place weak springs e Brushes morn out e ReDlace brushes if worn to a 1 2 inch or less f Dirty Commutator f With generator running clean commutator with To 0000 sand paper Use...

Page 283: ... burned out a Replace bulb b Fisrure not grounded b Check for good bonding benveen iisture and structure Tighten mounting screws c Loose connection c Check all connections in circuit d Defective or switch d Replace fiuture or switch LANDING LIGHTS i Lamp fails to light a Circuit breaker tripped a Check for short circuit Reset circuit breaker b Lamp burned out b Replace lamp c Loose connection or d...

Page 284: ...STALL WARNING CIRCUIT CONT D IN DICATION PROBABLE CAUSE REMARKS 2 Horn sbys on a Grounded circuit between a Test for ground horn and switch b Defective switch b Check switch operation 13 20 ...

Page 285: ... o i the various i irs u i t s in mo st instances has 5een ignored V te m a to r I 1 1 3 Lights Co n t d nnunciator 11 jS Control Panel and Indicator 14 50 Autopilot H 14 14 8 Courtesy and Baggage il o Battery and E x te rn ai Power 1 4 7 Do me and Reading 1 4 41 Cabin Temperature C o n trol 1 4 73 Ele ctr o lu mincie n t Panel I 1 51 Cigarette 14 66 Engine Instrument 1 5j Cowl Flap Actuators iii ...

Page 286: ... on most of the iol loaing type switches and relays 2 Position 3 Position q I O I j O 2 Pole Pressure Switch MOTORS r i Low Current High Current 2 Wire 3 Wire CIRCUIT BREAKERS i O 3 O O 5AO O A O Push Pull Toggle Push to Beset TERMINAL BOARDS 8 BUS BARS OOO151 13123 Terminal Board Terminal Board with Bus Bar Open Bus Bar sa aoel 14 2 ...

Page 287: ...t t tt C i I iultiple Conductor Shielded Wire Twisted Wiring Cables Plug and Receptacle GROUND CONNECTORS a I r a LIGHIS I 77 Case Ground Ground Connection Connection Press to Test Light Light MISCELLANEOUS iililllt V V Battery Capacitor Heating Element Thermocouple v Speaker or Electrical Instrument Warning Horn 60 369 88 14 3 ...

Page 288: ... TAXILIGHT i I COWLFLAPS LH LANDING LIGHT a a C LINDER HEAD aND 011 TEMPERATURE PH LANDING LIGHT o i I i NE QUANTITY LH FUEL 800ST Ili l STARTER AND IGNITION r4388 Rn FUEL acosT CIGARETTE SnD109VS FL Hd2Nla LIGHTER PsZRIO dlH ITERNATORICENEI TOII VENT AND CONDENSER BLOWEREVnPORArOR BLOWER PdZSIO v 3H I Eiternal Porer leloy 6 RH SLorter i elo II LH Storter 2 Bat erv Bu 7 Limiler 12 aH Storter 3 8oi...

Page 289: ... LANDING GEAR RELAY NAVIGATION LIGHTS B FLAPS ICELIGHTS 1Eil TURN AND SLIP TAXILIGHT 1 COwLFLAPS LH LANDING LIGHT n CYLINDER HEAD AND 311 TEMPERATURE Pn LANDING LIGHT U FUEL OUANTITY LH FUEL BOOST 8 3 STARTER AND IGNITION pajse RH FUEL 8005T CIGARETTE P12N18 LIGHTER RADIO 3US I ExlernaI Porer Pslay 6 RH S ortsr Rslo II LH Storier 2 Batlsry Bui 7 Limiter II RH Slar er 3 Ba tery 8 Bui IJ PH Al erno ...

Page 290: ...AT I i a SURFACE DEICE 862910 P6 c 6 i a zn rua BOOST 1 pa elo LH FUEL BOOST HEATER 3LOWE4 I I I FUEL OUANTITY LANDING GEAR MOTOR a I I u CYLINDER HEAD TEMP LANDING GEAR RELAY I U OIL TEMP FUIPMOTOI n COWL FII S FLAP POSITION P61C10 u STARTER AND IGNITION ALTERNATOR FIELD INSTRUMENT LIGHTS ALT AND CIG LTR 3 1 3 CABIN LIGHTS THROTTLE NnRNINC P63B10 C ALT OUT LIGHTS PITCH TRIM C P90A18 GENERATOR ONL...

Page 291: ... P45A2 f I I I I P 384N fB A2 I X1 D45C 18 pd5 B18 pdST 18 PdSE18 X1 Ejl X2 P46X18N 4 56TC 369 87 i Bus 2 E cternal Power Safety Relay 3 E cternnl Power Receptacle 4 Battery 5 Battery Relay 6 Battery Switch Figure 14 2 Battery and External Power TG 1 thru TG 83 14 7 ...

Page 292: ...GHTS I T TO P4jF18 STALL WXRNING W6r20 f P4j 2 I I I I I I P43A2N I la i X1 I X2 Pd5C 18 P45B18 P4SE18 X2 1 46X18N CL P i Bus 2 External Power Safety Relay 3 External Power Receptacle 1 Battery 3 Battery Relay 6 Battery Switch 561C 369 9 Figure 14 2 Battery and External Power TG 84 and after 14 8 ...

Page 293: ...BAT BoDe I L Sosw IP K10A20 J5A20 J 56TC 369 10 1 C ire u it B r e ake r 8 L H Mag R H E ngin e 2 R H Engine ignition Switch 9 R H Mag R H Engine 3 Starting Vibr ator 10 R H Ce ner ator Firewall Connector 1 I H Engine Ignition Switch 11 L H Mag L ii Engine 5 L H Starter 12 R H Mag L H Engine 6 L H Ge n e r ato r And Starter F ir e wall C onnec to r 13 L H Start e r Relay 7 R H Starter 14 Battery B...

Page 294: ...J3A18 m BAT BO Ot 7 I L rv SW C3 K10A20 J5A 20 i Circuit Sr caker 9 R H MaLS R H Engine 2 R H Eneine IL nition Switch 10 R ii Generator Fire WallCo nnec tor 3 Sta rtin V i b ra to r 1 1 L H M L i i Engine 1 L H Encine l nition Switch 12 R H Ma L H Engine 5 L H Starter 13 L H Starter Relay L ti Cc n c ra to r And S ta r re r F i re wall C onnec to r 14 B at te ry Bus R H Starter 15 R H Starter Rela...

Page 295: ... RET KISXZON L 1 R 0 13X18 I E I BAT SW I i r K10A20 J5X20 i Circuit Breaker 9 R H JI R H Engine 2 R H Engine ignition SwitCh 10 R H Generator Fire Wall Connector 3 Starting Vibrator 11 L H Engine 1 L I i Engine ignition Switch 12 R tI ZvIar3 L H Engine 5 L E Starter 13 L H Starter Relay 6 L H Generator And Starter Firewall Connector ld Bat eryBus 7 R ii Starter 15 L H Starter Relay 8 L H ag R H E...

Page 296: ...18 P69A18 p82A18N P85A18 P78Dlsl I IP78B18 P69B181 I llP69D18 P71A18 P 2A18N P78C18 P79A18 P69C18 P3 E6N P28E6N L P67A18 L P84B18e u r kl O O P84A18 m P79B18 P79B18 P67B18 P76A18 ru P75A18 P76D18 Q1 567C 369 41 1 Battery Bus 2 Annunciator Test Switch 8 Loadmeter 14 Firewall Connector Generator Starter 3 Emergency Excitation Supply 9 Shunt 75 amp 50 my 15 Voltage Regulator Overvoltage Relay 4 ReEul...

Page 297: ...I m rn c P76C18 P76A18 T P27X10 P82A18N P85A18 P78D18 P78B18 P69 B18 P69D18 P71A18 P72A18N PJV1ON L K16B18 1 1 Psscia P37E6N L P84B18 P78C18 IC 7r L P67d18 L d 5A P77A18 SA K18A18LiiO s OC O P81A18eP69A18 P84A18 P67A18 561C 369 43 1 Battery Bus 2 Annunciator Test Switch 8 Loadmeter 15 Voltage Regulator Overvoltage Relay 3 Emergency Excitation Supply 9 Shunt 75 amp 50 my 16 Fuse Alternator Stater 4...

Page 298: ...8D18 P78B18 P69B18 P69D18 P 1A1B P 2A18N P3UION PZ IPION P2BE6N IL P76B18 P69C18 L P37E6N I pe4sla 8 Or P6 A18 1 d 54 bP77A18 P81A18 56 P78A18PS4A18 O O P67A18 eP69A18 567C 369 44 i Battery Bus 2 Annunciator Test Switch 8 L oadmeter 15 VulBge Regulator Overvoltage Relay 3 Emergency Excitation Supply 9 Shunt 75 amp 50 my 16 F use Alternator Stater 4 Regulator Select Switch 10 NotUsed 17 Fase Altern...

Page 299: ...4B10 I TP6B O A A H F 3 D G I E B C C B E I G D J F H mT I 6P18 I I PBSBi8 1Pd9D18 P71A18 P72A18N P4AION P82A18N p85A18 P78D18 P6A 10h P32A6N J P77B18 P69C18 L P38A6N L P78C18 L P76C18 P76B18 O rl L3 2 P77A18 P84A18 10A P67A18 O O P78A18 P69A18 P84A B 1 Battery Bus 7 Loadmeter 13 Fuse Alternator Stater 2 Alternator Out Relay 8 Shunt 75 amp 50 my 14 Fuse Alternator Field 3 Emergency Excitation Supp...

Page 300: ...P13 B1 L Q or D L or G G1 or CI I I I I I G or C L or G Q or D P29A18 F or A EB or K T I P115A1s T EB or K F or A P25B18 P11OB18NS m e PI1IBlsN P25A1S P30A18 P49A18 P50B18 PllA1S P29B18 P27B2 P30E18 PllE1S P3C2 O m En m o BA 46 m 7 r tO E Pi8 92N P11IA1SN P1 OA18N P37D2N L L L 567C 369 45 11 Oventoltage Relay 2 12 Fuse Generator Control 16 Firewali Connector Generator Starter i BatteryBus 6 Contro...

Page 301: ...C L or G Q or D P36A18 t f P18A18 P29A18 F oi A EB or K P49B18 T I P115A18 17 EB or K F or A P21B10 m ms m l1 6 moais m I P16A18 P50B18 m 0 id A P29B18 PI1IB18N P1IOB18N P27E6 P16B18 P21A18 P3A6 P3E6 P30B18 P2 A6 m t rn m hm I I t A Il m m P22A6N F12136n PI11A18N PI1OA18K P43A6N P43B6N L L L J 56TC 369 X i Ballerv Bus 6 Fuse Loadmeter ii Control Relay 16 Generator 2 Cul rrnl Linliter Gcnerator 7 L...

Page 302: ...20 E12A20 E16X20 E12A20 6 r I E15X20N E1 ABON E11 20N E11 20N P Routing When Nacelle Fuel Transmitter Is Installed 56TC 369 46 i Fuel Quantity Circuit Breaker 5 Leading Edge Fuel Cell Inboard Transmitter 2 Printed Circuit Board 6 Leading Edge Fuel Ceil Outboard Transmitter 3 Fuel Quantity Indicator 7 Nacelle Fuel Transmitter Optional 4 Wing Tank Outboard Transmitter Figure 14 6 Fuel Quantity Indic...

Page 303: ...NST LLEG THE BOX SECTION TKANS IITTER IS O IITTED WIRE ROUTING WHEN OPTIONAL NACELLE FUEL CELL IS INSTALLE D PRLNTED CIRCUIT BOARD IS IOIINTED ON INDICATOR WITH NO WIRES BETWEEN 567C 369 41 i Circuit Breaker Fuel Quantity Indicator 3 Printed Circuit Board 1 Box Section Fuel Cell Transmitter 5 Leading Edge Fuel Cell Inboard Trrulsmitter 6 Leadin Edge Fuel Ceil Oueboard Transmitter 7 Naceile Fuel Ce...

Page 304: ...n 72 TS 13 II T TS o o O i 1 Q O IZ1PI2ON B B i E17820 E13820 E22820N E17 A20 I El 3420 E17 20 E13820 L1 i n i Circuit Br aC r Piin d Circuit Board 3 Fu l Ouanti y Indicator E14i20 El 8420 4 Inboard Tranimitt r 5 Ouiboard Tranrmitt r b Nac il Zi l V r o E19h20 E15 20 o r i D E16A20N E20 20N 567C 369 38 Figure 14 6 Fuel Quantity indicator TG 84 and after 14 20 ...

Page 305: ...B 17 17 1 1 IC eL I I B Q4B1 6 4A16 6A1 6 a 6B1 6 r 7 r i L I L 95A16N 97A16r T 1 IL 5 6TC 3 69 4 8 1 Annunciator Test Switc h 2 C i r cult Bre ake r 3 Fuel Boost Pump 4 Pr e s sur e Switch 5 Fuel Boo st Annune i ator Figure 14 7 Fuel Boost Pumps TG 1 TG 3 thru TG 15 TG 18 thru TG 20 TG 22 TG 23 TG 25 thru TG 27 TG 29 TG 30 TG 36 and TG 37 14 21 ...

Page 306: ...TE glsls Q3B16 I I I a gsA16 g4n16 s C A X 0 PIC B QlB16 06816 B d f n o 1 Q7A16N Q5A16N I_ 1L 1 Annunciator Test Switch 2 Boost Pump Circuit Breaker 56TC 369 49 3 Boost Pump Switch 4 Fuel Boost Pump 5 Pressure Switch 6 Fuel Boost FailAnnunciator Figure 14 7 Fuel Boost Pumps TG 2 TG 16 TG 17 TG 21 TG 24 TG 28 TG 31 thru TG 35 TG 38 and after Aircraft complying with S B 67 36 14 22 ...

Page 307: ...814 SLACK BLACK_L 1 ri Q4A 4N Q2A14N WHITE WHITE Q6X20 gsczo P E31 Q6sz0 JDz0 A A C 9 3 cs Q B 6C20 TO ANNUNCIATOR Q 5E20 1 Boost Pump Circuit Breaker 2 Boost Pump Switch 3 Fuel Boost Pump 4 Pressure Switch Figure 14 7 Fuel Boost Pump TG 84 and after 14 23 ...

Page 308: ...B18 B 56TC 369 SO Circuit Breaker 2 L H Cylinder Head and Oil T e mpe ratu re Indicator 3 Fi r ew all Connecto r Ac c e s sorie s 4 Oil Te mpe r ature Bulb 5 Cylinder Head Temperature Bulb 6 R H Cylinder Head and Oi 1 Te mperatu re Indic ator 7 Fir ew all Connecto r Ac c e s sorie s 8 Cylinder Head Te mper atur e Bulb 9 Oil Te mpe rature Bulb Figure 1 4 8 Cy I inder Head a nd Oil Temperature indic...

Page 309: ...6A20 B j E6B18 B 56 TC 3 6 9 51 1 Circuit Br eaker 2 Cylinder Head T e mper atur e Indic at or 3 L H F ir ewall 4 L H Oil T e m pe r atur e Bulb L H C ylinde r Head T e m pe ratur e Bulb 6 Oil T e m pe ratur e Indicator 7 R H Firewall Connector Ace essories 8 R H Oil T e mpe r atur e Bulb 9 R H Cylinder Head Tem per atur e Bulb Figure 14 8 Cylinder Head and Oil Temperature indicator TG 4 TG 25 TG ...

Page 310: ...N 8 ESA20 I B A i Oil Temperature Circuit Breaker 2 Cylinder Head Temperature Circuit Breaker 3 Cylinder Head Temperature Indicator 1 L H Firewall 5 L H OilTemperature Bulb 6 L H Cylinder Head Temperature Bulb 7 OilTemperature Indicator 8 R H Firewail Connector Accessories 9 R H Oil Temperature Bulb 10 R H Cylinder Head Temperature Bulb 161C 369 13 igure 14 8 Cylinder Head and Oii Temperature Indi...

Page 311: ...BIC CK PBLACK WHITE WHITE i i WHITE 18 WHITE 18 1 56TC 365 52 1 Circuit Breaker 2 L H Cowl Flap Control Switch 3 R H Cowl Flap Control Switch 4 L H Firewall Connector En ine Accessories 5 R H Firewall Connector Engine Accessories 6 L H Cowl Flap Motor 7 R H Cowl Flap Motor Figure 14 9 Cowl Flap Acautaors TG 1 thru TG 51 14 31 ...

Page 312: ... T RED YELLOW YELLOW RED PI n BWCK BWCK WHITE WHITE t WHITE WHITE 18 18 1 I Circuit Breaker 2 L H Cowl Flap Control Switch 3 R H Cowl Flap Control Switch 4 L H Firewail Connector En ine Accessories 567 3 369 53 5 R H Firewall Connector Engine Accessories 6 L H Cowl Flap iMotor 7 R H Cowl Flap Motor 8 Cowl Flap Open Indicator Figure 14 9 Cowl Flap Actuators TG 52 thru TG 83 14 28 ii ...

Page 313: ... II RED YEL LOW YEL LOW BLACK SLXCK RED WHIT E WHITE W HIT E WHITE 1 3 18 _L i sarc ap l4 1 Circuit B r e a ke r 2 L H Cowl Flap Control Swite h 3 R H Cowl Flap Co ntro I S wi te h i L ii F i r ewall Connector En ine i e c e ss o r ie s R H Firewall Connec to r Engine X c c e s so r ie s 6 L H Cow Flap Motor 7 R ii Cowi Flap iMotor Figure 14 9 Cowl Ftap Actuators TG 84 and after 14 29 ...

Page 314: ... E30B 8 L I O c E35B18 4 E35A20 7 1 I I I E31A20 6 E29G20 E E32G18N I L 1 i r L I E32BlsN I I O I I I I I I I I r O E29F20 1 E33AlsN E32C20N A 8 6 E B 6 F 1 Inverter 2 Fuse 3 L H Fuel Flow Transmitter 567C 369 41 4 Firewall Connector Accessories 5 Fuel Flow Indicator 6 Firewall Connector Accessories 10 7 R H Fuel Flow Transmitter Figure 14 10 Fuel Flow Indicator TG 1 thru TG 83 14 30 ...

Page 315: ...20 I r II T E29A20 1 I I I I I E33A20 7 ILC E33B20 II E E31B20N Y II L E31A20N 1 III I I I I E37A20N I I E37B20N O I I I I E27D20 E28A20hT E38A20N LT A lil ACDEBCf 1 Circuit Breaker 2 Inverter 3 Fuse 4 L H Fuel Flow Transmitter 5 Firewall Connector Accessories 6 Fuel Flow Indicator 7 Fireu all Connertor Accessories B 56TC3W3 8 R H Fuel Flow Transmitter Figure 14 10 Fuel Flow Indicator TG 84 and af...

Page 316: ...tch Gear Safety System 18 R H Throttle Switch Gear Safety System 19 Test Switch Gear Safety System 20 Pressure Switch 70 MPH G15B20 G7820 7 _I Iczo I I I I IP G20A20 G1D 6k13C21A20 1 G1 RZ 1 TEST I OFF C15B20 S Z GllA20 I G 2A20 I G23A20 G2A20N G2B20N L G22A20 i 1 C2 3 Ct to I C14A20 G14A G6B20 UP TO FLIGHT G13A12 G19 I G18A20 BCCn 820 G6R20 110 RED BLACK m1 20 m NO NC AIR GND O C21A20 P 40 R 3 20...

Page 317: ...fety System G8A20 1 I I 1 19 Test Switch Gear Safety System 20 Pressure Switch 70 MPH G15B20 O G7B20 o T4 Iczo I I I I m llA2 G20A20 LG6C20 O 1 i Gt4 R2 2h n In I I I TEST OFF Gl1A20 G1 5B20 05 02 G12A20 G23A20 G2A20h C2B20N L I Im c2 3 Ct I C D t r G14A20 G14A C 3 G6B20G22A20 UP TO FLIGHT 3A10 j HOUR METER OPTIONAL G19 _L WHITE 12 G18A20 RED 1 BLACK 12 G6C20 I IG4A mQ1 20 ID m r Gh D NO NC m G25A...

Page 318: ...LY 40Q EXTE JDED L JD THROTTLE low h G5 20 C LOSZD RIG AND CONNECT L UDMG GE R SAFETY SWITCH I I COhrlPLIANCE WITH S I 0417 350 i Landing Gear Motor Circuit Breaker 9 Up Limit Switch 7 Throttle Warning Circuit Breaker 10 Landing Gear Jllotor 3 Landing Gear Control Circuit Breaker 11 L H Throttle Warning Switch 1 Control Switch 12 R H Throttle Warning Switch 5 Down Limit Switch 13 Warning Horn ij G...

Page 319: ...ENDED iWD THROTTLE G5X20 G25B20N n RIG CON IECT LilNDING GE R SXTETY SWITCH IN COMPLWNCE WITH S i 0417 350 i Landing Gear Lrotor Circuit Breaker 9 Up Limit Snritch 2 Throttle Warning Circuit 8rea er 10 Landing Gear i otor 3 Landing Gear Control Circuit Breaker 11 L H Thro tle Warning Switch 1 Control Switch 12 R H Throttle Warning Switch J Down Limit Switch 13 WarningHorn 6 Gear Down Light la Warn...

Page 320: ...LIGHTS I SC16 C3A16 CIRCTirT BREAKER r L1A18 I BLUE 18 C3C16 2 11B20 t WMTE 20 D 0 160Z 3 12520 e RED 10 C6A12N C13A20N _I I PRINTED CIRCUIT BOARD MOUNTED O INDICATOR TERMINALS i Circuit Breaker Flap 2 Flap Control Switch 3 Up Limit Switch 4 15 Limit Switch 5 Down Limit Switch 6 Flap Position Transmitter 7 Printed Circuit Board 8 Flap Position Indicator 9 FlapMotor Figure 14 13 Wing Flaps TG 1 thr...

Page 321: ... I B LUE 10 I C5B14 C11B20 f WHITE 20 95 I I I I ys A o Iso r 1zs20 e I 3 C6A14N C18A20N I r PRINTED CIRCUIT BOARD MCUNTED ON INDICATOR 1 Circuit Breaker Flap TERMMALS 2 Flap Control Switch 3 Ut Limit Switch 4 163 Limit Switch 5 14 Limit Switch 6 Down Limit Switch 7 FlaD Position Transmitter 8 Printed Circuit Board 9 Flap Position Indicator 10 Flap Iotor 67C 369 17 11 Circuit Breaker Indicator Fig...

Page 322: ... I I I II LEFT j 1 Q a I F49418 P49C18 1 T P49818 IU OUT I W3 29W3EZO TO 10 CENER TOR ALTERN TOR aDlo aaculr clnculr I EI r PJOA18 3 PSOCIB n RIGHT P50818 R 2 T I i Circuit a oic r I I I Dimming I loy OUT W3FZO P 3 T rt Sritch W1 20 LIEZO i Bloc ing Diod El 5 Lights B LEFT Csn rator Oplionol C F ZJ I ZA20 o L w A L p W3G20 OPEN W3H20 TOCOWL FLXP ACTUATOR LIFZO B LI RIGHT C F O C 2 1 i K5A20 W a LP...

Page 323: ... Circuit Breaker 2 L H Wing Ice Light 56TC 369 SS Figure 14 15 Wing ice Light TG 1 thru TG 83 L25X20N WIRE FURNISHEI WITH LIGHT 1 3A 1 Circuit Breaker 2 L H Wing Ice Light Figure 14 15 Wing ice Light TG 84 and after 14 3 ...

Page 324: ... Rotating Beacon 3 Lower Rotating Beacon Figure 14 16 Rotating Beacon TG I t ru TG 83 L7A18 RED s L1 L8A18N WHITE I B 10 L7B18 L7C18 RED WHITE fIIO L48B18N Ll8A18N 3 WHITE I P 1 Circuit Breaker 2 Upper Rotating Beacon 61C 369 17 3 Lower Rotating Beacon Figure 14 lfj Rotating Beacon TG 84 and after 14 40 ...

Page 325: ... B When Optional Rotating Beacons are Installed this Routing Used and Flasher Omitted 56TC 369 59 1 Circuit Breaker 2 Navigational Lamp Flasher 3 L H Wing Navigational Lights 4 Tail Navigation Lights 5 R H Wing Navigational Lights Figure 14 17 Navigation Lights TG 1 thru TG 83 1 41 ...

Page 326: ...N UNC WT OR DIMMI NG I When Optional Ro ta ti ng B eac ons ar e In s talle d this Routing Used and Flas he r Omitted i Cir cult Br eaker 2 Navi gational L am p Flasher 3 L H Wing Navigational Lights 4 TailN avigation Lights 5 R Il Wing Navigational Lights Figure 14 17 Navigation Lights TG 84 and after 14 42 ...

Page 327: ... 6TC 369 5 7 1 Cir cult B reake r 2 Taxi Light Figure 14 18 Taxi Light 1 OA 6 10A 56 TC 36 9 58 1 Cir cult Breaker 2 L H Landing Light 3 Cir cult Breaker I R H Landing Light Figure 14 19 Landing Lights 14 43 ...

Page 328: ...L27ozo LjE20N ifL5D20 L5A20N L5B20N L5C20N i 56rC 3 9 60 i Cabin Lights Circuit Breaker 2 Instrument Panel Light Circuit Breaker 3 Rheostat 4 Reading Light Switch 5 Dome Light Switch 6 ReadingLight 7 Dome Light 8 Compass Light 9 Overhead Instrument Lights Figure 14 20 Dome and Reading Lights TG 1 thru TG 51 14 64 ...

Page 329: ... t L3D20 L3C20 c 2 c c c I I e C C C I iEl I L12C20N L Llzazow t l L12X20N _L 56TC 369 61 i Cabin Lights Circuit Breaker 7 Dome Light 2 Instrumene Panel Light 8 Compass Light Circuit Breaker 9 NotUsed 3 Rheostat 10 Resistor Re dinS Light Switch ii Switch 5 Dome LiShr Switch 12 0 h T Light 6 Reading Light 13 Clareshield Lights Figure 14 20 Dome and Reading Lights TG 52 thru TG 83 14 45 ...

Page 330: ...CZON 0 LJzAzo L27920 I L40C 0 L44820N dL28AZON G Ci L44420N I i Cabin Lighll C rcui Br ok r 2 Dom Ligh 3 P ading Light 4 Oom Lighl Srilch 5 Roading Liph Sri Lh 6 Compol and OAT Liph Sli ch 7 Mop Ligh Sritch 8 Map Ligh 9 Wh i Clock Ligh lo Ob T Liphe ii Clor lhi ld Conn ctor 12 Lioh Figure 14 21 Cabin and Map Lights ITG 84 and after 14 46 ...

Page 331: ...B L1 L66A2O 54 L66820 4Y L67A20N L67B20N IED WHIIE BLACX P i Crcui cak r 2 Pou r Uni and Conn aor 3 Slmb Ligh Figure 14 22 Bullock Strobe Light In nl ...

Page 332: ... WHITE WHITE WHITE Bmac alaac I I sLncK 8 m a s cl a a c I C g Rto nEo WHITE WHITE s Aa I I sLqac P A a c A C 1 Crcuit co e 2 Pown Unit 3 Pow unit bnrwcto 4 5 foil S rob Ught Tii a Ihob Light bn cm IH 7 Strob Light LH Figure 74 23 Hoskins Sbobe Light 1448 ...

Page 333: ...POWER P45F18 II P45G1B L76A18 LTI 20 L76818 El 176 320 BLACK B L76D20N i Ful 2 Court y Light Swilch I 3 NQM Bpggag Light Switch 4 Light 5 No B ggag Light l le Figure 14 24 Courtesy and Nose Baggage Lights TG 84 and after 14 49 ...

Page 334: ... L2M20 NOTE WIRING FURNISHED BY VENDOR IS NOT CODED 1 Circuit Breaker 56fC 369d2 2 Radio Light Rheostat 3 Instrument 4nd Edge Lights Rheostat 4 Landing Gear Visual Indicator Light 5 Rheostat Light 6 Tab Indicator Light 7 FuelSelector 8 Circuit Breaker And Switch Panel Lights Figure 14 25 Control Panel and Indicator Lights TG 1 thru TG 51 14 50 ...

Page 335: ...ED BY L2L20 VENDOR IS NOT CODED L2M20 56TC 369 63 2 Circuit Breaker 6 Tab Indicator Light 2 Radio Light Rheostat 7 FuelSelector 3 Instrument And Edge Lights Rheostat 8 Circuit Breaker And Switch Panel Lights 4 Landing Crear Visual Indicator Light 9 Switch Panel Light Rheostat 5 Rheostat Light 10 Switch Panel Light Assembly Figure 14 25 Control Panel Indicator Lights TG 52 thru TG 75 p lk50A ...

Page 336: ...820E131 L2A20 L26C20N L2820 _L 1 1 128C20 L31 A20 L28020 o 1 _L i L28E20 L28F20 1 Circuit Breaker 2 Aadio Instrument and Edge Light Rheostat 3 Dimming Transistor j6Tc 3692B9 4 Fuel Select Lights 5 Switch Panel Light Assembly 8 Tab Indicator Lights 7 Rheostat Light 8 Landing Gear Visual Indicator Figure 14 25 Control Panel Indicator Lights TG 77 thru TG 83 R Ik l ...

Page 337: ...D L13A20 PL4W20 L24A20 1A20N rn n L21A20N L23A20 L4X20 P Y L NOTE _I r j WIRING FURNISHED BY I VENDOR IS NOT CODED L _i 56TC 369 64 1 Circuit Breaker 6 L H Engine Lights 2 Rheostat 7 Oxygen Indicator Lights 3 Omni 2 Lights 8 Clock Light 4 Omni 81 Lights 9 Maplight 5 R H Engine Lights 10 Map Light Switch Figure 14 26 Instrument Panel Lights TG 1 thru TG 83 14 52 ...

Page 338: ... 4 Ammeter Lights 5 Fuel Pressure Lights 6 Manifold Pressure Lights 7 Tachometer Lights 10 m m m m m 8 Suction Light 9 Prop Anti Ice Light 10 Miuture Lights 11 Altimeter or Airspeed Lights L4S20 L4T20 e L4U20 L4V20 L4W20 L4X20 7 12 Engine Hour Meter or Flight Hour Meter Light 13 Altimeter Lights 14 Gyro Horizon Lights 15 Airspeed Lights 16 Clock Light 17 ADF Lights 18 and Bank Lights 19 Direction ...

Page 339: ... and a i r L2AZ0 5A EI g L4A20 ISA20N I OC IC RED BLACX nED a acK I i i Inltrum n Lioh l Circui Br ak r 2 El c ralvmin c n Lioh r Dim Control i Dimminp 4 In rt r 5 LH 5ri ch Pan i Lioh l Figure 14 27 Electroluminescent Panel Lights TG 84 and after 14 54 ...

Page 340: ...tWHITE LOAD OiL PRESS I P LO820 ELV TIE t tL32920N HEAD C1 n o g LJODZDN m N smcx i al cx CYL PRESS WHITE t LIIEZO LJICIO tWHITE TEMP JLACK IL32CZON L9C20 iFi FLAP L30E20N POS BLACKAILERON LH iWHITE all TEMP FUEL OTr WHITE LllF20 L30F20N IAB BL CI r9E2o FUEL PRESS I IWHITE llC20 VISUAL CG L30C2ON FUELSLACK OTr 1 Inr rumen Liph i Circuli Breai r 56rC 369 83 2 Dimming Zh o rat 3 Dimming Tranriilor J...

Page 341: ... C00RD WHITE WHITE WHITE WHITE i L78H20N L78 20N L78L20N L78M20N r Lt8AZON 1 L78GZ0N I L78020N A L7da 20N L78FZON L78E20N L78CZON L78B20N f f WHlrE n WHITEWI ITE AIR PRESS M HORIZWHI1E WHI E OYRO AIR SPEED CLOCK BLACK 8LACK BLACK BLACK BLACK t t i t j L57R20 L57P20 LS7MZO L57L20 R57520 57N20 56TC 369 84 i Inllrum n Ligh l Circuit 2 Oimming Rh orlo 3 Dimming 4 Omni Ligh r 5 Inr rum nt W dp Lighn W ...

Page 342: ...9A ON 1 Z 2 L 9B O TC 89 ond afl r rLS6aZON L PAZON P 6 I L56AZON it L5 laZ0 L5 1C20 R L54020 i i In rrum n Ligh l Circuli BI a r 2 Dim Cun rol 1 Oim Tronlirlor Clar ihi ld Conn ctor 5 Ini tvm nr Flood Ligh i Figure 14 30 Instrument Flood Lights TG 84 and after 14 57 ...

Page 343: ...01A22 26 n cszsAzz 12 2 1 o n Cs30Azz 10 11 EH 7 C C600A22 211 Jt Cj31A22 6 r 1 52 C552A22 7 F 1 49 C549A22 29 33 C532A22 13 C c c552czz A C 552 322 A A 1 20 C 520A22 30 13 C533A22 13 10 10 C5j2D22 B i I C569A22 12 14 1 26 C526A22 31 wt c53 A22 Is e I t C561A22N I C561A22N C564A20 it C568A22 12 13 1 8 C508A22 32 12 24 i Il L L C567A22 12 12 i8 F Cj62A22 33 jgt Cj36A22 12 18 1 46 C 546A22 C CS46A22...

Page 344: ...8 C17A18 VP 33 56TC 6P 36 i Pitch Trim Circuit Br o r 2 Control Column Coil d Cord 3 Trim Co ntrol Sritch 4 Trim Actuator 5 Conl ant 5o d R iltor 751110W 6 5 pac d Co ntrol P ii ito r 5 On Z 5 W I A DJ 7 Trim ON Off Sri ch 8 Bui Figure 14 32 Pitch Tri m TG 84 and after 14 59 ...

Page 345: ...28C20 H25A2P H27820 1 H23C20 r H26A20N A 8l H30A20N I 122420 IPI I H2 A20 H23B20 A B H29A20N I 56TC 369 67 1 Circuit Breaker 2 Surface Deice Switch 3 Surface Deice Relay 4 Surface Deice Time Delay Relay 5 R H Deice Valve 6 L H Deice Valve Figure 14 33 Surface Deice TG 1 thru TG 51 14 60 ...

Page 346: ...O COMPUTER I B I il H40A20N O H 30 B 2 O I HzlFaa i c I i LS IIElLS m H 30A20 A o_C9 H31A20N A 8 7 K H 2 9A 20 1 L 1 Cir cult Br eaker 2 Surface Deice Switch D H39 20N H i 3 Surface Deice Relay I 4 Surface Deice Time Delay Relay H29B20N 5 L H Variable Pressure Regulator 1_ 6 R H Variable Pressure Regulator 7 Ejector Distributor Valve WI TH H 14 AUTOPILOT 8 Auto piI o t Valve 9 Auto pil o t Valve 1...

Page 347: ... H24B 20 H19A20N 2 13 I 1 126 A20N H27A 20 P H23E20 1 C r cult B r eaker I H 2 3F 2 0 i A 2 Surf ac e De i c e Switch 3 Sur fac e Dei c e Relay Suriace Deice Time Delay Relay H33A 20N 1 C 5 L H Pressure Regulator 6 R H i r e s sure Regulator 7 Ejec tor Dis tributer Valve 567C 169 19 Figure 14 33 Surface Deice TG 84 and after 14 62 ...

Page 348: ...16 IltH3A16N X O c F H6B16 B C C n a n B 1 Circuit Breaker 2 Shunt 3 Ammeter 567C 369 69 4 Timer 5 R H Fi rew all Connec to r Engine Ac c e s so rie s 6 L H Firewall Connector E ngine Accesso ries 7 Brush Block 8 L H SLip Ring 9 L H Pro pe lie r De i c e Boot 10 R H Slip Ring 11 R H Pro pe lier Dei ce Boot Figure 1 4 34 Pro pel ler Deice TG 1 thru TG 83 14 63 ...

Page 349: ...FJ 1 H5 laN I B a P c I H7B14 c A X O 3 P 1 Circuit Breaker 2 Shuni 3 Ammeter 4 Timer 5 RH Firewall Connector Engine Accessories 6 L H Firewall Connector Engine Accessories 7 Brush Block 8 L H SLip Ring 9 L H Propeller Deice Boot 10 R H SLip Ring 11 R ii Propeller Deics Boot Figure 14 34 Propelier Deice TG 84 and after 14 64 ...

Page 350: ...71 i Circuit Breaker 2 Wing Detector Switch 3 Switch Heater 4 Stall Warning Horn Figure 14 35 Stall Warning Horn TG 1 thru TG 83 iP a TO PZTOT HEAT W7A20 W8A20N L i Circuit Breaker 2 Wing Detector Switch 3 Switch Heater 4 StallWarning Horn Figure 14 35 Stall Warning Horn TG 84 and after 14 65 ...

Page 351: ...r Figure 14 36 Cigarette Lighter BAC CAB E2c 20N E22X20E2dB20N E23A20 L21A20 E25A20 g K 1 I I 1 K E22B18 E25B18 E21B20 E23B18 nla7n rslAIP LH RH 1 Tachometer 561C 369 72 2 Firewall Connector Engine Accessories 3 Tachometer Generator Figure 14 37 Tachometer TG 1 thru TG 83 14 66 ...

Page 352: ...0 E43k20 In IQ K I i I 1 X E 6B20 E43B20 Et5B20 E42B20 il e A I Sl i TBJ Z B I IB r r RH i Tachometer 2 Firewall Connector En ine Accessories 3 Tachometer Generator Connector d Tachometer Probe 56 C 364 22 Figure 14 37 Tachometer TG 84 and after 14 67 ...

Page 353: ...73 i Circuit Breaker 2 L K Pitot Heater 3 RH Pitot Heater Optional Figure 14 38 Pitot Heat TG 1 thru TG 83 W7Azo TO STALL WARNING SWITCH HEATER d SA F5A20 FSA20 ii 6 FSrl20N 1 F4Aa0N L i Circuit Breaker a L H Pitot Heater 3 R Pitot Heater Figure 14 38 Pitot Heat TG 84 and after 14 68 ...

Page 354: ... En ine Hour Meter Figure 14 39 Engine Hour Meter TG 1 thru TG 83 I P r 6P F C M4A20 MUOX B I i Circuit Breaker Stall Warning 2 Oil PressureS vitch 3 Engine Hour Meter Figure 14 39 Engine Hour Meter TG 84 and after TG l hru TG a3 67C 369 17 TG 84 ond ai r Figure 14 40 Flight Hour Meter TG 84 and after 14 69 ...

Page 355: ...9 75 i Circuit Breaker 2 Turn and Slip indicator Figure 14 41 Turn and Slip Indicator ITG 1 thru TG 83 Ljl d f F3A20 IA n F2A20N C i Circuit Breaker 2 Turn and Slip Indicator Figure 14 41 Turn and Slip Indicator TG 84 and after 14 70 ...

Page 356: ...t Breaker Switch 2 L Fuel Vent Heater 3 RH Fuel Vent Heater Figure 14 42 Heated Fuel Vent TG 1 thru TG 83 L1 n HllOA20 L SA n H112A20 tWhite L 1 Circuit Breaker Switch 2 L H Fuel Vent Heater 3 R Fuel Vent Heater Figure 14 42 Heated Fuel Vent TG 84 and after 14 71 ...

Page 357: ... B A D C 1 4 9 10 2 3 8 7 6 5 H95A18 5 A HB1A18 m m H77B18 m MOT H75B18 H81A18 i Cabin Temperature Control Circuit Breaker 10 Fuse Automatic Heat 19 Heater Resistor 2 Ventilation Blower Circuit Breaker 11 Fuse Manual Heat 20 Overtemperature Safety Switch 5 7C 369 77 3 Air Valve Su itch 12 Temperature Control Rheostat 21 Heaterlgnitor 4 Diode 13 Landing Gear Up Limit Switch 22 Cabin Temperature Con...

Page 358: ...18 1 4 9 10 2 3 8 7 6 S B A IOI OB EhTD 6 E D C B A 6 I I95A18 B A D m H77B18 m MOT m H77S1 1 Cabin Temperature Control Circuit Breaker 10 Fuse Automatic Heat 19 Heater Resistor 2 Ventilation Blower Circuit Breaker 11 Fuse Manual Heat 20 Opertemperature Safety Switch 567C 369 76 3 Air V 1 e Switch 12 Temperature Control Rheostat 21 Heater Ignitor 22 Cabin Temperature Control Box 4 Diode 13 Landing...

Page 359: ...2 6 8 7 3 5 H95A18 B A 6 C El EIl H81A18 H77B18 m I I I IMOT m A EFFECTIVE H7751 H64A18N TG 52 THRU TG 62 1 Cabin Temperature Control Circuit Breaker 10 Fuse Automatic Heat 19 Heater Resistor 2 Ventilation Blower Circuit Breaker Il Fuse Manual Heat 20 Overtemperature Safety Switch 3 Air Valve Switch 12 Temperature Control Rheostat 21 Heaterlgnitor 4 Diode 13 Landing Gear Up Limit Switch 22 Cabin T...

Page 360: ... re uit B r eake r 1 O Resistor 2 i I e at e r C ont rol Circuit Breaker 1 1 Ov e rt e m pe r atu r e Safety Switch 3 Ve nt ilat ion Blowe r Relay 1 2 He at e r ignitor Swite h 4 Ventilation B lowe r 13 He at e r ignitor Air Valve Swite h 1 4 Ductstat Heat C ont rol 6 Heat e r Switch 1 5 Landing Gear Up Lim it S wite h 7 Landing Ge a r Down L im it Switch 1 6 He ate r Fuel Pu m p 8 Co m bu st i on...

Page 361: ...63B 18N L i Ventilation Blower Circuit Breaker r0 Resistor 2 Heater Control Circuit Breaker 11 Overtemperature Saiety Switch 3 Ventilation Blower Relay 12 Heater ignitor Switch i Ventilation Blower 13 HeaterSanitor 3 Air Valve Switch 14 Ductstat Heat Control 6 Heater Switch 15 Landing Gear Up Limit Switch 7 Landing Gear Down Limit Switch 16 Heater Fuel Pump 8 Combustion Blower 17 Heater Fuel Pump ...

Page 362: ...BLANK PAGE 14 77 ...

Page 363: ...2 Heater Solenoid Valve 23 Heater Fuel Pump 24 Combustion Blower 25 Heater Fuel PumD 26 Ductstat Heat Control 27 TemDerature Control Rheostat 28 Heater Air Conditioner Select Relay 29 Heater and Air Conditioner Cycle Relay 30 Hot Gas By Pass Solenoid Valve 31 Cabin Temperature Control Box 32 Cabin Air Temoerature Sensor 33 Outside Air Temperature Sensor 34 Heater Discharge Temperature Sensor 35 La...

Page 364: ... o H33A18 m H94D18 I I59A18 0 NC H94A18 HIGH 6 20 5 H45C16 J I39B18 I I H43A18N H45B1 m a H68A18 m BLACK AI TO H64Ar8n H63A18N 5 20 H93A18 GND NO H45D18 0 6 COOL I H60A18 0 L 1 BLACK m H60B18 H58B18 T H59B18 K105A18 C A 8 HGDCle 4 H441A18 L l v H11 6A18H107B18NH1SB1B HIGA1Ba re 3A H107A18 I I m H32A18 m H47A18ru H67A18 L b H34A18 m H33A18 I I I H32A18 hH69A1 z I H6 C18 H99A18 H56A18N II H79B18N P ...

Page 365: ...d18 H45f18 H94D18 H61C18 NC H94A18 I IIGH 6 20 c 5 114 jC 1 8 J H39B18 Ilt H43A18N BLACK H45 018 m H68A18 Eljj H4jD18 Q H64A18E H63A18Fu GNDNO 5 20 H93A18 4UTO b COUL L 1 H63A16 L BLACK m HfiUnlG H58Blfi II59B18 H105A18 6 A B L6 H106A18 H46B18 2F H46A18 r H60C18 H44A18 m 5A H107A18 h_ En I EO H32A18 m H107B18h L H47A181u H67plp I I I h H34A18 m H32A18 I _I bH69A1 H67D18 I I I mS t I H59D18 H99A18 ...

Page 366: ...Solenoid Valve 23 Heater Fuel Pump 24 Combustion Blower 25 Heater Fuel Pump 26 Ducts ta t Hea t Control 2 7 Temperature Contr ol Rh eo s ta t 28 Heater Air Conditioner Select Relay 29 He at er and Air Conditioner Cycle Relay 30 Hot Ga s By Pass Soleno id V alv e 3 1 Cabin T e mp e ra tur e Control Box 3 2 Cabin Air T e m pe ratur e S ens o r 33 Outside Air Temperature Sensor 34 Heater Discharge Te...

Page 367: ...oted in this shop manual guarantee that the item will reach the period are based on average usage and average environmental without malfunction as the aforementioned conditions factors cannot be controlled by the manufacturer SPECIAL CONDITIONS CAUTIONARY NOTICE NOTE Airplanes operated for Air Taxi or other than normal operation and airplanes operated in humid tropics or cold On Condition items ar...

Page 368: ...titute the O n co ndition requ irem ent Any pitting corrosion cracking distortion or visible wear noted during the seal replacement will also constitute the re qu ire m ent for an overhaul Nose Gear On condition Leaking or collapsed struts that cannot be corrected by seal replacement wi II constitute the On condition requirement Any pitting corrosion cracking distortion or visible wear noted durin...

Page 369: ...Raytheon Aircraft BEECH TURBO BARON 56TC AND A56TC SHOP MANUAL THIS FAG E I NTE NTIONALLY LE FT B LAN K Page 2 of 2 Oct 31 37 Temporary Revision No 15 1 ...

Page 370: ...ing Service Bulletin No 1 0 0 9 W E v e r y 1200 hours maximum 1600 hours per Engine controls On condition Engine vibration isolator mounts On condition Exhaust system On condition Starter Inspect at engine overhaul and overhaul or replace on condition Generator or Alternator On condition Oil cooler On condition replace when contaminated Propeller Every 1000 hours not to exceed 2 years ejr maximum...

Page 371: ...lves On condition Fuel selector valve Inspect every 500 hours Overhaul every 1000 hours Fuel pump engine driven Every 1600 hours Fuel boost pump Overhaul 800 hours Hose carrying flammable liquids When condition warrants at engine overhaul or 5 years from date of delivery whichever occurs first All other hoses On condition Float valve On condition INSTRUMENTS Turn and bank indicator On condition Al...

Page 372: ...ays On condition Voltage regulators On condition Heater vibrator points Every t000 hours of heater operation Starter Inspect at engine overhaul and overhaul or replace on condition Starter relay On condition Generator or alternator On condition UTILlTY SYSTEMS H 14 Autopilot servo air filter Replace every 1000 hours Cabin heater Pressure test every 500 hours of heater operation or every 1000 hours...

Page 373: ...Condenser blower brushes 500 hours Evaporator blower On condition Evaporator blower brushes 500 hours Oxygen regulator Every 7000 hours or 48 months Oxygen cylinder Hydrostatically test every 3 years replace every 12 years or LF 3S0 retills ICC Regulation MISCELLANEOUS Wing bolts Replace 10 yeats after the initial inspection or when condition warrants Sze Section i for inspection criterion 83 Ij j...

Page 374: ... accomplished within each 12 month period for compliance with the Federal Aviation Regulations To the extent that the airplane is operated in excess of 100 hours per year Beech Aircraft Corporation strongly recommends that the airplane be inspected at 100 hour intervals rather than annually The 100 hour interval between performance of the procedures specified herein should NEVER be exceeded by mor...

Page 375: ... and doors for security and security damage b Check cylinders for evidence of burned paint b Check wings fuselage and control surfaces for damage c Check intake and exhaust systems for leaks and security c Check windshield for cleanliness d Check baffles for security holes cracks d Check battery terminals and vent hoses for bending and close fit around cylinders security and obstructions e Check c...

Page 376: ...ure and temperature setting i Check propeller governor to operate at predetermined rpm settings d Correct fuel pressure reading j All seat belts are properly secured and the buckles e All lights work properly work correctly f Fuel quantity gages read correctly k Check magnetos for normal drop off g Fuel tank selectors work properly i Check idle speed adjustment h Heat and ventilating system operat...

Page 377: ...AUTION position Check condition and operation of complete landing gear system Do not operate the turbocharger if leaks exist in the ducting or if air cleaner is not filtering POWER PLANT efficiently Dust leaking into the turbocharger can damage the turbocharger and engine a Inspect all electrical wiring for general condition and proper anchorage v Check all flexible air ducts for deiaminarion I re...

Page 378: ...roper c Check condition and operation of all moveable travel controlsurfaces f Check instrument plumbing and wiring for leaks I d Check that the drain holes in the left and right Co dition and security upper wing fittings are open g Check windows for visibility cracks and distor e Check that static ports are free from obstructions tio f See Section 3 for wing bolt inspection criterion and h Check ...

Page 379: ...er plate and ounting oracket until the brush block is ference by operating the engine at near take off properly located power with the radio gear turned on if under these conditions noise or interference occurs when the i Estimate the contact angle of the brush block in deicer switch is ON and disappears when the s itch relation to the slip rings If this angle is not appro i is OFF refer to the tr...