2. To remove tee bar with assembled parts:
A.
Remove the access panel to the aft section of the fuselage.
B.
Relieve cable tension from the stabilator control cables at one of the stabilator cable turnbuckles
in the aft section of the fuselage.
C.
Relieve tension from the aileron control cables and chains at the turnbuckle that connects the
chains at the top of the tee bar.
D .
Disconnect the control chains from the control cables where the chains and cables join by removing
the cotter pins, nuts, bolts and bushings.
E.
If the control wheel assemblies have not been previously disconnected from the tee bar assembly,
separate the control wheel tubes at the flexible joints by removing the nuts, washers and bolts.
F.
Remove the tunnel plate just aft of the tee bar by laying back enough tunnel carpet to remove the
plate attachment screws.
G.
Remove the two aileron control cable pulleys attached to the lower section of the tee bar by
removing the pulley attachment bolt.
H.
Disconnect the stabilator control cables from the lower end of the tee bar assembly.
I.
Disconnect the necessary control cables, such as the propeller pitch control, mixture control, etc.,
that will allow the tee bar assembly to be removed.
J.
Remove the tee bar assembly by removing the attachment bolts with washers and nuts which arc
through each side of the floor tunnel, and lifting it up and out through the right side of the cabin.
INSTALLATION OF CONTROL COLUMN ASSEMBLY. (Refer to Figure 27-6.)
1. To install tee bar assembly:
A.
Swing the tee bar assembly into place from the right side of the cabin and secure with attachment
bolts, washers and nuts inserted through each side of the floor tunnel.
B .
Connect the stabilator control cables to the lower end of the tee bar with bolt, washer, nut and
cotter pin. Allow the cable ends free to rotate.
C.
Place the aileron control cables around the pulleys that attach to the lower section of the tee bar;
position pulleys and secure with bolt, washers and nut.
D.
Install the control wheel per Step 2.
E.
Place the control wheels in neutral (centered) position and install the aileron control chains on the
control wheel sprockets and idler cross-over sprockets. The turnbuckle must be centered between
the two control wheel sprockets.
F.
Loosen the connecting bolts of the idler sprockets to allow the chain to fit snug around the control
wheel sprockets and over the idler sprockets.
G.
Connect the aileron control cables to the ends of the chains with bolts, bushings, nuts and cotter
pins.
H.
Adjust the chain turnbuckle between the two control wheel sprockets to allow the control wheels
to be neutral and obtain proper cable tension as given in Figure 27-5. It may be necessary in
order to have both control wheels neutral to set the chain turnbuckle to neutralize the wheels and
then set cable tension with the turnbuckles located under the floor panel aft of the main spar.
Before safetying the turnbuckle, check that when the ailerons are neutral, the control wheels will
be neutral and the chain turnbuckle centered. Also the aileron bellcranks should contact their
stops before the control wheel hits its stop. Maintain .030 to .040 clearance between sprocket pin
and adjustable stop bolts on models having adjustable tee bar stops.
I.
Set stabilator cable tension with the turnbuckle in the aft section of the fuselage. Check safety of
all turnbuckles upon completion of adjustments.
PIPER AIRCRAFT
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
27-10-02
Page 27-12
Revised: June 20, 1995
1K14
Summary of Contents for SEMINOLE PA-44-180
Page 38: ...CHAPTER DIMENSIONS AND AREAS 1B14...
Page 49: ...CHAPTER LIFTING AND SHORING 1C1...
Page 53: ...CHAPTER LEVELING AND WEIGHING 1C5...
Page 58: ...CHAPTER TOWING AND TAXIING 1C10...
Page 62: ...CHAPTER PARKING AND MOORING 1C14...
Page 65: ...CHAPTER REQUIRED PLACARDS 1C17...
Page 70: ...CHAPTER SERVICING 1C22...
Page 98: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E2...
Page 108: ...CHAPTER ENVIRONMENTAL SYSTEM 1E12...
Page 189: ...CHAPTER AUTOFLIGHT 1H21...
Page 192: ...CHAPTER COMMUNICATIONS 1H24...
Page 202: ...CHAPTER ELECTRICAL POWER 1I10...
Page 228: ...CHAPTER EQUIPMENT FURNISHINGS 1J12...
Page 233: ...CHAPTER FIRE PROTECTION 1J17...
Page 238: ...CHAPTER FLIGHT CONTROLS 1J24...
Page 304: ...2A18 CHAPTER FUEL...
Page 325: ...2B17 CHAPTER HYDRAULIC POWER...
Page 357: ...2D1 CHAPTER ICE AND RAIN PROTECTION...
Page 414: ...CHAPTER LANDING GEAR 2F13...
Page 479: ...2I6 CHAPTER LIGHTS...
Page 488: ...2I16 CHAPTER NAVIGATION AND PITOT STATIC...
Page 503: ...2J7 CHAPTER OXYGEN...
Page 524: ...2K6 CHAPTER VACUUM...
Page 535: ...2K19 CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTIPURPOSE PARTS...
Page 546: ...INTENTIONALLY LEFT BLANK PA 44 180 180T AIRPLANE MAINTENANCE MANUAL 2L6 PIPER AIRCRAFT...
Page 547: ...2L7 CHAPTER STRUCTURES...
Page 582: ...CHAPTER DOORS 3A18...
Page 593: ...CHAPTER STABILIZERS 3B8...
Page 604: ...CHAPTER WINDOWS 3B22...
Page 611: ...CHAPTER WINGS 3C10...
Page 624: ...CHAPTER PROPELLER 3D1...
Page 643: ...CHAPTER POWER PLANT 3D21...
Page 667: ...CHAPTER ENGINE FUEL SYSTEM 3F1...
Page 681: ...CHAPTER IGNITION 3F16...
Page 712: ...CHAPTER ENGINE INDICATING 3H1...
Page 730: ...CHAPTER EXHAUST 3H19...
Page 734: ...CHAPTER OIL 3I1...
Page 743: ...CHAPTER STARTING 3I11...
Page 755: ...CHAPTER TURBINES 3J1...