Schweizer 269C-1, Rotorcraft Flight Manual Supplement

Page 1: ...Rotorcraft Flight Manual For Schweizer 300CB Helicopter Model 269C 1 INSTRUMENT AVIONICS INSTALLATIONS 1 CSP C1 1A Date of Original Approval October 3 1995 Date of Rev 9 Approval Approved By Acting Ma...

Page 2: ...Apr 1996 30 17 Apr 1996 10 1 29 Mar 2001 31 21 May 1997 10 2 29 Mar 2001 32 09 Jan 1998 10 3 29 Mar 2001 33 23 Jul 1999 10 4 29 Mar 2001 34 23 Jul 1999 11 17 Apr 1996 35 23 Jul 1999 12 17 Apr 1996 36...

Page 3: ...ed to include KX 165 Hot Mic Transfer Channel Increment Switch KR87 KR 21 KMA 24H KI 229 KN 62A KCS55A and Avionics Master Switch Revised to include KI209 Indicator and Transmitter Receiver Audio Moni...

Page 4: ...This page is intentionally left blank SCHWEIZER MODEL 269C 1 HELICOPTER CSP C1 1A 4 FAA Approved 03 Oct 1995 Revised 02 Mar 2001...

Page 5: ...rocedures 4 1 KY 96A 196A VHF Comm Transceiver 4 2 KT 76A Transponder 4 2B GTX 320 320A Transponder 4 2C GTX 327 Transponder Oper Instructions 4 3 KX 155 165 VHF NAV COMM 4 4 Navigation Indicators KI...

Page 6: ...ter Switch 4 14 Transmitter Receiver and Audio Monitor Selector Switches 4 15 GNC 25 250XL 4 16 GPS 150 4 17 GPS 150XL 4 18 KLN 89B GPS 4 19 GNS 430 COMM NAV GPS Section V Performance Data Section VI...

Page 7: ...function of all installed equipment This supplement must be carried in the applicable basic FAA approved 300CB Model 269C 1 Rotorcraft Flight Manual when the rotorcraft is equipped with any of the ins...

Page 8: ...igation System a placard Garmin P N 161 00024 00 S A C P N 269A4646 265 or equivalent stating GPS limited to VRF use only must be installed in clear view and be easily readable by the pilot If this ai...

Page 9: ...l unnecessary electrical equipment should be turned OFF to conserve battery power Specific emergency procedures for avionics are provided in the individual operating instructions where applicable SCHW...

Page 10: ...itch is depressed on the side placarded ICS the crewmember with the footswitch has his microphone connected to the aircraft intercom system When the footswitch is depressed on the side placarded XMIT...

Page 11: ...96A COMM Transceiver TSO d MODES OF OPERATION A Frequency Mode Frequency selection is accomplished in the Standby Entry mode by changing the frequency display in the STBY window of the display with t...

Page 12: ...is successful The transponder code is entered by rotating the code control knobs During some operations ATC may request the pilot to IDENT which will require a momentary depressing of the IDENT push...

Page 13: ...only tests the reply light Pressing the IDENT button causes the special identification pulse to be added to any normal Mode A or Mode C replies and it lights the reply light for 20 seconds ON provides...

Page 14: ...e reply light there is instead a circled R that shows up on the lower left cor ner of the display for a reply indicator The IDENT button acti vates 18 seconds of IDENT and adds the word IDENT to the u...

Page 15: ...er minute selected in the Configuration mode This altitude display can be pilot configured to read flight level feet or meters When changing codes in ON or ALT do not pass through codes 0000 governmen...

Page 16: ...This page is intentionally left blank SCHWEIZER MODEL 269C 1 HELICOPTER CSP C1 1A 10 4 FAA Approved 03 Oct 1995 Revised 29 Mar 2001...

Page 17: ...round band edge is also utilized when in crementing or decrementing the KHZ portion of the STBY display To tune the radio to the desired operating frequency the desired frequency must be entered into...

Page 18: ...e the USE frequency to be placed in blind storage and the STBY frequency in the blind storage to be displayed in the USE window display In radial mode of operation the right hand win dow of NAV displa...

Page 19: ...The vol ume of voice ident can be adjusted by turning this knob Note If dual Nav s are installed a placard will be lo cated on the receiver and on the corresponding NAV in dicator to correlate the NA...

Page 20: ...NAV Indicators for use with the KX 155 KI 203 VOR LOC Indicator TSO d KI 208 VOR LOC Indicator TSO d KI 209 VOR LOC Indicator TSO d SCHWEIZER MODEL 269C 1 HELICOPTER CSP C1 1A 14 FAA Approved 03 Oct...

Page 21: ...v USE and STBY frequencies when momentarily toggled to CHAN Should the remote frequency transfer channel increment switch be come disabled manual operation of the avionics will be necessary to change...

Page 22: ...essage on the left side of the display will be illuminated and the indicator needle will point to the relative bearing of the selected station In order to tell if there is a sufficient signal for navi...

Page 23: ...nd active frequencies to be exchanged TIMERS A FLT ET Button If elapsed time ET is currently displayed the FLT ET button will cause the flight timer to be displayed Pressing this button again will exc...

Page 24: ...will roll over from 5 to 0 and under 0 to 5 With the knob pulled out the 1 s of seconds digit may be changed It rolls over from 9 to 0 and un der from 0 to 9 The larger knob modifies the minutes It ro...

Page 25: ...FLIGHT TIMER or ELAPSED TIMER Set and Reset ELAPSED TIMER ON OFF VOL control switch Frequency Select Knobs KI 227 ADF Indicator Note ADF bearing information may be displayed on KI 229 RMI Refer to KI...

Page 26: ...525A operation When the ADF receiver is tuned to a station the yellow ADF pointer indicates the magnetic heading to the station Thus if the pilot desires to fly toward the station he merely turns his...

Page 27: ...the compass card The servo drive com pass card displays heading information derived from ARINC type X Y Z compass headings The double pointer is dedicated solely to a ADF DC SIN COS source The single...

Page 28: ...SUFFICIENT SPIN DOWN TIME PRIOR TO ANY AIRCRAFT MOVEMENT Set the navigation receiver to the desired VOR LOC station and ro tate the course select knob to adjust the selected course pointer to the desi...

Page 29: ...tes the relative position of the selected course For backcourse operation set the course pointer to the FRONT INBOUND localizer course The deviation bar posi tion relative to the symbolic aircraft the...

Page 30: ...except the heading information will be solely derived from the KG 102A Gyro There will be no magnetic correction from the KMT 112 KA 51B Slaving Accessory And Controls If the KI 525A NAV flag appears...

Page 31: ...omentarily interrupted in GS T mode Nor mal operation is re established by switching to FREQ or RMT mode When the KN 62A is locked to a ground station range is displayed to the nearest 0 1 nautical mi...

Page 32: ...measured on a slant from aircraft to ground station and should not be confused with actual ground distance The difference between ground distance and slant range distance is smallest at low altitude...

Page 33: ...knob INT VOL Intercom volume control on the front panel This control af fects the volume of intercom only it does not affect the volume of the audio inputs selected with the pushbuttons When the outer...

Page 34: ...ystems The outer marker is normally positioned on the front localizer course near the point where the glideslope approach path intersects the minimum inbound altitude after the procedure turn Distance...

Page 35: ...the KR 21 marker sensitivity switch first be placed in high sensitivity position until aural and or lamp indication is received The control switch may be turned to low sensitivity to reduce the durat...

Page 36: ...es Switch A also simulta neously connects the selected transmitter audio to the aircraft headphones regardless of the position of headphones audio moni tor switches B C and D If installed Example When...

Page 37: ...s Both COMM 1 and COMM 2 receive audio will be heard on the aircraft headphones in this ex ample The receive audio of the communications system selected on the transmit selector switch can not be turn...

Page 38: ...key for more than two seconds will always tune the active frequency to 121 50 mhz emergency A TX will show up to the right of the active frequency during transmit The GNC 250 250XL will not transmit...

Page 39: ...ush to test its own lamp function IF there is a flashing light be side the STAT key repeated by the instrument panel mounted GPS MESSAGE light press the GPS 150 STAT status mes sage key once to read t...

Page 40: ...unction IF there is a flashing light beside the MSG key repeated by the instrument panel mounted GPS MESSAGE light press the GPS 150XL MSG key once to read the message and again to return to the previ...

Page 41: ...wed by three dashes or the present read ing of a connected HSI course arrow or other connected and switch selected remote omni bearing selector After equipment turn on and its self test it is necessar...

Page 42: ...ne is distance to destination waypoint The second line down may be waypoint name or ground speed depending upon which display page is selected The third line down usually says LEG or a three digit num...

Page 43: ...center and right hand side functions only as a GPS navigation receiver with moving map display The double ended arrow l key marked C is used to trade the COMM active and standby frequencies Pressing t...

Page 44: ...S page is cursor highlighted push the GPS PUSH CRSR knob and the ENT button is pressed this frequency is then transferred to the standby register of the COM or VLOC frequency display VOR LOC left righ...

Page 45: ...to nav igate directly there Pressing the OBS button allows the pilot to navigate along any chosen bearing to or radial from the waypoint like using the omni bearing selector for a VOR Press the CLR bu...

Page 46: ...unit for GNC250XL weighs 2 6 lbs and is lo cated at longitudinal arm 57 8 in the standard instrument panel The removable panel unit for GPS150 receiver weighs 2 1 pounds at 55 5 aft for a main instrum...