Cessna Cardinal RG 1974 Page 168 Owner'S Manual Download

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Cessna Aircraft Company
Model 177RG

Supplement No.

DP-014-17

Section 9
Supplements

Page 12

Revision 0

CREW
(LED
LIT)

Selected
Radios.
Pilot.
Copilot.
MUSIC
1.

Selected
Radios.
Copilot.
Pilot.
MUSIC 1.

Passengers
MUSIC 2.
(MUSIC 1 in
Dual
ADF)

Aircraft
radio
activity.
MKR
activity.
Pilot or
Copilot
ICS
activity.

ALL
(LED
OFF)

Selected
Radios.
Pilot.
Copilot.
Passeng
ers.
MUSIC
1.

Selected
Radios.
Pilot.
Copilot.
Passenger
s.
MUSIC 1.

Selected
Radios.
Pilot.
Copilot.
Passengers
MUSIC 1.

Aircraft
radio
activity.
MKR
activity.
ICS
activity.

MONO/STEREO HEADSET

The use of stereo headsets is highly recommended. If

monaural headsets are plugged into stereo jacks that do not

have a switch installed the unit will not be damaged. Use of a

monaural headset in a stereo jack shorts the right headset

channel output to ground. A person listening on a monaural

headset will hear only the left channel from the GMA 340 in

both ears. If a monaural headset is used at one of the

passenger positions, any other passenger listening on a

stereo headset will hear audio in their left ear only, unless their

headset has a stereo/mono switch and it is set for mono. In

units without Mod 4 incorporated, if the pilot uses a monaural

headset in a stereo jack, no audio will be heard during failsafe

UNCONTROLLED

COPY

WHEN

DONLOADED

Summary of Contents for Cardinal RG 1974

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Page 93: ...nts Section Section 9 of the Cessna 177RG Cardinal RG Pilot s Operating Handbook Information in this supplement either adds to supersedes or deletes information in the basic Pilot s Operating Handbook...

Page 94: ...Revised Pages Description of Revision Approved Date of Revision 0 1 7 Initial edition 10 05 2018 LIST OF EFFECTIVE PAGES Page Number Revision Date of Revision 1 0 10 05 2018 2 0 10 05 2018 3 0 10 05...

Page 95: ...or later applicable revision should be referred to for operating instructions SECTION 2 LIMITATIONS WARNING For safety reasons GTN 650 operational procedures must be learned on the ground WARNING To r...

Page 96: ...or later applicable revision and Garmin GTN 625 635 650 Pilot s Guide P N 190 01004 03 revision M or later applicable revision Garmin GTN 6XX Cockpit Reference Guide and Garmin GTN 625 635 650 Pilot...

Page 97: ...ob Controls volume of the COM and NAV radios Press to use the IDENT function of the NAV radio Pressing and holding the volume knob will change the frequency to emergency frequency Large and Small Knob...

Page 98: ...m Moment lb in Moment kG m 1 GTN 650 NAV COM with rack and backplate 7 05 3 198 70 6 1 793 497 73 5 73 2 GTN 650 Antenna 0 46 0 209 100 2 54 46 0 53 SUMMARY 7 51 3 407 543 73 6 26 Table 1 Weight and...

Page 99: ...01004 04 revision L or later applicable revision and Garmin GTN 625 635 650 Pilot s Guide P N 190 01004 03 revision M or later applicable revision Operation of the Garmin GTN 650 system is described...

Page 100: ...U N C O N T R O L L E D C O P Y W H E N D O N L O A D E D...

Page 101: ...plements Section Section 9 of the Cessna 177RG Cardinal RG Pilot s Operating Handbook Information in this supplement either adds to supersedes or deletes information in the basic Pilot s Operating Han...

Page 102: ...Description of Revision Approved Date of Revision 0 1 9 Initial edition 10 05 2018 LIST OF EFFECTIVE PAGES Page Number Revision Date of Revision 1 0 10 05 2018 2 0 10 05 2018 3 0 10 05 2018 4 0 10 05...

Page 103: ...revision should be referred to for operating instructions SECTION 2 LIMITATIONS No Change SECTION 3 EMERGENCY PROCEDURES No Change SECTION 4 NORMAL PROCEDURES Normal operating procedures are describe...

Page 104: ...or ON keys or by a remote avionics master switch After power on a start up page is displayed while the unit performs a self test Figure 1 Garmin GTX 330 Transponder SECTION 6 WEIGHT AND BALANCE Weigh...

Page 105: ...ent lb in Moment kG m 1 GTX 330 Transponder with rack and connectors 4 19 1 901 70 6 1 793 295 81 3 41 2 KA 61 Antenna 0 40 0 181 70 74 1 797 28 3 0 33 SUMMARY 4 59 2 082 324 11 3 74 Table 1 Weight an...

Page 106: ...tandby mode When in standby mode the transponder will not reply to any interrogations ON In this mode the transponder replies to interrogations as indicated by the Reply Symbol Replies do not include...

Page 107: ...ata entry restoring the previous code You may press the CLR key up to five seconds after code entry is complete to return the cursor to the fourth digit The numbers 8 and 9 are not used for code entry...

Page 108: ...s Also displays Outside Air Temperature Density Altitude Contrast Display and ADS B Operation START STOP Starts and stops the Altitude Monitor Count Up Count Down and Flight timers CRSR Initiates Flig...

Page 109: ...entry dialog if the ALLOW PILOT TO EDIT FLT ID option is enabled during installation configuration PRESSURE ALT Displays the altitude data supplied to the GTX 330 in feet hundreds of feet i e flight l...

Page 110: ...U N C O N T R O L L E D C O P Y W H E N D O N L O A D E D...

Page 111: ...ents Section Section 9 of the Cessna 177RG Cardinal RG Pilot s Operating Handbook Information in this supplement either adds to supersedes or deletes information in the basic Pilot s Operating Handboo...

Page 112: ...Revision 0 1 14 Initial edition 10 05 2018 LIST OF EFFECTIVE PAGES Page Number Revision Date of Revision 1 0 10 05 2018 2 0 10 05 2018 3 0 10 05 2018 4 0 10 05 2018 5 0 10 05 2018 6 0 10 05 2018 7 0...

Page 113: ...e P N 190 00356 00 revision K or later applicable revision should be referred to for operating instructions SECTION 2 LIMITATIONS Limitations 1 The use of the Garmin GNS 430W system is not permitted f...

Page 114: ...tified as a NON WGS84 WPT by a system message NON WGS84 WPT waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS known as WGS84 a...

Page 115: ...is an aid to navigation and is designed to facilitate the use of authorized government charts not replace them Land and water data is provided only as a general reference to your surroundings The posi...

Page 116: ...ary means is not permitted for the following instrument approaches using GPS guidance LNAV Lateral Navigation approach LNAV V GPS approach using published LNAV minima L VNAV Lateral Navigation and Ver...

Page 117: ...30W system controls POWERING ON THE UNIT 1 Turn the COM power volume knob clockwise to turn the unit on and set the desired radio volume 2 The Main and GPS software version page appears briefly follow...

Page 118: ...the ENT key 5 When the GPS receiver has acquired a sufficient number of satellites to determine a position the Map Page will automatically appear showing your present position The Garmin GNS 430W syst...

Page 119: ...rsor around the page FREQUENCY SELECTION 1 If the tuning cursor is not currently in the desired window COM or VLOC press the small left knob momentarily to switch the highlight between the COM and VLO...

Page 120: ...s Page 10 Revision 0 SECTION 5 PERFORMANCE No Change SECTION 6 WEIGHT AND BALANCE Weight and longitudinal centre of gravity of installed components of the Garmin GNS 430W system on Cessna Model 177RG...

Page 121: ...Moment lb in Moment kG m 1 GNS 430W NAV COM GPS with rack and backplate 6 19 2 808 70 6 1 793 437 01 5 04 2 GNS 430W Antenna 0 46 0 209 100 2 54 46 0 53 SUMMARY 6 65 3 017 483 01 5 57 Table 1 Weight a...

Page 122: ...disable the ident tone The large left knob COM VLOC is used to tune the megahertz MHz value to the left of the decimal point of the standby frequency for the communications transceiver COM or the VLOC...

Page 123: ...changes which relate to the currently displayed page The clear key CLR is used to erase information or cancel an entry Press and hold this key to immediately display the Default Navigation Page regard...

Page 124: ...a waypoint using the OBS Page or an external OBS selector on your HSI or CDI The message key MSG is used to view system messages and important warnings and requirements The flight plan key FPL allows...

Page 125: ...d in the Supplements Section Section 9 of the Cessna 177RG Cardinal RG Pilot s Operating Handbook Information in this supplement either adds to supersedes or deletes information in the basic Pilot s O...

Page 126: ...Description of Revision Approved Date of Revision 0 1 9 Initial edition 10 05 2018 LIST OF EFFECTIVE PAGES Page Number Revision Date of Revision 1 0 10 05 2018 2 0 10 05 2018 3 0 10 05 2018 4 0 10 05...

Page 127: ...ttitude indicator SECTION 2 LIMITATIONS Limitations 1 Information provided by the BF Goodrich 1100 14 attitude indicator is secondary indication Attitude indication provided by the BF Goodrich 1100 14...

Page 128: ...ged position may be evident but is not abnormal 1 Apply power to the indicator Note that power flag stows out of view Allow two minutes for presentation stabilization 2 Rotate the airplane adjustment...

Page 129: ...should be momentarily caged after the airplane is returned to level flight 1 Adjust the miniature airplane to obtain desired pitch attitude presentation after take off SECTION 5 PERFORMANCE No Change...

Page 130: ...Component Weight lb Weight kg CG Arm in CG Arm m Moment lb in Moment kG m 1 1100 14 Attitude Indicator 2 70 1 225 74 2 1 885 200 34 2 31 Table 1 Weight and longitudinal centre of gravity of installed...

Page 131: ...s pitch and roll displays that are mechanically linked to a spinning mass gyroscope The horizon bar moves behind the symbolic airplane Precession error is corrected by pulling the PULL TO CAGE knob Fi...

Page 132: ...roll and pitch gimbals in caged position 5 Airplane Adjustment Knob Turning the knob moves the miniature airplane up and down a minimum of 4 re lative to the middle position 6 Horizon Line Indicates...

Page 133: ...light by the actuation of the caging system Taxiing Errors A pitch and roll indicator display error of approximately 1 will occur during a sudden 90 gro und turn A pitch indicator display error of app...

Page 134: ...U N C O N T R O L L E D C O P Y W H E N D O N L O A D E D...

Page 135: ...ble and must be inserted in the Supplements Section Section 9 of the Cessna 177RG Cardinal RG Pilot s Operating Handbook Information in this supplement either adds to supersedes or deletes information...

Page 136: ...EVISIONS Rev No Revised Pages Description of Revision Approved Date of Revision 0 1 5 Initial edition 10 05 2018 LIST OF EFFECTIVE PAGES Page Number Revision Date of Revision 1 0 10 05 2018 2 0 10 05...

Page 137: ...CO detector indicates elevated cabin CO levels CO is an odorless toxic gas present in engine exhaust which causes headaches drowsiness and possible loss of consciousness CO levels may become elevated...

Page 138: ...sor Avoid use of solvents detergents or aerosol sprays near the sensor Temporarily tape off openings in top and bottom of sensor housing when cleaning cabin interior Figure 1 B196 carbon monoxide dete...

Page 139: ...s of the C696 1 carbon monoxide detector and B196 carbon monoxide detector lamp The B196 carbon monoxide detector lamp is installed in the Instrument panel The C696 1 carbon monoxide detector is insta...

Page 140: ...U N C O N T R O L L E D C O P Y W H E N D O N L O A D E D...

Page 141: ...le and must be inserted in the Supplements Section Section 9 of the Cessna 177RG Cardinal RG Pilot s Operating Handbook Information in this supplement either adds to supersedes or deletes information...

Page 142: ...LOG OF REVISIONS Rev No Revised Pages Description of Revision Approved Date of Revision 0 1 4 Initial edition 10 05 2018 LIST OF EFFECTIVE PAGES Page Number Revision Date of Revision 1 0 10 05 2018 2...

Page 143: ...raft prepared by Drabpol Sp Jawna P Drabczy ski i Wsp lnik company SECTION 2 LIMITATIONS No Change SECTION 3 EMERGENCY PROCEDURES No Change SECTION 4 NORMAL PROCEDURES Ohmite Rheostats RES10R cabin li...

Page 144: ...ES10R potentiometer is a simple knob that provides a variable resistance to control cabin lighting dimming Turning the shaft of the potentiometer change the amount of resistence on either side of the...

Page 145: ...be inserted in the Supplements Section Section 9 of the Cessna 177RG Cardinal RG Pilot s Operating Handbook Information in this supplement either adds to supersedes or deletes information in the basi...

Page 146: ...S Rev No Revised Pages Description of Revision Approved Date of Revision 0 1 6 Initial edition 10 05 2018 LIST OF EFFECTIVE PAGES Page Number Revision Date of Revision 1 0 10 05 2018 2 0 10 05 2018 3...

Page 147: ...eries on Cessna Model 177RG aircraft prepared by Drabpol Sp Jawna P Drabczy ski i Wsp lnik company SECTION 2 LIMITATIONS No Change SECTION 3 EMERGENCY PROCEDURES No Change SECTION 4 NORMAL PROCEDURES...

Page 148: ...ge 4 Revision 0 SECTION 5 PERFORMANCE No Change SECTION 6 WEIGHT AND BALANCE Weight and longitudinal centre of gravity of installed Honeywell Hobbs hour meter indicator 85000 Series on Cessna Model 17...

Page 149: ...Component Weight lb Weight kg CG Arm in CG Arm m Moment lb in Moment kG m 1 Hobbs hour meter 0 50 0 227 74 7 1 897 37 35 0 43 Table 1 Weight and longitudinal centre of gravity of installed Honeywell H...

Page 150: ...lements Page 6 Revision 0 SECTION 7 SYSTEMS DESCRIPTION The Honeywell Hobbs hour meter indicator 85000 Series display the measurement of the aircraft engine operation time SECTION 8 HANDLING AND MAINT...

Page 151: ...be inserted in the Supplements Section Section 9 of the Cessna 177RG Cardinal RG Pilot s Operating Handbook Information in this supplement either adds to supersedes or deletes information in the basic...

Page 152: ...S Rev No Revised Pages Description of Revision Approved Date of Revision 0 1 6 Initial edition 10 05 2018 LIST OF EFFECTIVE PAGES Page Number Revision Date of Revision 1 0 10 05 2018 2 0 10 05 2018 3...

Page 153: ...LIMITATIONS Limitations Information provided by the Falcon Gauge model ALTN3ME 2 altimeter indicator is secondary indication Altimeter indication provided by the Falcon Gauge model ALTN3ME 2 altimeter...

Page 154: ...ters reading with barometric window millibars reading Figure 1 Falcon Gauge model ALTN3ME 2 altimeter indicator SECTION 5 PERFORMANCE No Change SECTION 6 WEIGHT AND BALANCE Weight and longitudinal cen...

Page 155: ...CHANGE Item Component Weight lb Weight kg CG Arm in CG Arm m Moment lb in Moment kG m 1 ALTN3ME 2 Altimeter 0 50 0 227 74 1 88 37 0 43 Table 1 Weight and longitudinal centre of gravity of installed Fa...

Page 156: ...Section 9 Supplements Page 6 Revision 0 SECTION 7 SYSTEMS DESCRIPTION Falcon Gauge model ALTN3ME 2 altimeter indicator is standby pressure 2 1 4 altimeter SECTION 8 HANDLING AND MAINTENANCE No Change...

Page 157: ...plements Section Section 9 of the Cessna 177RG Cardinal RG Pilot s Operating Handbook Information in this supplement either adds to supersedes or deletes information in the basic Pilot s Operating Han...

Page 158: ...Revision 0 1 14 Initial edition 10 05 2018 LIST OF EFFECTIVE PAGES Page Number Revision Date of Revision 1 0 10 05 2018 2 0 10 05 2018 3 0 10 05 2018 4 0 10 05 2018 5 0 10 05 2018 6 0 10 05 2018 7 0...

Page 159: ...IMITATIONS No Change SECTION 3 EMERGENCY PROCEDURES No Change SECTION 4 NORMAL PROCEDURES Normal operating procedures are described in the Garmin GMA 340 audio panel Pilot s Guide P N 190 00149 10 rev...

Page 160: ...left small knob 5 7 controls ON OFF function 1 Marker Beacon Lights 2 Marker Beacon Receiver Audio Select Mute Button 3 Marker Beacon Receiver Sensitivity Indicator LEDs 4 Marker Beacon Receiver Sens...

Page 161: ...Mic Selection Buttons 15 Split COM Button 16 Aircraft Radio Audio Selection Buttons NAV1 NAV2 DME ADF 17 Annunciator Test Button 18 Locking Screw Access 19 Photocell Automatic Annunciator Dimming SECT...

Page 162: ...t kG m 1 GMA 340 Audio Panel with rack and connectors 1 76 0 798 72 4 1 839 127 42 1 47 2 Cobham Comant CI 102 Marker beacon antenna 0 6 0 272 105 2 2 672 63 12 0 727 SUMMARY 2 36 1 07 190 54 2 197 Ta...

Page 163: ...tive com audio is always heard on the headphones Additionally each audio source can be selected independently by pressing COM 1 COM 2 or COM 3 13 When selected in this way they remain active as audio...

Page 164: ...normal Split COM operation Note If the COM radios utilize a transmit interlock system the Split COM function may require that this feature is enabled Refer to the radio s installation manual for guida...

Page 165: ...the PA function Pilot and copilot PA microphone speaker levels are adjustable through an access hole in the top of the unit AUXILIARY ENTERTAINMENT INPUTS The GMA 340 and 340H provide two stereo ente...

Page 166: ...input six total has a dedicated VOX circuit to ensure that only the active microphone s is are heard when squelch is broken This represents a vast improvement over single gate systems and reduces the...

Page 167: ...l The passengers are on their own intercom channel and can communicate with each other but cannot communicate with the crew or hear the aircraft radios ALL mode allows full intercom communication betw...

Page 168: ...dsets is highly recommended If monaural headsets are plugged into stereo jacks that do not have a switch installed the unit will not be damaged Use of a monaural headset in a stereo jack shorts the ri...

Page 169: ...al marker beacon functions the GMA 340 provides an audio muting function The LEDs illuminate and an associated keyed tone is heard when MKR audio is selected when the aircraft passes over a 75 MHz mar...

Page 170: ...tion is similar to selecting any other audio source on the GMA 340 If the second button press occurs while marker beacon signal is received then the marker audio is muted but not deselected The button...

Page 171: ...st be inserted in the Supplements Section Section 9 of the Cessna 177RG Cardinal RG Pilot s Operating Handbook Information in this supplement either adds to supersedes or deletes information in the ba...

Page 172: ...Description of Revision Approved Date of Revision 0 1 9 Initial edition 10 05 2018 LIST OF EFFECTIVE PAGES Page Number Revision Date of Revision 1 0 10 05 2018 2 0 10 05 2018 3 0 10 05 2018 4 0 10 05...

Page 173: ...Limitations 1 Information provided by the Insight Avionics G4 secondary engine monitor system is advisory only Engine parameters provided by the Insight Avionics G4 engine monitor system are not aircr...

Page 174: ...ed fuel loss from leakage fuel vent overflow or theft will of course produce erroneous results Be sure to cross reference the information on the primary fuel quantity gauges 3 Check Flight Manual Pilo...

Page 175: ...after starting the engine the white EGT bar graph columns will begin to appear on the system display Each white column corresponds to the Exhaust Gas Temperature EGT of a cylinder The columns are num...

Page 176: ...loads turbulence and landing shock Integrates and logs data from system TAS Air Data and GPS for the complete picture SD Card stores all engine air winds aloft and fuel data in PC compatible form Spec...

Page 177: ...r aircraft manufacturer Each aircraft s limits are published in the Type Certificate or Flight Manual Figure 1 Insight Avionics G4 controls SECTION 5 PERFORMANCE No Change SECTION 6 WEIGHT AND BALANCE...

Page 178: ...cator 0 50 0 227 75 1 905 37 5 0 43 2 Engine Temperature Probes with Components total 2 07 0 939 27 0 686 55 89 0 64 3 Engine Monitoring System Wiring Harness 2 20 0 998 59 1 499 129 8 1 50 SUMMARY 4...

Page 179: ...RIPTION Refer to the Insight Avionics G Series Pilot s Guide revision 1 or later applicable revision Operation of the Insight Avionics G4 engine monitor system is described in the Insight Avionics G S...

Page 180: ...U N C O N T R O L L E D C O P Y W H E N D O N L O A D E D...

Page 181: ...be inserted in the Supplements Section Section 9 of the Cessna 177RG Cardinal RG Pilot s Operating Handbook Information in this supplement either adds to supersedes or deletes information in the basi...

Page 182: ...edition 10 05 2018 LIST OF EFFECTIVE PAGES Page Number Revision Date of Revision 1 0 10 05 2018 2 0 10 05 2018 3 0 10 05 2018 4 0 10 05 2018 5 0 10 05 2018 6 0 10 05 2018 7 0 10 05 2018 8 0 10 05 201...

Page 183: ...ating instructions SECTION 2 LIMITATIONS No Change SECTION 3 EMERGENCY PROCEDURES EMERGENCY OPERATION If the KI 525 input power warning flag appears the compass system has experienced a power failure...

Page 184: ...the KI 525A compass card may indicate a failure in the slaving system and may not necessarily be annunciated by the HDG flag If a slaving failure should occur the SLAVE IN button on the KA 51Ashould...

Page 185: ...ll times and should be referred to for operating instructions OPERATING INSTRUCTIONS 1 Until power is applied to the KCS 55A System and the directional gyro is up to speed a red flag labeled HDG will...

Page 186: ...t of the KI 525A Indicator In operation this warning flag will be visible whenever an inadequate navigation signal is being received 6 For normal navigation set the NAV receiver to the desired VOR or...

Page 187: ...d the symbolic aircraft gives a true picture of where your aircraft is located with respect to the Localizer course Following this procedure provides the correct sensing whether flying a front or back...

Page 188: ...ect to the display 1 Lubber Line A fixed white marker at the top of the display that indicates aircraft magnetic heading on the Compass Card 2 To From Indicator Indicates the direction to the VOR stat...

Page 189: ...Pointer Chartreuse triangular pointers on either side of the display Represents the actual aircraft deviation from the glideslope path When unusable glideslope information is present the glideslope p...

Page 190: ...e side or the other Since the entire VOR and Localizer display rotates with the Compass Card the angular relationship between the Deviation Bar and the Symbolic Aircraft provides a pictorial symbolic...

Page 191: ...quadrant of the display whenever an unusable VOR or Localizer signal is being received Figure 2 KA 51A controls Slaving Meter This meter indicates the difference between the displayed heading and the...

Page 192: ...ght to eliminate left compass card error Counterclockwise Adjustment When the system is in the free gyro mode the counterclockwise manual heading drive switch will rotate the compass card to the left...

Page 193: ...Flux Valve with mounting tray 1 54 0 699 112 2 845 172 48 1 99 3 KG 102A Directional Gyro with antivibration mount 4 81 2 182 202 92 5 154 976 05 11 25 4 KA 51A Slaving Accessory 0 20 0 091 74 35 1 88...

Page 194: ...ning the display functions of the standard Directional Gyro the VOR and LOC deviation indicator with Glideslope display The KA 51A Slaving Control and Compensator Unit provides selecting the slaved gy...

Page 195: ...m power is present The fast slaving mode is initiated when power is applied and is switched to the slow slave mode when the slaving error is reduced to zero The fast slave rate is 180 degree minute Th...

Page 196: ...ope path with respect to the aircraft The position of the deviation bar with respect to the symbolic aircraft indicates the relative position of the selected course For backcourse operation set the co...

Page 197: ...not being received A continuous large deflection of the Slaving Meter or large discrepancies between the Magnetic Compass and the KI 525A Compass Card may indicate a failure in the slaving system If...

Page 198: ...U N C O N T R O L L E D C O P Y W H E N D O N L O A D E D...

Page 199: ...upplements Section Section 9 of the Cessna 177RG Cardinal RG Pilot s Operating Handbook Information in this supplement either adds to supersedes or deletes information in the basic Pilot s Operating H...

Page 200: ...ion of Revision Approved Date of Revision 0 1 10 Initial edition 10 05 2018 LIST OF EFFECTIVE PAGES Page Number Revision Date of Revision 1 0 10 05 2018 2 0 10 05 2018 3 0 10 05 2018 4 0 10 05 2018 5...

Page 201: ...TION 2 LIMITATIONS No Change SECTION 3 EMERGENCY PROCEDURES No Change SECTION 4 NORMAL PROCEDURES Normal operating procedures are described in the Bendix King Silver Crown Plus Avionics Systems Pilot...

Page 202: ...ting feature of the KR 87 will cause the audio output to be muted unless the receiver is locked onto a valid station This reduces interstation noise and aids the pilot in identifying usable stations I...

Page 203: ...age 5 Revision 0 Figure 1 KI 227 01 control functions SECTION 5 PERFORMANCE No Change SECTION 6 WEIGHT AND BALANCE Weight and longitudinal centre of gravity of installed components on Cessna Model 177...

Page 204: ...t kG m 1 KI 227 ADF Indicator 0 71 0 322 74 45 1 891 52 86 0 61 2 KR 87 ADF 3 20 1 452 70 68 1 795 226 18 2 61 3 KA 44B ADF Antenna 2 80 1 27 105 2 2 672 294 56 3 39 SUMMARY 6 71 3 044 573 6 6 61 Tabl...

Page 205: ...upted carrier for identification purposes A Beat Frequency Oscillator BFO function is provided to permit these stations to be more easily identified Pushing the BFO switch will cause a 1000Hz tone to...

Page 206: ...0 and roll under when turning the knob counterclockwise at 0 to 9 With the small knob pulled out the 1 s digit may be set Its operation is the same as for the 10 s digit Turning the large knob change...

Page 207: ...be displayed until a value of 59 minutes and 59 seconds is reached On the next count the display will shift to hours and minutes Elapsed Timer This timer has two modes Count Up and Count Down When pow...

Page 208: ...hing for 15 seconds after a number is set in or until the RST FLT ET or FRQ button is pressed The number preset will remain unchanged until the RST button is pressed When the RST button is pressed aft...

Page 209: ...e inserted in the Supplements Section Section 9 of the Cessna 177RG Cardinal RG Pilot s Operating Handbook Information in this supplement either adds to supersedes or deletes information in the basic...

Page 210: ...Description of Revision Approved Date of Revision 0 1 9 Initial edition 10 05 2018 LIST OF EFFECTIVE PAGES Page Number Revision Date of Revision 1 0 10 05 2018 2 0 10 05 2018 3 0 10 05 2018 4 0 10 05...

Page 211: ...perating instructions SECTION 2 LIMITATIONS Information provided by the Bendix King KI 209 VOR LOC Glideslope indicator is not aircraft primary navigation information and in case of any discrepancy pi...

Page 212: ...th card on which the desired course is selected The course selected serves as a reference for all VOR indications The reciprocal course is identified under the bottom course index VOR LOC DEVIATION IN...

Page 213: ...ideslope signal is unreliable or the receiver has malfunctioned Figure 1 KI 209 Control Functions SECTION 5 PERFORMANCE No Change SECTION 6 WEIGHT AND BALANCE Weight and longitudinal centre of gravity...

Page 214: ...mponent Weight lb Weight kg CG Arm in CG Arm m Moment lb in Moment kG m 1 KI 209 VOR LOC Indicator 1 19 0 54 72 65 1 845 86 45 1 Table 1 Weight and longitudinal centre of gravity of installed Bendix K...

Page 215: ...The intercept angle should be reduced as the deviation needle approaches an on course condition center to prevent excessive course bracketing To determine the bearing and fly To a selected VOR statio...

Page 216: ...utbound on the front course approach corrections are made away from the needle deflection The localizer course width is narrow compared to VOR course width and requires much smaller course corrections...

Page 217: ...pe needle deflects upward the aircraft is below the glideslope and must climb to center the needle If the needle deflects downward the aircraft is above the glide path and must descend to remain on th...

Page 218: ...U N C O N T R O L L E D C O P Y W H E N D O N L O A D E D...

Page 219: ...nd must be inserted in the Supplements Section Section 9 of the Cessna 177RG Cardinal RG Pilot s Operating Handbook Information in this supplement either adds to supersedes or deletes information in t...

Page 220: ...d Pages Description of Revision Approved Date of Revision 0 1 8 Initial edition 10 05 2018 LIST OF EFFECTIVE PAGES Page Number Revision Date of Revision 1 0 10 05 2018 2 0 10 05 2018 3 0 10 05 2018 4...

Page 221: ...d be referred to for operating instructions SECTION 2 LIMITATIONS No Change SECTION 3 EMERGENCY PROCEDURES No Change SECTION 4 NORMAL PROCEDURES Normal operating procedures are described in the Bendix...

Page 222: ...the display shows range and frequency In Ground Speed Time to Station GS T mode the KN 62A holds the last internally selected frequency and displays range speed and time to station The frequency hold...

Page 223: ...ure 2 KN 62A ground speed time to station mode Figure 3 KN 62A remote mode SECTION 5 PERFORMANCE No Change SECTION 6 WEIGHT AND BALANCE Weight and longitudinal centre of gravity of installed component...

Page 224: ...in CG Arm m Moment lb in Moment kG m 1 KN 62A DME 2 60 1 179 70 95 1 802 184 47 2 13 2 KA 61 DME Antenna 0 40 0 181 70 74 1 797 28 3 0 33 SUMMARY 3 1 36 207 77 2 46 Table 1 Weight and longitudinal cen...

Page 225: ...djusts the brightness of the display to compensate for changes in ambient light level The dimming is controlled by a photocell mounted behind the front panel to the left of the display Backlighting of...

Page 226: ...ft 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 and long range These distances m...

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