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Cessna Aircraft Company
Model 177RG

Supplement No.

DP-014-14

Section 9
Supplements

Page 6

Revision 0

COMPONENTS INSTALLED DURING CHANGE

Item

Component

Weight

[lb]

Weight

[kg]

CG Arm

[in]

CG Arm

[m]

Moment

[lb-in]

Moment

[kG m]

KI 227 ADF Indicator

0,71

0,322

74,45

1,891

52,86

0,61

KR 87 ADF

3,20

1,452

70,68

1,795

226,18

2,61

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

Table 1 - Weight and longitudinal centre of gravity of installed components of the Bendix King ADF
system KR 87 on Cessna Model 177RG aircraft after change.

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Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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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