Garmin GFC 500 Manual Download Page 3

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190-02291-06 Rev. 2

AFMS

– GFC 500 Autopilot in Textron 182 Series

Page i

Garmin International, Inc

Log of Revisions

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT

GFC 500 Autopilot with ESP

Installed in

Textron Aviation 182E / 182F / 182G / 182H / 182J / 182K / 182L / 182M /

182N / 182P / 182Q / 182R / 182S / 182T / T182 / T182T

And

Cessna F182P / F182Q

REV

NO.

PAGE NO(S)

DESCRIPTION

DATE OF

APPROVAL

FAA APPROVED

ALL

Original Issue

12/21/2017

Robert G. Murray

Garmin ODA STC

Unit Administrator

ALL

Added VNAV

See Cover

Summary of Contents for GFC 500

Page 1: ......

Page 2: ...permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed and to print one copy of this manual or of any...

Page 3: ...SUPPLEMENT GFC 500 Autopilot with ESP Installed in Textron Aviation 182E 182F 182G 182H 182J 182K 182L 182M 182N 182P 182Q 182R 182S 182T T182 T182T And Cessna F182P F182Q REV NO PAGE NO S DESCRIPTION...

Page 4: ...AFMS GFC 500 Autopilot in Textron 182 Series 190 02291 06 Rev 2 Page ii This page intentionally left blank...

Page 5: ...MINSPD 3 3 Section 3A Non Normal Procedures 3 5 AUTOPILOT ABNORMAL DISCONNECT 3 5 AUTOPILOT PRE FLIGHT TEST FAIL 3 5 LOSS OF NAVIGATION INFORMATION 3 5 LOSS OF AIRSPEED DATA 3 6 LOSS OF ALTITUDE DATA...

Page 6: ...C APPROACH GS out 4 8 GPS APPROACH LPV LNAV VNAV LP V or LNAV V 4 9 GPS APPROACH LP LNAV 4 9 LOC BC APPROACH 4 10 VOR APPROACH 4 11 DISABLING ESP 4 12 Section 5 Performance 5 1 Section 6 Weight and Ba...

Page 7: ...es or adds to the basic POH AFM only as set forth below Users of the manual are advised to always refer to the supplement for possibly superseding information and placarding applicable to operation of...

Page 8: ...tor GA Go Around GFC 500 Garmin Autopilot GMC 507 Autopilot Mode Control Panel GNSS Global Navigation Satellite System GPS Global Positioning System GS Glideslope GSA Garmin Servo Actuator HDG AFCS he...

Page 9: ...tions associated with the GFC 500 Autopilot installation in this airplane Table 1 1 Table of Installed Equipment Interfaces DEVICE TYPE Manufacturer Model If not installed note N A Additional Informat...

Page 10: ...tion Vertical Autopilot Modes Pitch PIT Level Zero vertical speed Go Around GA Altitude Hold Vertical Speed Altitude Capture via Altitude Preselect Indicated Airspeed IAS Vertical Navigation VNAV GPS...

Page 11: ...n 5 50 A pilot must be seated in the left pilot s seat with seatbelt fastened during all autopilot operations Do not use autopilot during takeoff and landing The GFC 500 AFCS preflight test must compl...

Page 12: ...AFMS GFC 500 Autopilot in Textron 182 Series 190 02291 06 Rev 2 Page 2 2 This page intentionally left blank...

Page 13: ...d for high elevator control forces 3 Aircraft Attitude MAINTAIN REGAIN AIRCRAFT CONTROL 4 Elevator Trim RE TRIM if necessary using Elevator Tab Wheel 5 AUTOPILOT Circuit Breaker PULL NOTE Do not relea...

Page 14: ...FAILURE Red PTRIM on G5 display This failure will only occur if the optional pitch trim servo is installed 1 Indicates a failure of the pitch trim servo 2 Control Wheel GRIP FIRMLY 3 AP DISC TRIM INT...

Page 15: ...NOTE Overspeed protection mode provides a pitch up command to decelerate the airplane at or below the maximum autopilot operating speed UNDERSPEED PROTECTION MINSPD MINSPD displayed on G5 AIRSPEED AI...

Page 16: ...AFMS GFC 500 Autopilot in Textron 182 Series 190 02291 06 Rev 2 Page 3 4 This page intentionally left blank...

Page 17: ...amber AP with a red X the autopilot will not be available however the flight director will still be functional AUTOPILOT PRE FLIGHT TEST FAIL Amber AP with a red X in G5 autopilot status box 1 Indica...

Page 18: ...ion on the G5 if a pitch trim servo is installed LOSS OF ALTITUDE DATA Red X through altitude tape on the G5 display NOTE If altitude data is lost while the autopilot is tracking altitude the autopilo...

Page 19: ...fer to the normal procedures section of this AFMS MANUAL PITCH TRIM WITH AUTOPILOT ENGAGED If a pitch trim servo is installed the autopilot will normally trim the airplane as required However during r...

Page 20: ...ilot in Textron 182 Series 190 02291 06 Rev 2 Page 3 8 3 Manual Elevator Trim RE TRIM as required Electric pitch trim should be considered inoperative until the cause of the mistrim has been investiga...

Page 21: ...Off Upon engagement the autopilot will be set to hold the current attitude of the airplane if the flight director was not previously on In this case ROL and PIT will be annunciated Autopilot Engageme...

Page 22: ...to the airplane s current indicated airspeed 3 AIRSPEED Reference ADJUST using UP DN Wheel 4 Throttle ADJUST INCREASE POWER to climb DECREASE POWER to descend 5 Green ALT VERIFY Upon Altitude Capture...

Page 23: ...is not set below the current aircraft altitude No waypoints with altitude constraints in the flight plan Glideslope or Glidepath is the active flight director pitch mode OBS mode is active Dead Reckon...

Page 24: ...re When the GA button is pressed the Flight Director command bars will command go around pitch attitude and wings level The pilot must select the CDI to the appropriate navigation source and select th...

Page 25: ...otate to set track bug to desired track NOTE If track bug is reset too quickly the airplane could turn in the opposite direction as the track bug s movement NAVIGATION VOR 1 Navigation Source SELECT C...

Page 26: ...Desired Course 4 Intercept Heading ESTABLISH in HDG or ROL mode 5 NAV Key PRESS NOTE If the Course Deviation Indicator CDI is greater than one dot from center the autopilot will arm the GPS mode The...

Page 27: ...A button PRESS Execute Missed Approach Procedure 8 Apply GA power NOTE Pressing the GA button will not disconnect the autopilot Select NAV or HDG mode to fly the missed approach procedure If the Cours...

Page 28: ...AV Key PRESS verify LOC ARMED 4 LOC Mode VERIFY airplane Captures and Tracks LOC Course 5 Altitude Preselect SET to next required step down altitude 6 Missed Approach Altitude SET when in ALT mode at...

Page 29: ...wer 9 Set missed approach altitude in the altitude preselect NOTE Pressing the GA button will not disconnect the autopilot Select NAV or HDG mode to fly the missed approach procedure GPS APPROACH LP L...

Page 30: ...ARMED when heading is within 75 degrees of BC course 4 BC Mode VERIFY airplane Captures and Tracks BC Course 5 Altitude Preselect SET to next required step down altitude 6 Missed Approach Altitude SE...

Page 31: ...Key PRESS verify VOR ARMED 4 VOR Mode VERIFY airplane Captures and Tracks VOR Course 5 Altitude Preselect SET to next required step down altitude 6 Missed Approach Altitude SET when in ALT mode at th...

Page 32: ...on 182 Series 190 02291 06 Rev 2 Page 4 12 DISABLING ESP ESP can be disabled on the G5 attitude indicator with the following procedure ESP will default to Enabled on the next power cycle 1 G5 Knob PRE...

Page 33: ...190 02291 06 Rev 2 AFMS GFC 500 Autopilot in Textron 182 Series Page 5 1 SECTION 5 PERFORMANCE No Change...

Page 34: ...AFMS GFC 500 Autopilot in Textron 182 Series 190 02291 06 Rev 2 Page 5 2 This page intentionally left blank...

Page 35: ...500 Autopilot in Textron 182 Series Page 6 1 SECTION 6 WEIGHT AND BALANCE No change to loading information Refer to current weight and balance report and equipment list for changes to empty weight mom...

Page 36: ...AFMS GFC 500 Autopilot in Textron 182 Series 190 02291 06 Rev 2 Page 6 2 This page intentionally left blank...

Page 37: ...director autopilot trim or ESP functions They are used solely to provide independent monitoring of the GFC 500 Airspeed and Altitude Information The GFC 500 requires airspeed and altitude information...

Page 38: ...rther from the normal flight envelope the servo torque will increase until the maximum torque level is reached in an attempt to return the airplane into the normal flight envelope Once the airplane re...

Page 39: ...ive in roll the engagement limit indication that was crossed either Left or Right will move to the lower disengagement limit indication The opposite roll limit remains at the engagement limit Figure 7...

Page 40: ...ause the autopilot to disconnect Pressing the red AP DISC TRIM INT button on the pilot s control wheel Actuating the manual electric trim switch if installed Pushing the AP Key on the GMC 507 mode con...

Page 41: ...T Key ALT nnnnn 10 FT Vertical Speed VS Key VS nnnn 2000 to 2000 FPM 100 FPM IAS Hold IAS Key IAS nnn 65 to 165 KT 1 KT Vertical Path Tracking VNAV VNV Key VNAV VNAV Target Altitude Capture ALTV Glide...

Page 42: ...PR Key GPS 30 Approach ILS Arm Capture Track Glideslope Mode Automatically Armed LOC 30 Takeoff or Go Around GA Button TO or GA Wings Level LVL Level LVL Key LVL Wings Level ESP Roll Attitude Engageme...

Page 43: ...o Trim Input Fault The inputs to the trim system are invalid The trim system needs service Autopilot Annunciations Autopilot has failed Autopilot and trim are inoperative and flight director is not av...

Page 44: ...tron 182 Series 190 02291 06 Rev 2 Page 7 8 LIGHTING When the aircraft s dimming bus is selected off or full dim GMC 507 mode control panel lighting is controlled by integrated photocells which sense...

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