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AFMS

– GFC 500 Autopilot in Textron 182 Series

190-02291-06 Rev. 2

Page 4

–10

LOC BC APPROACH

Navigation Source. .................................................................................... SELECT CDI to VHF Nav

Tune and Identify an ILS station frequency

Course Pointer .................................................................................. SET CDI to LOC Front Course

NOTE

Ensure that the current heading will result in a capture of the selected course.

3. NAV Key .................................................................................................. PRESS, verify BC 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 ......................................................... SET when in ALT mode at the MDA

At Missed Approach Point:

7. AP DISC / TRIM INT button .................................... PRESS, Continue visually for a normal landing

8. GO AROUND (GA) button ....................................... PRESS, Execute Missed Approach Procedure

9. Apply GA power.

NOTE

Pressing the GA button will not disconnect the autopilot. Select NAV or HDG mode to fly the
missed approach procedure.

Содержание GFC 500

Страница 1: ......

Страница 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...

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

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

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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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