Garmin Cessna Caravan G1000 파일럿 매뉴얼 - 페이지 13

{카테고리_이름} Garmin Cessna Caravan G1000에 대한 파일럿 매뉴얼을 온라인으로 검색하거나 PDF를 다운로드하세요. Garmin Cessna Caravan G1000 16 페이지. Integrated flight deck
Garmin Cessna Caravan G1000에 대해서도 마찬가지입니다: 파일럿 매뉴얼 (6 페이지), 파일럿 매뉴얼 (32 페이지), 파일럿 매뉴얼 (25 페이지), 파일럿 매뉴얼 (34 페이지), 파일럿 매뉴얼 (21 페이지), 비행기 비행 매뉴얼 보충 자료 (33 페이지), 파일럿 매뉴얼 (22 페이지)

SAMPLE SYSTEM OPERATION/FAILURE MODE SCENARIOS FOR FAA-S-8081-4D

The following table gives recommendations on simulating various partial panel conﬁgurations by pulling circuit breakers.

NOTE: Due to the differences in autopilot interfaces, the recommendations for autopilot engagement are generic and may

not be suitable for all aircraft.

Failure to Be Simulated

Loss of AHRS and ADC*

(simulates loss of all primary ﬂight instru-

ments)

Loss of AHRS

(attitude and heading)

Loss of ADC

(airspeed, altitude and vertical speed)*

Loss of PFD

NOTE: * When the ADC has failed, pressure altitude data is no longer available to the transponder. As a result, the transpon-

der loses its Mode C (i.e., altitude reporting) capability. Therefore, without the required coordination with the appropriate

air trafﬁc control facility, failing the ADC should be avoided in Class B and C airspaces, or within the Mode C veil of Class B

airspace.

190-00368-02 Rev. A

Examiner Action

Pull AHRS and ADC circuit breakers.

Pull AHRS circuit breaker.

Pull ADC circuit breaker.

Pull PFD circuit breakers.

This action prevents the tuning of the COM

1/NAV 1 frequencies; COM 2 must be tuned to

the proper frequency and must be in use.

Garmin G1000 Guide for Designated Pilot Examiners & Certiﬁed Flight Instructors

Applicant Action

Control the aircraft by reference to the backup

attitude, altitude and airspeed indicators; en-

gage the autopilot if it is rate-based and has

its own gyro source in roll mode.

Control the aircraft by reference to the backup

attitude indicator; engage the autopilot if it is

rate-based and has its own gyro source in roll

mode.

Control the aircraft by reference to the PFD at-

titude presentation and the backup airspeed

and altitude indicators; engage the autopilot

in roll, HDG, or NAV mode.

Control the aircraft by reference to the MFD in

reversionary mode (this mode also removes all

moving map presentations).