Garmin Cessna Caravan G1000 Uçak Uçuş El Kitabı Eki - Sayfa 19

Araç Navigasyon sistemi Garmin Cessna Caravan G1000 için çevrimiçi göz atın veya pdf Uçak Uçuş El Kitabı Eki indirin. Garmin Cessna Caravan G1000 33 sayfaları. Integrated flight deck
Ayrıca Garmin Cessna Caravan G1000 için: Pilot El Kitabı (16 sayfalar), Pilot El Kitabı (6 sayfalar), Pilot El Kitabı (32 sayfalar), Pilot El Kitabı (25 sayfalar), Pilot El Kitabı (34 sayfalar), Pilot El Kitabı (21 sayfalar), Pilot El Kitabı (22 sayfalar)

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Garmin Cessna Caravan G1000 Uçak Uçuş El Kitabı Eki

MOONEY

M20R

d) ERRONEOUS OR LOSS OF ENGINE AND FUEL DISPLAYS

Loss of an engine parameter is indicated by a red X through

the data field. Erroneous information may be identified by in-

dications which do not agree with other system information.

Erroneous indications may be determined by comparing a

display with other displays and other system information.

1. Set power based on throttle lever position, engine noise and speed.

2. Monitor other indications to determine the health of the engine.

3. Use known power settings in the POH Chapter V for approximate

fuel flow values.

4. Use other system information, such as annunciator messages, fuel

quantity and flow, to safely complete the flight.

e) ERRONEOUS OR LOSS OF WARNING/CAUTION

ANNUNCIATORS

Loss of an annunciator may be indicated when engine or fuel

displays show an abnormal or emergency situation and the

annunciator is not present. An erroneous annunciator may

be identified when an annunciator appears which does not

agree with other displays or system information.

1. If an annunciator appears, treat it as if the condition exists. Refer to

the POH/AFM Emergency or Abnormal procedures or the proce-

dures contained in this AFMS.

2. If a display indicates an abnormal condition but no annunciator is

present, use other system information, such as engine displays, fuel

quantity and flow, to determine if the condition exists. If it cannot be

determined that the condition does not exist, treat the situation as if

the condition exists. Refer to the POH/AFM Emergency or Abnormal

procedures or the procedures contained in this AFMS.

ISSUED 11 - 2004

REVISION A 06--2005

REVISION B 03--2006

GARMIN G1000 INTEGRATED AVIONICS SYSTEM

NOTE:

AFM SUPPLEMENT

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FAA APPROVED