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钻石42飞机飞行手册 DA 42 Airplane Flight Manual(33)

时间:2011-10-28 13:17来源:蓝天飞行翻译 作者:admin
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Proceed according to:
3.7.2 - HIGH CURRENT

3.2.8 L/R ENG FIRE
L/R ENG FIRE  Left / Right engine fire detected 

Engine fire can lead to a total loss of power due to engine failure as well as severe structural damage:
Proceed according to the following procedures as applicable:

3.8.1 - ENGINE FIRE ON GROUND
3.8.2 - ENGINE FIRE DURING TAKE-OFF
3.8.3 - ENGINE FIRE IN FLIGHT
Page 3 - 12  Rev. 5  15-Nov-2007  Doc. No. 7.01.05-E 

 

3.2.9 L/R STARTER

L/R STARTER  Left / Right engine starter is engaged 

Proceed according to:
3.7.3 - STARTER MALFUNCTION
3.2.10 DOOR OPEN
DOOR OPEN  Front and/or rear canopy and/or baggage door are/is not closed and locked. 

Proceed according to:

3.9.2 - UNLOCKED DOORS
Doc. No. 7.01.05-E  Rev. 5  15-Nov-2007  Page 3 - 13 

 


3.3 G1000 SYSTEM WARNINGS
3.3.1 RED X
A red X through any display field, such as COM frequencies, NAV frequencies, or engine data, indicates that display field is not receiving valid data.
3.3.2 POSN ERROR
POSN ERROR  The system will flag and no longer provide GPS based navigational guidance. 

Revert to the G1000 VOR/ILS receivers or an alternate means of navigation other than the G1000 GPS receivers.
3.3.3 ATTITUDE FAIL
ATTITUDE FAIL  The display system is not receiving attitude reference information from the AHRS; accompanied by the removal of sky/ground presentation and a red X over the attitude area. 

Revert to the standby attitude indicator.

3.3.4 AIRSPEED FAIL
The display system is not receiving airspeed input from the air data computer; accompanied by a red X through the airspeed display.
AIRSPEED FAIL
Revert to the standby airspeed indicator.
Page 3 - 14  Rev. 5  15-Nov-2007  Doc. No. 7.01.05-E 

 

3.3.5 ALTITUDE FAIL

The display system is not receiving altitude input from the air data computer; accompanied by a red X through the altimeter display.
ALTITUDE FAIL
Revert to the standby altimeter.

3.3.6 VERT SPEED FAIL
The display system is not receiving vertical speed input from the air data computer; accompanied by a red X through the vertical speed display.
VERT SPEED FAIL
Determine vertical speed based on the change of altitude information.

3.3.7 HDG
The display system is not receiving valid heading input from the AHRS; accompanied by a red X through the digital heading display.
HDG
Revert to the emergency compass.
3.3.8 WARN
WARN  RAIM position warning - nav deviation bar removed. 

1. CDI softkey .......................... switch to VOR/LOC

Doc. No. 7.01.05-E  Rev. 5  15-Nov-2007  Page 3 - 15 

 
 
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