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钻石42飞机飞行手册 DA 42 Airplane Flight Manual(46)

时间:2011-10-28 13:17来源:蓝天飞行翻译 作者:admin
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END OF CHECKLIST
Doc. No. 7.01.05-E  Rev. 5  15-Nov-2007  Page 3 - 53 

 


3.9 OTHER EMERGENCIES
3.9.1 SUSPICION OF CARBON MONOXIDE CONTAMINATION IN THE CABIN
Carbon monoxide (CO) is a gas which is developed during the combustion process. It is poisonous and without smell. Increased concentration of carbon monoxide gas can be fatal. The occurrence of CO in the cabin is possible only due to a defect. If a smell similar to exhaust gases is noticed in the cabin, the following measures should be taken:
1.
Cabin heat & Defrost...................  OFF


2.
Ventilation ...........................  open


3.
Emergency windows ...................  open


4.  
Forward canopy ...................... unlatch, push up and lock in
"cooling-gap“ position

 

CAUTION
The maximum demonstrated airspeed for emergency opening the front canopy in flight is 120 KIAS. Do not exceed 120 KIAS.
END OF CHECKLIST 3.9.2 UNLOCKED DOORS
Page 3 - 54  Rev. 5  15-Nov-2007  Doc. No. 7.01.05-E 

 

1.  
Airspeed ............................ reduce


2.  
Canopy ............................. check visually if closed


3.  
Rear passenger door .................. check visually if closed


4.  
Front baggage doors .................. check visually if closed

 

WARNING
Never unlock the rear passenger door during flight. It may break away.
5.  If it is not possible to lock the canopy or the rear passenger door, or if one or both of the front baggage doors are open, land on the nearest suitable airfield.
END OF CHECKLIST 3.9.3 DEFECTIVE PROPELLER RPM REGULATING SYSTEM
Doc. No. 7.01.05-E  Rev. 5  15-Nov-2007  Page 3 - 55 

 

CAUTION
The power lever should be moved slowly, in order to avoid over-speeding and excessively rapid RPM changes. The light wooden propeller blades produce more rapid RPM changes than metal blades.
WARNING
In case of a malfunction of the engine control unit it is possible that the propeller blades will remain in the position of highest pitch. In this case the reduced engine performance should be taken into consideration.
(a) Oscillating RPM
1.
POWER setting....................... change


2.
ECU SWAP.......................... ECU B

 

if the problem does not clear:
NOTE
If the problem does not clear itself, switch back to AUTO and land on the nearest suitable airfield.
CONTINUED


(b) Propeller overspeed
NOTE
This procedure applies for continued propeller overspeed due to a malfunction in the propeller constant speed unit or a engine control unit malfunction.
 
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