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% adjustment is installed: verify
% proper locking
7. Safety harnesses ..................... all on and fastened
8. POWER lever ........................ check IDLE
9. Parking brake ........................ set
10. AVIONIC MASTER ................... check OFF
11. GEAR selector ....................... check DOWN
12.ECU SWAP.......................... check AUTOMATIC
13.ALTERNATORS ...................... check ON
14.ELECT. MASTER ..................... ON
CAUTION
When switching the ELECT. MASTER ON, the electrically driven hydraulic gear pump may activate itself for 5 to 20 seconds in order to restore the system pressure. Should the pump continue to operate continuously or periodically, terminate flight preparation. There is a malfunction in the landing gear system.
CONTINUED
Page 4A - 20 Rev. 5 15-Nov-2007 Doc. No. 7.01.05-E
15.G1000.............................. wait until power-up completed. Press ENT on MFD to acknowledge.
NOTE
The engine instruments are only available on the MFD after item 15 has been completed.
16.Fuel temperature ..................... check
% WARNING % If Diesel Fuel or a blend of Diesel Fuel with Jet Fuel is used, % (approved only if M.M 42-037 is incorporated), or if the fuel % grade is unknown, the engine must not be started if the fuel % temperature indication prior to operation is below -5 °C % (+23 °F).
% Operation with a fuel temperature below -5 °C (+23 °F) is not % permitted, as safe operation of the engine under those % conditions cannot be ensured and the engine can stop.
NOTE
Make sure which fuel grade is being used (see Section 7.9.5). If it is not possible to determine the fuel grade, the Diesel Fuel temperature limitations must be observed.
END OF CHECKLIST 4A.6.3 STARTING ENGINE
Doc. No. 7.01.05-E Rev. 5 15-Nov-2007 Page 4A - 21
1.
Strobe lights (ACL) .................... ON
2.
ENGINE MASTER .................... ON (L/R)
NOTE
It is recommended to start the LH engine (pilot side) first. If required by operational reasons, the RH engine can also be started first.
3.
Annunciations ........................ check .L/R ENGINE GLOW“ ON
4.
Annunciations/Engine/System Page ....... check OK/normal range
WARNING
Before starting the engine the pilot must ensure that the propeller area is free, and no persons can be endangered.
After the L/R ENGINE GLOW indication is extinguished:
5. START KEY ......................... START L/R as required / release when engine has started.
CONTINUED
Page 4A - 22 Rev. 5 15-Nov-2007 Doc. No. 7.01.05-E
CAUTION
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本文链接地址：钻石40系列飞机维护手册 DA 40 SERIES AIRPLANE MAINTENANCE MANUAL 3(9)
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