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钻石40系列飞机维护手册 DA 40 SERIES AIRPLANE MAINTENANCE MANUAL 3(4)

时间:2011-10-28 13:42来源:蓝天飞行翻译 作者:admin
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Page 4A - 8  Rev. 5  15-Nov-2007  Doc. No. 7.01.05-E 


Check procedure:
a) 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. There is a malfunction in the landing gear system.
b) Fuel quantity .........................  check indication, verify using alternate means (see Section 7.9.5)
c) Position lights, strobe lights (ACL) ........  check for correct function

CAUTION
Do not look directly into the anti collision lights.
d) Landing/Taxi light ..................... check for correct function
e) Stall warning/stall heat/Pitot heat ......... check

% NOTE % The stall warning switch gets slightly warmer on ground only % and STAL HT FAIL is indicated on the PFD.
CONTINUED
Doc. No. 7.01.05-E  Rev. 5  15-Nov-2007  Page 4A - 9 


f)  Gear warning/ Fire detector TEST BUTTON ............ PUSH, check aural alert/fire
detection warning and aural alert % and CHECK GEAR caution (if % installed)
CAUTION
If the aural alert or the warning on the PFD does not appear, terminate flight. Unscheduled maintenance is necessary.
g) Control stick ......................... pull fully aft/hold at backstop
h) FLAPS.............................. set LDG position
i) POWER Lever........................ set MAX
j) Variable elevator backstop .............. check function/control stick must

move slightly forward during power
lever forward movement k) POWER Lever........................ set IDLE l) Variable elevator backstop .............. check function/control stick must
regain full movement during power lever retraction m) FLAPS.............................. set UP position
CAUTION
The proper function of the variable elevator backstop is indispensable for the safety of flight, as the handling qualities during power-on stalls are degraded significantly. For more details see Chapter 7- AIRPLANE DESCRIPTION AND SYSTEMS.
If the variable elevator backstop does not function properly, terminate flight.
CONTINUED
Page 4A - 10  Rev. 5  15-Nov-2007  Doc. No. 7.01.05-E 


n) ELECT. MASTER ..................... OFF o) Flight controls ........................ check freeand correct movement up to full deflection p) Trims............................... check freeand correct movement up to full deflection
END OF CHECKLIST
II. Walk-around check, visual inspection
CAUTION
A visual inspection means: examination for damage, cracks, delamination, excessive play, load transmission, correct attachment and general condition. In addition control surfaces should be checked for freedom of movement.
 
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