2............…............…............…..........…....................1
(c) Set the aileron back to normal (Ref 27-11-00).
S 735-720-001
(5) Rudder Position Test
(a)
Make sure the rudder and rudder trim control system are operational (Ref 27-21-00).
(b)
Make sure the rudder is at the neutral position.
(c)
On the tester, set the SUBFRAME to 0.
(d)
Make sure the tester display shows between 7670 and 0102 when the WORDs are set to 12 and 44.
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MAINTENANCE MANUAL
(e)
Set the left rudder pedal to the full forward position.
(f)
Make sure the tester display shows between 6050 and 6262 when the WORDs are set to 12 and 44.
(g)
Set the right rudder pedal to the full forward position.
(h)
Make sure the tester display shows between 1510 and 1722 when the WORDs are set to 12 and 44.
S 865-875-001
(6)
Set the rudder position back to normal (Ref 27-21-00).
S 735-723-001
(7)
Horizontal Stabilizer Position Test
(a)
Make sure the horizontal stabilizer trim control system is operational (Ref 27-41-00).
(b)
On the tester, the WORD to 24.
(c)
Set the stabilizer to the 0 trim position.
(d)
Make sure the tester display shows between 0660 and 0740 when the SUBFRAMEs are set to 2 and 4.
(e)
Set the stablizer to 15.5 trim position.
(f)
Make sure the tester display shows between 7040 and 7120 when the SUBFRAMEs are set to 2 and 4.
S 865-929-001
(8)
Set the stabilizer back to the normal position (Ref 27-41-00).
S 735-724-001
(9)
Trailing Edge Flaps Position Test
(a)
Make sure the trailing edge (T.E.) flaps system is operational (Ref 27-51-00).
(b)
Make sure the trailing edge flaps are up.
(c)
Open these circuit breakers on the overhead circuit breaker panel, P11, and attach DO-NOT-CLOSE tags 1) 11H12, FLAP POS IND LEFT
(d)
Make sure the circuit breaker on the overhead circuit breaker panel, P11, is closed: 1) 11H13, FLAP POS IND RIGHT
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本文链接地址：757 AMM 飞机维护手册 仪表 CHAPTER 31 - INSTRUMENTS 1(68)
