(5) Move the power levers forward until the PWR UPTRIM light on engine instrument
panel comes on (power levers should be above FLT IDLE + 12 degrees).
NOTE:
Operation of PWR UPTRIM light confirms function of overtorque switch,
relay 7712−K5 and power uptrim circuits (see Chapter 61).
(6) Release 'press−to−test' switch. Check indicator pointer and digital display indicate
zero % and PWR UPTRIM light goes out.
(7) Repeat steps (4), (5) and (6) for the right torque indicator 'press−to−test' switch.
NOTE:
Operation of PWR UPTRIM light confirms function of right indicator
overtorque switch relay 7712−K4 and associated power uptrim circuits
(see Chapter 61).
(8) Open circuit breakers, steps (2) and (3). Check indicator pointer on each indicator
moves off−scale and digital displays are blanked. Close circuit breakers.
MASTER
EFFECTIVITY: See Pageblock 77−10−00 page 1
D
S ERIES 100
AIRCRAFT MAINTENANCE MANUAL
77−10−00
Page 3
Jun 20/2005