T-45C TS, ADV & IUT EMFP-07
Canopy and Flight Control Emergency Procedures
III. Rudder trim hardover 1.8.1.6.3.1
NOTE: The rudder trim system is interconnected with the
yaw damper, which is part of the control augmentation
system. A malfunction of certain CONTR AUG system
components (e.g., yaw damper controller or yaw damper
actuator) could cause undesirable rudder inputs.
A.
Indications - Same as runaway trim
B.
Procedures - See NATOPS
PROGRESS CHECK
Question 1 — 1.8.1.6.8.2
What airspeed should you maintain if your speed brakes fail
to retract?
ANSWER: Max range or max endurance as the situation
dictates
Sg 3, fr 2
Lesson Organization
IV. Flap/slat malfunctions
CANOPY AND FLIGHT CONTROL
A.
Flap position indicator failure 1.8.1.8.3.1
EMERGENCY PROCEDURES
*
Speed brake failure
1.
Indications
*
Trim malfunctions
*
Flap/slat malfunctions
*
Control augmentation failure
a.
Indicator light fails to come on/off when
*
Canopy
flaps change position
Sg 3, fr 3-4, 5-6
b.
Indicator lights show different flap positions
Flap Indicator Failure
between cockpits
c.
Visual confirmation of flap position
Original (9-98)
Page 7-7
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