T-45C TS, ADV & IUT EMFP-07
Canopy and Flight Control Emergency Procedures
REFRESHER
Recall:
*
That the T-45C ailerons, stabilator, speed brakes, flaps, and
slats are hydraulically operated
*
The location and function of T-45C flight controls, trim control,
and indicators
*
The T-45C warning and caution advisory panel lights
associated with the canopy, control augmentation,
and flight control systems
PRESENTATION
NOTE: Procedural steps preceded by an asterisk (*) are consid-
ered immediate action items. You must be able to accomplish
these steps without reference to the checklist.
I.
Speed brake failure (fails to retract) 1.8.1.6.8.1.1, 1.8.1.6.8.2
Sg 1, fr 2
Lesson Organization
A.
Indications
CANOPY AND FLIGHT CONTROL
1.
SP BRK advisory light illuminated
EMERGENCY PROCEDURES
*
Speed brake failure
2.
Lack of aircraft acceleration
*
Trim malfunctions
*
Flap/slat malfunctions
*
Control augmentation failure
3.
Continued noise or buffeting
*
Canopy
4.
Visual confirmation by wingman
Sg 1, fr 3
Speed Brake Fails to
B.
Procedures
Retract
1.
Attempt to retract from both cockpits, if able
2.
Airspeed - MAX RANGE OR MAX ENDURANCE AS
THE SITUATION DICTATES
3.
Land as soon as practical
Original (9-98)
Page 7-4
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