UJPT, E2-C2, ADV, & IUT EMFP-05
Canopy and Flight Control Emergency Procedures
REFRESHER
Recall:
*
That the T-45A ailerons, stabilator, speed brakes, flaps, and
slats are hydraulically operated
*
The location and function of T-45A flight controls, trim
control, and indicators
*
The T-45A warning/caution panel (WCP) 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. The student must be able to ac-
complish 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
Sg 1, fr 3
1.
SPEED BRAKE advisory light illuminated
Speed Brake Fails to
Retract
2.
Lack of aircraft acceleration
3.
Continued noise or buffeting
4.
Visual confirmation by wingman
B.
Procedures
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 practicable
Page 5-4
(9-98) Original
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