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Home > Aviation Maintenance and Training Volume 2 > > Control augmentation system - P-12600138
Flaps Failure (Flaps fail to extend) - P-12600137
Indications - P-12600139

Emergency Flight Procedures - index
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T-45C TS, ADV & IUT EMFP-07
Canopy and Flight Control Emergency Procedures
V.
Control augmentation system
Sg 4, fr 2
Lesson Organization
A. C AUG failure 1.8.1.6.1.4
CANOPY AND FLIGHT CONTROL
1.
Indications
EMERGENCY PROCEDURES
*
Speed brake failure
*
Trim malfunctions
a.
C AUG caution light is ON
*
Flap/slat malfunctions
*
Control augmentation
failure
NOTE: C AUG caution light will illuminate
* Canopy
whenever the switch is off, inputs from GINA
are invalid, system has internal failure, system
Sg 4, fr 3 (2 overlays)
is in BIT.
Control Augmentation
Failure
b.
Yaw damping, turn coordination, speed brake to
stabilator interconnect (SBI), and rudder trim
are inoperative
2.
Procedures - See NATOPS
VI. Canopy
Overlay 1
A. Unlocked 1.5.4.4.2
Overlay 2
?
Sg 11, fr 2
If the canopy is unlocked, when will the MASTER
Lesson Organization
ALERT flash and CANOPY caution light illuminate?
CANOPY AND FLIGHT CONTROL
EMERGENCY PROCEDURES
ANSWER: Anytime the canopy is unlocked, the CANOPY
*
Speed brake failure
caution light will be illuminated. The MASTER ALERT flashes
*
Trim malfunctions
*
Flap/slat malfunctions
and warning tone sounds when the canopy is still unlocked and
*
Control augmentation failure
the throttle position is advanced above 95%.
*
Canopy
Original (9-98)
Page 7-10






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