UJPT, E2-C2, ADV, & IUT EMFP-05
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
IV. Flap/slat malfunctions
Sg 3, fr 2
Lesson Organization
A.
Flap indicator failure 1.8.1.8.3.1
Sg 3, fr 3-4, 5-6
Flap Indicator Failure
1.
Indications
a.
Indicator fails to move when flaps change
position
b.
Indicators show different flap positions between
cockpits
c.
Visual confirmation of flap position
(9-98) Original
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