T-45C TS, ADV & IUT EMFP-07
Canopy and Flight Control Emergency Procedures
2.
Procedures
Sg 3, fr 7, 8
Split Flaps After
Lowering
a.
Confirm flap position visually, if possible
b.
Fly optimum AOA approach for flap/slat
condition
B.
Uncommanded roll/yaw 1.8.1.6.13.2
1.
Indications
Sg 3, fr 9, 10
Split Flaps After
a.
Aircraft rolls/yaws while lowering or raising
Raising
flaps/slats
b.
Aircraft rolls/yaws while flaps/slats extended
NOTE: The above indications probably indicate
an asymmetrical wings flaps condition
2.
Procedures - See NATOPS
LESSON NOTE
Split slats are an unlikely emergency in the T-45C. Explain that
the indications will be the same as split flaps, and both follow
the uncommanded roll/yaw procedure.
NOTE: You should expect more control problems with split flaps
than split slats due to the fact that there will be a greater drag
difference between the wings. In either case, a constant AOA/
airspeed approach to short field arrestment will minimize your
controllability problems.
Original (9-98)
Page 7-8
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