UJPT, E2-C2, ADV, & IUT EMFP-05
Canopy and Flight Control Emergency Procedures
2.
Procedures
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
Sg 3, fr 7, 8
1.
Indications
Split Flaps After
Lowering
a.
Aircraft rolls/yaws while lowering or raising
flaps/slats
Sg 3, fr 9, 10
Split Flaps After
Raising
b.
Aircraft rolls/yaws while flaps/slats extended
NOTE: The above indications probably indicate
an asymmetrical wings flaps condition
2.
Procedures - See NATOPS
LESSON NOTES
Split slats are an unlikely emergency in the T-45A. Explain that
the indications will be the same as split flaps, and both follow
the uncommanded roll/yaw procedure.
NOTE: Explain to students that they 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 their controllability problems.
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(9-98) Original
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