T-45C TS, ADV, & IUT NFamFP-02
Night Emergency Procedures
b.
Execution signal: lights come back on
steady
4.
Extend or retract speed brakes as
appropriate
a.
Preparatory signal: 3 dashes with
external lights
b.
Execution signal: lights come back on
steady
5.
Execute lead change
a.
Signal: lead aircraft turns anti-collision
lights on; if external lights are
inoperative, leader shines flashlight on
own helmet, then shines light on
wingman
b.
Response: wingman turns anti-
collision lights off and assumes lead; if
external lights are inoperative,
wingman shine flashlight at leader and
then on own helmet and assumes lead
Sg 11, fr 1
XI. Inadvertent IMC 1.8.1.10.10.2
NIGHT EMERGENCY
PROCEDURES
A. Switch to instrument scan and advise controller
and/or night safety pilot of problem and
*
Wheel brake failure
intentions
*
Failure to reach line speed
*
Takeoff abort
CAUTION: Intermittent IMC is vertigo
*
Engine failure on takeoff
inducing. Rely on your instruments.
*
Generator failure with low
battery voltage
B. Verify pitot heat switch ON
*
Double inverter failure
*
Total electrical failure
C. If IMC expected to last more than a few
*
GINA failure
seconds, perform a gentle 180-degree turn to fly
*
TACAN bearing failure
out of IMC in direction opposite to entry
*
NORDO
*
Inadvertent IMC
D. If VFR conditions not reached within 1-2
*
Lost aircraft situations
minutes, request clearance from controller and/
or night safety pilot to descend to VFR
(conditions permitting)
(9-99) Original
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