T-45C TS, ADV & IUT EMFP-03
Operational and Ejection Emergency Procedures
II.
Aircraft control emergencies 10.7.9.1.2, 1.8.1.6.1.3,
Sg 2, fr 2
1.8.1.10.6.2
Lesson Organization
A.
Departure/spin
OPERATIONAL AND
EJECTION EMERGENCY
PROCEDURES
1.
Indications: The angle of attack indicator is used to
* Emergency egress
* Aircraft control emergencies
determine if the aircraft is in an upright or inverted
* Ejection situations, requirements,
and criteria/envelopes
spin, while the turn needle will always point in the
* Comm procedures for operational
emergencies
direction of the spin.
* Ditching
* SAR operations
NOTE: If the engine flames out, the right MFD is
lost and the left MFD reverts to the ADI display and
will operate for 3 minutes.
a.
Departure: Instrument indications and aircraft
motion about all axes will vary depending on the
maneuver performed when the aircraft
departed, but instruments and aircraft motion
will not have stabilized.
b.
Spin
(1) Upright
(a) AOA: above 28 units (pegged)
(b) G: Positive
(c) Turn needle: pegged on direction of
spin
(d) Airspeed oscillating between
80-140 knots
(2) Inverted
(a) AOA: 0 units (pegged)
(b) G: Negative
Original (9-98)
Page 3-6
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