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Home > Aviation Maintenance and Training Volume 2 > > Presentation - P-12600089
Motivation - P-12600088
Fig 1:  ECA Failure (Full Trim)

Emergency Flight Procedures - index
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T-45C TS, ADV & IUT EMFP-04
Engine and Hydraulic Emergency Procedures
PRESENTATION
NOTE: Italicized passages are excerpted from NATOPS.
I.
Fuel system malfunctions
Sg 1, fr 2
Lesson Organization
A. ECA failure 1.8.1.1.9.1.2
ENGINE AND HYDRAULIC
EMERGENCY PROCEDURES
NOTE: In the unlikely event of an ECA failure in a full
* Fuelsystem
trim condition, fuel flow will be reduced: the EGT and
malfunctions
rpm will decrease, and the thrust available will be
* Hydraulic system
governed by the maximum rpm obtained. The thrust may
malfunctions
be reduced as much as one third of the normal full
* Engine malfunctions
throttle value. Very low idle rpm may occur, and the
throttle must be handled carefully to avoid stall or
flameout.
NOTE:  ECA total failure will, in most instances, result in
a no-trim condition, increasing the rpm and EGT. The
EGT and rpm must be controlled carefully within limits by
throttle manipulation. Do not exceed 90% above
20,000 feet, or 95% below 20,000 feet.
1.
Indications
a.
ECA failure (full trim, both lanes)
Sg 1, fr 3
ECA Failure (Single
Lane)
(1) MASTER ALERT light flashes and caution
tone sounds
(2) ECA 2 caution light illuminates
(3) Fuel flow decreases
(4) EGT decreases
Sg 1, fr 4
(5) RPM decreases
Fig 1: ECA Failure
(Full Trim)
Original (9-98)
Page 4-4






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