T-45C TS, ADV & IUT EMFP-04
Engine and Hydraulic Emergency Procedures
III.
Engine malfunctions and situations which may require
Sg 3, fr 2
precautionary approach 1.8.1.1.4.2, 1.8.1.1.7.2
Lesson Organization
ENGINE AND HYDRAULIC
A.
EGT/RPM malfunctions (in flight)
EMERGENCY PROCEDURES
* Fuel system
malfunctions
1.
Indications
* Hydraulic system
malfunctions
a.
N1
* Engine malfunctions
(1) MASTER ALERT light flashes and warning
tone sounds
Sg 3, fr 3, pg 1
Fig 9: RPM Malfunc-
(2) EGT/RPM warning light illuminates when
tion (1 Overlay)
N1 RPM > 112.4 + 1% or EGT > 650 + 8C
b.
N2 RPM gauge exceeds 104%
Sg 3, fr 5
EGT Malfunction
NOTE: The EGT/RPM light will illuminate in-flight
(1 Overlay)
if either of the following occur: transient/
exceeds 650 + 8o C.
Overlay 1
Sg 3, fr 7
Fig 9: RPM Malfunc-
tion
Figure 9: RPM MALFUNCTIONS
Original (9-98)
Page 4-18
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