T-45A UJPT, E2-C2, ADV, & IUT Eng-02
Engine
(2) Maximum-rated thrust (MRT):
610 degrees C, time restricted to
30 minutes per flight hour
(3) Maximum continuous: 550
degrees C, time unrestricted
(4) Idle: 450 degrees C, time
unrestricted
(5) Transient/acceleration: 645
degrees C, time restricted to less
than 20 seconds
(6) Ground start: 550 degrees C with
a transient overshoot of 20
degrees C; time restricted to 10
seconds
(7) Airstart: 600 degrees C with a
transient overshoot of 50 degrees
C; time restricted to 10 seconds
c.
Fuel flow
(1) Idle: 300-400 pph
(2) Maximum: 6,410 pph
d.
Fire detection system
(1) Consists of two sets of automatic
resetting firewire elements
(a) One encircles engine bay
(b) One encircles GTS bay
(2) Detects fire or overheat condition
in GTS and engine bays
(8-03) Original
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