Introduction to NATOPS & T-45A Configuration
T-45A UJPT, E2-C2, ADV, & IUT Eng-01
2.
Landing gross weight (lb): 13,360 FCLP
13,360 Field
13,360 Carrier
3.
Usable fuel weight (lb): 2,776 JP-4
2,904 JP-5
2,861 JP-8
4.
Operating weight empty (lb): 10,557 (with
wing pylons) 10,403 (without pylons)
5.
Max permissible Mach/airspeed (clean
loading): 1.04/550 KIAS, whichever is less
6.
Max g: +7.3, -3
NOTE: Max g is a design specification.
Actual operating limitations are contained in
the T-45A NATOPS Manual, Chapter 4.
7.
Maximum altitude - 41,000 ft MSL
8.
The T-45A is not an all-metal A/C. Some
components, i.e., ailerons, speed brakes,
and main gear doors, are made of "super
plastics"
Sg 3, fr 1
III. Major aircraft systems overview
Lesson Organization
A.
Engine system 1.4.6.3.1.1
Sg 3, fr 1
1.
Description: You have a (F405-RR-401)
Chamber
Internal Gearbox
N2 Turbine
N1 Turbine
single, non-afterburning twin spool turbofan
N1 Turbine
engine with a two-stage low-pressure (N1)
Bearing
and a five-stage high-pressure (N2)
compressor driven by respective single-
Oil Tank
Location
N2 Turbine
stage low- and high-pressure turbines, with
Intershaft
N1 Compressor
Bearing
Bearing
Bearing
HS Gearbox
Front Bearing
Engine Fuel
Controls Cambox
self-starting gas turbine start capability
T-45A ENGINE
2.
Function
a.
The engine produces static-installed
thrust of 5,527 lb at sea level
(8-03) Original
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