MILITARY SPECIFICATION SHEET
STARTER, AIRCRAFT engine. AIR TURBINE MODEL A-24
The complete requirements for procuring the air turbine starter
described herein shall consist of this document and the issue in effect
of Specification MIL-S-19557C (AS).
APPLICABLE
PARAGRAPH OF
SPECIFICATION
Envelope:
3.8.1
Figure 1
Wt, Max (Lb): 30
3.7
6.3.1
Aircraft Model:
c-2, E-2
-
4.5.16
Engine Model:
T56
Quick-Attach-Detach Mounting:
3.8.2.1
Yes
Engine Accessory Drive:
3.8.2.2
AND20002, Type XIIS
Figure 1
3.8.3
Air Inlet and Exhaust Connections:
Rotation Viewed from Anti-Drive End:
Clockwise
3.5.5
3.9.1
3.3.2
Exposure Temperature Range (°F): -100 to +275
3.3.2
Ambient Temperature Operating Range (°F): -65
to +160
Control Valve:
3.3.2.3
Opening Rate, Max: 22 psig per sec for the first
4.5.1.1
1 sec.
4.5.6
Clsong Time, Max: 0.5 sec
N avy Model: ATSCV-1
335.75.7
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