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Page Title:
Starter, Aircraft Engine, Air Turbine, Model A-14-1 |
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|  MIL-S-19557/1(AS)
11 September 1972
MILITARY SECIFICATION SHEET
STARTER, AIRCRAFT ENGINE, AIR TURBINE, MODEL A-14-1
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
Figure 1
Envelope:
3.8.1
Wt. Max (Lb): 23
3.7
A-4 (Probe Starter)
Aircraft Model:
6.3.1
J65
Engine Model:
4.5.16
Quick-Attach-Detach Mounting: Yes
3.8.2.1
AND20002, Type XIIS
Engine Accessory Drive:
3.802.2
Air Inlet and Exhaust Connections: Figure 1
3.8.3
Rotation Viewed from Anti-Drive End: Clockwise
3.595
3.9.1
-100 to +275
Exposure Tem perature Range (F):
3.3.2
-65 to +160
Ambient Temperature Operating Range (F):
3.3.2
Control Valve:
3.3.2.3
22 psig per sec for the first
Opening Rate, Max:
4.5.1.1
.1 sec
4.5.6
Closing Time Max: 0.5 sec
Navy Model: ATSCV-1
Rated Conditions:
3.5.1
Output Drive Speed (RPM): 1100
Output Drive Torque, Min (Lb-Ft): 140
Airflow, Max (Lb per Min): 60
Air Inlet Total Pressure (In. Hg A): 100
Air Inlet Total Temperature (F): 350
Cutout Speed (RPM): 3150 250
3.5.1
3.5.7
Automatic Shutoff Control: Either turbine wheel speed
3.5.7
or output drive speed may be sensed for control
operation.
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