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Page Title:
Starter, Aircraft Engine, Air Turbine. Model A-29 |
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|  MILITARY SPECIFICATION SHEET
STARTER, AIRCRAFT ENGINE, AIR TURBINE. MODEL A-29
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
3.8.1
Envelope:
Figure 1
Wt, Max (Lb): 23
3.7
Overhung Moment, Max (In Lb):
3.7.1
625
6.3.1
Aircraft Model:
S-3
Engine Model: TF34
4.5.16
Quick-Attach-Detach Mounting: Buttonhole-type mounting flange
3.8.2.1
in accordance with MS 3332-2 (Type G)
Engine Accessory Drive:
MS 3327-9S
3.8.2.2
Air Inlet and Exhaust Connections:
3.8.3
Figure 1
Rotation Viewed from Anti-Drive End: Clockwise
3.5.5
3.9.1
3.3.2
Exposure Temperature Range (F): -100 to +350
Ambient Temperature Operating Range (F): -65 to +160
3.3.2
3.3.2.3
Control Valve:
Opening Rate, Max: 22 psig per sec in the first .5 Sec.
4.5.1.1
Opening Time, Max: 3.0 sec.
4.5.6
Closing Time, Max: 2.0 sec
Navy Model: Not Assigned
3.5.1
Rated Conditions:
Output Drive Speed (RPM): 2100
Output Drive Torque, Min (Lb-Ft): 140
Airflow, Max (Lb per Min): 70
Air Inlet Total Pressure Max (In, Hg A): 90
Air Inlet Total Temperature Max (F): 3325
3.5.1
Cutout Speed (RPM): 3900 100
3.5.7
Automatic Shutoff Control: Either turbine wheel speed or output
3.5.7
drive speed may be sensed for control operation.
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