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Page Title:
Starter, Aircraft Engine, Air Turbine, Model A-30 |
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|  MIL-S-19557/10A(AS)
9 February 1987
SUPERSEDING
MIL-S-19557/10(AS)
1 April 1983
MILITARY SPECIFICATION SHEET
STARTER, AIRCRAFT ENGINE, AIR TURBINE, MODEL A-30
This specification sheet is approved for use by the Naval Air Systems
Command, Department of the Navy, and is available for use by all
Departments and Agencies of the Department of Defense.
The complete requirements for procuring the starter described herein shall
consist of this document and the latest issue of Specification MIL-S-19557(AS).
REQUIREMENTS
Applicable paragraphs
of MIL-S-19557C(AS)
Figures 1 and 2
Envelope:
3.8.1
Weight, Max (Lb): 30.0 (including insulation
3.7
blanket, if required)
Overhung Moment, Max (In Lb): 166
3.7.1
Aircraft Model: F-18
6.1
Engine Model: F404
4.5.16
Quick-Attach-Detach Mounting: V Band coupling flange
3.8.2.1
mount in accordance with AS964 except as shown on
Figures 1 and 2
Enqine Accessory Drive: AS969-2S type pad on
3.8.2.2
Aircraft Mounted Accessory Drive (AMAD). Gearbox
modified to adapt to Figures 1 and 2
Air Inlet and Exhaust Connections:
3.8.3
Figures 1 and 2
Air Inlet Pressure Loads
3.8.3.2
Maximum Normal Pressure 51 PSIG
Maximum Single Failure Pressure 83 PSIG
Proof Pressure 165 PSIG
AMSC N/A
FSC 2995
Approved for public release; distribution is unlimited.
DISTRIBUTION STATEMENT A.
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