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| MIL-S-85419 (AS)
2.2 Other Publications. The following documents form a part of
this specification to the extent specified herein. Unless
otherwise indicated, the issue in effect on date of invitation
for bids or request for proposal shall apply.
AMERICAN NATIONAL STANDARDS INSTITUTE (ANSI)
Surface Texture
B46.1-1962
(Application for copies should be addressed to the American
Standards Institute, 1430 Broadway, New York, NY 10018.)
SOCIETY OF BRITISH AEROSPACE COMPANIES, LTD.
Accessory Drives and Mounting Pads
RS263
(Taper Flange and Involute
Splines)
(Application for copies should be addressed to the Society of
British Aerospace Companies, LTD., Technical Section, 29 King
Street, London SW1Y 6RD, England, U.K.)
3.
REQUIREMENTS
3.1 Precedence. The contract shall have precedence over any
specification.
Any deviation from this specification or from
subsidiary specifications or standards, where applicable, is
subject to approval in writing by the procuring activity.
3.2 First Article. The parts furnished under this specification
shall be a product which has been inspected and passed the first
article inspection specified herein (see 4.2). The Naval Air
Propulsion Center (PE61), Trenton, New Jersey 08628, is the
activity responsible for approving equipment submitted under this
specification.
3.3 Dimensions.
The aircraft engine gas turbine starter/APU
components defined in 3.6.3 shall conform-to the dimensions shown
in Figures 1A through 9. Where only maximum or minimum
dimensions are shown, the starter need not have the shape shown,
but the starter, including all protrusions, shall be contained
within the outline shown. Design details which are shown but are
not specifically required are shown as examples and for
information only; such details are optional.
3.4 Data. Unless otherwise specified in the contract, data
cited in this specification is only required as part of the first
article submittal.
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