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| ![]() MIL-F-8615D
2.2 Other publications. The following documents form a part of this specifi-
cation to the extent specified herein. Unless otherwise indicated, the issue
in effect on date of invitation for bids or request for proposal shall apply.
Society of Automotive Engineers
Pressure Drop Test for Fuel System Components
ARP 868
(Copies of the above publication may be obtained from the Society of Automotive
Engineers, Two Pennsylvania Plaza, New York, New York 10001.)
American Society for Testing and Materials
Aviation Turbine Fuels
ASTM-D1655
ASTM-E380-74
Metric Practice Guide
(Copies of the above documents may be obtained from the American Societ for
Testing and Materials, 1916 Race Street, Philadelphia, PA 19106.)
3.
REQUIREMENTS
3.1 First article. Unless otherwise specified, the assemblies furnished. under
this specification shall have been inspected and passed the first artic
inspection specified herein.
3.2 Item specification. A specification providing all design and performance
details shall be submitted by the contractor to the procuring agency for ap-
proval. The item specification shall reiterate all applicable requirements of
this specification inserting the necessary specific and special requirements.
The item specification shall include a specification control drawing.
3.2.1 Drawings. The installation and outline drawings shall be in accordance
with MIL-D-1OOO. At the time and place of first article approval, the data
shall include the detailed assembly drawing(s) with the parts list showing
the material, coating, temper, special finishes for all parts and applicable
processes and assembly procedures, as applicable.
3.2.2 Weight. The allowable wet and dry weights of the component shall be
stated in the item specification.
3.3 Selection of standards and specifications. Standards and specificat ions
for commodities and services not specified herein, shall be selected in accord-
ance with MIL-STD-143.
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