MIL-P-5238C
12 September 1974
SUPERSEDING
MIL-P-5238B
2 February 1961
MILITARY SPECIFICATION
PUMP, CENTRIFUGAL, FUEL BOOSTER, AIRCRAFT,
GENERAL SPECIFICATION FOR
This specification is approved for use by all Departments
and Agencies of the Department of Defense.
SCOPE
1.
1.1 This specification covers the general requirements for aircraft tank
mounted centrifugal type, fuel booster pumps, used for engine feed or transfer.
2.
APPLICABLE DOCUMENTS
2.1 The following documents of the issue in effect on date of invitation for
bids or request for proposal, form a part of this specification to the extent
specified herein.
SPECIFICATIONS
Federal
QQ-P-416
Plating, Cadmium (Electrodeposited)
Military
MIL-D-1OOO
Drawings, Engineering and Associated Lists
Wiring; Aircraft, Selection and Installation of
MIL-W-5088
MIL-P-5315
Packing, Preformed, Hydrocarbon Fuel Resistant
MIL-H-5440
Hydraulic Systems, Aircraft Types I & II, Design,
Installation, and Data Requirements for
MIL-G-5572
Gasoline, Aviation, Grades 80/87, 100/130, 115/145
MIL-T-S624
Turbine Fuel, Aviation, Grades JP-4 and JP-5
MIL-C-6021
Casting, Classification and Inspection of
MIL-E-6051
Electromagnetic Compatibility Requirements, Systems
MIL-R-6855
Rubber, Synthetic, Sheets, Strips, Molded or Extruded Shapes
MIL-S-7742
Screw Threads, Standard, Optimum Selected Series, General
Specification for
Valve, Check, Aircraft Fuel System
MIL-V-7899
MIL-F-8615
Fuel System Components, General Specification for
Screw Threads, Controlled Radius, Root with Increased Minor
MIL-T-8879
Diameter, General Specification for
FSC 2915
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