• Shopping Cart
    There are no items in your cart
We noticed you’re not on the correct regional site. Switch to our AMERICAS site for the best experience.
Dismiss alert
Meet Inform Select. Always-on access to the Standards your organisation relies on. Explore Inform Select

MIL-P-5238 Revision C:1974

Current

Current

The latest, up-to-date edition.

Pump, Centrifugal, Fuel Booster, Aircraft, General Specification For

Available format(s)

PDF

Language(s)

English

Published date

12-09-1974

£13.91
Excluding VAT

Gives general requirements for aircraft tank mounted pumps, used for engine feed or transfer

DevelopmentNote
INACTIVE FOR NEW DESIGN 28/8/96
DocumentType
Standard
Pages
23
PublisherName
US Military Specs/Standards/Handbooks
Status
Current

This specification covers the general requirements for aircraft tank mounted centrifugal type, fuel booster pumps, used for engine feed or transfer.

DEFSTAN 00-970(PT0)/9(2012) : 2012 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/14(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/11(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/12(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/13(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/8(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
SAE AIR1749 Aircraft Engine Fuel Feed and Transfer Component Pressure Definitions
SAE ARP1401B Aircraft Fuel System and Component Icing Test

MIL-P-5315 Revision B:1964 PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT (S/S BY SAE-AMS-P-5315)
MIL R 6855 : E RUBBER, SYNTHETIC, SHEETS, STRIPS, MOLDED OR EXTRUDED SHAPES
MIL T 5624 : R TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5
MIL-E-6051 Revision D:1967 Electromagnetic Compatibility Requirements, Systems (S/S by MIL-STD-464)
MIL-G-5572 Revision F:1969 Gasoline, Aviation: Grades 80/87, 100/130, 115/145 (S/S by ASTM-D910)
MIL-F-8615 Revision D:1976 Fuel System Components, General Specification for (S/S by SAE-ARP8615)
MIL-H-5440 Revision H:1993 Hydraulic Systems, Aircraft, Design and Installation Requirements for (S/S by SAE-AS5440)
QQ-P-416 Revision F:1991 Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416)
MIL-W-5088 Revision L:1991 Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881)
MIL C 6021 : H NOTICE 1 CASTINGS, CLASSIFICATION AND INSPECTION OF
MIL V 7899 : C VALVE, CHECK, AIRCRAFT FUEL SYSTEM
MIL-S-7742 Revision D:1991 Screw Threads, Standard, Optimum Selected Series: General Specification for

£13.91
Excluding VAT