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|  MIL-P-85315
1.0 SCOPE
1.1 Scope - This specification covers the requirements for an aircraft fuel
booster (or transfer) ejector pump. The pump shall meet all requirements herein
and the requirements of MIL-P-85315, General Ejector Pump Specification.
1.2 Classification - The fuel booster (or transfer) ejector shall be of the
following
(insert the contractor's model designation; also include
a brief description of the ejector and its operation.)
2.0 APPLICABLE DOCUMENTS
2.1 The following documents, of the issue in effect on date of invitation for
proposals, form a part of this specification to the extent specified herein:
SPECIFICATIONS
Military
MIL-P-85315
Pump, Ejector, Air Vehicle, Fuel, General Specification for
Grades 80/87, 91/96, 100/130, 115/145
Aviation;
Gasoline,
MIL-G-5572
Jet Fuel, Grades JP-3, JP-4, and JP-5
MIL-T-5624
Jet Fuel, Grade JP-8
MIL-T-83133
STANDARDS
Military
(list all additional Government publications not covered
this specification which are applicable to this pump).
3.0 REQUIREMENTS
3.8.1 Calibration - The ejector shall have the capacities, rated flows, dis-
charge pressures, specified by the Contractor, using fuel in accordance with
MIL-P-85315. (Insert the applicable specification number)
3.11 Dimensions - A drawing shall be furnished with this model specification,
showing the outline and mounting dimensions for the ejector.
3.12 Mass - The weight of the ejector, complete as a working assembly, shall
kg.
not exceed
4.0 QUALITY ASSURANCE PROVISIONS
4.6.2 Calibration - The ejector shall be operated over its entire permissible
(Data covering discharge pressure shall be recorded.)
range of flow rates.
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