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|  MIL-S-22518A(AS)
test sample shall be plainly identified by securely attached tags clearly
and durably marked with the following information, and shall be forwarded
to the Commanding Officer, Naval Air Propulsion Center, Attn: PE62,
Trenton, New Jersey 08628, after obtaining authorization from the qualifying
activity for submittal of the qualification test samples:
Sample for Qualification Test
Submittal by (name) (date) for qualification test
in accordance with the requirements of
Specification MIL-S-22518A(AS) (date) under
authorization (reference letter authorizing tests).
Starter, Air Turbine, Accessory Drive, Combination,
Aircraft Engine, General Specification for
Manufacturer's Part Number
Name of Manufacturer
Specification Sheet Number or other identification
Navy Work Unit Assignment Number
4.3.1.1
Qualification test report. The supplier shall
furnish performance data on each model ATS/AD they propose to have
qualified to the qualifying activity in accordance with the requirements
of 4.3.1 herein. The data shall be in the form shown on Figures 1
through 5, and may be estimated or calculated until the ATS/AD has been
tested. After that time, performance data shall be based on test results.
The report shall demonstrate that the size of the ATS/AD is within the
envelope configuration specified on the applicable Specification Sheet.
The ATS/AD installation configuration shall be as shown thereon and
shall be subject to approval by the qualifying activity. Manufacturers
interested in qualifying ATS/ADs to this specification are required to
coordinate installation with the qualifying activity prior to fabrication
of qualification units. The manufacturer's approved installation drawing
shall form a part of this specification.
4.3.1.2
Drawings and diagrams. The manufacturer shall
furnish the following drawings and diagrams to the qualifying activity
with the submission of the qualification test samples.
a.
ATS/AD installation drawing - the drawing shall
show ATS/AD center of gravity, all connecting fittings, clearance required
for installation and removal, filter locations and cleaning instructions
if applicable.
b.
Electrical diagram - the electrical diagram
shall show all electrical circuits up to the connecting points of the
aircraft electrical system.
c.
A complete cutaway or cross-sectional drawing
of the ATS/AD and all components showing all parts in their normal
assembled position and shall specify part numbers of all parts or components
subassemblies. The following data shall be furnished on or together
with the assembly drawing:
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