 |
|||
|
Page Title:
Test method of interchangeability |
|
||
| ||||||||||
|
|  MIL-T-63536(AR)
4.7.2 Repair parts. At least two parts of concurrent repair parts shall
be subjected to the interchangeability test specified in 4.7.3. Failure of
any part to meet the interchangeability requirements shall be cause for
rejection, subject to reconditioning and further test. A sample consisting of
double the number of parts used in the original test shall be tested using the
test methods specified above.
4.7.3 Test method of interchangeability. Control assemblies shall be
tested by disassembling and then reassembling the parts specified below. Parts
shall be disassembled from the control and identical parts placed together and
mixed. Any commercial part (screws, pins, etc.) rendered unserviceable by
disassembly shall be replaced without penalty to the interchangeability test.
List of Interchangeable Parts
Drawing
Component
11830922
Logic Control Unit Assembly
11830441
Component Assembly, Power Supply and Clearing
11830988
Component Assembly, Torque Command
11830531
Case, Logic Control Unit
11830724
Component Assembly, Coincidence Sensor
11830797
Component Assembly, Interconnection
11830798
Component Assembly, Depression Limit
4.7.4 Repair parts. Concurrent repair parts shall be tested by
disassembling two control assemblies previously tested in 4.7.3 and then
reassembling them using the concurrent repair parts. No hand refinement of
parts will be allowed, and the assembled control assemblies shall operate and
function as intened. This test may be performed independently of the control
assembly interchangeability testing specified in 4.7.1 and at more frequent
intervals using accepted drive assemblies taken from current production.
4.8 Proof test (first article inspection only). When specified in the
contract (see 6.2) three Logic Control Unit Assemblies shall be forwarded
to the site specified by the contracting agency and assembled to an accepted
Universal Turret Subsystem (UTS). The Logic Control Unit Assemblies shall
function in accordance to the intent of the design and with no evidence of
malfunction. When approved by the contracting agency, this test may be
performed at the aircraft system level.
5. PACKAGING
5.1 Preservation, packaging, packing and marking. The logic control
assemblies shall be prepared, packaged, packed and marked in accordance with
the requirements of the Preservation and Packaging Data for Drawing P11830922
for the level of protection specified in the contract. (See 6.2.)
5.1.1 Spare parts or replacement parts. Spare parts or replacement parts
shall be cleaned, perserved, packaged and packed as specified in the contract
or order.
36
|
|
Privacy Statement - Press Release - Copyright Information. - Contact Us |
Click
here for thousands of PDF manuals