MIL-STD-2199A APPENDIX B
e. Prepare the bare steel area(s) and sleeve end prep area(s) for application of GRP in accordance with A.3.1.1 as applicable.
f. Apply sealing/fairing compound to contour the sleeve end to the shaft in accordance with A.2.2.3.
g. Allow a minimum of 2 hours for the fairing compound to cure and then accomplish steps B.3.1.2.2.2.i through k.
B.3.1.3 Waterborne inspection and repair. Refer to S0600-AA-PR0-130/13 for further direction.
B.3.2 Reports. Comments on the results of the in-service inspection shall be forwarded with the initial inspection report specified. A brief description of corrective repairs which may be necessary shall be forwarded with the final inspection report required.
32
For Parts Inquires call Parts Hangar, Inc (727) 493-0744
© Copyright 2015 Integrated Publishing, Inc.
A Service Disabled Veteran Owned Small Business