(c)
Verification that all appropriate plugs and caps are installed.
WARNING: TAPE SHALL NOT BE USED TO COVER ELECTRICAL CONNECTORS OR FLUID FITTINGS/OPENINGS. ADHESIVE RESIDUE CAN INSULATE ELECTRICAL CONNECTORS AND CONTAMINATE HYDRAULIC OR FUEL UNITS.
(d)
Check for damage, corrosion, and deterioration.
(e)
Ensure certain components are kept in the proper packaging to protect them from damage, i.e., indicators, rate gyroscopes, fire bottles and so on.
(f)
Ensure that Electrostatic Discharge Sensitive Devices (ESDs) are protected with protective bags or caps. If units are in plastic bags do not remove them.
(g)
Verification that all appropriate documentation, in accordance with Figure 8-2 of this section, is properly completed and signed.
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A Wholly Owned Subsidiary of AMES, Inc.
(h) Receiving inspection for aircraft fasteners shall include a sample visual inspection for general workmanship and the presence of physical and chemical test certification from the manufacturer or other FAA regulated source.
NOTE: If the materials/components don’t meet the above criteria, you must fill out the quarantine paperwork and place them in the Quarantine area. The Manager of Quality Control will check on all quarantines for proper disposition.
F. Verify that the identification on the part has not been tampered with, i.e., stamped over, label or part/serial numbers improper/missing, vibro-etch or serial numbers located at other than the normal location, except modified parts. Ensure that the shelf life and/or life limit has not expired, if applicable.
G. Conduct a visual inspection of the part and supporting documents to the extent necessary to determine if the part is traceable to: 1) a prior source and 2) bear acceptable documentation that conforms to at least one of the receipt requirements listed in Appendix A. The following are examples of positive forms of identification:
(1)
FAA form 8130-3, Authorized Release Certificate, with FAR 43.9 release.
(2)
E.A.S.A. - European Aviation Safety Agency.
NOTE: This is only acceptable if it cites the part meets the required FAA standards in block 13.
Maintenance records or release document with approval for return to service.
Airline Condition Tag.
FAA TSO markings.
FAA PMA markings.
FAA Production or Type Certificate (PC, TC) holder, i.e., Boeing, Douglas, PWA, GE, etc. The certificate number is to be listed on certification documents.
Shipping ticket / invoice from Production Approval Holder (PAH).
Direct ship authority letter from PAH.
NOTE: For definitions of abbreviations and acronyms see Explanation of Terms.
Evaluate any visible irregularities (e.g., altered or unusual surface, absence of required plating, evidence of prior usage, scratches, new paint over old, attempted exterior repair, pitting or corrosion). 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：AMES MATERIAL SERVICES, INC.PROCEDURES MANUAL(27)
