MIL-STD-867 Temper Etch InspectionThis standard establishes requirements and test for performing temper etch inspection of carburized steels and tool and low alloy steels, which are heat treated above 1.24 x 109 Pascal PA 1.26 x 102 kilogram - force/square millimeter Kgf/mm2 or 1.8 x 105 pound - force/square inch psi. This standard applies to aircraft and missiles structural and propulsion system components when MIL-HDBK-6870 for guidance only and/or MIL-STD-866 are reference documents in the solicitation or contract.

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MIL-STD-867C

6.   NOTES

(This section contains information of a general or explanatory nature that may be helpful, but is not mandatory.)

6.1   Intended use.   This standard provides the step by step process and procedures for temper etch to be used during repair process and acquisition of spares for the landing gear of all military aircraft.

6.2     Subject term (key word) listing.

Equipment Materials Process

6.3    Changes from previous issue.   The margins of this standard are marked with vertical lines to indicate modifications generated by this change.  This was done as a convenience only and the Government assumes no liability whatsoever for an inaccuracies in these notations.  Bidders and contractors are cautioned to evaluate the requirements of this document based on the entire content irrespective of the marginal notations.

CONCLUDING MATERIAL

Custodian:        Preparing Activity: Air Force - 70                                                                        Air Force - 70

(Project: NDTI-2009-002)

NOTE:    The activities listed above were interested in this document as of the date of this document.  Since organizations and responsibilities can change, you should verify the currency of the information above using ASSIST Online database at https://assist.daps.dla.mil.

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