MIL-STD-1798 Mechanical Equipment And Subsystems Integrity ProgramThe purpose of this standard is to describe the general process to achieve and maintain the physical and functional integrity of the mechanical elements of aircraft systems. The goal of this integrity program is to achieve the desired level of safety and aircraft availability at the most economic cost across the life cycle of the weapon system. This standard allows the process to be tailored in a competitive environment to meet specific equipment, subsystem, and/or system requirements. The Mechanical Equipment and Subsystems Integrity Program MECSIP is implemented in the planning process and continued until retirement of the system.

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MIL-STD-1798C

(Copies of these documents are available from AFLCMC/ENRS, 2145 MONAHAN WAY, WRIGHT-PATTERSON AFB OH  45433-7017; e-mail: AFLCMC/EN_EZ Engineering Standards.)

FEDERAL AVIATION ADMINISTRATION (FAA) ADVISORY CIRCULARS

AC 25-27A                              Development of Transport Category Airplane EWIS ICA Using an Enhanced Zonal Analysis Procedure

AC 25.1309-1A                       System Design and Analysis

AC 25.1701-1                         Certification of EWIS on Transport Category Airplanes

ORDER

Order 8110.101                      Type Certification Procedures For Military Commerical

Derivative Aircraft

(Copies of these documents are available online at www.faa.gov.)

2.3  Non-Government publications.

The following documents form a part of this document to the extent specified herein.  Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract.

AIR TRANSPORT ASSOCIATION OF AMERICA, INC.

ATA Publication MSG-3         Operator/Manufactured Scheduled Maintenance

Development

(Requests for this document should be addressed to the Air Transport Association of America, Inc.; 1301 Pennsylvania Avenue, NW; Suite 1100; Washington DC  20004-1707  USA; https://publications.airlines.org.)

SAE INTERNATIONAL

AMS-A-21180                         Aluminum-Alloy Castings, High Strength

AMS2175                               Casting, Classification and Inspection of

AMS5343                               Steel, Corrosion Resistant, Investment Castings

16Cr - 4.1Ni - 0.28Cb (Nb) - 3.2Cu Homogenization, Solution, and Precipitation Heat Treated (H1000)

150 ksi (1034 MPa) Tensile Strength (17-4)

AS50881                                Wiring, Aerospace Vehicle

(Copies of these documents are available from  SAE International, 400 Commonwealth Drive, Warrendale PA  15096-0001 USA; www.sae.org.)

2.4  Order of precedence.

Unless otherwise noted herein or in the contract, in the event of a conflict between the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.

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