MIL STD 1843 : 0
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
RELIABILITY-CENTERED MAINTENANCE FOR AIRCRAFT, ENGINES AND EQUIPMENT
09-08-1995
Describes maintenance requirements using Reliability-Centered Maintenance Analysis for Air Force aircraft and engine systems, structures and equipment, including special and common Support Equipment, communications and Electronics equipment, weapons, vehicles and similar items.
| Committee |
AREA ILSS
|
| DevelopmentNote |
NOTICE 1 - Notice of Cancellation without Replacement. (01/2013)
|
| DocumentType |
Standard
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
| Supersedes |
| MIL M 5096 : E | MANUAL, TECHNICAL, INSPECTION MAINTENANCE REQUIREMENTS WORK CARD, INSPECTION LUBRICATION REQUIREMENTS, ACCEPTANCE FUNCTIONAL CHECK FLIGHT PROCEDURES, CHECK LISTS, FUNCTION CHECK FLIGHT, CHARTS, INSPECTION SEQUENCE |
| GEIA TA HB 0009 : 2013 | RELIABILITY PROGRAM HANDBOOK |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-HDBK-87244 Base Document:1995 | AVIONICS/ELECTRONICS INTEGRITY |
| MIL-STD-1388-2 Revision B:1991 | DOD REQUIREMENTS FOR A LOGISTIC SUPPORT ANALYSIS RECORD |
| SAE ARP5638 | RMS Terms and Definitions |
| SAE JA6097_201305 | Using a System Reliability Model to Optimize Maintenance Costs A Best Practices Guide |
| NASA MSFC HDBK 3074 : 2002 | SELECTION METHODOLOGY FOR ORBITAL REPLACEABLE UNITS |
| MIL-STD-1530 Revision D:2016 | AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) |
| MIL M 5096 : E | MANUAL, TECHNICAL, INSPECTION MAINTENANCE REQUIREMENTS WORK CARD, INSPECTION LUBRICATION REQUIREMENTS, ACCEPTANCE FUNCTIONAL CHECK FLIGHT PROCEDURES, CHECK LISTS, FUNCTION CHECK FLIGHT, CHARTS, INSPECTION SEQUENCE |
| MIL-STD-1783 Base Document:1984 | ENGINE STRUCTURAL INTEGRITY PROGRAM (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503) |
| MIL-STD-1388-1 Revision A:1983 | LOGISTIC SUPPORT ANALYSIS |
| MIL-STD-1629 Revision A:1980 | PROCEDURES FOR PERFORMING A FAILURE MODE, EFFECTS AND CRITICALITY ANALYSIS |
| MIL-STD-721 Revision C:1981 | DEFINITIONS OF EFFECTIVENESS TERMS FOR RELIABILITY MAINTAINABILITY, HUMAN FACTORS, AND SAFETY |
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