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  • JSGS-87231 Revision A:1995

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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    ENGINES, AIRCRAFT, TURBINE

    Available format(s):  PDF

    Superseded date:  06-02-2001

    Language(s): 

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Table of Contents - (Show below) - (Hide below)

    1 SCOPE
      1.1 Structure
      1.2 Handbook
      1.3 Deviations
      1.4 Environmental impact statement
    2 APPLICABLE DOCUMENTS
      2.1 General
      2.2 Government documents
      2.3 Non-Government publications
      2.4 Order of precedence
      2.5 Streamlining
    3 REQUIREMENTS
      3.1 Design
      3.2 Performance and operability
      3.3 Environmental conditions
      3.4 Integrity
      3.5 Reliability and maintainability
      3.6 Combat survivability
      3.7 Subsystems
      3.8 Software resources
      3.9 Engine system controls and externals (C&E) evaluation
      3.10 Engine qualification
    4 EVALUATION AND QUALIFICATION
      4.1 Design (configuration) and construction
      4.2 Performance and operability
      4.3 Environmental conditions
      4.4 Integrity
      4.5 Reliability and maintainability (R&M)
      4.6 Combat survivability
      4.7 Subsystems
      4.8 Software resources
      4.9 Engine system controls and external (C&E) evaluation
      4.10 Engine qualification
    5 PACKAGING
      5.1 Preparation for storage and shipment
    6 NOTES
      6.1 Intended use
      6.2 Acquisition requirements
      6.3 Consideration of data requirements
      6.4 Definitions
      6.5 Symbols, subscripts, abbreviations and acronyms
      6.6 Material safety data sheets
      6.7 Subject term (key word) listing
      6.8 Metrication
      6.9 Responsible engineering office
      6.10 Streamlining
      6.11 Spec tree
      6.12 Tables and figures
      6.13 Changes from previous issue
    APPENDIX A - ENGINES, AIRCRAFT, TURBINE, HANDBOOK FOR

    Abstract - (Show below) - (Hide below)

    Describes establishes the item definition, performance, operating characteristics, reliability, maintainability, subsystems, physical characteristics, general design, installation, and interface requirements for manned aircraft gas turbine engines.

    General Product Information - (Show below) - (Hide below)

    Committee FSC 2840
    Development Note Supersedes MIL E 87231. A NOTICE 1 - Notice of Cancellation/Superseded by JSSG 2007. (04/2004)
    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Superseded
    Superseded By

    Standards Referencing This Book - (Show below) - (Hide below)

    SAE ARP 755 : 2014 AIRCRAFT PROPULSION SYSTEM PERFORMANCE STATION DESIGNATION AND NOMENCLATURE
    MS33540 Revision J:1986 SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR
    MS33787 Revision D:1984 WRENCHING ELEMENT, EXTERNAL SPLINE, DIMENSIONS FOR
    MIL-E-5607 Revision F:1983 ENGINE, GAS TURBINE, PREPARATION FOR STORAGE AND SHIPMENT OF, PROCESS FOR
    SAE ARP 1179 : 2011 AIRCRAFT GAS TURBINE ENGINE EXHAUST SMOKE MEASUREMENT
    VV-F-800 Revision E:1987 FUEL OIL, DIESEL
    MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    MIL-STD-130 Revision N:2007 IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
    MIL STD 2084 : 0 GENERAL REQUIREMENTS FOR MAINTAINABILITY OF AVIONIC AND ELECTRONIC SYSTEMS AND EQUIPMENT
    MIL H 27267 : B HOSE TETRAFLUOROETHYLENE, HIGH TEMPERATURE, MEDIUM PRESSURE
    MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    MIL H 25579 : E HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR
    MIL C 85704 : B CLEANING COMPOUND, TURBINE ENGINE GAS PATH
    TIA 455-21 : A1988(R2012) FOTP-21 MATING DURABILITY FOR FIBER OPTIC INTERCONNECTING DEVICES
    MIL-E-6051 Revision D:1967 ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM
    MS9006 Revision C:1963 RECESSES-CROSS, LOW TORQUE DRIVE, DIMENSIONS AND GAGE DIMENSIONS FOR
    SAE AMS 2432 : 2013 SHOT PEENING, COMPUTER MONITORED
    MIL-M-38510 Revision J:1991 MICROCIRCUITS, SPECIFICATION FOR
    SAE AS 568 : 2014 AEROSPACE SIZE STANDARD FOR O-RINGS
    SAE ARP 1256 : 2011 PROCEDURE FOR THE CONTINUOUS SAMPLING AND MEASUREMENT OF GASEOUS EMISSIONS FROM AIRCRAFT TURBINE ENGINES
    MIL STD 470 : B MAINTAINABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS)
    MIL-STD-889 Revision C:2016 DISSIMILAR METALS
    MIL E 5400 : T ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR
    MIL-STD-1529 Base Document:1955 VENDOR SUBSTANTABLE FOR AEROSPACE PROPULSION SYSTEM ITEMS
    MIL-STD-1815 Revision A:1983
    MIL C 7024 : D CALIBRATING FLUID, AIRCRAFT FUEL SYSTEM COMPONENTS
    SAE AMS 2432 : 2013 SHOT PEENING, COMPUTER MONITORED
    SAE AS 870 : 2015 WRENCHING CONFIGURATION, BI-HEXAGONAL (12 POINT) DRIVE, DESIGN STANDARD FOR
    MIL C 38999 : J CONNECTOR, ELECTRICAL, CIRCULAR, MINIATURE, HIGH DENSITY, QUICK DISCONNECT (BAYONET THREADED & BREECH COUPLING) ENVIRONMENT RESISTANT, REMOVABLE CRIMP & HERMETIC SOLDER CONTACTS
    MS33588 Revision E:1984 NUTS, SELF LOCKING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY USAGE REQUIREMENTS FOR
    TT-S-735 Revision A:1988 STANDARD TEST FLUIDS, HYDROCARBON
    TIA 455-20 : B2004(R2013) OPTICAL FIBRES - PART 1-46: MEASUREMENT METHODS AND TEST PROCEDURES - MONITORING OF CHANGES IN OPTICAL TRANSMITTANCE
    MIL-F-17874 Revision B:1965 FUEL SYSTEMS, AIRCRAFT, INSTALLATION AND TEST OF
    MS33537 Revision E:1974 INSERT, SCREW THREAD, HELICAL COIL, COARSE AND FINE THREAD, STANDARD DIMENSIONS FOR
    MIL-STD-1818 Revision A:1993 ELECTROMAGNETIC EFFECTS REQUIREMENTS FOR SYSTEMS
    MIL-C-24621 Revision B:1991 COUPLER, PASSIVE, FIBER OPTIC, GENERAL SPECIFICATION FOR (METRIC)
    MIL STD 1800 : A NOTICE 1 HUMAN ENGINEERING PERFORMANCE REQUIREMENTS FOR SYSTEMS
    MIL-STD-882 Revision E:2012 System Safety
    MIL-S-8879 Revision C:1991 SCREW THREADS, CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER, GENERAL SPECIFICATION FOR
    MIL-STD-471 Revision A:1973 MAINTAINABILITY DEMONSTRATION
    MIL S 19500 : J SEMICONDUCTOR DEVICES, GENERAL SPECIFICATION FOR
    MIL-STD-100 Revision G:1997 ENGINEERING DRAWINGS
    MIL-STD-1472 Revision G:2012 HUMAN ENGINEERING
    SAE ARP 1420 : 2002 GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES
    MIL F 16884 : J FUEL, NAVAL DISTILLATE
    MIL-H-46855 Revision B:1979 HUMAN ENGINEERING REQUIREMENTS FOR MILITARY SYSTEMS, EQUIPMENT & FACILITIES
    MIL C 85045 : E CABLES, FIBER OPTICS, (METRIC), GENERAL SPECIFICATION FOR
    SAE AS 681 : 2016 GAS TURBINE ENGINE PERFORMANCE PRESENTATION FOR COMPUTER PROGRAMS
    MIL-STD-721 Revision C:1981 DEFINITIONS OF EFFECTIVENESS TERMS FOR RELIABILITY MAINTAINABILITY, HUMAN FACTORS, AND SAFETY
    MIL-STD-2173 Base Document:1986 RELIABILITY-CENTERED MAINTENANCE REQUIREMENTS FOR NAVAL AIRCRAFT, WEAPONS SYSTEMS AND SUPPORT EQUIPMENT
    MIL-T-5544 Revision C:1991 THREAD COMPOUND, ANTISEIZE, GRAPHITE-PETROLATUM
    MIL-STD-785 Revision B:1980 RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION
    MS33602 Base Document:1967 BOLT, SELF RETAINING AIRCRAFT RELIABILITY AND MAINTAINABILITY DESIGN AND USAGE REQUIREMENTS FOR
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