• JSSG-2006 Base Document:1998

    Current The latest, up-to-date edition.

    JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES

    Available format(s):  PDF

    Language(s):  English

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

    Add To Cart

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

    1 SCOPE
      1.1 Scope
      1.2 Application
      1.3 Use
      1.4 Deviations
    2 APPLICABLE DOCUMENTS
      2.1 General
      2.2 Government documents
      2.3 Non-Government publications
      2.4 Order of precedence
    3 REQUIREMENTS
      3.1 Detailed structural design requirements
      3.2 General parameters
      3.3 Specific design and construction parameters
      3.4 Structural loading conditions
      3.5 Aeroacoustic durability
      3.6 Vibration
      3.7 Aeroelasticity
      3.8 Required structure survivability - nuclear
      3.9 Required structure survivability - nonnuclear
      3.10 Strength
      3.11 Durability
      3.12 Damage tolerance
      3.13 Durability and damage tolerance control
      3.14 Sensitivity analysis
      3.15 Force management
      3.16 Production facilities, capabilities, and processes
      3.17 Engineering data requirements
    4 VERIFICATION.
      4.1 Detailed structural design requirements
      4.2 General parameters
      4.3 Specific design and construction parameters
      4.4 Structural loading conditions
      4.5 Aeroacoustic durability
      4.6 Vibration
      4.7 Aeroelasticity
      4.8 Required structure survivability - nuclear
      4.9 Required structure survivability - nonnuclear
      4.10 Strength
      4.11 Durability
      4.12 Damage tolerance
      4.13 Durability and damage tolerance control
      4.14 Sensitivity analyses
      4.15 Force management
      4.16 Production facilities, capabilities, and processes
      4.17 Engineering data requirements verification
    5 PACKAGING
      5.1 Packaging
    6 NOTES
      6.1 Definitions
      6.2 Acquisition requirements
      6.3 Subject term (key word) listing
      6.4 International interest
      6.5 Responsible engineering office
    APPENDIX A

    Abstract - (Show below) - (Hide below)

    Describes the joint structural performance and verification requirements for the airframe.

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

    Committee FSG 15GP
    Development Note Supersedes MIL HDBK 336/2. (01/2014)
    Document Type Standard
    Product Note NEW CHILD NOT 1 2019 IS NOW ADDED
    Publisher US Military Specs/Standards/Handbooks
    Status Current
    Supersedes

    Standards Referenced By This Book - (Show below) - (Hide below)

    SAE ARP 1311 : 2015 LANDING GEAR STRUCTURES AND MECHANISMS
    MIL-STD-8591 Base Document:2005 AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE)
    MIL-STD-2088 Revision B:2007 BOMB RACK UNIT (BRU), SINGLE STORE, AIRCRAFT
    MIL-STD-1587 Revision D:2017 MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS
    MIL-HDBK-510 Revision A:2014 AEROSPACE FUELS CERTIFICATION
    SAE ARP 1598 : 2013(R2018) LANDING GEAR SYSTEM DEVELOPMENT PLAN
    MIL-HDBK-1823 Revision A:2009 NONDESTRUCTIVE EVALUATION SYSTEM, RELIABILITY ASSESSMENT
    MIL-HDBK-510-1 Revision A:2010 AEROSPACE FUELS CERTIFICATION
    SAE ARP 5812 : 2017 ACTUATORS, LINEAR MECHANICAL, GENERAL SPECIFICATION GUIDE
    SAE AS 94900 : 2007 AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR
    SAE ARP 1281 : 2002 ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR
    MIL-HDBK-6870 Revision B:2012 NONDESTRUCTIVE INSPECTION PROGRAM REQUIREMENTS FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS
    MIL-HDBK-6870 Revision C:2020 NONDESTRUCTIVE INSPECTION PROGRAM REQUIREMENTS FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS
    MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA
    SAE ARP 5770 : 2012 MECHANICAL CONTROL DESIGN GUIDE
    MIL-DTL-9490 Revision E:2008 FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    JSSG-2009 Revision A:2013 Air Vehicle Subsystems
    MIL-STD-1530 Revision D:2016 AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP)
    MIL-DTL-7700 Revision H:2014 FLIGHT MANUAL, PERFORMANCE DATA APPENDIX, MISSION CREW MANUAL, SUPPLEMENTAL MANUAL, AND ABBREVIATED FLIGHT CREW CHECKLIST
    SAE ARP 94910 : 2012 AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR

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

    MIL-I-81550 Revision C:1983 INSULATING COMPOUND, ELECTRICAL, EMBEDDING, REVERSION RESISTANT SILICONE
    MIL W 87161 : 0 WIRE STRAND, NONFLEXIBLE, FOR AIRCRAFT CONTROL
    MIL S 46059 : C NOTICE 1 STEEL, CARBON & ALLOY, EXTRUDED SHAPES
    MIL HDBK 5 : G_VOL2 METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES
    MIL-M-24041 Revision C:1981 MOLDING AND POTTING COMPOUND
    MIL-R-9299 Revision C:1968 RESIN, PHENOLIC, LAMINATING
    SAE AMS 4890 : 2012 COPPER-BERYLLIUM ALLOY CASTINGS, 97CU - 2.1BE - 0.52CO - 0.28SI, SOLUTION HEAT TREATED (TB00)
    MIL-STD-1530 Revision D:2016 AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP)
    MIL A 8892 : 0 AIRPLANE STRENGTH AND RIGIDITY, VIBRATION
    MIL-A-46146 Revision B:1990 ADHESIVE-SEALANTS, SILICONE, RTV, NONCORROSIVE (FOR USE WITH SENSITIVE METALS AND EQUIPMENT)
    QQ-P-35 Revision C:1988 PASSIVATION TREATMENTS FOR CORROSION-RESISTANT STEEL
    MIL A 8893 : 0 AIRPLANE STRENGTH AND RIGIDITY, SONIC FATIGUE
    MIL-A-8863 Revision C:1993 AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES
    MIL-M-46062 Revision C:1985 MAGNESIUM ALLOY CASTINGS, HIGH STRENGTH
    MIL-STD-2066 Base Document:1981 CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN
    SAE AMS 5581 : 2010 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SEAMLESS OR WELDED TUBING, 62NI - 21.5CR - 9.0MO - 3.7CB (NB), ANNEALED
    QQ-A-200 Revision E:1980 ALUMINUM ALLOY, BAR, ROD, SHAPES, STRUCTURAL SHAPES, TUBE AND WIRE, EXTRUDED, GENERAL SPECIFICATION FOR
    MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    MIL-T-81556 Revision A:1983 TITANIUM & TITANIUM ALLOYS, EXTRUDED BARS AND SHAPES, AIRCRAFT QUALITY
    MIL-T-81259 Revision B:1991 TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR
    MIL-H-6875 Revision H:1989 HEAT TREATMENT OF STEEL RAW MATERIALS
    MIL-A-22771 Revision D:1984 ALUMINUM ALLOY FORGINGS, HEAT TREATED
    MIL B 85110 : A BAR, REPEATABLE RELEASE HOLDBACK, AIRCRAFT LAUNCHING, GENERAL DESIGN REQUIREMENTS FOR
    MIL-G-25871 Revision B:1978 GLASS, LAMINATED, AIRCRAFT GLAZING
    MIL-STD-5400 Base Document:1992 ELECTRONIC EQUIPMENT, AIRBORNE, GENERAL REQUIREMENTS FOR
    ASTM G 85 : 2011 : REDLINE Standard Practice for Modified Salt Spray (Fog) Testing
    MIL-S-8802 Revision F:1990 SEALING COMPOUND, TEMPERATURE-RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES, HIGH ADHESION
    MIL A 008861 : A
    MIL-E-6051 Revision D:1967 ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM
    MIL-A-8870 Revision C:1993 AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
    MIL-STD-45662 Revision A:1988 CALIBRATION SYSTEMS REQUIREMENTS
    QQ-C-390 Revision B:1983 COPPER ALLOY CASTINGS (INCLUDING CAST BAR)
    MIL S 5002 : D SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS
    QQ-A-367 Revision H:1973 ALUMINUM ALLOY FORGINGS
    MIL-G-5485 Revision D:1993 GLASS; LAMINATED, FLAT, BULLET RESISTANT
    ASME B46.1 : 2009 SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY)
    MIL-T-9046 Revision J:1983 TITANIUM AND TITANIUM ALLOY, SHEET, STRIP AND PLATE
    MIL-STD-2175 Revision A:1993 CASTING, CLASSIFICATION AND INSPECTION OF
    MIL-HDBK-275 Revision A:1976 GUIDE FOR SELECTION OF LUBRICANTS, FLUIDS AND COMPOUNDS FOR USE IN FLIGHT VEHICLES AND COMPONENTS
    MIL P 7034 : D PULLEY, GROOVE, ANTIFRICTION BEARING, GREASE LUBRICATED, AIRCRAFT
    MIL-STD-889 Revision C:2016 DISSIMILAR METALS
    MIL-STD-866 Revision C:2007 Grinding of Chrome Plated Steel and Steel Parts Heat Treated to 180,000 PSI or Over
    MIL-P-9400 Revision C:1991 PLASTIC LAMINATE AND SANDWICH CONSTRUCTION PARTS, AIRCRAFT STRUCTURAL PROCESS SPECIFICATION REQUIREMENTS
    MIL A 8862 : 0 AIRPLANE STRENGTH AND RIGIDITY, LANDPLANE, LANDING AND GROUND HANDLING LOADS
    MIL-F-7190 Revision B:1985 FORGING, STEEL, FOR AIRCRAFT AND AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS
    MIL-STD-838 Revision C:1983 LUBRICATION OF MILITARY EQUIPMENT
    MIL-STD-1595 Revision A:1982 QUALIFICATION OF AIRCRAFT, MISSILE AND AEROSPACE FUSION WELDERS
    MIL I 6870 : E INSPECTION PROGRAM REQUIREMENTS NONDESTRUCTIVE FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS
    MIL F 9490 : D FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-STD-1515 Revision A:1978 FASTENER SYSTEMS FOR AEROSPACE APPLICATION
    MIL S 8516 : F SEALING COMPOUND, POLYSULFIDE RUBBER, ELECTRIC CONNECTORS AND ELECTRICAL SYSTEMS CHEMICALLY CURED
    MIL-L-22589 Revision D:1991 LAUNCHING SYSTEM, NOSE GEAR TYPE, AIRCRAFT
    MIL-STD-1757 Revision A:1983 LIGHTNING QUALIFICATION TEST TECHNIQUES FOR AEROSPACE VEHICLES AND HARDWARE
    MIL-STD-2219 Revision A:2005 FUSION WELDING FOR AEROSPACE APPLICATIONS
    MIL H 83282 : C HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, AIRCRAFT, METRIC, NATO CODE NUMBER H 537
    MIL-STD-1568 Revision D:2015 Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems
    MIL-STD-1587 Revision D:2017 MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS
    MIL-STD-2000 Revision A:1991 STANDARD REQUIREMENTS FOR SOLDERED ELECTRICAL AND ELECTRONIC ASSEMBLIES
    ASTM E 390 : 2015 : REDLINE Standard Reference Radiographs for Steel Fusion Welds
    MIL-B-7883 Revision B:1968 BRAZING OF STEELS, COPPER, COPPER ALLOYS, NICKEL ALLOYS, ALUMINUM AND ALUMINUM ALLOYS
    MIL-S-8879 Revision C:1991 SCREW THREADS, CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER, GENERAL SPECIFICATION FOR
    MIL A 008870 : A AIRPLANE STRENGTH AND RIGIDITY FLUTTER, DIVERGENCE AND OTHER AEROELASTIC INSTABILITIES
    MIL-A-8871 Revision A:1971 AIRPLANE, TESTS, STRENGTH AND RIGIDITY FLIGHT AND GROUND OPERATIONS
    MIL-M-38795 Revision B:1982 MANUAL, TECHNICAL, SYSTEM PECULIAR CORROSION CONTROL PREPARATION OF.
    MIL S 23586 : E SEALING COMPOUND, ELECTRICAL, SILICONE RUBBER, ACCELERATOR REQUIRED
    MIL-T-29586 Base Document:1991 THERMOSETTING POLYMER MATRIX, UNIDIRECTIONAL CARBON FIBER REINFORCED PREPREG TAPE (WIDTHS UP TO 60 INCHES), GENERAL SPECIFICATION FOR
    MS33522 Revision C:1984 RIVET, BLIND, STRUCTURAL, MECHANICALLY LOCKED AND FRICTION RETAINER SPINDLE, (RELIABILITY MAINTAINABILITY) DESIGN AND CONSTRUCTION REQUIREMENTS
    MIL-A-21180 Revision D:1984 ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH
    MIL-T-83399 Base Document:1972 TEST FOR REMOVAL OF FLUX RESIDUES
    MIL S 81733 : C SEALING AND COATING COMPOUND CORROSION INHIBITIVE
    MIL-A-8866 Revision C:1987 AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
    MIL-S-29574 Base Document:1989 SEALING COMPOUND, POLYTHIOETHER, FOR AIRCRAFT STRUCTURES, FUEL AND HIGH TEMPERATURE RESISTANT, FAST CURING AT AMBIENT AND LOW TEMPERATURE
    ASTM B 194 : 2015 : REDLINE Standard Specification for Copper-Beryllium Alloy Plate, Sheet, Strip, and Rolled Bar
    MIL-STD-1599 Base Document:1980 BEARINGS, CONTROL SYSTEM COMPONENTS, AND ASSOCIATED HARDWARE USED IN THE DESIGN AND CONSTRUCTION OF AEROSPACE MECHANICAL SYSTEMS AND SUBSYSTEMS
    SAE AMS 5343 : 2014 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)
    MIL A 008862 : A AIRPLANE STRENGTH AND RIGIDITY, LANDING AND GROUND HANDLING LOADS
    MIL-S-8784 Revision B:1971 SEALING COMPOUND, LOW ADHESION, FOR REMOVABLE PANELS AND FUEL TANK INSPECTION PLATES
    MIL-D-8708 Revision C:1991 DEMONSTRATION REQUIREMENTS FOR AIRPLANES
    MIL-W-6858 Revision D:1978 WELDING RESISTANCE, SPOT AND SEAM
    MIL-R-9300 Revision B:1968 RESIN, EPOXY, LOW-PRESSURE LAMINATING
    NAS411:2013 HAZARDOUS MATERIALS MANAGEMENT PROGRAM
    MIL A 008865 : A NOTICE 1 AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS
    SAE AMS 5593 : 2016 NICKEL ALLOY, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE, 45.5NI - 25.5CR - 3.2CO - 3.2MO - 3.2W - 18.5FE, SOLUTION HEAT TREATED
    MIL-B-5087 Revision B:1964 BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
    MIL G 81322 : E GREASE, AIRCRAFT, GENERAL PURPOSE, SIDE TEMPERATURE RANGE, NATO CODE NUMBER G-395
    MIL C 6021 : H NOTICE 1 CASTINGS, CLASSIFICATION AND INSPECTION OF
    MIL-W-6873 Revision C:1991 WELDING FLASH CARBON AND ALLOY STEEL
    MIL-F-83142 Revision A:1969 FORGING, TITANIUM ALLOYS, PREMIUM QUALITY
    MIL-F-7179 Revision G:1993 FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM
    MIL A 83444 : 0 AIRPLANE DAMAGE TOLERANCE REQUIREMENTS
    MIL-A-8860 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR
    MIL-S-7742 Revision D:1991 SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR
    MIL-STD-295 Base Document:1956 BILL OF MATERIAL, PREPARATION OF
    • Access your standards online with a subscription

      Features

      • Simple online access to standards, technical information and regulations
      • Critical updates of standards and customisable alerts and notifications
      • Multi - user online standards collection: secure, flexibile and cost effective