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    JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    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 : 0 AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE)
    MIL STD 1587 : D MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS
    MIL HDBK 510 : A AEROSPACE FUELS CERTIFICATION
    SAE ARP 1598 : 2013(R2018) LANDING GEAR SYSTEM DEVELOPMENT PLAN
    MIL HDBK 1823 : A NONDESTRUCTIVE EVALUATION SYSTEM, RELIABILITY ASSESSMENT
    MIL HDBK 510-1 : A 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 : B NONDESTRUCTIVE INSPECTION PROGRAM REQUIREMENTS FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS
    MIL-HDBK-6870C:2020 NONDESTRUCTIVE INSPECTION PROGRAM REQUIREMENTS FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS
    MIL HDBK 516 : C AIRWORTHINESS CERTIFICATION CRITERIA
    SAE ARP 5770 : 2012 MECHANICAL CONTROL DESIGN GUIDE
    MIL DTL 9490 : E FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    JSSG 2009 : A AIR VEHICLE SUBSYSTEMS (JOINT SERVICE SPECIFICATION GUIDE)
    MIL STD 1530 : D AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP)
    MIL DTL 7700 : H 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 : C 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 : C MOLDING AND POTTING COMPOUND
    MIL R 9299 : C 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 : D AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP)
    MIL A 8892 : 0 AIRPLANE STRENGTH AND RIGIDITY, VIBRATION
    MIL A 46146 : B ADHESIVE-SEALANTS, SILICONE, RTV, NONCORROSIVE (FOR USE WITH SENSITIVE METALS AND EQUIPMENT)
    QQ P 35 : C PASSIVATION TREATMENTS FOR CORROSION-RESISTANT STEEL
    MIL A 8893 : 0 AIRPLANE STRENGTH AND RIGIDITY, SONIC FATIGUE
    MIL A 8863 : C AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES
    MIL M 46062 : C MAGNESIUM ALLOY CASTINGS, HIGH STRENGTH
    MIL STD 2066 : 0 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 : E ALUMINUM ALLOY, BAR, ROD, SHAPES, STRUCTURAL SHAPES, TUBE AND WIRE, EXTRUDED, GENERAL SPECIFICATION FOR
    MIL STD 810 : G ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    MIL T 81556 : A TITANIUM & TITANIUM ALLOYS, EXTRUDED BARS AND SHAPES, AIRCRAFT QUALITY
    MIL T 81259 : B TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR
    MIL H 6875 : H HEAT TREATMENT OF STEEL RAW MATERIALS
    MIL A 22771 : D ALUMINUM ALLOY FORGINGS, HEAT TREATED
    MIL B 85110 : A BAR, REPEATABLE RELEASE HOLDBACK, AIRCRAFT LAUNCHING, GENERAL DESIGN REQUIREMENTS FOR
    MIL G 25871 : B GLASS, LAMINATED, AIRCRAFT GLAZING
    MIL STD 5400 : 0 ELECTRONIC EQUIPMENT, AIRBORNE, GENERAL REQUIREMENTS FOR
    ASTM G 85 : 2011 : REDLINE Standard Practice for Modified Salt Spray (Fog) Testing
    MIL S 8802 : F SEALING COMPOUND, TEMPERATURE-RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES, HIGH ADHESION
    MIL A 008861 : A
    MIL E 6051 : D ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM
    MIL A 8870 : C AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
    MIL STD 45662 : A CALIBRATION SYSTEMS REQUIREMENTS
    QQ C 390 : B COPPER ALLOY CASTINGS (INCLUDING CAST BAR)
    MIL S 5002 : D SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS
    QQ A 367 : H ALUMINUM ALLOY FORGINGS
    MIL G 5485 : D GLASS; LAMINATED, FLAT, BULLET RESISTANT
    MIL T 9046 : J TITANIUM AND TITANIUM ALLOY, SHEET, STRIP AND PLATE
    MIL STD 2175 : A CASTING, CLASSIFICATION AND INSPECTION OF
    MIL HDBK 275 : A 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 : C DISSIMILAR METALS
    MIL STD 866 : C GRINDING OF CHROME PLATED STEEL AND STEEL PARTS HEAT TREATED TO 180,000 PSI OR OVER
    MIL P 9400 : C 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 : B FORGING, STEEL, FOR AIRCRAFT AND AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS
    MIL STD 838 : C LUBRICATION OF MILITARY EQUIPMENT
    MIL STD 1595 : A 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 : A FASTENER SYSTEMS FOR AEROSPACE APPLICATION
    MIL S 8516 : F SEALING COMPOUND, POLYSULFIDE RUBBER, ELECTRIC CONNECTORS AND ELECTRICAL SYSTEMS CHEMICALLY CURED
    MIL L 22589 : D LAUNCHING SYSTEM, NOSE GEAR TYPE, AIRCRAFT
    MIL STD 1757 : A LIGHTNING QUALIFICATION TEST TECHNIQUES FOR AEROSPACE VEHICLES AND HARDWARE
    MIL STD 2219 : A 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 : D MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS
    MIL STD 1587 : D MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS
    MIL STD 2000 : A STANDARD REQUIREMENTS FOR SOLDERED ELECTRICAL AND ELECTRONIC ASSEMBLIES
    ASTM E 390 : 2015 : REDLINE Standard Reference Radiographs for Steel Fusion Welds
    MIL B 7883 : B BRAZING OF STEELS, COPPER, COPPER ALLOYS, NICKEL ALLOYS, ALUMINUM AND ALUMINUM ALLOYS
    MIL S 8879 : C 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 : A AIRPLANE, TESTS, STRENGTH AND RIGIDITY FLIGHT AND GROUND OPERATIONS
    MIL M 38795 : B MANUAL, TECHNICAL, SYSTEM PECULIAR CORROSION CONTROL PREPARATION OF.
    MIL S 23586 : E SEALING COMPOUND, ELECTRICAL, SILICONE RUBBER, ACCELERATOR REQUIRED
    MIL T 29586 : 0 THERMOSETTING POLYMER MATRIX, UNIDIRECTIONAL CARBON FIBER REINFORCED PREPREG TAPE (WIDTHS UP TO 60 INCHES), GENERAL SPECIFICATION FOR
    MS 33522 : C RIVET, BLIND, STRUCTURAL, MECHANICALLY LOCKED AND FRICTION RETAINER SPINDLE, (RELIABILITY MAINTAINABILITY) DESIGN AND CONSTRUCTION REQUIREMENTS
    MIL A 21180 : D ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH
    MIL T 83399 : 0 TEST FOR REMOVAL OF FLUX RESIDUES
    MIL S 81733 : C SEALING AND COATING COMPOUND CORROSION INHIBITIVE
    MIL A 8866 : C AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
    MIL S 29574 : 0 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 : 0 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 : B SEALING COMPOUND, LOW ADHESION, FOR REMOVABLE PANELS AND FUEL TANK INSPECTION PLATES
    MIL D 8708 : C DEMONSTRATION REQUIREMENTS FOR AIRPLANES
    MIL W 6858 : D WELDING RESISTANCE, SPOT AND SEAM
    MIL R 9300 : B RESIN, EPOXY, LOW-PRESSURE LAMINATING
    NAS 411 : 0 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 : B 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 : C WELDING FLASH CARBON AND ALLOY STEEL
    MIL F 83142 : A FORGING, TITANIUM ALLOYS, PREMIUM QUALITY
    MIL F 7179 : G FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM
    MIL A 83444 : 0 AIRPLANE DAMAGE TOLERANCE REQUIREMENTS
    MIL A 8860 : B AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR
    MIL S 7742 : D SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR
    MIL STD 295 : 0 BILL OF MATERIAL, PREPARATION OF
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