JSSG-2006 Base Document:1998
Current
The latest, up-to-date edition.
JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES
English
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
Describes the joint structural performance and verification requirements for the airframe.
Committee |
FSG 15GP
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DevelopmentNote |
Supersedes MIL HDBK 336/2. (01/2014)
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DocumentType |
Standard
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Pages |
497
|
ProductNote |
NEW CHILD NOT 1 2019 IS NOW ADDED
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PublisherName |
US Military Specs/Standards/Handbooks
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Status |
Current
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Supersedes |
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 |
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 |
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