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JSSG-2006 Base Document:1998

Current
Current

The latest, up-to-date edition.

JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES
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Language(s)

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
DevelopmentNote
Supersedes MIL HDBK 336/2. (01/2014)
DocumentType
Standard
Pages
497
ProductNote
NEW CHILD NOT 1 2019 IS NOW ADDED
PublisherName
US Military Specs/Standards/Handbooks
Status
Current
Supersedes

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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
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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
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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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