SAEITC TS120-6
Current
The latest, up-to-date edition.
TS120 AGS2000 Series Stiffnuts (including Clinch Nuts) BA and BSF Threads for Aircraft
Hardcopy , PDF
English
01-05-2014
FOREWORD
1. BACKGROUND
2. SCOPE
3. ASSOCIATED DOCUMENTS
4. LIST OF TABLES
5. LIST OF FIGURES
SECTION ONE: GENERAL REQUIREMENTS
6 DEFINITIONS
7 DESIGN AND DIMENSIONS
8 MATERIAL AND MANUFACTURE
9 FREEDOM FROM DEFECT
10 PROTECTIVE COATING
11 SCREW THREADS
12 SQUARENESS OF FACE TO THREAD
13 IDENTIFICATION AND MARKING
SECTION TWO: INSPECTION AND TESTING
14 QUALIFICATION PROCEDURE
15 PRODUCTION BATCH ACCEPTANCE
16 INSPECTION OF SAMPLES
17 TESTING OF SAMPLES
18 TEST BOLTS
19 TORQUE TEST
20 BOLT TOLERANCE TEST
21 ENDURANCE TEST
22 TORSIONAL STRENGTH TEST
23 THRUST TEST
24 HIGH TEMPERATURE TORQUE TEST
25 LOW TEMPERATURE TORQUE TEST
26 CLINCHING TEST FOR CLINCH NUTS
APPENDIX A: EQUIPMENT FOR TESTING STIFFNUTS
APPENDIX B: FITTING AND TESTING OF CLINCH NUTS
APPENDIX C: MATERIALS FOR STIFFNUTS AND CLINCH NUTS
Describes the dimensions, material, finish, testing and identification of aircraft stiffnuts with BA and BSF threads.
DevelopmentNote |
Amendment Record is available separately, see SBAC TS 120 AR. (05/2014)
|
DocumentType |
Standard
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Pages |
32
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ProductNote |
New child AR 2014 is added
|
PublisherName |
SAE Industry Technologies Consortia
|
Status |
Current
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Supersedes |
DEFSTAN 00-970(PT1)SEC4/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
DEFSTAN 00-970(PT1)SEC4/14(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
DEFSTAN 00-970(PT1)SEC4/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
DEFSTAN 00-970(PT1)SEC4/6(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FORD SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
DEFSTAN 00-970(PT1)SEC4/13(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
DEFSTAN 00-970(PT7)SEC2/SUPP4/6(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D) |
DEFSTAN 91-114/1(2003) : 2003 | LUBRICATING OIL, AIRCRAFT CONTROLS: ANTIFREEZING JOINT SERVICE DESIGNATION: OM-150 |
DEFSTAN 03-25/5(2008) : 2008 | SULFURIC ACID ANODIZING OF ALUMINIUM AND ALUMINIUM ALLOYS |
BS 2A 61:1962 | Specification for aluminium alloy hexagonal headed bolts (B.A. and B.S.F. threads) for aircraft |
BS EN 2133:2010 | Aerospace series. Cadmium plating of steels with specified tensile strength ≤ 1450 MPa, copper, copper alloys and nickel alloys |
BS 84:2007 | Parallel screw threads of Whitworth form. Requirements |
BS 2A 25:1962 | Specification for steel hexagonal-headed bolts (B.A. and B.S.F. threads) for aircraft |
DEFSTAN 03-19/4(2010) : 2010 | ELECTRO-DEPOSITION OF CADMIUM |
DEFSTAN 80-217/1(2002) : 2002 | CORROSION PREVENTIVE COMPOUND: SOFT FILM, COLD APPLICATION NATO CODE: C-614 JOINT SERVICES DESIGNATION: PX-1 |
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