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SAEITC TS120-6

Current

Current

The latest, up-to-date edition.

TS120 AGS2000 Series Stiffnuts (including Clinch Nuts) BA and BSF Threads for Aircraft

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-05-2014

€190.59
Excluding VAT

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
Pages
32
ProductNote
New child AR 2014 is added
PublisherName
SAE Industry Technologies Consortia
Status
Current
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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