MIL-T-9046 Revision J:1983
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
TITANIUM AND TITANIUM ALLOY, SHEET, STRIP AND PLATE (S/S BY SAE-AMS-T-9046)
Available format(s)
PDF
Published date
11-01-1983
Publisher
Superseded date
17-09-1999
€16.67
Excluding VAT
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PACKAGING
6. NOTES
Covers aircraft quality titanium and titanium alloy metal sheet, strip and plate products.
| DevelopmentNote |
J NOTICE 1 - Notice of Validation J NOTICE 2 - Notice of Cancellation/Superseded by SAE AMS T 9046 (04/2004)
|
| DocumentType |
Standard
|
| Pages |
26
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| Standards | Relationship |
| SAE AMS4918N | Similar to |
| SAE AMS4911N | Similar to |
| SAE AMS4902K | Identical |
| SAE AMS4900P | Similar to |
| SAE AMS4909K | Similar to |
| SAE AMS4916K | Similar to |
| SAE AMS4917H | Similar to |
| SAE AMS4915L | Similar to |
| SAE AMS4919H | Similar to |
| SAE AMS4910R | Similar to |
| SAE MAM4911B | Similar to |
| SAE AMS4907K | Similar to |
| SAE AMS4901T | Similar to |
| SAE AMST9046B | Similar to |
| MMM-A-132 Revision B:1994 | Adhesives, Heat Resistant, Airframe Structural, Metal to Metal |
| MIL-S-29574 Base Document:1989 | SEALING COMPOUND, POLYTHIOETHER, FOR AIRCRAFT STRUCTURES, FUEL AND HIGH TEMPERATURE RESISTANT, FAST CURING AT AMBIENT AND LOW TEMPERATURE (S/S BY SAE-AMS3277, SEE NOTICE 1 FOR ADDITIONAL INFORMATION) |
| MIL STD 248 : D | WELDING AND BRAZING PROCEDURE AND PERFORMANCE QUALIFICATION |
| MIL P 85582 : B | PRIMER COATINGS: EPOXY, WATERBORNE |
| MIL-C-81769 Base Document:1972 | Chemical Milling of Metals, Specification for (S/S by SAE-AMS-C-81769) |
| MIL S 81733 : C | SEALING AND COATING COMPOUND CORROSION INHIBITIVE |
| TT-R-2918 Revision A:2001 | Remover, Paint, No Hazardous Air Pollutants (HAPS) |
| MIL R 007885 : C SUPP 1 | RIVETS; BLIND, STRUCTURAL, LOCKED AND FRICTION RETAINED SPINDLE, GENERAL SPECIFICATION FOR |
| SAE AMSC81769A | Chemical Milling of Metals, Specification for |
| MIL-HDBK-1587 Base Document:1996 | Materials and Process Requirements for Air Force Weapons Systems (S/S by MIL-STD-1587) |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| MIL-STD-1312-21 Base Document:1985 | FASTENER TEST METHODS, METHOD 21, SHEAR JOINT FATIGUE CONSTANT AMPLITUDE (S/S BY NASM1312-21) |
| MIL-S-83318 Revision A:1991 | SEALING COMPOUND, LOW TEMPERATURE CURING, QUICK REPAIR INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES (S/S BY SAE-AMS-S-83318) |
| MIL-S-8802 Revision F:1990 | SEALING COMPOUND, TEMPERATURE-RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES, HIGH-ADHESION (S/S BY SAE-AMS-S-8802) |
| SAE AMSC19853 | Carbon Removing Compound (For Use in Agitated Tank) |
| MIL-STD-278 Revision F:1987 | WELDING AND CASTING STANDARD (REPLACEMENT DOCUMENT NAVSEA TECH PUB S9074-AR-GIB-010/278) |
| MIL-C-87936 Revision A:1985 | Cleaning Compounds, Aircraft Exterior Surfaces, Water Dilutable (S/S by MIL-C-87937) |
| MIL-C-43616 Revision C:1981 | Cleaning Compounds, Aircraft Surface (S/S by A-A-59921) |
| SAE MA2005B | Tube Fittings, Aerospace Fluid Systems, Separable, For 24° Cone, General Specification, Metric (ISO 7169) |
| MIL-C-83982 Base Document:1974 | Compound, Sealing, Fluid Resistant (S/S by MIL-S-81733) |
| TT-R-248 Revision B:1981 | REMOVER, PAINT AND LACQUER, SOLVENT TYPE |
| MIL-C-83873 Revision A:1993 | Cleaning Compound, Precoating Surface, Aircraft and Aerospace Ground Equipment (Age) (S/S by MIL-C-87937) |
| MIL-STD-1547 Revision B:1992 | Electronic Parts, Materials, and Processes for Space and Launch Vehicles |
| MIL-T-81533 Revision A:1967 | Trichloroethane 1, 1, 1, (Methyl Chloroform) Inhibited, Vapor Degreasing (No S/S Document) |
| MIL-PRF-85704 Revision C:1998 | CLEANING COMPOUND, TURBINE ENGINE GAS PATH |
| SAE AMS3259B | Sealing Compound, Polythioether Nonchromated, Corrosion Inhibiting for Intermittent Use to 360°F (182°C) |
| JSSG-2006 Base Document:1998 | Aircraft Structures |
| MIL-F-18280 Revision F:1995 | Fittings, Flareless Tube, Fluid Connection (S/S by SAE-AS18280) |
| MIL-HDBK-270 Revision A:1991 | Metallic Materials for Low Magnetic Applications, Magnetic Permeability and Electrical Conductivity, Characteristics of (Metric) |
| MIL S 22499 : C | SHIM STOCK, LAMINATED |
| MIL R 83056 : 0 | RAIN REPELLENTS, IN-FLIGHT APPLIED, AIRCRAFT WINDSHIELD |
| MIL C 85704 : B | CLEANING COMPOUND, TURBINE ENGINE GAS PATH |
| P-C-444 Revision B:1983 | Cleaning Compound, Solvent Soluble, Grease Emulsifying |
| MIL-DTL-22499 Revision D:1998 | Shim Stock, Laminated (S/S by SAE-AMS-DTL-22499) |
| NAVSEA S9074 AQ GIB 010/248 : 0 | REQUIREMENTS FOR WELDING AND BRAZING PROCEDURE AND PERFORMANCE QUALIFICATION |
| NASA HDBK 6025 : 2014 | GUIDELINES FOR THE SPECIFICATION AND CERTIFICATION OF TITANIUM ALLOYS FOR NASA FLIGHT APPLICATIONS |
| MIL-S-7124 Revision B:1966 | SEALING COMPOUND, POLYSULFIDE, ACCELERATOR REQUIRED, FOR AIRCRAFT STRUCTURES (S/S BY SAE-AMS-S-7124) |
| MIL-PRF-29607 Base Document:1996 | Cleaning Compound, Avionics Components, Non-Ozone Depleting |
| MIL-A-8243 Revision D:1985 | Anti-Icing and Deicing-Defrosting Fluids (S/S by SAE-AMS1424) |
| MIL C 87937 : B | CLEANING COMPOUND, AEROSPACE EQUIPMENT |
| MIL-R-7885 Revision D:1988 | Rivets, Blind, Structural, Mechanically LockedSpindleand Friction Locked Spindle, General Specification for |
| MIL C 29602 : 0 | CLEANING COMPOUNDS, FOR PARTS WASHERS AND SPRAY CABINETS |
| MIL-PRF-81733 Revision D:1998 | Sealing and Coating Compound, Corrosion Inhibitive |
| MIL-R-81294 Revision D:1990 | Remover, Paint, Epoxy, Polysulfide, and Polyurethane Systems |
| MIL-R-81903 Revision A:1977 | Remover, Acid Activated, for Amine-Cured Epoxy Coating Systems |
| MIL-R-81835 Base Document:1971 | REMOVER, ORGANIC COATING, HOT TANK TYPE (S/S BY SAE-AMS-R-81835) |
| MIL C 83488 : C | COATING, ALUMINUM, ION VAPOR DEPOSITED |
| MIL-DTL-83488 Revision D:1999 | Coating, Aluminum, High Purity |
| MIL C 85570 : B (1) | CLEANING COMPOUND, AIRCRAFT, EXTERIOR |
| MIL-W-5013 Revision L:1991 | Wheel and Brake Assemblies, Aircraft General Specification For |
| MIL L 23699 : E | LUBRICATING OIL, AIRCRAFT TURBINE ENGINES, SYNTHETIC BASE |
| SAE AMSR81835 | Remover, Organic Coating, Hot Tank Type |
| ASTM E 146 : 1983 | Methods of Chemical Analysis of Zirconium and Zirconium Alloys (Silicon, Hydrogen, and Copper) (Withdrawn 1989) |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-STD-410 Revision E:1991 | NONDESTRUCTIVE TESTING PERSONNEL QUALIFICATION AND CERTIFICATION (SEE NAS410 AS A POSSIBLE REPLACEMENT) |
| ASTM E 120 : 2000 | Standard Test Methods for Chemical Analysis of Titanium and Titanium Alloys (Withdrawn 2003) |
| SAE AMS2631D | Ultrasonic Inspection Titanium and Titanium Alloy Bar, Billet and Plate |
| SAE AMS2249G | Chemical Check Analysis Limits Titanium and Titanium Alloys |
| MIL-STD-163 Revision C:1978 | Steel Mill Products Preparation for Shipment and Storage (S/S by ASTM-A700) |
| ASTM E 8 : 2004 | Standard Test Methods for Tension Testing of Metallic Materials |
| ASTM E 290 : 2014 : REDLINE | Standard Test Methods for Bend Testing of Material for Ductility |
| MIL-STD-105 Revision E:1989 | Sampling Procedures and Tables for Inspection by Attributes (See Notice 3 for Replacement Information) |
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