MIL-T-9046 Revision J:1983
Superseded
Superseded
TITANIUM AND TITANIUM ALLOY, SHEET, STRIP AND PLATE (S/S BY SAE-AMS-T-9046)
Available format(s)
PDF
Published date
01-11-1983
Publisher
Superseded date
09-17-1999
US$20.00
Excluding Tax where applicable
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J NOTICE 1 - Notice of Validation J NOTICE 2 - Notice of Cancellation/Superseded by SAE AMS T 9046 (04/2004)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Superseded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, 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) |
Summarise
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