SAE AMS QQ A 250/5 : 2014
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
ALUMINUM ALLOY ALCLAD 2024, PLATE AND SHEET
Hardcopy , PDF
11-06-2021
English
13-02-2014
Covers the specific requirements for 2024 aluminum alloy alclad plate and sheet; the general requirements are covered in AMS-QQ-A-250.
Committee |
AMS-D
|
DevelopmentNote |
Supersedes QQ A 250/5 (F). (06/2005)
|
DocumentType |
Standard
|
Pages |
9
|
PublisherName |
SAE International
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
MIL-PRF-7907 Revision C:2007 | Cleaning Compound, Decontaminating (for Soiled and Radioactive Contaminated Surfaces) |
MIL-PRF-32239 Revision A:2014 | COATING SYSTEM, ADVANCED PERFORMANCE, FOR AEROSPACE APPLICATIONS |
MIL-PRF-29608 Revision C:2016 | CLEANING AND CLEANING-LUBRICATING COMPOUNDS, ELECTRICAL CONTACT |
SAE AMS 3374 : 2013 | SEALING COMPOUND AIRCRAFT FIREWALL, SILICONE |
MIL-PRF-85322 Revision C:2014 | COATING, ELASTOMERIC, POLYURETHANE, RAIN-EROSION |
MIL-PRF-6799 Revision L:2010 | COATINGS, SPRAYABLE, STRIPPABLE, PROTECTIVE, WATER EMULSION |
NASM 1312-21 : 2004 | FASTENER TEST METHODS METHOD 21 SHEAR JOINT FATIGUE, CONSTANT AMPLITUDE |
SAE AS 5272 : 2016 | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING, PROCUREMENT SPECIFICATION |
ASTM F 1110 : 2009 | Standard Test Method for Sandwich Corrosion Test |
P-W-2891 Revision A:2002 | WIPE SOLVENTS, EXEMPT AND NON-EXEMPT |
SAE AMS 4466 : 2017 | ALUMINUM ALLOY, SHEET AND PLATE, ALCLAD, 4.4CU - 1.5MG - 0.60MN (ALCLAD 2024, -T361 SHEET & PLATE), SOLUTION HEAT TREATED, 6% COLD WORKED AND NATURALLY AGED |
MIL-DTL-85052-5 Revision A:2016 | CLAMP, LOOP, ALUMINUM 2024-T42, 275 DEGREES F, ETHYLENE PROPYLENE |
MIL-PRF-23377 Revision K:2012 | PRIMER COATINGS: EPOXY, HIGH-SOLIDS |
MIL-PRF-81352 Revision C:2005 | COATINGS, AIRCRAFT TOUCH-UP |
SAE AMS C 7438 : 2014 | CORE MATERIAL, ALUMINUM, FOR SANDWICH CONSTRUCTION |
MIL-STD-186 Revision F:2002 | PROTECTIVE FINISHING SYSTEMS FOR ROCKETS, GUIDED MISSILES, SUPPORT EQUIPMENT AND RELATED MATERIALS |
MIL-DTL-85052-10 Revision A:2016 | CLAMP, LOOP, ALUMINUM 2024-T42, 275 DEGREES F, NITRILE BUTADIENE RUBBER FUEL AND PETROLEUM BASED HYDRAULIC FLUID RESISTANT |
SAE AMS 3604 : 2015 | HEAT RESISTANT ALUMINIZED PAINT |
MIL-DTL-3928 Revision H:2016 | SWITCHES, RADIO-FREQUENCY TRANSMISSION LINE, (COAXIAL AND MICROSTRIP), GENERAL SPECIFICATION FOR |
MIL-DTL-85052-6 Revision A:2016 | CLAMP, LOOP, ALUMINUM 2024-T42, 400 DEGREES F, FLUOROSILICONE |
SAE AMS P 21600 : 2013 | PAINT SYSTEM, FLUORESCENT, REMOVABLE, FOR AIRCRAFT APPLICATION |
MIL-DTL-85052-8 Revision A:2016 | CLAMP, LOOP, ALUMINUM 2024-T42, 500 DEGREES F, SILICONE RUBBER, FABRIC REINFORCED |
SAE AMS 3603 : 2002 | PROTECTIVE FILM, HIGH PERFORMANCE, POLYMERIC PRESSURE SENSITIVE ADHESIVE, FOR AIRCRAFT EXTERIOR APPLICATIONS |
SAE AMS DTL 22499 : 2013 | SHIM STOCK, LAMINATED |
ASTM F 1110 : 2009 : R2014 | Standard Test Method for Sandwich Corrosion Test |
MIL-DTL-85052-9 Revision A:2016 | CLAMP, LOOP, ALUMINUM 2024-T42, 550 DEGREES F, POLY-TETRAFLUOROETHYLENE (PTFE) |
SAE AMS 3381 : 2014 | SEALING COMPOUND, AIRCRAFT FIREWALL, NON-SILICONE |
MIL-DTL-19834 Revision C:2006 | PLATES, IDENTIFICATION OR INSTRUCTION, METAL FOIL, ADHESIVE BACKED, GENERAL SPECIFICATION FOR |
SAE AMS 4475 : 2017 | Aluminum Alloy, Coiled Sheet, Alclad 4.4Cu – 1.5Mg – 0.60Mn (Alclad 2024; -T4 Coiled Sheet) Solution Heat Treated |
MIL-PRF-85582 Revision E:2012 | PRIMER COATINGS: EPOXY, WATERBORNE |
MIL-PRF-32587 Base Document:2018 | Remover, Paint, Hap-Free, Neutral |
MIL-DTL-85052-7 Revision A:2016 | CLAMP, LOOP, ALUMINUM 2024-T42, 212 DEGREES F, CHLOROPRENE |
SAE AMS 3144 : 2012 | PRIMER, ANODIC ELECTRODEPOSITION FOR AIRCRAFT APPLICATIONS |
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