SAE AMS 1527 : 2014
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
CLEANER FOR AIRCRAFT EXTERIOR SURFACES, WATER-MISCIBLE, FOAM-ON, PRESSURE-SPRAYING
Available format(s)
Hardcopy , PDF
Superseded date
02-05-2020
Superseded by
Language(s)
English
Published date
01-01-2014
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGMENT
7. REJECTIONS
8. NOTES
This specification covers a water-miscible, foam-on, pressure spraying cleaner in the form of a liquid.
| Committee |
AMS-J
|
| DocumentType |
Standard
|
| Pages |
6
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| I.S. EN 4688:2012 | AEROSPACE SERIES - PAINTS AND VARNISHES - CORROSION INHIBITING TWO COMPONENTS COLD CURING PRIMER FOR MILITARY APPLICATION |
| 17/30371343 DC : 0 | BS EN 4688 - AEROSPACE SERIES - PAINTS AND VARNISHES - CORROSION RESISTANT CHROMATED TWO COMPONENT COLD CURING EPOXY PRIMER - HIGH CORROSION RESISTANCE FOR MILITARY APPLICATION |
| 17/30371344 DC : 0 | BS EN 4689 - AEROSPACE SERIES - PAINTS AND VARNISHES - TWO COMPONENTS COLD CURING POLYURETHANE FINISH - HIGH FLEXIBILITY AND CHEMICAL AGENT RESISTANCE FOR MILITARY APPLICATION |
| BS EN 4687:2012 | Aerospace series. Paints and varnishes. Chromate free non corrosion inhibiting two components cold curing primer for military application |
| PREN 4689 : 200P1 | AEROSPACE SERIES - PAINTS AND VARNISHES - TWO COMPONENTS COLD CURING POLYURETHANE FINISH - HIGH FLEXIBILITY AND CHEMICAL AGENT RESISTANCE FOR MILITARY APPLICATION |
| UNI EN 4689 : 2013 | AEROSPACE SERIES - PAINTS AND VARNISHES - TWO COMPONENTS COLD CURING POLYURETHANE FINISH - HIGH FLEXIBILITY AND CHEMICAL AGENT RESISTANCE FOR MILITARY APPLICATION |
| 17/30371341 DC : 0 | PREN 4687 - AEROSPACE SERIES - PAINTS AND VARNISHES - CHROMATE FREE (NON CORROSION INHIBITING) TWO COMPONENT COLD CURING PRIMER - CHROMATE FREE PRIMER FOR MILITARY APPLICATION |
| BS EN 4689:2012 | Aerospace series. Paints and varnishes. Two components cold curing polyurethane finish. High flexibility and chemical agent resistance for military application |
| I.S. EN 4687:2012 | AEROSPACE SERIES - PAINTS AND VARNISHES - CHROMATE FREE NON CORROSION INHIBITING TWO COMPONENTS COLD CURING PRIMER FOR MILITARY APPLICATION |
| UNI EN 4688 : 2013 | AEROSPACE SERIES - PAINTS AND VARNISHES - CORROSION INHIBITING TWO COMPONENTS COLD CURING PRIMER FOR MILITARY APPLICATION |
| UNI EN 4687 : 2013 | AEROSPACE SERIES - PAINTS AND VARNISHES - CHROMATE FREE NON CORROSION INHIBITING TWO COMPONENTS COLD CURING PRIMER FOR MILITARY APPLICATION |
| EN 4689:2012 | Aerospace series - Paints and varnishes - Two components cold curing polyurethane finish - High flexibility and chemical agent resistance for military application |
| EN 4687:2012 | Aerospace series - Paints and varnishes - Chromate free non corrosion inhibiting two components cold curing primer for military application |
| EN 4688:2012 | Aerospace series - Paints and varnishes - Corrosion inhibiting two components cold curing primer for military application |
| I.S. EN 4689:2012 | AEROSPACE SERIES - PAINTS AND VARNISHES - TWO COMPONENTS COLD CURING POLYURETHANE FINISH - HIGH FLEXIBILITY AND CHEMICAL AGENT RESISTANCE FOR MILITARY APPLICATION |
| PREN 4688 : 200P1 | AEROSPACE SERIES - PAINTS AND VARNISHES - CORROSION INHIBITING TWO COMPONENTS COLD CURING PRIMER FOR MILITARY APPLICATION |
| PREN 4687 : 200P1 | AEROSPACE SERIES - PAINTS AND VARNISHES - CHROMATE FREE NON CORROSION INHIBITING TWO COMPONENTS COLD CURING PRIMER FOR MILITARY APPLICATION |
| BS EN 4688:2012 | Aerospace series. Paints and varnishes. Corrosion inhibiting two components cold curing primer for military application |
| SAE AMS 4049 : 2016 | ALUMINUM ALLOY, SHEET AND PLATE, ALCLAD 5.6ZN - 2.5MG - 1.6CU - 0.23CR (ALCLAD 7075; -T6 SHEET - T651 PLATE) SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 2475H : 2009 | PROTECTIVE TREATMENTS, MAGNESIUM ALLOYS |
| SAE AMS 4911 : 2014 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4 V, ANNEALED |
| MIL-STD-2073-1 Revision E:2008 | STANDARD PRACTICE FOR MILITARY PACKAGING |
| SAE AMS 4376 : 2011(R2018) | PLATE, MAGNESIUM ALLOY - 3.0AL - 1.0ZN - 0.20MN (AZ31B-H26) COLD ROLLED AND PARTIALLY ANNEALED |
| SAE AMS 4037 : 2014 | ALUMINUM ALLOY, SHEET AND PLATE, 4.4CU - 1.5MG - 0.60MN (2024; -T3 FLAT SHEET, -T351 PLATE) SOLUTION HEAT TREATED |
| MIL-STD-870 Revision C:2007 | Cadmium Plating, Low Embrittlement, Electrodepositon |
| MIL-PRF-25690 Revision B:1993 | PLASTIC, SHEET AND FORMED PARTS, MODIFIED ACRYLIC BASE, MONOLITHIC, CRACK PROPAGATION RESISTANT |
| SAE AMS 2825 : 1987 | MATERIAL SAFETY DATA SHEETS |
| SAE AMS 2470 : 2013 | ANODIC TREATMENT OF ALUMINUM ALLOYS, CHROMIC ACID PROCESS |
| SAE AMS 5045 : 2015 | STEEL, SHEET AND STRIP, 0.25 CARBON, MAXIMUM HARD TEMPER |
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