SAE AMS 1526 : 2008
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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CLEANER FOR AIRCRAFT EXTERIOR SURFACES, WATER-MISCIBLE, PRESSURE-SPRAYING TYPE
Hardcopy , PDF
02-05-2020
English
01-01-2008
1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGMENT
7. REJECTIONS
8. NOTES
Specifies a water-miscible, low-foaming cleaner in the form of a liquid.
Committee |
AMS-J
|
DocumentType |
Standard
|
Pages |
6
|
PublisherName |
SAE International
|
Status |
Superseded
|
SupersededBy |
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 |
SAE AMS 3077 A : 1994(S2018) | COMPOUND, CORROSION PREVENTIVE, SOFT FILM, THIXOTROPIC, COLD 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 |
PREN 4860 P1 : 2018 | AEROSPACE SERIES - ENVIRONMENTAL TESTING - TEST XB: ABRASION OF MARKINGS, LETTERINGS, SURFACES AND MATERIALS CAUSED BY RUBBING OF FINGERTIPS AND HANDS |
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 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 ARP 4916 : 2011 | MASKING AND CLEANING OF EPOXY AND POLYESTER MATRIX THERMOSETTING COMPOSITE MATERIALS |
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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