SAE AMS 1536 : 2008

Superseded

View Superseded by

CLEANER FOR AIRCRAFT COMPONENTS COLD TANK TYPE, SOLVENT-BASE

Available format(s)

Hardcopy , PDF

Superseded date

09-13-2018

Language(s)

English

Published date

01-01-2008

Publisher

SAE International

1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGMENT
7. REJECTIONS
8. NOTES

Describes a liquid tank-type cleaner, primarily for removal of greasy soils, carbon or rubber from painted and unpainted aircraft components, such as wheels and landing gear, by immersing in cleaner as supplied, or as solvent diluted. Not suitable for plastic or aircraft windows, due to possibility of crazing.

Committee	AMS-J
DocumentType	Standard
Pages	7
PublisherName	SAE International
Status	Superseded
SupersededBy	SAE AMS 1536C : 2018
Supersedes	SAE AMS 1536 : 2001

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
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-A-356 Revision A:1946	ASPHALTUM (GILSONITE)
MIL-C-306 Revision C:1978	CARBON BLACK, POWDERED, DRY
ASTM D 93 : 2016-07	TEST METHODS FOR FLASH POINT BY PENSKY-MARTENS CLOSED CUP TESTER
MIL-L-6082 Revision E:1990	LUBRICATING OIL, AIRCRAFT PISTON ENGINE (NONDISPERSANT MINERAL OIL)
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