Standard Practice for Effects of Cleaners on Unpainted Aircraft Surfaces

SIGNIFICANCE AND USE
3.1 This practice is used to ensure that candidate aircraft surface cleaners do not leave a residue which, on drying, would leave a permanent stain requiring polishing to remove.
SCOPE
1.1 This practice describes the procedure used to determine the effect of cleaners on unpainted aircraft surfaces. Visual observation is used for determining streaking or permanent stains which require polishing to remove.  
1.2 The values stated in inch-pound units are to be regarded as the standard. The values given in parentheses are for information.  
1.3 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use.  
1.4 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

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Status
Published
Publication Date
30-Apr-2019
Current Stage
Ref Project

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ASTM F485-08(2019) - Standard Practice for Effects of Cleaners on Unpainted Aircraft Surfaces
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This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the
Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
Designation: F485 − 08 (Reapproved 2019)
Standard Practice for
Effects of Cleaners on Unpainted Aircraft Surfaces
ThisstandardisissuedunderthefixeddesignationF485;thenumberimmediatelyfollowingthedesignationindicatestheyearoforiginal
adoption or, in the case of revision, the year of last revision.Anumber in parentheses indicates the year of last reapproval.Asuperscript
epsilon (´) indicates an editorial change since the last revision or reapproval.
1. Scope 4. Reagents and Materials
1.1 This practice describes the procedure used to determine 4.1 Reagents:
the effect of cleaners on unpainted aircraft surfaces. Visual 4.1.1 Reagent water in accordance with Specification
observation is used for determining streaking or permanent D1193, Type IV.
stains which require polishing to remove. 4.1.2 Methyl n-propyl ketone (MPK).
1.2 The values stated in inch-pound units are to be regarded 4.2 Materials:
as the standard. The values given in parentheses are for 4.2.1 Aluminum 7075-T6 Alclad in accordance with indus-
information. try standard SAE-AMS-QQ-A-250/13.
4.2.2 Titanium Alloy 6A14V in accordance with industry
1.3 This standard does not purport to address all of the
standard SAE-AMS-T-9046, Composition AB-1.
safety concerns, if any, associated with its use. It is the
responsibility of the user of this standard to establish appro-
5. Preparation of Test Specimens
priate safety, health, and environmental practices and deter-
5.1 Prepare two panels, each 2 by 6 by 0.020 in. (50 by 152
mine the applicability of regulatory limitations prior to use.
by 0.51 mm), from alclad aluminum and titanium alloy and
1.4 This international standard was developed in accor-
clean them with methyl n-propyl ketone.
dance with internationally recognized principles on standard-
ization established in the Decision on Principles for the
6. Preparation of Test Solution
Development of International Standards, Guides and Recom-
mendations issued by the World Trade Organization Technical
6.1 Make the solutions of the cleaner to be tested in reagent
Barriers to Trade (TBT) Committee. water (see 4.1.1) in accordance with the dilutions recom-
mended by the manufacturer.
2. Referenced Documents
7. Procedure
2.1 ASTM Standards:
D1193 Specification for Reagent Water
7.1 Immerse the cleaned test specimens for 3 to 5 min in a
2.2 Industry Standards:
sufficient quantity of the cleaning solution to cover approxi-
SAE-AMS-QQ-A-250/13 Aluminum Alloy Alclad 7075,
mately one half of the panel. After removing from the test
Plate and Sheet
solution, immediately place the panels at 45° from the hori-
SAE-AMS-T-9046 Titanium and Titanium Alloy, Sheet,
zontal in a mechanical convection oven maintained at 150 6
Strip, and Plate (Composition AB-1)
5 °F (65.5 6 2 °C) for 30 min.At the end of the 30 min period,
remove the panels from the oven, cool to room temperature,
3. Significance and Use
rinse on each side within 15 min under running tap water for
...

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