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SEALING COMPOUNDS, QUICK REPAIR, LOW TEMPERATURE CURING POLYSULFIDE, FOR AIRCRAFT STRUCTURES

contributor authorNAVY - AS - Naval Air Systems Command
date accessioned2017-09-04T15:46:55Z
date available2017-09-04T15:46:55Z
date copyright29508
date issued1980
identifier otherPWQPDAAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/49659
description abstractThis specification establishes requirements for two types and classes of a two component, low temperature curing, polysulfide, sealing compound for use as a quick-repair material for aircraft structure. Intended Use: The sealing compound covered by this specification is intended for use as a quick repair, low temperature curing aircraft structural sealant which gives "fly-away" capability in 2 to 3 hours when cured at temperatures of at least 75°F. When cured as low as 45°F, type II sealants provide a 4 hour "fly-away" capability and type I - 8 hours. The sealing compounds have a minimum shelf life of 6 months when stored at temperatures below 80°F. After the 6 month storage period, the material should be tested to determine its usefulness. In addition, the 6 month shelf life can be extended by storage at refrigeration temperature (approximately 40°F). The sealing compounds furnished under this specification are to be used with the manufacturer's recommended primer to obtain optimum results.
languageEnglish
titleMIL-S-85420num
titleSEALING COMPOUNDS, QUICK REPAIR, LOW TEMPERATURE CURING POLYSULFIDE, FOR AIRCRAFT STRUCTURESen
typestandard
page86
statusActive
treeNAVY - AS - Naval Air Systems Command:;1980
contenttypefulltext


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