Be or that tho system, as instclleud, was adequate. monitoring plan end available results.) 3.3.3 Moterial Damage (See Teb CH, for Washdovn Systor After the aircrceft arc removed from the ships, thoy will be inspected in as much deteil as possible (governed by the radiologicsl situ:tion) to determine any physical or strubural damage thet can be attributed to the effects of oither the contaminant or the washdown system, Various circuits will be tusted, end, unless the radiological situetion precludes it, the engine will be run, Results of this inspection and test vill be used to predict useability of eircraft after washdown and, if the effects ero deleterious, will be used (1) to design counter- moeesures against these effects, or (2) to remove the causes of those effects, 3.4 (Sec Tab C-5 for inspection schedule end aveilable results.) Effectiveness of Manuel Decontemination Nothods and Equipment , After the tvo planes have boen removed from the ships, and tho forcgoing tests and studies have been conducted, mnanuol cecontaminetion proccdures will be ccrried out. 3.421 These will be testcd on both planes. Equipment to be Used Soe Section 4.5. 3.4.2 Methods end Procedures to be Used An outline of these 1s 3.4.3 included in Tab C-6, Efficiency of Contamination Removal This measurement will be used to indicate the amount of residucl activity removeable after washdown (ABLE plane) end the amount of original rctivity removeble (BAKER plene) by the various decontamination nethods, Residusl contamination will be measured, giving the efficiency of cech method end the total of all methods or combinetions of methods, Availnble results cre given in Tab C6, 3.44 Cost of Docontemination S71. LGVIS FRC & complete record will be maintained of the amounts of naterials end manpower exponded during each operation, An analysis of this record will yield information rogarding the material unit cost of decontaminating fightcr sircraft, Rates of operation will be recorded. 5 oY