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wall thickness 0.035 in. used on plumbing installation engines no. 1 2 and 4
aisi 304 tubing anld per mil-t-850 (asg) 0.5 in. outside tube dia wall thickness 0.028 in. used on plumbing installation engines no. 1 2 and 3
the boeing company. the end item identification is c-135 acft
the boeing company. the end item identification is kc-135 tanker airplane
the boeing company. kc-135 is the aircraft mission design series
heat shield assy nsn 1560000152144. the end item identification is c-135 stratolifter
rod end connector nsn 5340000152142. the style designator is a connector
goodrich aerospace canada ltd. crespassivated is the special features
eaton aerospace llc. cres per qq-s-763b cl 440ccond a1.083 in. lg0.2493in. id0.777 in. od is the general characteristics item description
hydraulic system access manifold nsn 4730000152136. the special feature is 3.500 inches long
safety relief valve nsn 4820000152135. the thread class is 3a 1st end.
flexible shaft assembly casing nsn 3040000152133. the outside diameter is 0.490 inches minimum and 0.520 inches maximum
screw thread insert nsn 5325000152114. another reference number is 690775-3
screw thread insert nsn 5325000152112. another reference number is 693547-5
governor housing nsn 2995000152111. another reference number is 693817
mechanical drive housing nsn 3040000152110. another reference number is 693041b
aircraft structural plate nsn 1560000152105. the aircraft mission design series is c-135
round plain nut nsn 5310000152092. the nut style is round
hamilton sundstrand corporation. lgm-30 is the end item identification
hamilton sundstrand corporation. the reference data and literature is t.o. 35c1-2-48-3 fig 6-23
hamilton sundstrand corporation. the special feature is the t.o. 35c1-2-48-3 fig 6-20
