Engine Oil Pump Assembly Housings
131 part numbers
-
1.650 inches material thickness
-
aircraft eng t-56 end application
-
iron cast housing material
-
aircraft eng j47 end application
-
aircraft eng j47 end application
-
aircraft eng j65 end application
-
aircraft eng tf-41 end application
-
j52 engine end application
-
2.820 inches overall length
-
2.380 inches overall width
-
aircraft engine tf33 end application
-
aluminum alloy housing material
225119
NSN 2995-00-092-0141
Cross Reference:
239764
198840
NSN 2995-00-092-1951
Cross Reference:
239759
236582
NSN 2995-00-098-2976
Cross Reference:
243708
-
j57 engine end application
-
engine model tf30 end application
-
t-56 aircraft engines end application
-
magnesium alloy housing material
-
j57 engine end application
-
aircraft engines j57 end application
-
aircraft eng j-47, j-79, t-58 and t-64 end application
-
aluminum alloy housing material
-
anodize housing surface treatment
-
no. 4 bearing pump, j-57 turbine engine fsc application data
-
aircraft engine j-33 end application