Pneumatic System Compon Test Sets - Page 5 of 7
153 products in this catalog
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Application: F111 aircraft ground support equip
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Literature: To 1f-111a-4-18 & 33d5-8-129-1
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Application: F111 aircraft ground support equip
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Literature: To 1f-111a-4-18 & 33d5-8-129-1
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Application: Breather pressurizing valve
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Literature: To 7j6-7-16-3
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Width: 21.500 inches
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Depth: 18.500 inches
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Feature: Single item w/housing
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Designed: Flow test; leakage test
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Classification: Jj-7.2
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Width: 20.000 inches
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Depth: 12.000 inches
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Quantity: 20
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Accommodation: Not included
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Location: Aluminum carrying case
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Literature: T.O. 33d7-8-40-4
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Width: 12.000 inches
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Length: 24.000 inches
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Feature: Multiple item w/carrying case
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Designed: Weapons bay fuel tank
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Height: 6.000 inches
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Application: Used in support of the f4 acft
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Literature: T.O. 33d7-8-40-4
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Feature: Multiple item w/carrying case
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Designed: Oxygen and pressure suit systems
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Literature: T.O. 33d2-10-16-1
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Application: Used in support of the turbo jet engine j85-7
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Features: To name: seal leakage tester
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Literature: To 33d4-6-198-4
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Literature: To 33d4-6-198-4
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Width: 4.000 inches
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Length: 8.000 inches
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Application: F-15 acft
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Feature: Single item w/carrying case
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Designed: Leak testing of the lox system
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Width: 4.000 inches
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Length: 8.000 inches
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Application: F-15 acft
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Feature: Single item w/carrying case
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Designed: Leak testing of the lox system
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Width: 4.000 inches
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Length: 8.000 inches
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Application: F-15 acft
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Feature: Single item w/carrying case
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Designed: Leak testing of the lox system
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Literature: T.O. 33d2-10-16-1
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Application: F102 acft
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Literature: T.O. 33d2-10-12-2/4; t. O. 15x11 -2-1
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Width: 19.000 inches
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Length: 22.000 inches
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Measure: 5016.000 cubic inches
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Feature: Single item w/carrying case
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Designed: Pneumatic pressure tests
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Features: To name: tester, ball valve
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Literature: To 6j15-10-136-13
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Features: To name: tester, ball valve
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Literature: To 6j15-10-136-13
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Features: To name: tester, ball valve
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Literature: To 6j15-10-136-13
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Application: J79 aircraft engine
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Feature: Single item w/housing
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Literature: T.O. 33d4-6-209-1
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Application: J79 aircraft engine
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Feature: Single item w/housing
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Literature: T.O. 33d4-6-209-1
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Feature: Single item w/housing
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Designed: Afterburner manifold leakage
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Literature: To 33d4-6-68-54
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Feature: Single item w/housing
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Designed: Afterburner manifold leakage
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Literature: To 33d4-6-68-54
