Control Test Sets - Page 7 of 10
234 products in this catalog
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Width: 6.625 inches
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Length: 19.000 inches
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Rating: 115.0 volts
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Rating: 400.0 hertz
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Application: Displacement gyroscope
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Application: F-5 aircraft
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Agency: Northrop grumman
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Feature: Multiple item w/carrying case
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Designed: Alignment of wing flap leading edge
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Literature: To 1f-5a-4-2
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Application: Master warning system controller series r7640
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Description: Functional tests controller
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Literature: To 8d3-12-17-3
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Rating: 115.0 volts or 220.0 volts
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Rating: 400.0 hertz
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Application: F-4 aircraft age
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Relationship: Operating
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Feature: Single item w/housing
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Rating: 115.0 volts or 220.0 volts
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Rating: 400.0 hertz
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Application: F-4 aircraft age
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Relationship: Operating
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Feature: Single item w/housing
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Application: J-79-15, j-79-17 aircraft engine
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Feature: Single item w/housing
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Designed: Engine temperature
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Literature: T.O. 33d4-6-159-11
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Application: J-79-15, j-79-17 aircraft engine
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Feature: Single item w/housing
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Designed: Engine temperature
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Literature: T.O. 33d4-6-159-11
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Rating: 115.0 volts
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Rating: 400.0 hertz
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Application: F4c aircraft test equipment
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Relationship: Operating
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Feature: Multiple item w/housing
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Rating: 115.0 volts
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Rating: 400.0 hertz
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Application: F4c aircraft test equipment
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Relationship: Operating
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Feature: Multiple item w/housing
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Features: To name: mechanical advantage shifter tester
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Literature: To 33d3-32-2-4
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Application: Series 386720 central gearbox
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Features: To name: calibrator, governor
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Description: Tests and calibrates governor assembly
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Literature: To 2ja16-2-3
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Width: 14.000 inches
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Length: 15.000 inches
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Rating: Between 115.0 volts and 200.0 volts
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Rating: 400.0 hertz
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Relationship: Alternate operating
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Width: 14.000 inches
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Length: 15.000 inches
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Rating: Between 115.0 volts and 200.0 volts
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Rating: 400.0 hertz
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Relationship: Alternate operating
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Application: A7d, a10a, a37, f4 acft
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Classification: Aa-9.0
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Features: To name: continuity checker
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Application: A7d, a10a, a37, f4 acft
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Classification: Aa-9.0
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Features: To name: continuity checker
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Application: F100a, f100c/e/f aircraft test equipment
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Classification: Aa-9.0
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Literature: T.O. 33d2-14-16-1/4
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Data: Cockpit air temperature control system
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Application: F-111a aircraft age.
