QB78222-30
Coils and Transformers
TRANSFORMER,POWER
QB78222-30
Honeywell Intl Inc Defense Avionics
TRANSFORMER,POWER
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Technical Characteristics
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Mounting Facility Quantity
4 single group
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Center To Center Distance Between Mounting Facilities Parallel To Width
1.250 inches nominal single mounting facility single center group
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Criticality Code Justification
feat
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Center To Center Distance Between Mounting Facilities Parallel To Length
1.375 inches nominal single mounting facility single center group
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Special Features
weapon system essential
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Body Width
1.812 inches nominal
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Winding Tap Location (Non-Core)
err-070
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Mounting Method
threaded stud single group
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Winding Operating Voltage
12.60 ac volts nominal single component all secondary
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End Item Identification
aircraft, tomcat f-14; engine, aircraft t-56; aircraft, awacs, e-3a; aircraft, sof (ac-130h, mc-130h, ec-130e, hc-130); aircraft, hornet f/a-18; land combat support system (lcss); ta-4j aircraft; f4n aircraft; aircraft, orion p-3
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Winding Function And Quantity
1 primary single component and 2 secondary single component
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Body Length
1.938 inches nominal
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Winding Operating Current
2.0 amperes ac maximum single component all secondary
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Reliability Indicator
not established
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Frequency Rating
400.0 hertz nominal single component
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Winding Operating Voltage
57.50 ac volts nominal single component single primary and 99.70 ac volts nominal single component single primary and 115.00 ac volts nominal single component single primary and 120.00 ac volts nominal single component single primary
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Input-Output Phase Relationship
single phase to single phase single component
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Winding Shielding Method
internal shield grounded to inclosure single component
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Inclosure Type
hermetically sealed
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Thread Series Designator
unc single group
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Body Height
2.750 inches nominal
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Terminal Type And Quantity
10 solder stud
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Thread Direction (Non-Core)
err-070
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Nominal Thread Size
0.138 inches single group