Air Data Computers - Page 5 of 8
178 part numbers
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gulfstream-4 acft end application
9B-81010-8
NSN 6610-01-444-0573
Cross Reference:
04606
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1 terminal quantity
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connector, receptacle terminal type
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plate mounting type
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115.0 alternating current voltage rating in volts
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28.0 direct current voltage rating in volts
804800-4-006
NSN 6610-01-448-0939
Cross Reference:
ZC8-60-102-1-12
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115.0 and 28.0 alternating current voltage rating in volts
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pacer dawn end application
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external power source
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air intelligence input method
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electrostatic sensitive features provided
7-519720001
NSN 6610-01-453-4269
Cross Reference:
50-158-01, 7-519720001-3
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ah-64 longbow end application
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falcon 900, dassault aviation end application
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challenger 604 end application
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115.0 alternating current voltage rating in volts
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28.0 direct current voltage rating in volts
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-55.0/+85.0 degrees celsius storage tempurature range
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kc13 (r) end application
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between 3.670 inches and 3.690 inches unpackaged unit width
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calculates true air speed functional description
525-10080-1
NSN 6610-01-479-7353
Cross Reference:
50-056-01
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external power source
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air data input intelligence type
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electrical intelligence input method
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a310-222 airbus end application
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a310-222 airbus end application
133-340143-3
NSN 6610-01-482-4202
Cross Reference:
133-340143-1
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t6 joint primary aircraft trainer end application
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product model kdc481t end application
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air data special features
501-1797-22
NSN 6610-01-488-5465
Cross Reference:
ADC-3000AB
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external power source
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electrical intelligence input method
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used in dpu-85n (display processor unit) special features
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rack mounting type
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14.000 inches unpackaged unit length
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5.000 inches unpackaged unit width
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8.580 inches unpackaged unit height
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honeywell planning drawing tbd0001 reference data and literature
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aircraft, embraer, model erj135 anderj145 end application
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external power source
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electrical intelligence input method
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comes with autopilot special features
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aircraft, embraer, model erj135 and erj145 end application
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external power source
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electrical intelligence input method
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embraer aircraft end application