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COLLINS 332D-11T 622-4565-001

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Purchase Availability

Condition List PriceAvailabilityQuantity
Overhaul Exchange Request Quote 6 in-stock
Serviceable Exchange Request Quote 10 in-stock
New Outright DocumentationRequest Quote Check Availability
New Surplus Outright Request Quote Check Availability
Overhauled Outright Request Quote Check Availability
Serviceable Outright Request Quote Check Availability
As Removed Outright Request Quote 5 in-stock

Repair Capabilities

Option Rate Fees Expedited Turn Time Quantity
Overhaul P&L: $2,115.00
2 days(additional fee applies)
Repair Labor: $1,114.00
2 days(additional fee applies)
Function Test Labor: $238.00
Evaluation Labor: $358.00
Loaner Request Quote Recert:$238.00
Rent Request Quote $70.00 / day


  • Contains capabilities for fast and normal erection
  • Provides monitor signal to indicate proper erection and speed
  • Three-wire 400 Hz synchro outputs conforming to ARINC specification are provided in both pitch and roll axes
  • Equipment features built-in starting cycle, roll cutout, and monitoring circuits
  • Fast erection is automatic during starting
  • Both manual recycling and self-testing can readily be provided by appropriate external wiring
  • Transmits pitch and roll attitude for flight director indicator
  • A source of attitude reference information used in integrated flight systems and automatic flight control systems


  • 6.8 lbs
  • 115 +/-10% Vac
  • Operating- -54° to +70° C (-65° to +158° F) Storage- -65° to +70° C (-85° to +158° F)
  • Starting- 550 mA Running- 300 mA
  • -1,000 to +40,000 ft (-300 to +12,200 km)
  • 5 5/8 x 6 3/16 x 7 3/4 in (WxHxL)
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