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Purchase Availability

Condition List PriceAvailabilityQuantity
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As Removed Outright Request Quote Check Availability

Repair Capabilities

Option Rate Fees Expedited Turn Time Quantity
Overhaul P&L: $1,952.002 days(additional fee applies)
Repair Labor: $1,023.002 days(additional fee applies)
Function Test Labor: $232.00
Evaluation Labor: $348.00


  • 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
  • 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
  • Contains capabilities for fast and normal erection
  • Both manual recycling and self-testing can readily be provided by appropriate external wiring
  • Provides monitor signal to indicate proper erection and speed
  • Unit has stiffer rubber mounts


  • 5 5/8 x 6 3/16 x 7 3/4 in (WxHxL)
  • 7.2 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)
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