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COLLINS VERTICAL REFERENCE 792-6694-004

792-6694-004
Yes
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Purchase Availability

Condition List PriceAvailabilityQuantity
Overhaul Exchange Request Quote Check Availability
New Outright DocumentationRequest Quote Check Availability
New Surplus Outright Request Quote Check Availability
Overhauled Outright Request Quote Check Availability
As Removed Outright Request Quote Check Availability

Repair Capabilities

Option Rate Fees Expedited Turn Time Quantity
Overhaul P&L: $1,895.002 days(additional fee applies)
Repair Labor: $998.002 days(additional fee applies)
Function Test Labor: $232.00
Evaluation Labor: $348.00


Features

  • 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

Specs

  • 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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