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HONEYWELL AUTOPILOT COMPUTER 4008519-947

4008519-947
Yes
In-stock
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Purchase Availability

Condition List PriceAvailabilityQuantity
Overhaul Exchange Request Quote Check Availability
Serviceable Exchange Request Quote 2 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 Check Availability

Repair Capabilities

Option Rate Fees Expedited Turn Time Quantity
Overhaul T & M
2 days(additional fee applies)
Repair Labor: $1,662.00
2 days(additional fee applies)
Function Test Labor: $407.00
Evaluation Labor: $523.00
Loaner Request Quote Recert:$250.00
Rent Request Quote $70.00 / day


Features

  • Unit provides roll, pitch and yaw axis control by processing command and error signals to drive the aileron, elevator and rudder control surfaces.
  • This autopilot computer processes information about the aircraft actual attitude versus a desired attitude as a function of selected flight mode to produce pitch, roll and yaw control outputs.
  • It also includes autopilot controller selectable modes which will produce pitch and roll outputs for any flight director modes except go around.

Specs

  • 12.65 in (321.3 mm) L (without handle) x 2.79 in (70.9 mm) W x 7.62 in (193.5 mm) H (maximums)
  • 7.0 lbs (3.18 kg)
  • 28 +/-1 Vdc 115 +/-1 Vac
  • DC- 1.5 to 4 A AC- 1 A
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