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HONEYWELL AUTOPILOT COMPUTER 4008519-924

4008519-924
Yes
In-stock
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Purchase Availability

Condition List PriceAvailabilityQuantity
New Outright DocumentationRequest Quote Check Availability
New Surplus Outright Request Quote Check Availability
As Removed Outright Request Quote 1 in-stock

Repair Capabilities

Option Rate Fees Expedited Turn Time Quantity
Overhaul T & M
2 days(additional fee applies)
Repair Labor: $1,711.00
2 days(additional fee applies)
Function Test Labor: $419.00
Evaluation Labor: $538.00


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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24/7 Support

Parts Sales & Exchanges

800.228.1836 / +1 402.475.4125

Overhauls & Repairs

800.562.6377 / +1 402.475.2611

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