Part #:

Model: DGS-65

Collins Aerospace - Directional Gyro
Part Number :

  • Directional Gyro used in Collins MCS-65 Magnetic Compass System
  • Used in conjunction with FDU-70 Flux Detector Unit, and either CCU-65 Control & Compensator Unit or RCP-65 Remote Compensation Unit
  • Contains air-erected directional gyro and compass electronics
  • Compass electronics combines the short-term directional information from the gyro with long-term heading information from the FDU-70 to obtain accurate heading information for use or display by electromechnical or electronic horizontal situation indicators (HSIs), radio magnetic indicators (RMIs), course indicators, and digital autopilots
  • 28VDC aircraft input power
  • Mounted on a surface perpendicular to aircraft yaw axis within 1 degree
  • Version available that provides slaving meter drive signal and sends DG mode annunciation data on serial bus (-002 see table below)
Dimensions: 6.00"W x 5.210"H x 9.50"L Weight: 5.6 lbs.
TSO: C6c Temperature: -55 to +70C (continuous)
Altitude: up to 55000 ft. Shock: 6g
Warmup Time: 2 minutes (approx) Accuracy: +-2 degrees of local magnetic heading
Part NumberDirectional Gyro Description:
622-6136-001 Original production version, no longer in production, superceded by -002
622-6136-002 With slave meter and DG annunciation data output as described above


- Directional Gyro

NSN: 6615-01-311-6126

Price Condition Status
- Directional Gyro

NSN: 6615-01-308-3085

Price Condition Status

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Negotiating the exchange price of a unit only limits the allowable repair cap for the core unit. Southeast Aerospace's exchange transactions are based on the return of economically repairable core unit. Once the core is received and evaluated, the core repair cost incurred by SEA cannot exceed 75% of the original exchange price. That is, it cannot cost SEA more than 75% of the original OH/SV exchange price collected from the customer. Therefore, when and if an SEA exchange price is discounted, there is a risk that additional charges may be assessed once the core is returned and evaluated.

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