What was found
(CAN) AFTER TAKEOFF #2 HYDRAULIC SYSTEM PRESSURE AND QUANTITY INDICATED ZERO. INSPECTION FOUND THE MAIN LANDING GEAR SEQUENCE VALVE SEPARATED BETWEEN THE VALVE BODY AND THE ELECTRICAL SOLENOID.
- Difficulty date
- December 18, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Dhav DHC8102
- Engine
- Pwa PW120A
- System (JASC)
- 3230 · Landing Gear Retraction/Extension System
- Part
- Valve
- Part number
- 54C546347
- Condition
- Broken
- Location
- Landing Gear
- Part time
- 25,448 hours
- Component
- Kaiser
- Stage of operation
- CL
- Nature of condition
- K
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.