What was found
(CAN) NR 1 HYDRAULIC SYSTEM GRADUALLY LOST PRESSURE, WARNING LIGHT CAME ON AND NR 1 SYSTEM WAS SHUT DOWN. POST-LANDING CHECK REVEALED HYDRAULIC FLUID LEAKING FROM T/R SERVO ACTUATOR.
- Difficulty date
- September 29, 1999
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Make and model
- Bell 212
- Engine
- Pwa PT6T3
- System (JASC)
- 6730 · Rotorcraft Servo System
- Part
- Servo
- Part number
- 212076004003
- Condition
- Leaking
- Location
- Tail Rotor
- Stage of operation
- CR
- Nature of condition
- F, J
- Precautionary procedure
- A
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.