What was found
(CAN) LOSS OF HYDRAULIC FLUID ON LANDING. NR 8 GROUND SPOILER CYLINDER SPLIT IN TWO AT PISTON SIDE. REPLACED.
- Difficulty date
- May 26, 1999
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Boeing 7372A9C
- Engine
- Pwa JT8D9A
- System (JASC)
- 2782 · Leading Edge Slat Actuator
- Part
- Actuator
- Part number
- 65449617
- Condition
- Split
- Location
- Le Flap
- Component
- Boeing · 65449617
- Stage of operation
- LD
- Nature of condition
- K
- Precautionary procedure
- H
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.