What was found
LOSS OF HYDRAULIC BOOST DUE TO HYDRAULIC FLUID LEAKING FROM SMALL HOLE ON PRESSURE LINE FROM HYDRAULIC PUMPS TO FILTER HEAD. INTERNAL BREAKDOWN DUE TO RUBBER SWELLING. REPLACED PRESSURE LINE. OPS CHECK OK.
- Difficulty date
- July 20, 1995
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Aircraft
- N37741
- Make and model
- Bell 206B
- Aircraft serial
- 1695
- System (JASC)
- 2910 · Hydraulic System, Main
- Part
- Line
- Part number
- 70010H000A180
- Condition
- Leaking
- Location
- Hyd Pump
- Stage of operation
- IN
- Nature of condition
- K
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.