What was found
(CAN) UPON INITIAL INSTALLATION OF HYDRAULIC HOSE (TAIL ROTOR CONTROL SERVO) THE FLARE FITTING SPLIT ALONG LENGTH OF FLARE NUT/FERRULE (ONE PIECE). HOSE RETURNED TO MFG FOR WARRANTY REPLACEMENT.
- Difficulty date
- April 8, 2003
- Submitted
- April 14, 2003
- Operation
- Air carrier
- Make and model
- Snias AS350B2
- Aircraft time
- 8,343 hours
- Engine
- Tmeca ARRIEL1D1
- System (JASC)
- 6720 · Tail Rotor Control System
- Part
- Hose
- Part number
- 704A34412047
- Condition
- Cracked
- Location
- Hyd System
- Stage of operation
- IN
- How discovered
- 9
- Nature of condition
- K
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.