What was found
DURING A ROUTINE 100-HOUR INSPECTION, FOD DAMAGE FOUND TO RT ENGINE AXIAL COMPRESSOR ROTORS AND STATOR VANES. UNABLE TO ESTABLISH EXACT SOURCE OF FOD. OPERATOR TO REVIEW CURRENTLY USED LANDING SITES.
- Difficulty date
- October 9, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Aircraft
- N109TW
- Make and model
- Agusta A109C
- Aircraft serial
- 7650
- Engine
- Allsn 250C20
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Module
- Part number
- 23050833
- Condition
- Fod Damage
- Location
- Axial Comp
- Part time
- 683 hours
- Stage of operation
- IN
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.