What was found
(CAN) COMBUSTION CHAMBER CRACKED 1.5 INCH IN LENGTH ON BACKEND CONE.AT 3 O CLOCK POSITION FRONT OF V BAND.
- Difficulty date
- July 6, 2000
- Submitted
- January 19, 2001
- Operation
- Air carrier
- Make and model
- Bell 205A1
- Aircraft time
- 18,098 hours
- Engine
- Lyc T5313B
- System (JASC)
- 7240 · Turbine Engine Combustion Section
- Part
- Combustion Chamb
- Part number
- 113062005
- Condition
- Cracked
- Location
- Engine
- Stage of operation
- IN
- How discovered
- V
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.