What was found
(CAN) DURING START THE #2 ENGINE TEMPERATURE WAS HOTTER THAN #1 ENGINE. THE COMPRESSOR BLEED VALVE WAS CHANGED AND DURING SUBSEQUENT STARTS THE TEMPERATURE WAS COOLER. TREND MONITORING CONFIRMED THE COOLER OPERATION.
- Difficulty date
- February 7, 1997
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Dhav DHC6300
- Engine
- Pwa PT6A27
- System (JASC)
- 7532 · Compressor Bleed Valve
- Part
- Bleed Valve
- Part number
- 310082903
- Condition
- Orifice Dirty
- Location
- Compressor
- 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.