What was found
AIRCRAFT EXPERIENCED TRANSIENT OVER TEMP. HOT SECTION INSPECTION C/W, NO DAMAGE NOTED FROM OCCURRENCE. SUSPECT CAUSE IS AIR LEAK AT BLEED VALVE PR LINE. LEAK CHECK MUST BE DONE WITH BLEED CONTROL SOLENOID IN OPEN POSITION.
- Difficulty date
- November 4, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Aircraft
- N911SA
- Make and model
- Bell 206L1
- Aircraft serial
- 45383
- Engine
- Allsn 250C28B
- System (JASC)
- 7530 · Compressor Bleed Control
- Part
- Tube
- Part number
- 23001804
- Condition
- Leak
- Location
- Bleed Valve
- Component
- 23005367
- Stage of operation
- NR
- Nature of condition
- M
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.