What was found
(AUS) NR 1 ENGINE SHUT DOWN FOLLOWING LT WING OVERHEAT WARNING.INVESTIGATION FOUND THE CLAMP ATTACHED TO THE PNEUMATIC FLOWCONTROL VALVE DOWNSTREAM FROM THE NO1 ENGINE BLEED PORT CORRODEDAND RUPTURED CAUSING EXCESSIVE AIR LEAKS.
- Difficulty date
- April 6, 2003
- Submitted
- May 6, 2003
- Operation
- General aviation
- Make and model
- Reims F406
- Engine
- Pwa PT6A112
- Propeller
- Mcauly 3GFR34C701
- System (JASC)
- 3610 · Pneumatic Distribution System
- Part
- Clamp
- Part number
- W901B24DE
- Condition
- Corroded
- Location
- Pneumatic Sys
- Stage of operation
- CR
- How discovered
- O
- Nature of condition
- J
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.