What was found
FLIGHT CREW REPORTED THE RIGHT BLEED FAULT LIGHT ILLUMINATED DURING CLIMBOUT. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE DUAL TEMP CONTROL VALVE, GROUND RAN WITH ALL INDICATIONS NORMAL.
- Difficulty date
- September 24, 2000
- Submitted
- June 12, 2001
- Operation
- Air carrier
- Aircraft
- N125CH
- Make and model
- Saab SF340A
- Aircraft serial
- 340A125
- Aircraft time
- 28,934 hours, 34,573 cycles
- Engine
- Ge CT75A2
- Propeller
- Rotol R3894123F25
- System (JASC)
- 7500 · Engine Bleed Air System
- Part
- Control Valve
- Part number
- 7769022
- Condition
- Failed
- Location
- Bleed Air
- Stage of operation
- CL
- How discovered
- O
- Nature of condition
- J
- Precautionary procedure
- D
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.