What was found
(CAN) TUBE CHAFED INSIDE SUPPORTING CLAMP P/N S2894-24 TUBE 6555511-17 AND CLAMP (REVISED P/N 471-24) REPLACED LT AND RT ENGINE. THIS WAS FOUND DURING PERFORMANCE OF SB 560-71-05 WHICH WAS TO INSPECT TUBE AND INSTALL REVISED CLAMP.
- Difficulty date
- April 19, 2004
- Submitted
- June 4, 2004
- Operation
- General aviation
- Make and model
- Cessna 560CESSNA
- Aircraft time
- 26 hours
- Engine
- Pwa PW535A
- System (JASC)
- 7530 · Compressor Bleed Control
- Part
- Tube
- Part number
- 655551117
- Condition
- Worn
- Location
- Bleed Air
- Stage of operation
- IN
- How discovered
- C
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.