What was found
(CAN) NR 2 ENGINE WOULD NOT DEVELOP FULL POWER. HP BLEED CONTROL LINE CRACKED AND SHEARED OFF AT 13TH STAGE CONNECTION.
- Difficulty date
- April 16, 1998
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Boeing 727221
- Engine
- Pwa JT8D17
- System (JASC)
- 7530 · Compressor Bleed Control
- Part
- Line
- Part number
- 451077
- Condition
- Sheared
- Location
- Nr 2 Engine
- Stage of operation
- TO
- Nature of condition
- R
- Precautionary procedure
- C
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.