Service difficulty report · Plenum · Cndair CL600*

Difficulty date
March 11, 2004
Submitted
July 22, 2004
Operation
General aviation
Make and model
Cndair CL600*
Engine
Lyc ALF502*
Part
Plenum
Part number
3846068
Condition
Fractured
Location
Apu
Component
Apu
Component part number
GTCP36100E
Stage of operation
IN
How discovered
9
Nature of condition
O
Precautionary procedure
K

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

(CAN) WHEN APU STARTED IT WOULD NOT ACCELERATE PAST 40 PERCENT. INVESTIGATION FOUND A LARGE BREACH OF PLENUM ASSY. NATURE OF FRACTURES APPEARS TO BE FATIGUE RELATED DUE TO VIBRATION. APU REMOVED AND FURTHER INVESTIGATION REVEALED A COMPLETELY DETACHED PIECE BROKEN BRACKET RESTING IN THE COMPRESSOR INLET DUCT. PIECE WAS IDENTIFIED AS A BROKEN FLANGE FROM THE INSIDE OF THE INLET DUCT. INSPECTION OF THE COMPRESSOR ROTOR SHOWED SIGNIFICANT DAMAGE FROM CONTACT WITH THE BRACKET. ELBOW TUBE ASSEMBLY P/N 3846007-1 ATTACHED TOTHE INLET PLENUM WAS ALSO FOUND TO BE LOOSE AND WORN FROM VIBRATION. WHEN THISAPU WAS INSTALLED IT WAS REPORTED TO HAVE A HIGH PITCH WHINE. THE CAUSE WAS NOT DETECTIBLE. IT OPERATED NORMALLY UNTIL