What was found
AFTER Z STIFFENER REMOVAL, CRACK WAS FOUND AT ACOUSTIC PANEL SKIN OF THE RH UPPER TRANSCOWL ACOUSTIC PANEL SKIN OF THE RH UPPER TRANSCOWL WAS REPAIRED PER EA CRJ954-21346 REV IR
- Difficulty date
- January 31, 2026
- Submitted
- August 1, 2026
- Operation
- Air carrier
- Aircraft
- N295PQ
- Make and model
- Cndair CL6002D24
- Aircraft serial
- 15295
- Aircraft time
- 27,099 hours, 20,831 cycles
- System (JASC)
- 7830 · Engine Thrust Reverser
- Part
- Acoustic Panel
- Part number
- CN6242103204
- Condition
- Cracked
- Location
- Zone 400
- Stage of operation
- IN
- How discovered
- V
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.