Service difficulty report · Attach Angle · Cndair CL6002C10

Difficulty date
December 9, 2020
Submitted
January 21, 2021
Operation
Air carrier
Aircraft
N758EV
Make and model
Cndair CL6002C10
Aircraft serial
10210
Aircraft time
36,124 hours, 26,338 cycles
Part
Attach Angle
Condition
Corroded
Location
Body Fairing
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

CORROSION ALONG THE FWD FUSELAGE BODY FAIRING (191BB & 192BB) ATTACH STRAP AND ATTACH ANGLE MATING SURFACE APPROXIMATELY FS 613-FS 661, STR 20R-STR 20L. C-CHECK RO 1/17/2021. REMOVED CORROSION ON TEE ATTACH ANGLE AT BL 0 BETWEEN FS 629-661, REF CRJ700 SRM 51-21-06-001-001-A01. MECHANICALLY MEASURED REMAINING MATERIAL AND FOUND TO BE OUT OF LIMITS, REF CRJ700 SRM 53-82-55-101-001-A01 AND DWG SH670-39063 REV A. REMOVED AND REPLACED TEE ANGLE WITH NEW TEE ANGLE P/N SH670-39063-3. REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-39050 REV H. REMOVED CORROSION ON WING FAIRING STRUCTURE STRAP AT FS 629 LT & RT, REF CRJ700 SRM 51-21-06-001-001-A01. BLENDS ARE WITHIN LIMITS FOR STRAP, REF CRJ700 SRM 53-82-55-101-001-A01. RESTORED FINISH AND RE-APPLIED SELF CONTOURING PAD TO WING FAIRING STRAP STRUCTURE, REF CRJ700 SRM 51-21-16-001-001-A01 TEMP REVISION 51-0068 AND SRM 51-23-00-001-001-A01. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.