Service difficulty report · Frame · Cndair CL6002C10

Difficulty date
November 3, 2020
Submitted
January 8, 2021
Operation
Air carrier
Aircraft
N609SK
Make and model
Cndair CL6002C10
Aircraft serial
10020
Aircraft time
42,111 hours, 31,503 cycles
Part
Frame
Condition
Corroded
Location
Zone 100
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

FS 333.00 CIRCUMFERENTIAL JOINT BETWEEN STRINGERS 20L/21L AND 21L/22L HAS CORROSION. C-CHECK RO 1/5/2021. REMOVED CORROSION AT CIRCUMFERENTIAL JOINT FS 333.00 BETWEEN STRINGER 20L/21L AND STRINGER 21L/22L, REF CRJ 700 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS OF FS 333.00 BUTTSTRAP BETWEEN STR 20L AND STR 21L IS .095 AND BETWEEN STR 21L AND STR 22L IS .063, REF DWG SH670-32435 REV A. MINIMUM REMAINING MATERIAL THICKNESS BETWEEN STR 20L AND STR 21L IS .082 AND BETWEEN STR 21L AND STR 22L IS .061. FS 333.00 BUTTSTRAP IS FOUND TO BE OUT OF LIMITS DUE TO DAMAGE NOT BEING LESS THEN 20X OF FASTENERS AND EDGE OF SKIN AS WELL AS BEING MORE THAN 10% OF ORIGINAL MATERIAL THICKNESS LOST BETWEEN STR 20L AND STR 21L, REF CRJ 700 SRM 53-00-00-101-001-A01. RECEIVED AND COMPLIED WITH REO 670-53-21-1868 REV. DATED 2020-11-16. DAMAGE FOUND TO BE WITHIN LIMITS. NO LEAKS NOTED.