Service difficulty report · Stringer · Cndair CL6002C10

Difficulty date
June 1, 2016
Submitted
June 20, 2016
Operation
Air carrier
Aircraft
N708EV
Make and model
Cndair CL6002C10
Aircraft serial
10060
Aircraft time
33,074 hours, 23,493 cycles
Part
Stringer
Condition
Corroded
Location
Fuselage
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.

What was found

STR 21R CORRODED BETWEEN FS 349-FS 364. REMOVED RIVETS FROM STR 21R FROM FS 333-FS 379 IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01. RECEIVED NEW STR 21R, FS 333-379 PICKED UP ALL HOLES COMMON TO FUSELAGE SKIN, PICKED UP HOLES IN VERTICAL LEG OF STR 21R MINUS HOLES FOR BRACKET, SN 670-41524-5, REF SRMS 51-40-11-001-001-A01 AND DWG SH 670-31950. FINISHED PICKING UP HOLES IN STR 21R, FS 333-379 REF SRM 51-400-11-001-001-A01 AND DWG SH670-31350. INSTALLED FASTENERS IN SR 21R, FS 333-379 COMMON TO ACFT SKIN REF SRM 51-42-06-001-001-A01 AND DWG SH670-31-350. INSTALLED 4 EA LOCK FASTENERS COMMON TO FUSELAGE SKIN AT FS 333 IAW SRM 51-42-21-001-001-A01, DWG SH670-31950 AT STR 21R.