Service difficulty report · Window Frame · Cndair CL6002B19

Difficulty date
July 22, 2021
Submitted
August 6, 2021
Operation
Air carrier
Aircraft
N466AW
Make and model
Cndair CL6002B19
Aircraft serial
7899
Aircraft time
37,591 hours, 36,458 cycles
Part
Window Frame
Part number
601R332244
Condition
Gouged
Location
Cockpit
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

CO- PILOTS SIDE WINDOW POST SPLICE STRAP PN 601R33224-4 HAS NUMEROUS SCRATCHES AND GOUGES ON UPPER AND LOWER AREAS. AIRCRAFT REMOVED FROM SERVICE, BLENDED 11 TOOLING MARKS ON RH WINDSHIELD SIDE POST SPLICE STRAP. MEASUREMENTS: P1=L=3.00Ï¿½XW=1.500Ï¿½XD=0.008Ï¿½, ORIGINAL THICKNESS 0.190Ï¿½, REMAINING THICKNESS 0.177Ï¿½ P2=L=1.00Ï¿½XW=0.700Ï¿½XD=0.001Ï¿½,ORIGINAL THICKNESS 0.190Ï¿½,REMAINING THICKNESS 0.179Ï¿½ P3=L=1.700Ï¿½XW=1.200Ï¿½XD=0.004Ï¿½, ORIGINAL THICKNESS 0.190Ï¿½, REMAINING THICKNESS 0.181Ï¿½ P4=L=2.500Ï¿½ X W=1.00Ï¿½XD=0.004Ï¿½, ORIGINAL THICKNESS 0.290Ï¿½,REMAINING THICKNESS 0.283Ï¿½P5=L=1.500Ï¿½XW=1.00Ï¿½XD=0.004Ï¿½,ORIGINAL THICKNESS 0.250Ï¿½, REMAINING THICKNESS 0.241Ï¿½ P6=L=1.800Ï¿½XW=0.500Ï¿½XD=0.003Ï¿½, ORIGINAL THICKNESS 0.290Ï¿½, REMAINING THICKNESS 0.285Ï¿½ P7=L=1.00Ï¿½XW=0.800Ï¿½XD=0.001Ï¿½,ORIGINAL THICKNESS 0.250Ï¿½,REMAINING THICKNESS 0.244Ï¿½ P8=L=1.500Ï¿½XW=1.00Ï¿½XD=0.005Ï¿½,ORIGINAL THICKNESS 0.290Ï¿½,REMAINING THICKNESS 0.277Ï¿½ P9=L=3.00Ï¿½X W=1.00Ï¿½X D=0.003Ï¿½, ORIGINAL THICKNESS 0.190Ï¿½, REMAINING THICKNESS 0.175Ï¿½ P10= L=1.500Ï¿½XW=0.800Ï¿½XD=0.005Ï¿½, ORIGINAL THICKNESS 0.190Ï¿½, REMAINING THICKNESS 0.174Ï¿½ P11= L=1.200Ï¿½XW=0.800"XD=0.006Ï¿½, ORIGINAL THICKNESS 0.190Ï¿½,REMAINING THICKNESS 0.174Ï¿½ BLENDED DAMAGES IAW REO 601R-53-11-3719 REV (--) DATED 2021-07-28. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS AND PERFORMED IAW REO 601R-53-11-3719 REV (--) DATED 2021-07-28.