N921EV

Part: DOOR FRAME — CRACKED (PAX DOORWAY) · airframe 34,333 hrs · 34,719 cycles

TRANSFER FROM EAML 660702 : TRANSFERRED FROM CAMP 22966043. PASSENGER DOOR AFT FRAME HAS A CRACK RUNNING APPROX. 3" ALONG ANGLE JUST BELOW WHERE DOOR PULLEY IS ATTACHED. (R-O 6/19/21 - IN SERVICE - FILED CLOSED)REPAIRED MCD AFT FORMER UNDER PULLEY MOUNTING BRACKET IN REF TO REO 601R-52-11-2880, REV.--, DATED 2021-06-19. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 33,672 hrs · 33,835 cycles

FLOOR SEAT TRACK LBL 9 FS 409+18 TO FS 559+4 CORRODED BEYOND LIMITS, REQUIRES REPLACEMENT. C-CHECK RO 11/24/2020. INSTALLED A NEW SEAT TRACK, IAW CRJ200 AMM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 33,672 hrs · 33,835 cycles

CENTER INTERCOSTAL CORRODED AT DOOR DATUM 2 OF PAX DOOR. C-CHECK RO 11/24/2020. REMOVED AND REPLACED CENTER INTERCOSTAL AT DATUM 2 OF PAX DOOR, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: SKIN — CORRODED (EXTERIOR) · airframe 33,672 hrs · 33,835 cycles

INTERNAL SIDE OF EXTERNAL SKIN CORRODED AT DOOR DATUM 2 AND FS 329.5. C-CHECK RO 11/24/2020. REPAIRED PAX DOOR OUTER SKIN AT DATUM 2 AND FS 329.5, IAW MHIRJ REO. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. WEIGHT ADDED 0.18 LBS.

Part: SKIN — CHAFED (FUSELAGE) · airframe 33,672 hrs · 33,835 cycles

WHILE PERFORMING REINSPECT FOR RA REPAIRED CENTER WING LOWER PLANK CHAFFED AT LT AFT OUTBOARD CORNER UNDER PANEL 193AB, PER REO, REQUIRES SPECIAL DETAILED INSPECTIONS, NDT INSPECT REWORKED AREA. ADDITIONAL DAMAGE WAS FOUND AND EDDY CURRENT WAS UNABLE TO BE PERFORMED. ADDITIONAL DAMAGE NEEDS EVALUATED FOR ENGINEERING DISPOSTION. C-CHECK RO 11/24/2020. REPAIRED CHAFED AREA OF LOWER WING PLANK AT LT OUTBOARD CORNER UNDER PANEL 193AB, IAW MHIRJ REO. COMPLETED SKYWEST TASK CARD AND ATTACHED FORM M-337. WEIGHT AND BALANCE NOT AFFECTED.

Part: PRESSURE DECK — CORRODED · airframe 33,672 hrs · 33,835 cycles

LT PRESSURE FLOOR SILL PANEL HAS 17 AREAS OF CORROSION AROUND SCREW HOLES AT FRAME STATIONS 424, 429, 435, 441, 447, 453, 459, 467, 478, 486, 493, 503, 518, 522, 531, 539 AND 555. C-CHECK RO 11/24/2020. COMPLETED REO. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. COMPLETED SKYWEST TASK CARD AND ATTACHED FORM M-337. WEIGHT AND BALANCE NOT AFFECTED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 33,672 hrs · 33,835 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED. C-CHECK RO 11/24/2020. REPLACED PAX DOOR AFT DRAG ANGLE, IAW CRJ 200 SRM. REFERENCE REO FOR MATERIAL CALL OUT AND FASTENER SIZE. REFERENCE MX TRAN 21722399 JOB 9781981 OPERATIONS 484 FOR INSTALL OF DRAG ANGLE.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 33,672 hrs · 33,835 cycles

RT PRESSURE FLOOR SILL PANEL HAS SEVERAL AREAS OF CORROSION AROUND SCREW HOLES AT FRAME STATIONS 424, 428, 435, 441, 447, 453, 459, 467, 486, 493, 501, 507, 521, 531, 537, 542, 548 AND 555. C-CHECK RO 11/24/2020. COMPLETED REO. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. COMPLETED SKYWEST TASK CARD AND ATTACHED FORM M-337. WEIGHT AND BALANCE NOT AFFECTED.

Part: INTERCOSTAL — DAMAGED (ZONE 200) · airframe 33,672 hrs · 33,835 cycles

LT EMERGENCY EXIT SURROUND STRUCTURE INTERCOSTAL FWD OF OPENING AT FS 444, BETWEEN STRINGERS 9L AND 10L, HAS TOOLING DAMAGE. C-CHECK RO 11/24/2020. REMOVED AND REPLACED LT EMERGENCY EXIT INTERCOSTALS AT FS 444 AT STR 9L AND 10L, IAW CRJ 200 SRM. COMPLETED TASK CARD. NO WEIGHT CHANGED NOTED.

Part: FRAME SPLICE — CORRODED (FUSELAGE) · airframe 33,672 hrs · 33,835 cycles

UPPON REMOVAL OF FS 333.00 FRAME LOWER SEGMENT, FOUND FS 333.00 CIRCUMFRENTIAL SPLICE TO BE CORRODED AT STR 27. C-CHECK RO 11/24/2020. REPAIRED FS 333 FRAME, IAW MHIRJ REO. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: DOOR FRAME — CRACKED (PAX DOORWAY) · airframe 33,672 hrs · 33,835 cycles

PAX DOOR UPPER SILL, STRINGER 3L IS CRACKED AT FS 379.00. C-CHECK RO 11/24/2020. REPAIRED STR 3L AT FS 379, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM M-337. NO WEIGHT CHANGE.

Part: BRACKET — CRACKED (WINDOW POST) · airframe 33,672 hrs · 33,835 cycles

RT WINDSHIELD SIDEPOST LOWER AFT BRACKET IS CRACKED. C-CHECK RO 11/24/2020. REMOVED DAMAGED RT WINDSHIELD SIDEPOST LOWER AFT BRACKET. LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE BRACKET, IAW CRJ200. COMPLETED TASK CARD, FORM M-337 ATTACHED. WEIGHT AND BALANCE NOT AFFECTED.

Part: BRACKET — CRACKED (ZONE 200) · airframe 33,672 hrs · 33,835 cycles

FS 621.00 TO FS 625.30 ANGLES AT STGR 14L AND 14R ARE CRACKED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED 2 EA ANGLES AT FS 621-625.30 STR 14L AND 14R, IAW CRJ200 SRM.

Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 33,672 hrs · 33,835 cycles

PAX DOOR FORWARD ANCHOR FITTING SERRATED PLATE IS CORRODED. C-CHECK RO 11/24/2020. REPLACED PAX DOOR FORWARD ANCHOR FITTING SERRATED PLATE, PER CRJ 200 AMM TORQUE WRENCH 204360 DUE 30-SEP-21.

Part: DOOR SILL — CORRODED (ZONE 100) · airframe 33,672 hrs · 33,835 cycles

CARGO DOOR SILL HAS MULTIPLE AREAS OF CORROSION ALONG LENGTH OF SILL. C-CHECK RO 11/24/2020. REMOVED AND REPLACED CARGO SILL, IAW REO FORM M-337 AND MAJOR REPAIR TASK CARD COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 33,672 hrs · 33,835 cycles

LBL 27.00 FLOORBEAM IS CORRODED AT (1) LOCATION BETWEEN FS 559.00+96 AND FS 559.00+112. C-CHECK RO 11/24/2020. PERFORMED A MAJOR REPAIR TO FLOOR BEAM AT LBL 27 BETWEEN FS 559.00+96 AND FS 559.00+112, IAW CRJ200 SRM. COMPLETED SKYWEST MAJOR REPAIR TASK CARD. FORM M-337 IS ATTACHED. WEIGHT AND BALANCE NOT AFFECTED.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 33,672 hrs · 33,835 cycles

RBL 9.00 FLOORBEAM CAP IS CORRODED AROUND MOST NUTPLATES ON THE INBOARD SIDE OF BEAM BETWEEN FS 409.00+128 TO FS 559.00. C-CHECK RO 11/24/2020. REPAIRED RBL 9 FLOORBEAM CAP, IAW REO. FORM 337 AND MAJOR REPAIR TASK CARD COMPLETED AND ATTACHED. WEIGHT CHANGE 2.29 LBS. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 33,672 hrs · 33,835 cycles

RBL 27.00 FLOORBEAM CAP IS HEAVILY CORRODED AT FS 559.00+80, INBOARD AND OUTBOARD SIDE OF BEAM. C-CHECK RO 11/24/2020. REMOVED AND REPLACED RBL 27.00 FLOORBEAM CAP AT FS 559+64 TO FS 559+112, IAW CRJ200 SRM. FORM 337 AND MAJOR REPAIR TASK CARD COMPLETED AND ATTACHED. WEIGHT CHANGE NEGLIGIBLE.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 33,672 hrs · 33,835 cycles

CARGO SEAT TRACK ON LBL 9.00 JUST FORWARD OF FS 621.00 IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED SEAT TRACK, IAW CRJ200 AMM.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 33,672 hrs · 33,835 cycles

LBL 9.00 FLOORBEAM CAP IS CORRODED AROUND MOST NUTPLATES ON THE INBOARD SIDE OF BEAM BETWEEN FS 409.00+128 TO FS 559.00. C-CHECK RO 11/24/2020. REPAIRED LBL 9.00 FLOORBEAM CAP IS CORROSION AROUND MOST NUTPLATES ON THE INBOARD SIDE OF BEAM BETWEEN FS 409.00+128 TO FS 559.00, IAW REO. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 33,672 hrs · 33,835 cycles

CARGO SEAT TRACKS BETWEEN FS 559.00+80 AND FS 559.00+96 AT RBL 27.00, RBL 9.00, LBL 9.00 AND LBL 27.00 ARE CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED CARGO SEAT TRACKS BETWEEN FS 559.00+80 AND 559.00+96 AT RBL 27.00, RBL 9.00, LBL 9.00 AND LBL 27.00, IAW CRJ-200 AMMS. CALIBRATED TOOL: TORQUE DRIVER WVACT2759, CAL: 15-JUN-20 CAL DUE: 30-JUN-21.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 33,672 hrs · 33,835 cycles

CARGO SEAT TRACK BETWEEN FS 559.00+112 AND APPROXIMATELY FS 570.00, RBL 9.00 AND LBL 9.00 ARE CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED TRACK, IAW CRJ200 AMM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 33,672 hrs · 33,835 cycles

SEAT TRACK ON RBL 9.00 IS CORRODED BETWEEN FS 409.00+128 TO FS 559.00. C-CHECK RO 11/24/2020. REMOVED AND REPLACED SEAT TRACK ON RBL 9.00 BETWEEN FS 409.00+128 TO FS 559.00, IAW CRJ200 AMM. REFERENCE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 33,672 hrs · 33,835 cycles

RBL 9.00 FLOORBEAM CAP IS CORRODED AT MULTIPLE LOCATIONS ON THE INBOARD SIDE BETWEEN FS 559.00 AND FS 559.00+48. C-CHECK RO 11/24/2020. REMOVED AND REPLACED FLOORBEAM CAP FROM FS 559+10-FS 559+112, IAW MHIRJ REO. FLOORBEAM CAP FABRICATED, IAW CRJ 200 SRM. REFERENCE CONTINUATION CARD FOR DETAILS OF WORKED PERFORMED. FORM M337 AND MAJOR REPAIR TASK CARD COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED.

Part: FITTING — CRACKED (ZONE 100) · airframe 33,672 hrs · 33,835 cycles

FS 461.00 FLOORBEAM FITTING IS CRACKED ON THE OUTBOARD SIDE OF BEAM, RBL 9.00. C-CHECK RO 11/24/2020. REMOVED AND REINSTALLED FLOOR BEAM FITTING AT RBL 9 FS 461, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGES NOTED.

Part: FRAME — CORRODED (ZONE 100) · airframe 33,672 hrs · 33,835 cycles

FS 333 FRAME IS CORRODED BETWEEN STGR 25L AND STGR 25R. C-CHECK RO 11/24/2020. REMOVED AND REPLACED LOWER FRAME SEGMENT FS 333 LOWER FRAME SEGMENT, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 33,672 hrs · 33,835 cycles

STGR 27 IS CORRODED BETWEEN FS 319 AND FS 349. C-CHECK RO 11/24/2020. REPAIRED STGR 27 BETWEEN FS 319 AND FS 349 BY STRINGER SPLICE REPAIR, IAW CRJ SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 33,672 hrs · 33,835 cycles

RBL 9 FLOORBEAM INBOARD AND OUTBOARD CLIP ANGLE AT FS 280 IS CRACKED. C-CHECK RO 11/24/2020. REMOVED AND FABRICATED NEW AND REPLACED RBL 9 INBOARD AND OUTBOARD CLIP ANGLE AT FS 280, IAW CRJ 200 SRM AND IN REF TO REO. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: DOUBLER — CORRODED (BS 286) · airframe 33,672 hrs · 33,835 cycles

FLOOR SUPPORT BOLT HOLE DOUBLER AT FS 286 RBL 37 IS CORRODED. C-CHECK RO 11/24/2020. INSTALLED SERVICABLE BOLT HOLE DOUBLER, IAW CRJ 200 SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 33,672 hrs · 33,835 cycles

FS 280 CROSSBEAM AND FWD "J" ANGLE ARE CORRODED BETWEEN LBL 11 AND RBL 27. C-CHECK RO 11/24/2020. REMOVED AND INSTALLED J-ANGLE AT FS 280, IAW CRJ-200 SRM. INSTALLED FS 280 CROSSBEAM CENTER SECTION OF PREVIOUS REPAIR, IAW CRJ-200 SRM AND REF BOMBARDIER REO FOR FASTENER CALL OUT.

Part: FRAME — CORRODED (ZONE 100) · airframe 33,672 hrs · 33,835 cycles

FS 319 FRAME IS CORRODED BETWEEN STGR 26L AND STGR 25R. C-CHECK RO 11/24/2020. REMOVED AND REPLACED LOWER FRAME SEGMENT AT FS 319, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: STRAP — CORRODED (DOOR SILL) · airframe 33,672 hrs · 33,835 cycles

PAX DOOR LOWER SILL FRAME STRAP IS CORRODED AT FS 349. C-CHECK RO 11/24/2020. REPAIRED PAX DOOR LOWER SILL FRAME STRAP, IAW CRJ200 SRM. REFER TO CONTINUATION CARD FOR REPAIR DETAILS.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 33,672 hrs · 33,835 cycles

RBL 9 FLOOR BEAM IS CORRODED BETWEEN FS 409+52 AND FS 409+128. C-CHECK RO 11/24/2020. PERFORMED MAJOR REPAIR ON RBL 9 FLOORBEAM CAP BETWEEN FS 409+48.00 AND FS 409+118.00, IAW CRJ200 SRM AND MHIRJ REO. COMPLETED TASK CARD FOR STRUCTURAL MAJOR REPAIR. FORM M-337 ATTACHED. WEIGHT CHANGE NEGLIGABLE.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 33,672 hrs · 33,835 cycles

LBL 9 FLOOR SEAT TRACK FS 364-FS400 SEGMENT IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED SEAT TRACK, IAW CRJ200 AMM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 33,672 hrs · 33,835 cycles

RBL 9 FLOOR SEAT TRACK FS 364-FS 400 SEGMENT IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED SEAT TRACK, IAW CRJ200 AMM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 33,672 hrs · 33,835 cycles

LBL 9 FLOOR SEAT TRACK FS 400-FS 409+128 SEGMENT IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED SEAT TRACK SEGMENT, IAW CRJ200 AMM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 33,672 hrs · 33,835 cycles

LBL 9 FLOORBEAM IS CORRODED BETWEEN FS 409+5 AND FS 409+128. C-CHECK RO 11/24/2020. PERFORMED MAJOR REPAIR TO LBL 9 FLOOR BEAM CAP FROM FS 409+5.00 TO FS 409+118.00, IAW CRJ200 SRM AND MHIRJ REO. COMPLETED TASK CARD FOR STRUCTURAL MAJOR REPAIR. FORM M-337 ATTACHED WEIGHT CHANGE NEGLIGABLE.

Part: SUPPORT ANGLE — CORRODED (DOOR SILL) · airframe 33,672 hrs · 33,835 cycles

PAX DOOR SILL FLOOR SUPPORT ANGLES AND CUPS ARE CORRODED BETWEEN FS 310 AND FS 349. C-CHECK RO 11/24/2020. REMOVED AND REPLACED PAX DOOR SILL FLOOR SUPPORT ANGLE AT FS 310-FS 349, IAW CRJ200 SRM.

Part: MOUNT — CORRODED (FLOOR SUPPORT) · airframe 33,672 hrs · 33,835 cycles

FLOOR SUPPORT BOLT HOLE DOUBLER AT FS 297 RBL 6 IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED FLOOR SUPPORT BOLT HOLE DOUBLER AT FS 297 RBL 6, IAW CRJ-200 SRMS.

Part: BOLT — CORRODED (LT SPOILER HINGE) · airframe 33,672 hrs · 33,835 cycles

LEFT SPOILERON OUTBOARD HINGE BOLT STOPPER BRACKET HAS 1 EA CORRODED BOLT AND INBOARD HINGE STOPPER BRACKETS HAVE 4 EA CORRODED BOLTS. C-CHECK RO 11/24/2020. REMOVED AND REPLACED LT SPOILERON OUTBOARD HINGE BOLT STOPPER BRACKET BOLT (1 EA) AND INBOARD HINGE BOLT STOPPER BRACKET BOLTS (4 EA), IAW CRJ200 AMM.

Part: BOLT — CORRODED (LT SPOILER HINGE) · airframe 33,672 hrs · 33,835 cycles

LEFT SPOILERON HINGE BOLTS HAVE CORRODED NUTS (3 EA) AT THE OUTBOARD, CENTER AND INBOARD LOCATIONS. C-CHECK RO 11/24/2020. REMOVED AND REPLACED HARDWARE, IAW CRJ200 AMM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: BOLT — CORRODED (HORIZONTAL STAB) · airframe 33,672 hrs · 33,835 cycles

HORIZONTAL STAB FWD STEADY FITTING 5 EA LOWER MOUNT BOLTS ARE CORRODED. C-CHECK RO 11/24/2020. REPLACED 5 CORRODED BOLTS ON THE HORIZONTAL STAB FWD FITTING LOWER MOUNT, IAW CRJ 200 AMM. CALIBRATED TORQUE WRENCH USED NR WVACT203581 DUE 31-DEC-20.

Part: NUT — CORRODED (LT SPOILER) · airframe 33,672 hrs · 33,835 cycles

LEFT FLIGHT SPOILER HINGE BOLTS HAVE CORRODED NUTS (3 EA) AT THE CENTER AND OUTBOARD HINGES. C-CHECK RO 11/24/2020. REMOVED AND REPLACED WITH SERVICEABLE NUTS (P/N MS17825-6, 1 EA AND MS17825-5, 2 EA ON LEFT HAND FLIGHT SPOILER CENTER AND OUTBOARD HINGES, IAW CRJ 200 AMM.

Part: BEAM — CORRODED (RT WING TE FLAP) · airframe 33,672 hrs · 33,835 cycles

RT INBOARD FLAP, INBOARD VANE SLIDING BEAM, INBOARD SPRING AND HARDWARE ARE CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED CORRODED HARDWARE, IAW CRJ200 AMM.

Part: BOLT — CORRODED (RT WING TE FLAP) · airframe 33,672 hrs · 33,835 cycles

RT OUTBOARD FLAP INBOARD HINGE ARM LOCATED AT WS 178.00 AND OUTBOARD HINGE ARM LOCATED AT WS 264.00 ATTACHING HARDWARE FOUND TO BE CORRODED AND REQUIRES REPLACEMENT. C-CHECK RO 11/24/2020. REMOVED AND REPLACED RT OUTBOARD FLAP HINGE ARM HARDWARE, IAW CRJ200 AMM.

Part: BOLT — CORRODED (SPOILER PCU) · airframe 33,672 hrs · 33,835 cycles

OUTBOARD GROUD SPOILER PCU MOUMTING BOLT NUTS 2 EA ARE CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED NUT, IAW CRJ200 AMM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: BOLT — CORRODED (TE FLAPS HINGE) · airframe 33,672 hrs · 33,835 cycles

MOUNTING HARDWARE ON LT AND RT OUTBOARDD FLAP CENTER HINGES LOCATED AT WS 220.00 FOUND TO BE CORRODED AND REQUIRE REPLACEMENT. C-CHECK RO 11/24/2020. REMOVED AND REPLACED LT AND RT MOUNTING HARDWARE FOR OUTBOARD FLAP CENTER HINGE ARMS, IAW CRJ200 AMM.

Part: HINGE ARM — CORRODED (LT WING TE FLAP) · airframe 33,672 hrs · 33,835 cycles

LT OUTBOARD FLAP INBOARD HINGE ARM LOCATED AT WS 178.00 AND OUTBOARD HINGE ARM LOCATED AT WS 26400 ATTACHING HARDWARE FOUND TO BE CORRODED AND REQUIRES REPLACEMENT. C-CHECK RO 11/24/2020. REMOVED AND REPLACED HARDWARE AT LT OUTBOARD FLAP HINGE ARMS AT WS 178 AND WS 264, IAW CRJ200 AMM.

Part: BONDING WIRE — CORRODED (LT SPOILER PCU) · airframe 33,672 hrs · 33,835 cycles

LEFT OUTBOARD FLIGHT SPOILER OUTBOARD PCU BONDING WIRE HARDWARE IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED BONDING WIRE, IAW CRJ200 AMM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: CONTROL UNIT — CORRODED (LT AILERON) · airframe 33,672 hrs · 33,835 cycles

LEFT AILERON NR 3 (OUTBOARD) PCU ROD END IS CORRODED. C-CHECK RO 11/24/2020. REMOVED LT AILERON NR 3 (OUTBOARD) PCU, IAW CRJ 200 AMM. INSTALLED A SERVICEABLE PCU, IAW SKYWEST TASK CARD. RIGS, OPERATIONS, AND LEAK CHECK GOOD.

Part: CONTROL UNIT — CORRODED (RT AILERON) · airframe 33,672 hrs · 33,835 cycles

RIGHT AILERON NR 3 (OUTBOARD) PCU ROD END IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED RT AILERON NR 3 PCU, IAW SKYWEST TASK CARD. OPERATIONS, LEAKS, AND RIG CHECK GOOD.

Part: SKIN — DAMAGED (ZONE 100) · airframe 33,672 hrs · 33,835 cycles

DURING REMOVAL OF 132AL FOUND 8 ELONGATED HOLES IN FUSELAGE SKIN DOUBLER. C-CHECK RO 11/24/2020. REMOVED AND REPLACED DOUBLER, IAW CRJ200 SRM. FORM M-337 AND MAJOR REPAIR TASK CARD COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: FRAME — CORRODED (ZONE 100) · airframe 33,672 hrs · 33,835 cycles

FS 589 FRAME IS CORRODED BETWEEN STRG 18L TO 19L. C-CHECK RO 11/24/2020. REPAIRED FRAME SEGMENT BY REPLACEMENT, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 33,672 hrs · 33,835 cycles

REAR PRESSURE BULKHEAD FLOORBOARD SUPPORT BETWEEN LBL 36 TO LBL 42 THE SUPPORT ANGLE IS CRACKED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED ANGLE, IAW CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: SUPPORT BRACKET — CRACKED (DOOR TRACK) · airframe 33,672 hrs · 33,835 cycles

CARGO DOOR TRACK BOTTOM SUPPORT CLIP AT FS 574 IS CRACKED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED CLIP, IAW CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: FRAME — CORRODED (ZONE 100) · airframe 33,672 hrs · 33,835 cycles

FS 605 FRAME IS CORRODED BETWEEN STRG 21L TO 22L AND 25L TO 25R. C-CHECK RO 11/24/2020. REMOVED AND REPLACED FS 605 LOWER FRAME SEGMENT, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTCHED COMPLETED FORM M-337. NO WEIGHT CHANGES NOTED.

Part: SUPPORT ANGLE — CRACKED (CRGO DOOR BEAM) · airframe 33,672 hrs · 33,835 cycles

FS 621 CARGO DOOR BEAM SUPPORT CLIP IS CRACKED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED CLIP, IAW CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: LINK — CORRODED (FLUTTER DAMPER) · airframe 33,672 hrs · 33,835 cycles

LT AND RT AILERON FLUTTER DAMPER LINKS HEAVILY CORRODED, REQUIRES REPLACEMENT. C-CHECK RO 11/24/2020. REMOVED CORRODED LINKS FROM LT/RT AILERON FLUTTER DAMPERS AND INSTALLED NEW LINKS, IAW CRJ 200 AMM. OPERATIONAL CHECKS ARE GOOD, IAW CRJ AMM. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: PUMP — OUT OF TOLERANCE (FUEL BOOST) · airframe 33,672 hrs · 33,835 cycles

RT WING FUEL BOOST PUMP CUTOUT HAS MULTIPLE INDICATIONS 50% FSH AROUND ENTIRE CIRCUMFERENCE OF THE VERTICAL & HORIZONTAL LANDINGS. FAILED NDT INSPECTION. C-CHECK RO 11/24/2020. REPAIRED RT WING FUEL BOOST PUMP CUTOUT, IAW REO. FORM 337 AND MAJOR REPAIR TASK CARD COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: INTERCOSTAL — CRACKED (SERVICE PANEL) · airframe 33,672 hrs · 33,835 cycles

INTERCOSTAL UNDER EXTERNAL SERVICES PANEL IS CRACKED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED INTERCOSTAL UNDER EXTERNAL SERVICES PANEL, IAW CRJ 200 SRM. REFERENCE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: HOUSING — GOUGED (CRGO DOOR HANDLE) · airframe 33,672 hrs · 33,835 cycles

CARGO DOOR HANDLE HOUSING IS GOUGED AT THE FORWARD SIDE. C-CHECK RO 11/24/2020. REMOVED AND REPLACED CARGO DOOR HOUSING, IAW CRJ 200 SRM. OPERATIONS CHECK GOOD. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM M-337. NO WEIGHT CHANGE.

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 32,147 hrs · 32,051 cycles

HYD 3 LOW PRESS. RAN QRH WITH MANUAL GEAR EXTENSION. REPLACED #3 HYDRAULIC PRESSURE MANIFOLD FILTER ASSY PLUG O-RING. SERVICED AND BLED THE #3 HYDRAULIC SYSTEM IAW AMM. ALL OPS CHECKS ARE GOOD AND NO LEAKS ARE NOTED.

Part: STRUT — LOW (NLG) · airframe 31,951 hrs · 31,844 cycles

GEAR DISAGREE ON RETRACTION AFTER TAKEOFF. QRH RESOLVED THE WARNING. ALL INDICATIONS NORMAL ON LANDING. (FLT#3552) CLOSED PERFORMED SERVICING OF THE NLG STRUT IAW AMM. OPS TEST OF THE GEAR EXTENSION AND RETRACTION WAS GOOD IAW AMM. NO DEFECT NOTED OR ANY MESSAGES SHOWN DURING ENTIRE OPS TEST.

Part: WATER SEPARATOR — ODOR · airframe 31,732 hrs · 31,589 cycles

FA REPORTED STRONG SMELL FROM FRONT GALLEY OF AIRCRAFT, WITH 1 PASSENGER NEAR THE FRONT OF THE AIRCRAFT REPORTING A SMELL LIKE BURNING RUBBER. THERE WAS NO INDICATION OF SMOKE, FIRE, OR FUMES ANYWHERE THROUGHOUT THE REST OF THE CABIN OR IN THE COCKPIT AND NO INDICATIONS OF ANY PROBLEMS VIA EICAS. (FLT#4198) CLOSED PERFORMED TROUBLESHOOTING - NOTICED AN ODOR COMING FROM THE FLIGHT ATTENDANTS AIR VENT IN GALLEY, VERIFIED WITH THE FLIGHT ATTENDANT ON BOARD AT ARRIVAL THAT THE ODOR WAS THE SAME THAT SHE SMELLED. RAN ENGINES TO SEE IF ODOR INTENSIFIED IAW AMM. REMOVED AND REPLACED THE LH AND RH WATER SEPARATOR COALESCER BAG IAW AMM. NO UNUSUAL ODORS REMAIN.

Part: POST — CRACKED (BS 409) · airframe 29,298 hrs · 28,871 cycles

FS 409 VERTICAL POST AT LBL 18 OTBD SIDE IS CRACKED. INSTALLED A NEW VERTICAL POST ASSY IAW REO AND SRM.

Part: POST — CRACKED (BS 409) · airframe 29,298 hrs · 28,871 cycles

BS 409 VERTICAL POST LBL 18 HAS AN INDICATION NOTED AT AFT FLANGE RADIUS APPROX .300 IN LENGTH 50 % FSH. INSTALLED A NEW VERTICAL POST ASSY IAW REO AND SRM.

Part: POST — CRACKED (BS 409) · airframe 29,298 hrs · 28,871 cycles

BS 409 VERTICAL POST RBL 18 OTBD SIDE HAS INDICATIONS NOTED AT AFT FLANGE RADIUS APPROX .300 IN LENGTH 50 % FSH. INSTALLED A NEW VERTICAL POST IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 29,298 hrs · 28,871 cycles

RIGHT CARGO FLOOR SUPPORT FROM BS 559+80 TO 621 HAS CORROSION IN MULTIPLE LOCATIONS. REPAIRED THE FLOOR SUPPORT IAW REO.

Part: SUPPORT ANGLE — CORRODED (BS 574) · airframe 29,298 hrs · 28,871 cycles

BS 574 TRANSVERSE BEAM CAP FROM RBL 27 TO FLOOR SUPPORT HAS CORROSION IN MULTIPLE LOCATIONS. REMOVED AND REPLACED TRANSVERSE BEAM CAP IAW SRM.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 29,298 hrs · 28,871 cycles

LEFT CARGO FLOOR SUPPORT HAS CORROSION IN SEVERAL LOCATIONS FROM BS 559+80 TO 559+112. REPAIRED THE FLOOR SUPPORT IAW REO.

Part: BEAM — CORRODED (BS 349) · airframe 29,298 hrs · 28,871 cycles

RIGHT TRANSVERSE BEAM AT BS 349 IS CORRODED. REPAIRED THE TRANSVERSE BEAM IAW REO.

Part: FRAME — CORRODED (BS 605) · airframe 29,298 hrs · 28,871 cycles

BS 605 FRAME IS CORRODED BETWEEN STRINGERS 26 TO 27L. REPAIRED IAW SRM.

Part: SKIN — SCRATCHED (BS 605-621) · airframe 29,298 hrs · 28,871 cycles

FUSELAGE EXTERNAL SKIN SCRATCHED 3 X .02 X .003 INCHES BETWEEN BS 605 & 621, STRINGERS 14 AND 15R. REPAIRED IAW SRM.

Part: CIRCUIT BREAKER — TRIPPED · airframe 27,522 hrs · 26,916 cycles

FORWARD GALLEY CURVED OVERHEAD EMERGENCY LIGHT LT TIP LIGHT, INOPERATIVE. SYSTEM SELF RESET. FAULT NO LONGER EXIST IAW MCC. NO FURTHER ACTION REQUIRED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,508 hrs · 26,897 cycles

CURVED OVERHEAD EMERGENCY EXIT LIGHT AT ROW 8 INOPERATIVE. R & R NR 2 BATTERY PACK IAW AMM 33-51-04, REF SUP 33-51-04, ITEM 17. OPS CHECK GOOD. ACFT OK FOR SERVICE.

Part: ROD — BENT (SERVICE DOOR) · airframe 27,270 hrs · 26,650 cycles

F/A REPORTS SERVICE DOOR DIFFICULT TO OPEN. CAPTAIN COULD NOT OPEN FROM OUTSIDE. FOUND INTERNAL STABILIZER ROD BENT. REMOVED AND REPLACED INTERNAL STABILIZER ROD IAW CMM 52-41-12. OPS, RIG, AND LEAK CHECKED GOOD. NO FURTHER DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,120 hrs · 24,324 cycles

EMERGENCY FLOOD LIGHT AT PAX DOOR INOPERATIVE. REPLACED NR 2 BATTERY TRAY IAW AMM 33-51-04.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 24,738 hrs · 23,904 cycles

RIGHT NR 2 EMERGENCY LIGHT AFT OF EMERGENCY EXIT ON EXTERIOR OF ACFT JUST, ABOVE THE WING IS INOPERATIVE. R & R BULB ON RT NR 2 EMERGENCY LIGHT REF AMM TASK 33-51-21-000-801 & 33-51-21-400-801, OPS TEST GOOD IPC 33-51-21, ITEM 18.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 24,738 hrs · 23,903 cycles

EMERGENCY EXIT LIGHTS AT WARDROBE BOTH LOWER LIGHTS, FWD SERVICE DOOR LIGHT AND GALLEY LOWER LIGHTS ARE INOPERATIVE. TROUBLESHOOT EMERGENCY EXIT LIGHTS DS3LY, DS9LY, DS10LY AND DS11LY. DISCONNECTED CONNECTORS J11LY, AND P10LY, J9LY AND P8LY, J20LY AND P21LY, J23LY AND P22LY AND THEN RECONNECTED THEM BACK IAW WM 33-51-00. PERFORMED OPS TEST OF EMERGENCY EXIT LIGHTS 33-51-00-710-801. OPS CHECKED GOOD FOR ALL LIGHT DISCONNECTED BUT DS11LY. FOUND BATTERY PACK NR 1 WAS FAILING TO PROVIDE POWER TO TB110-4. R & R BATTERY CHARGER NR 1 SERVICEABLE CHARGER IAW AMM 33-51-05-000-801 AND 33-51-05-400-801 IPC SUPP 33-51-04, REV C.

Part: ATTACH ANGLE — CRACKED · airframe 24,738 hrs · 23,903 cycles

AFT PRESSURE BULKHEAD LT SIDE, LOWER INTERCOSTAL TO FUSELAGE SKIN CLIP CRACKED 601R36008-209, MAC32QC 3/1/15 (AA). REMOVED AFT PRESSURE BULKHEAD LT LOWER INTERCOSTALS TO FUSELAGE SKIN CLIP. REMOVED AFT PRESSURE BULKHEAD 4TH LOWER INTERCOSTAL FUSELAGE CLIP IAW SRM 51-42-21. REMOVED INTERCOSTALS AT STR14 AND STR15 LT ON AFT PRESSURE BULKHEAD FOR FOM IAW SRM 51-42-06. INSTALLED INTERCOSTALS AT STR 14 & 15 LT ON AFT PRESSURE BULKHEAD IAW SRM 51-42-06. INSTALLED AFT PRESSURE BULKHEAD LT SIDE LOWER INTERCOSTAL TO FUSELAGE SKIN CLIP IAW SRM 51-42-21.

Part: ANGLE — CRACKED (INTERCOSTAL) · airframe 24,738 hrs · 23,903 cycles

AFT PRESSURE BULKHEAD, LT SIDE, 3RD FROM BOTTOM INTERCOSTAL CLIP CRACKED, FROM INTERCOSTAL TO FUSELAGE, 601R36008-141. REMOVED INTERCOSTAL AT STR14 AND STR LT SIDE ON AFT PRESSURE BULKHEAD FOR FOM IAW SRM 51-42-06. INSTALLED INTERCOSTALS AT STR14 & 15 LT SIDE ON AFT PRESSURE BULKHEAD IAW SRM 51-42-00. REMOVED AFT PRESSURE BULKHEAD LT SIDE 3RD FROM BOTTOM INTERCOSTAL CLIP IAW SRM 51-42-21. INSTALLED INTERCOSTAL LT SIDE 3RD FROM BOTTOM IAW SRM 51-42-21.

Part: ANGLE — CRACKED · airframe 24,738 hrs · 23,903 cycles

AFT PRESSURE BULKHEAD, LT SIDE, 2ND FROM BOTTOM INTERCOSTAL CLIP CRACKED, FROM INTERCOSTAL TO FUSELAGE CLIP, 601R36008-143. REMOVED INTERCOSTAL AT STR 14 AND STR 15 LT SIDE ON AFT PRESSURE BULKHEAD FOR FOM IAW SRM 51-42-06. INSTALLED INTERCOSTAL AT STR 14 AND 15 LT SIDE ON AFT PRESSURE BULKHEAD IAW SRM 51-42-06, 51-42-21. REMOVED AFT PRESSURE BULKHEAD LT SIDE 2ND FROM BOTTOM INTERCOSTAL CLIP IAW SRM 51-42-21. INSTALLED INTERCOSTAL CLIP LT SIDE 2ND FROM BOTTOM IAW SRM 51-42-21. FINISHED INSTALLING INTERCOSTALS AT STR 14 AND 15 LT SIDE AFT PRESSURE BULKHEAD IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 24,738 hrs · 23,903 cycles

RBL9 FLOORBEAM CAP SEVERELY CORRODED IN 3 SPOTS BETWEEN FS559.00+64 TO FS559.00+84. REPAIRED FLOOR SUPPORT IAW SRM 53-00-43. COMPLIED WITH REO 601R-53-00-595. COMPLIED WITH EC/TC REO 601R-53-00-595.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 24,738 hrs · 23,903 cycles

FLOOR SEAT RAIL AT RBR9 BETWEEN FS 409.00+128 TO FS 559.00 HAS EXFLOATION CORROSION IN SEVERAL PLACES. REMOVED FLOOR SEAT RAIL AT RBR9 BETWEEN FS 409.00 + 128 TO FS 559.00 IAW AMM 53-01-11-000-802. DRILLED UP NEW SEAT RAIL AT RBR 9 BETWEEN FS 409.00 + 128 TO FS 559.00 IAW SRM 51-40-11. INSTALLED NEW SEAT RAIL AT RBR 9 BETWEEN FS 409+128 TO FS 559.00 IAW AMM 51-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,738 hrs · 23,903 cycles

CARGO FLOOR TIE TRACK CORRODED AT FS559+103 559+112 & 559+120. R & R CARGO FLOOR TIE AT FS 559 + 103, 559 + 112, 559 + 120 IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,732 hrs · 23,897 cycles

FLOOR SEAT RAIL SEGMENT LBL9 559+109-559+120 CORRODED. FABRICATED SEAT RAIL IAW GREO 601R-53-00-485, REV A. R & R SEAT RAIL IAW AMM 53-01-11-000/400-802. COMPLIED WITH EC/TC REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,719 hrs · 23,881 cycles

FLOOR SEAT RAIL SEGMENT LBL9 559+84-559+93 CORRODED. FABRICATED SEAT RAIL IAW GREO 601R-53-00-485, REV A. R & R SEAT RAIL IAW AMM 53-01-11-000/400-802. COMPLIED WITH EC/TC REO 601R-53-00-485.

Part: BRACKET — CRACKED (BS 484) · airframe 24,719 hrs · 23,881 cycles

OTBD INTERCOSTAL "L" BRACKET OTBD OF RBL36 AT FS 484.00 IS CRACKED THROUGH THE TOP 3 RIVETS. RECEIVED REO 601R-53-41-1882. COMPLIED WITH REO 601R-53-41-1882. COMPLIED WITH EC/TC REO 601R-53-41-1882.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,732 hrs · 23,897 cycles

FLOOR SEAT RAIL SEGMENT RBL9 559+4-559+84 CORRODED. REMOVED FLOOR SEAT RAIL IAW AMM 53-01-11-000-802. INSTALLED FLOOR SEAT RAIL IAW AMM 53-01-11-400-802. COMPLIED WITH EC/TC REO 601R-53-00-485 FABRICATED SEAT RAIL IAW GREO 601R-53-00-485, REV A.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,719 hrs · 23,881 cycles

FLOOR SEAT RAIL SEGMENT RBL9 559+84-559+93 CORRODED. COMPLIED WITH EC/TC REO 601R-53-00-485. FABRICATED SEAT RAIL IAW GREO 601R-53-00-485, REV A. R & R SEAT RAIL IAW AMM 53-01-11-000/400-802. COMPLIED WITH EC/TC REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,732 hrs · 23,897 cycles

FLOOR SEAT RAIL SEGMENT LBL27 559+78-559+92. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. R & R SEAT RAIL IAW AMM 53-01-11-000/400-802. COMPLIED WITH EC/TC REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,732 hrs · 23,897 cycles

FLOOR SEAT RAIL SEGMENT, RBL27 559+78-559+92, CORRODED. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. R & R SEAT RAIL IAW AMM 53-01-11-000/400-802. COMPLIED WITH EC/TC REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,732 hrs · 23,897 cycles

FLOOR SEAT RAIL SEGMENT, RBL9 559+109-559+120, CORRODED. FABRICATED SEAT RAIL IAW GREO 601R-53-00-485, REV A. R & R SEAT RAIL IAW AMM 53-01-11-000/400-802. COMPLIED WITH EC/TC REO 601R-53-00-485.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 24,719 hrs · 23,881 cycles

OTBD INTERCOSTAL "L" BRACKET OTBD OF LBL36 AT FS 484.00 IS CRACKED THROUGH THE TOP RIVET. RECEVIED REO 601R-53-41-1882. COMPLIED WITH REO 610R-53-41-1882. ECTC REO 601R-53-41-1882 HAS BEEN ACCOMPLISHED.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 24,731 hrs · 23,896 cycles

CORROSION ON FLOOR SUPPORT STRUCTURE AT FS 409.00+123. REMOVED CORROSION AT FS 409.00+123 AT RBL9 IAW SRM 51-21-06. COMPLIED WITH REO 601R-53-41-1884, REV A.

Part: SEAT TRACK — CORRODED (BS 366-394) · airframe 24,719 hrs · 23,881 cycles

CORROSION ON FLOOR SEAT TRACKS BETWEEN FS 366.00 AND FS 394.50 LT AT SEVERAL LOCATION COMPLIED WITH EC/TC 601R-53-00-485. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. REMOVED CORRODED SEAT TRACK. INSTALLED NEW FABRICATED SEAT TRACK IN REF TO AMM 53-01-11-04 & 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 24,719 hrs · 23,881 cycles

CORROSION ON FLOOR SEAT TRACKS BETWEEN FS 394.50 AND FS 409.00+121 LT AT SEVERAL LOCATIONS. COMPLIED WITH EC/TC REO 601R-53-00-485 AND FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. REMOVED SEAT RAIL IAW AMM 53-01-11-000-802. INSTALLED SEAT RAIL IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 24,719 hrs · 23,881 cycles

CORROSION ON FLOOR SEAT TRACK BTW FS 364.00 AND FS 394.50 RT AT SEVERAL LOCATIONS. COMPLIED WITH EC/TC 601R-53-00-485. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV.A. REMOVED CORRODED SEAT TRACK IN REF TO AMM 53-01-11-000-802. INSTALLED NEW FABRICATED SEAT TRACK AT FS 364 TO 394.50 IN REF TO AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 24,731 hrs · 23,896 cycles

CORROSION ON FLOOR SEAT TRACKS BETWEEN FS 394.50 AND FS 409.50 RT AT SEVERAL LOCATIONS. REMOVED SEAT RAILS, 3 EA BETWEEN FS395.50-409.00+ 126 AT RBL9 IAW AMM 53-01-11-000-802. INSTALLED SEAT RAIL IAW AMM 53-01-11-400-802. COMPLIED WITH ECTC REO 601R-53-00-596.

Part: FLOOR SUPPORT — CORRODED · airframe 24,719 hrs · 23,881 cycles

CORROSION ON COCKPIT FLOOR SUPPORT FORWARD ANGLE. REMOVED FINISH AND CORROSION IAW SRM TR 51-31 (5142-00). RESTORED FINISH AS NEEDED REF: STS EA 32-2015-080. RECIEVED STS EA 32-2015-080. COMPLIED WITH SECTION I PERMANENT REPAIR 1.A, B AND C, AT ITEM NR 1 AND NR 4 AND COMPLIED WITH SECTION I-PERMANENT REPAIR 1. D AND E ALL STEPS OF STS AE 32-2015-080 COMPLETED.

Part: SEAT TRACK — CORRODED (BS 499-559) · airframe 24,719 hrs · 23,881 cycles

RT SIDE SEAT RAIL BETWEEN FS 499.00 TO FS 559.00+112 HAS EXFLOATION CORROSION. NO DAMAGE FOUND ON SEAT RAIL BETWEEN FS 499-FS 535.02 SEAT RAIL ENDS AT FS 559.00+75. R & R RT SIDE SEAT RAIL, STA 535.02-559.00+79 IAW AMM 53-01-11-000-802 & 53-01-11-400-802. COMPLIED WITH REO 601R-53-00-505.

Part: STRAP — CORRODED (BS 559) · airframe 24,719 hrs · 23,881 cycles

CROSSBEAM STRAP AT FS 559.00 BETWEEN THE LT SILL AND LBL 27 IS CORRODED. REMOVED CORRODED CROSSBEAM STRAP AT FS 559 BETWEEN THE LT SILL AND LBL 27 IN REF TO SRM 51-42-06-00. INSTALLED NEW SERVICEABLE CROSSBEAM STRAP AT FS 559 BETWEEN THE LT SILL AND LBL27 IN REF TO SRM 51-42-06-00, DWG 601R-31025.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 24,731 hrs · 23,896 cycles

CORROSION ON FLOOR STRUCTURE BETWEEN FS 409.00+5-409.00+121 AND RBL9 AT SEVERAL LOCATIONS. REMOVED CORROSION AT FS 409.00+5-409.00+121 AND RBL9 AT SEVERAL LOCATION IAW SRM 51-21-06. REPAIRED IAW SRM 53-00-43-001-001.

Part: ANGLE — CRACKED (BS 621) · airframe 24,719 hrs · 23,881 cycles

INSIDE AFT EQUIPMENT BAY, AFT PRESSURE BH 621 HAS A CLIP CRACKED AT LT SIDE STR 14LT. R & R CLIP ON AFT PRESSURE BULKHEAD 621 AT STRINGER 14L IAW SRM 51-40-11-00 AND SRM 51-42-21-00.

Part: ANGLE — CRACKED (BS 621) · airframe 24,719 hrs · 23,881 cycles

INSIDE AFT EQUIP BAY, AFT PRESSURE BH 621 HAS A CLIP CRACKED AT RT SIDE STR 14RT R & R CLIP ON AFT PRESSURE BULKHEAD 621 AT STRINGER 14R IAW SRM 51-40-11-00 AND SRM 51-42-21-00.

Part: BULKHEAD WEB — CRACKED · airframe 24,222 hrs · 23,375 cycles

DURING AFT PRESSURE BULKHEAD INSPECTION AWL 53-61-153 02, FOUND CRACK INDICATION RUNNING FROM BEHIND TOP OF AFT DOOR TRACK AT LBL 27.50 AND WL 126.0. CUT OUT CRACKED BULKHEAD WEB. FABRICATED REPAIR FILLER, & DOUBLERS AND INSTALLED IAW REO 601R-53-61-1541, REV. E. MAJOR REPAIR IAW GMM. 5-3.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,777 hrs · 22,930 cycles

CABIN EMERGENCY LIGHT NR 2 IN CEILING INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-16. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,124 hrs · 22,288 cycles

FLOOD LIGHT AT PAX DOOR INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-51-19. OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,124 hrs · 22,288 cycles

BOTH WARDROBE EMERGENCY EXIT LIGHTS INOPERATIVE. R & R NR 2 EMERGENCY LIGHT CHARGER IAW AMM 33-51-04.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,695 hrs · 21,863 cycles

FWD WARDROBE EMERGENCY EXIT FLOOR LIGHT INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-51-10. OPS CHECKED GOOD.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 22,518 hrs · 21,686 cycles

PAX DOOR INNER HANDLE CRACKED. R & R DAMAGED, PAX DOOR INNER HANDLE WITH NEW PN 600-31887-15 IAW AMM 52-11-25. MAJOR REPAIR IAW GMM 5-3.

Part: DIODE — FAILED (THRUST REVERSER) · airframe 22,531 hrs · 21,697 cycles

RECEIVED RT THRUST REVERSE UNLOCK MESSAGE IN FLIGHT. COMPLIED WITH QRH, AFTER SHUTTING DOWN RT ENGINE, ACFT LANDED. R & R DIODE IN JB-4 IAW 20-18-10. OPS TEST OF RT ENGINE THRUST REVERSER CHECKED GOOD IAW AMM 71-00-00.

Part: PDU — UNSERVICEABLE (THRUST REVERSER) · airframe 22,505 hrs · 21,669 cycles

RIGHT THRUST REVERSER UNLOCKED IN FLIGHT, DIVERTED, COMPLIED WITH QRH. EMERGENCY DECLARED. R & R THRUST REVERSER PDU IAW AMM 78-32-03 AIPC REF 78-32-03, ITEM 5. NO FURTHER DEFECTS NOTED AT THIS TIME, ACFT RETURNED TO SERVICE.

Part: SKIN — DENTED (BS 250-265) · airframe 22,226 hrs · 21,376 cycles

DENT/GOUGE BETWEEN BS 250 AND 265 S21L. BLENDED GOUGE WITHIN DENT IAW SRM 51-12-00. DAMAGE FOUND TO BE OUT OF LIMITS REF SRM 53-00-31. REPAIRED IAW REO 601R-53-11-2576.

Part: DOOR — LACK OF LUBE (SERVICE) · airframe 21,033 hrs · 20,133 cycles

SERVICE DOOR HARD TO OPEN AND CLOSE. CLEANED AND LUBED SERVICE DOOR. OPS CHECKED SERVICE DOOR GOOD IAW AMM 52-41-07. ACFT OK FOR SERVICE.

Part: SKIN — CORRODED (CENTER WING) · airframe 20,992 hrs · 20,088 cycles

CENTER WING TANK CUTOUT, 510BB, HAS AREAS OF CORROSION ON OTBD EDGE. REPAIRED IAW REO 601R-57-21-030 AND SRM 51-21-06.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 20,992 hrs · 20,088 cycles

ANGLE FROM HINGE SIDE OF ASD FOUND TO BE CORRODED. R & R ANGLE IAW SRM 51-42-06.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 20,784 hrs · 19,869 cycles

F/A FLASHLIGHT INOPERATIVE. R & R F/A FLASHLIGHT IAW AMM 25-60-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,551 hrs · 19,615 cycles

EXTERNAL EMERGENCY LIGHT NR 7 AFT OF LT OVERWING EXIT INOPERATIVE. LAMPED EXTERNAL EMERGENCY LIGHT NR 7 AFT OF LT OVERWING EXIT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: SELECTOR VALVE — UNSERVICEABLE (MLG) · airframe 20,243 hrs · 19,285 cycles

AFTER TAKEOFF, GEAR DISGREE WARNING, COMPLIED WITH QRH AND RECEIVED THREE GREEN, RETURNED TO DEPARTURE, R & R MLG SELECTOR VALVE IAW AMM 32-32-10, OPS CHECK GOOD. SDR CLOSED.

Part: PROXIMITY SENSOR — OUT OF ADJUST (MLG) · airframe 20,228 hrs · 19,270 cycles

GEAR UP DISAGREE MESSAGE. GEAR DISAGREE WITH HANDLE IN UP POSITION. NOSE GEAR ICON RED, MAINS AMBER. FOLLOWED QRH AND EXTENDED GEAR VIA MANUAL RELEASE. MSGS WENT OUT WHEN MANUAL EXTENSION COMPLETE. LANDED WITHOUT INCIDENT. ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION. READJUSTED UPLOCK PROXIMITY SENSOR IAW AMM 32-61-05. OPS CHECK GOOD WITH 10 GEAR SWINGS. NO DEECTS NOTED. SDR CLOSED.

Part: LANDING GEAR — FAILED · airframe 20,228 hrs · 19,270 cycles

REPEAT WRITE UP, GEAR DISAGREE WARNING MESSAGE WITH GEAR HANDLE IN UP POSITION. NOSE GEAR ICON RED. MAINS REMAIN AMBER. COMPLIED WITH QRH AND EXTENDED GEAR WITH MANUAL RELEASE. MESSAGE WENT OUT WITH EXTENSION HANDLE STOWED. LANDED WITHOUT INCIDENT. ACFT RETURNED TO DEPARTURE AFTER T/O. EMERGENCY DECLARED. R & R NLG AND MLG PRIORITY VALVES. IAW AMM 32-33-15 AND 32-33-15. R & R NLG EXT/RET ACTUATOR, IAW AMM 32-33-01. BLED AIR FROM HYD SYS 3 IAW AMM 29-10-00. PERFORMED FUNCTIONAL TEST OF LANDING GEAR EXT/RET SYS IAW AMM 32-30-00. ALL OPS TESTS COMPLIED WITH SATISFACTORY. NO DEFECTS NOTED.

Part: ISOLATOR — BROKEN (BULKHEAD) · airframe 20,079 hrs · 19,093 cycles

ONE ISOLATOR BROKEN IN CARGO COMPATMENT AFT BULKHEAD LT SIDE BOTTOM. R & R 1 BROKEN ISOLATOR IN CARGO COMPATMENT AFT BULKHEAD LEFT SIDE BOTTOM IAW SRM 51-42-13.

Part: TORQUE LINK — BINDING (NLG) · airframe 19,901 hrs · 18,888 cycles

GEAR DISAGREE MESSAGE ON TAKEOFF. NOSE GEAR DID NOT RETRACT. COMPLIED WITH CHECKLIST. ALL GEAR DOWN AND LOCKED. LANDING GEAR RETRACTION SYSTEM. ENROUTE, DIVERTED DUE TO MX, EMERGENCY DECLARED. R & R UPPER AND LOWER TQ LINKS IAW AMM 32-21-10. ADJUSTED NLG UPLOCK IAW AMM 32-32-05 AND SERVICED NLG IAW AMM 12-12-32. OPS CHECKED GOOD.

Part: PRIORITY VALVE — MALFUNCTIONED (MLG) · airframe 19,889 hrs · 18,876 cycles

GEAR UP DISAGREE AFTER TAKEOFF NOSE GEAR REMAINED DOWN. PERFORMED MANUAL GEAR EXTENSION USING QRH. RETURNED TO DEPARTURE, EMERGENCY DECLARED. REPLACED PRIORITY VAVE IAW AMM 32-33-15. LEAK AND OPS CHECKED GOOD.

Part: OVERHEAT LOOP — FALSE ACTIVATION · airframe 19,529 hrs · 18,464 cycles

DURING CLIMB WITH NO ANTI-ICE ON , LEFT 14TH STAGE BLEED AIR DUCT WARNING , FOLLOWED QRH AND ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. R & R LOOP A59KW IAW AMM 36-21-04. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,863 hrs · 17,717 cycles

AFT CENTER CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED, OPS CHECKED GOOD IAW AMM 33-51-00.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 18,378 hrs · 17,174 cycles

FLAPS FAIL AT 20 DEGREES PRIOR TO LANDING. COMPLIED WITH QRH. LANDED WITHOUT INCIDENT (EMERGENCY DECLARED AS A PRECAUTION) R & R BRAKE POSITION SENSOR IAW AMM 27-51-10, AIC REF 27-51-00 ITEM 10G. R & R SKEW DETECTION UNIT IAW AMM 27-51-15, REF 27-51-15 ITEM 5. R & R RT NR 4 FLEX DRIVE SHAFT IAW AMM 27-53-10, REF 27-53-00 ITEM 20C. RIG AND OPS CHECKED GOOD. COMPLIED WITH EC/TC AD 2009-06-12 ON W/O 220906.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,071 hrs · 16,825 cycles

NR 8 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED NR 8 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 18,007 hrs · 16,750 cycles

EMERGENCY LIGHT AT FLOOR ENTRANCE DAMAGED. R & R EMERGENCY LIGHT IAW AMM 33-51-19. OPS CHECK GOOD PLACARD REMOVED.

Part: LIGHT — DAMAGED (CABIN) · airframe 17,902 hrs · 16,640 cycles

EMERGENCY LIGHT AT FLOOR AT PASSENGER DOOR ENTRANCE DAMAGED. (OPEN)

Part: FRAME — CRACKED (BS 193) · airframe 17,735 hrs · 16,464 cycles

FOUND FRAME CRACKED AT INTERSECTION OF FS 193.00 FRAME ABOVE STRINGER 16L. CUT AWAY DAMAGE FLOOR, FABRICATED FILLER, DOUBLER, AND ANGLE. COMPLIED WITH NDT IAW GREO 601R-53-11-081, NDTM 51-20-00 PART 1 AND NDTM 53-00-096, PART 6, NO DEFECTS NOTED. INSTALLED NEW REPAIR PARTS REF REO 601R-53-11-081 AND REO 601R-53-11-2136.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 17,444 hrs · 16,129 cycles

REFER TO PREVIOUS DMIL NR 628548-2 CEILING LEVEL EMERGENCY FLOOD LIGHT AT ROW 2 IS OUT. R & R ROW NR 2 CEILING LEVEL EMERGENCY FLOOD LIGHT BULB IAW AMM 33-51-16. OPS CHECK GOOD DMIL NR 628548-2 CLEARED AND PLACARD REMOVED. (CLOSED)

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 17,440 hrs · 16,124 cycles

THE CEILING LEVEL EMERGENCY FLOODLIGHT AT ROW 2 IS INOP. ( CABIN EMERGENCY LIGHTS: CEILING LEVEL EMERGENCY FLOODLIGHTS ) R & R ROW NR 2 CEILING LEVEL EMERGENCY FLOOD LIGHT BULB IAW AMM 33-51-16. OPS CHECK GOOD DMIL NR 628548-2 CLEARED AND PLACARD REMOVED.

Part: HANDLE — BINDING (SERVICE DOOR) · airframe 17,307 hrs · 15,980 cycles

SERVICE DOOR WILL NOT OPEN FROM OUTSIDE OUTER HANDLE JAMMED. REMOVED AND REPLACED SERVICE DOOR OUTER HANDLE IAW AMM 52-41-03, OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 17,001 hrs · 15,616 cycles

THE SECOND OVERHEAD EMERGENCY LIGHT IS INOP. REPLACED THE SECOND OVERHEAD EMERGENCY LIGHT BULB. OPS CHECK GOOD. DONE IAW THE AMM CHAPTER 33-51-16.

Part: CONNECTOR — MISINSTALLED (EMERGENCY LIGHT) · airframe 16,341 hrs · 14,836 cycles

EMERGENCY FLOOD LIGHT ON SIDE OF WARDROBE INOP. TROUBLESHOT, FOUND ELECT CONNECTORS FOR FLOOR LEVEL FLOODLIGHT (DS9LY) AND FLOOR PROX EXIT SIGN PASS DOOR (DS10LY) SWAPPED. RECONNECTED CONNECTORS IN CORRECT POSITIONS IAW AMM TASK 33-51-19-400-801 AND WDM 33-51-00. OPS TEST OF THE EMERG LIGHTS GOOD IAW AMM TASK 33-51-00-710-801.

Part: SKIN — CORRODED (BS 574 S24-27R) · airframe 16,324 hrs · 14,816 cycles

FS 574 RT SIDE BETWEEN STR 27R & 24R HAS MINOR CORROSION ON EXTERNAL SKIN WHERE BELLY FAIRING MEETS SKIN ON STR 26R JUST AFT OF BELLY FAIRING. BLENDED OUT CORROSION IAW REO 601R-53-61-3785 STEP 1. PERFORMED EDDY CURRENT IAW REO 601R-53-61-3785 STEP 2. NO INDICATIONS NOTED. COMPLIED WITH REO 601R-53-61-3785 STEPS 3, 4 AND 5. C/W NOTES 1, 2, 4, 8 & 9 IAW REO 601R-53-61-3785. COMPLIED WITH (HFEC) OF REPAIR CUTOUT IAW REO 601R-53-61-3785 REV A, SHEET 3, NOTE 3 & NDTM PT 1 51-20-06. NO INDICATIONS NOTED. C/W REO 601R-53-61-3785 STEPS 5, 6, 7, 10, 11, 12, 13. REO 601R-53-61-3785 REV A HAS BEEN ACCOMPLISHED. ALL RII'S HAVE BEEN ACCOMPLISHED IAW GMM 5-2 PRIOR TO A/C RETURN TO SERVICE.

Part: SUPPORT — CRACKED (BS 484) · airframe 16,324 hrs · 14,816 cycles

CONTINUATION OF MWC 335 SUPPORT CLIP CRACKED AT UPPER OTBD FASTENER AREA AT FS 484 LBL 2.0 AND CROSS SUPPORT BEAM PREVIOUSLY REPAIRED. EC/TC REQUIRED. REPAIR TO THE INTERCOSTALS AT FS 484 BETWEEN BL 27.00 AND BL 36.00 IS COMPLETED IAW REO 601R-53-41-059, AND MEETS WITH ALL THEIR REQUIREMENTS. (CLOSED)

Part: SILL — CORRODED · airframe 16,324 hrs · 14,816 cycles

PAX DOOR LOWER SILL ANGLE HAS MAJOR CORROSION. REMOVED PASSSENGER DOOR LOWER SILL ANGLE AND LOCATED FASTENER HOLES IN NEW SILL ANGLE IAW SRM 51-42-06, 51-42-13, 51-42-21 AND 51-40-11. INSTALLED NEW SILL ANGLE IAW SRM 51-42-06, 51-42-13, 51-42-21, 51-40-11.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 16,324 hrs · 14,816 cycles

FWD FLOOR ANGLE AT FS 280 IS CORRODED AND REQUIRES REPLACEMENT. REMOVED AND REPLACED FWD FLOOR ANGLE AT STA 280 IAW SRM 51-42-06 AND 51-42-21.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 16,324 hrs · 14,816 cycles

CARGO SEAT TRACK CORRODED AT FS 559, RBL 27. REMOVED SEAT TRACKS AND FITTING IAW AMM 51-41-02. RECEIVED SERVICEABLE SEAT TRACK & FITTING FROM STORES, LOCATED AND INSTALLED IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 16,324 hrs · 14,816 cycles

CARGO BAY SEAT TRACK CORRODED AT FS 559+80 TO FS 559+112, LBL 9, 2EA. REMOVED SEAT TRACKS IAW SRM 51-41-02. RECEIVED SERVICEABLE SEAT TRACKS FROM STORES. LOCATED AND INSTALLED SEAT TRACKS IAW SRM 51-41-02.

Part: WEB — CRACKED (BS 280) · airframe 16,324 hrs · 14,816 cycles

FS 280, WEB CRACKED BELOW FLOOR OTBD OF RBL 9 AND OTBD LBL 9, CORRODED AT FLOOR BETWEEN RBL 9 AND LBL 9. C/W EC/TC REO 601R-53-11-926 IAW REO 601R-53-11-926 REV B.

Part: PLACARD — WORN (PAX DOOR) · airframe 16,324 hrs · 14,816 cycles

PAX DOOR STEP "EXIT" PLACARD ON NR3 STEP FROM BOTTOM IS WORN. REMOVED PAX DOOR STEP "EXIT" IAW AMM 11-30-00-000-801. INSTALLED NEW EXIT PLACARD ON PAX DOOR IAW AMM 11-30-00-400-801.

Part: WEB — CORRODED (BS 409) · airframe 16,324 hrs · 14,816 cycles

SUPPORT WEB AT FWD UPPER CORNER AT OTBD SIDE OF LBL 9 AND F.S. 409+16 APPEARS TO BE CRACKED. PERFORMED EDDY CURRENT INSPECTION OF LBL 9.0 FS 409.0+16 O/B WEB SUSPECTED AREA IAW NDTM PART 1, 51-20-06. NO INDICATONS NOTED AT THIS TIME. TOUCHED UP SUPPORT WEB AT FWD UPPER CORNER AT OTBD SIDE OF LBL 9.0 & FS 409.0+16 IAW SRM 51-22-01.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 16,324 hrs · 14,816 cycles

CARGO BAY SEAT TRACK CORRODED AT FS 559+80 TO FS 559+112, RBL 9, 2EA.

Part: ANGLE — CRACKED (BS 484) · airframe 16,324 hrs · 14,816 cycles

SUPPORT CLIP CRACKED AT UPPER, OTBD FASTENER AREA AT FS 484, LBL 36 AND CROSS SUPPORT BEAM, PREVIOUSLY REPAIRED. STEPS 1 & 2 HAVE BEEN PREVIOUSLY REPAIRED AND FOUND TO BE IN SERVICEABLE CONDITION IAW REO 601R-53-41-059. CUT EDGE REQUIRE NDI. COMPLIED WITH STEP REO 601R-53-41-059B PERFORMED EDDY CURRINT OF LBL 36, FS 484 IAW NDTM 51-20-06. NO INDICATONS NOTED AT THIS TIME. FABRICATED REPAIR ANGLE IAW STEP 5/13/6 OF REO 601R-53-41-059. ANGLE REQUIRES NDI. COMPLIED WITH STEP 13 OF REO 601R-53-1-059B. PERFORMED EDDY CURRENT OF FABRICATED ANGLE IAW NDTM 51-20-06. NO INDICATIONS NOTED AT THIS TIME. REQUIRES ANGLE TO BE PAINTED AND INSTALLED. REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE IAW STEPS 8-14 OF REO 601R-53-41-059. EC/TC REQUIRED.

Part: PLACARD — DETERIORATED (CABIN) · airframe 16,324 hrs · 14,816 cycles

ALL 4 EXTERNAL PLACARDS ON THE CREW ESCAPE HATCH ARE WORN. APPLIED NEW SILKSCREENS ON EXTERNAL CREW ESCAPE HATCH IAW MM 11-10-03-400-801. (CLOSED)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 16,324 hrs · 14,816 cycles

SUPPORT CLIPS AT FS 280, RBL 9.0 ARE CRACKED. REPLACEMENT OF SUPPORT CLIP AT FS 280, RBL 9.0 IAW REO 601R-53-11-926, REV B.

Part: BULKHEAD — CRACKED (BS 559) · airframe 16,324 hrs · 14,816 cycles

FOUND FS 559 LT CAP ANGLE AT LBL 18.0 HAS INDICATION NOTED APPROX .2" IN LENGTH 80 PERCENT FSH AND FS 559 RT BULKHEAD WEB AT WL 59.10 INBD OF RBL 18.0 HAS INDICATION NOTED APPROX .2" IN LENGTH 60 PERCENT FSH, FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260. ASA RII COMPLIED WITH: 5300007.

Part: FRAME — CORRODED (BS 349) · airframe 16,324 hrs · 14,816 cycles

THERE IS AN AREA OF LIGHT SURFACE CORROSION ON AFT FACE OF FS 349 JUST LT OF 6 O'CLOCK POSITION INTERNALLY. UPON ASSESSING THE DAMAGE, FOUND THE CORROSION ON AFT FACE OF FS 349.00 BOTTOM FRAME SECTION TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-00, FIG 102 (SHEET 2). INSTALLED NEW SERVICEABLE FRAME SECTION AT FS 349 IAW SRM 51-42-06, 51-40-11, 51-42-21, 51-42-13, 51-25-00, AND 51-23-00. PAINTED EXTERIOR ROW OF RIVETS AT FS349 IAW SRM 51-25-01.

Part: PLACARD — WORN (ESCAPE HATCH) · airframe 16,324 hrs · 14,816 cycles

ALL PLACARDS ON EXTERIOR CREW ESCAPE HATCH NEED REPLACED.

Part: ANGLE — CRACKED (BS 621-625) · airframe 16,324 hrs · 14,816 cycles

AFT EQUIPMENT COMPARTMENT FS 621.00 TO 625.00 OBLIQUE ANGLES LT AND RT SIDES ARE CRACKED .5" LONG IN AFT RADIUS. REMOVED CRACKED OBLIQUE ANGLES ON AFT EQUIPMENT COMPARTMENT AT LT AND RT SIDES OF FS 621 TO 625 IAW SRM 51-42-21. INSTALLED NEW SERVICEABLE OBLIQUE ANGLES ON AFT EQUIPMENT COMPARTMENT LT AND RT SIDES OF FS 621 TO 625 IAW SRM 51-40-11 AND 51-42-21.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,160 hrs · 14,625 cycles

CEILING EMERGENCY LIGHT 2ND FROM FRONT IS INOP. RELAMPED CEILING EMERGENCY LIGHT 2ND FROM FRONT IAW AMM 33-51-16. OPS CHECK GOOD. RELAMPED CEILING EMERGENCY LIGHT 2ND FROM FRONT IAW AMM 33-51-16. OPS CHECK GOOD. (CLOSED)

Part: HANDLE — FAILED (SERVICE DOOR) · airframe 15,777 hrs · 14,170 cycles

UNABLE TO OPEN SERVICE DOOR FROM THE OUTSIDE. INSIDE HANDLE SPINS ON SHAFT. OPENED AND CLOSED DOOR SEVERAL TIMES OPS CK GOOD AMM 52-40-00. (SDR CLOSED)

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 15,358 hrs · 13,692 cycles

FLAPS FAIL AT 0 IN FLIGHT, EMERGENCY DECLARED. C/W TROUBLE SHOOTING FOR FLAP FAILURES IAW AD 2009-06-12 ON WO 147802. A/C RETURN TO SERVICE. MCO CLEARED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,067 hrs · 13,376 cycles

AFT EXTERNAL EMERGENCY LIGHT INOP ON LT SIDE.

Part: DOOR — STIFF (MAIN PAX) · airframe 14,640 hrs · 12,911 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN.

Part: DOOR — BINDS (SERVICE DOOR) · airframe 14,408 hrs · 12,655 cycles

CATERING REPORTS DIFFICULTY OPENING SERVICE DOOR.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,663 hrs · 10,940 cycles

REAR PRESSURE BULKHEAD WEB THAT SURROUNDS LINTEL ATTACHMENT FITTING HAS A INDICATION NOTED APPROX .1 INCH IN LENGTH 60 PERCENT FULL SCREEN HEIGHT FAILED NDT INSPECTION. REPAIRED LINTEL FITTING IAW REO 601R-53-61-1230 AND REO 601R-53-61-1230.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 12,663 hrs · 10,940 cycles

FORWARD PRESSURE BULKHEAD AT FS 202.75 SHOWS EVIDENCE OF A CRACK .750 INCH LONG FROM TOP OF HOLE FOR PARKING BRAKE CABLE. PERFORMED EDDY CURRENT INSPECTION, INDICATION NOTED APPROX .5 INCH, FAILED NDT. LT FS 202.75 BULKHEAD WEB REQUIRES REPAIR. REMOVED PARKING BRAKE CABLE FROM BULKHEAD. REPAIRED CRACKED BULKHEAD. APPLIED CORROSION INHIBITING COMPOUND & INSTALLED PARKING BRAKE CABLE. ADJUSTED CABLE. OPS TEST OF THE PARKING BRAKE SYS GOOD. C/W ASA ECTC EO 600-53-217CW.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,663 hrs · 10,940 cycles

RIGHT FS 484 FLOOR SUPPORT INTERCOSTAL ANGLE CRACKED 1 INCH. REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE WITH NEW IAW REO 610R-53-41-059 REV A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,663 hrs · 10,940 cycles

INBOARD AND OUTBOARD FLOOR SUPPORT CLIPS CRACKED AT FS 280, LBL 9.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,663 hrs · 10,940 cycles

OUTBOARD FLOOR SUPPORT CLIP CRACKED AT FS 280, RBL 9.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 12,663 hrs · 10,940 cycles

CARGO DOOR SUPPORT BEAM LOWER ANGLE CRACKED .3 INCH LONG AT FS 621 BULKHEAD.

Part: TRACK — CRACKED (CARGO DOOR) · airframe 12,663 hrs · 10,940 cycles

CARGO DOOR FWD TRACK U-CHANNEL CRACKED .1 INCH LONG AT BOTTOM OF TRACK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 12,507 hrs · 10,791 cycles

RT AFT EXTERIOR EMER LIGHT INOP. RELAMPED RT AFT EXTERIOR EMER LIGHT IAW CRJ 200 AMM 35-51-21.

Part: LIGHT — INOPERATIVE (ROW 4C) · airframe 12,495 hrs · 10,780 cycles

EMERGENCY LIGHTING AT ROW 4C INOP R & R EMERGENCY LIGHTING STRIP AT 4C. IAW AMM 33-51-01. OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,626 hrs · 10,052 cycles

GALLEY LOWER EMERGENCY LIGHT HAS SEVERAL INOP BULBS.

Part: LIGHT — INOPERATIVE (ROW 4-9) · airframe 11,179 hrs · 9,676 cycles

FOUND EMERGENCY FLOOR TRACK LIGHTING INOP FROM ROW 4 TO 9.

Part: WARNING SYSTEM — INTERMITTENT (COCKPIT) · airframe 10,898 hrs · 9,448 cycles

ON DEPARTURE OUT OF ATL, RECEIVED A "RENG MOIL PRESS" INTERMITTENTLY. COMPLIED WITH QRH AND EVENTUALLY SHUT DOWN THE RIGHT ENG, A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. EMERGENCY EQUIPMENT ON STANDBY.

Part: LIGHT — INOPERATIVE (ROWS6CD-12CD) · airframe 10,741 hrs · 9,306 cycles

CABIN FLOOR EMERGENCY LIGHTS AT ROWS 6CD THRU 12CD ARE INOP.

Part: SIGN — INOPERATIVE (PAX AIRSTAIRS) · airframe 10,316 hrs · 8,963 cycles

EXIT SIGN ON PAX STAIRS NOT ILLUMINATING.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 9,211 hrs · 7,818 cycles

LEFT SIDE 640 DOUBLER SUSPECT CRACKED. FLT 4538 CX.

Part: STRIP — CRACKED (CABIN) · airframe 8,613 hrs · 7,319 cycles

EMERGENCY LIGHT STRIP ON FLOOR IS CRACKED. CRACK IS LOCATED AT (APPROX) ROW 8.

Part: LIGHT — BROKEN (CABIN) · airframe 7,868 hrs · 6,682 cycles

EMERGENCY FLOOR LIGHT STRIP HAS BROKEN LAMP.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 7,868 hrs · 6,682 cycles

FOUND FS 280 CLIP CRACKED, I/B OF RBL 9.0.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 7,868 hrs · 6,682 cycles

NR 2 AT O/B RIB HALF (601R23030) FITTING CRACKED (LT HORIZONTAL STAB IN PCU PANEL).

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,868 hrs · 6,682 cycles

FOUND AFT DRAG ANGLE ON PAX DOOR IS CRACKED. (MARKED)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 7,868 hrs · 6,682 cycles

RANRC 122. LT FLOOR SUPPORT ANGLE AT FS621 CRACKED.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 7,868 hrs · 6,682 cycles

RANRC 123. RT FLOOR SUPPORT ANGLE AT FS621 CRACKED.

Part: LIGHT — DAMAGED (CABIN)

DURING A HANGAR INSPECTION, THE EMERGENCY FLOOR TRACK LIGHT, AT ROW 9 AND AFT END CAP, WAS FOUND TO BE DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR TRACK LIGHT AT ROW 9 AND AFT END CAP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: FLASHLIGHT — INOPERATIVE (CABIN)

DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANTS FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLIGHT ATTENDANTS FLASHLIGHT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

FLT 4164 - DURING A MAINTENANCE CHECK IN MCN, THE RIGHT FORWARD EXTERNAL OVERWING EMERGENCY LIGHT AND THE CENTER AISLE EMERGENCY LIGHT AT ROW 9 WERE FOUND TO BE INOPERATIVE. MAINTENANCE WILL REMOVE AND REPLACE THE NR 2 POWER SUPPLY (BATTERY PACK), AND THE RIGHT FORWARD EXTERNAL OVERWING EMERGENCY LIGHT ASSEMBLY. (M)