N762SK

Part: STRINGER — CORRODED (ZONE 100) · airframe 47,552 hrs · 31,666 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA60500-670-53-61-1695 N762SK MXCODEID52397-PR - STRINGER 23L HAS CORROSION FROM FS1000.00 TO FS1031.00. PERFORMED A REO REPAIR. REF REO REO 670-53-61-1695 REV-- DATED: 2020-07-14. THIS REPAIR IS VALID FOR 8000 FLIGHT HOURS FROM THE TIME OF REPAIR., PART NUMBER: - , SERIAL NUMBER: 10226, POSITION: (C-CHECK RO 7/12/2024) PERFORMED REPAIR AT STR 23L FROM FS 969 TO FS 1031.00 IAW CRJ 700 SRM 53-00-03,SRM 51-42-06,AMM 53-62-33,SRM 51-42-21,SRM 51-21-11,SRM 51-25-06,AMM 20-70-00,SRM 51-25-16PERFORMED NDT ET INSPECTION BY BARON NDT,LLC FAA CRS# 5NDR545D REPORT# S061024-9 P.O# 172296 DATE OF INSPECTION 10-JUN-2024,SEE REPORT FOR DETAILSCAL TOOL:ROUGHNESS TESTER ID:AV-6062 CAL DUE: AUG-2024

Part: WINDSHIELD — CRACKED · airframe 45,798 hrs · 30,148 cycles

FOS FRONT WINDSHIELD HAS A CRACK, TOP RIGHT CORNER (FILED CLOSED) REMOVED AND REPLACED RH FO WINDSHIELD IAW CRJ 700 AMM 56-11-01. ALSO SEE ATTACHED TASK CARD FOR WORK PERFORMED. OPERATIONAL CHECK OF HEAT AND LEAK CHECKS GOOD. PLEASE REFERENCE AML 1128513 PLEASE REFERENCE AML 1128522

Part: NONE — CRACKED · airframe 44,645 hrs · 29,158 cycles

TRANSFER FROM EAML 952061 : CAPTAINS SIDE WINDOW CRACKED ALL THE WAY ACROSS (FLIGHT #3099 FILED CLOSED) REMOVED AND REPLACED CAPTAIN SIDE WINDOW IAW TASK CARD 56-220-1000-SKY SEE CP 25191983 FOR LEAK CHECK. / SIDE WINDOW TEMPERATURE CONTROLLER OPS CHECK GOOD AT THIS TIME.

Part: FRAME — CORRODED (BS 364) · airframe 40,384 hrs · 26,020 cycles

FS364.00 FRAME IS CORRODED ON LOWER FLANGE AT STRINGER 27. CUT AWAY DAMAGE FROM FS364 FRAME SECTION FROM STR24L - STR24R, FABRICATED REPAIR PARTS AND INSTALLED NEW FRAME IAW SRM, DRAWING.

Part: HINGE FITTING — NO TEST (NLG DOOR) · airframe 40,384 hrs · 26,020 cycles

NLG AFT DOOR - FAILS CLEARANCE CHECK - EXCESSIVE GAP AT FWD RH EDGE. (C-CHECK) RO 7/25/2020 REMOVED AND INSTALLED NEW LH AND RH NLG AFT DOOR HINGE FITTINGS. REF BOMBARDIER DWG AND CRJ700 SRM. CLEARANCE AND LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 40,384 hrs · 26,020 cycles

FS280 LOWER BULKHEAD STIFFENER AT RBL 26 FOUND CRACKED (C-CHECK) RO 7/25/2020 REPLACED RBL26 LOWER BULKHEAD STIFFENER AT FS280.00 REF CRJ-700 SRM AND BOMBARDIER DWG. COMPLIED WITH SKYWEST TASKCARD.

Part: BEAM — CRACKED (PAX DOOR) · airframe 40,384 hrs · 26,020 cycles

FOUND AFT BEAM OF PAX DOOR CRACKED. REMOVED AND REPLACED AFT BEAM ASSY IAW SRM.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 40,384 hrs · 26,020 cycles

UPON INSTALLATION OF AFT DRAG ANGLE OF PAX DOOR, FOUND TO BE CRACKED AT PREVIOUS REPAIR LOCATION. REMOVED AND REPLACED AFT DRAG ANGLE IAW SRM.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 40,384 hrs · 26,020 cycles

COMPLETE REO REPAIR FOR CORROSION ON LH FS280.00 FLOOR BEAM. COMPLIED WITH REO REPAIR OF LH FS280 FLOR BEAM COMPLIED WITH SKYWEST TASK CARD

Part: FLOORBEAM — CRACKED (BS 280) · airframe 40,384 hrs · 26,020 cycles

LH FS280 FLOOR BEAM LBL12 OUTBOARD ANGLE CRACKED (C-CHECK) RO 7/25/2020 INSTALLED NEW L/H LBL 12 ANGLE COMMON TO F.S. 280.00 REF: CRJ-700 S.R.M., DWG. COMPLIED WITH SKYWEST TASK CARD

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 40,384 hrs · 26,020 cycles

PAX DOOR AFT WEB STIFFENER FOUND TO BE CRACKED @ MID LOCATION . REMOVED AND REPLACED AFT WEB STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 40,384 hrs · 26,020 cycles

UPON ACCESSING PAX DOOR FWD WEB FOUND STIFFENER P/N 601R317742-1 TO BE CRACKED AT FASTENER HOLE. RECEIVED NEW PAX DOOR FWD WEB STIFFENER AND INSTALLED ON CAMP 21112197 JOB 710226124 OP 21.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 40,384 hrs · 26,020 cycles

F.S.280.00 FLOOR BEAM HAS CORROSION BETWEEN RBL9 AND LBL9 AT SEVERAL SPOTS. REPLACED RT FLOOR CROSSBEAM IAW SRM, AND DWG.

Part: DOOR SILL — CORRODED · airframe 40,384 hrs · 26,020 cycles

SERVICE DOOR LOWER SILL P/N: SH670-31980-13 FOUND CORRODED. BLENDED AND RESTORED CORRODED SERVICE DOOR LOWER SILL IAW REO. ALL STEPS OF REO COMPLIED WITH IN THEIR ENTIRETY.

Part: WEB — CORRODED (FLOOR) · airframe 40,384 hrs · 26,020 cycles

SERVICE DOOR SECOND FROM FWD PROTECTOR FLOOR WEB FOUND CORRODED. REMOVED AND REPLACED CORRODED SERVICE DOOR SECOND FROM FWD PROTECTOR FLOOR WEB WITH NEW (P/N SH670-32040-3) WITH NEW HARDWARE, REF DWG# SH670-31950 REV Y AND SRM.

Part: WEB — CORRODED (FLOOR) · airframe 40,384 hrs · 26,020 cycles

SERVICE DOOR FOURTH FROM FWD PROTECTOR FLOOR WEB FOUND CORRODED. REMOVED AND REPLACED CORRODED SERVICE DOOR FORTH FROM FWD PROTECTOR FLOOR WEB WITH NEW (P/N SH670-32040-4) WITH NEW HARDWARE, IAW DWG AND SRM.

Part: WEB — CORRODED · airframe 40,384 hrs · 26,020 cycles

SERVICE DOOR FIRST FROM FWD PROTECTOR FLOOR WEB FOUND CORRODED. REMOVED AND REPLACED CORRODED SERVICE DOOR FIRST FROM FWD PROTECTOR FLOOR WEB WITH NEW (P/N SH670-32040-3) WITH NEW HARDWARE, REF DWG# SH670-31950 REV Y AND CRJ700 SRM 51-42-21-001-001 A01. SEE CONTINUATION CARD FOR FURTHER DETAILS. C/W 51-900-1002-SKY

Part: WEB — CORRODED (FLOOR) · airframe 40,384 hrs · 26,020 cycles

SERVICE DOOR THIRD FROM FWD PROTECTOR FLOOR WEB FOUND CORRODED. REMOVED AND REPLACED CORRODED SERVICE DOOR THIRD FROM FWD PROTECTOR FLOOR WEB WITH NEW (P/N SH670-32040-4) WITH NEW HARDWARE, IAW DWG AND SRM.

Part: FITTING — CORRODED (PAX DOOR) · airframe 40,384 hrs · 26,020 cycles

PAX DOOR AFT CLOSING FITTING FOUND CORRODED. (C-CHECK) RO 7/25/2020 REPLACED PAX DOOR AFT CLOSING FITTING. REF: CRJ700 SRM COMPLIED WITH SKYWEST TASKCARD.

Part: HINGE — DAMAGED (PAX DOOR) · airframe 40,384 hrs · 26,020 cycles

PAX DOOR HINGE ( FUSELAGE SIDE ) NEED REPLACEMENT DUE TO ELONGATED LUG HOLES. SEE JOB 710226121 OP 181 FOR DAMAGE EVAL. (C-CHECK) RO 7/25/2020 COMPLIED WITH REPLACEMENT OF THE PAX DOOR PIANO HINGE FUSELAGE SIDE REF CRJ-700 SRM AND BOMBARDIER DWG NO. COMPLIED WITH SKYWEST TASKCARD. PRESSURE CHECK GOOD.

Part: SEAT TRACK — CORRODED (BS 785-868) · airframe 40,384 hrs · 26,020 cycles

RIGHT SIDE SEAT TRACK JUST AFT OF THE EMERGENCY DOOR, BS 785-868, HAD CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW AMM.

Part: STRINGER — CORRODED (BS 1015-1031) · airframe 40,384 hrs · 26,020 cycles

STRINGER 26R HAD CORROSION BETWEEN BS 1015 TO 1031. BLENDED & EVALUATED THE STRINGER. FOUND OUT OF LIMITS IAW SRM. PERFORMED A REPAIR OF THE STRINGER IAW SRM. ALL CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 349-477) · airframe 40,384 hrs · 26,020 cycles

THE SEAT TRACK AT RBL 9, BS 349 - 477 HAD CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (BS 677-761) · airframe 40,384 hrs · 26,020 cycles

RIGHT SEAT TRACK JUST FWD OF THE EMERGENCY DOOR, BS 677-761, HAD CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 40,384 hrs · 26,020 cycles

LEFT SEAT TRACK FWD OF THE EMERGENCY DOOR HAD CORROSION. REMOVED AND INSTALLED A NEW SEAT TRCK IAW AMM.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 40,384 hrs · 26,020 cycles

RIGHTSEAT TRACK, BS 581 TO 677 HAD CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (BS 394-477) · airframe 40,384 hrs · 26,020 cycles

THE SEAT TRACK AT LBL 27, BS 394 TO 477 HAD CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW AMM.

Part: FRAME — CORRODED (BS 1015) · airframe 40,384 hrs · 26,020 cycles

THE FRAME AT FS1015.00 FROM STRINGER 26L TO 26R HAS CORROSION. THE FRAME WAS FOUND OUT OF LIMITS, NO DAMAGE ALLOWED TO ATTACHING FLANGE IAW SRM (ORIGINAL: .050) - (REMAINING: .047) - (LOSS: .003). REMOVED AND REPLACED THE FRAME IAW SRM AND DRAWING.

Part: STRINGER — CORRODED (BS 1000-1031) · airframe 40,384 hrs · 26,020 cycles

STRINGER 23L HAD CORROSION BETWEEN BS 1000 TO 1031. PERFORMED AN REO REPAIR. ALL CHECKED GOOD.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 40,384 hrs · 26,020 cycles

BS 349 - 364 INTERCOSTAL AT STRINGER 26R WAS CORRODED ON THE AFT BOTTOM EDGE. REMOVED, REPLACED AND INSTALLED A NEW ATTACHMENT ANGLE ON THE INTERCOSTAL IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (BS 785-868) · airframe 40,384 hrs · 26,020 cycles

LEFT SIDE SEAT TRACK JUST AFT OF THE EMERGENCY DOOR BS 785-868, HAD CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACKS IAW AMM.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 40,384 hrs · 26,020 cycles

BS 349 - 364 INTERCOSTAL ON STRINGER 27L WAS CORRODED AFT INNER SIDE. THE INERCOSTAL WAS FOUND OUT OF LIMITS, NO DAMAGE ALLOWED TO THE ATTACHING FLANGE OF THE INTERCOSTAL IAW SRM. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM, AND DRAWING.

Part: FRAME — CORRODED (BS 1000) · airframe 40,384 hrs · 26,020 cycles

THE FRAME AT BS 1000 AT STRINGER 21L HAD CORROSION. BLENDED THE CORROSION AND FOUND OUT OF LIMITS IAW SRM. (ORIGINAL: .050) - (REMAINING: .037) - (LOSS: .013). CUT AWAY DAMAGE, FABRICATED AND INSTALLED NEW REPAIR ANGLE FLANGE IAW REO, AND SRM.

Part: PLATE — CORRODED (BS 280) · airframe 40,384 hrs · 26,020 cycles

* THE FS280.00 SACRIFICIAL PLATE FROM LBL9.00 TO RBL 9.00 HAS CORROSION. INSTALLED NEW SACRIFICIAL PLATE OF FS280. IAW SRM, AND DWG.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 40,384 hrs · 26,020 cycles

LEFT SEAT TRACK, BS 581 TO 677 HAD CORROSION. REMOVED, AND INSTALLED A NEW SEAT TRACK IAW AMM.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 40,384 hrs · 26,020 cycles

BS 349 - 364 INTERCOSTAL ON STRINGER 27R WAS CORRODED AROUND FASTENERS. THE INTERCOSTAL WAS FOUND OUT OF LIMITS, DUE TO NO ALLOWABLE DAMAGE TO THE ATTACHED FLANGE IAW SRM. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM, AND DRAWING. RESTORED ACCESS AND FINISH.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 40,384 hrs · 26,020 cycles

PAX DOOR MID CAP ANGLE HAS CORROSION AROUND SCREW HOLES. REMOVED AND REPLACED CORRODED PAX DOOR MID CAP ANGLE WITH NEW IAW DWG AND SRM.

Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 40,384 hrs · 26,020 cycles

SEAT TRACK, BS 485 TO 565 HAD CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK RBL9 IAW AMM.

Part: FITTING — CORRODED (BS 310) · airframe 40,384 hrs · 26,020 cycles

THE WARDROBE FITTING AT BS 310 BETWEEN LT SILL AND LBL 27 HAD CORROSION. INSTALLED NEW WARDROBE FITTING IAW SRM, AND DWG.

Part: SEAT TRACK — CORRODED (BS 437-477) · airframe 40,384 hrs · 26,020 cycles

THE SEAT TRACK AT LBL 9, BS 437 TO 477 HAD CORROSION. INSTALLED A NEW SEAT TRACK IAW AMM.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 40,384 hrs · 26,020 cycles

STRINGER 25R SPLICE AT BS 333 JOINT HAD CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM, AND DRAWING. (ORIGINAL: .063) - (REMAINING: .048) - (LOSS: .015). REMOVED AND REPLACED THE STRINGER SPLICE IAW DRAWING, AND SRM.

Part: GUSSET — CORRODED (BS 533) · airframe 40,384 hrs · 26,020 cycles

FWD CARGO, BS 533, STRINGER 27 CORNER GUSSET CORRODED. REPLACED THE GUSSET IAW SRM.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 40,384 hrs · 26,020 cycles

* SERVICE DOOR LOWER SEAL STRIKER SCREW HOLES ARE CORRODED. REMOVED CORROSION FROM SERVICE DOOR LOWER SEAL STRIKER "OUT OF LIMITS" REF CRJ700 SRM (ORIGINAL: .120) - (REMAINING: .077) - (LOSS: .043). REMOVED AND REPLACED SERVICE DOOR LOWER SEAL STRIKER REF DRAWING, AND SRM. LEAK CHECKS GOOD

Part: MOUNT — CORRODED (BS 533) · airframe 40,384 hrs · 26,020 cycles

FWD BAGGAGE - FS 533 BETWEEN STGRS 27 AND 26L - D RING CUP MOUNTING BRKT CORRODED AROUND NUTPLATES. REMOVED CORROSION FROM FWD BAGGAGE BAY D RING CUP BRACKET AT FS533 BETWEEN STGR27 AND STGR26L, REF CRJ 700 SRM, PART IS OUT OF LIMITS DUE TO NO DAMAGE ALLOWED IAW SRM. REMOVED AND REPLACED D RING CUP BRACKET. SEE CONTINUATION CARD FOR DETAILS

Part: SEAT TRACK — CORRODED (BS 485-677) · airframe 40,384 hrs · 26,020 cycles

PASSENGER CABIN RT SEAT TRACK BETWEEN BS 485 AND 677, RBL 9, HAD MULTIPLE AREAS OF CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW AMM

Part: FLOORBEAM — CRACKED (BS 280) · airframe 40,384 hrs · 26,020 cycles

* LH FS280 / LBL9 INBD ANGLE IS POSSIBLE CRACKED. FLAGGED (C-CHECK) RO 7/25/2020 REPLACED LH FS280 IB ANGLE AT LBL9 REF CRJ-700 SRM AND BOMBARDIER DWG. COMPLIED WITH SKYWEST TASKCARD.

Part: DOUBLER — CORRODED (BS 533) · airframe 40,384 hrs · 26,020 cycles

* FWD BAGGAGE - FS 533 STGR 26L - BUTTERFLY DBLR CORRODED AROUND FSTNRS. REMOVED CORROSION FROM BUTTERFLY DOUBLER IN FWD BAGGAGE AT FS533 STRG26L IAW CRJ700 SRM, NO ALLOWABLE LIMITS IAW CRJ700 SRM, REPLACED DOUBLER IAW EO DWG, CRJ700 SRM, DWG. COMPLIED WITH SKYWEST TASK CARD

Part: SUPPORT ANGLE — CORRODED (BS 280) · airframe 40,384 hrs · 26,020 cycles

*AVIONICS CRAWLWAY SUPPORT ANGLE AT APPROX. FS280 HAS CORROSION. (C-CHECK) RO 7/25/2020 REMOVED & REPLACED FLOOR SUPPORT ANGLE ON FS280 LWR BULKEAD IN AVIONICS BAY WITH A "NEW" FLOOR SUPPORT ANGLE PER MHIRJ DRWG SEE ATTACHED CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS

Part: FRAME — CORRODED (BS 333) · airframe 40,384 hrs · 26,020 cycles

* LH FS333.00 / BETWEEN STGR 18-19 BOTH SIDES FRAME ARE CORRODED. FLAGGED (C-CHECK) RO 7/25/2020 --FRAME FS333 BETWEEN STR18L - STR19L "OUT OF LIMITS" DUE TO OVER LAPPING DAMAGE IN MULTIPLE ELEMENTS REF SRM. REMOVED AND REPLACED FRAME SECTOR FS333 BETWEEN STR18L - STR21L REF SRM, DRAWING. COMPLIED WITH SKYWEST TASKCARD. LEAK CHECKS GOOD.

Part: MOUNT — CORRODED (BS 533) · airframe 40,384 hrs · 26,020 cycles

* FWD BAGGAGE - FS 533 BETWEEN STGRS 23L AND 22L - D RING CUP MOUNTING BRKT CORRODED AROUND FSTNRS AS MARKED (C-CHECK) RO 7/25/2020 REMOVED CORROSION FROM FWD BAGGAGE BAY D RING CUP AT FS533 BETWEEN STGR23L AND STGR22L, REF CRJ 700 SRM, PART IS OUT OF LIMITS DUE TO NO DAMAGE ALLOWED REF CRJ 700 SRM. REMOVED AND REPLACED D RING CUP. SEE CONTINUATION CARD FOR DETAILS

Part: DOOR SILL — CORRODED (GALLEY DOOR) · airframe 40,384 hrs · 26,020 cycles

*GALLEY SERVICE DOOR SILL INNER ANGLE HAS MULTABLE AREA'S OF CORROSION. FLAGGED (C-CHECK) RO 7/25/2020 --GALLEY SERVICE DOOR SILL INNER ANGLE "OUT OF LIMITS" DUE TO CORROSION ON MULTIPLE ELEMENTS REF CRJ700 SRM --REMOVED AND REPLACED THE GALLEY SERVICE DOOR SILL INNER ANGLE REF DRAWING, CRJ700 SRM. COMPLIED WITH SKYWEST TASKCARD. LEAK CHECKS GOOD.

Part: DOOR SILL — CORRODED (PAX DOOR) · airframe 40,384 hrs · 26,020 cycles

* PAX DOOR LOWER SILL ANGLE HAS SEVERAL AREA'S OF CORROSION. REMOVED AND REPLACED CORRODED PAX DOOR LOWER SILL ANGLE WITH NEW USING NEW FASTENERS, REF BOMBARDIER DWG AND SRM.

Part: MOUNT — CORRODED (BS 549-565) · airframe 40,384 hrs · 26,020 cycles

* FWD BAGGAGE - BETWEEN FS'S 549 AND 565 - STGRS 27 AND 26L - D RING CUP MOUNTING BRKT 1) CORRODED AT FSTNRS AS MARKED 2) HAS SCREW BROKEN OFF IN NUTPLATE (C-CHECK) RO 7/25/2020 --BLENDED CORROSION ON THE D RING MOUNTING CUP BRACKET BETWEEN FS549 - FS565 STR27L - STR26L "OUT OF LIMITS" NO DAMAGE ALLOWED REF CRJ700 SRM. --REMOVED AND REPLACED FWD BAGGAGE BAY D RING MOUNTING CUP BRACKET BETWEEN FS549 - FS565 STR27L -STR26L REF CRJ700 SRM, REO, DRAWING. COMPLIED WITH SKYWEST TASKCARD. LEAK CHECKS GOOD.

Part: STRINGER — CORRODED (BS 319-333) · airframe 40,384 hrs · 26,020 cycles

STRINGER STGR25, HAS CORROSION BETWEEN FS319 AND FS333. REMOVED CORROSION FROM THE STRINGER, "OUT OF LIMITS" IAW SRM (ORIGINAL: .063) - (REMAINING: .032) - (LOSS: .031) / --REMOVED AND REPLACED THE STRINGER IAW DRAWING, AND SRM.

Part: STRINGER — CORRODED (BS 319-333) · airframe 40,384 hrs · 26,020 cycles

*FUSELAGE INTERNAL STRUCTURE €“ STRINGER STGR26, HAS CORROSION BETWEEN FS319 AND FS333. REMOVED CORROSION FROM STR26R BETWEEN FS319 - FS333 "OUT OF LIMITS" REF SRM (ORIGINAL: .063) - (REMAINING: .035) - (LOSS: .028). REMOVED AND REPLACED THE STRINGER IAW DRAWING, AND SRM.

Part: STRINGER — CORRODED (BS 333) · airframe 40,384 hrs · 26,020 cycles

STGR26 SPLICE AT FS333 JOINT HAS CORROSION. REMOVED CORROSION FROM THE STRINGER SPLICE "OUT OF LIMITS" REF SRM, DRAWING (ORIGINAL: .063) - (REMAINING: .032) - (.031) / --REMOVED AND REPLACED THE STRINGER SPLICE IAW DRAWING, AND SRM.

Part: SEAT TRACK — CORRODED (BS 485-677) · airframe 40,384 hrs · 26,020 cycles

PASSENGER CABIN LT SEAT TRACK BETWEEN BS 485 AND 677 HAD MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM.

Part: DOUBLER — CORRODED (BS 581) · airframe 40,384 hrs · 26,020 cycles

* FWD BAGGAGE - FS 581 STGR 26L - BUTTERFLY DBLR CORRODED AROUND FSTNRS (C-CHECK) RO 7/25/2020 REMOVED FWD BAGGAGE - FS 581 STGR 26L - BUTTERFLY DBLR CORRODED AROUND FSTNRS AND INSTALLED NEW REPLACEMENT JOINT PLATE P/N SH670-33793-3 WITH NEW FASTENERS AT FWD BAGGAGE DOOR SURROUND STRUCTURE FS.581.00 AS PER CRJ700 SRM TASK REF. BOMBARD. DWG.

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 40,384 hrs · 26,020 cycles

PAX DOOR AFT WEB STIFFENER WAS CRACKED WHERE PAX DOOR MOTTOR MOUNT ATTACHED. REMOVED AND REPLACED AFTE WEB STIFFENER IAW SRM.

Part: DOOR FRAME — CORRODED (PAX DOOR) · airframe 40,384 hrs · 26,020 cycles

PAX DOOR FWD FORMER HAS CORROSION (C-CHECK) RO 7/25/2020 --PAX DOOR FWD FORMER "OUT OF LIMITS" DUE TO CORROSION IN MORE THAN ON ELEMENT AT A GIVEN CROSS SECTION REF REO --REMOVED AND REPLACED THE PAX DOOR FWD FORMER REF DRAWING, CRJ700 SRM. LEAK CHECKS GOOD.

Part: DOOR FRAME — CORRODED (PAX DOOR) · airframe 40,384 hrs · 26,020 cycles

PAX DOOR FORMER AT FS329.41 BET. INTERCOSTAL DD5 AND DD6 HAS CORROSION (C-CHECK) RO 7/25/2020 --PAX DOOR FORMER AT FS329.41 DD5 & DD6 "OUT OF LIMITS" DUE TO CORROSION AT MORE THAN ONE ELEMENT AT A GIVEN CROSS SECTION REF REO. --REMOVED AND REPLACED THE PAX DOOR FORMER AT FS329.41 BETWEEN DD5 & DD6 REF CRJ700 SRM, DRAWING. LEAK CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 40,384 hrs · 26,020 cycles

PAX DOOR CENTER INTERCOSTALL DD6 WAS CORRODED (C-CHECK) RO 7/25/2020 PAX DOOR INTERCOSTAL DD6 CENTER HAS CORROSION IN MORE THAN ONE ELEMENT AT A GIVEN CROSS SECTION, FOUND OUT OF LIMIT REF REO, AND CRJ 200 SRM. REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD6 WITH NEW P/N 601R318057-1 REF CRJ700 SRM AND BOMBARDIER DWG. UPON REMOVAL OF PAX DOOR CENTER INTERCOSTAL FOUND CLIP COMMON TO FS329.41 FORMER TO HAVE EXFOLIATING CORROSION RESULTING IN 100% MATERIAL LOSS. / REMOVED AND REPLACED DD6 INTERCOSTAL CENTER CLETE WITH NEW P/N 600-31902-269 CRJ700 SRM AND BOMBARDIER DWG, LEAK CHECKS GOOD

Part: FRAME — CORRODED (BS 319) · airframe 40,384 hrs · 26,020 cycles

FRAME @ FS319 STGR17L-STGR21L IS CORRODED (C-CHECK) RO 7/25/2020 --FRAME FS319 STR17L - STR21L "OUT OF LIMITS" DUE TO CORROSION ON TWO LOCATIONS ON THE FRAME REF CRJ700 SRM --REMOVED AND REPLACED FRAME FS319 BETWEEN STR17L - STR21L REF CRJ700 SRM, DRAWING. COMPLIED WITH SKYWEST TASKCARD. LEAK CHECKS GOOD.

Part: STRUCTURE — CORRODED (BS 310-333) · airframe 40,384 hrs · 26,020 cycles

BACKUP SILL @ STGR21L FS310-FS333 IS CORRODED (C-CHECK) RO 7/25/2020 --BACKUP SILL AT STR21L FS310-333 "OUT OF LIMITS" DUE TO SUBSEQUANT LOCATION OF ALLOWABLE DAMAGE REF CRJ700 SRM --REMOVED AND REPLACED THE BACKUP SILL AT STR21L FS310-333 REF DRAWING, CRJ700 SRM. COMPLIED WITH SKYWEST TASKCARD. LEAK CHECKS GOOD.

Part: STRUCTURE — CORRODED (BS 333-349) · airframe 40,384 hrs · 26,020 cycles

BACKUP SILL @ STGR21L FS333-FS349 IS CORRODED (C-CHECK) RO 7/25/2020 --BACKUP SILL AT STR21L, FS333 - FS349 "OUT OF LIMITS" DUE TO CORROSION ON TWO LOCATIONS REF CRJ700 SRM--REMOVED AND REPLACED THE BACKUP SILL AT STR21L BETWEEN FS333 - FS349 REF DRAWING, CRJ700 SRM. LEAK CHECKS GOOD.

Part: WEB — CORRODED (PAX DOOR) · airframe 40,384 hrs · 26,020 cycles

PAX DOOR AFT WEB CORRODED IN VARIOUS LOCATIONS. REMOVED, REPLACED AND INSTALLED NEW PAX DOOR AFT WEB IAW SRM.

Part: WASHER — CORRODED (RT TE FLAPS) · airframe 40,384 hrs · 26,020 cycles

RT FLAP SYSTEM TORQUE TUBE RETAINER LOOPS, HARDWARE CORRODED. REMOVED AND REPLACED THE HARDWARE WITH NEW IAW SRM.

Part: BOLT — CORRODED (TE FLAPS) · airframe 40,384 hrs · 26,020 cycles

FLAP SYSTEM TORQUE TUBE RETAINER LOOP UNDER PANEL 691 HB, HARDWARE CORRODED. REMOVED AND REPLACED THE HARDWARE WITH NEW IAW SRM.

Part: DOOR SILL — CORRODED (AFT CARGO) · airframe 40,384 hrs · 26,020 cycles

*AFT CARGO DOOR SILL IS CORRODED. (MARKED) (C-CHECK) RO 7/25/2020 REMOVED AND REPLACED LOWER SILL ON AFT CARGO ENTRY PER CRJ 700 SRM AND INSTALLATION DWG. COMPLIED WITH SKYWEST SKYCARD.

Part: SKIN — DENTED (BS 364-394) · airframe 40,384 hrs · 26,020 cycles

POSSIBLE DENTS AND DISTORTIONS ON EXTERNAL SKIN JUST AFT OF PAX DOOR APPROX. FROM FS364.00 AND FS394.00 BET STGR 23L TO STGR 17R (C-CHECK) RO 7/25/2020 --DENTS ARE "OUT OF LIMITS" DUE TO SUBSEQUENT LOCATION OVER STR21L & STR22L, NO DAMAGE ALLOWED REF CRJ700 SRM --COMPLIED WITH MHIRJ REO BY ENSURING DENTS ARE CRACK FREE, SMOOTH IN CONTOUR AND REPLACING FASTENERS AS NECESSARY. RESTORED FINISH. COMPLIED WITH SKYWEST TASKCARD. LEAK CHECKS GOOD.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 40,384 hrs · 26,020 cycles

*RIGHT HAND INBOARD FLAP LOWER SURFACE HAS (5) EACH SMALL DENTS BETWEEN THE INBOARD EDGE OF THE FLAP AND ITS HINGE. (MARKED) (C-CHECK) RO 7/25/2020 REPAIRED THE RIGHT HAND INBOARD FLAP LOWER SURFACE REF CRJ700 SRM, DAMAGE CUT-OUT AND EXTERNAL NON-FLUSH DOUBLER INSTALLATION. COMPLIED WITH SKYWEST TASK CARD

Part: FLOORBEAM — CRACKED (BS 847) · airframe 38,714 hrs · 24,656 cycles

FLOOR SUPPORT BEAM LOCATED AT LBL9 FS 847 IS CRACKED AT I/B SIDE FLANGE. COMPLIED WITH REPAIR ON FLOOR SUPPORT BEAM IAW REO.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 32,620 hrs · 19,692 cycles

AFT BAG BAY SILL DOUBLER HAS CORROSION AROUND NUT PLATE HOLES FS1031-FS1047. C-CHECK, INSTALLED AFT BAG BAY DOOR SILL DOUBLER IAW SRM.

Part: BRACKET — CORRODED (LT WING) · airframe 32,620 hrs · 19,692 cycles

FWD ATTACH ANGLE BRACKET ON AFT SIDE OF LT WING AFT SPAR FOR PANEL 542AZ CORRODED. C-CHECK, INSTALLED REPLACEMENT ATTACH ANGLE BRACKET IAW SRM. LEAK CHECK GOOD.

Part: BRACKET — CORRODED (RT WING) · airframe 32,620 hrs · 19,692 cycles

FWD ATTACH ANGLE BRACKET ON AFT SIDE OF RT WING AFT SPAR FOR PANEL 642AZ CORRODED. C-CHECK, INSTALLED REPLACEMENT ATTACH ANGLE BRACKET FOR ACCESS PANEL 642AZ ON RT WING AFT SIDE OF AFT SPAR IAW SRM. LEAK CHECK GOOD.

Part: STRAP — CORRODED (FUSELAGE) · airframe 32,620 hrs · 19,692 cycles

RT SIDE, FS909, AFT WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE HAS CORROSION ON LOWER STRAP P/N SH670-39341-3. C-CHECK, REPLACED LWR STRAP ON RT AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE AT FS909 IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 32,620 hrs · 19,692 cycles

LT, FS 879, AFT WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE HAS CORROSION ON LOWER STRAP P/N SH670-39333-9. C-CHECK, REPLACED LWR STRAP ON LT WING TO BODY FAIRING SUPPORT STRUCTURE AT FS 879 IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 32,620 hrs · 19,692 cycles

FS909, AFT WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE HAS CORROSION ON MID STRAP P/N SH670-39338-3. C-CHECK, REPLACED STRAP ON AFT WING TO BODY FUSELAGE SUPPORT STRUCTURE AT FS909 IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 32,620 hrs · 19,692 cycles

RT, FS 879, AFT WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE HAS CORROSION ON LOWER STRAP P/N SH670-39333-9. C-CHECK, REPLACED LWR STRAP ON RT WING TO BODY FAIRING SUPPORT STRUCTURE AT FS 879 IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 32,620 hrs · 19,692 cycles

LT SIDE, FS909, AFT WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE HAS CORROSION ON LOWER STRAP P/N SH670-39341-3. C-CHECK, INSTALLED LT LWR STRAP LOCATED AT FS909 LT AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 32,620 hrs · 19,692 cycles

LT SIDE, FS939, AFT WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE HAS CORROSION ON LOWER ANGLE P/N SH670-39265-5. C-CHECK, REPLACED LWR ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 32,620 hrs · 19,692 cycles

PAX DOOR SILL FLOOR ANGLE IS CORRODED ALONG BACKSIDE AND SEVERAL AREA'S ALONG THE TOP. C-CHECK, REMOVED CORRODED FLOOR SILL ANGLE ON PAX DOOR AND INSTALLED NEW DOOR SILL ANGLE MID CAP IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,620 hrs · 19,692 cycles

FS295 FRAME REQUIRES REPAIR ON LOWER FLANGE BETWEEN STR27 AND STR26L DUE TO OUT OF LIMITS CORROSION. C-CHECK, COMPLIED WITH REPAIR TO THE FS 295 FRAME IAW REO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,620 hrs · 19,692 cycles

FS 319 FRAME HAS CORROSION BETWEEN STR 26R AND STR 25L. C-CHECK, COMPLIED WITH REPAIR IAW REO.

Part: PANEL — CHAFED (LT WING) · airframe 32,620 hrs · 19,692 cycles

LT WING PANEL 584ET HAS CHAFING. C-CHECK, REPLACED CHAFED PANEL 584ET IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,620 hrs · 19,692 cycles

FS 295.00 FRAME CORRODED BETWEEN STR 27 AND 26 LT. C-CHECK, FS295 FRAME REPAIRED IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 32,620 hrs · 19,692 cycles

AFT BAGGAGE BAY SILL IS CORRODED. C-CHECK, REMOVED AND REPLACED DAMAGED AFT BAGGAGE BAY DOOR SILL WITH NEW SERVICEABLE DOOR SILL IAW SRM. PRESSURIZATION LEAK CHECK GOOD.

Part: CHANNEL — CRACKED (CARGO DOOR TRACK) · airframe 28,959 hrs · 17,135 cycles

THE AFT CARGO DOOR FWD TRACK LOWER MID SURROUND FRAME SUPOORT CHANNEL LOWER FLANGE IS CRACKED AND BENT, MARKED WITH GREEN TAPE, C-CHECK RO 3/24/15, REPAIRED THE AFT CARGO DOOR FWD TRACKS LOWER MID SURROUND FRAME SUPPORT CHANNEL LOWER FLANGE.

Part: ATTACH FITTING — DAMAGED (DOOR HINGE) · airframe 28,959 hrs · 17,135 cycles

PAX DOOR HINGE LUG NR 1 ROLL PIN HOLE IS ELONGATED, C-CHECK, COMPLIED WITH PERMANENT REPAIR OF STS EA FURTHER ACTION REQUIRED.

Part: ATTACH FITTING — GOUGED (DOOR HINGE) · airframe 28,959 hrs · 17,135 cycles

PAX DOOR HINGE AT THE AFT LUG LAND IS GOUGED, C-CHECK RO 3/24/15, REPAIRED AFT LUG LAND OF PAX DOOR HINGE REF REO REPAIR TYPE IV, STEPS 1-3 AND DWG SH670-31876, REV F, DATED 1997-03.

Part: STRUCTURE — CRACKED (BS 193) · airframe 28,959 hrs · 17,135 cycles

FWD EQUIPMENT COMPARTMENT LANDING CRACKED ON LT SIDE AT BS 193 AND WL 79.5. REPAIRED IAW REO.

Part: STRUCTURE — CRACKED (BS 193) · airframe 28,959 hrs · 17,135 cycles

FWD EQUIPMENT COMPARTMENT LANDING CRACKED ON RT SIDE AT BS 193 AND WL 79.5. REPAIRED IAW REO.

Part: ATTACH FITTING — GOUGED (DOOR HINGE) · airframe 28,959 hrs · 17,135 cycles

FROM THE FWD SIDE OF PAX DOOR TO MIDLINE- THE HINGE LUGS 5,6 AND 11 AND LUGS FROM THE AFT SIDE OF PAX DOOR TO MIDLINE, AT 1-5, AND 9 AND 10, ON PAX DOOR HINGE HALF, MARKED, ARE GOUGED/NICKED, C-CHECK, RO 3/24/15. REPAIRED PAX DOOR HINGE, DOOR SIDED, CHAFED LUGS WITHIN LIMITS REF REO.

Part: LATCH — CHAFED (LT NACELLE DOOR) · airframe 28,959 hrs · 17,135 cycles

LEFT NACELLE LATCH DOOR ASSY CHAFED. REPAIRED IAW EA.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 27,384 hrs · 16,280 cycles

FWD F/A FLASHLIGHT INOPERATIVE. R & R BATTERY, OPS CHECK GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 26,670 hrs · 15,908 cycles

INTERIOR EMERGENCY LIGHT JUST AFT OF THE SERVICE DOOR IS DAMAGED. REPLACED INTERIOR EMERGENCY FLOOD LIGHT ASSY IAW AMM.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 26,215 hrs · 15,674 cycles

LAST TWO EMERGENCY LIGHTS DO NOT ILLUMINATE, RECHARGED THE BATTERY PACKS.

Part: BALLAST — FAULTY (CABIN) · airframe 25,274 hrs · 15,194 cycles

BURNED ODOR AROUND ROW 2C. OVERHEAD LIGHTS EXTINGUISHED OVER THE SAME ROW. FLT 6226 REPLACED BALLAST FOR OVERHEAD LIGHTS AT ROW 2 SEATS CD.

Part: PANEL — CHAFED (TE FLAP) · airframe 24,633 hrs · 14,837 cycles

RT WING INBD FLAP PANEL 684 ET CHAFED OUT OF LIMITS. C-CHECK REPLACED RT WING INBD FLAP PANEL 684 ET IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 24,633 hrs · 14,837 cycles

FS 280 STRINGER 3L CRACK. C-CHECK REPAIRED CRACK IAW REO.

Part: STRUCTURE — CHAFED (FUSELAGE) · airframe 24,633 hrs · 14,837 cycles

CHAFE GOUGE JUST AFT OF FS 977.00 AT STRINGER 27. C-CHECK REPAIRED IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,988 hrs · 13,915 cycles

EXIT ROW OVERHEAD EMERGENCY EXIT LIGHT BURNED OUT. (FLT 6249) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,222 hrs · 13,480 cycles

NR 1 OVERHEAD LIGHT BURNED OUT. (FLT 6304) RELAMPED OVERHEAD LIGHT.

Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 21,851 hrs · 13,276 cycles

THE LEFT ENGINE FORWARD MOUNT UPPER LINK HAS CORROSION ON THE BUSHINGS. (SERVICE) INSTALLED A SERVICABLE LEFT ENGINE FORWARD MOUNT UPPER LINK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,769 hrs · 13,229 cycles

ONE BULB IS OUT ON FLOOR LEVEL EMERGENCY EXIT ROW ON AIRCRAFT'S RIGHT SIDE. (FLT 5782) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 21,634 hrs · 13,150 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6365) FOUND CONNECTER TO NR 1 EMERGENCY LIGHT DISCONNECTED AND WAS RECONNECTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,239 hrs · 12,330 cycles

OVERHEAD EMERGENCY LIGHT IS OUT NEXT TO HINGE OF SERVICE DOOR. (FLT 5216) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,239 hrs · 12,330 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5480) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,060 hrs · 12,220 cycles

NR 5 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6353) RELAMPED EMERGENCY LIGHT.

Part: PANEL — WORN (RT AILERON) · airframe 19,980 hrs · 12,168 cycles

RIGHT AILERON UPPER FIXED LEADING EDGE WORN. (C-CHECK) REPLACED RIGHT AILERON UPPER FIXED LEADING EDGE PANEL IN REFERENCE TO SRM.

Part: PANEL — WORN (LT AILERON) · airframe 19,980 hrs · 12,168 cycles

LEFT AILERON UPPER FIXED LEADING EDGE WORN. (C-CHECK) REPLACED LEFT AILERON UPPER FIXED LEADING EDGE PANEL IN REFERENCE TO SRM.

Part: BEAM — CRACKED (BS 280) · airframe 19,980 hrs · 12,168 cycles

C-CHECK, FS 280 BEAM CRACKED AT LBL 11.0 AND RBL 11.0. REPAIRED FS 280 BEAM CRACKED AT LBL 11.0 AND RBL 11.0.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,964 hrs · 12,158 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6324) RELAMPED EMERGENCY LIGHT.

Part: SKIN — DENTED (WING) · airframe 19,980 hrs · 12,168 cycles

C-CHECK, DENT FOUND ON RIGHT INBOARD LEADING EDGE ABOVE LANDING LIGHT LENS. REPAIR DENT ON RIGHT INBOARD LEADING EDGE ABOVE LANDING LIGHT LENS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,748 hrs · 12,037 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5326) RELAMPED EMERGENCY LIGHT.

Part: COVER — MISSING (CABIN) · airframe 19,559 hrs · 11,927 cycles

FLOOR LEVEL EMERGENCY FLOOD LIGHT AT SERVICE DOOR COVER MISSING. (FLT 6273) REPLACED FLOOR LEVEL SERVICE DOOR EMERGENCY FLOOD LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,435 hrs · 11,859 cycles

NR 5 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5417) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,374 hrs · 11,827 cycles

NR 5 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6283) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,213 hrs · 11,741 cycles

NR 4 CEILING EMERGENCY LIGHT IS OUT. (FLT 6216) RELAMPED EMERGENCY LIGHT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 19,037 hrs · 11,631 cycles

APPROXIMATELY 50 PERCENT OF INTERIOR EMERGENCY LIGHTS NOT WORKING. (FLT 6207) CHARGED EMERGENCY LIGHTS WITH APU GENERATOR PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,657 hrs · 11,437 cycles

NR 1 AND NR 2 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 5456) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,578 hrs · 11,396 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 9 IS OUT. (FLT 5449) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,480 hrs · 11,349 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6483) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,285 hrs · 11,237 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5424) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,037 hrs · 11,082 cycles

NR 5 CEILING EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,814 hrs · 10,945 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6348) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,592 hrs · 10,821 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 15 IS OUT. (FLT 5314) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,985 hrs · 10,466 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6616) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,934 hrs · 10,436 cycles

#4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6414) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,276 hrs · 10,055 cycles

THE 2ND TO LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 1127) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 16,211 hrs · 10,018 cycles

RIGHT EXTERIOR NR 2 EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,141 hrs · 9,984 cycles

AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 6508) RELAMPED EMERGENCY LIGHT.

Part: BEAM — CRACKED (FUSELAGE) · airframe 15,316 hrs · 9,522 cycles

FS 280 BEAM CRACKED ON BOTH SIDES. (C-CHECK) REPLACE BEAM PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,316 hrs · 9,522 cycles

CEILING EMERGENCY FLOOD LIGHT INOPERATIVE, NR 2 FROM BACK OF AIRCRAFT. (FLT 6466) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,316 hrs · 9,522 cycles

MOST AFT CEILING EMERGENCY LIGHT INOPERATIVE. (FLT 6948) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,796 hrs · 9,209 cycles

NR 5 EMERGENCY CEILING LIGHT INOP. (FLT 6889) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,429 hrs · 8,973 cycles

NR 6 EMERGENCY CEILING LIGHT INOP. (FLT 6187) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,124 hrs · 8,791 cycles

AFT INTERIOR EMERGENCY FLOODLIGHT INOP. (FLT 6381) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,410 hrs · 8,372 cycles

MOST AFT CEILING EMERGENCY LIGHT INOP. (FLT 6217) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,441 hrs · 8,390 cycles

CEILING LIGHT AT THE EMERGENCY EXIT ROW LEFT SIDE INOP. (FLT 6720) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,307 hrs · 7,726 cycles

LAST AFT CEILING EMERGENCY FLOODLIGHT INOP. (FLT 5980) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — MISSING (CABIN) · airframe 12,178 hrs · 7,658 cycles

RIGHT WING FLOOR LEVEL EMERGENCY LIGHT IS MISSING A BULB. (FLT 5898) REPLACED RT OVERWING FLOOR LEVEL EXIT SIGN BULB IAW MM 33-51-15.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,068 hrs · 7,590 cycles

EMERGENCY CEILING LIGHT ABOVE ROW 15 INOP. (FLT 5890) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,966 hrs · 7,523 cycles

EMERGENCY LIGHT INOP. (FLT 6065) RELAMPED EMERGENCY LIGHT.

Part: PRINTED CKT BOARD — DEFECTIVE (EMERGENCY LIGHT) · airframe 11,198 hrs · 7,083 cycles

EMERGENCY LIGHTS CYCLE ON AND OFF EN ROUTE. (FLT 6209) REPLACED PRINTED CIRCUIT BOARD NR 5 IN JB11.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 10,513 hrs · 6,674 cycles

FLT 6542 - AFT EMERGENCY LIGHT INOP. RELAMPED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 11,438 hrs · 7,208 cycles

FS 280 BEAM CRACKED AND CORRODED. (C CHECK) REPAIRED PER REO.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 9,991 hrs · 6,339 cycles

FLT 6638 - AFT CEILING EMERGENCY LIGHT INOP. RELAMPED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 7,649 hrs · 4,900 cycles

COCKPIT FLOOR SUPPORT IS CRACKED AT FS 280, FOUND AT C-CHECK. INSTALLED COCKPIT FLOOR SUPPORT PER CRJ700/900 SRM 51-42-06-001-001-A01.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 7,649 hrs · 4,900 cycles

FS 280 BEAM IS CRACKED AT LBL 9, FOUND AT C-CHECK. REPAIRED FLOORBEAM AT FS 280 PER CRJ700/900 SRM 51-42-068 AND REO 670-53-11-265.

Part: HANDLE — BINDING (ESCAPE HATCH) · airframe 7,649 hrs · 4,900 cycles

CREW ESCAPE HATCH HANDLE BINDS, FOUND AT C-CHECK. RIGGED CREW ESCAPE HATCH LATCH MECHANISM PER CRJ7/9 AMM 52-22-02-820-801-A01. OPS CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 6,319 hrs · 4,095 cycles

FLT 6690 - CEILING EMERGENCY FLOOD LIGHT IS INOP. RELAMPED CEILING FLOOD LIGHT IAW CRJ 700 AMM 33-51-09. OPS CHECK GOOD.

Part: ACM — SMOKE (RIGHT) · airframe 5,700 hrs · 3,710 cycles

FLT 6056 - FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. REPLACED RIGHT ACM IAW CRJ MM 21-51-08. OPS CHECK GOOD.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 3,431 hrs · 2,315 cycles

PAX DOOR FWD & AFT HANDRAIL SUPPORT CRACKED. DISCOVERED DURING C-CHECK INSPECTION. FABRICATED AND INSTALLED DOUBLERS AND ANGLES.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 1,466 hrs · 1,033 cycles

RIGHT WINDSHIELD SHATTERED WHILE CLIMBING THROUGH FL 320. REPLACED RIGHT WINDSHIELD IAW CRJ 700 MM 56-11-01, P/N OFF: 601R33033-55 (NP-139321-14), S/N OFF: 05160H2240.

Part: DETECTOR — MALFUNCTIONED (TE FLAPS) · airframe 733 hrs · 514 cycles

FLAPS HALFSPEED STATUS MESSAGE. REPLACED THE LEFT O/B AND THE LEFT I/B SKEW DETECTORS PER CRJ MM 27-52-45. OPERATIONAL CHECK GOOD PER CRJMM 27-50-00 LT I/B, 5913163 SN OFF A1382, LH O/B PN 5913164 SN OFF A1351.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 425 hrs · 285 cycles

"FLAPS HALFSPEED" STATUS MSG. REPLACED NR 1 SFECU IAW MM 27-51-05. OPERATIONAL CHECK GOOD.

Part: CONTROLLER — MALFUNCTIONED (FLAP/SLATS) · airframe 353 hrs · 233 cycles

FLAPS HALFSPEED MESSAGE. REPLACED SFECU1 IAW MM 27-51-05. OPERATIONAL CHECK GOOD.

Part: FLAP — OUT OF RIG (LEFT) · airframe 256 hrs · 175 cycles

FLAPS HALFSPEED STATUS MESSAGE IN TAXI OUT. RIGGED LT IB SKEW DETECTOR. CLEAR INHIBITS. OPERATIONAL CHECKS GOOD. IAW 27-51-00.

Part: CONTROLLER — MALFUNCTIONED (SLAT/FLAPS) · airframe 220 hrs · 155 cycles

SLATS HALF SPEED STATUS MESSAGE DISPLAYED. REPLACED SFECU 2 IAW AMM 27-51-05. OPERATIONAL CHECK GOOD.