N763SK

Part: SLAT TRACK — CORRODED (ZONE 500) · airframe 48,006 hrs · 32,302 cycles

L5 SLAT TRACK SHOWS PITTING CORROSION ON TRACK FACE. (C-CHECK RO 2/18/2025) REPAIRED DAMAGE ON L5 SLAT TRACK FACE IAW REO 670-57-42-1920 REV-- DATE 2025-01-17 AND CRJ700 SRM 51-12-00, 57-40-00, AMM 27-81-00, 27-81-39. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S011425-4, P.O# 175152, DATE OF INSPECTION 14JAN2025. SEE REPORT FOR DETAILS. TOOLS USED: DEPTH GAUGE AJ-1511 CAL DUE: SEPT2025, DIGITAL CALIPER AV-7803 CAL DUE: JAN2025, DIGITAL CALIPER AV-7805 CAL DUE: JAN2025

Part: SLAT TRACK — CORRODED (ZONE 500) · airframe 48,148 hrs · 32,426 cycles

L5 SLAT TRACK SHOWS PITTING CORROSION ON TRACK FACE. (C-CHECK RO 2/18/2025) REPAIRED DAMAGE ON L5 SLAT TRACK FACE IAW REO 670-57-42-1920 REV-- DATE 2025-01-17 AND CRJ700 SRM 51-12-00, 57-40-00, AMM 27-81-00, 27-81-39. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S011425-4, P.O# 175152, DATE OF INSPECTION 14JAN2025. SEE REPORT FOR DETAILS. TOOLS USED: DEPTH GAUGE AJ-1511 CAL DUE: SEPT2025, DIGITAL CALIPER AV-7803 CAL DUE: JAN2025, DIGITAL CALIPER AV-7805 CAL DUE: JAN2025

Part: SKIN — CORRODED (ZONE 100) · airframe 48,148 hrs · 32,426 cycles

CORROSION ON EXTERNAL SKIN AT TCAS ANTENNA LANDING BETWEEN FS295 TO FS310.00 STR27 (C-CHECK RO 2/18/2025) FABRICATED 1- DOUBLER 2- FILLER WITH MATERIAL 2024T3 .063" AND INSTALLED REPAIR ON EXTERNAL SKIN AT TCAS ANTENA LANDING BETWEEN FS 295.00 AND FS 310.00 STR 27, IAW BOMBARDIER REO 670-53-21-2537 REV -- DATED 2024-12-25. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S122724-1, P.O# 175036 DATE OF INSPECTION 23 DEC 2024. SEE REPORT FOR DETAIL. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S122324-3, P.O# 175036 DATE OF INSPECTION 23 DEC 2024. SEE REPORT FOR DETAILS. CAL TOOL: DIGITAL CALIPER AV-7805, DUE DATE JAN 2025, DIGITAL SCALE AV-4800 CAL DUE DEC 2024. SRM 51-21-06

Part: SKIN — CORRODED (ZONE 100) · airframe 48,006 hrs · 32,302 cycles

CORROSION ON EXTERNAL SKIN AT TCAS ANTENNA LANDING BETWEEN FS295 TO FS310.00 STR27 (C-CHECK RO 2/18/2025) FABRICATED 1- DOUBLER 2- FILLER WITH MATERIAL 2024T3 .063" AND INSTALLED REPAIR ON EXTERNAL SKIN AT TCAS ANTENA LANDING BETWEEN FS 295.00 AND FS 310.00 STR 27, IAW BOMBARDIER REO 670-53-21-2537 REV -- DATED 2024-12-25. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S122724-1, P.O# 175036 DATE OF INSPECTION 23 DEC 2024. SEE REPORT FOR DETAIL. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S122324-3, P.O# 175036 DATE OF INSPECTION 23 DEC 2024. SEE REPORT FOR DETAILS. CAL TOOL: DIGITAL CALIPER AV-7805, DUE DATE JAN 2025, DIGITAL SCALE AV-4800 CAL DUE DEC 2024. SRM 51-21-06

Part: JOINT — CORRODED (ZONE 100) · airframe 48,148 hrs · 32,426 cycles

CIRCUMFERENTIAL JOINT FROM FS280.00 TO FS282.86 HAS SIGNS OF CORROSION BETWEEN STGR 22L AND 23L (C-CHECK RO 2/18/2025) REPAIRED CIRCUMFERENTIAL JOINT FROM FS280.00 TO FS282.86, BETWEEN STGR 22L AND STGR 23L IAW REO 670-53-21-2539 REV--, DATED 2024-12-31. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S121624-1, PO# 174849, DATE OF INSPECTION: 16 DEC 2024. SEE REPORT FOR DETAILS.CRJ700 SRM 51-42-06, SRM 51-25-16, SRM 51-21-11, 51-21-06

Part: JOINT — CORRODED (ZONE 200) · airframe 48,006 hrs · 32,302 cycles

CIRCUMFERENTIAL JOINT FROM FS280.00 TO FS282.86 HAS SIGNS OF CORROSION BETWEEN STGR 22L AND 23L (C-CHECK RO 2/18/2025) REPAIRED CIRCUMFERENTIAL JOINT FROM FS280.00 TO FS282.86, BETWEEN STGR 22L AND STGR 23L IAW REO 670-53-21-2539 REV--, DATED 2024-12-31. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S121624-1, PO# 174849, DATE OF INSPECTION: 16 DEC 2024. SEE REPORT FOR DETAILS.CRJ700 SRM 51-42-06, SRM 51-25-16, SRM 51-21-11, 51-21-06

Part: DRAG ANGLE — CRACKED (ZONE 100) · airframe 48,006 hrs · 32,302 cycles

R/H AFT VERT DRAG ANGLE CRACKED (C-CHECK RO 2/18/2025) REPAIRED RH AFT VERT DRAG ANGLE IAW REO 670-55-31-018 REV-A DATE 2016-11-10 AND CRJ700 SRM 51-21-11, 51-25-06, 51-25-16, 51-42-22.

Part: BRACKET — CRACKED (ZOEN 600 SLAT) · airframe 48,006 hrs · 32,302 cycles

R/H WING #1 SLAT #3 SLAT TRACK BOX BRACKET CRACKED. (C-CHECK RO 2/18/2025) REPAIRED DAMAGED SLAT TRACK BOX BRACKET ON RH WING #1 SLAT #3 SLAT TRACK BOX IAW REO 670 57-42-577 REV-- DATE 2016-12-02 AND CRJ700 AMM 20-70-00, 28-11-00.

Part: SLAT TRACK — CRACKED (ZONE 600) · airframe 48,148 hrs · 32,426 cycles

R/H WING #1 SLAT #3 SLAT TRACK BOX BRACKET CRACKED. (C-CHECK RO 2/18/2025) REPAIRED DAMAGED SLAT TRACK BOX BRACKET ON RH WING #1 SLAT #3 SLAT TRACK BOX IAW REO 670 57-42-577 REV-- DATE 2016-12-02 AND CRJ700 AMM 20-70-00, 28-11-00. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S123024-3, P.O# 175036, DATE OF INSPECTION 30DEC2024. SEE REPORT FOR DETAILS. TOOL USED: DIGITAL SCALE AV-8473 CAL DUE: AUG2025

Part: DRAG ANGLE — CRACKED (ZONE 200) · airframe 48,148 hrs · 32,426 cycles

R/H AFT VERT DRAG ANGLE CRACKED (C-CHECK RO 2/18/2025) REPAIRED RH AFT VERT DRAG ANGLE IAW REO 670-55-31-018 REV-A DATE 2016-11-10 AND CRJ700 SRM 51-21-11, 51-25-06, 51-25-16, 51-42-22. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S010625-3, P.O# 175152, DATE OF INSPECTION 01JAN2025. SEE REPORT FOR DETAILS.

Part: NONE — CRACKED · airframe 43,941 hrs · 28,831 cycles

CA SIDE WINDSCREEN OUTSIDE GLASS SHATTERED AT CRUISE / ALSO HAD A L WINDSHIELD HEAT IN CRUISE (FLIGHT 3019 - FILED CLOSED) R&R CAPTAIN'S WINDSHIELD IN REFERENCE TO TASK CARD 56-220-1000-SKY. OPS/LEAK CHECK GOOD. PLEASE REFERENCE AML 890895 FOR LH WINDSHIELD HEAT MESSAGE FOR CORRECTIVE ACTION

Part: BRAKE — OVERHEATED (NR 4) · airframe 41,657 hrs · 27,091 cycles

BRAKE OVERHEAT CAUTION MESSAGE POSTED IN CRUISE FLIGHT #4 BTMS ERRATTIC. (B1 CODES: 007476 / 007471 / 007472) / C: MEL 32-46-1D / CAT"C" DUE 06/14/2021 / BRAKE OVERHEAT (FLIGHT 3276 ) -DEFERRED #4 BRAKE BTMS PER CRJ 700 MEL 32-46-1D. COMPLIED WITH MX ACTION. AUTHORIZED BY MX CONTROL. PLACARD INSTALLED.

Part: BRAKE — OVERTEMP (RIGHT) · airframe 40,960 hrs · 26,607 cycles

D: BRAKE OVHT WARNING MESSAGE ENROUTE / C: PREFORMED FAULT CONFORMATION PER CRJ700 FIM TASK 32-46--00 FOUND RT OUTBOARD (NR 4) SENSOR FAULTED. DEFERRED NR 4 SENSOR PER MEL 32-46-1D. MX ACTION COMPLIED WITH, PLACARD INSTALLED / CAT C DUE 06MAR21 / BRAKE OVHT WARNING MESSAGE ENROUTE FLIGHT 3059 - FILED CLOSED FEB 24, 2021 STATION: MOB--PREFORMED FAULT CONFORMATION PER CRJ700 FIM TASK 32-46--00 FOUND RT OUTBOARD (NR 4) SENSOR FAULTED. DEFERRED NR 4 SENSOR PER MEL 32-46-1D. MX ACTION COMPLIED WITH, PLACARD INSTALLED.

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 40,449 hrs · 26,247 cycles

AFT DRAG ANGLE FOUND TO BE CRACKED. C-CHECK RO 11/12/2020. REPAIRED AFT DRAG ANGLE, IAW CRJ 700 REO. MAJOR REPAIR TASK CARD AND FORM 337 COMPLETED AND ATTACHED REFERENCE CAMP CONTINUE CARD 21747514 FOR MAINTENANCE PERFORMED.

Part: HINGE — GOUGED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

FUSELAGE PAX DOOR HINGE HALF AFT MOST LANDING IS GOUGED. C-CHECK RO 11/12/2020. REPAIRED FUSELAGE PAX DOOR HINGE HALF AFT MOST LANDING, IAW BOMBARDIER REO. MAJOR REPAIR TASK & FORM M-337 COMPLETED. NO WEIGHT CHANGE REQUIRED. DETAILED VISUAL INSPECTION DUE AT 31946 FLIGHT CYCLES WITH A REINSPECT EVERY 5700 FLIGHT CYCLES, REF ATTACHED CONTUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: HINGE — GOUGED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR HINGE AFT MOST LUG IS GOUGED. C-CHECK RO 11/12/2020. REPAIRED PAX DOOR HINGE AFT MOST LUG GOUGE, IAW BOMBARDIER REO. MAJOR REPAIR TASKS & FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE REQUIRED. DETAILED VISUAL INSPECTION OF THE LUG IS REQUIRED AT 31946 CYCLES WITH A REINSPECT EVERY 5700 CYCLES, REF ATTACHED CONTIUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

ANGLE P/N 601R317052-1 CORRODED, REQUIRES REPLACEMENT. C-CHECK RO 11/12/2020. LOCATED AND DRILLED NEW PASSENGER DOOR ANGLE, IAW CRJ SRM INSTALLED NEW PASSENGER DOOR ANGLE P/N 601R317052-1 CRJ 700 SRM. NO WEIGHT CHANGE. COMPLIED WITH M-337 AND M-131.

Part: ATTACH ANGLE — CORRODED (DOOR POST) · airframe 40,449 hrs · 26,247 cycles

RT 280 POST J ANGLE ATTACH CLIP CORROSION. C-CHECK RO 11/12/2020. FOUND DOOR POST CLIPS TO BE CORRODED OUT OF LIMITS. CORROSION DEPTH .010, MAX ALLOWED IS .006. REMOVED AND REPLACED CORRODED DOOR POST ATTACH CLIPS, IAW CRJ-700 SRM. WVAC TENG4886 CAL DATE:15-JUN-20 DUE 30-JUN-21 (DEPTH GAUGE).

Part: ANGLE — CORRODED (DOOR POST) · airframe 40,449 hrs · 26,247 cycles

LT 280 POST J ANGLE ATTACH CLIP CORROSION. FOUND DOOR POST CLIPS TO BE CORRODED OUT OF LIMITS. CORROSION DEPTH .013, MAX ALLOWED IS .006. REMOVED AND REPLACED CORRODED DOOR POST ATTACH CLIPS, IAW CRJ-700 SRM. WVAC TENG4886 CAL DATE:15-JUN-20 DUE 30-JUN-21 (DEPTH GAUGE).

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PULL IN CAM DOUBLER CRACKED P/N 601R318094-1. C-CHECK RO 11/12/2020. REMOVED AND REPLACED PAX DOOR PULL IN CAM DOUBLER, IAW CRJ 700 SRM. MAJOR REPAIR TASK & FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE REQUIRED, REF ATTACHED CONTIUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR INTERCOSTAL DD3 CENTER IS CORRODED. C-CHECK RO 11/12/2020. INSTALLED NEW PASSENGER DOOR INTERCOSSTAL DD3 P/N 601R318056-1, IAW CRJ 700 SRM. NO WEIGHT CHANGE. COMPLIED WITH M-337 AND M-131.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR INTERCOSTAL DD6 AT FS 311.75 IS CORRODED. C-CHECK RO 11/12/2020. INSTALLED NEW PASSENGER DOOR INTERCOSTAL DD6 P/N 601R31902-485, IAW CRJ 700 SRM. NO WEIGHT CHANGE. COMPLIED WITH M-337 AND M-131.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR INTERCOSTAL DD4 AT FS 347.25 IS CORRODED. C-CHECK RO 11/12/2020. INSTALLED NEW INTERCOSTAL DD4 P/N 601R31902-317, IAW CRJ SRM. NO WEIGHT CHANGE. COMPLIED WITH M-337 AND M-131.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR INTERCOSTAL DD4 AT FS 311.75 IS CORRODED. C-CHECK RO 11/12/2020. INSTALLED NEW INTERCOSTAL DD4 P/N 601R318093-1, IAW CRJ 700 SRM. NO WEIGHT CHANGE. COMPLIED WITH M-337 AND M-131.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR INTERCOSTAL DD6 AT FS 347.25 IS CORRODED. C-CHECK RO 11/12/2020. INSTALLED NEW PASSENGER DOOR DD2 INTERCOSTAL P/N 601R318051-1, IAW CRJ 700 SRM. NO WEIGT CHANGE. COMPLIED WITH M-337 AND M-131.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR INTERCOSTAL DD2 AT FS 347.25 IS CORRODED. C-CHECK RO 11/12/2020. INSTALLED NEW PASSENGER DOOR INTERCOSTAL DD2 FS 347.25 P/N 601R318052-1, IAW CRJ 700 SRM. NO WEIGHT CHANGE. COMPLIED WITH M-337 AND M-131.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR DD6 INTERCOSTAL IS CORRODED BETWEEN FS 311 AND 347. C-CHECK RO 11/12/2020. REMOVED AND REPLACED PAX DOOR DD6 INTERCOSTAL BETWEEN FS 311 AND FS 347, IAW CRJ 700 SRM AND ATTACHED MAJOR REPAIR SKY CARD NO WEIGHT CHANGE. MAJOR REPAIR 337 IS ATTACHED, REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR DD7 INTERCOSTAL IS CORRODED BETWEEN FS 347 AND FS 338. C-CHECK RO 11/12/2020. INSTALLED NEW DD7 INTERCOSTAL P/N 601R318825-1, IAW CRJ 700 SRM. NO WEIGHT CHANGE. COMPLIED WITH M-337 AMD M-131.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR INTERCOSTAL BETWEEN FS 320 AND FS 327 BETWEEN DD7 AND DD8 IS CORRODED. C-CHECK RO 11/12/2020. INSTALLED NEW PASSENGER DOOR INTERCOSTAL P/N 601R318083-1, IAW CRJ 700 SRM. NO WEIGHT CHANGE. COMPLIED WITH M-337 AND M-131.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR CLIP ANGLE AT FS 327 BETWEEN DD7 AND DD8 IS CORRODED. C-CHECK RO 11/12/2020. REMOVED AND REPLACED THE PAX DOOR CLIP ANGLE AT FS 327 BETWEEN DD7 AND DD8, IAW CRJ 700 SRM & ATTACHED MAJOR REPAIR SKY CARD REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. NO WEIGHT CHANGE 337 FORM IS ATTACHED.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR DD5 INTERCOSTAL IS CORRODED BETWEEN FS 311 AND FS 320. C-CHECK RO 11/12/2020. REMOVED AND REPLACED PAX DOOR DD5 INTERCOSTAL, IAW CRJ 700 SRM AND ATTACHED MAJOR REPAIR SKY CARD. NO WEIGHT CHANGE. MAJOR REPAIR 337 IS ATTACHED, REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR DD5 INTERCOSTAL IS CORRODED BETWEEN FS 338 AND FS 347. C-CHECK RO 11/12/2020. INSTALLED NEW PASSENGER DOOR DD5 INTERCOSTAL P/N 601R31902-317, IAW CRJ SRM. NO WEIGHT CHANGE. COMPLIED WITH M-337 AND M-131.

Part: DOOR FRAME — CORRODED (PAX DOORWAY) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR FS 320 FRAME IS CORRODED BETWEEN DD4 AND DD6. C-CHECK RO 11/12/2020. REMOVED AND REPLACED PAX DOOR FS 320 FRAME, IAW CRJ 700 SRM AND ATTACHED MAJOR REPAIR SKY CARD NO WEIGHT CHANGE MAJOR REPAIR 337 IS ATTACHED, REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR CLIP ANGLE AT FS 338 DD5 IS CORRODED. C-CHECK RO 11/12/2020. REMOVED AND REPLACED PAX DOOR CLIP P/N 600-31902-269, IAW CRJ 700 SRM. WEIGHT NOT EFFECTED. COMPLIED WITH M-337 AND M-131.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR CLIP ANGLE AT FS 338 DD4 IS CORRODED. C-CHECK RO 11/12/2020. REMOVED AND REPLACED PAX DOOR CLIP ANGLE AT FS 338 DD4, IAW CRJ-700 SRM. MAJOR REPAIR TASK AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE REQUIRED. REFERENCE ATTACHED CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR DD7 INTERCOSTAL IS CORRODED BETWEEN FS 311 AND FS 320. C-CHECK RO 11/12/2020. INSTALLED NEW PASSENGER DOOR INTERCOSTAAL P/N 601R318826-1 AO1, IAW CRJ SRM. NO WEIGHT CHANGE. COMPLIED WITH M-337 AND M-131.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR CLIP ANGLE AT FS 338 DD6 IS CORRODED. C-CHECK RO 11/12/2020. REMOVED AND REPLACED PAX DOOR CLIP ANGLE P/N 600-31902-269, IAW CRJ 700 SRM. MAJOR REPAIR TASK & FORM M-337 COMPLETED AND ATTACHED. WEIGHT CHANGE NOT REQUIRED. REFERENCE ATTACHED SKY CARD FOR WORK PERFORMED.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR DD4 INTERCOSTAL IS CORRODED BETWEEN FS 311 AND FS 347. C-CHECK RO 11/12/2020. INSTALLED NEW PAX DOOR INTERCOSTAL DD4 PN 601R318081-1, IAW CRJ 700 SRM. SEE CAMP CONTINUE CARD FOR MAINTENANCE PERFORMED. NO WEIGHT CHANGE. COMPLIED WITH M-337 AND M-131.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR DD3 INTERCOSTAL IS CORRODED BETWEEN FS 311 AND FS 329. C-CHECK RO 11/12/2020. REMOVED AND REPLACED PAX DOOR DD3 INTERCOSTAL BETWEEN FS 311 AND FS 329, IAW CRJ 700 SRM AND ATTACHED MAJOR REPAIR SKY CARD. NO WEIGHT CHANGE. MAJOR REPAIR 337 IS ATTACHED, REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 40,449 hrs · 26,247 cycles

RT FS 280 BEAM IS CORRODED BEYOND ALLOWABLE LIMITS, IAW CRJ700 SRM. C-CHECK RO 11/12/2020. REPLACED RT BEAM, IAW CRJ-700 SRM. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. PART FOR PART REPLACEMENT, NO WEIGHT CHANGE REQUIRED. REFERENCE ATTACHED CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: SKIN — GOUGED (RT AILERON) · airframe 40,449 hrs · 26,247 cycles

RT AILERON LOWER LEADING EDGE SKIN AND HINGE FITTING ARE GOUGED AT WS 318 APPROXIMATELY .125IN L X .125IN W X .020IN DEEP. C-CHECK RO 11/12/2020. COMPLETED REPAIR TO RT AILERON LOWER LEADING EDGE SKIN AND HINGE FITTING ARE GOUGED AT WS 318 APPROXIMATELY .125IN L X .125IN W X .020IN DEEP, IAW BOMBARDIER REO.

Part: FORMER — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR AFT FORMER IS CORRODED BETWEEN DOOR DATUM AND DD1. C-CHECK RO 11/12/2020. REMOVED AND REPLACED PAX DOOR AFT FORMER BETWEEN DOOR DATUM AND DD1, IAW CRJ 700 SRM AND ATTACHED MAJOR REPAIR SKY CARD. NO WEIGHT CHANGE. MAJOR REPAIR 337 IS ATTACHED, REF ATTACHED CONTIUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR CLIP ANGLE AT FS 323 DD1A IS CORRODED. C-CHECK RO 11/12/2020. REMOVED AND REPLACED PAX DOOR CLIP ANGLE P/N 600-31902-269, IAW CRJ 700 SRM. WEIGHT CHANGE NOT EFFECTED. COMPLIED WITH M-337 AND M-131.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR CLIP ANGLE AT FS 320 DD1A IS CORRODED. C-CHECK RO 11/12/2020. REMOVED AND REPLACED PAX DOOR CLIP ANGLE AT FS 320, IAW CRJ 700 SRM. MAJOR REPAIR TASK AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE REQUIRED. REFERENCE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR DD2 INTERCOSTAL IS CORRODED BETWEEN FS 311 AND FS 347. C-CHECK RO 11/12/2020. INSTALLED NEW PASSENGER DOOR DD2 INTERCOSTAL P/N 601R318053-3, IAW CRJ 700 SRM. NO WEIGHT CHANGE. COMPLIED WITH M-337 AND M-131.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 40,449 hrs · 26,247 cycles

LT FS 280 BEAM CORRODED BEYOND ALLOWABLE LIMITS, IAW CRJ700 SRM, REQUIRES REPLACEMENT. C-CHECK RO 11/12/2020. REPLACED LT BEAM, IAW CRJ-700 SRM. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. PART FOR PART REPLACEMENT, NO WEIGHT CHANGE REQUIRED. REFERENCE ATTACHED CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR CLIP ANGLE AT FS 329 DD1A IS CORRODED. C-CHECK RO 11/12/2020. FABRICATED AND REPLACED PAX DOOR CLIP ANGLE AT FS 329 DD1A, IAW CRJ 700 SRM PER DRAWING AND ATTACHED MAJOR REPAIR SKY CARD. NO WEIGHT CHANGE. MAJOR REPAIR 337 IS ATTACHED, REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR DD1 INTERCOSTAL IS CORRODED BETWEEN FS 338 AND FS 347. C-CHECK RO 11/12/2020. INSTALLED NEW PASSENGER DOOR INTERCOSTAL P/N 601R31902-318, IAW CRJ 700 SRM. NO WEIGHT CHANGE. COMPLIED WITH, M-337 AND M-131.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 40,449 hrs · 26,247 cycles

RBL 9 FLOOR SEAT TRACK FS 485-581 SEGMENT IS CORRODED. C-CHECK RO 11/12/2020. REMOVED AND REPLACED CORRODED SEAT TRACK FS 485-581, IAW CRJ 700 AMM.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 40,449 hrs · 26,247 cycles

RBL 9 FLOOR SEAT TRACK FS 684-838 SEGMENT IS CORRODED. C-CHECK RO 11/12/2020. REMOVED AND REPLACED SEAT TRACK AT RBL 9 FS 684-838, IAW CRJ 700 AMM.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 40,449 hrs · 26,247 cycles

RBL 9 FLOOR SEAT TRACK FS 349-485 SEGMENT IS CORRODED. C-CHECK RO 11/12/2020. REMOVED AND REPLACED RBL 9 FLOOR SEAT TRACK FS 349-485 SEGMENT AND 1 EACH NUTPLATE, IAW CRJ 700 SRM CRJ 700 AMM.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 40,449 hrs · 26,247 cycles

LBL 9 FLOOR SEAT TRACK FS 581-684 SEGMENT IS CORRODED. C-CHECK RO 11/12/2020. REMOVED AND REPLACED LBL 9 SEAT TRACK AT FS 581-684, IAW CRJ700 AMM.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 40,449 hrs · 26,247 cycles

LBL 9 FLOOR SEAT TRACK FS 684-838 SEGMENT IS CORRODED. C-CHECK RO 11/12/2020. REMOVED AND REPLACED SEAT TRACK FROM FS 684-838, IAW CRJ200 AMM WVACT200612 CAL DATE 16-MAR-20 DUE 31-MAR-21.

Part: SUPPORT — CORRODED (CABIN) · airframe 40,449 hrs · 26,247 cycles

LT SIDE SILL IS CORRODED BETWEEN FS 485 AND FS 517. C-CHECK RO 11/12/2020. REMOVED AND REPLACE LT SIDE SILL BETWEEN FS 485 TO FS 501, IAW CRJ 700 SRM REF AND SKYWEST TASK CARD ATTACHED CONTINUATION CARD FOR DETAILS OF WORK. PERFORMED NO WEIGHT CHANGE, M-337 IS ATTACHED.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 40,449 hrs · 26,247 cycles

LBL 9 FLOOR SEAT TRACK FS 374-485 SEGMENT IS CORRODED. C-CHECK RO 11/12/2020. REMOVED AND REPLACED LBL 9 FLOOR SEAT TRACK SEGMENT FROM FS 374-485, IAW CRJ-700.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 40,449 hrs · 26,247 cycles

LBL 9 FLOOR SEAT TRACK FS 485-581 SEGMENT IS CORRODED. C-CHECK RO 11/12/2020. REMOVED SEART TRACK AT LBL 9 FS 485-581 AND REPLACED WITH NEW SERVICEABLE SEAT TRACK, IAW CRJ-700 AMM.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 40,449 hrs · 26,247 cycles

RT FLOOR SILL IS CORRODED BETWEEN FS 349 AND FS 409 UPPER AND LOWER SURFACE. C-CHECK RO 11/12/2020. REMOVED AND REPLACED RT FLOOR SILL BETWEEN FS 349 AND FS 409, IAW CRJ 700 SRM REF ATTACHED CONTINUATION CARD, SW TASK CARD, AND 337 FOR DETAILS OF WORK. PERFORMED NO WEIGHT CHANGE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 40,449 hrs · 26,247 cycles

RT FLOOR SILL IS CORRODED BETWEEN FS 280 AND FS 319. C-CHECK RO 11/12/2020. INSTALLED RT FLOORSILL BETWEEN FS 280 AND FS 319, IAW CRJ 700 SRM. NO WEIGHT CHANGE. COMPLIED WITH M-337 AND M-131.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 40,449 hrs · 26,247 cycles

SERVICE DOOR SILL FLOOR SUPPORT ANGLES BETWEEN FS 319 AND FS 349 ARE CORRODED. C-CHECK RO 11/12/2020. INSTALLED NEW SERVICE DOOR SUPPORT ANGLES BETWEEN FS 319 AND FS 349, IAW CRJ700 SRM. RESTORED PAINT ON FASTNERS, IAW SRM.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 40,449 hrs · 26,247 cycles

LBL 27 FLOOR SEAT TRACK FS 364-485 SEGMENT IS CORRODED. C-CHECK RO 11/12/2020. REMOVED, FABRICATED AND REPLACED SEAT TRACK, IAW CRJ 700 AMM.

Part: SEAT TRACK — CORRODED (BS 581-684) · airframe 40,449 hrs · 26,247 cycles

RBL 9 FLOOR SEAT TRACK FS 581-684 SEGMENT IS CORRODED. C-CHECK RO 11/12/2020. REMOVED DAMAGED SEAT TRACK BETWEEN FS 581-FS 684 AT RBL 9 AND INSTALLED NEW SERVICEABLE SEAT TRACK, IAW CRJ700-AMM.

Part: INTERCOSTAL — CORRODED (CABIN) · airframe 40,449 hrs · 26,247 cycles

INTERCOSTAL BETWEEN FS 394.00 AND FS 409.00 BETWEEN STRINGER 26L AND STRINGER 27 IS CORRODED ALONG FLANGE. C-CHECK RO 11/12/2020. INSTALLED NEW INTERCOSTAL, IAW CRJ 700 SRM. NO WEIGHT CHANGE. COMPLIED WITH M-337 AND M-131.

Part: DOUBLER — CORRODED (TCAS ANTENNA) · airframe 40,449 hrs · 26,247 cycles

ANTENNA DOUBLER AT STRINGER 27 BETWEEN FS 295.00 AND FS 310.00 IS HEAVILY CORRODED AROUND ANTENNA CUTOUT AND APPROXIMATELY (12) SOLID FASTENERS. C-CHECK RO 11/12/2020. LOCATED, DRILLED AND INSTALLED ANTENNA DOUBLER AT STR 27 BETWEEN FS 295.00-FS 310.00, IAW CRJ 700 SRM. SEE CAMP CONTINUE CARD 21607101 FOR MAINTENANCE PERFORMED. NO WEIGHT CHANGE. COMPLIED WITH M-131.

Part: NUT PLATE — CORRODED (CABIN) · airframe 40,449 hrs · 26,247 cycles

NYLON GUIDE FITTING NUTPLATE PLATE ON THE FWD SIDE OF FS 364.00 IS CORRODED BETWEEN STRINGER 26R AND STRINGER 27. C-CHECK RO 11/12/2020. REMOVED AND REPLACED SH670-32457-2, IAW CRJ 700 SRM.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 40,449 hrs · 26,247 cycles

FS 280.00 FORWARD "J" ANGLE IS HEAVILY CORRODED. C-CHECK RO 11/12/2020. REMOVED AND REPLACED J ANGLE AT FS 280, IAW CRJ-700 SRM.

Part: INTERCOSTAL — CORRODED (CABIN) · airframe 40,449 hrs · 26,247 cycles

INTERCOSTAL BETWEEN FS 394.00 AND FS 409 BETWEEN STRINGER 26R AND STRINGER 27 IS CORRODED ALONG FLANGE. C-CHECK RO 11/12/2020. REMOVED AND REPLACED INTERCOSTAL BETWEEN FS 394.00 AND FS 409 BETWEEN STRINGER 26R AND STRINGER 27R, IAW CRJ 700. NO WEIGHT CHANGE. COMPLIED WITH M-337 AND M-131.

Part: INTERCOSTAL — CORRODED (CABIN) · airframe 40,449 hrs · 26,247 cycles

INTERCOSTAL BETWEEN FS 349.00 AND FS 364.00, BETWEEN STRINGER 26R AND STRINGER 27 IS HEAVILY CORRODED ON THE OUTBOARD FLANGE. C-CHECK RO 11/12/2020. INSTALLED NEW INTERCOSTAL FS 349.00-FS 364 BETWEEN STR 26L AND 27, IAW CRJ 700 SRM. SEE CONTINUE CARD 21607125 FOR MAINTENANCE PERFORMED. NO WEIGHT CHANGE. COMPLIED WITH M-337 AND M-131.

Part: ANGLE — CORRODED (BS 280) · airframe 40,449 hrs · 26,247 cycles

FS 280.00 RT WEB ANGLE IS CORRODED AT RBL 9.00 AND AT NUTPLATE LOCATION JUST OUTBOARD OF RBL 9.00. C-CHECK RO 11/12/2020. REMOVED AND REPLACED WEB, IAW CRJ-700 SRM. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. PART FOR PART REPLACEMENT, NO WEIGHT CHANGE REQUIRED. REFER TO ATTCHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: FRAME — CORRODED (BS 349) · airframe 40,449 hrs · 26,247 cycles

FS 349.00 IS CORRODED ON THE FORWARD FACE BETWEEN STRINGER 26L AND STRINGER 26R. C-CHECK RO 11/12/2020. LOCATED AND DRILLED RECEIVED PART SH670-31357-5S, IAW CRJ 700 SRM. SEE CAMP CONTINUE CARD NR 21607118 FOR MAINTENANCE PERFORMED. NO WEIGHT CHANGE. COMPLIED WITH M-337 AND M131.

Part: STRINGER — CORRODED (CABIN) · airframe 40,449 hrs · 26,247 cycles

STRINGER 27 IS CORRODED AT (4) LOCATIONS BETWEEN FS 280.00 AND FS 295.00. C-CHECK RO 11/12/2020. REMOVED AND REPLACED STGR 27, IAW CRJ-700 SRM. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE. REFERENCE ATTACHED CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 40,449 hrs · 26,247 cycles

INTERCOSTAL BETWEEN FS 349.00 AND FS 364.00, BETWEEN STRINGER 26L AND STRINGER 27 IS HEAVILY CORRODED ON THE OUTBOARD SIDE. C-CHECK RO 11/12/2020 INSTALLED NEW INTERCOSTAL, IAW CRJ 700 FS 349-FS 36 BETWEEN STR 26L-STR 27, IAW CRJ 700 SRM. SEE CAMP CONTINUE CARD FOR MAINTENANCE PERFORMED. NO WEIGHT CHANGE. COMPLIED WITH M-337 AND M-131.

Part: ANGLE — CORRODED (BS 280) · airframe 40,449 hrs · 26,247 cycles

FS 280.00 LT WEB ANGLE IS CORRODED AT LBL 9.00 AND AT NUTPLATE LOCATION JUST OUTBOARD OF LBL 9.00. C-CHECK RO 11/12/2020. REMOVED AND REPLACED WEB, IAW CRJ-700 SRM. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. PART FOR PART REPLACEMENT, NO WEIGHT CHANGE REQUIRED. REFER TO ATTCHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: DOOR SILL — CORRODED (AFT CARGO) · airframe 40,449 hrs · 26,247 cycles

AFT CARGO DOOR SURROUND LOWER FLOOR SILL IS CORRODED. C-CHECK RO 11/12/2020. REMOVED AND REPLACED AFT CARGO DOOR SURROUND LOWER FLOOR SILL, IAW CRJ 700 SRM & SKY CARD MAJOR REPAIR 337 IS ATTACHED. NO WEIGHT CHANGE, REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 40,449 hrs · 26,247 cycles

LT INBOARD FLAP LOWER SURFACE IS DENTED AT FLS 32.5, 2 IN FROM TRAILING EDGE APPROXIMATELY 1 IN LONG X .125IN WIDE X .020 DEEP. C-CHECK RO 11/12/2020. REPAIRED LT INBOARD FLAP LOWER SKIN AT FLS 32.5, IAW CRJ-700 SRM. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. WEIGHT CHANGE OF +2.62 IBS. REFERENCE ATTACHED CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: FORMER — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR FWD FORMER AT FS 311.75 CORRODED. C-CHECK RO 11/12/2020. REMOVED AND REPLACED PAX DOOR FORMER AT FS 311.75, IAW CRJ 700 ARM AND ATTACHED SKY CARD. M-337 IS ATTACHED AND NO WEIGHT CHANGE.

Part: SKIN — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR FWD SIDE PANEL (WEB) CORRODED IN SEVERAL LOCATIONS. C-CHECK RO 11/12/2020. REMOVED AND REPLACED PAX DOOR FWD SIDE PANEL, IAW CRJ 700 SRM.

Part: WEB — CORRODED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

PAX DOOR AFT SIDE PANEL (WEB) CORRODED IN SEVERAL LOCATIONS. C-CHECK RO 11/12/2020. REMOVED AND REPLACED PAX DOOR AFT SIDE PANEL P/N 601R3117071-11S, IAW CRJ 700 SRM.

Part: HINGE — GOUGED (PAX DOOR) · airframe 40,449 hrs · 26,247 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA-PAX DOOR PIANO HINGE FUSELAGE SIDE LUG NR 22 SMALL NICK ON UPPER SURFACE & LAND NR 27 HAS GOUGE FROM MIGRATED HINGE PIN ROLL PIN. REPAIRED LUG NR 22 TYPE 1 AND LAND NR 27 TYPE 4 REPAIR, REF REO. DETAILED VISUAL INSPECT, PER NDTM, PART NUMBER: -, SERIAL NUMBER: 10228, POSITION. C-CHECK RO 11/12/2020. COMPLIED WITH DETAILED VISUAL INSPECTION, PER NDTM FOUND GOUGE ON LANDING NR 27 REPAIRED GOUGE, IAW MHIRJ REO ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED ANALYSIS TO DETERMINE ADDITIONAL REQUIREMENTS WILL BE COMPLETED WITHIN 12 MONTHS FROM ISSUE DATE OF THIS REPAIR. NO WEIGHT CHANGE. COMPLIED WITH M-337 AND M-131.

Part: COMPUTER — MALFUNCTIONED (FUEL SYSTEM) · airframe 38,437 hrs · 24,674 cycles

RIGHT WING AND TOTAL FUEL QUANTITIES WENT BLANK. FL 3218 CLOSED. REMOVED AND REPLACED FUEL QUANTITY GAUGING COMPUTER.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 38,278 hrs · 24,555 cycles

PRESSURE FLOOR FWD SEAL ANGLE, HAD TWO OVERSIZED FASTENER HOLES AT FS693 RBL 36 INBD ROW. (C-CHECK) RO: 06/28/2019 REPAIR WAS COMPLETED IAW REO.

Part: PANEL — CHAFED (LT WING) · airframe 32,714 hrs · 20,011 cycles

CHAFE ON PANEL 584EB. REPLACED THE PANEL IAW SRM.

Part: STRINGER — CORRODED (BS 953-969) · airframe 32,714 hrs · 20,011 cycles

STRINGER 23R BETWEEN BS 953 - 969 CORRODED. REPLACED THE STRINGER SECTION IAW SRM. PRESSURE CHECK SATISFACTORY.

Part: ANGLE — CORRODED (WASTE PANEL) · airframe 32,714 hrs · 20,011 cycles

INTERNAL FUSELAGE AFT LAVATORY WASTE SUPPORT STRUCTURES BETWEEN BS 953 AND 969, STRINGERS 22 - 23R HAS CORROSION AT UPPER AFT CORNER. REMOVED WASTE SERVICING SURROUND STRUCTURE AFT NUTPLATE ANGLE INSTALLED NEW AFT NUTPLATE ANGLE IAW SRM. PRESSURE CHECKED GOOD.

Part: SKIN — CORRODED (BS 549) · airframe 32,714 hrs · 20,011 cycles

CORROSION ON THE SKIN LT SIDE OF BS 549 BELOW STRINGER 17L AND ABOVE THE FWD CARGO DOOR UPPER LINTEL. REMOVED AND REPLACED THE REINFORCING ANGLE AND INSTALLED A DOUBLER IAW EA. A PRESSURIZATION TEST OF THE REPAIRED AREA WAS COMPLETED IAW AMM.

Part: FLOOR SUPPORT — CORRODED (BS 1031-1032) · airframe 32,714 hrs · 20,011 cycles

CORROSION ON THE AFT CARGO FLOOR SUPPORT LBL 27 BETWEEN BS 1031 - 1032.5. REPAIRED IAW SRM AND REO.

Part: STRAP — CORRODED (BS 908) · airframe 32,714 hrs · 20,011 cycles

CORROSION FOUND FROM BLUE WATER AT BS 908 LOWER WING TO FUSELAGE FAIRING STRUCTURE ON LOWER MID STRAP. REPLACED THE LOWER MID STRAP IAW SRM.

Part: ANGLE — CORRODED (BS 939) · airframe 32,714 hrs · 20,011 cycles

CORROSION FOUND FROM BLUE WATER AT BS 939. LOWER WING TO FUSELAGE FAIRING STRUCTURE LT ANGLE TO RT ANGLE CORRODED. INSTALLED A NEW LT LOWER WING BODY FAIRING SUPPORT ANGLE, AND NEW CENTER ANGLE IAW SRM.

Part: DOOR SILL — CORRODED (AFT CARGO) · airframe 32,714 hrs · 20,011 cycles

AFT CARGO DOOR SURROUND STRUCTURE LOWER SILL IS CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM. LEAK CHECKED TESTS GOOD AT THIS TIME.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 32,714 hrs · 20,011 cycles

SERVICE DOOR SURROUND STRUCTURE LOWER SEAL STRIKER HAS CORROSION. REPLACED THE LOWER SEAL STRIKER IAW SRM. PRESSURIZATION CHECKED TESTS GOOD.

Part: CAP — DENTED (PAX DOOR) · airframe 32,714 hrs · 20,011 cycles

PAX DOOR FWD END CAP DENTED. INSTALLED A NEW FWD END CAP IAW SRM.

Part: STRAP — CORRODED (BS 280) · airframe 32,714 hrs · 20,011 cycles

BS 280 BUTTSTRAP CORRODED BETWEEN STRINGERS 26L AND 26R. REPAIRED IAW EA. PRESSURE CHECKED GOOD.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 32,714 hrs · 20,011 cycles

TWO DENTS UNDER SIDE OF INBOARD FLAP. REPAIRED THE FLAP IAW EA.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 30,263 hrs · 18,087 cycles

RIGHT EMERGENCY EXIT LIGHT FAILED. R & R THE NR 3 BATTERY PACK.

Part: THRESHOLD — BENT (PAX DOORWAY) · airframe 29,437 hrs · 17,569 cycles

PAX DOOR THRESHOLD IS PEELING UP, BENT UP, ON AFT CORNER. BENT DOWN PAX DOOR THRESHOLD IAW SRM.

Part: PANEL — CHAFED (LT WING) · airframe 29,437 hrs · 17,569 cycles

PANEL 584ET IS CHAFED. BLENDED OUT DAMAGE AND RESTORED FINISH TO REWORKED AREA IAW SRM.

Part: STRUCTURE — CRACKED (THRUST REVERSER) · airframe 29,437 hrs · 17,569 cycles

LEFT ENGINE LOWER INBD CASCADE CRACKED. REPAIRED CRACK IN LT ENGINE LOWER INBD CASCADE IAW STS EA. PERFORMED FUNCTIIONAL TEST OF THE THRUST REVERSER IAW AMM FUNCTIONAL TEST GOOD.

Part: SLIDER — GOUGED (TRANS COWL) · airframe 29,437 hrs · 17,569 cycles

GOUGE ON RT LOWER TRANS-COWL INBD SLIDER. COMPLIED WITH THE REPAIR ON RT LOWER TRANSCOWL SLIDER IAW REO.

Part: FLOOR PANEL — CRACKED (TRU BAY) · airframe 29,437 hrs · 17,569 cycles

TRU FLOOR CRACKED AT FS 193.00 NEAR ADG PUMP. REPAIRED CRACKED TRU FLOOR AT FS 193.00 NEAR ADG PUMP IAW STS EA.

Part: STRUCTURE — CRACKED (TRU BAY FLOOR) · airframe 29,437 hrs · 17,569 cycles

CRACK ON LT SIDE OF TRU FLOOR AT BS 193. REPAIRED THE LT SIDE OF TRU FLOOR IAW REO.

Part: ROLLER — GOUGED (AFT CARGO DOOR) · airframe 29,437 hrs · 17,569 cycles

AFT CARGO BAY AFT DOOR TRACK FOR DOOR UPPER ROLLER HAS DAMAGE, GOUGED ON UPPER AND LOWER SIDES OF TRACK, FS 1047. REPAIRED AFT BAG BAY-AFT CARGO DOOR TRACK AT BS 1047 IAW EA.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 29,437 hrs · 17,569 cycles

MAIN AVIONICS COMPARTMENT DOOR SURROUND STRUCTURE INTERCOSTAL S27 RT HAS CORROSION AT FS 364. BLENDED AVIONICS COMPARTMENT DOOR SURROUND STRUCTURE AT FS 364.00 INTERCOSTAL 27RT IAW SRM.

Part: RETAINER — DAMAGED (FWD CARGO DOOR) · airframe 29,437 hrs · 17,569 cycles

FWD CARGO BAY DOOR OUTER LOWER SEAL RETAINER IS WORN AT FWD AND AFT CORNERS AND IS DAMAGED AND DENTED IN CENTER OF DOOR, 2EA AREAS. REPAIRED FWD BAGGAGE BAY DOOR OUTER LOWER SEAL RETAINER WITH PERMANENT REPAIRS FOR GOUGES AND DENTS AT FWD, AFT AND CENTER LOCATIONS IAW REO.

Part: LUG — GOUGED (ZONE 200) · airframe 29,437 hrs · 17,569 cycles

LUG DAMAGED. REPAIRED IAW REO.

Part: FAN — FAILED (NR 1 RECIRC) · airframe 29,040 hrs · 17,321 cycles

ODOR IN CABIN, RECIRCULATION FAN 1 FAILED. R & R THE NR 1 RECIRCULATION FAN IAW AMM. OPS CHECKED GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 28,479 hrs · 17,010 cycles

WHEN TESTING EMEGENCY LIGHTS THEY TURN ON FOR APPROXIMATELY 2 SEC, DIMLY, THEN IMMEDIATELY TURN OFF. R & R ALL BATTERY PACKS, IAW AMM . OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 26,972 hrs · 16,154 cycles

FIRST OFFICER`S FLASHLIGHT IS INOPERATIVE. R & R FLASHLIGHT BATTERY IAW AMM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,722 hrs · 16,016 cycles

LT NR 3 EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R BATTERY PACK CHARGER IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,713 hrs · 16,012 cycles

EMERGENCY EXIT ROW LIGHT ON RT SIDE INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY NR 4 IAW AMM.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 26,699 hrs · 16,002 cycles

RT OVERWING EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. REPLACED THE FAILED MID POWER SUPPLY. OPS CHECKED GOOD.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 26,713 hrs · 16,012 cycles

RT OVERWING EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. REPLACED BATTERY CHARGER ASSY CONNECTED TO PS38 IAW AMM. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,713 hrs · 16,012 cycles

PORTIONS OF EMERGENCY LIGHTS ARE INOPERATIVE. CHARGED EMERGENCY LIGHT BATTERIES. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,699 hrs · 16,002 cycles

PORTIONS OF EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED ELBP AND CHARGED SYSTEM. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,583 hrs · 15,940 cycles

EMERGENCY EXIT SIGN AT FWD GALLEY, FLOOR LEVEL HAS ONE LAMP BURNED OUT. REPLACED THE LAMP.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,344 hrs · 15,811 cycles

RIGHT OVER WING EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGER.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,300 hrs · 15,785 cycles

RT LOWER EMERGENCY EXIT LIGHT AT OVERWING EXIT DOES NOT ILLUMINATE. REPLACED NR 3 AND 4 EMERGENCY POWER SUPPLY UNIT BATTERY PACKS AND BATTERY CHARGERS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,294 hrs · 15,778 cycles

LOWER EMERGENCY EXIT LIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,454 hrs · 15,324 cycles

NR 4 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT 6366 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,344 hrs · 15,256 cycles

EMERGENCY LIGHT AC LT OVERWING INOPERATIVE. FLT 6230 RELAMPED LT OVERWING "EXIT" SIGN.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,130 hrs · 15,129 cycles

EMERGENCY LIGHT DOES NOT ILLUMINATE. FLT 5198 ALLOWED EMERGENCY LIGHT BATTERIES TO CHARGE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 25,064 hrs · 15,097 cycles

RT SIDE FS 280 ANGLE AT BL 26 HAS CRACK ON LOWER END. C-CHECK REMOVED CRACKED RT BL 26 ANGLE & INSTALLED NEW ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 25,064 hrs · 15,097 cycles

LT SIDE FS 280 ANGLE AT BL 26 HAS CRACK AT LOWER END. C-CHECK REMOVED CRACKED LT SIDE FS 280 ANGLE AT BL 26 & INSTALLED NEW IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,064 hrs · 15,097 cycles

LT SIDE WALL SEAT TRACK SECTION FS 581.00-677.00 HAS ONE AREA OF CORROSION AT FS 613.00. C-CHECK BLENDED CORROSION ON THE LT SIDE WALL SEAT TRACK AT FS 581.00 TO FS 677.00 IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,064 hrs · 15,097 cycles

LT SIDE WALL SEAT TRACK SECTION FS 708.00-761.85 HAS FOUR AREAS OF CORROSION AT FS 714.00, 720.00, 726.00 & 730.00. C-CHECK BLENDED THE CORROSION ON THE LT SIDE WALL SEAT TRACK FS 708.00 TO FS 761.85 IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,064 hrs · 15,097 cycles

RT SIDE WALL SEAT TRACK SECTION FS 379-485 HAS ONE AREA OF CORROSION AT FS 394.00. C-CHECK BLENDED CORROSION ON THE RT SIDE WALL SEAT TRACK FS 379 TO FS 485 IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,064 hrs · 15,097 cycles

RT SIDE WALL SEAT TRACK SECTION FS 677.00-708.00 HAS ONE AREA OF CORROSION AT FS 695.00. C-CHECK BLENDED CORROSION ON THE RT SIDE WALL SEAT TRACK FS 677.00 TO FS 708.00 IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,064 hrs · 15,097 cycles

LT SIDE WALL SEAT TRACK SECTION FS 761.85-863.00 HAS TWO AREAS OF CORROSION AT FS 761.85 & 781.00. C-CHECK BLENDED THE CORROSION ON THE LT SIDE WALL SEAT TRACK FS 761.85 TO FS 863.00 IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,064 hrs · 15,097 cycles

RT SIDE WALL SEAT TRACK SECTION FS 761.85-863.00 HAS TWO AREAS OF CORROSION AT FS 761.85 & 781.00. C-CHECK BLENDED CORROSION ON THE RT SIDE WALL SEAT TRACK AT FS 761.85 TO FS 863.00 IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,064 hrs · 15,097 cycles

LT SIDE WALL SEAT TRACK SECTION FS 677.00-708.00 HAS TWO AREA OF CORROSION AT FS 695.00 & 706.00. C-CHECK BLENDED THE CORROSION ON THE LT SIDE WALL SEAT TRACK FS 677.00 TO FS 708.00 IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,064 hrs · 15,097 cycles

RT SIDE WALL SEAT TRACK SECTION FS 581.00-677.00 HAS ONE AREA OF CORROSION AT FS 613.00. C-CHECK BLENDED CORROSION ON THE RT SIDE WALL SEAT TRACK FS 581.00 TO FS 677.00 IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,064 hrs · 15,097 cycles

LT SIDE WALL SEAT TRACK SECTION FS 485.00-581.00 HAS ONE AREA OF CORROSION AT FS 522.00. C-CHECK BLENDED CORROSION ON THE LT SIDE WALL SEAT FS 485.00 TO FS 581.00 IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,064 hrs · 15,097 cycles

LT SIDE WALL SEAT TRACK SECTION FS 379-485 HAS THREE AREAS OF CORROSION AT FS 389.00, 404.00 & 422.00. C-CHECK REMOVED THE CORROSION FROM THE LT SIDE WALL SEAT TRACK FS 379 TO FS 485 IAW REO.

Part: LEVER — CHAFED (PAX DOOR) · airframe 25,064 hrs · 15,097 cycles

PASSENGER DOOR FWD PULL IN LEVER CHAFED. C-CHECK BLENDED OUT CHAFE ON PASSENGER DOOR FWD PULL IN LEVER IAW REO.

Part: SKIN — CHAFED (FUSELAGE) · airframe 25,064 hrs · 15,097 cycles

AIRCRAFT BELLY HAS SCRATCH AT FS 977.0. C-CHECK BLENDED CHAFED AREA AFT OF FS 977 IAW REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 25,064 hrs · 15,097 cycles

LT AILERON HAS CHAFE ON UPPER LE OTBD SIDE. C-CHECK REPAIRED LT AILERON UPPER SKIN OTBD SIDE IAW REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 25,064 hrs · 15,097 cycles

LT AILERON HAS CHAFE ON UPPER LE INBD SIDE. C-CHECK REPAIRED LT AILERON UPPER SKIN APPROXIMATELY AILS 311.54 STATION IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,307 hrs · 14,684 cycles

CABIN EMERGENCY LIGHTS BURNED OUT. FLT#5218 RELAMPED.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 23,030 hrs · 13,945 cycles

LEFT EMERGENCY EXIT DOOR LIGHT DOES NOT ILLUMINATE. (FLT 6200) REPLACED AFT EMERGENCY POWER SUPPLY UNIT.

Part: SEAT BELT — FAULTY (COCKPIT) · airframe 22,221 hrs · 13,440 cycles

F/O SEATBELT WILL NOT RELEASE. (FLT 5653) REPLACED F/OS SEATBELT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,939 hrs · 13,274 cycles

ALL EMERGENCY LIGHTS IN FWD SECTION OF CABIN FAILED TO STAY ON. (FLT 5607) REPLACED NR 1 EMERGENCY BATTERY PACK AND CHARGING ASSEMBLY.

Part: SIGN — INOPERATIVE (CABIN) · airframe 21,738 hrs · 13,156 cycles

EMERGENCY SIGN TO THE LEFT OF SERVICE DOOR BURNT OUT. (FLT 5540) RELAMPED EMERGENCY SIGN.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 20,946 hrs · 12,692 cycles

GALLEY EMERGENCY EXIT SIGN HAS A LIGHT OUT. (FLT 6248) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,443 hrs · 12,402 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5464) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,274 hrs · 12,309 cycles

NR 3 OVERHEAD EMERGENCY LIGHT INOPERATIVE. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 20,204 hrs · 12,279 cycles

EMERGENCY EXIT SIGN AT MAIN CABIN DOOR HAS 1 BULB OUT. (FLT 6344) RELAMPED EXIT SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,972 hrs · 12,142 cycles

NR 5 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5525) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,972 hrs · 12,142 cycles

NR 6 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4728) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,840 hrs · 12,077 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6254) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,755 hrs · 12,027 cycles

NR 5 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5180) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,570 hrs · 11,927 cycles

SECOND TO LAST OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,434 hrs · 11,864 cycles

OVERHEAD AFT EMERGENCY LIGHT IS OUT. (FLT 6300) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,242 hrs · 11,740 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 15 IS OUT. (FLT 5292) RELAMPED EMERGENCY LIGHT.

Part: PUMP — LEAKING (NR 1 ENGINE) · airframe 18,830 hrs · 11,515 cycles

HYD 1 LO PRESSURE IN FLIGHT WITH QUANTITY AT 0 PERCENT. (FLT 5392) REPLACED NR 1 EDP, SERVICED NR 1 HYDRAULICS SYSTEM. REPLACED ALL 4 SYSTEM 1 HYDRAULIC FILTERS. P/N 66190-05 S/N OFF S/N K1290.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,606 hrs · 11,399 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5428) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,492 hrs · 11,339 cycles

AFT CEILING EMERGENCY LIGHT IS OUT. (FLT 5422) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,343 hrs · 11,261 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,251 hrs · 11,212 cycles

NR 4 CEILING EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,463 hrs · 10,793 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6222) RELAMPED EMERGENCY LIGHT.

Part: BALLAST — FAILED (CABIN) · airframe 17,028 hrs · 10,557 cycles

ELECTRICAL SMELL FROM ROW 2 AREA. (FLT 6876) REPLACED SIDEWALL AND CEILING LIGHT BALLAST ASSEMBLIES AT ROW 3.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 17,009 hrs · 10,547 cycles

ELECTRICAL BURNING SMELL NEAR ROW 2-3. (FLT 6539) REPLACED CABIN LIGHTING BALLAST AT ROW 2.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 15,560 hrs · 9,698 cycles

FS 280 FLOORBEAM CRACKED. (C-CHECK) REPAIR PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,374 hrs · 9,588 cycles

EMERGENCY LIGHT AT ROW 7 IS INOPERATIVE. (FLT 6155) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 14,882 hrs · 9,291 cycles

THE FLOOR LEVEL EMERGENCY EXIT SIGN ON A/C LEFT HAS 1 BULB OUT. (FLT 6160) RELAMPED FLOOR LEVEL EMERGENCY EXIT SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,475 hrs · 9,055 cycles

NR 4 EMERGENCY CEILING LIGHT INOP. (FLT 6470) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,407 hrs · 9,012 cycles

NR 3 EMERGENCY CEILING LIGHT INOP. (FLT 6431) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 13,882 hrs · 8,689 cycles

NR 1 CABIN FLOODLIGHT INOP. (FLT 5904) OPERATIONAL CHECKS NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 13,578 hrs · 8,496 cycles

FLOOR LEVEL EMERGENCY LIGHT AT SERVICE DOOR BROKEN. (SVC CHECK) REPLACED LIGHT ASSEMBLY.

Part: TRIM SWITCH — OUT OF ADJUST (RUDDER) · airframe 13,235 hrs · 8,293 cycles

ON GROUND, ACTIVATED RUDDER TRIM TO RIGHT, TRIM RAN FULL RIGHT UNCOMMANDED. (FLT 6566) RE-GAPPED RUDDER TRIM SWITCH INSTALLATION.

Part: SIGN — INOPERATIVE (CABIN) · airframe 13,113 hrs · 8,209 cycles

EXIT SIGN AT MAIN CABIN DOOR INOP. RELAMPED EXIT SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,969 hrs · 8,120 cycles

FLT 6352 - NR 1 EMERGENCY EXIT LIGHT INOP. RELAMPED.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 11,444 hrs · 7,210 cycles

PASSENGER DOOR INTERCOSTAL CRACKED. (C CHECK) REPAIRED PER SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 11,444 hrs · 7,210 cycles

FS280 CORRODED. (C CHECK)REPAIRED PER REO.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 10,408 hrs · 6,590 cycles

FLT 6592 - NR 1 EMERGENCY LIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 10,080 hrs · 6,398 cycles

FLT 5812 - ONE OVERHEAD EMERGENCY FLOODLIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 9,671 hrs · 6,171 cycles

FLT 6669 - SECOND TO LAST OVERHEAD EMERGENCY LIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 9,144 hrs · 5,858 cycles

FLT 6366 - FORWARD CEILING EMERGENCY FLOOD LIGHT OUT. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,057 hrs · 5,806 cycles

NEXT TO LAST CEILING EMERGENCY FLOODLIGHT INOP (FLT 6452). RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 8,008 hrs · 5,164 cycles

LAST OVERHEAD EMERGENCY LIGHT ON CEILING IS INOP. (FLT 6502) RELAMPED AFT EMERGENCY DOME LIGHT IAW AMM 33-51-00. OPS CHECK GOOD AT THIS TIME.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 7,605 hrs · 4,940 cycles

NR 3 OVERHEAD POD EMERGENCY LIGHT IS INOP. SECURED WIRING CONNECTION ON LIGHT ASSEMBLY. OPS CHECK GOOD.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 7,567 hrs · 4,920 cycles

FS 280 FLOORBEAM IS CRACKED, FOUND AT C-CHECK. REPLACED WITH NEW FS280 FLOORBEAM PER REO670-53-11-047.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 7,567 hrs · 4,920 cycles

FS 280 COCKPIT FLOORBEAM IS CORRODED, FOUND AT C-CHECK. COMPLIED WITH FLOORBEAM REPAIRS PER CRJ700/900 SRM 51-42-07 PG 10.

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 1) · airframe 6,393 hrs · 4,195 cycles

FLT 6274 - O2 MASKS DROPPED ON RIGHT SIDE OF ROW 1. SECURED RIGHT SIDE O2 MASKS IAW MM 35-21-05. OPS CHECK GOOD AT THIS TIME.

Part: CONTACT — DIRTY (EMERGENCY LIGHTS) · airframe 4,720 hrs · 3,105 cycles

OVERHEAD EMERGENCY FLOOD LIGHT BY LAV IS INOP. CLEANED CONTACTS ON EMERGENCY LIGHT. OPS CHECK GOOD.

Part: WEB — CRACKED (PAX DOOR) · airframe 3,960 hrs · 2,618 cycles

PAX DOOR AFT WEB TOP STEP AND MIDSTEP RADIUS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. COMPLIED WITH REO 670-52-11-104.

Part: WEB — CRACKED (PAX DOOR) · airframe 3,960 hrs · 2,618 cycles

PAX DOORS FWD WEB 2ND & 3RD TOP STEP RADIUS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER PER 670-52-11-104 IN CONJUNCTION WITH DEVIATION REO 670-52-11-252.

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 2,574 hrs · 1,681 cycles

AT 3,000' MSL INITIALLY GOT "CABIN ALT" CAUTION FOLLOWED BY "CABIN ALT WARNING" AND THE DEPLOYMENT OF THE O2 MASKS. REPLACED CABIN PRESSURE CONTROL PANEL IAW CRJ 700/400 MM 21-33-01. OPERATIONAL CHECKS GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 1,270 hrs · 808 cycles

PITCH FEEL FAULT STATUS MSG ON EICAS. REPLACED NR 2 SSCU IAW CRJ MM 27-61-05. OPERATIONAL CHECK GOOD.