N912EV

Part: WINDSHIELD — CRACKED (LEFT WINDSHIELD) · airframe 44,189 hrs · 40,558 cycles

TRANSFER FROM EAML 1494907 : LEFT WINDSHIELD CRACKED AND GOT L WSHLD HEAT CAUTION IN FLIGHT. (FLIGHT 5213 - FILED CLOSED) REMOVED AND REPLACED LH WINDSHIELD IN ACCORDANCE WITH AMMM:56-11-01 AND TASK CARD:56-220-1000-SKY. OPS CHECKS AND LEAKS CHEKS GOOD AT THIS TIME. CALIBRATED TOOLING:TORQUE DRIVER S/N# 1017401785 CAL DUE DATE: 10/31/2025TORQUE WRENCH S/N# 1121732223 CAL DUE DATE: 03/31/2025

Part: SKIN — DAMAGED (ZONE 500) · airframe 43,982 hrs · 40,341 cycles

LIGHTNING STRIKE FOUND ON L/H AILERON TRAILING EDGE (FILED CLOSED) COMPLIED WITH TEMPORARY REPAIR FOR LIGHTNING STRIKE DAMAGES FOUND ON LH AILERON TRAILING EDGE PER REO 601R-57-61-862 REV-- DATED 2024-08-09. REFERENCE CHILD CAMPS FOR EDDY CURRENT AND CONDUCTIVITY TESTS. TEMPORARY REPAIR REQUIRES VISUAL REINSPECT EVERY 150 FH. PERMANENT REPAIR DUE IN 3100 FH AT 46,598.70 TAT. COMPLIED WITH 51-900-1003-SKYAND COMPLETED M-337.

Part: SKIN — DAMAGED (LT AILERON) · airframe 43,509 hrs · 39,856 cycles

LIGHTNING STRIKE FOUND ON L/H AILERON TRAILING EDGE (FILED OPEN) COMPLIED WITH TEMPORARY REPAIR FOR LIGHTNING STRIKE DAMAGES FOUND ON LH AILERON TRAILING EDGE PER REO 601R-57-61-862 REV-- DATED 2024-08-09. REFERENCE CHILD CAMPS FOR EDDY CURRENT AND CONDUCTIVITY TESTS. TEMPORARY REPAIR REQUIRES VISUAL REINSPECT EVERY 150 FH. PERMANENT REPAIR DUE IN 3100 FH AT 46,598.70 TAT. COMPLIED WITH 51-900-1003-SKYAND COMPLETED M-337.

Part: SKIN — DAMAGED (LT AILERON) · airframe 43,982 hrs · 40,341 cycles

LIGHTNING STRIKE FOUND ON L/H AILERON TRAILING EDGE (FILED CLOSED) COMPLIED WITH TEMPORARY REPAIR FOR LIGHTNING STRIKE DAMAGES FOUND ON LH AILERON TRAILING EDGE PER REO 601R-57-61-862 REV-- DATED 2024-08-09. REFERENCE CHILD CAMPS FOR EDDY CURRENT AND CONDUCTIVITY TESTS. TEMPORARY REPAIR REQUIRES VISUAL REINSPECT EVERY 150 FH. PERMANENT REPAIR DUE IN 3100 FH AT 46,598.70 TAT. COMPLIED WITH 51-900-1003-SKYAND COMPLETED M-337.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

LBL27 FLOORBEAM BETWEEN FS559+112 AND FS621 FOUND TO BE CORRODED. (C-CHECK RO 9/28/2022) INSTALLED NEW SERVICEABLE LBL27 FLOORBEAM BETWEEN FS559+112 AND FS621 IAW CRJ 200 SRM 51-42-21AND 51-40-11. COMPLETED MAJOR STRUCTURAL REPAIR SKYCARD 51-900-1003-SKY AND COMPLETED M-337 FORM ATTACHED. PART FOR PART REPLACEMENT, NO WEIGHT CHANGE. REFERENCE CONTINUE CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

FOUND PAX DOOR LOWER AFT CORNER SEAL RETAINER TO BE CORRODED AND CRACKED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED SEAL RETAINER IAW CRJ200 SRM 51-42-06. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

FOUND CORROSION ON MOUNTING PLATE AT GROUND AIR CONDITION CONNECTION AT FS 574.00 AND FS 589.00 BETWEEN STR 22R AND STR24R (C-CHECK RO 9/28/2022) REMOVED OLD AND INSTALLED NEW MOUNTING PLATE AT GROUND AIR CONDITION CONNECTIOC AT FS 574.00 AND FS 589.00 BETWEEN STR22R AND STR24R IAW CRJ 200 SRM 51-42-06 & CRJ 200 SRM 51-42-21. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

AVI BAY DOOR SEAL RETAINERS (4EA) FOUND TO BE CORRODED OUT OF LIMITS. REPLACEMENT REQUIRED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED AVI BAY DOOR SEAL RETAINERS (4EA) IAW CRJ 200 SRM 51-42-06 REV 39 DATED 10 MAR 2022. MAJOR REPAIR TASK CARD 51-900-1003-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

FOUND PAX DOOR INTERCOSTAL DD6 AFT SIDE TO BE CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PA.X DOOR INTERCOSTAL DD6 IAW CRJ200 SRM 51-42-06. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

AVI DOOR INTERCOSTAL FROM F.S. 349.00 TO F.S. 364.00 BETWEEN STGR 27R AND STGR 26R IS CORRODED (C-CHECK RO 9/28/2022) INSTALLED NEW SERVICEABLE INTERCOSTAL IAW CRJ 200 SRM 51-42-06 & CRJ 200 SRM 51-42-21.COMPLETED SKY CARD 51-900-1003-SKY AND COMPLETED M-337 FORM ATTACHED. PART FOR PART REPLACEMENT ,NO WEIGHT CHANGE. REFERENCE CONTINUE CARD FOR WORK PERFORMED.

Part: NONE — CRACKED · airframe 40,579 hrs · 36,907 cycles

STRINGER 3L IS CRACKED FWDD OF FS 379.00. (C-CHECK RO 9/28/2022) REPAIRED STR 3L IAW CRJ200 SRM 53-00-03 STRINGERS - SPLICE REPAIRS. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

LBL 9 FLOOR BEAM HAS CORROSION DAMAGE BETWEEN F.S.409.00+80 - F.S.409.00+96 (C-CHECK RO 9/28/2022) REPAIRED CORROSION AT LBL9 BETWEEN F.S.409.00+80 - F.S.409.00+96LBL 9 FLOOR BEAM IAW CRJ 200 SRM 53-00-43. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CRACKED · airframe 40,579 hrs · 36,907 cycles

OUTBD FLOORBEAM WEB AT RBL9 BETWEEN FS409+32 AND FS409+48 FOUND TO BE CRACKED. REPLACEMENT REQUIRED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED OUTBD FLOORBEAM WEB AT RBL9 BETWEEN FS409+32 AND FS409+48 WITH NEW SERVICEABLE PART IAW CRJ 200 SRM 51-42-06 AND 51-42-21. MAJOR REPAIR TASK CARD 51-900-1003-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

FOUND PAX DOOR FWD FORMER TO BE HEAVLY CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED FWD FORMER ON PAX DOOR IAW CRJ 200 SRM 51-42-06 AND 51-42-21REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPLETED M-337 FORM ATTACHED. NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

FOUND PAX DOOR INTERCOSTAL DD1A AFT SIDE TO BE CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD1A IAW CRJ 200 SRM 51-42-06. REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPLETED M-337 FORM ATTACHED. NO WEIGHT CHANGE

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

FOUND PAX DOOR INTERCOSTAL DD5 AFT TO BE CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD5 IAW CRJ 200 SRM 51-42-06 .REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPLETED M-337 FORM ATTACHED. NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

FOUND PAX DOOR FWD FORMER BETWEEN DD4-DD5 TO BE CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR FWD FORMER BETWEEN DD4-DD5 IAW CRJ 200 SRM 51-42-06. REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPLETED M-337 FORM ATTACHED. NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

FOUND PAX DOOR INTERCOSTAL DD1 AFT TO BE CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD1 IAW CRJ 200 SRM 51-42-06.REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPLETED M-337 FORM ATTACHED. NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

FOUND PAX DOOR INTERCOSTAL DD7 MID TO BE CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD7 IAW CRJ 200 SRM 51-42-06.REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPLETED M-337 FORM ATTACHED. NO WEIGHT CHANGE.

Part: NONE — CRACKED · airframe 40,579 hrs · 36,907 cycles

INBD FLOORBEAM WEB AT RBL9 BETWEEN FS409+32 AND FS409+48 FOUND TO BE CRACKED. REPLACEMENT REQUIRED. (C-CHECK RO 9/28/2022) INSTALLED NEW SERVICABLE FLOOR BEAM WEB IAW CRJ 200 SRM 51-40-11, 51-42-21, 51-42-06. COMPLETED SKY CARD 51--900-1003 SKY AND COMPLETED M-337 FORM ATTACHED. PART FOR PART, NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

FOUND PAX DOOR INTERCOSTAL DD2 AFT TO BE CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD2 IAW CRJ 200 SRM 51-42-06. REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPLETED M-337 FORM ATTACHED. NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

AVIONICS DOOR INNER AFT EDGE ANGLE IS CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED AVI DOOR INNER AFT EDGE ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-21 REV39 DATED 3/10/2021.MAJOR REPAIR TASK CARD 51-900-103-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

AVIONICS DOOR INNER FWD EDGE ANGLE IS CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED AVIONICS DOOR INNER FWD EDGE ANGLE IAW CRJ200 SRM 51-42-06.REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPLETED M-337 FORM ATTACHED. NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

CAP ANGLE AT F.S.409.00 IS CORRODED FROM STR26.5L TO 26.5R ON BOTH FWD AND AFT ATTACHING FLANGES. (C-CHECK RO 9/28/2022) / COMPLIED WITH MHIRJ REO 601R-53-21-3563 REV. -- DATED 2022-08-16. REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPLETED M-337 FORM ATTACHED. NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

F.S.409.00 AFT LOWER SPLICE ANGLE AT STR 27 IS CORRODED. (C-CHECK RO 9/28/2022) / REMOVED AND REPLACED THE F.S 409.00 AFT LOWER SPLICE ANGLE PN:601R32200-17 IAW CRJ-200 SRM 51-42-06 AND 51-42-21.REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPLETED M-337 FORM ATTACHED. NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

AVIONICS DOOR INNER UPPER EDGE ANGLE IS CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED AVIONICS DOOR INNER UPPER EDGE ANGLE IAW CRJ 200 SRM 51-42-06. REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPLETED M-337 FORM ATTACHED. NO WEIGHT CHANGE.

Part: NONE — CRACKED · airframe 40,579 hrs · 36,907 cycles

FS589 FRAME FROM STGR20L TO STGR17L IS CRACKED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED FS. 589 FRAME FROM STGR 20L TO 17L IAW CRJ 200 SRM 51-42-06, 51-42-21 AND 51-40-11 COMPLETED SKY CARD 51-900-1003 AND COMPLETED M-337 FORM ATTACHED. REFERENCE CONTINUE CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

AVIONICS DOOR INNER LOWER EDGE ANGLE IS CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED AVIONICS DOOR INNER LOWER EDGE ANGLE IAW CRJ200 SRM 51-42-06 AND 51-42-21. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

PAX DOOR,INTERCOSTAL DD4 IS CORRODED BETWEEN F.S20.163 -F.S327.763. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED DOOR INTERCOSTAL DD4 IAW CRJ 200 SRM 51-42-06, 51-42-21.REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPLETED M-337 FORM ATTACHED. NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

INTERSOSTAL BETWEEN FS349 AND FS364 BETWEEN STGR16L AND STGR17L. IS CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED WITH NEW INTERCOSTAL BETWEEN FS349 AND FS364 BETWEEN STGR16L AND STGR17L IAW CRJ200 SRM 51-42-06 AND 51-42-21. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

INTERCOSTAL BETWEEN FS295 AND FS310 BETWEEN STGR15L AND STGR16L IS CORRODED. (C-CHECK RO 9/28/2022) REPLACED INSTALLED INTERCOSTAL AT FS 295 - FS310 BETWEEN STGR15L - STGR16L PN# 601R31109-15 IAW CRJ200 SRM 51-42-06 AND 51-42-21. REFERENCE CONTINUE CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

PAX DOOR, INTERCOSTAL DD4 IS CORRODED BETWEEN F.S311.75 -F.S320.163. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD4 IAW CRJ 200 SRM 51-42-06.REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPLETED M-337 FORM ATTACHED. NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

PAX DOOR , INTERCOSTAL DD3 IS CORRODED BETWEEN F S 338.963 -F S 347.25 (C-CHECK RO 9/28/2022) REMOVED AND REPLACED THE PAX DOOR INTERCOSTAL DD3 IAW CRJ 200 SRM 51-42-06. REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPLETED M-337 FORM ATTACHED. NO WEIGHT CHANGE.

Part: NONE — GOUGED · airframe 40,579 hrs · 36,907 cycles

PAX DOOR FUSELAGE FWD CAM FITTING IS GOUGED. (C-CHECK RO 9/28/2022) REPLACED PAX DOOR FUSELAGE FWD CAM FITTING IAW CRJ200 SRM 51-42-21. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

PAX DOOR, INTERCOSTAL DD5 IS CORRODED BETWEEN F.S311.75 -F.S320.163. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD5 IAW CRJ 200 SRM 51-42-06 .REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPLETED M-337 FORM ATTACHED. NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

PAX DOOR , INTERCOSTAL DD4 IS CORRODED BETWEEN F.S338.963- F.S 347.25. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD4 IAW CRJ 200 SRM 51-42-06. REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPLETED M-337 FORM ATTACHED. NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

PAX DOOR ,INTERCOSTAL DD6 IS CORRODED BETWEEN F.S 320.163 -F.S327.763. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED INTERCOSTAL DD6 IAW CRJ200 SRM 51-42-06 AND 51-42-21. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

PAX DOOR , INTERCOSTAL DD3 IS CORRODED BETWEEN F.S 320.163- FS327.763. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD3 IAW CRJ 200 SRM 51-42-06, 51-42-21.REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPLETED M-337 FORM ATTACHED. NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

PAX DOOR ,INTERCOSTAL DD6 IS CORRODED BETWEEN F.S 311.75 - F.S 320.163. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED INTERCOSTAL DD6 IAW CRJ200 SRM 51-42-06. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

PAX DOOR , INTERCOSTAL DD2 IS CORRODED BETWEEN F S 320.163 -F S 327.763. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR FRAME IAW CRJ 200 SRM 51-42-06, 51-42-21REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPLETED M-337 FORM ATTACHED. NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

FS 589 FRAME SUPPORT ANGLE CORRODED BETWEEN STR 20R AND STR 20L (C-CHECK RO 9/28/2022) REMOVED AND REPLACED NEW SERVICEABLE FS 589.00 FRAME SUPPORT ANGLE IAW CRJ 200 SRM 51-42-06 & CRJ 200 SRM 51-42-21. REFERENCE CONTINUE CARD FOR WORK PERFORMED .

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

PAX DOOR , INTERCOSTAL DD3 IS CORRODED BETWEEN F.S311.75- F.S 320.163. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD3 IAW CRJ 200 SRM 51-42-06. REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPLETED M-337 FORM ATTACHED. NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

FS319 FRAME IS CORRODED BETWEEN STGR18L AND STGR21L. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED FS319 FRAME P/N: 601R32003-63 IAW CRJ 200 SRM 51-42-06 AND 51-42-21 REV 39 DATED 10 MAR 2022. MAJOR REPAIR TASK CARD 51-900-1003-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGTH CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

LH FLOOR SILL IS CORRODED ON TOP AND BOTTOM SURFACE BETWEEN FS349 AND FS409. (C-CHECK RO 9/28/2022) REPAIRED LH FLOOR SILL TOP AND BOTTOM SURFACE BETWEEN FS349 AND FS409. IAW MHIRJ REO 601R-53-21-3564 REV -- DATED 2022-09-08 COMPLETED SYY TRACK TASK CARD 51-900-1003-SKY AND FORM 337 NO WEIGHT CHANGE.REFERENCE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CRACKED · airframe 40,579 hrs · 36,907 cycles

FS280 FLOOR BEAM ANGLE AT RBL9 IS CRACKED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED FS 280, RBL 9, OUTBOARD CLIP IAW CRJ 200 SRM 51-42-21

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

STGR21L INTERCOSTAL BETWEEN FS333 AND FS349 IS CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED STGR21L INTERCOSTAL BETWEEN FS333 AND FS349 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. MAJOR REPAIR TASK CARD 51-900-1003-SKY AND FORM M-337 COMPLETED AND ATTACHED NO WEIGHT CHANGE NOTED. REF CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

PAX DOOR SILL LOWER FLOOR SUPPORT ATTACH ANGLE IS CORRODED. (C-CHECK RO 9/28/2022) PAX DOOR SILL LOWER ATTACH ANGLE FOUND TO BE OUT OF LIMITS IAW CRJ 200 SRM 53-00-00 DUE TO THE AMOUNT OF CORROSION ANGLE REQUIRES REPLACEMENT. REMOVED PAX DOOR UPPER SILL ATTACH ANGLE FOR ACCESS IAW CRJ 200 SRM 51-42-06 AND REINSTALLED PAX DOOR UPPER SILL ATTACH ANGLE IAW CRJ200 SRM 51-42-0 REMOVED PAX DOOR SILL LOWER FLOOR SUPPORT ATTACH ANGLE IAW CRJ200 SRM 51-42-06 AND 51-42-21. INSTALLED PAX DOOR SILL LOWER FLOOR SUPPORT ATTACH ANGLE IAW CRJ200 SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED, AND DEBURRED NEW LOWER FLOOR SUPPORT ATTACH ANGLE PN# 601R31527-221S IAW CRJ200 SRM 51-40-11. OPS CHECKS GOOD. REFERENCE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

STGR21L INTERCOSTAL BETWEEN FS310 AND FS319 IS CORRODED. (C-CHECK RO 9/28/2022) INSTALLED NEW SERVICABLE INTERCOSTAL PN:601R-31527-19 IAW CRJ-200 SRM 51-42-06 AND 51-42-21.COMPLETED SKYWEST MAJOR REPAIR SKY CARD 51-900-1003-SKY AND M-337 FORM ATTACHED. PART FOR PART REPLACEMENT NO WEIGHT CHANGE. REFERENCE CONTINUE CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

STGR21L INTERCOSTAL BETWEEN FS319 AND FS333 IS CORRODED. (C-CHECK RO 9/28/2022) UPON FURTHER INVESTIGATION. FOUND DISCREPENT INTERCOSTAL RUNS FROM F.S.310 TO F.S.333. REFERENCE JOB:9772895 OP:89 FOR REPLACEMENT OF INTERCOSTAL.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

AVI DOOR INTERCOSTAL IS CORRODED BETWEEN STGR 27 TO STGR 26L. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED INTERCOSTAL IAW CRJ200 SRM 51-42-06 AND 51-42-21. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

RH FLOOR SILL PLATE IS CORRDED BETWEEN FS529 AND FS544 (C-CHECK RO 9/28/2022) REPAIRED RH FLOOR SILL IAW REO 601R-53-41-0666 REV. C, DATED 2012-11-06. MAJOR REPAIR TASK CARD 51-900-1003-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

LBL 9 FLOOR BEAM IS CORRODE BETWEEN TWO DIFFERENT LOCATIONS FIRST IS AT F.S. 409 AND THE SECOND IS AT 409+48 TO F.S. 409+64. (C-CHECK RO 9/28/2022) REPAIRED LBL 9 FLOORBEAM IAW CRJ200 SRM 53-00-43 REPAIR #2. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

RBL9 FLOOR BEAM IS CORRODED BETWEEN TWO LOCATIONS FIRST IS BETWEEN F.S. 409+16 TO 409+32 THE SECOND IS 409 TO F.S. 409+16. (C-CHECK RO 9/28/2022) REPAIRED RBL 9 FLOORBEAM IAW CRJ200 SRM 53-00-43 REPAIR #2. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

FS559 TENSION STRAPS, LH AND RH SIDE BETWEEN LBL AND RBL 27-45 ARE CORRODED (C-CHECK RO 9/28/2022) REMOVED AND REPLACED FS559 TENSION STRAPS IAW CRJ200 SRM 51-42-06 AND 51-42-22. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

FRAME FS 574.0 HAS CORROSION BETWEEN STGR 24R AND 24L (C-CHECK RO 9/28/2022) REMOVED AND REPLACED FRAME AT FS574 BETWEEN STR 24R AND 24L IAW CRJ200 SRM 51-42-06 AND 51-42-21. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

CARGO DOOR SILL IS CORRODED (C-CHECK RO 9/28/2022) INSTALLED NEW SERVICEABLE CARGO DOOR SILL IAW CRJ200 SRM 51-42-06, 51-42-13 & 51-42-21. REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR TASK CARD 51-900-1003-SKY AND COMPLETED M-337 FORM ATTACHED. NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

FRAME AT FS 605.0 HAS CORROSION FROM STGR 24R TO 20L (C-CHECK RO 9/28/2022) INSTALLED NEW F.S 605.0 FRAME IAW CRJ 200 SRM 51-42-06 & CRJ 200 SRM 51-42-21. REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-1003- SKY AND COMPLETED M-337 FORM ATTCHED. PART FOR PART REPLACEMENT, NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

FRAME AT FS 589.0 HAS CORROSION BETWEEN STGR 22R AND 20L (C-CHECK RO 9/28/2022) REMOVED AND REPLACED FRAME AT FS 589.0 BETWEEN STGR 22R AND 20L IAW CRJ200 SRM 51-42-06 AND 51-42-21. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 40,579 hrs · 36,907 cycles

INSIDE MAINTENANCE DOOR 172BR FOUND INTERCOSTAL JUST AFT F.S. 574, BETWEEN STGR 22R-24R CORRODED (C-CHECK RO 9/28/2022) UPON FURTHER EVALUATION, FOUND THE PART IN QUESTION TO BE AN ANGLE ATTACHING TO THE AFT SIDE OF F.S.574.00. NOT AN INTERCOSTAL. ANGLE IS CORRODED OUT OF LIMITS IAW CRJ-200 SRM 53-00-00 DUE TO CORROSION ACROSS MULTIPLE ELEMENTS AND AREA OF CORROSION. LOCATED AND DRILLED NEW UPPER ANGLE PN# 601R35226-31 PO# W88262 AND LOWER ANGLE PN# 601R35226-35 PO# W88262 IAW CRJ 200 SRM 51-40-11. INSTALLED NEW UPPER AND LOWER ANGLE IAW CRJ 200 SRM 51-42-06. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — DENTED · airframe 40,579 hrs · 36,907 cycles

EXTERNAL FUSELAGE SKIN HAS 2EA DENTS ON THE UPPER SKIN PANEL BETWEEN FS 654.50 - FS 672.20, STR 4L - STR 6L. (C-CHECK RO 9/28/2022) FOUND THE 2EA DENTS ON THE UPPER SKIN PANEL BETWEEN FS 654.50 - FS 672.20, STR 4L - STR 6L TO BE OUT OF LIMITS PER CRJ-200 SRM 53-61-31 AND 53-00-31. REPAIR REQUIRED. REPAIRED IAW MHIRJ REO 601R-53-61-7873 REV. -- DATED 2022-09-06. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY AND FORM 337. NO WEIGHT CHANGE. REFERENCE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CHAFED · airframe 40,579 hrs · 36,907 cycles

L/H I/B FLAP FLAP VANE CHAFED AT FLS 56-57 APPROX 1.25 L X .5 WIDE (C-CHECK RO 9/28/2022) REMOVED AND REPLACED LEADING EDGE SKIN IAW CRJ200 SRM 51-42-13. ATTACHED SKYCARD 51-900-1003-SKY AND FORM M-337. REF CONTINUATION CARD FOR WORK PERFORMED

Part: NONE — CHAFED · airframe 40,579 hrs · 36,907 cycles

L/H I/B FLAP FLAP VANE CHAFED AT FLS 104 TO 105 APPROX 1.25 L X .25 WIDE (C-CHECK RO 9/28/2022) REMOVED AND REPLACED L/E SKIN AT L/H I/B FLAP VANE IAW CRJ 200 SRM 51-42-13. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS ON WORK PERFORMED

Part: NONE — CHAFED · airframe 40,579 hrs · 36,907 cycles

R/H I/B FLAP - FLAP VANE CHAFED AT FLS 140-141 APPROX 1.25 L X .5 WIDE (C-CHECK RO 9/28/2022) REMOVED AND REPLACED R/H I/B FLAP VANE LEADING EDGE SKIN BETWEEN FLS 140 AND FLS 141 IAW CRJ 200 SRM 51-42-13 AND 51-40-11 . ATTACHED SKYCARD 51-900-1003-SKY AND FORM M-337 . REF CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CHAFED · airframe 40,579 hrs · 36,907 cycles

R/H I/B FLAP - FLAP VANE CHAFED AT FLS 56-57 APPROX 1.25 L X .5 WIDE (C-CHECK RO 9/28/2022) REMOVED AND REPLACED RH FLAP VANE LEADING EDGE SKIN BET. FLS 56 AND 57 IAW CRJ 200 / SRM 51-42-13 AND SRM 51-40-11

Part: NONE — CHAFED · airframe 40,579 hrs · 36,907 cycles

L/H I/B FLAP FLAP VANE CHAFED AT FLS 140-141 APPROX 1.25 L X .375 WIDE (C-CHECK RO 9/28/2022) REMOVED AND REPLACED LH INBD FLAP VANE L/E SKIN IAW CRJ200 SRM 51-42-13. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — DAMAGED · airframe 40,579 hrs · 36,907 cycles

TRANSFER FROM EAML 958906 : FOUND DAMAGE MCD AT THE PASSENGER DOOR PULLEY BRACKET ASSEMBLY (DWG: 601R317106, REF). THE FS349.00 FORMER WAS PREVIOUSLY REPAIRED PER REO 601R-52-11-2015 AND THE REPAIR ANGLE 601R-52-11-2015-3 IS TORN. FURTHER DAMAGE IS DEFORMATION TO THE RAIN GUTTER (P/N: 601R317079-1) (C-CHECK RO 9/28/2022) REMOVED AND REPLACED FS349 PAX DOOR FORMER IAW CRJ200 SRM 51-42-21 AND 51-42-06. REMOVED AND REPLACED RAIN GUTTER IAW CRJ200 SRM 51-42-06. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: WARNING MESSAGE — ILLUMINATED (MLG) · airframe 39,043 hrs · 35,556 cycles

***CAT II DOWNGRADED*** / D:GEAR DISAGREE WARNING MESSAGE DURING DECENT TO XWA, AFTER COMPLYING WITH THE QRH THE GEARS DROPPED NORMALLY. / C:MEL 32-30-1 / CAT "A" DUE 1 FLT DAY BY 09/11/2021 / MX ACTION COMPLIED WITH / GEAR DISAGREE WARNING MESSAGE DURING DECENT TO XWA, AFTER COMPLYING WITH THE QRH THE GEARS DROPPED NORMALLY. (FLIGHT 5359 - FILED CLOSED) SEP 10, 2021 STATION: XWA--DEFERRED LANDING GEAR RETRACTION SYSTEM PER MEL 32-30-1. MX ACTION COMPLIED WITH. AIRCRAFT OK FOR SERVICE. **CAT II DOWNGRADED**

Part: LANDING GEAR — STUCK (NOSE) · airframe 38,530 hrs · 35,094 cycles

D: GEAR DISAGREE AFTER TAKEOFF FROM CID WITH NOSE GEAR APPEARING STUCK DOWN AND GREEN. RAN QRH, GOT THREE GREEN AND LANDED UNEVENTFULLY. / C: MEL 32-30-1 / CAT A DUE 5/31/21 / **CAT II NOT AUTHORIZED** / GEAR DISAGREE AFTER TAKEOFF FROM CID WITH NOSE GEAR APPEARING STUCK DOWN AND GREEN. RAN QRH, GOT THREE GREEN AND LANDED UNEVENTFULLY. (FLIGHT 4649, FILED CLOSED) MAY 30, 2021 STATION: CID--DEFFERED LANDING GEAR RETRACTION SYSTEM PER CRJ 200 MEL 32-30-1. MX ACTIONS COMPLIED WITH AND PLACARDS INSTALLED. / ***CAT II NOT AUTHORIZED** / MAY 30, 2021 STATION: FWA -- SEE CAMP# 22879414 FOR NLG PROX SENSOR PS14GA BRACKET REPLACEMENT AND CAMP # 22879696 FOR HARNESS REPLACEMENT. / PERFORMED 3 COMPLETE LANDING GEAR EXTENSION AND RETRACTION CYCLES IN REFERENCE TO AMM 32-32-00 - OPS CHECK GOOD AT THIS TIME. / SEE CAMP # FOR CAT II RETURN TO SERVICE TASK CARD, AIRCRAFT UPGRADED TO CAT II STATUS / THIS CLEARS DMI, PLACARDS REMOVED

Part: RIB — CORRODED (LT WING) · airframe 35,933 hrs · 32,367 cycles

LT WING, FORWARD BATT RIB IS CORRODED AT THE BOTTOM. (C-CHECK) RO: 07/13/2019 REMOVED CORROSION ON LT WING FORWARD BATT RIB IAW SRM AND REO.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 35,933 hrs · 32,367 cycles

SERVICE DOOR SILL HAS MULTIPLE AREAS OF CORROSION. (C-CHECK) RO: 07/13/2019 REMOVED AND REPLACED SERVICE DOOR SILL IAW SRM.

Part: UNKNOWN — UNKNOWN (MLG INDICATOR) · airframe 35,699 hrs · 32,093 cycles

GEAR DISAGREE ON APPROACH. NOSE GEAR DID NOT SHOW GREEN. FOLLOWED QRH AND GEAR DID EXTEND PROPERLY TO SHOW 3 GREENS. (FLT#3886) CLEARED PSEU FAULTS. PERFORMED GVI ON NLG. NO DEFECTS NOTED. PERFORMED FUNCTIONAL TEST OF NLG EXTENSION AND RETRACTION IAW AMM. CAN NOT DUPLICATE FAULT AFTER MULTIPLE EXTENSION / RETRACTIONS. NLG FUNCTIONAL TEST GOOD AT THIS TIME.

Part: CONTROL PANEL — MALFUNCTIONED (ADG) · airframe 33,495 hrs · 29,598 cycles

ON ROTATION FELT LOUD VIBRATION. VIBRATION CONTINUED, RETURNED TO FIELD. REMOVED AND REPLACED ADG AUTO DEPLOY PANEL. OPS CHECKED GOOD. PERFORMED VISUAL INSPECTION IAW AMM. NO DEFECTS NOTED.

Part: OVERHEAT LOOP — FAILED (RT NACELLE) · airframe 32,986 hrs · 29,054 cycles

RT ENGINE 14TH STAGE DUCT WARNING MESSAGE CREW COMPLIED WITH QRH . DECLARED AN EMERGENCY. THE RT ENGINE PULLED BACK TO IDLE. REPLACED THE RT PYLON LOOP AND THE SYSTEM OPS CHECKED GOOD.

Part: TERMINAL — FAILED (WINDSHIELD) · airframe 31,646 hrs · 27,540 cycles

DURING CLIMB OUT, NOTICE A BAD ODOR. A FEW MINUTES LATER, SAW SMOKE FROM THE RT WINDSHIELD MAIN POWER ATTACHMENT BLOCK. DECLARED EMERGENCY & RETURNED TO FIELD. INSPECTED THE RT WINDSHIELD POWER WIRE TERMINALS FOUND ONE TERMINAL TO BE DEFECTIVE. INSTALLED TWO NEW RING TERMINALS IAW ESPM. OPS CHECKED GOOD.

Part: WARNING MESSAGE — ILLUMINATED (NOT REPORTED) · airframe 27,374 hrs · 23,197 cycles

FLIGHT RETURNED TO FIELD DUE TO AN UNCOMMANDED SPEED LOSS. INTERROGATED MDC AND FOUND FAULTS LOGGED AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 27,227 hrs · 23,035 cycles

F/A FLASHLIGHT INOPERATIVE. R & R THE F/A FLASHLIGHT BATTERY. OPS CHECKED GOOD IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,249 hrs · 22,055 cycles

NR 3 EMERGENCY CEILING LIGHT IS BURNED OUT. FLT 4676 RELAMPED.

Part: BULKHEAD — DENTED (FUSELAGE) · airframe 25,157 hrs · 20,964 cycles

FS 621 BULKHEAD RBL 5, APPROXIMATELY 56.5" ABOVE FLOOR HAS DENT THAT IS APPROXIMATELY 650" LONG X .500" WIDE X .170" DEEP. C-CHECK REPAIRED THE DENT ON FS 621 BULKHEAD RBL 5, APPROXIMATELY 56.5" ABOVE THE FLOOR IAW REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 25,157 hrs · 20,964 cycles

LT AILERON UPPER LE IS CHAFED FROM JUST INBD OF THE INBD HINGE TO THE OTBD EDGE OF THE AILERON. C-CHECK REPAIRED TOP SURFACE OF LT AILERON LE SKIN IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,157 hrs · 20,964 cycles

FS 621 BULKHEAD HAS CRACK AT RBL 27.50 APPROXIMATELY 6 INCHES ABOVE FLOOR. C-CHECK REPAIRED THE FS 621 BULKHEAD CRACK AT RBL 27.50 IAW REO.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 25,157 hrs · 20,964 cycles

CHAFE ON INBD END OF LT INBD FLAP VANE LE SKIN. C-CHECK REPAIRED LT INBD FLAP VANE LE INBD SECTION IAW REO.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 25,157 hrs · 20,964 cycles

CHAFE ON OTBD END OF LT INBD FLAP VANE LE SKIN. C-CHECK REPAIRED LT INBD FLAP VANE LE OTBD SECTION IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 25,157 hrs · 20,964 cycles

CHAFE ON RT INBD FLAP VANE OTBD LE SECTION. C-CHECK REPAIRED RT INBD FLAP VANE LE OTBD SECTION IAW REO.

Part: SKIN — CHAFED (TE FLAP) · airframe 25,157 hrs · 20,964 cycles

LT INBD FLAP LIGHT CHAFE ON UPPER SKIN DOUBLER UNDER PANEL 584BB. C-CHECK REPAIRED AREA UNDER INBD FLAP PANEL 584BB IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 25,157 hrs · 20,964 cycles

CHAFE ON RT INBD FLAP VANE INBD LE SECTION. C-CHECK REPAIRED RT INBD FLAP VANE LE INBD SECTION IAW REO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 25,157 hrs · 20,964 cycles

MAIN AVIONICS COMPARTMENT DOOR CUT-OUT HAS CORROSION ON THE INSIDE OF THE DOOR CUT-OUT SKIN, CORROSION IS EVIDENT ALL THE WAY AROUND THE SKIN. C-CHECK BLENDED OUT CORROSION ON THE MAIN AVIONICS BAY DOOR SURROUND INNER SKIN BETWEEN FS 364-FS 394 IAW REO.

Part: SKIN — CHAFED (TE FLAP) · airframe 25,157 hrs · 20,964 cycles

LT INBD FLAP CHAFING ON UPPER SKIN DOUBLER UNDER PANEL 584CB. C-CHECK REPAIRED AREA UNDER INBD FLAP PANEL IAW REO.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 25,157 hrs · 20,964 cycles

CHAFE ON MID AREA OF LT INBD FLAP VANE LE SKIN. C-CHECK REPAIRED LT INBD FLAP VANE LE MID SESCTION IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 25,157 hrs · 20,964 cycles

CHAFE ON RT INBD FLAP VANE MID LE SECTION. C-CHECK REPAIRED RT INBD FLAP VANE LE MID SECTION IAW REO.

Part: SKIN — CHAFED (TE FLAP) · airframe 25,157 hrs · 20,964 cycles

LT INBD FLAP CHAFE ON UPPER SKIN DOUBLER UNDER PANEL 584AB. C-CHECK REPAIRED AREA UNDER INBD FLAP PANEL 584AB IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,146 hrs · 20,954 cycles

OVERHEAD EMERGENCY LIGHT ABOVE ROW 13 IS BURNED OUT. FLT#4561 RELAMPED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,731 hrs · 20,563 cycles

EMERGENCY LIGHTS DO NOT ILLUMINATE. (FLT 4567) RECHARGED EMERGENCY BATTERIES.

Part: WIRE — BROKEN (CABIN) · airframe 24,367 hrs · 20,224 cycles

EMERGENCY FLOOR LEVEL FLOOD LIGHT BY MAIN CABIN DOOR DOES NOT ILLUMINATE. (FLT 4547) RE-PINNED AND CONNECTED BROKEN WIRE.

Part: MOUNT BOLT — GALLED (RT ENGINE) · airframe 23,632 hrs · 19,514 cycles

UPPER AND LOWER MOUNT BOLTS ON RIGHT ENGINE FORWARD MOUNT ARE SCARRED. (SERVICE) REPLACED UPPER AND LOWER PIN BOLTS IN REFERENCE TO REO.

Part: FUEL CONTROL — DEFECTIVE (APU) · airframe 23,551 hrs · 19,430 cycles

THE APU AUTO SHUTDOWN AND SMOKE CAME OUT OF THE INLET WITH HIGH SMELL OF FUEL. (FLT 4762) REPLACED FUEL CONTROL UNIT AND FUEL SOLENIOD IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,032 hrs · 18,926 cycles

NR 8 EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,032 hrs · 18,926 cycles

RIGHT SIDE AFT EMERGENCY EXIT OVERWING LIGHT AND LEFT SIDE FRONT EMERGENCY EXIT OVERWING LIGHT BURNED OUT. (FLT 4621) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,019 hrs · 18,912 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4623) RELAMPED EMERGENCY LIGHT.

Part: INVERTER — FAILED (CABIN) · airframe 23,019 hrs · 18,912 cycles

INTERIOR EMERGENCY LIGHT AT EMERGENCY EXIT IS OUT. (FLT 4522) REPLACED EMERGENCY BATTERY INVERTER NR 2 IN REFERENCE TO AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,467 hrs · 18,373 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4538) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,441 hrs · 18,345 cycles

FLT 4680, NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,256 hrs · 18,186 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 10-11 IS OUT. (FLT 4448) RELAMPED EMERGENCY LIGHT.

Part: TERMINAL BLOCK — DEFECTIVE (CABIN) · airframe 22,138 hrs · 18,068 cycles

THE 2ND FROM AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4656) REPLACED TERMINAL BLOCK 104-4 AND NR 3 EMERGENCY LIGHT BATTERY CHARGER FUSE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,978 hrs · 17,896 cycles

THE 2ND FROM AFT CEILING EMERGENCY LIGHT IS NOT WORKING. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,863 hrs · 17,780 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,746 hrs · 17,671 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4542) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,718 hrs · 17,647 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4540) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,682 hrs · 17,615 cycles

OVERHEAD EMERGENCY LIGHTS 2 & 4 ARE INOPERATIVE. (FLT 4594) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,659 hrs · 17,594 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4691) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,598 hrs · 17,532 cycles

NR 2 AND NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4756) RELAMPED EMERGENCY LIGHTS.

Part: CONTROL PANEL — FAILED (COCKPIT) · airframe 21,557 hrs · 17,490 cycles

LANDING GEAR WOULD NOT RETRACT. (FLT 4508) REPLACED LANDING GEAR CONTROL PANEL. P/N 74552-5 S/N 1104

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,554 hrs · 17,487 cycles

THE 2ND AND 4TH OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 7771) RELAMPED EMERGENCY LIGHT.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 21,509 hrs · 17,447 cycles

LEFT INBOARD FLAP VANE LEADING EDGE SKIN CHAFED. (C-CHECK) REPLACE LEFT INBOARD FLAP VANE LEADING EDGE SKIN PER REO.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,480 hrs · 17,422 cycles

RIGHT WING CENTER EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 4554) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,469 hrs · 17,412 cycles

NR 2 AND 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4493) RELAMPED EMERGENCY LIGHTS.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,428 hrs · 17,379 cycles

FS 202 PRESSURE BULKHEAD CRACKED AT BRAKE LINE. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,452 hrs · 18,357 cycles

CRACK AT FS 559.0 PRESSURE BULKHEAD TO LEFT SIDE. (C-CHECK) REPAIRED PER REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,452 hrs · 18,357 cycles

SURFACE CORROSION ON FLOORBEAM AT FS 590 LBL 27. (C-CHECK) REPLACED PER REO.

Part: SKIN — DENTED (FUSELAGE) · airframe 22,452 hrs · 18,357 cycles

DENT IN FUSELAGE 3 INCHES BELOW 1 INCH AFT CARGO DOOR OPENING. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,452 hrs · 18,357 cycles

CRACK INDICATION NOTED TO FS 559.0 PRESSURE BULKHEAD AT RIGHT SIDE. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,211 hrs · 17,189 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4630) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,787 hrs · 16,828 cycles

NR 2 CEILING EMERGENCY LIGHT IS OUT. (FLT 4494) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,695 hrs · 16,753 cycles

EMERGENCY LIGHT FORWARD OF MAIN CABIN DOOR EXTERNAL IS OUT. (FLT 4723)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,503 hrs · 16,596 cycles

EMERGENCY CEILING LIGHT 2ND FROM AFT IS OUT. (FLT 4719) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,065 hrs · 16,233 cycles

NR 2 CEILING EMERGENCY LIGHT INOPERATIVE. (FLT 4658) RELAMPED EMERGENCY LIGHT.

Part: MOUNT — CORRODED (LT ENGINE) · airframe 19,500 hrs · 15,746 cycles

ONE LEFT ENGINE FWD MOUNT PIN IS GALLED. (ENGINE CHANGE) INSTALLED SERVICEABLE MOUNT PIN AS REQUIRED.

Part: LINK ASSY — GALLED (ENGINE) · airframe 19,500 hrs · 15,746 cycles

LEFT ENGINE FORWARD YOKE LINK ASSEMBLY IS GALLED. (ENGINE CHANGE) REMOVED AND REPLACED LEFT ENGINE FORWARD YOKE LINK ASSEMBLY PER AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 17,793 hrs · 14,300 cycles

FLT 4508 - CABIN CEILING EMERGENCY FLOODLIGHT NR 3 INOP. RELAMPED.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 17,257 hrs · 13,876 cycles

AFT PORTION OF THE FLOOR EMERGENCY LIGHT STRIP INOP. (FLT 4809) RESEATED CONNECTOR.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,287 hrs · 13,898 cycles

FS 621 BULKHEAD CARGO TRACK FITTING CRACKED. (C CHECK) REPAIRED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 16,965 hrs · 13,638 cycles

FS 621 LINTEL FITTING CRACKED. (C CHECK) REPAIR IN PROGRESS PER REO.

Part: STRUCTURE — CRACKED (CARGO BAY) · airframe 16,965 hrs · 13,638 cycles

FS 621 BULKHEAD CARGO TRACK INTERFACE CRACKED. (C CHECK) REPAIR PER REO IN PROGRESS.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 16,974 hrs · 13,644 cycles

PASSENGER DOOR DRAG ANGLE CRACKED. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,925 hrs · 13,608 cycles

CEILING LEVEL EMERGENCY FLOODLIGHT INOP. (FLT 4717)RELAMPED.

Part: LIGHT — BROKEN (GALLEY) · airframe 16,536 hrs · 13,318 cycles

FLT 4704 - EMERGENCY FLOOD LIGHT IN GALLEY BROKEN. REPLACED LIGHT ASSEMBLY.

Part: SUPPORT BEAM — CRACKED (ENGINE) · airframe 16,473 hrs · 13,275 cycles

ENGINE SUPPORT BEAM CRACKED, SB COMPLIANCE. REPLACED CRACKED ANGLE PER SRM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 16,215 hrs · 13,070 cycles

FLT 4376 - LEFT SIDE VIEW FLIGHT DECK WINDOW CRACKED DURING DESCENT. REPLACED WINDOW.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,091 hrs · 12,976 cycles

FLT 4728 - AFT CEILING EMERGENCY LIGHT INOP. RELAMPED.

Part: QUICK DISCONNECT — DISCONNECTED (HYD SYSTEM) · airframe 15,271 hrs · 12,357 cycles

FLT 3981 - AFTER TAKEOFF "HYDRAULIC 1 LO PRESS" AND "HYD 1 EDP" CAUTION MESSAGES DISPLAYED. RECONNECTED NR 1 EDP QUICK CONNECT FITTING 'P' SAFETY FITTING.

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY) · airframe 13,546 hrs · 11,041 cycles

FORWARD CARGO SMOKE DETECTOR GIVES FALSE WARNING. REPLACED SMOKE DETECTOR IAW MM 26-15-00. OPS CHECK GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 13,451 hrs · 10,971 cycles

CARGO COMPARTMENT FRAME HAS SIGNS OF CORROSION UNDER FLOORBOARD 281LLF, FOUND AT C-CHECK. REMOVED MINOR CORROSION ON THE FRAME PER CRJ200 SRM 5-21-06 PG 1-4.

Part: BEARING — FAILED (LT AILERON LINK) · airframe 13,451 hrs · 10,971 cycles

LT AILERON INBD AND OTBD PCU LINK BEARINGS FAIL BACKLASH CHECK, FOUND AT C-CHECK. REPLACED LEFT AILERON INBOARD AND OUTBOARD PCU LINKS IAW CRJ200 AMM 27-14-15-000-801 AND 27-14-15-400-801.

Part: FRAME — CRACKED (BS 621) · airframe 13,451 hrs · 10,971 cycles

STA 621 LEFT OUTBOARD FRAME IS CRACKED, FOUND AT C-CHECK. REPLACED DAMAGED AREA OF FLOOR SUPPORT ANGLE AT STA 621.00 PER CRJ200 REO 601R-53-61-117 REV C.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,451 hrs · 10,971 cycles

FS 280 FLOOR SUPPORT BEAM IS CRACKED AT RBL9, FOUND AT C-CHECK. COMPLIED WITH REPAIR OF FLOOR SUPPORT BEAM PER CRJ200 REO 53-11-171 REV D SCHEME B.

Part: BEARING — WORN (AILERON LINK) · airframe 13,451 hrs · 10,971 cycles

RIGHT AILERON INBOARD AND OUTBOARD PCU LINK BEARINGS FAIL BACKLASH CHECK, FOUND AT C-CHECK. REPLACED AILERON PCU LINKS PER CRJ200 AMM 27-14-15-00-801/400-801.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,451 hrs · 10,971 cycles

FS 280 FLOOR SUPPORT BEAM IS CRACKED AT LBL 9, FOUND AT C-CHECK. COMPLIED WITH REPAIR OF FLOOR SUPPORT BEAM PER CRJ200 REO 53-11-171 REV D SCHEME B.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,451 hrs · 10,971 cycles

FS 280 FLOOR SUPPORT BEAM IS CRACKED AT LBL9, FOUND AT C-CHECK. REPAIRED DAMAGED SECTION OF FLOOR ANGLE AT STA 280 LBL9 IAW CRJ200 REO 601R-53-11-138 REV NC.

Part: BEARING — WORN (LT AILERON) · airframe 13,451 hrs · 10,971 cycles

LEFT AILERON HINGE BEARINGS ARE WORN, FOUND AT C-CHECK. REPLACED AILERON HINGE BEARINGS PER CRJ200 AMM TASK 20-26-00-910-810.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 8,800 hrs · 7,465 cycles

SERVICE DOOR EMERGENCY EXIT LIGHT INOP (EXTERIOR). REPLACED LAMP FOR SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT. OPERATIONAL CHECK GOOD. REF 37-51-21.

Part: TRIM SWITCH — INOPERATIVE (COCKPIT) · airframe 8,759 hrs · 7,434 cycles

FIRST OFFICER`S TRIM SWITCH DOESN'T WORK IN EITHER DIRECTION. REPLACED F/O'S STAB TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD.

Part: TRIM SWITCH — FAILED (COCKPIT) · airframe 8,672 hrs · 7,365 cycles

CAPT SIDE TRIM SWITCH FAILED ON APPROACH. REPLACED CAPTAINS STAB TRIM SWITCH REF AMM 27-41-05. OPERATIONAL CHECK GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,572 hrs · 7,291 cycles

FOUND FORWARD SECTION OF EMERGENCY LIGHTS INOP. REPLACED NR 2 EMERGENCY LIGHT INVERTER AND LIGHT POWER STRIP FROM ROW 1 TO ROW 6. OPERATIONAL CHECK GOOD.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 9,459 hrs · 7,970 cycles

ENGINE SUPPORT BEAM CRACKED AT FS 627 WL 111.09 LBL 37.5 COMING FROM FWD INBD CORNER OF LOWER ACCESS PANEL, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS TO ENGINE SUPPORT BEAM AT FS627; WL 111.09 LBL 37.5 FORWARD CORNER IAW CRJ 200 SRM 51-42-06 PP 11 AND 51-42-20 P 23.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 9,459 hrs · 7,970 cycles

FS 640 RT SIDE RE-INFORCEMENT ANGLE CRACKED AT STR 10, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW REINFORCEMENT ANGLE; SPLICE PART 601-37065-3 IAW CRJ200 SRM 51-42-06 PG 11-17 AND 51-42-21 PG 15-19.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 9,459 hrs · 7,970 cycles

FS 280 AT 9:00 INCH BL LT AND RT; INBD AND OTBD BRACKETS WHICH ATTACH CABIN SEAT RAIL BEAMS TO THE 280 FS ARE CRACKED TOTAL 4, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW BRACKETS; PN 601R31113-57 (2 EA) AND 601R3113-58 (2 EA) IAW CRJ200 SRM 51-42-21 PARA 5-10 & SRM 51-42-13 PARA 6-8. REFERENCE REO 601R-53-11-137 REV NC; REO 601R-53-11-138 REV NC; AND STANDARD REPAIR 601R-53-0057A.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 9,459 hrs · 7,970 cycles

ENGINE BEAM SUPPORT CRACKED AT FS 627 WL 111.09 RBL 37.5 COMING FROM FWD INBD CORNER OF LOWER ACCESS PANEL, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS (-1; -2; -3; -4; -6; & -7) TO ENGINE BEAM SUPPORT AT FS 627 WL 111.09 RBL 37.5 IAW CRJ200 SRM 51-42-06 PG 11 AND 51-42-20 PG 23.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 9,459 hrs · 7,970 cycles

BRACKET CRACKED ON LEFT SIDE AFT SIDE OF FS 621.0 APPROXIMATELY WL 90 (3RD STRINGER DOWN FROM ENG BEAM, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP; PN 601R-35012-51 PO 60148 ON LT FS 621 WL 90 IAW CRJ200 SRM 51-42-06 PG 11 AND SRM 51-40-11 PG 2-5.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 9,459 hrs · 7,970 cycles

BRACKET CRACKED ON RIGHT SIDE OF FS 621.0 APPROXIMATELY WL 90 3RD STRINGER DOWN FROM ENG BEAM, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP; PN 601R-35012-52 PO 58248 ON RT FS 621 WL 90 IAW CRJ200 SRM 51-42-06 PG 11 AND SRM 51-40-11 PG 2-5.

Part: RIB — CRACKED (RT WING) · airframe 9,459 hrs · 7,970 cycles

RIGHT WHEEL WELL BATT RIB IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLERS INBOARD AND OUTBOARD RIGHT SIDE AS PER REO 601R-57-51-046.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 8,313 hrs · 7,074 cycles

EMERGENCY FLOOR LIGHTS AT ROW 2 INOPERABLE. CLEANED CONNECTIONS AT POWER STRIP AND OPS CHECK NORMAL.

Part: ACM — MALFUNCTIONED (LEFT) · airframe 7,440 hrs · 6,339 cycles

FLIGHT 5263 - LEFT PACK HIGH PRESSURE CAUTION. CND, FOUND NO DEFECT WITH THE LT AC SYSTEM.

Part: LAMP — BURNED OUT (GALLEY)

DURING A GROUND INSPECTION, THE LOWER INTERIOR EMERGENCY LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LOWER INTERIOR EMERGENCY LIGHT BY THE SERVICE DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT CHECK, THE LT FORWARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LT FORWARD EMERGENCY LIGHT. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: SELECTOR VALVE — MALFUNCTIONED (NLG)

DURING CLIMB-OUT FROM ROC-ATL, UPON GEAR RETRACTION THE CREW RECEIVED A GEAR DOOR OPEN RED WARNING MESSAGE. ATTEMPTS TO RECYCLE THE GEAR WERE UNSUCCESSFUL. THE QRH WAS COMPLIED WITH AND THE AIRCRAFT RETURNED TO ROC. THE TOWER ROLLED THE EMERGENCY VEHICLES AS A PRECAUTION AND THE AIRCRAFT LANDED SAFELY IN ROC. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR NLG DOOR SELECTOR VALVE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ODOR — DETECTED (CABIN)

DURING DESCENT INTO DFW FROM MGM, AT APPROX 18,000 FT THE PAX REPORTED AN ODOR OF SMOKE IN CABIN AROUND ROWS 4 - 6 WITH NO VISIBLE SIGNS. QRH PROCEDURES WERE COMPLIED WITH & AN EMERGENCY LANDING MADE SAFELY INTO DFW. ODOR DISSIPATED APPROXIMATELY THREE MINUTES PRIOR TO LANDING WITH NO PASSENGER EVACUATION NECESSARY UPON LANDING. MX INSPECTED AVIONICS BAY, MLG BAYS, PROX SENSOR ELECTRONIC UNITS ON THE LT & RT SIDES & ACM WITH NO DEFECTS NOTED. PACKS AND APU WAS ALSO INSPECTED AND OPERATED WITH NO DEFECTS NOTED. MAINTENANCE SUSPECTS THE ODOR CAME FROM THE TEMP RISE IN THE PACKS WHEN SWITCHING FROM THE ENGINE TO THE AUXILIARY POWER UNIT. AIRCRAFT OK FOR SERVICE. (M)