N961SW

Part: WARNING MESSAGE — FALSE ACTIVATION (APU BAY) · airframe 46,954 hrs · 40,487 cycles

APU OVERTEMP WARNING ON DESCENT - COMPLETED QRH - NO FURTHER ACTION. (FLIGHT 5436 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28321232 WITH THE FOLLOWING CORRECTIVE ACTION: "CHECK APU OIL AND FOUND APU OIL WAS FULL. PREFORMED OPS CHECK IN REFERENCE TO AMM 49-10-00. RAN APU FOR 25 MINITUES WITH L AND R PACK SYSTEMS RUNNING. EGT STAYED IN THE GREEN DURING THE ENTIRE DURRATION OF THE OPS CHECK. INTERROGATED APU ECU BEFORE SHUT DOWN AND FOUND OIL TEMP WAS AT 179 DEGREES FAHRENHEIT. NO APU OVERTEMP WARNING MESSAGE POPULATED. COULD NOT DUPLICATE FAULT. OPS CHECK GOOD AT THIS TIME. "

Part: LANDING GEAR — WARNING MESSAGE · airframe 46,721 hrs · 40,255 cycles

GEAR DISAGREE WARNING MESSAGE UPON SELECTING GEAR DOWN. NOSE GEAR TOOK AN ABNORMAL AMOUNT OF TIME TO EXTEND, BUT DID COME DOWN AFTER APPROXIMATELY 20 SECONDS. QRH PROCEDURE COMPLETED FOR SAFETY (FLIGHT 5861 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28101686 WITH THE FOLLOWING CORRECTIVE ACTION: "TROUBLE SHOT GEAR DISAGREE DURING FLIGHT REFERENCING THE FIM 32-60-09. NO ABNORMALITIES FOUND AT THIS TIME. DOWNLOADED FDR AND FOUND GEAR WAS EXTENDED WITH FLAPS AT 0 DEGREES ON SINGLE PUMP OPERATION. DUE TO 3A ACMP PRESSURE DROPPING TO 2024 PSI DURING THAT TIME , REMOVED AND REPLACED HYDRAULIC PUMP 3A REFERENCING APPLICABLE STEPS IN THE AMM 29-12-03. OPS CHECK GOOD AT THIS TIME. SEE CP 28102670 FOR LEAK CHECK. EXTENSION/ RETRACTION TIMES ON BOTH SINGLE AND DUAL PUMP OPERATION WITHIN LIMITS AT THIS TIME REFERENCING THE AMM 32-30-00. "

Part: LANDING GEAR — WARNING MESSAGE (NOSE) · airframe 46,718 hrs · 40,253 cycles

GEAR DISAGREE WARNING MESSAGE UPON SELECTING GEAR DOWN. NOSE GEAR TOOK AN ABNORMAL AMOUNT OF TIME TO EXTEND, BUT DID COME DOWN AFTER APPROXIMATELY 20 SECONDS. QRH PROCEDURE COMPLETED FOR SAFETY (FLIGHT 5861) OPEN

Part: WINDOW — CRACKED (COCKPIT) · airframe 46,689 hrs · 40,223 cycles

DUE TO R WINDOW HEAT CAUTION MESSAGE ON FINAL APPROACH AND FINDING CRACK IN RH SIDE WINDOW, RH COCKPIT SIDE WINDOW NEEDS TO BE REPLACED. (FILED CLOSED)REMOVED RH COCKPIT SIDE WINDOW IAW AMM 56-12-01. (REF. CP 28066446 FOR INSTALLATION OF NEW SIDE WINDOW).

Part: NONE — SHEARED · airframe 44,194 hrs · 37,684 cycles

FLOOR SUPPORT BEAM FS280-FS 295 NEAR FWD O/B GALLEY MOUNT FITTING HAS SHEARED RIVET WITH CRACKS AROUND FASTENER HOLE (C-CHECK RO 7/26/2022) COMPLIED WITH MHIRJ REO 601R-53-21-3556 REV-- DATED: 2022-07-09. COMPLETED SKYCARD 51-900-1003-SKY AND COMPLETED M-337 FORM ATTACHED . REFERENCE CONTINUE CARD AND SKY CARD FOR WORK PERFORMED. NO WEIGHT CHANGE NOTED,

Part: ANGLE — CORRODED · airframe 44,194 hrs · 37,684 cycles

F.S.589.00 REINFORCING ANGLE IS CORRODED FROM STR22R TO STR27. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED F.S 589 ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED SKYCARD 51-900-1003-SKY AND COMPLETED M-337 FORM ATTACHED . NO WEIGHT CHANGE. REFERENCE CONTINUE CARD AND SKY CARD FOR WORK PERFORMED

Part: NONE — CORRODED · airframe 44,194 hrs · 37,684 cycles

RH OB FLAP UPPER SKIN HAS A FEW SMOKING RIVETS, MID SPAN ON REAR SPAR. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED "SMOKING" RIVETS IAW MHIRJ REO 601R-57-53-1242, REV -- DATED 2022-06-27. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR WORK PERFORMED.

Part: NONE — CRACKED · airframe 44,194 hrs · 37,684 cycles

FS333 FRAME IS CRACKED BETWEEN STGR 0 AND STGR 1L. (C-CHECK RO 7/26/2022) REPLACED FRAME SECTOR 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 — CRACKED · airframe 44,194 hrs · 37,684 cycles

STGR 3L IS CRACKED AT FS280. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED ANGLE AT FS280, STGR 3L IAW CRJ 200 SRM TASKS 51-40-11, 51-42-06 AND 51-42-21 REV. 38B DATED 25 NOV. 2022. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY. FORM M-337 COMPLETE AND IS ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CRACKED · airframe 44,194 hrs · 37,684 cycles

RH WHEEL WELL BRAKE FUSE AFT MOUNTING BRACKET IS CRACKED. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED RH WHEEL BRAKE FUSE BRACKETS P/N: 601R75278-11 AND 601R75262-157 IAW CRJ 200 SRM 51-40-11 AND 51-42-06 REV. 38B DATED 25 NOV 2020. 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 44,194 hrs · 37,684 cycles

L/H FLOOR SILL IS CORRODED BETWEEN F.S. 424 TO F.S. 439. (C-CHECK RO 7/26/2022) REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS , COMPLIED WITH REO 601R-53-41-666 REV-C DATED 2012-11-06 ON L/H FLOOR SILL .FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CRACKED · airframe 44,194 hrs · 37,684 cycles

R/H INBOARD AND OUTBOARD F.S. 484 CLIPS ARE CRACKED. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED R/H INBOARD AND OUTBOARD F.S. 484 CLIPS IAW CRJ 200 SRM 51-42-06, 51-42-21 REV. 38B DATED 25 NOV 2020 AND REO 601R-53-41-059 REV. C DATED 2020-03-11. MAJOR REPAIR TASK CARD AND FORM M-337 COMPLETED AND ATTACHED.NO WEIGHT CHANGE NOTED SEE CONTINUE CARD FOR DETAILS

Part: NONE — CORRODED · airframe 44,194 hrs · 37,684 cycles

TOP OF FLOOR BEAM CORRODED IN MULTIPLE LOCATIONS BETWEEN FS 409.+32 AND FS 409+95 AT LBL 9. (C-CHECK RO 7/26/2022) REPLACED FLOOR BEAM CAP IAW CRJ 200 REO 601R-53-31-1233 REV-- DATED: 2024-06-24. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 44,194 hrs · 37,684 cycles

TOP OF FLOOR BEAM CORRODED IN MULTIPLE LOCATIONS BETWEEN FS 409.00 AND FS 409+95 AT RBL 9. (C-CHECK RO 7/26/2022) REPLACED FLOOR BEAM CAP IAW CRJ 200 REO 601R-53-31-1233 REV-- DATED: 2024-06-24. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 44,194 hrs · 37,684 cycles

RBL9 FLOOR BEAM IS CORRODED INBOARD SIDE BETWEEN F.S. 473 TO F.S. 484. (C-CHECK RO 7/26/2022) REPAIRED RBL9 FLOOR BEAM UPPER FLANGE BETWEEN FS473.15- FS499 IAW MHIRJ REO 601R-53-41-3038. REV.-- DATED 2022-06-29. FORM M-337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 44,194 hrs · 37,684 cycles

R/H FLOOR SILL IS CORRODED BETWEEN F.S. 409+128 TO F.S.513. (C-CHECK RO 7/26/2022) REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW CRJ 200 REO 601R-53-41-666 REV-C DATED: 2012-11-06. COMPLETED 337 AND 51-900-1003-SKY ATTACHED. REFERENCE CONTINUE CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 44,194 hrs · 37,684 cycles

F.S. 589 FRAME IS CORRODED BETWEEN STGR 26L TO 26R. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED F.S. 589 LOWER FRAME SEGMENT IAW CRJ 200 SRM 51-42-06 AND 51-42-21 REV. 38B DATED 25 NOV 2020. 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 44,194 hrs · 37,684 cycles

LBL9 FLOOR BEAM INBOARD SIDE IS CORRODED BETWEEN F.S. 473 TO F.S. 484. (C-CHECK RO 7/26/2022) COMPLIED WITH MHIRJ REO 601R-53-41-3037 REV-- DATED: 2022-06-29. COMPLETED SKYCARD 51-900-1003-SKY AND COMPLETED 337 ATTACHED. +.38 WEIGHT CHANGE. REFERENCE CONTINU CARD AND SKY CARD FOR WORK PERFORMED .

Part: NONE — CORRODED · airframe 44,194 hrs · 37,684 cycles

PAX DOOR DD4 AFT INTERCOSTAL FOUND TO BE CORRODED. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED PAX DOOR DD4 AFT INTERCOSTAL IAW CRJ 200 SRM 51-42-06 REV. 38B DATED 25 NOV 2020 . 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 44,194 hrs · 37,684 cycles

PAX DOOR DD4 MID INTERCOSTAL FOUND TO BE CORRODED. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED PASSENGER DOOR DD4 MID INTERCOSTAL IAW CRJ 200 SRM 51-42-06 AND 51-42-21 REV. 38B DATED 25 NOV 2020. 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 44,194 hrs · 37,684 cycles

PAX DOOR FORMER BETWEEN DD4 & DD5 MIDDLE FOUND TO BE CORRODED. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED PASSENGER DOOR FORMER BETWEEN DD4 AND DD5 IAW CRJ 200 SRM 51-42-21 REV. 38B DATED 25 NOV 2020. 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 44,194 hrs · 37,684 cycles

FRAME CORRODED AT FS 319.00 BETWEEN STGR 23L AND 24R. (C-CHECK RO 7/26/2022) REMOVED AMD REPLACED 319 FRAME IAW CRJ 200 SRM 51-42-06 AND 51-42-21 REV. 38B DATED 25 NOV 2020. MAJOR REPAIR TASK CARD 51-900-1003-SKY AND M-337 FORM COMPLETED AND ATTACHED. CONTINUATION CARD FOR WORK PERFORMED. PART FOR PART REPLACEMENT NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 44,194 hrs · 37,684 cycles

AVI. DOOR SURROUNDING STRUCTURE AFT MID SUPPORT INTERCOSTALS 2 EA ARE COORRODED. (C-CHECK RO 7/26/2022) FOUND CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED 2 EA AVI DOOR SURROUND INTERCOSTALS IAW CRJ 200 SRM 51-42-06 AND 51-42-21 DATED 11/25/2020 ALSO PERFORMED SKY CARD 51-900-1003-SKY AND ATTACHED FORM M-337. NO CHANGE TO WEIGHT AND BALANCE. REF CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 44,194 hrs · 37,684 cycles

PAX DOOR DD5 INTERCOSTAL FOUND TO BE CORRODED. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED PAX DOOR DD5 INTERCOSTAL IAW CRJ 200 SRM 51-42-06 REV. 38B DATED 25 NOV 2020 . 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 44,194 hrs · 37,684 cycles

FOUND PAX DOOR INTERCOSTAL DD6 AND 2 EA CLIPS TO BE CORRODED. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD6 AND 2 EA CLIPS IAW CRJ 200 SRM 51-42-06 AND 51-42-21 REV. 38B DATED 25 NOV 2020 . 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 44,194 hrs · 37,684 cycles

PAX DOOR DD3 MID INTERCOSTAL FOUND TO BE CORRODED. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED PASSENGER DOOR DD3 MIDD INTERCOSTAL IAW CRJ 200 SRM 51-42-06 REV. 38B DATED 25 NOV 2020. 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 — DENTED · airframe 44,194 hrs · 37,684 cycles

R/H WING OUTBOARD FLAP VANE IS DENTED BETWEEN W.S. 162 TO W.S. 178. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED R/H WING OUTBOARD FLAP VANE BETWEEN W.S. 162 TO W.S. 178 IAW CRJ 200 SRM 51-42-13 REV 38B DATED 11/25/2020. REF CONTINUATION CARD FOR WORK PERFORMED. M337 AND SKYCARD 51-900-1003 SKY COMPLIED WITH. NO CHANGE TO WEIGHT AND BALANCE.

Part: NONE — CORRODED · airframe 44,194 hrs · 37,684 cycles

PAX DOOR DD1A AFT INTERCOSTAL FOUND TO BE CORRODED. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED PAX DOOR DD1A AFT INTERCOSTAL IAW CRJ 200 SRM 51-42-06 REV. 38B DATED 25 NOV 2020 . 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 44,194 hrs · 37,684 cycles

PAX DOOR DD1A MID INTERCOSTAL FOUND TO BE CORRODED. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED PASSENGER DOOR DD1A MID INTERCOSTAL IAW CRJ 200 SRM 51-42-06 AND 51-42-21 REV. 38B DATED 25 NOV 2020. 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 44,194 hrs · 37,684 cycles

PAX DOOR FORMER AND CLIP BETWEEN DD4 & DD5 FOUND TO BE CORRODED ON FWD SIDE. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED PASSENGER DOOR FORMER AND CLIP BETWEEN DD4 AND DD5 IAW CRJ 200 SRM 51-42-06 REV. 38B DATED 25 NOV 2020. 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 — CHAFED · airframe 44,194 hrs · 37,684 cycles

PAX DOOR HINGE(DOOR SIDE) FOUND TO HAVE INTERNAL CHAFE DAMAGE. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED PAX DOOR HINGE (DOOR SIDE) IAW CRJ 200 SRM 51-42-06 AND 51-42-21 REV. 38B DATED 25 NOV 2020. 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 44,194 hrs · 37,684 cycles

PAX DOOR DD2 AFT INTERCOSTAL FOUND TO BE CORRODED. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED PAX DOOR DD2 AFT INTERCOSTAL IAW CRJ 200 SRM 51-42-06 REV. 38B DATED 25 NOV 2020 . 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 44,194 hrs · 37,684 cycles

FRAME CORRODED AT FS 333.00 BETWEEN STGR 25L AND 24R. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED FRAME AT FS 333.00 BETWEEN STGR 25L AND 24R IAW CRJ 200 SRM 51-42-06 , SRM 51-42-21 REV. 38 B DATED 25 NOV 2020 MAJOR REPAIR TASK CARD SKYCARD 51-900-1003-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE. REF CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 44,194 hrs · 37,684 cycles

PAX DOOR DD1 MID INTERCOSTAL FOUND TO BE CORRODED. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED PAX DOOR DD1 MID INTERCOSTAL IAW CRJ 200 SRM 51-42-06 AND 51-42-21 REV. 38B DATED 25 NOV 2020 . 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 — DENTED · airframe 44,194 hrs · 37,684 cycles

PAX DOOR LOWER MID SEAL RETAINER FOUND TO BE DENTED. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED PAX DOOR LOWER MID SEAL RETAINER IAW CRJ 200 SRM 51-42-06 AND REV. 38B DATED 25 NOV 2020. 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 44,194 hrs · 37,684 cycles

PAX DOOR DD1 AFT INTERCOSTAL FOUND TO BE CORRODED. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED PAX DOOR DD1 AFT INTERCOSTAL IAW CRJ 200 SRM 51-42-06 REV. 38B DATED 25 NOV 2020 . 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 44,194 hrs · 37,684 cycles

PAX DOOR DD3 AFT INTERCOSTAL FOUND TO BE CORRODED. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED PAX DOOR DD3 AFT INTERCOSTAL IAW CRJ 200 SRM 51-42-06 REV. 38B DATED 25 NOV 2020 . 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 44,194 hrs · 37,684 cycles

PAX DOOR DD6 INTERCOSTAL FOUND TO BE CORRODED ON FWD SIDE. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED PASSENGER DOOR INTERCOSTAL DD6 IAW CRJ 200 SRM 51-42-06 REV. 38B DATED 25 NOV 2020. 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 44,194 hrs · 37,684 cycles

PAX DOOR DD7 INTERCOSTAL FOUND TO BE CORRODED ON FWD SIDE. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED PASSENGER DOOR DD7 INTERCOSTAL IAW CRJ 200 SRM 51-42-06 REV. 38B DATED 25 NOV 2020. 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 44,194 hrs · 37,684 cycles

FOUND PAX DOOR FWD FORMER TO BE CORRODED. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED PAX DOOR FWD FORMER IAW CRJ 200 SRM 51-42-06 AND 51-42-21 REV. 38B DATED 25 NOV 2020. 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 — WORN · airframe 44,194 hrs · 37,684 cycles

LH OB FLAP VANE SUPPORT FITTING TANG AT FLS296 HAS EXCESSIVE WEAR. (C-CHECK RO 7/26/2022) REPAIRED LH OB FLAP VANE SUPPORT FITTING IAW REO BOMBARDIER 601R-57-53-195 REV-F DATE 2017-12-19. AND REO 601R-57-53-016 REV-NC DATED: 96-09-20. COMPLETED SKYCARD 51-900-1003-SKY AND COMPLETED M-337 FORM ATTACHTED. NO WEIGHT CHANGE NOTED. REFERENCE SKYCARD AND CONTINUE CARD FOR WORK PERFORMED.

Part: NONE — DENTED · airframe 44,194 hrs · 37,684 cycles

LH OB FLAP LOWER SKIN IS DENTED AT FLS268 10IN FWD OF TE. (C-CHECK RO 7/26/2022) LH OB FLAP LOWER SKIN DENT AT FLS268 10IN FWD OF TE WAS FOUND OUT OF LIMITS IAW CRJ 200 SRM 57-53-00. COMPLIED WITH CRJ 200 SRM 57-53-00 REPAIR NO.3 REV.38 B DATED 25 NOV 2020 FOR REPAIR OF DENT. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CHAFED · airframe 44,194 hrs · 37,684 cycles

LH OB FLAP VANE LE IS CHAFED AT FLS297. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED FLAP VANE CAP I.A.W. BOMBARDIER CRJ200 SRM 51-40-11, 51-23-00, 51-25-06, 51-25-16, AND 51-42-13 REV.38B, DATED 11/25/2020. COMPLIED WITH SKYWEST MAJOR REPAIR TASK CARD 51-900-1003-SKY. M-337 COMPLETE. NO CHANGE WEIGHT AND BALANCE, SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CHAFED · airframe 44,194 hrs · 37,684 cycles

LH OB FLAP VANE LE IS CHAFED AT FLS282. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED FLAP VANE CAP IAW CRJ-200-SRM-51-40-11 AND 51-42-13. 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 — FAILED · airframe 44,194 hrs · 37,684 cycles

FOUND FS409+128 VERTICAL POSTS BL0.0 LEFT HAND SIDE WL 69.0 HAS INDICATION NOTED .400 LONG 80%FSH AT AFT FLANGE RADIUS FAILED NDT INSPECTION (C-CHECK RO 7/26/2022) COMPLIED WITH REO 601R-53-41-889. COMPLETED SKYCARD 51-900-1003-SKY AND COMPLETED M-337 FORM ATTACHED. REFERENCE CONTINUE CARD AND SKY CARD FOR WORK PERFORMED. NO WEIGHT CHANGE.

Part: NONE — CRACKED · airframe 44,194 hrs · 37,684 cycles

PAX DOOR AFT FORMER IS CRACKED JUST BELOW THE POWER ASSIST MOTOR PULLEY (C-CHECK RO 7/26/2022) REMOVED AND REPLACED PAX DOOR AFT FORMER IAW CRJ 200 SRM 51-42-06 AND 51-42-21 REV. 38B DATED 25 NOV 2020. 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 — DAMAGED · airframe 44,194 hrs · 37,684 cycles

THE ADF ANTENNA HAS ONE NUTPLATE SPINNING WITH THE SCREW STILL INSTALLED AND REQUIRES REPLACEMENT.THE LH MIDDLE NUTPLATE. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED 1EA NUTPLATE ON HAT CHANNEL AND RE-INSTALLED HAT CHANEEL IAW CRJ 200 SRM 51-42-06. MAJOR REPAIR TASK 51-900-1003-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — DENTED · airframe 44,194 hrs · 37,684 cycles

WHILE REMOVING STABILIZER VERTICAL LEADING EDGE FOUND PROTRUDING DENT APROX 12" ABOVE T/E OF THE L/H PYLON (C-CHECK RO 7/26/2022) REPAIRED DENT IAW REO 601R-53-61-7844 REV. - - DATED 6/15/22. SEE CONTINUATION 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 — CHAFED · airframe 44,194 hrs · 37,684 cycles

R/H INBOARD FLAP, FLAP VANE IS CHAFED AT (3) LOCATIONS ALONG THE LEADING EDGE FROM CONTACT WITH FLAP VANE STOPS. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED R/H INBOARD FLAP VANE MID. LEADING EDGE CAP I.A.W. BOMBARDIER CRJ200 SRM 51-42-13 REV.38B, DATED 11/25/2020. COMPLETED SKYWEST M-337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY. WEIGHT AND BALANCE NOT EFFECTED.

Part: NONE — CRACKED · airframe 44,194 hrs · 37,684 cycles

L/H FORWARD FUSELAGE SKIN IS CRACKED AT THE L/H TRU DOOR AFT LATCH CUTOUT IN THE FORWARD LOWER RADIUS OF THE LATCH CUTOUT. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED L/H FWD FUSE SKIN IAW SRM 51-42-13, 51-42-06 AND REO 601R-53-11-3775 REV-- DATED:2022-06-13. COMPLETED TASK CARD 51-900-1003-SKY ATTACHED AND COMPLETED M-337 FORM ATTACHED. REFERENCE CONTINUE CARD AND SKYCARD FOR WORK PERFORMED. PART FOR PART REPLACEMENT NO WEIGHT CHANGE NOTED.

Part: NONE — DENTED · airframe 44,194 hrs · 37,684 cycles

PAX DOOR HAS DENT ON OUTER SKIN ( MARKED) (C-CHECK RO 7/26/2022) REPAIRED PAX DOOR OUTER SKIN DENT IAW MHIRJ REO 601R-52-11-2925 REV. -- DATED 2022-06-14. MAJOR REPAIR TASK CARD 51-900-1003-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 40,530 hrs · 34,386 cycles

ATTEMPTED TO RETRACT GEAR ON DEPARTURE, GEAR DISAGREE WARNING WITH NOSE DOOR OPEN WARNING FLIGHT 5493 CLOSEDTHIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 19896892 WITH THE FOLLOWING CORRECTIVE ACTION: "PERFORMED ADJUSTMENT OF THE NOSE LANDING GEAR CENTERED/EXTENDED PROXIMITY-SENSORS IAW AMM. ADJUSTMENT GOOD AT THIS TIME. PERFORMED GEAR EXTENSION AND RETRACTION 13 TIMES IAW AMM. OPS CHECK GOOD AT THIS TIME. NO FAULTS NOTED."

Part: ACTUATOR — FAILED (RT MLG) · airframe 39,743 hrs · 33,670 cycles

RECEIVED €ŒGEAR DISAGREE€? ON THE RIGHT MAIN ON TAKEOFF. MESSAGE CLEARED BEFORE QRH COMPLETED. (FLT#5803) FO: 07/05/2019 CLOSED REMOVED AND REPLACED RT MLG SIDE STAY ACTUATOR IAW AMM.

Part: STRUT — LOW (NLG) · airframe 39,440 hrs · 33,386 cycles

GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF WITH THE NOSE GEAR REMAINING DOWN AND LOCKED. BOTH MAIN GEAR INDICATED €ŒUP€?. HAD ASSOCIATED €ŒNOSE DOOR OPEN€? WARNING MESSAGE AS WELL AS TWO CAUTION MESSAGES, €ŒSTEERING INOP€? AND €ŒWOW INPUT.€? RAN QRH PROCEDURE AND LANDED NORMALLY WITH ALL THREE GEAR INDICATING DOWN AND LOCKED. (REPO FLT#1361) CLOSED COMPLIED WITH NOSE STRUT SERVICING OPS AND DIMENSION CHECKS GOOD, NO LEAKS NOTED. COMPLIED WITH NUMEROUS GEAR SWINGS AND EMERGENCY GEAR EXTENSIONS IAW AMM. OPS CHECKS GOOD.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 39,438 hrs · 33,384 cycles

DRAIN MAST INTERNAL DOUBLER AT FS 605 HAS CORROSION. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED DRAIN MAST INTERNAL DOUBLER P/N 301R43216-11 AT FS 605 IAW SRM. LEAK AND OPS CHECKS SATISFACTORY IAW AMM.

Part: HINGE — DAMAGED (FUSELAGE) · airframe 39,438 hrs · 33,384 cycles

PAX DOOR HINGE ( FUSELAGE SIDE) DAMAGED. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED PAX DOOR HINGE ( FUSELAGE SIDE) IAW SRM. LEAK CHECK SATISFACTORY.

Part: TRUNNION — DAMAGED (LT WING) · airframe 39,438 hrs · 33,384 cycles

FOUND 2EA OVERSIZE FASTENERS IN LT TRUNNION IN HOLES 14, 19. (C-CHECK) RO: 05/07/2019 REAMED OVERSIZE HOLES IN LT TRUNNION LOWER PLANK AND INSTALLED NEW FASTENERS IAW REO.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,438 hrs · 33,384 cycles

SEVERAL AREAS OF CORROSION ON LT PRESSURE FLOOR SILL SKIN. (C-CHECK) RO: 05/07/2019 REMOVED CORROSION IN 12 AREAS ON LT PRESSURE FLOOR SILL PANEL BETWEEN FS 409+128 AND FS559, IAW REO ALL CHECKS OKAY.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,438 hrs · 33,384 cycles

SEVERAL AREAS OF CORROSION ON RT PRESSURE FLOOR SILL SKIN. (C-CHECK) RO: 05/07/2019 BLENDED OUT CORROSION ON RT PRESSURE FLOOR SILL PANEL FROM FS 409+128 TO FS 559 AT VARIOUS LOCATIONS IAW REO.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,438 hrs · 33,384 cycles

SERVICE DOOR SILL ANGLE PN 601R38303-225 HAS SPOTS OF CORROSION. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED NEW SILL ANGLE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,438 hrs · 33,384 cycles

FRAME FS605 CORRODED STR26L €“ STR26R. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED FRAME AT FS605 STR26L - STR26R IAW SRM. LEAK CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,438 hrs · 33,384 cycles

FLOOR SUPPORT ANGLE CORRODED FS621 LBL9 €“ LBL27. (C-CHECK) RO: 05/07/2019 REMOVED CORROSION FROM FLOOR SUPPORT ANGLE FS621 LBL9-LBL27 COMPLIED WITH AL STEPS OF REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,438 hrs · 33,384 cycles

FLOORBEAM FS409+10 €“ FS409+40 RBL9 CORRODED AT FASTENER HOLE LOCATIONS. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED FLOORBEAM CAP AT FS409.00+5 - FS409.00+42 IAW SRM AND REO.

Part: SKIN — CHAFED (ZONE 300) · airframe 39,438 hrs · 33,384 cycles

RIGHT HAND SIDE AFT EXTERIOR SKIN HAS CHAFING AND CORROSION WHERE APU EXHAUST SHEILD ATTACHES TO AIRCRAFT. (C-CHECK) RO: 05/07/2019 BLENDED CHAFING AND CORROSION WHERE APU EXHAUST SHEILD ATTACHES TO AIRCRAFT IAW SRM AND REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,438 hrs · 33,384 cycles

FLOORBEAM CORRODED AROUND NUT PLATE LOCATIONS FS610 €“ FS620 LBL27. (C-CHECK) RO: 05/07/2019 COMPLIED WITH PERMANENT REPAIR FLOORBEAM CORROSION AROUND NUT PLATE LOCATIONS FS610 €“ FS620 LBL27 IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,438 hrs · 33,384 cycles

FLOORBEAM CORRODED AROUND NUT PLATE LOCATIONS FS561 €“ FS569 LBL27. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED NEW FLOORBEAM LBL 27 FROM FS 574 TO FS 559+24 IAW REO.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,438 hrs · 33,384 cycles

CARGO DOOR SILL CORRODED FS562 €“ FS621 LBL43. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED CARGO DOOR SILL FROM FS589.00 - 621.00 IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,438 hrs · 33,384 cycles

FLOORBEAM CORRODED AROUND NUT PLATE LOCATIONS FS569 €“ FS610 LBL27. (C-CHECK) RO: 05/07/2019 REPLACED FLOORBEAM FS569 - FS610 LBL27 WITH NEW P/N 601R35031-263 IAW REO.

Part: FAIRING — DAMAGED (ZONE 300) · airframe 39,438 hrs · 33,384 cycles

FAIRING 326CL IS CHAFED/GOUGED WHERE IT INTERFACES WITH THE VISOR PANEL. (C-CHECK) RO: 05/07/2019 REMOVED DAMAGE ON PANEL 326CL AND COMPLIED WITH ALL STEPS OF REO.

Part: DOOR — CHAFED (LT MLG) · airframe 39,438 hrs · 33,384 cycles

LT MLG DOOR FORWARD SIDE HAS CHAFING 2 LOCATIONS. (C-CHECK) RO: 05/07/2019 BLENDED LT MLG DOOR FWD SIDE CHAFES 2 LOCATIONS IAW SRM.

Part: STRUCTURE — GOUGED (SERVICE DOOR) · airframe 39,438 hrs · 33,384 cycles

SERVICE DOOR OUTER HANDLE CUT-OUT HAS SEVERAL GOUGES. (C-CHECK) RO: 05/07/2019 BLENDED OUT DAMAGE AREAS 5 EA ON SERVICE DOOR OUTER HANDLE CUT OUT, COMPLIED WITH ALL STEPS OF REO.

Part: PAN — CORRODED (SERVICE DOOR) · airframe 39,438 hrs · 33,384 cycles

SERVICE DOOR AFT PAN HAS CORROSION AT LOWER CORNER. (C-CHECK) RO: 05/07/2019 BLENDED SERVICE DOOR AFT PAN AT LOWER CORNER IAW SRM AND REO.

Part: PANEL — DENTED (RT WING) · airframe 39,438 hrs · 33,384 cycles

DENTS ON RT WING MIDDLE LEADING EDGE (C-CHECK) RO: 05/07/2019 REPLACED RT WING CENTER LEADING EDGE WITH NEW LEADING EDGE PANEL P/N 601R12044-8S IAW SRM.

Part: ACCESS DOOR — DENTED (GROUND AIR) · airframe 39,438 hrs · 33,384 cycles

SEVERAL DENTS FOUND BELOW GROUND AIR CONNECTION DOOR AT APPROXIMATELY FS559 TO FS579. (C-CHECK) RO: 05/07/2019 COMPLIED WITH PERMANENT REPAIR GRD AIR DOOR DENTS, IAW REO, ALL CHECKS OKAY.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,011 hrs · 29,431 cycles

FWD FUSELAGE BELLY AT FS 250.0 HAS A DENT. C-CHECK, ALL STEPS COMPLETED FOR PERMANENT REPAIR TO DENT LOCATED AT FS 250 IAW REO.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 35,011 hrs · 29,431 cycles

LEFT INBOARD FLAP VANE SKIN L/E, RT SECTION IS CHAFED. C-CHECK, REMOVED AND REPLACED LEFT INBD FLAP VANE L/E RT SECTION IAW SRM.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 35,011 hrs · 29,431 cycles

RIGHT INBOARD FLAP VANE L/E SKIN IS CHAFED AT CENTER SECTION. C-CHECK, REMOVED AND REPLACED RT INBD FLAP CENTER FLAP VANE LEADING EDGE CAP IAW SRM.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 35,011 hrs · 29,431 cycles

LEFT INBOARD VANE SKIN INBOARD L/E SECTION CHAFED. REMOVED AND REPLACED LEFT INBD VANE SKIN INBD L/E SECTION IAW SRM.

Part: FLAP — CHAFED (LT WING) · airframe 35,011 hrs · 29,431 cycles

LEFT INBOARD FLAP CENTER SECTION OF L/E IS CHAFED. C-CHECK, REMOVED AND REPLACED LEFT INBD FLAP CENTER L/E SECTION IAW SRM.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 35,011 hrs · 29,431 cycles

RIGHT INBOARD FLAP VANE L/E SKIN IS CHAFED AT LEFT SECTION. C-CHECK, REMOVED AND REPLACED THE RIGHT INBOARD FLAP VANE L/E SKIN IAW SRM.

Part: SEAL — LEAKING (SERVICE DOOR) · airframe 32,611 hrs · 27,243 cycles

WHILE CLIMBING, ACFT WAS PRESSURIZING NORMAL AND AT 32,000 FT CREW REPORTED VERY LOUD NOISE COMING FROM SERVICE DOOR. THEN CABIN PRESSURE STARTED TO CLIMB UNTIL IT REACH 8000. CREW STARTED TO DESCEND AND CABIN ALT KEPT CLIMBING UNTIL REACHED 11,000 FT THEN CREW DECLARED EMERGENCY. R & R FORWARD SERVICE DOOR SEAL IAW AMM. PRESSURIZED ACFT LEAK CHECK OF SERVICE DOOR SEAL, NO LEAKS NOTED.

Part: CONTROL HANDLE — FAILED (MLG) · airframe 32,110 hrs · 26,783 cycles

AFTER TAKEOFF, CREW RECEIVED A GEAR DISAGREE, NOSE GEAR DID NOT RETRACT, C/W QRH, RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. R & R LANDING GEAR CONTROL HANDLE ASSY IAW AMM. C/W GEAR EXTENSION, RETRACT CYCLES AND EMERGENCY EXTENSION IAW AMM OPS CHECK GOOD. PN ON 7-45502-T, SN ON 1162, PN OFF 7-45502-5, SN OFF 1469.

Part: PROXIMITY SENSOR — FAILED (NLG) · airframe 31,677 hrs · 26,397 cycles

AFTER TAKEOFF, THE CREW RECEIVED A NOSE WHEEL STEERING INOPERATIVE INDICATION, FOLLOWED BY A GEAR DISAGREE. NOSE GEAR DID NOT RETRACT. NO EMERGENCY DECLARED. VERIFIED NOSE WHEEL STEERING OPS WITH GEAR DOWN. R & R WOW 1 PROXIMITY SENSOR ON NOSE GEAR IAW AMM PERFORMED GEAR SWINGS IAW AMM NO FAULTS NOTED.

Part: SKIN — DAMAGED (BS 605) · airframe 30,573 hrs · 25,424 cycles

LEFT SIDE EXTERNAL FUSELAGE SKIN HAS A CREASE AT BS 605 BETWEEN STR 21 - 22L. REPAIRED IAW EA.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 30,573 hrs · 25,424 cycles

RIGHT INBD FLAP, OTBD VANE CAP HAS A CHAFE. BLENDED CHAFE ON INBD FLAP VANE CAP, FOUND TO BE BEYOND LIMITS OF REO. R & R VANE CAP ON RT INBD FLAP, OTBD END. RESTORED FINISH AND IDENTIFIED VANE CAP IAW EA.

Part: SKIN — CORRODED (BS 559) · airframe 30,573 hrs · 25,424 cycles

EXTERNAL FUSELAGE SKIN HAS CORROSION AT 2 EA FAIRING MOUNT HOLES, AT BS 559+33, BETWEEN STRINGERS 22 - 23R. SKIN REPAIRED IAW EA.

Part: SKIN — CHAFED (RT AILERON) · airframe 30,573 hrs · 25,424 cycles

RIGHT AILERON CHAFED ALONG UPPER L/E. RT AILERON UPPER L/E SKIN REPAIRED IAW REO.

Part: SKIN — DENTED (BS 589) · airframe 30,573 hrs · 25,424 cycles

DENT AFT OF BS 589 BELOW STRINGER 21 MEASURES 1.5 X 1.5 X .06 DEEP. REPAIRED DENT IAW EA.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL FLOW PRESS) · airframe 29,632 hrs · 24,655 cycles

DURING DESCENT AT 24,000 FT, RECEIVED LT FUEL LOW PRESSURE MESSAGE, NO SECONDARY INDICATIONS, FUEL WAS 310 PPH, OCCURED WHEN THROTTLE WAS BROUGHT BACK TO FLIGHT IDLE. PERFORMED OPS CHECK OF FUEL LOW PRESSURE SWITCH IAW AMM, AND RAN ENGINES WITH CREW AS REQUIRED, MESSAGE NOT SHOWN.

Part: AMPLIFIER — FLUCTUATES (INDICATION SYS) · airframe 28,943 hrs · 24,088 cycles

RETURNED TO DEPARTURE DUE TO RT ENGINE N1, N2, OIL PRESSURE, AND FUEL FLUCTUATIONS. REPLACED AMPLIFIER. OPS CHECKED GOOD.

Part: ENGINE — OVERTEMP (LEFT) · airframe 28,508 hrs · 23,752 cycles

REJECTED TAKEOFF DUE TO ITT EXCEEDENCE ON LT ENGINE DURING T/O ROLL. COMPLIED WITH OVER TEMP INSPECTION IAW CARD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,404 hrs · 23,657 cycles

EMERGENCY EXIT SIGN, LOWER, NEXT TO GALLEY SERVICE DOOR, LAMPS INOPERATIVE, REPLACED LAMPS.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 28,218 hrs · 23,521 cycles

RECEIVED CABIN AFT CAUTION. AUTO 1 AND AUTO 2 WOULD NOT CONTROL CABIN. MANUAL MODE WOULD CONTROL CABIN. PERFORMED OPS TEST OF THE PRESSURIZATION CONTROLS IAW AMM. OPS CHECKED GOOD AT THIS TIME.

Part: LIGHT — FAULTY (CABIN) · airframe 27,389 hrs · 22,883 cycles

SMOKE & SMELL ASSOCIATED WITH INTERIOR LIGHTS AT SEAT 6A. FLT 6362 REPLACED SIDEWALL LIGHT FIXTURE AT SEATS 5A & 6A.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,106 hrs · 22,676 cycles

EMERGENCY LIGHTS DO NOT ILLUMINATE. FLT 6262 ALLOWED EMERGENCY LIGHTS TO CHARGE. OPERATIONS CHECKED GOOD.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 26,410 hrs · 22,132 cycles

PARKING BRAKE PASS THRU HOLE IN FS 202 HAS MULTIPLE CRACKS. C-CHECK REPAIRED IAW REO.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 26,410 hrs · 22,132 cycles

LT FS484 CABLE PULLEY SUPPORT INBD CLIP IS CRACKED. C-CHECK REPLACED IAW REO & SRM.

Part: PANEL — CHAFED (LT AILERON) · airframe 26,410 hrs · 22,132 cycles

LT WING AILERON PANEL 599AB IS CHAFED. C-CHECK BLENDED IAW REO.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 26,410 hrs · 22,132 cycles

LT INBD FLAP VANE LE CHAFED ON THE OTBD SIDE. C-CHECK REPAIRED IAW REO.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 26,410 hrs · 22,132 cycles

LT INBD FLAP VANE LE CHAFED IN THE CENTER. C-CHECK BLENDED IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,410 hrs · 22,132 cycles

CRACK AT FS 621 BULKHEAD WEB FWD FACE, ABOVE UPPER CARGO DOOR TRACK FITTING. C-CHECK REPAIRED IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 26,410 hrs · 22,132 cycles

LT INBD FLAP VANE LE CHAFFED IN THE CENTER BEYOND LIMITS. C-CHECK REPLACED PN 601R14303-51 IAW SRM.

Part: PANEL — CHAFED (LT AILERON) · airframe 26,410 hrs · 22,132 cycles

LT WING AILERON PANEL 599BB IS CHAFED. C-CHECK BLENDED IAW REO.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 26,410 hrs · 22,132 cycles

RT INBD FLAP VANE LE SKIN CHAFED. C-CHECK REPLACED IAW REO.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 26,410 hrs · 22,132 cycles

RT INBD FLAP VANE LEADING SKIN CHAFED NEAR CENTER. C-CHECK REPAIRED IAW REO.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 26,410 hrs · 22,132 cycles

RT INBD FLAP VANE LE SKIN CHAFED AT OTBD END. C-CHECK REPAIRED IAW REO.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 25,802 hrs · 21,660 cycles

EMERGENCY FLOOR LIGHTING STRIP BY SEAT 10 C/D DOES NOT ILLUMINATE. (FLT 5232) RE-CONNECTED EMERGENCY FLOOR LIGHT STRIP AT SEAT 10 C/D. OPS CHECK GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,678 hrs · 21,569 cycles

NR 4 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 6449) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,559 hrs · 21,482 cycles

EMERGENCY EXIT SIGN FORWARD SIDE OF SERVICE DOOR DOES NOT ILLUMINATE. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 25,430 hrs · 21,382 cycles

FORWARD FLOOR EMERGENCY LIGHTS DO NOT ILLUMINATE. (FLT 6224) RECONNECTED LIGHT STRIP INTO SOCKET.

Part: RESTRICTOR — FAILED (SELECTOR VALVE) · airframe 22,961 hrs · 19,435 cycles

GEAR COMES UP SLOW AFTER TAKEOFF. (FLT 6406) REPLACED MLG SELECTOR VALVE RESTRICTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,061 hrs · 18,721 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5429) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,873 hrs · 18,580 cycles

FS 621 BULKHEAD WEB CRACKED AT UPPER LINTEL FITTING. (C-CHECK) REPAIR PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,844 hrs · 18,556 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5508) RELAMPED EMERGENCY LIGHT.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 21,614 hrs · 18,331 cycles

"GEAR DISAGREE" WARNING. (FLT 6366) REPLACED 3B HYDRAULIC PUMP. P/N ON 848847, S/N OFF MX670403.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,401 hrs · 18,146 cycles

RIGHT OVERWING CENTER EMERGENCY LIGHT IS OUT. (FLT 5636) RELAMPED EMERGENCY LIGHT.

Part: UNKNOWN — DAMAGED · airframe 21,066 hrs · 17,875 cycles

(FLT 6515) HAIL DAMAGE TO FUSELAGE AND FLIGHT CONTROLS.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 20,773 hrs · 17,656 cycles

GEAR DISAGREE MESSAGE AND NOSE GEAR DID NOT RETRACT. (FLT 6472) ADJUSTED NOSE LANDING GEAR PROX SENSOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,709 hrs · 17,603 cycles

AFT EMERGENCY OVERHEAD LIGHT IS OUT. (FLT 6382) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,368 hrs · 17,337 cycles

AFT CEILING EMERGENCY LIGHT OUT. (FLT 6275) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,923 hrs · 16,967 cycles

NR 3 LEFT EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 5840)RELAMPED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,923 hrs · 16,967 cycles

LEFT MIDDLE EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 5829)RELAMPED.

Part: MOTOR — DEFECTIVE (PAX DOOR) · airframe 18,808 hrs · 16,055 cycles

PAX DOOR DIFFICULT TO OPEN. (FLT 6593) REPLACED MAIN CABIN DOOR ASSIST MOTOR.

Part: PANEL — UNSECURE (CABIN) · airframe 18,635 hrs · 15,925 cycles

BACK LIGHTING BEHIND EMERGENCY LIGHT AND PAX SIGNS INOPERATIVE. (FLT 6741) RE-SECURED PASSENGER SIGNS EMERGENCY LIGHT PANEL.

Part: MECHANISM — LACK OF LUBE (MAIN DOOR) · airframe 18,091 hrs · 15,460 cycles

MAIN DOOR HANDLE DIFFICULT TO OPERATE. (FLT 6178) LUBED DOOR LOCKING MECHANISM.

Part: LINER — MISSING (RT ENGINE) · airframe 17,444 hrs · 14,897 cycles

FOUND RIGHT ENGINE CONTAINMENT CASE LINING MISSING. (FLT 1054) REPLACED CONTAINMENT CASE.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 17,339 hrs · 14,810 cycles

FS 280 FLOORBEAM CRACKED. (C CHECK) REPLACED BEAM PER REO.

Part: CASE — CRACKED (LT ENGINE) · airframe 17,340 hrs · 14,811 cycles

LEFT ENGINE LPT CASE CRACKED AT 3 O'CLOCK POSITION, OUT OF LIMITS. (C CHECK) REPLACED ENGINE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,900 hrs · 15,302 cycles

RIGHT LOWER FLANGE AND CLIPS AT FS 280 CRACKED. (C CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,630 hrs · 15,059 cycles

FS 559 PRESSURE BULKHEAD CRACKED AT CAP ANGLE RADIUS. (C CHECK) REPAIRING PER REO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 17,822 hrs · 15,227 cycles

FS 280 FLOORBEAM CRACKED. (C CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,374 hrs · 14,027 cycles

AFT EMERGENCY CEILING LIGHT INOP. (FLT 6450) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,164 hrs · 13,865 cycles

MOST AFT EMERGENCY CEILING LIGHT INOP. (FLT 6073) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,993 hrs · 13,712 cycles

NR 3 EMERGENCY FLOOD LIGHT INOP. (FLT 5959) RELAMPED NR 3 CEILING EMERGENCY FLOOD LIGHT IAW CRJ MM 200 33-51-16.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,814 hrs · 12,756 cycles

FLT 6639 - REAR LIGHT STRIP EMERGENCY LIGHTS INOP. REPLACED LIGHT STRIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,763 hrs · 12,712 cycles

FLT 6374 - RIGHT WING AFT EMERGENCY EXIT LIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 14,663 hrs · 12,628 cycles

FLT 6245 - FURTHEST AFT EMERGENCY OVERHEAD LIGHT INOP. RELAMPED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 13,787 hrs · 11,964 cycles

FLT 5900 - FIRST OFFICERS WINDSHIELD CRACKED. REPLACED RIGHT WINDSHIELD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 13,617 hrs · 11,828 cycles

FLT 5923 - LAST CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 13,169 hrs · 11,454 cycles

FLT 5887 - EMERGENCY CEILING FLOOD LIGHT INOP. RELAMPED.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 13,572 hrs · 11,790 cycles

C-CHECK, PASSENGER DOOR ANGLE CRACKED. REPAIRED PER SRM.

Part: STRINGER CLIP — CRACKED (BS 625 S14L) · airframe 13,572 hrs · 11,790 cycles

C-CHECK, FS 625 LEFT STRINGER CLIP AT STRINGER 14L CRACKED. REPLACED PER SRM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 12,765 hrs · 11,119 cycles

AFT CEILING EMERGENCY POD LIGHT IS NOT WORKING. (FLIGHT NR 5929) RELAMPED AFT CEILING EMERGENCY LIGHT PER 33-21-01. OPS CHECK GOOD.

Part: LIGHT — SHORTED (COCKPIT) · airframe 10,970 hrs · 9,549 cycles

FLT 6436 - MAP LIGHTS INOP. FIRST OFFICERS MAP LIGHT POPS THE CIRCUIT BREAKER. SECURED LOOSE HARDWARE ON MAP LIGHT.

Part: FLAP — DAMAGED (LT WING) · airframe 10,859 hrs · 9,449 cycles

LEFT OUTBOARD FLAP IS DAMAGED ALONG TRAILING EDGE. REPLACED FLAP PER 27-54-05.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 8,286 hrs · 7,205 cycles

PAX DOOR, AFT DRAG ANGLE IS CRACKED ADJACENT TO THE PAX DOOR ASSIST MOTOR CABLE PULLEY BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE SECTION AND SPLICE ANGLE PER REO NR 601R-52-11-513 REV 'A' SHEET 1 OF 3.

Part: HAND RAIL — CRACKED (PAX DOOR) · airframe 8,286 hrs · 7,205 cycles

PAX DOOR - AFT WEB IS CRACKED AT HANDRAIL STOW BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER AND REPAIR ANGLES ON PAX DOOR AFT SIDE PANEL IAW REO 601R-52-11-702 REV.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 8,286 hrs · 7,205 cycles

RT 621.0 FLOORBEAM OTBD SIDE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLES AT STA 621.0 RT FLOOR SUPPORT PER REO 601R-53-61-117 REV C.

Part: SUPPORT — CRACKED (BS 625) · airframe 8,286 hrs · 7,205 cycles

RT STA 625 BETWEEN STR 12 AND 13 SUPPORT CLIP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP PN 601 35012-52; PONR 70576 AT RT FS 625 BETWEEN STR 12/13 PER CRJ200 REO 601R 53-61-422.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 8,286 hrs · 7,205 cycles

LT STA 621.0 FLOORBEAM OTBD SIDE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE AND REPAIR ANGLE PER BOMBARDIER AEROSPACE REO601R-53-61-117 REV C DATED 2004-AUG-25.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 8,286 hrs · 7,205 cycles

FS 484 INTERCOSTAL CRACKED AT LEFT OUTBOARD SIDE DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLE AT OB FS 484 IAW CRJ200 REO 601R-53-41-059 .

Part: SUPPORT — CRACKED (BS 625) · airframe 8,286 hrs · 7,205 cycles

LT STA 625 BETWEEN STR 12 AND 13 SUPPORT CLIP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP PN 601 35012-51 AT LT FS625 BETWEEN STR 12/13 PER CRJ200 REO 601R 53-61-422.

Part: WEB — CRACKED (PAX DOOR) · airframe 8,286 hrs · 7,205 cycles

PAX DOOR, FWD WEB IS CRACKED UNDER THE HANDRAIL STOW BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED EXTERNAL DOUBLER AND REPAIR ANGLES ON PAX DOOR FWD SIDE PANEL IAW REO NR 601R-52-11-702 REV A.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 5,042 hrs · 4,332 cycles

FLOOR EXIT SIGN BY SEAT 8A IS INOP. REPLACED NR 2 INVERTER IAW AMM CH 33-51-00. OPERATIONAL CHECK GOOD.

Part: SWITCH — INTERMITTENT (EMERGENCY LIGHT) · airframe 4,953 hrs · 4,245 cycles

2ND AND 3RD ROWS OF EMERGENCY EXIT LIGHTS INTERMITTENT. REPLACED FA STATION TOGGLE SWITCH. OPERATIONAL CHECK GOOD IAW MM 33-51-01 AND 33-51-00.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 4,903 hrs · 4,202 cycles

EMERG LIGHT STRIP (FLOOR) ON RIGHT SIDE IS BURNED OUT. REPLACED NR 2 EMERGENCY BATTERY PACK NR 2 IAW CRJ MM 33-51-04. OPERATIONAL CHECK GOOD, PN ON 2013-1A SN ON 36254 OFF 83055.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 4,792 hrs · 4,109 cycles

FORWARD SECTION OF EMERGENCY LIGHTS ON CABIN FLOOR INOP. REPLACED FWD BATTERY PACK BALLAST. OPERATIONAL CHECK GOOD.

Part: LIGHT — LOOSE (ROWS 2-5) · airframe 4,674 hrs · 4,003 cycles

EMERGENCY LIGHTS ROWS 2, 3, 4, 5 INOP. RECONNECTED STRIP. OPERATIONAL CHECK GOOD.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 3,857 hrs · 3,323 cycles

FS 280 LBL 9.0 OUTBOARD FLOORBEAM ATTACH ANGLE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, 51-23-00.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 3,857 hrs · 3,323 cycles

FS 280 AT RBL 9.0 INBOARD AND OUTBOARD FLOORBEAM ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, 51-23-00.

Part: CONTROL LEVER — MALFUNCTIONED (TE FLAPS) · airframe 2,576 hrs · 2,222 cycles

AFTER LANDING CHECK FLAPS FAIL CAUTION AFTER RETRACTING TO 30 DEGREES. REPLACED FLAP CONTROL LEVER, OPERATIONAL CHECKED GOOD. P/N OFF 292-65253-1, S/N OFF 592.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 2,241 hrs · 1,921 cycles

STAB CH1 INOP AND MACH TRIM MESSAGES IN CLIMB (FL240). CLEANED BOTH TRIM SWITCHES AND REPLACED HSTCU IAW CRJ MM 27-41-01. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — INOPERATIVE (STAB TRIM) · airframe 2,159 hrs · 1,853 cycles

STAB TRIM CHANEL 1 STATUS MESSAGE IN FLIGHT. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR, HORIZONTAL STAB MOTOR CONTROL UNIT AND HSTCU IAW AMM 27-42-01AND MM27-42-05. OPERATIONAL CHECK GOOD. P/N: 7060-9 S/N OFF: 1184

Part: MOTOR — MALFUNCTIONED (STAB TRIM) · airframe 2,128 hrs · 1,825 cycles

STAB TRIM CHANNEL 1 DISENGAGED IN FLIGHT. REPLACED MOTOR CONTROL UNIT FOR STAB TRIM. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 1,529 hrs · 1,299 cycles

STAB CHANNEL 1 INOP AFTER T/O. REMOVED AND REPLACED HSTCU, OPERATIONAL CHECK GOOD IAW 27-40-00.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 411 hrs · 352 cycles

STAB TRIM CH 2 FAILS FFOD CHECK. REMOVED AND REPLACED STAB TRIM ACTUATOR AND MOTOR CONTROL PER TASK CARD RII 27-415. OPS CHECK GOOD. P/N 7062-3, S/N ON 786, S/N OFF 1184.

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM) · airframe 245 hrs · 203 cycles

STAB CHANNEL 1 INOPERATIVEDL2428M4 STATUS MESSAGE UPON EXTENSION OF FLAPS, WOULD NOT ENGAGE. REMOVED AND REPLACED HSTCU PER CRJ MM 27-40-00.