N923SW

Part: SMOKE DETECTOR — ACTIVATED (CARGO BAY) · airframe 48,401 hrs · 41,331 cycles

WE OBSERVED A CARGO SMOKE WARNING MESSAGE PASSING THROUGH 16000 FEET 10 MINUTES AFTER DEPARTING KPSP. WE DECLARED THE EMERGENCY AND COMPLIED WITH THE SMOKE CARGO QRH PROCEDURE. AT THIS TIME, THE CARGO FAN FAIL MESSAGE APPEARED.AFTER DISCHARGING BOTH CARGO FIRE BOTTLES THE CARGO SMOKE WARNING MESSAGE WAS REPLACED BY CARGO BTL LO CAUTION MESSAGE. THERE WAS NO INDICATION IN THE CABIN OF ANY SMOKE. (FLT 2201 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 31612 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED LH AND RH CARGO FIREBOTTLES IAW CRJ200 AMM 26-25-01 WITH NEW SERVICEABLE UNITS. DURING OP CHECK, WHEN POWER APPLIED APPLIED TO AIRCRAFT, BOTH BOTTLES DISCHARGED UNCOMMANDED. SEE CAMP ITEM CP 31969 FOR CONTINUE MAINTENANCE."

Part: SMOKE WARNING — ILLUMINATED (CARGO BAY) · airframe 48,401 hrs · 41,331 cycles

WE OBSERVED A CARGO SMOKE WARNING MESSAGE PASSING THROUGH 16000 FEET 10 MINUTES AFTER DEPARTING KPSP. WE DECLARED THE EMERGENCY AND COMPLIED WITH THE SMOKE CARGO QRH PROCEDURE. AT THIS TIME, THE CARGO FAN FAIL MESSAGE APPEARED.AFTER DISCHARGING BOTH CARGO FIRE BOTTLES THE CARGO SMOKE WARNING MESSAGE WAS REPLACED BY CARGO BTL LO CAUTION MESSAGE. THERE WAS NO INDICATION IN THE CABIN OF ANY SMOKE. (FLT 2201 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 31612 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED LH AND RH CARGO FIREBOTTLES IAW CRJ200 AMM 26-25-01 WITH NEW SERVICEABLE UNITS. DURING OP CHECK, WHEN POWER APPLIED APPLIED TO AIRCRAFT, BOTH BOTTLES DISCHARGED UNCOMMANDED. SEE CAMP ITEM CP 31969 FOR CONTINUE MAINTENANCE."

Part: NONE — CORRODED · airframe 46,142 hrs · 39,408 cycles

*CORROSION ON ANGLE AT FS621 AT APPROXIMATELY LBL32. (C-CHECK RO 12/04/2021) *CORROSION ON ANGLE AT FS621 AT APPROXIMATELY LBL32. REO 601R-53-61-117 REV. -E DATED 2018-01-15 ,CRJ-200-SRM 51-42-06, AND CRJ-200-SRM 51-42-21. COMPLIED WITH 51-900-1003-SKY AND LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS

Part: NONE — DEFECTIVE · airframe 46,142 hrs · 39,408 cycles

FS621 BULKHEAD HAS 2EA FASTENER HOLES WITH DEFECT MARKED HAS #1 AND #8 COMMON TO HORIZONTAL STIFFENER AT RBL27 AND LBL27. (C-CHECK RO 12/04/2021) REPAIRED FS621 BULKHEAD HAS 2EA FASTENER HOLES AT #1 AND #8 COMMON TO HORIZONTAL STIFFENER AT RBL27 AND LBL27. REF REO 601R-53-61-7745 REV. -- DATED 2021-11-16 . COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD . SEE CONTINUATIN CARD FOR DETAILS

Part: NONE — DENTED · airframe 46,142 hrs · 39,408 cycles

PAX DOOR HAVE A DENT ON AFT CORNER OUTER SKIN BETWEEN FS338.00 AND FS347.25 (C-CHECK RO 12/04/2021) REPAIRED PAX DOOR DENT ON AFT CORNER OUTER SKIN BETWEEN FS338.00 AND FS347.25 PER REO601R-52-11-2902 DATED 2021-11-14. COMPLIED WITH 51-900-1003-SKY.

Part: NONE — CRACKED · airframe 46,142 hrs · 39,408 cycles

INTERCOSTAL PN.601R350121-1 IS CRAKED ON THE AFT SIDE OF THE FS.621 BULKHEAD, OTBD ON STGR.16L (C-CHECK RO 12/04/2021) REMOVED, LOCATED, DRILLED AND REPLACED INTERCOSTAL PN.601R350121-1 CRAKED ON THE AFT SIDE OF THE FS.621 BULKHEAD, OTBD ON STGR.16L IAW DWG 601-35012 REV -D, CRJ200 SRM 51-42-21 AND SRM 51-40-11. COMPLIED WITH 51-900-1003-SKY SEE CONTINUATION CARD FOR DETAILS

Part: NONE — CRACKED · airframe 46,142 hrs · 39,408 cycles

R/H SIDE CLIP AT FS 625.0 STR 14 IS CRACKED. (C-CHECK RO 12/04/2021) REMOVED AND REPLACED R/H SIDE CLIP WITH NEW AT FS 625.0 STR 14 REF CRJ 200 SRM 51-42-21, CRJ 200 SRM 51-40-06, CRJ 200 51-21-16 AND DWG 601-35012 REV -D COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: NONE — DAMAGED · airframe 46,142 hrs · 39,408 cycles

REPLACE RH INBOARD FLAP OUTBOARD VANE CAP LEADING EDGE (C-CHECK RO 12/04/2021) REMOVED AND INSTALLED RH INBOARD FLAP OUTBOARD VANE CAP LEADING EDGE IAW CRJ 200 SRM 51-42-10 PG 4 AND DWG 601R14302 REV E. COMPLIED WITH 51-900-1003-SKY . SEE CONTINUATION CARD FOR DETAILS

Part: NONE — DAMAGED · airframe 46,142 hrs · 39,408 cycles

REPLACE RH INBOARD FLAP INBOARD VANE CAP LEADING EDGE (C-CHECK RO 12/04/2021) REMOVED AND INSTALLED NEW RH INBOARD FLAP INBOARD VANE CAP LEADING EDGE REF CRJ-200-SRM 51-42-13 AND DRAWING 601R14302 REV E . COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS

Part: NONE — DAMAGED · airframe 46,142 hrs · 39,408 cycles

REPLACE RH INBOARD FLAP CENTER VANE CAP LEADING EDGE (C-CHECK RO 12/04/2021) REMOVED AND INSTALLED NEW R/H INBOARD FLAP CENTER VANE CAP REF CRJ 200 SRM 51-42-10 PG 4. AND DWG 601R14302 REV E. COMPLIED WITH 51-900-1003-SKY

Part: NONE — CORRODED · airframe 46,142 hrs · 39,408 cycles

*RBL9 FLOOR BEAM CAP HAS CORROSION BETWEEN FS559+48 AND FS559+79. (C-CHECK RO 12/04/2021) REMOVED AND INSTALLED NEW FLOOR BEAM SECTION FOR FS 559+10 TO FS 570 REF REO 601R-53-51-608 REV -- DATED 2021-11-10 AND DRAWING 601R31119 REV H . COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS

Part: NONE — CHAFED · airframe 46,142 hrs · 39,408 cycles

RH AILERON HAS CHAFFING ON UPPER FWD LEADING EDGES. (C-CHECK RO 12/04/2021) REMOVED AND INSTALLED NEW R/H AILERON LEADING EDGE SKIN REF CRJ-200 SRM 51-42-06, SRM 51-42-21, SRM 51-42-22 AND DWG CC670-13000 REV -D. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS

Part: NONE — CORRODED · airframe 46,142 hrs · 39,408 cycles

*CORROSION ON CROSSBEAM CAP STRIP AT FS589 BETWEEN LBL9 AND LBL27. (C-CHECK RO 12/04/2021) REMOVED AND REPLACED CAP STRIP P/N 601R35031-165 WITH A NEW UNIT IAW CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND BOMBARDIER DRAWING 601R35031 REV. Y. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: NONE — CORRODED · airframe 46,142 hrs · 39,408 cycles

*FLOOR BEAM UPPER CAP AT LBL9 BETWEEN FS569 AND FS610 HAS CORROSION. (C-CHECK RO 12/04/2021) REPLACED FLLOR BEAM LBL9 BETWEEN FS569 AND FS610 PER CRJ200 SRM 51-23-00 , SRM 51-42-21 , SRM 51-45-00 , / SRM 51-42-22 & SRM 51-42-34 PER STEPS 1 THROUGH 5 OF MHI RJ R.E.O. 601R-53-61-7744 REV. -- DATED 2021-11-06 . C/W WITH SKYWEST TASK CARD 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS

Part: NONE — CORRODED · airframe 46,142 hrs · 39,408 cycles

*FLOOR BEAM UPPER CAP AT LBL27 BETWEEN FS569 AND FS610 HAS CORROSION AND CRACKS. (C-CHECK RO 12/04/2021) REPLACED FLOOR BEAM LBL9 BETWEEN FS569 AND FS610 PER CRJ200 SRM 51-23-00 , SRM 51-42-21 , SRM 51-45-00, SRM 51-42-22 & SRM 51-42-34 PER MHI RJ R.E.O. 601R-53-61-7744 REV. -- DATED 2021-11-06, REF BOMBARD DWG 601R35031 REV AG. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: NONE — CORRODED · airframe 46,142 hrs · 39,408 cycles

*CORROSION ON RH FLOOR SILL BETWEEN FS559 AND FS559+16. (C-CHECK RO 12/04/2021) REMOVED AND REPLACED RH FLOOR SILL BETWEEN FS.559-FS.559+16. REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21 AND DWG 601R31003 REV.K. ALL CHECKS GOOD. COMPLIED WITH 51-900-1003-SKY.

Part: NONE — GOUGED · airframe 46,142 hrs · 39,408 cycles

*RIGHT AILERON IS GOUGED ON THE FWD AREA OF THE RIB @STA 302.649 (C-CHECK RO 12/04/2021) REMOVED AND INSTALLED NEW RIB P/N CC670-13025-2, REF. MHIRJ 200 DWG. CC670-13000, REV. D, CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-13. SEE CONTINUATION CARD FOR DETAILS

Part: NONE — CRACKED · airframe 46,142 hrs · 39,408 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: AD 2019-08-04/02 40000 FC - COMPLY WITH PARAGRAPH (J) OF AD 2019-08-04 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL 53-61-153 OF BOMBARDIER TR 2B-2187, DATED JUNE 22, 2011, TO APPENDIX B€“AIRWORTHINESS LIMITATIONS, OF PART 2 OF THE BOMBARDIER CL-600-2B19 MRM. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO) 601R-53-61-1240, REVISION D, DATED OCTOBER 31, 2016. AND MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE, PART NUMBER: - , SERIAL NUMBER: 7664, POSITION: (C-CHECK RO 12/04/2021) COMPLIED WITH PARAGRAPH (J) OF AD 2019-08-04/02 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL 53-61-153 OF BOMBARDIER TR 2B-2187, DATED JUNE 22, 2011, TO APPENDIX B€“AIRWORTHINESS LIMITATIONS, OF PART 2 OF THE BOMBARDIER CL-600-2B19 MRM. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO) 601R-53-61-1240, REVISION D, DATED OCTOBER 31, 2016. AND; MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE. COMPLIED WITH SERIAL NUMBER 7664. COMPLIED WITH PERMANENT REPAIR REF REO 601R-53-61-1240 REV -D DATED 2016-10-31, AND COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY

Part: NONE — GOUGED · airframe 46,142 hrs · 39,408 cycles

*SERVICE DOOR HAS GOUGES ON EXTERNAL SKIN. AREAS MARKED (C-CHECK RO 12/04/2021) BLENDED GOUGE DAMAGE FROM SERVICE DOOR EXTERNAL SKIN REF CRJ 200 SRM 51-12-00. BLENDED AREA FOUND TO BE OUT OF LIMIT REF CRJ 200 SRM 52-00-31. REPAIRED SERVICE DOOR EXTERNAL SKIN REF REO 601R-52-41-474 REV -- DATED 2021-10-25. SEE CONTINUATION CARD FOR DETAILS

Part: NONE — DENTED · airframe 46,142 hrs · 39,408 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA55795-601R-53-61-7268 REV 923SW MXCODEID50571-PR - LARGE DENT IN OUTSIDE FUSELAGE SKIN AT CARGO DOOR CUT OUT LOWER AFT CORNER FS605.00 - FS619.00 BELOW STR17L. COMPLIED WITH TEMPORARY REPAIR PER REO 601R-53-61-7268 REV. PERMANENT REPAIR DUE WITHIN 5600 FLT HRS BY 49296.4., PART NUMBER: - , SERIAL NUMBER: 7664, POSITION: (C-CHECK RO 12/04/2021) REPAIRED DENT IN FUSELAGE SKIN AT AFT CARGO DOOR CUTOUT LOWER/AFT CORNER PER REO 601R-53-00-034 REV -J, DATED 2014-05-22 AND CRJ200 SRM 51-42-21. SEE CONTINUATION CARD FOR DETAILS. CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: DOOR FRAME — CRACKED (PAX DOORWAY) · airframe 45,450 hrs · 38,824 cycles

PAX DOOR CUTOUT, UPPER/FWD STOP-FITTING IS CRACKED. (FILED CLOSED) REMOVED AND INSTALLED NEW PAX DOOR CUTOUT, UPPER/FWD STOP-FITTING WITH SERVICEABLE PART IAW CRJ 200 SRM 51-42-21. / REF CP 22736778 FOR OPS CHECKS DISCREPANCIES.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 43,270 hrs · 36,844 cycles

*L/H FLOOR SEAT TRACK AT LBL9 HAS MULTIPLE AREA OF CORROSION FROM FS364 TO FS409. (C-CHECK) RO: 10/22/19. BLENDED FLOOR SEAT TRACKS AT LBL9 FS364.00 TO FS409.00 IAW SRM, FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED SEAT TRACKS LBL9 FS364.00 TO FS 409.00 IAW AMM.

Part: FRAME — CORRODED (BS 333) · airframe 43,270 hrs · 36,844 cycles

FOUND CORROSION ON FS 333 FRAME BETWEEN STR 18R TO STR 23R. (C-CHECK) RO: 10/22/19. REMOVED CORROSION ON FS 333 FRAME AT STRINGER 23R AND 24R IAW SRM. FOUND OUT OF LIMIT IAW SRM 53-00-00.REMOVED AN INSTALLED FS 333 NEW FRAME SECTOR FROM STR 18R TO STR 23R IAW SRM. LEAK CHECKS GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 43,270 hrs · 36,844 cycles

* R/H FLOOR SUPPORT STRUCTURE FLOOR EDGE MEMBER ( SILL ) / FS559.0+80 TO FS621.0 , (C-CHECK) RO: 10/22/19. 559+80 TO 569 FOUND OUT OF LIMITS, REPLACED. SILL FOUND WITHIN LIMITS BOMBARDIER.

Part: FLOOR SUPPORT — CORRODED (BS 310) · airframe 43,270 hrs · 36,844 cycles

*L/H FLOOR SUPPORT AT FS310, APPROX LBL40 HAS CORROSION. LOCATED NEAR THE FWD END OF THE PAX DOOR. MARK WITH GREASE PENCIL. (C-CHECK) RO: 10/22/19. PERFORMED BLEND OUT OF CORROSION AT L/H FLOOR SUPPORT FS 310.00, LBL 40. IAW SRM. FOUND TO BE WITHIN LIMITS. RESTORED FINISH.

Part: FLOOR SUPPORT — CORRODED · airframe 43,270 hrs · 36,844 cycles

*PLATES ON FLOOR SUPPORT IN FWD CABIN WHERE THE WARDROBE MOUNTS HAVE CORROSION AROUND THE BOLT HOLES. LOCATIONS ARE OTBD AFT, INBD FWD, AND INBD AFT. (C-CHECK) RO: 10/22/19. BLENDED OUT CORROSION ON WARDROBE FLOOR SUPPORT MOUNT PLATES, FABRICATED NEW WARDROBE FLOOR MOUNT PLATE FOR INBD AFT LOCATION, REMOVED DAMAGED PLATE AND INSTALLED NEW PLATE IAW SRM, RESTORED FINISH AT ALL LOCATIOSIAW SRM.

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 43,270 hrs · 36,844 cycles

FS 409.00 + 128 RBL 27.00 VERTICAL BEAM IS CRACKED LOWER INBOARD CORNER AS MARKED. (C-CHECK) RO: 10/22/19. REPLACED WITH NEW FS409.00+128 RBL27.00 VERTICAL BEAM IAW. LEAK CHECK AND OPS TEST GOOD.

Part: FRAME — CORRODED (BS 513) · airframe 43,270 hrs · 36,844 cycles

FS 513 APPROX STR17 R/H FRAME FWD LOWER INBOARD CORNER HAS CORROSION AS MARKED. (C-CHECK) RO: 10/22/19. PERFORMED BLEND OUT OF CORROSION AT FS 513.00 APPROX. STGR.17 FRAME FWD. LOWER I/B CORNER. IAW SRM. FOUND TO BE WITHIN LIMITS. IAW SRM. RESTORED FINISH.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 43,270 hrs · 36,844 cycles

*R/H INBD FLAP VANE LEADING EGDE IS CHAFED AT 3EA LOCATIONS. INBD,CNT, AND OTBD. (C-CHECK) RO: 10/22/19. BLENDED OUT CHAFFING AT 3 EACH LOCATIONS ON THE RH IB FLAP VANE TO A SMOOTH CONTOUR.FOUND THE O/B AND I/B WITH IN LIMITS AND MIDDLE OUT OF LIMITS. REMOVED AND REPLACED MIDDLE VANE SKIN WITH NEW ONE.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 43,270 hrs · 36,844 cycles

*L/H FLOOR SEAT TRACK AT LBL9 HAS MULTIPLE AREA OF CORROSION FROM FS409 TO FS409+128. (C-CHECK) RO: 10/22/19. BLENDED FLOOR SEAT TRACKS AT LBL9 FS409.00 TO 409+128 IAW SRM, FOUND TO BE OUT OF LIMITS IAW SRM, REMOVED AND REPLACED SEAT TRACKS LBL9 FS409 TO FS409+128 IAW AMM.

Part: FRAME — CORRODED (BS 349) · airframe 43,270 hrs · 36,844 cycles

*CORROSION FOUND ON FRAME FS349.00, STGR27 .FLAGGED. (C-CHECK) RO: 10/22/19. BLENDED OUT OF CORROSION ON FRAME AR FS349.00 STGR27 IAW SRM 51-21-06. FOUND TO BE WITHIN LIMITS IAW SRM. RESTORED TOPCOAT FINISH.

Part: ANGLE — CRACKED (BS 280 FLOORBEAM) · airframe 43,270 hrs · 36,844 cycles

FS280 RBL9 I/B ANGLE CRACKED IN RADIUS, TOP OF ANGLE. (C-CHECK) RO: 10/22/19. FABRICATED NEW ANGLE AND REPLACED IAW REO.

Part: FLOOR SUPPORT — CORRODED (NO REPORTED) · airframe 43,270 hrs · 36,844 cycles

*FLOOR SUPPORT AT PAX DOOR OPEN HAS CORROSION ON THE CUPS FOR THE HAND RAIL SUPPORT STRUTS. (C-CHECK) RO: 10/22/19. PERFORMED BLEND OUT OF CORROSION ON PAX DOOR CUT OUT SURROUND FLOOR STRUCTURE IAW SRM. FOUND TO BE WITHIN LIMITS. RESTORED FINISH.

Part: BRACKET — DAMAGED (NLG PROX SENSOR) · airframe 40,782 hrs · 34,658 cycles

AFTER TAKE OFF, PUT THE GEAR UP BUT NOSE GEAR WOULD NOT COME UP. WARNING ILLUMINATED, GEAR DISAGREE. PERFORMED QRH AND DIVERTED. REPLACED THE OLEO PROXIMITY SENSOR BRACKET AND ADJUSTED THE SENSOR IAW AMM.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 38,658 hrs · 32,797 cycles

FS 280 FWD FLOORBEAM ANGLE UPPER SURFACE HAS CORROSION. REMOVED AND REPLACED FWD FLOORBEAM ANGLE IAW SRM.

Part: PLATE — CHAFED (RT WING TE FLAP) · airframe 38,658 hrs · 32,797 cycles

RIGHT WING AFT FLAP HINGE ARM UNDER PANEL 683BB CHAFED ON THE INBD & OTBD GUIDE PLATE. REPLACED THE GUIDE PLATES IAW SRM.

Part: PLATE — GOUGED (RT WING TE FLAP) · airframe 38,658 hrs · 32,797 cycles

RIGHT WING AFT FLAP HINGE ARM LOCATED UNDER PANEL 686BB HAS GOUGE INBD GUIDE PLATE. REPLACED OUT OF LIMITS ATTACHMENT BRACKET IAW SRM.

Part: HINGE ARM — GOUGED (RT WING TE FLAP) · airframe 38,658 hrs · 32,797 cycles

RIGHT WING FLAP AFT HINGE ARM LOCATED UNDER PANEL 695BB HAS A GOUGE AND HAS A WORN INBD GUIDE PLATE. REMOVED AND REPLACED BRACKET WITH SERVICEABLE BRACKET IAW SRM.

Part: LEVER — CHAFED (PAX DOOR) · airframe 38,658 hrs · 32,797 cycles

PAX DOOR FWD PULL IN LEVER CHAFED. REPLACED LEVER IAW REO. WARNING AND OPERATIONAL CHECKED GOOD

Part: CONTROL PANEL — FAILED (MLG) · airframe 38,609 hrs · 32,751 cycles

GEAR DISAGREE ON TAKEOFF. GEAR DID NOT RETRACT. RETURNED TO THE FIELD. REPLACED ACMP AND REPLACE GEAR SELECTOR PANEL. OPS NORMAL.

Part: THRUST REVERSER — MALFUNCTIONED (LEFT) · airframe 37,680 hrs · 31,918 cycles

LEFT THRUST REVERSER UNLOCK MESSAGE IN FLIGHT. RAN QRH, LEFT THRUST REVERSER DID NOT STOW, INSTRUCTED TO SHUT DOWN LEFT ENGINE IAW QRH. LANDED SINGLE ENGINE UNEVENTFULLY.

Part: TRANSDUCER — MALFUNCTIONED (RT ENGINE OIL) · airframe 34,827 hrs · 29,363 cycles

ACFT RETURNED TO DEPARTURE AFTER THE RT ENGINE OIL PRESSURE WENT TO ZERO ON CLIMB OUT. CREW FOLLOWED THE QRH PROCEDURE AND SHUTDOWN THE RT ENG. CREW REPORTED THAT THEY DID NOT LAND OVERWEIGHT AND THEY DID DECLARE AN EMERGENCY. R & R NR 2 ENGINE OIL PRESSURE TRANSDUCER IAW AMM. RAN ENGINE NR 2 AND OIL PRESSURE INDICATION NORMAL AND NO LEAKS NOTED.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 34,127 hrs · 28,747 cycles

LT INBD FLAP OTBD CENTER FLAP VANE CAP CHAFED OUT OF LIMITS. R & R THE FLAP VANE IAW REO AND SRM.

Part: LIGHT — FAILED (EXTERIOR) · airframe 31,839 hrs · 26,769 cycles

LEFT EXTERNAL NR 2 EMERGENCY LIGHT INOPERATIVE. R & R EXTERNAL NR 2 EMERGENCY LIGHT IAW AMM.

Part: SKIN — DENTED (BS 201) · airframe 31,839 hrs · 26,769 cycles

THERE IS A DENT LOCATED ON THE LT SIDE FUSELAGE AT BS 201. BETWEEN S23-24L. REPAIRED IAW REO.

Part: SKIN — DENTED (BS 193-202) · airframe 31,786 hrs · 26,731 cycles

FOUND A DENT ON THE LEFT FUSELAGE SKIN BETWEEN BS 193 AND 202.75 S23-24L IN THE RVSM ZONE 4. REPAIRED IAW REO.

Part: SHUTOFF VALVE — FAILED (RT A/C PACK) · airframe 31,365 hrs · 26,403 cycles

RECEIVED RT PACK HIGH PRESSURE CAUTION. COULD NOT OBTAIN CLIMB THRUST WITH OUT OVERPRESSURIZING RT PACK. R & R RT PACK PRSOV IAW AMM. NO RT PACK "HI PRESS" CAUTION MESSAGE PRESENT DURING SINGLE PACK OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,270 hrs · 26,334 cycles

LIGHTED EMERGENCY EXIT SIGN ADJACENT TO THE PAX DOOR HAS ONE LAMP INOPERATIVE. REPLACED THE LAMP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,947 hrs · 26,070 cycles

EMERGENCY OVERHEAD LIGHT IS BURNED OUT, RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,458 hrs · 25,646 cycles

EMERGENCY LIGHT POD AT MCD IS BURNED OUT, REPLACED LAMP.

Part: POST — CRACKED (FUSELAGE) · airframe 29,804 hrs · 25,152 cycles

CRACK NOTED ON FS 409+128 VERT POST AT LBL18, INBD C-CHANNEL IN THE AFT RADIUS. C-CHECK COMPLIED WITH PERMANENT REPAIR OF FS409 + 128 VERT POST IAW REO & SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,804 hrs · 25,152 cycles

CRACK NOTED ON FS 621 BULKHEAD WEB, FWD FACE, ALONG BL0.0 AT APPROXIMATELY WL115. C-CHECK COMPLIED WITH PERMANENT REPAIR OF FS 621 BULKHEAD IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 29,804 hrs · 25,152 cycles

LT INBD FLAP VANE CHAFED ON THE INBD SIDE. C-CHECK CHAFE ON THE LT INBD FLAP VANE INBD LE SECTION, WAS BLENDED IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 29,804 hrs · 25,152 cycles

CRACK NOTED ON FS 409+128 VERT POST AT BL0.0, RT C-CHANNEL IN THE AFT RADIUS. C-CHECK COMPLIED WITH PERMANENT REPAIR OF FS409 + 128 VERT POST IAW REO & SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 29,804 hrs · 25,152 cycles

FS 280 RBL 9 INBD CLIP CRACKED. C-CHECK REPLACED CLIP AT FS 280 RBL 9 WITH NEW FABRICATED CLIP IAW REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 29,804 hrs · 25,152 cycles

LBL 9 FS 280 INBD & OTBD CLIPS CRACKED. C-CHECK REPLACED LBL 9 FS 280 INBD & OTBD CLIPS IAW REO.

Part: FAIRING — CHAFED (TE FLAP) · airframe 29,804 hrs · 25,152 cycles

RT WING FLAP STUB FAIRING IS CHAFED. C-CHECK REPLACED RT WING FLAP STUB IAW SRM & REO.

Part: VANE — CHAFED (TE FLAP) · airframe 29,804 hrs · 25,152 cycles

RT INBD FLAP VANE CHAFED ON THE INBD SIDE. C-CHECK CHAFE ON THE RT INBD, FLAP VANE, INBD LE SECTION WAS BLENDED IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 29,804 hrs · 25,152 cycles

RT INBD FLAP VANE CHAFED ON THE OTBD SIDE. C-CHECK CHAFE ON THE RT INBD. FLAP VANE, OTBD, LE SECTION, WAS BLENDED IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 29,804 hrs · 25,152 cycles

LT INBD FLAP VANE CHAFED IN THE MIDDLE. C-CHECK CHAFE ON THE LT INBD FLAP VANE OTBD MIDDLE LE WAS BLENDED IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 29,804 hrs · 25,152 cycles

RT INBD FLAP VANE CHAFED IN THE MIDDLE. C-CHECK CHAFE ON THE RT INBD, FLAP VANE, OTBD MID LE SECTION, WAS BLENDED IAW REO.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 29,804 hrs · 25,152 cycles

FS202 FWD LT SIDE IS CRACKED ABOVE PARKING BRAKE CONTROL ROD. C-CHECK PERMANENTLY REPAIRED FS 202 FWD LT SIDE CRACK AT PARKING BRAKE CONTROL ROD PASS THRU IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 29,804 hrs · 25,152 cycles

LT INBD FLAP VANE CHAFED ON THE OTBD SIDE. C-CHECK CHAFE ON THE LT INBD FLAP VANE, OTBD LE SECTION WAS BLENDED IAW REO.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 29,552 hrs · 24,957 cycles

EMERGENCY LIGHTS ON FLOOR LEVEL BETWEEN ROWS 1-5 DO NOT ILLUMINATE. FLT#5370 REPAIRED CONNECTOR FOR FLOOR TRACK LIGHTS 2-5.

Part: WINDOW — CRACKED (COCKPIT) · airframe 28,168 hrs · 23,868 cycles

F/O'S SIDE WINDOW CRACKED. (FLT 6473) REPLACED RIGHT SIDE WINDOW IAW AMM. P/N ON: NP139322-12 S/N ON: 12305H5316 P/N OFF: NP139322-6 S/N OFF: 030107R2172.

Part: WIRE HARNESS — FAILED (NLG STEERING) · airframe 27,741 hrs · 23,532 cycles

ON TAXI AIRCRAFT PULLS TO THE RIGHT, RUDDER AND TILLER INPUTS JERKY, VEERED SHARPLY TO LEFT, STEERING INOP MESSAGE. (FLT 6248) REPLACED NOSE WHEEL STEERING HARNESS ASSEMBLY, ADJUSTED THE LEFT RVDT. P/N: 17300-233

Part: SCUFF PLATE — DAMAGED (FUSELAGE) · airframe 27,698 hrs · 23,502 cycles

SCUFF PLATE DAMAGED BELOW CARGO DOOR. (FLT 5606) REPLACED CARGO DOOR SCUFF PLATE IAW REO AND AMM.

Part: UNKNOWN — ODOR · airframe 27,191 hrs · 23,118 cycles

GAS SMELL WAS DETECTED AFTER STARTING THE APU. (FLT 5333) INSPECTED APU FUEL LINE OVERBOARD DRAIN NO LEAKS NOTED, FUEL SMELL DISSIPATED.

Part: INVERTER — FAILED (CABIN) · airframe 26,726 hrs · 22,761 cycles

FLOOR LEVEL ELECTRO LUMINESCENT AND LOWER EMERGENCY LIGHT AT SEAT 8D IS INOPERATIVE. (FLT 5444) REPLACED EMERGENCY LIGHT INVERTER AT ROW 9 IN REFERENCE TO AMM.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 26,686 hrs · 22,731 cycles

FLOOR LEVEL ELECTRO LUMINESCENT AND LOWER EMERGENCY EXIT LIGHTS AT ROW 8CD ARE INOPERATIVE. (FLT 5620) RESET CIRCUIT BREAKER AT 4 C2.

Part: CONNECTOR — OUT OF ADJUST (CABIN) · airframe 26,624 hrs · 22,684 cycles

FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 6 TO 8 ARE INOPERATIVE. (FLT 5603) ADJUSTED FLOOR STRIP EMERGENCY LIGHTING CONNECTION AT SEATS 6 TO 8BC IN REFERENCE TO MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,348 hrs · 22,458 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,164 hrs · 22,298 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5468) RELAMPED EMERGENCY LIGHT.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 25,824 hrs · 22,042 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. (FLT 6433) LUBRICATED THE MAIN CABIN DOOR IN REFERENCE TO 200 AMM.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 25,365 hrs · 21,668 cycles

FLT 6347, AFT OVERHEAD EMERGENCY LIGHT IS OUT. RESEATED THE CONNECTION FOR THE AFT OVERHEAD LIGHTING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,294 hrs · 21,612 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6432) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,139 hrs · 21,490 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5554) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,110 hrs · 21,466 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6368) RELAMPED EMERGENCY LIGHT.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 25,038 hrs · 21,415 cycles

C-CHECK, FLOORBEAM UPPER SUPPORT ANGLE CRACKED AT FS 280 LBL 9. REPAIRED CRACK ON FLOORBEAM UPPER SUPPORT ANGLE AT FS 280 LBL 9.

Part: SILL — CORRODED (FUSELAGE) · airframe 25,038 hrs · 21,415 cycles

PASSENGER DOOR SILL CORRODED AT FLOOR SUPPORT LONGERON. (C-CHECK) REPAIR PASSENGER DOOR SILL AT FLOOR SUPPORT LONGERON.

Part: SEAL — DAMAGED (SERVICE DOOR) · airframe 24,704 hrs · 21,167 cycles

LOUD THUMPING SOUND EMANATING FROM SERVICE DOOR/GALLEY AREA. (FLT 6472) REPAIRED SERVICE DOOR SEAL PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,613 hrs · 21,088 cycles

CEILING LEVEL EMERGENCY LIGHT AT ROW 5 IS OUT. (FLT 6389) REPLACED NR 3 EMERGENCY BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,613 hrs · 21,088 cycles

RIGHT SIDE EMERGENCY OVERWING EXIT SIGN IS OUT. (FLT 6389) REPLACED NR 4 EMERGENCY BATTERY PACK.

Part: LIGHT — BURNED OUT (CABIN) · airframe 24,456 hrs · 20,971 cycles

THE 3RD OVERHEAD EMERGENCY LIGHT NOT ILLUMINATED. (FLT 5376) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — DIRTY (CABIN) · airframe 24,456 hrs · 20,971 cycles

AFT 1/3 OF FLOOR EMERGENCY LIGHTS ARE OUT. (FLT 6250) CLEANED AND RE-SECURED AFT FLOOR EMERGENCY LIGHT CONNECTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,444 hrs · 20,957 cycles

NR 3 AND 4 OVERHEAD EMERGENCY LIGHT ARE OUT. (FLT 5312) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — LOOSE (CABIN) · airframe 24,355 hrs · 20,870 cycles

AFT ROW OF FLOOR EMERGENCY LIGHTS ARE OUT. (FLT 5502) RE-SECURED LOOSE CONNECTORS ON AFT ROW EMERGENCY FLOOR LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,187 hrs · 20,724 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5424) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,124 hrs · 20,672 cycles

NR 3 OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 6292) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,993 hrs · 20,547 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6377) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,992 hrs · 20,545 cycles

THE 3RD OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5418) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,897 hrs · 20,457 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6456) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,761 hrs · 20,347 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6407) RELAMPED EMERGENCY LIGHT.

Part: UNKNOWN — DAMAGED · airframe 23,546 hrs · 20,190 cycles

FLT 5407, HAIL DAMAGE TO FUSELAGE AND FLIGHT CONTROLS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,471 hrs · 20,131 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6460) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,440 hrs · 20,099 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5478) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,440 hrs · 20,099 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5394) RELAMPED EMERGENCY LIGHT.

Part: RESERVOIR — DEFECTIVE (HYDRAULIC SYS) · airframe 23,248 hrs · 19,952 cycles

GEAR DISAGREE WARNING MSG RIGHT MAIN GEAR FAILED TO COME DOWN. RECYCLED GEAR HANDLE GEAR DEPLOYED NORMALLY. (FLT 6424) REPLACED NR 3 HYDRAULIC RESERVOIR, NR 3A AND NR 3B HYDRAULIC PUMP AND RIGHT MLG SIDESTAY ACTUATOR.

Part: SELECTOR VALVE — FAULTY (MLG) · airframe 23,215 hrs · 19,923 cycles

AFTER GEAR SELECTED DOWN RECEIVED GEAR DISAGREE WARNING MESSAGE. (FLT 6440) REPLACED MAIN GEAR SELECTOR VALVE AND RIGHT SIDE STAY ACTUATOR. P/N 750005000, S/N OFF 0935, P/N 17008-115, S/N OFF 00735

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,124 hrs · 19,850 cycles

EMERGENCY CEILING LIGHT ABOVE ROW 10 IS INOPERATIVE. (FLT 6692) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,917 hrs · 19,685 cycles

NR 2 CEILING EMERGENCY LIGHT IS OUT. (FLT 6581) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,300 hrs · 19,238 cycles

OVERHEAD EMERGENCY LIGHT OVER ROW 5 IS OUT. (FLT 6639) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,267 hrs · 18,314 cycles

BULB BURNED OUT ON THE MAIN CABIN DOOR EMERGENCY FLOOD LIGHT. (FLT 6138) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,006 hrs · 18,061 cycles

LOWER GALLEY EMERGENCY LIGHTS (3) BURNED OUT. (FLT 6826) RELAMPED LIGHT BULBS AS REQUIRED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,655 hrs · 17,760 cycles

FS 621 BULKHEAD WEB CRACKED AT TOP OF CARGO DOOR TRACK. (C CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,605 hrs · 17,724 cycles

FLOOR LEVEL EMERGENCY FLOOD LIGHT INOP. (FLT 6895) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,838 hrs · 17,096 cycles

NR 2 CEILING EMERGENCY LIGHT INOP. (FLT 6093) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,234 hrs · 16,609 cycles

CABIN EMERGENCY CEILING FLOODLIGHT NR 4 INOP. (FLT 6487)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,954 hrs · 16,356 cycles

CEILING EMERGENCY FLOODLIGHT NR 2 INOP. (FLT 6699) RELAMPED EMERGENCY LIGHT.

Part: HANDLE — DIRTY (PAX DOOR) · airframe 17,190 hrs · 14,972 cycles

FLT 6024 - UNABLE TO OPEN MAIN CABIN DOOR UPON ARRIVAL TO THE AIRCRAFT. CLEANED AND LUBRICATED PAX DOOR OUTER HANDLE.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 16,643 hrs · 14,532 cycles

LOWER FLOORBEAM ANGLE CRACKED AT LBL 9 FS 280(C-CHECK). REPAIRED PER REO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 16,643 hrs · 14,532 cycles

UPPER FLOORBEAM ANGLE CRACKED AT LBL 9 AND RBL 9 (C-CHECK). REPAIRED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 16,643 hrs · 14,532 cycles

C-CHECK, FLOOR SUPPORT INBOARD AND OUTBOARD CLIPS CRACKED AT LBL9 AND RBL9 FS280. REPAIRED PER REO.

Part: IDG — LOW (NR 2) · airframe 16,416 hrs · 14,345 cycles

ON CLIMBOUT NR 2 GEN WENT OFF LINE. DURING RESET PROCEDURE ADG INADVERTENTLY DEPLOYED. (FLT 6532)SERVICED IDG.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,861 hrs · 11,217 cycles

FLT 6108 - MULTIPLE EMERGENCY EXIT LIGHTS ARE INOP. REPLACED TB105-1 AND NR 2 BATT AND CHARGER ASSEMBLY. OPS CHECK GOOD, P/N 1-2013-1A, S/N ON - 57038, S/N OFF - 68998, P/N 2 - N549-3156.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,803 hrs · 11,169 cycles

EMERGENCY LIGHT OVER EXIT ROW INOP. REPLACED THE NR 2 AND NR 3 BATTERY CHARGERS AND DIODE ASSEMBLY IAW AMM 33-51-05. OPS CHECK GOOD.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 11,768 hrs · 10,289 cycles

FS 280 BEAM HAS CRACK AT RT BL9, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER, FILLER AND CLIP PER REO 601R-53-11-171 REV (C).

Part: ANGLE — CRACKED (BS 280) · airframe 11,768 hrs · 10,289 cycles

FS 280 CRACKED ANGLE CLIP AT LH BL9, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP AS PER CRJ200 SRM 51-42-21.

Part: STRINGER CLIP — CRACKED (BS 625 S14R) · airframe 11,768 hrs · 10,289 cycles

CLIP AT FS 625 STR 14R IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP AT STA 625.0 STR 14R PER CRJ200 SRM 51-42-21 PGS 15-17.

Part: WEB — CRACKED (PAX DOOR) · airframe 11,768 hrs · 10,289 cycles

CRACK IN STEP WEB BEHIND FWD HANDRAIL DOWN LOCK SUPPORT BRACKET ON PAX DOOR, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER (-5) REPAIR ANGLES (-8 AND -10) PER REO 670-52-11-104.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 11,768 hrs · 10,289 cycles

FOUND RT AND LT WHEEL WELL BOTH HYDRAULIC PRESSURE TRANSDUCER BRACKETS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW TRANSDUCER BRACKETS LT AND RT WHEEL WELL PN 601R75262-157 AND 159 AS PER CRJ200 SRM 51-42-06 PGS 11-18.

Part: ANGLE — CRACKED (BS 280) · airframe 11,768 hrs · 10,289 cycles

FS 280 CRACKED ANGLE CLIP AT RT BL9, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP AS PER CRJ200 SRM 51-42-21.

Part: STRINGER CLIP — CRACKED (BS 623) · airframe 11,768 hrs · 10,289 cycles

CLIP AT FS 623 STR 14 LEFT CRACK, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP AT FS 623 STR 14 LEFT PER CRJ200 SRM 51-42-06 AND 51-42-21.

Part: WEB — CRACKED (PAX DOOR) · airframe 11,768 hrs · 10,289 cycles

PAX DOOR AFT WEB HAS 1.25" CRACK BENEATH COUNTER BALANCE GAS STRUT FRAME, MID DOOR AREA, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS IAW REO 601R-52-11-702 REV A.

Part: DETECTOR — MALFUNCTIONED (TE FLAPS) · airframe 9,464 hrs · 8,277 cycles

FLAPS DEGRADED STATUS MESSAGE. REPLACED SKEW DETECTOR UNIT. RESET FCU. OPERATIONAL CHECK GOOD, PN 601R59014-1 SN/OFF A290.

Part: CAUTION MESSAGE — FALSE INDICATION (STALL WARNING) · airframe 9,296 hrs · 8,135 cycles

STALL FAIL CAUTION MESSAGE INTERMITTENT INFLIGHT AND WHILE TAXI. REPLACED CAPTAINS STICK SHAKER IAW MM 27-35-10. OPERATIONAL TEST GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 8,848 hrs · 7,730 cycles

LEFT WINDSHIELD CRACKED, CLIMBING THROUGH FL290. REPLACED LEFT WINDSHIELD IAW AMM 56-11-01, PN NP-239321-5, SN OFF 02059H9733.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 8,678 hrs · 7,576 cycles

STALL FAIL CAUTION MESSAGE ILLUMINATED ON APPROACH TO ORD WITH LANDING GEAR DOWN FLAPS 30 DEGREES. REPLACED STALL PROTECTION COMPUTER. OPERATIONAL CHECK GOOD IAW CRJ AMM 27-35-01.

Part: PROXIMITY SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 8,727 hrs · 7,626 cycles

FLAPS DEGRADED STATUS MSG. REPLACED NR 3 AND NR 4 ACTUATOR PROX SENSORS ON RT SIDE IAW M/M 27-51-15. OPERATIONAL CHECK GOOD.

Part: TRIM SWITCH — MALFUNCTIONED (COCKPIT) · airframe 8,666 hrs · 7,562 cycles

CAPTAIN TRIM SWITCH STICKS. REPLACED CAPTAIN TRIM SWITCH. OPERATIONAL CHECK GOOD IAW MM 27-41-00.

Part: SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 8,652 hrs · 7,548 cycles

FLAPS DEGRADED MSG. REPLACED LT SENSORS NR 3 AND 4 IAW 27-51-15, OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 8,426 hrs · 7,347 cycles

ON APPROACH TO SLC SELECTING FLAPS 8, FLAPS FAIL CAUTION MSG ILLUMINATED. REPLACED ALL RT AND LT FLAP ACTUATORS PER CRJ MM 27-53-00. OPERATIONAL CHECK GOOD.

Part: DETECTOR — MALFUNCTIONED (FLAP SKEW) · airframe 8,426 hrs · 7,347 cycles

FLAPS DEGRADED STATUS MSG INFLIGHT. REPLACED SKEW DETECTION UNIT IAW AMM 27-51-15, OPERATIONAL CHECK GOOD.

Part: WINDOW — FAILED (COCKPIT) · airframe 8,222 hrs · 7,167 cycles

RT SIDE WINDOW SHATTERED IN FLIGHT. REPLACED FO'S RIGHT SIDE WINDOW IAW CRJ MM 56-12-00, PN/OFF NP-139322-6, SN/OFF 02057H9529.

Part: CONTROL UNIT — MALFUNCTIONED (STAB) · airframe 8,112 hrs · 7,075 cycles

RECEIVED A -STAB CH 1 INOP- STATUS MSG. REPLACED MOTOR CONTROL UNIT. OPERATIONAL CHECK GOOD REF 27-41-00.

Part: TRANSMITTER — MALFUNCTIONED (TE FLAPS) · airframe 7,727 hrs · 6,738 cycles

FLAPS DEGRADED STATUS MESSAGE DISPLAYED IN FLIGHT. REPLACED LT FLAP POSITION TRANSMITTER IAW MM 27-55-01. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 7,598 hrs · 6,630 cycles

FLAP 1/2 SPEED MESSAGE AND FLAP FAIL. REPLACED FECU IAW AMM TASK 27-51-05. OPERATIONAL CHECK GOOD. FLAPS HALFSPEED.

Part: DOOR — OUT OF ADJUST (CARGO BAY) · airframe 7,598 hrs · 6,630 cycles

MCD WON'T OPEN. CHECKED RIGGING AND ADJUSTED IAW AMM 52-11-02. OPERATIONAL CHECK GOOD.

Part: DOOR — OUT OF ADJUST · airframe 7,586 hrs · 6,622 cycles

MAIN CABIN DOOR VERY HARD TO OPEN. READJUSTED FWD AND AFT UPPER SPIGOT'S IAW AMM 52-11-21. OPERATIONAL CHECK GOOD.

Part: DETECTOR — MALFUNCTIONED (TE FLAPS) · airframe 7,547 hrs · 6,582 cycles

'FLAPS DEGRADED' STATUS MSG. REPLACED SKEW DETECTOR UNIT IAW MM 27-51-15. OPERATIONAL CHECK GOOD, PN 601R59014-1 OFF A381.

Part: DETECTOR — MALFUNCTIONED (SKEW) · airframe 7,540 hrs · 6,576 cycles

FLAPS DEGRADED MESSAGE ON DESCENT INTO LAX. TROUBLESHOOT FLAPS DEGRADED MESSAGE. REMOVED AND REPLACED SKEW DETECTOR IAW CRJ 200 MM 27-50-00. FLAPS OPERATE NORMALLY. NO DEFECTS, PN 601R59014-1; SN OFF A312.

Part: FRAME — CRACKED (FUSELAGE) · airframe 8,244 hrs · 7,187 cycles

FWD AVIONICS BAY FS 280 LT FRAME CRACKED BL-+8 AND +11 INBOARD OUTBOARD. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED TWO NEW BRACKETS IAW REO 601R-53-11-136.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,244 hrs · 7,187 cycles

MAIN CABIN FS 484.00 BC 28RT WL 72 ANGLE CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW SUPPORT ANGLE IAW REO 601R-53-41-059.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,244 hrs · 7,187 cycles

AFT CARGO FS 621 LT SIDE ANGLE CRACKED. REPAIR ANGLE IAW REI 601R 53-61-117.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,244 hrs · 7,187 cycles

MAIN CABIN FS 484.00 BL36R WL 72 ANGLE CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR ANGLE IAW RO 601R 53-41-059.

Part: FRAME — CRACKED (FUSELAGE) · airframe 8,244 hrs · 7,187 cycles

FWD AVIONICS BAY FS 280 RT FRAME CRACKED BL- +8 AND +11 INBOARD OUTBOARD. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED TWO NEW BRACKETS IAW REO 601R 53-11-136.

Part: SWITCH — MALFUNCTIONED (AUTOPILOT) · airframe 7,444 hrs · 6,502 cycles

ON DESCENT AUTOPILOT ON STAB/MACH TRIM 1 AND 2 AND DISCONNECTED. REPLACED CAPT STAB DISCONNECT SWITCH IAW CRJ MM27-41-30. OPERATIONAL CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 6,982 hrs · 6,145 cycles

LEFT WINDOW CRACKED ON FINAL APPROACH. REPLACED LEFT SIDE WINDOW IAW AMM 56-12-01. OPERATIONAL CHECK GOOD.

Part: CONTROL PANEL — INOPERATIVE (RUDDER TRIM) · airframe 6,624 hrs · 5,821 cycles

RUDDER TRIM DOESN'T MOVE RUDDER TRIM. REMOVED AND REPLACED RUDDER TRIM/AILERON TRIM CONTROL PANEL. OPERATIONAL CHECKS GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB) · airframe 5,939 hrs · 5,242 cycles

ON TAXI, MACH TRIM CAUTION MESSAGE WITH STAB TRIM CH 2 STATUS MESSAGE, HAPPENED 3 TIMES ON TAXI FROM HANGAR TO GATE. REMOVED AND REPLACED HSTCU IAW MM 27-41-01. OPERATIONAL CHECK GOOD.

Part: STICK SHAKER — INOPERATIVE (COCKPIT) · airframe 5,939 hrs · 5,242 cycles

DURING STALL WARNING TEST, NO STICK SHAKER WARNING ON EITHER SIDE. REPLACED PILOTS CAPT'S SIDE SHAKER FOR YOKE, OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 5,374 hrs · 4,764 cycles

STAB TRIM AND MACH TRIM CAUTION MESSAGES CAME ON DURING TAXI. REMOVED AND INSTALLED SERVICEABLE HSTCU IAW CRJ MM 27-41-01. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (FLIGHT SPOILER) · airframe 5,152 hrs · 4,570 cycles

RT SPOILERON CAUTION MESSAGE. REMOVED AND REPLACED RT OB SPOILERON PCU AND FLIGHT SPOILER LEVER IAW MM 27-61-01. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (SPOILER) · airframe 4,979 hrs · 4,423 cycles

LT HAND SPOILERON INOPERATIVE. REMOVED AND REPLACED LT IB SPOILERON PCU. OPERATIONAL CHECK GOOD IAW CRJ MM 27-62-01.

Part: WIRE — BROKEN (STICK SHAKER) · airframe 4,698 hrs · 4,175 cycles

DURING FFOD STALL TEST, STICK SHAKER DID NOT ACTUATE. REPAIRED WIRING TO FIRST OFFICER'S STICK SHAKER IAW MM 27-35-00. OPERATIONAL CHECK GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 4,698 hrs · 4,175 cycles

PASSENGER DOOR EMERGENCY LIGHT BROKEN. REMOVED AND REPLACED PASSENGER DOOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.

Part: FLOOR SUPPORT — CRACKED (CARGO BAY) · airframe 4,079 hrs · 3,583 cycles

DISCOVERED DURING C-CHECK INSPECTION, CARGO COMPARTMENT FLOOR SUPPORT ANGLE CRACKED AT FS 621.00 RBL 42.00. DAMAGE REPAIRED IAW CRJ REO 601R-53-61-117 REV. ''A'' AND RII53-401.

Part: NUT — BROKEN (RUDDER) · airframe 4,079 hrs · 3,583 cycles

DISCOVERED DURING C-CHECK INSPECTION, RUDDER LEFT SIDE ANCHOR NUT BROKEN AT CENTER HINGE PANEL ATTACH POINT. REPLACED ANCHOR NUT IAW CRJ SRM 51-45-00. REPLACED SEALANT IAW SRM 51-23-00.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,278 hrs · 3,795 cycles

CRACKED INTERCOSTAL AT STA X484.00 BETWEEN LBL 27 AND LBL 36 (OUTBOARD). DISCOVERED DURING C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW REO 601R-53-41-059 REV A.

Part: BRACKET — CRACKED (COCKPIT) · airframe 4,079 hrs · 3,583 cycles

DISCOVERED DURING C-CHECK INSPECTION, BRACKET CRACKED ON LEFT LOWER SIDE OF COCKPIT ENTRANCE. REPLACED BRACKET IAW CRJ SRM 51-40-11, PARA. 4, 51-42-16.

Part: ECU — MALFUNCTIONED (SPOILER) · airframe 2,806 hrs · 2,469 cycles

FLT SPLRS FAULT STATUS MESSAGE INTERMITTENT. REMOVED AND REPLACED SECU. OPS CHECK GOOD IAW CRJ MM 27-00-00. S/N OFF: 01548.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 2,566 hrs · 2,276 cycles

STAB TRIM CH 1 WILL NOT ENGAGE. INSTALLED SERVICEABLE STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW MM 27-40-00, 27-42-01 AND 27-42-05. MCU P/N OFF/ON 7062-3, S/N OFF 230, S/N ON 468. OPS CHECK GOOD.

Part: TRIM PANEL — MALFUNCTIONED · airframe 1,427 hrs · 1,195 cycles

RUDDER TRIM INOP, RUDDER TRIM STUCK IN THE FULL RIGHT POSITION. REMOVED AND REPLACED TRIM PANEL IAW CRJ MM 27-12-10. OPS CHECK GOOD.PN ON 601R51226-23/01.

Part: DAMPER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 404 hrs · 365 cycles

NR 2 STATUS MESSAGE DURING FLIGHT. WOULD NOT RESET. SWAPPED FCC CARDS FROM TOP TO BOTTOM. REPLACED NR 2 YAW DAMPER W/SERVICEABLE UNIT IAW MM 22-22-01. PERFORMED EXTENSIVE FUNCTIONAL CHECKS OF BOTH NR 1 & 2 YAW DAMPER SYSTEMS. OPS CHECK GOOD ON GROUND AT THIS TIME.