N908SW

Part: NONE — NONE · airframe 46,999 hrs · 40,232 cycles

NON CONFORMING REPAIR FOUND AT RBL 9.0 OUTBOARD INTERCOSTAL AT FS 280.0 (C-CHECK RO 9-30-21) REMOVED AND REPLACEDRBL9 INTERCOSTAL @ FS280.00. REF DWG 601R31113 REV AC, CRJ200 SRM 51-42-06, AND CRJ200 SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: RETAINER — CORRODED (BS 349 S18R) · airframe 46,999 hrs · 40,232 cycles

SERVICE DOOR SURROUND AREA, CORROSION ON CLIP AT AFT CORNER FS349 AND STGR 18R. (C-CHECK RO 9-30-21) REMOVED AND REPLACED CLIP AT FS349, STGR 18R. REF. CRJ200 SRM 51-42-21, SRM 51-41-02 AND DWG# 601R38303 REV. AR TOOL : TUC5659 CAL. DUE DATE 02/28/22 / COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIR (**RII**)

Part: NONE — CRACKED · airframe 46,999 hrs · 40,232 cycles

FRAME AT FS333.00 ABOVE PAX DOOR IS CRACKED AT A TOOLING HOLE. LOCATION MARKED WITH FLAG (C-CHECK RO 9-30-21) REMOVED AND INSTALLED NEW FS333.00 FRAME BETWEEN STGR 0 & STGR 3L. REF: CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21, CRJ200 SRM 51-21-16, AND DWG 601R31020 REV F. LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

R/H OTBD FLAP HAS APPROX. 16 SMOKING RIVETS ON THE UPPER SKIN (C-CHECK RO 9-30-21) REMOVED AND REPLACED 16 EA. FASTENERS ON R/H OTBD FLAP UPR SKIN. REF REO 601R-57-53-1227 REV -- DATED 2021-08-19. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: RIB — GOUGED · airframe 46,999 hrs · 40,232 cycles

GOUGE ON RH IB FLAP RIB AT IB END. (C-CHECK RO 9-30-21) REMOVED AND INSTALLED NEW R/H INBOARD RIB AT INBOARD END AND RESTORED FINISH. REF: CRJ200 SRM 51-42-06, CRJ200 SRM 51-45-00, CRJ200 SRM 51-42-15, CRJ200 SRM 51-21-16 AND DWG. # 601R14002 REV K FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 57-52-00. SEE CONTINUATION CARD FOR DETAILS. SKYCARD 51-900-1003-SKY COMPLIED WITH

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

CORROSION UNDER STOP FITTINGS ON ANGLE AT SERVICE DOOR SURROUND AREA BETWEEN FS319 AND FS349. (C-CHECK RO 9-30-21) REMOVED AND REPLACED WITH SERVICE DOOR LOWER ANGLE REF CRJ200 SRM 51-42-06 AND 51-42-21 AND DRAWING 601R38303, REV AR. COMPLIED WITH 51-900-1003-SKY

Part: NONE — NONE · airframe 46,999 hrs · 40,232 cycles

AFTER REMOVAL OF PAX DOOR FOUND FUSELAGE SIDE HINGE-PIN HOLES TO BE OVERSIZE USING GO-NO/GO GAUGE G670-521104-101 (C-CHECK RO 9-30-21) REMOVED AND REPLACED PAX DOOR HINGE HALF ON THE FUSELAGE SIDE. REF DWG 601R31527 REV AM AND CRJ200 SRM 53-21-23 REPAIR NO. -01. LEAK CHECK GOOD. COMPLIED WITH 51-900-1003-SKY

Part: NONE — GOUGED · airframe 46,999 hrs · 40,232 cycles

*R/H OTBD FLAP INBD HINGE FITTINGS ON THE WING LOCATED AT WS178 HAVE SMALL GOUGES ON THE CENTER LUGS. (C-CHECK RO 9-30-21) BLENDED OUT GOUGE DAMAGE ON R/H OTBD FLAP HINGE CENTER LUG @ WS178.00 TO A SMOOTH CONTOUR AND RESTORED FINISH. REMAINING MATERIAL IN REWORKED AREA IS WITHIN LIMITS. REF REO 601R-57-21-3510 REV-- DATED 2021-08-26 ALL STEPS

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

R/H FLOOR SUPPORT STRAP AT FS559, RBL27 TO RBL45 IS CORRODED (C-CHECK RO 9-30-21) REMOVED AND REPLACED R/H FLOOR SUPPORT STRAP @ FS559.00 BETWEEN RBL27 & RBL45. REF DWG 601R31145 REV M & CRJ-200 SRM 51-42-06. PRESSURE LEAK CHECK GOOD. COMPLIED WITH 51-900-1003-SKY

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

* R/H PRESSURE FLOOR SILL PANEL HAS MULTIPLE SPOTS OF CORROSION, MARKED (C-CHECK RO 9-30-21) REMOVED CORROSION ON R/H PRESSURE FLOOR SILL PANEL REF REO 601R-53-41-666 REV -C DATED 2012-11-06 AND REO 601R-53-41-2955 REV -- DATED 2021-08-30. FOUND TO BE IN LIMITS . COMPLIED WITH ALL STEPS OF REO 601R-53-41-666 REV -C DATED 2012-11-06 AND REO 601R-53-41-2955 REV -- DATED 2021-08-30. COMPLIED WITH TASK CARD 51-900-1003-SKY. NO WEIGHT LOSE OR GAINS BLENDS ONLY.SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

* L/H PRESSURE FLOOR SILL PANEL HAS MULTIPLE SPOTS OF CORROSION, MARKED (C-CHECK RO 9-30-21) BLENDED CORROSION DAMAGE FROM L/H PRESSURE FLOOR SILL TO A SMOOTH CONTOUR AND RESTORED FINISH. REMAINING MATERIAL IN REWORKED AREAS IS WITHIN LIMITS. REF REO 601R-53-41-666 REV -C DATED 2012-11-06. COMPLIED WITH REO 601R-53-41-2955 REV -- DATED 2021-08-30. COMPLIED WITH TASK CARD 51-900-1003-SKY. PRESSURE CHECK GOOD.

Part: SKIN — CHAFED (RT WING) · airframe 46,999 hrs · 40,232 cycles

* BOTTOM WING PLANK IS CHAFED AT WS45.00R AND REAR SPAR DATUM, MARKED. (C-CHECK RO 9-30-21) BLENDED OUT CHAFE DAMAGE R/H BOTTOM WING PLANK AT WS45.00R TO A SMOOTH CONTOUR AND RESTORED FINISH. REMAINING MATERIAL IN REWORKED AREAS IS WITHIN LIMITS. REF REO 601R-57-21-880 REV -D DATED 2017/03/06 AND CRJ200 SRM 51-12-00. COMPLIED WITH TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD.

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

FAB TRACK SEAT 601R31032-21 FOR CAMP 23220100 JOB 27540101 OP 210 (C-CHECK RO 9-30-21) FABRICATED AND INSTALLED NEW SEAT TRACK 601R31032-21, USING EXTRUSION 20276-288-0-0A, PO# T55899, REF. BOMBARDIER REO 601R-53-00-485, REV. D, DATED 2018-01-29 A

Part: SKIN — CHAFED (LT WING) · airframe 46,999 hrs · 40,232 cycles

* BOTTOM WING PLANK IS CHAFED AT WS45.00L AND REAR SPAR DATUM, MARKED. (C-CHECK RO 9-30-21) BLENDED OUT CHAFE DAMAGE L/H BOTTOM WING PLANK AT WS45.00L TO A SMOOTH CONTOUR AND RESTORED FINISH. REMAINING MATERIAL IN REWORKED AREAS IS WITHIN LIMITS. REF REO 601R-57-21-880 REV -D DATED 2017/03/06 AND CRJ200 SRM 51-12-00. COMPLIED WITH TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD.

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

* SEAT RAIL FROM FS559+112 TO FS621 RBL9 IS CORRODED. (C-CHECK RO 9-30-21) REMOVED AND INSTALLED RBL9 SEAT TRACK FROM FS559+112 TO FS621 IAW CRJ200 AMM 53-01-11-000-802 AND CRJ200 AMM 53-01-11-400-802

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

* SEAT RAIL FROM FS559+80 TO FS621 LBL27 IS CORRODED. (C-CHECK RO 9-30-21) REMOVED AND INSTALLED NEW LBL27 SEAT TRACK FROM FS567.00 TO FS621 IAW CRJ200 AMM 53-01-11-000-802 AND CRJ200 AMM 53-01-11-400-802. NO CORROSION PRESENT ON LBL27 SEAT TRACK FROM FS559.00+80 TO FS567.00.

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

* SEAT RAIL FROM FS559+112 TO FS621 RBL27 IS CORRODED. (C-CHECK RO 9-30-21) REMOVED AND INSTALLED NEW RBL27 SEAT TRACK FROM FS559.00+112 TO FS621.00 IAW CRJ200 AMM 53-01-11-000-802 AND CRJ200 AMM 53-01-11-400-802

Part: FRAME — CORRODED (BS 589 S22L-26R) · airframe 46,999 hrs · 40,232 cycles

* FRAME AT FS589 IS CORRODED FROM STR22L TO STR26R (C-CHECK RO 9-30-21) REMOVED/REPLACED FS589.00 LOWER FRAME BETWEEN STGR 20L AND 20R. REF CRJ-200 SRM 51-42-06 AND DWG 601R36025 REV -P. COMPLIED WITH TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD.

Part: FLOORBEAM — CRACKED (BS 280 LBL9) · airframe 46,999 hrs · 40,232 cycles

SUSPECTED CRACK ON FWD SIDE OF FS280 BEAM AT LBL9 (C-CHECK RO 9-30-21) CRACK ON FWD SIDE OF FS 280.0 BEAM AT LBL 9.0 REPAIRED REF BOMBARDIER REO 601R-53-11-926 REV B DATED 2006/05/10 / COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: FLOORBEAM — CORRODED (BS 597 RBL 27) · airframe 46,999 hrs · 40,232 cycles

* FLOOR BEAM AT RBL27 HAS CORROSIONON OUTBOARD FLANGE AT APPROX FS597. (C-CHECK RO 9-30-21) REPAIRED RBL27 FLOOR BEAM OTBD FLANGE AT APPROX FS597.00 REF CRJ200 SRM 53-00-43 REPAIR NO.1. COMPLIED WITH 51-900-1003-SKY

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

* AFT OUTBOARD WARDROBE MOUNT PLATE IS CORRODED (C-CHECK RO 9-30-21) REMOVED AND REPLACED WITH NE W AFT OTBD WARDROBE MOUNTING PLATE REF CRJ200 SRM 51-42-06, 51-42-13 AND DWG:601R38670, REV -T. COMPIED WITH 51-900-1003-SKY

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

* FLOOR BEAM ATTACH "T" BRACKET AT THE FORWARD CORNER OF THE SERVICE DOOR CUTOUT IS CORRODED. (C-CHECK RO 9-30-21) FOUND T BRACKET AT FWD CORNER OF SERVICE DOOR CUTOUT OUT OF LIMITS REF CRJ 200 SRM 53-00-00 AND REPLACED WITH A NEW T BRACKET REF CRJ 200 SRM 51-42-21 AND DRAWING 601R38303 REV AR.COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

* INBOARD FORWARD GALLEY MOUNT PLATE IS CORRODED (C-CHECK RO 9-30-21) REMOVED AND REPLACED WITH NEW INBD FWD GALLEY MOUNT PLATE REF CRJ200 SRM 51-42-06 AND DWG: 601R38669, REV N. COMPLIED WITH 51-900-1003-SKY

Part: CUP — CORRODED (HAND RAIL) · airframe 46,999 hrs · 40,232 cycles

* AFT PAX DOOR HANDRAIL CUP IS CORRODED (C-CHECK RO 9-30-21) / REMOVED AND REPLACED AFT PAX DOOR HANDRAIL CUP. REF DWG 601R31527 REV AM & CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

* FLOOR BEAM ATTACH "T" BRACKET AT FORWARD CORNER OF PAX DOOR CUTOUT IS CORRODED. (C-CHECK RO 9-30-21) REMOVED AND REPLACED WITH NEW "T" BRACKET, LOCATED AND DRILLED NEW BRACKET REF CRJ200 SRM 51-42-21,51-42-06, DWG 601R32002 REV Y COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

* INBOARD AFT GALLEY MOUNT PLATE IS CORRODED (C-CHECK RO 9-30-21) REMOVED AND REPLACED INBD AFT GALLEY MOUNT PLATE. REF DWG 601R38669 REV -N & CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: NONE — CRACKED · airframe 46,999 hrs · 40,232 cycles

* OUTBOARD CLIP RBL9 FLOORBEAM TO FS280 BEAM IS CRACKED. (C-CHECK RO 9-30-21) REMOVED AND INSTALLED NEW RBL9 OTBD CLIP @ FS280.00. REF CRJ200 SRM 51-42-21 & DWG 601R31113 REV AD. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

* RBL 9 SEAT RAIL IS CORRODED FROM FS364 TO FS409 (C-CHECK RO 9-30-21) REMOVED SEAT RAIL FS364.00-FS409.00 REF. CRJ200 AMM 53-01-11-000-802. AND INSTALLED SEAT RAIL FS364.00-FS409.00 REF. CRJ200 AMM 53-01-11-400-802, FOUND TO BE BE OUT OF LIMITS PER CRJ 200 SRM 53-21-49 TUC8607 DUE DATE: 28-FEB-22.

Part: BRACKET — CRACKED (BS 193) · airframe 46,999 hrs · 40,232 cycles

BRACKET CRACKED AT LH FS193.0 AT APPROXIMATELY WL 79.50. (MARKED). (C-CHECK RO 9-30-21) REMOVED AND REPLACED LH FS193.0 BRACKET AT APPROXIMATELY WL 79.50. REF DWG 600-33101 REV -R & CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

* FORWARD PAX DOOR HANDRAIL CUP IS CORRODED (C-CHECK RO 9-30-21) REMOVED AND REPLACED FWD PAX DOOR HANDRAIL CUP. REF DWG 601R31527 REV AM & CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: NONE — NONE · airframe 46,999 hrs · 40,232 cycles

* FLIGHT DECK FLOOR SUPPORT ANGLE AT FS280 IS CORRODED (C-CHECK RO 9-30-21) REMOVED/INSTALLED NEW FLIGHT DECK FLOOR SUPPORT ANGLE AT FS280.00 BEAM. REF DWG 600-33100 REV -Y, CRJ200 SRM 51-42-06, & CRJ200 SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: FLOOR SUPPORT — CORRODED (BS 349-394) · airframe 46,999 hrs · 40,232 cycles

* L/H FLOOR SILL IS CORRODED FROM FS349 TO FS394 (C-CHECK RO 9-30-21) CUT AWAY DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS FOR LH FS349.00 - FS360.00. CORROSION DAMAGE BETWEEN FS360.00 AND FS394.00 TO A SMOOTH CONTOUR AND RESTORED FINISH. REMAINING MATERIAL IN REWORKED AREAS ARE WITHIN LIMITS. REF REO 601R-53-21-3482 REV -- DATED 2021-08-25. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: FLOORBEAM — CORRODED (BS 409) · airframe 46,999 hrs · 40,232 cycles

*FS409.00+64 €“ FS409+80 FLOOR BEAM LBL9 OUTBOARD FLANGE HAS CORROSION. (MARKED) (C-CHECK RO 9-30-21) REPAIRED FS409.00+64 €“ FS409+80 LBL9 FLOOR BEAM OTBD FLANGE REF CRJ-200 SRM 53-00-43 REPAIR NO.- 1. COMPLIED WITH TASK CARD 51-900-1003

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

* LBL 9 SEAT RAIL IS CORRODED FROM FS364 TO FS409 (C-CHECK RO 9-30-21) REMOVED AND REPLACED LBL9 SEAT RAIL FROM FS364.00 TO FS409.00 REF CRJ200 AMM 53-01-11-000-802 & 53-01-11-400-802

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

*LH WING FLIGHT SPOILER OTBD ACTUATOR HAS CORRODED ATTACHING HARDWARE (C-CHECK RO 9-30-21) REPLACED ONE NUT AND COTTER KEY ON THE LH WING FLIGHT SPOILER OTBD ACTUATOR PER THE CRJ 200 AMM 27-64-05-400-801 STEP 1 THRU 3.8(C). / OPERATIONAL TEST GOOD. NO DEFECTS NOTED.

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

*LH WING SPOILERON INBD AND OTBD ACTUATORS HAVE CORRODED ATTACHING HARDWARE (C-CHECK RO 9-30-21) REMOVED AND INSTALLED NEW SERVICEABLE HARDWARE ON THE LH WING SPOILERON INBOARD AND OUTBOARD ACTUATORS. REF - CRJ 200 AMM 27-64-01-400-801 STEP 1 THRU STEP 2B (4) (A-H). / OPERATIONAL TEST GOOD. NO DEFECTS NOTED.

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

*LH HORIZONTAL STAB INBD HINGE ASSY HAS CORRODED ATTACHING HARDWARE (C-CHECK RO 9-30-21) REPLACED CORRODED HARDWARE WITH NEW HARDWARE ON LEFT HORIZONTAL STABILIZER TO ELEVATOR CENTER HINGE REF CRJ 200 AMM 27-34-01-400-801 STEP 3. C. TUC8619 CAL DUE 31 OCT 2021.

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

*RH HORIZONTAL STAB INBD HINGE ASSY HAS CORRODED ATTACHING HARDWARE (C-CHECK RO 9-30-21) REMOVED AND INSTALLED NEW SERVICEABLE HARDWARE ON THE RH HORIZONTAL STAB INBOARD HINGE ASSEMBLY. REF - CRJ 200 AMM 27-34-01-400-801 STEP 1 THRU STEP 3C (1-13). / OPERATIONAL TEST GOOD. NO DEFECTS NOTED.

Part: NONE — CORRODED · airframe 46,999 hrs · 40,232 cycles

*RH HORIZONTAL STAB CENTER HINGE ASSY HAS CORRODED HARDWARE (C-CHECK RO 9-30-21) REPLACED CORRODED HARDWARE WITH NEW HARDWARE ON RIGHT HORIZONTAL STABILIZER TO ELEVATOR CENTER HINGE REF CRJ 200 AMM 27-34-01-400-801 STEP 3. C. TORQUE WRENCH TUC8619 CAL DUE 31 OCT 2021.

Part: NONE — GOUGED · airframe 46,999 hrs · 40,232 cycles

A BAY DOOR FUSELAGE SIDE RH FWD FITTING GOUGED (C-CHECK RO 9-30-21) BLENDED GOUGE DAMAGE ON R/H FWD A-BAY DOOR FITTING TO A SMOOTH CONTOUR AND RESTORED FINISH, REF REO 601R-53-21-3474 REV -- DATED 2021-08-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: NONE — CHAFED · airframe 46,999 hrs · 40,232 cycles

RH FLAP VANE INBD CHAFFED (C-CHECK RO 9-30-21) BLENDED OUT CHAFFING ON RH IB FLAP VANE IB END , FOUND OUT OF LIMITS REF REO 601R-57-52-004 REV D 2012-12-19, AND REPLACED VANE CAP IB END REF CRJ 200 SRM 51-42-13 AND DRAWING 601R14302 REV E. / COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: NONE — CHAFED · airframe 46,999 hrs · 40,232 cycles

LH INBD FLAP VANE OUTBD END CHAFFED (C-CHECK RO 9-30-21) BLENDED OUT CHAFFING ON LH IB FLAP VANE OB END REF CRJ 200 SRM 51-12-00.FOUND TO BE OUT OF LIMITS REF SRM57-00-31. REMOVED AND INSTALLED NEW LH INBOARD FLAP VANE OUTBOARD CAP P/N 601R14303-43. REF. CRJ200 SRM 51-42-13 AND DWG # 601R14302 REV. E. COMPLIED WITH 51-900-1003-SKY

Part: NONE — DAMAGED · airframe 46,999 hrs · 40,232 cycles

REMOVE AND INSTALL RIGHT WING OUTBOARD FLAP HINGE BOX ASSEMBLY WS178.00, WS220.00 AND WS264.00 TO FOM PER AMM (C-CHECK RO 9-30-21) REMOVED RH OUTBOARD FLAP HINGE BOX AT WS 264.00 REF. CRJ 200 AMM 57-21-35-000-803.AND INSTALLED RH OUTBOARD FLAP HINGE BOX AT WS 264.00 REF CRJ 200 AMM 57-21-35-400-803 REMOVED RH OUTBOARD FLAP HINGE BOX AT WS 220.00 REF. CRJ 200 AMM 57-21-35-000-802.AND REINSTALLED RIGHT OUTBOARD FLAP HINGE BOX WS 220.00 REF CRJ 200 AMM 57-21-35-400-802. REMOVED RH OUTBOARD FLAP HINGE BOX AT WS 178.00 REF. CRJ 200 AMM 57-21-35-000-801.AND INSTALLED RH OUTBOARD FLAP HINGE BOX AT WS 178.00 REF CRJ 200 AMM 57-21-35-400-801. BOND CHECKS GOOD

Part: NONE — CRACKED · airframe 46,999 hrs · 40,232 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: 7540, POSITION: (C-CHECK RO 9-30-21) COMPLIED 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. COMPLIED WITH SERIAL NUMBER 7540. REF REO 601R-53-61-1240 REV -D DATED 2016-10-31 & REO 601R-53-61-7698 REV -- DATED 2021-08-17. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: NONE — BLOCKED · airframe 46,999 hrs · 40,232 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA44565-601R-52-41-295 N908SW CP17142390-PR - BLENDED AFT LWR PAN OF THE SERVICE DR REF REO 601R-52-41-295. PERM REPAIR REQUIRED WITHIN 6000 FH OF INCORPORATION OF THIS REO., PART NUMBER: 601R38302-91 - DOOR ASSY, SRVC/EMER EXIT, SERIAL NUMBER: 7540, POSITION: ONLY (C-CHECK RO 9-30-21) REMOVED/INSTALLED NEW SERVICE DOOR AFT LWR PAN. REF CRJ200 SRM 51-42-06, SRM 51-42-21, AND DWG# 601R38304 REV BN. LEAK AND OPERATIONAL CHECKS ARE SATISFACTORY, COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 45,830 hrs · 39,160 cycles

FLAPS FAIL CAUTION MESSAGE CLIMBING THROUGH 13000. FLIGHT # 5422 CLOSEDPERFORMED RESET OF FLAP FAIL MESSAGE IAW FIM, MESSAGE CLEARED. CYCLED FLAPS 5 FULL CYCLES NO DEFECTS NOTED. MCI CREATED FOR 10 FC FLY ON.

Part: SWITCH — FAILED (RT ENGINE) · airframe 44,569 hrs · 38,009 cycles

R/H ENG T/R UNLOCK IN FLIGHT PERFORMED QRH DID NOT CLEAR. (FLT#5228) RE-RIGGED THROTTLE LOCKOUT SWITCH IAW AMM. OPS CHECK GOOD, NO DEFECTS NOTED.

Part: WEB — CORRODED (PAX DOOR) · airframe 43,133 hrs · 36,736 cycles

PAX DOOR FWD WEB CORRODED AT UPPER END. (C-CHECK) RO: 09/11/2018. REMOVED AND REPLACED PAX DOOR FWD WEB IAW SRM.

Part: WEB — CORRODED (PAX DOOR) · airframe 43,133 hrs · 36,736 cycles

PAX DOOR AFT WEB CORRODED. (C-CHECK) RO: 09/11/2018. REMOVED AND REPLACED PAX DOOR AFT WEB IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 43,133 hrs · 36,736 cycles

CORROSION AROUND FLOORBOARD FASTENER HOLE LOCATED ON RT PRESSURE FLOOR SKIN (SILL) AT APPROXIMATE FS409+128 & APPROXIMATE RBL43. (C-CHECK) RO: 09/11/2018. REMOVED CORROSION FROM RT PRESSURE FLOOR SKIN (SILL) AT APPROXIMATE FS409+128 & APPROXIMATE RBL43 IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,133 hrs · 36,736 cycles

AT LBL 27 AFT CARGO FLOOR SUPPORT STRUCTURE HAS CORROSION (EXFOLIATION) AT NUT PLATE HOLE LOCATION BETWEEN FS621 TO FS 605.00. (C-CHECK) RO: 09/11/2018. LOCATED, DRILLED AND INSTALLED NEW CARGO FLOOR SUPPORT BETWEEN FS605-FS621 AT LBL 27 IAW REO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,133 hrs · 36,736 cycles

CORROSION ON FRAME AROUND FS 333 AND STR 27. (C-CHECK) RO: 09/11/2018. REMOVED AND REPLACED FRAME FS333 BETWEEN STR 23L AND 23R IAW SRM. LEAK CHECK GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 43,133 hrs · 36,736 cycles

MULTIPLE DENTS ON RIGHT SIDE OF FUSELAGE BETWEEN FS 640 - 718, STR 20 - 27. (C-CHECK) RO: 09/11/2018. REPAIRED MULTIPLE DENTS ON THE RIGHT SIDE OF THE FUSELAGE FS 640-FS 718 AND STR 20-27 IAW SRM AND REO.

Part: SKIN — DENTED (FUSELAGE) · airframe 43,133 hrs · 36,736 cycles

DENTS ON LEFT SIDE OF FUSELAGE BETWEEN FS 672 - 682, STR 18 - 19. (C-CHECK) RO: 09/11/2018. REPAIRED DENTS ON LEFT SIDE OF FUSELAGE BETWEEN FS 672 - 682, STR 18 - 19 IAW REO.

Part: ATTACH FITTING — GOUGED (FUSELAGE) · airframe 43,133 hrs · 36,736 cycles

AFT BAGGAGE BAY LT OUTBD FLOORBEAM ATTACHMENT TO PRESSURE BULKHEAD BL27.00 GOUGED. (C-CHECK) RO: 09/11/2018 BLENDED OUT GOUGE ON THE LT BL 27.00 FLOORBEAM FITTING AT THE PRESSURE BULKHEAD IN THE AFT CARGO IAW REO.

Part: SKIN — DENTED (FUSELAGE) · airframe 43,133 hrs · 36,736 cycles

MULTIPLE DENTS ON RIGHT SIDE OF FUSELAGE BETWEEN FS 589 - 640 , STR 20 - 27. (C-CHECK) RO: 09/11/2018. BLENDED DAMAGE ON RT FUSELAGE SKIN BETWEEN FS 589.00 & FS 605.00 AND STR 22R AND STR 26 IAW REO.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 43,133 hrs · 36,736 cycles

AFT PRESSURE SUPPORT ANGLE FS621, BETWEEN BL9-BL27.00 TO LT SCREW HOLES ARE CORRODED. (C-CHECK) RO: 09/11/2018. PERFORMED BLEND OUT REPAIRS TO THE AFT PRESSURE SUPPORT ANGLE FS621, BETWEEN BL9-BL27.00 TO LT SCREW HOLES IAW REO.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 38,884 hrs · 32,791 cycles

PAX DOOR BRACKET HAS CORROSION OUT OF LIMITS. REMOVED AND REPLACED THE BRACKET IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,884 hrs · 32,791 cycles

PAX DOOR INTERCOSTAL HAS OUT OF LIMITS CORROSION. REMOVED THE INTERCOSTAL AND INSTALLED A NEW INTERCOSTAL IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 38,884 hrs · 32,791 cycles

LEFT, INBD FLAP OTBD CENTER VANE CAP CHAFED. REPLACED THE VANE CAP IAW SRM AND EA.

Part: ACCESS PANEL — GOUGED (RT WING TE FLAP) · airframe 38,884 hrs · 32,791 cycles

RIGHT INBD FLAP ACCESS PANEL 684AB HAS A GOUGE NEAR THE FLAP VANE ACTUATOR ROD PASS THRU SLOT. REPAIRED THE ACCESS PANEL IAW EA.

Part: GEARBOX — FAILED (THROTTLE CONTROL) · airframe 35,320 hrs · 29,625 cycles

CREW WAS UNABLE TO BRING RT ENGINE BACK TO IDLE, FOLLOWED QRH AND SHUTDOWN THE RT ENGINE. EMERGENCY WAS DECLARED AND FLIGHT LANDED WITHOUT INCIDENT. R & R RT THROTTLED CONTROL GEAR BOX IAW AMM.

Part: CONTROL UNIT — OUT OF ADJUST (SPOILERS) · airframe 34,854 hrs · 29,241 cycles

SPOILER TAKEOFF CONFIGURATION ILLUMINATED. RIGGED LT SPOILER PCUS IAW AMM. OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,939 hrs · 28,502 cycles

CABIN CENTER FORWARD CEILING EMERGENCY LIGHT INOPERATIVE. R & R NR 1 CHARGER ASSY AND BATTERY, IAW AMM.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 33,939 hrs · 28,502 cycles

FLOOR EMERGENCY LIGHT ON THE WARDROBE INOPERATIVE. R & R CONNECTOR AND PIN IAW ESPM.

Part: PRESSURE DECK — CRACKED (BS 460) · airframe 33,939 hrs · 28,502 cycles

FS 460 BETWEEN LBL 9 & RBL 9 PRESSURE FLOOR HAS A CRACK. C-CHECK, REPAIRED CRACK AT FS 460 IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,939 hrs · 28,502 cycles

RIGHT INBD FLAP VANE L/E CAP CHAFED. C-CHECK, R & R FLAP VANE L/E IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,939 hrs · 28,502 cycles

LEFT INBD FLAP VANE CHAFED AT OTBD VANE ACTUATOR. C-CHECK, REPAIRED IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,939 hrs · 28,502 cycles

LEFT INBD FLAP VANE CHAFED AT CENTER VANE ACTUATOR. C-CHECK, REPAIRED LT INBD FLAP VANE CAP AT CENTER ACTUATOR, IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,939 hrs · 28,502 cycles

LEFT INBD FLAP VANE HAS CHAFING AT INBD VANE ACTUATOR. C-CHECK, REPAIRED LT INBD FLAP VANE AT INBD ACTUATOR, IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,939 hrs · 28,502 cycles

RIGHT INBD FLAP VANE CHAFED ON OTBD SIDE OF L/E. BLENDED RT INBD FLAP VANE IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,939 hrs · 28,502 cycles

RT INBD FLAP VANE CHAFED ON INBD SIDE OF L/E. REPLACED RT INBD FLAP VANE IAW SRM AND REO.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 33,939 hrs · 28,502 cycles

PAX DOOR AFT DRAG ANGLE REPAIR SPLICE HAS CRACK AT RADIUS. C-CHECK, REPLACED PAX DOOR AFT DRAG ANGLE SECTION WITH NEW, PN 601R 52-11-513-1 IAW SRM AND REO.

Part: WEB — CRACKED (ZONE 200) · airframe 33,939 hrs · 28,502 cycles

LT TRU FLOOR WEB CRACKED AT AFT OUTBD CORNER. C-CHECK, REMOVED DAMAGED ON LT TRU FLOOR WEB PERFORMED NDT, NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER, FILLER, AND FABRICATED REPAIR ANGLE, INSTALLED REPAIR IAW REO.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 33,511 hrs · 28,172 cycles

RT EXTERIOR MIDDLE OVERWING EMERGENCY LIGHT IS BURNED OUT. R & R RT EXTERIOR MIDDLE OVERWING EMERGENCY LIGHT BULB IAW AMM.

Part: INVERTER — FAILED (CABIN) · airframe 32,735 hrs · 27,613 cycles

EMERGENCY LIGHT ROW 2BC TO ROW 6BC FLOOR DOES NOT ILLUMINATE. REPLACED NR 2 INVERTOR ASSEMBLY IAW AMM.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 32,224 hrs · 27,246 cycles

2 CD TO 6 CD CABIN FLOOR EMERGENCY LIGHTS DO NOT ILLUMINATE. FLT 5425 RECONNECTED FLOOR TRACK EMERGENCY LIGHTS AT ROW 2 CD TO 6 CD IAW AMM.

Part: SKIN — OUT OF ALIGNMENT (RT WING) · airframe 32,174 hrs · 27,213 cycles

RT OTBD LE HOLES WILL NOT ALIGN. C-CHECK REPLACED RT OTBD LE SKIN PN 601R12062-2 IAW SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,564 hrs · 26,756 cycles

EXTERNAL EMERGENCY LIGHTS BURNED OUT. FLT#5485 RELAMPED.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 31,325 hrs · 26,570 cycles

RT CENTER OVERWING EMERGENCY EXIT LIGHT IS BURNED OUT. FLT#6205 RELAMPED.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 30,840 hrs · 26,212 cycles

DURING CLIMBOUT SMOKE STARTED FILLING COCKPIT. RAN QRH DETERMINED SMOKE WAS ASSOCIATED WITH THE PACKS. PERFORMED GROUND RUN AND OPS CHECK OF LT PACK. NO DEFECTS NOTED IAW AMM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 30,123 hrs · 25,652 cycles

F/O WINDOW SHATTERED INFLIGHT. (FLT 5582) REPLACED F/O'S SIDE WINDOW IAW AMM. P/N: NP-139322-12 S/N ON: 11292H4796 S/N OFF: 08337H2385

Part: SILL — CRACKED (FUSELAGE) · airframe 29,593 hrs · 25,249 cycles

CRACK FOUND IN RADIUS OF CARGO FLOOR SILL PLATE AT FS 589.00. (C-CHECK) CARGO FLOOR SILL PLATE REPLACED.

Part: SKIN — CRACKED (RT WING) · airframe 29,593 hrs · 25,249 cycles

FOUND CRACK ON RIGHT LOWER WING PLANK IN THE AREA OF THE REAR SPAR AND WING STATION 148.019. (C-CHECK) REPAIRED CRACK ON RIGHT LOWER WING PLANK IN THE AREA OF THE REAR SPAR AND WING STATION 148.019 IAW REO.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 29,593 hrs · 25,249 cycles

PILOT WINDSHIELD IS CRACKED IN TWO PLACES. (C-CHECK) INSTALLED NEW PILOT WINDSHIELD IAW AMM.

Part: POST — CRACKED (FUSELAGE) · airframe 29,593 hrs · 25,249 cycles

FS 409.0+128 BL 0.00 LT AND RT VERTICAL POSTS CRACK INDICATIONS NOTED AT AFT RADIUS. (C-CHECK) REPLACED FS 409.0 + 128 BL 0.00 LT AND RT VERTICAL POSTS IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,459 hrs · 25,137 cycles

EMERGENCY EXIT LIGHT ON LEFT SIDE IS OUT. (FLT 6245) RELAMPED EMERGENCY LIGHT.

Part: SKIN — DENTED (RT WING) · airframe 29,291 hrs · 25,013 cycles

DURING BIRD STRIKE INSPECTION FOUND DENT ON RIGHT WING LEADING EDGE BETWEEN WS 96-13 AND 106.40. (BIRD STRIKE INSPECTION) INSTALLED NEW RIGHT WING LEADING EDGE SKIN AND AFFECTED RIBS (3) BETWEEN WS 93.13 AND WS 106.40 IN REFERENCE TO SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,259 hrs · 24,986 cycles

RIGHT WING CAUTION EMERGENCY EXIT LIGHT IS OUT. (FLT 5638) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,892 hrs · 24,705 cycles

GALLEY SERVICE DOOR EMERGENCY LIGHT IS INOPERATIVE. (FLT 6192) REPLACED GALLEY EMERGENCY EXIT FORWARD FLOOR LIGHT ASSEMBLY IN REFERENCE TO AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,875 hrs · 24,691 cycles

MAIN CABIN DOOR FLOOR LEVEL EMERGENCY LIGHT IS OUT. (FLT 6345) RELAMPED IN REFERENCE AMM.

Part: SIGN — UNSECURE (CABIN) · airframe 28,632 hrs · 24,485 cycles

EMERGENCY EXIT ROW OVERHEAD EXIT SIGN FELL DOWN. (FLT 5422) REINSTALLED OVERWING EMERGENCY OVERHEAD LIGHT COVER.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,992 hrs · 23,980 cycles

FORWARD FUSELAGE EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 5240) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,903 hrs · 23,916 cycles

FORWARD EXTERIOR EMERGENCY LIGHT ON LEFT SIDE IS OUT. (FLT 5319) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,283 hrs · 23,403 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5443) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,722 hrs · 22,957 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6215) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,682 hrs · 22,910 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6255) RELAMPED EMERGENCY LIGHT.

Part: SEAT BELT — DEFECTIVE (COCKPIT) · airframe 26,692 hrs · 22,919 cycles

FIRST OFFICERS QUICK RELEASE SEAT BELT DIFFICULT TO UNLOCK. (FLT 5243) REPLACED CO-PILOTS QUICK RELEASE SEAT BELT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,566 hrs · 22,817 cycles

LEFT SIDE AFT EMERGENCY EXTERIOR LIGHT IS OUT. (FLT 5434) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,387 hrs · 22,665 cycles

NR 8 EXTERIOR AND NR 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 6328) RELAMPED EMERGENCY LIGHTS.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 26,292 hrs · 22,587 cycles

EMERGENCY FLOOR LEVEL LIGHTING OUT FROM ROW 9 BACK. (FLT 5358) REPLACED NR 4 EMERGENCY LIGHT CHARGER ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,292 hrs · 22,587 cycles

NR 4 CEILING LEVEL EMERGENCY LIGHT IS OUT. (FLT 6216) REPLACED NR 4 OVERHEAD EMERGENCY LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,240 hrs · 22,541 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5420) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,179 hrs · 22,493 cycles

RIGHT AFT EXTERNAL EMERGENCY LIGHT IS OUT. (FLT 5824) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,037 hrs · 22,369 cycles

FOUR EXTERIOR EMERGENCY LIGHTS BURNT OUT, 2 OVER RIGHT WING, 1 OVER LEFT WING, 1 AT PAX DOOR. (FLT 6241) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,972 hrs · 22,297 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5619) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,739 hrs · 22,108 cycles

NR 2 AND 3 OVERHEAD EMERGENCY LIGHT ARE OUT. (FLT 5489) RELAMPED EMERGENCY LIGHTS.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,776 hrs · 22,997 cycles

FS 559.0 PRESSURE BULKHEAD IS CRACKED AT RBL 9.0 WL 54.18 AND LBL 18.0 LOWER CAP ANGLE RADIUS. (C-CHECK) REPAIRED PER REO.

Part: POST — CRACKED (FUSELAGE) · airframe 26,776 hrs · 22,997 cycles

FS 409.0+128 VERTICAL POST AT LBL 18.00 OUTBOARD AFT RADIUS CRACKED. (C-CHECK) REPLACED FS 409.0 + 128 LBL 18 OUTBOARD POST SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 26,776 hrs · 22,997 cycles

INTERCOSTAL AT FS 461,0, RBL 9, W/L 97.0 IS CRACKED. (C-CHECK) REPLACED CRACKED INTERCOSTAL FITTING PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,323 hrs · 21,786 cycles

FLOOR MOUNTED EMERGENCY LIGHT STRIP AT ROW IS OUT. (FLT 6684) REPLACED THE CABIN ESCAPE PATH FLOOR EMERGENCY LIGHTS AT ROW 10.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,075 hrs · 21,600 cycles

LEFT AFT EXTERIOR EMERGENCY LIGHT BURNED OUT. (FLT 6403) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,075 hrs · 21,600 cycles

RIGHT SIDE MIDDLE OVERWING EMERGENCY LIGHT IS BURNED OUT. (FLT 6958) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,900 hrs · 21,460 cycles

EXTERIOR LEFT REAR EMERGENCY LIGHT IS OUT. (FLT 6496) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,391 hrs · 21,047 cycles

NR 1 EMERGENCY OVERWING LIGHT OUT. (FLT 6576) RELAMPED EMERGENCY LIGHT.

Part: CONTROLLER — FAULTY (WINDOW HEAT) · airframe 21,760 hrs · 18,848 cycles

LEFT WINDSHIELD HEAT CAUTION FOLLOWED BY SMOKE IN THE COCKPIT. (FLT 6072) REPLACED LEFT SIDE WINDSHIELD HEAT CONTROLLER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,696 hrs · 18,791 cycles

SECOND EMERGENCY CEILING LIGHT FROM FRONT OF AIRCRAFT INOP. (FLT 5800) RELAMPED EMERGENCY CEILING LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,586 hrs · 18,705 cycles

NR 1 EXTERIOR EMERGENCY LIGHT INOP. (FLT 6370)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,427 hrs · 18,565 cycles

NR 3 OVERHEAD EMERGENCY FLOOD LIGHT INOP. (FLT 6231) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,267 hrs · 18,425 cycles

SECOND EMERGENCY FLOOD LIGHT INOP. (FLT 5806) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,130 hrs · 18,310 cycles

NR 2 EMERGENCY CEILING FLOODLIGHT INOP. (FLT 6650) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,812 hrs · 18,057 cycles

RIGHT AFT OVERWING EMERGENCY LIGHT INOP. (SVC CHECK) RELAMPED EMERGENCY LIGHT.

Part: FITTING — CRACKED (CARGO BAY) · airframe 20,763 hrs · 18,017 cycles

UPPER CARGO DOOR TRACK FITTING INTERFACE AT FS 621 CRACKED. (C CHECK) REPAIRED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 21,130 hrs · 18,310 cycles

FS 621 LINTEL FITTING CRACKED. (C CHECK) REPAIRED PER REO.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 21,130 hrs · 18,310 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 21,130 hrs · 18,310 cycles

FS 202 BULKHEAD CLIP CRACKED. (C CHECK) REPLACED PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 21,130 hrs · 18,310 cycles

FS 625 CLIPS CRACKED. (C CHECK) REPLACED PER SRM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,705 hrs · 17,228 cycles

FLT 5882 - SECOND AFT EMERGENCY CEILING LIGHT INOP. RELAMPED.

Part: WINDOW — CRACKED (COCKPIT) · airframe 19,452 hrs · 17,027 cycles

FLT 6718 - FIRST OFFICERS SIDE WINDOW CRACKED AT CRUISE. REPLACED SIDE WINDOW, PN OFF NP-139322-6 SN OFF 03161H6060.

Part: LINKAGE — BROKEN (LT THROTTLE) · airframe 17,706 hrs · 15,560 cycles

FLT 6736 - LEFT ENGINE WENT TO IDLE CUTOFF WHILE REDUCING POWER. REPLACED THROTTLE QUADRANT ASSEMBLY AS REQUIRED PER AMM 76-11-01, P/N: FE210-008, S/N OFF: FR-787.

Part: FLANGE — CRACKED (FUSELAGE) · airframe 16,901 hrs · 14,859 cycles

CRACK FOUND ON LOWER FLANGE OF RBL9 AT STA 280. COMPLIED WITH REPAIRS IAW CRJ200 REO 601R-53-11-171 REV D REPAIR A.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 16,901 hrs · 14,859 cycles

CRACKING FOUND AT STA 280 UPPER FLANGE BETWEEN LBL 9 AND RBL 9, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO 601R-53-11-136 REV A.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 16,901 hrs · 14,859 cycles

FOUND AT C-CHECK, FORWARD COCKPIT FLOOR SUPPORT IS CRACKED. REPLACED FORWARD FLOOR SUPPORT PER CRJ200 SRM 51-42-06 PG 1-18.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 16,901 hrs · 14,859 cycles

CRACK FOUND ON LEFT SIDE OF STA 280 AT LBL 9, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO 601R-53-11-171 REV D.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 14,301 hrs · 12,584 cycles

LAST PART EMERGENCY LIGHTS WILL NOT ILLUMINATE.SECURED STRIP CONNECTION. OPERATIONAL CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,642 hrs · 11,165 cycles

EMERGENCY EXIT LIGHT IN CEILING NEAR LAVATORY INOP. REPLACED LIGHT REF CRJ MM CH. 33. OPERATIONAL CHECKS GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 11,935 hrs · 10,543 cycles

FOUND FORWARD FLOOR EMERGENCY LIGHT IS INOP. RESECURED ELECTRICAL CONNECTOR ON LIGHT STRIP. OPERATIONAL CHECKS GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM MOTOR) · airframe 11,904 hrs · 10,517 cycles

STAB TRIM 1 DISENGAGED INFLIGHT. REPLACED MCU IAW CRJ AMM 27-42-00, OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB) · airframe 11,887 hrs · 10,499 cycles

ON CLIMB-OUT, REPEATEDLY RECEIVED STAB CH1 INOP, STATUS MSG. REPLACED HSTCU IAW MM 27-41-01. OPERATIONAL CHECK GOOD.

Part: TRIM SYSTEM — MALFUNCTIONED (ELEVATOR) · airframe 11,604 hrs · 10,249 cycles

ELEVATOR STAB TRIM STUCK IN NOSE DOWN POSITION. REPLACE HSTCU AND MOTOR CONTROL UNIT IAW CRJ 200 MM 27-42-01, 27-42-05 AND 27-40-00. OPERATIONAL CHECK GOOD. P/N ON/OFF 8396-3, S/N OFF 715, P/N ON/OFF 7062-3, S/N OFF 1296.

Part: ACTUATOR — MALFUNCTIONED (STALL WARNING) · airframe 11,455 hrs · 10,112 cycles

STALL FAIL CAUTION MESSAGE OCCURRED JUST AFTER TAKEOFF. REPLACED STICK PUSHER ACTUATOR IAW CRJ 200 MM 27-35-15, OPERATIONAL CHECK GOOD IAW CRJ MM 27-35-15.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 10,580 hrs · 9,338 cycles

AFT OVERHEAD EMERGENCY FLOODLIGHT INOP. RELAMPED LIGHT. OPERATIONAL CHECK GOOD IAW AMM 33-51-00.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 10,342 hrs · 9,130 cycles

WHILE HOLDING SHORT OF RUNWAY, RECEIVED A INTERMITTENT "CARGO SMOKE" WARNING WITH ASSOCIATED AURAL WARNING. REPLACED NR 2 CARGO SMOKE DETECTOR. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 10,334 hrs · 9,120 cycles

LIGHTED EMERGENCY EXIT SIGN ON LEFT SIDE OF GALLEY SERVICE DOOR IS INOP. RESECURED CONNECTOR. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM) · airframe 10,296 hrs · 9,084 cycles

STAB CHANNEL 2 INOP, WOULDN'T ENGAGE. REPLACED STAB TRIM MOTOR CONTROL UNIT IAW CRJ MM 27-42-05. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,802 hrs · 8,686 cycles

EXIT LIGHT BY MCD INOP. REPLACED FORWARD LOWER EMERGENCY LIGHT ASSY BY MAIN CABIN DOOR. OPERATIONAL CHECK GOOD IAW CRJ MM 33-51-21.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,700 hrs · 7,775 cycles

LOWER EMERGENCY EXIT SIGN ON RIGHT OVERWING EXIT DOES NOT ILLUMINATE. REPAIRED CONNECTOR AT RIGHT OVERWING EXIT LIGHT. OPERATIONAL CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,716 hrs · 7,787 cycles

EMERGENCY LIGHT STRIP ON RIGHT SIDE BETWEEN ROWS 5 AND 8 INOPERATIVE. REPLACED LIGHT POWER STRIP TO CENTER EMERGENCY LIGHT STRIP. OPERATIONAL CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 8,321 hrs · 7,403 cycles

CENTER CEILING EMERGENCY LIGHT OUT IN CABIN NEAR ROW 5. RELAMPED CENTER CEILING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,175 hrs · 7,261 cycles

CRACKED ANGLES AT FS 280, LBL 9 AND EIE RBL 9.00. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE AT FS 280 LBL 9 UNDER FLOOR IAW SRM 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,175 hrs · 7,261 cycles

LEFT AND RIGHT ANGLES ON 625 BULKHEAD STRINGER 13L & 13R CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLES PER CRJ 200 SRM 51-40-11 PG 1, 53-61-17 PG 2.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 7,694 hrs · 6,817 cycles

ON SHORT FINAL IB GROUND SPOILER FAULT AND FLIGHT SPOILER FAULT MESSAGE. REMOVED AND REPLACED NR 2 SECU IAW MM 27-60-01. OPERATIONAL CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 6,817 hrs · 6,051 cycles

DURING STALL TEST SYSTEM WENT TO PUSHER AND -SHAKER- AT THE SAME TIME WITH NO DELAY IN BETWEEN. REMOVED AND REPLACED STALL PROTECTION COMPUTER. OPS CHECK GOOD IAW 27-35-01. P/N: 3995100208, S/N OFF: 752.

Part: WIRE — PULLED (STICK SHAKER) · airframe 6,390 hrs · 5,697 cycles

BOTH WIRES PULLED FROM CAPTAIN'S STICK SHAKER. REPAIRED BOTH WIRES ON CAPT'S STICK SHAKER AS NEEDED. PERFORMED OPS CHECK. ALL OPS CHECKS GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 6,160 hrs · 5,487 cycles

RIGHT WINDSHIELD CRACKED (OUTER PLY) ON CLIMBOUT. RETURNED TO AIRPORT. REPLACED RIGHT WINDSHIELD IAW MM 56-00-00 AND RII CARD RII 56-402. P/N: NP-13, S/N OFF: 01094H4926.

Part: PCU — MALFUNCTIONED (FLIGHT SPOILER) · airframe 5,946 hrs · 5,290 cycles

AFTER TAKEOFF, FLIGHT SPOILER FAULT STATUS MESSAGE PERSISTED TO DESTINATION. REMOVED AND REPLACED RIGHT INBOARD FLIGHT SPOILERS PCU IAW CRJ MM 27-62-01. OPS AND LEAK CHECKS GOOD.

Part: PDU — MALFUNCTIONED (TE FLAPS) · airframe 5,461 hrs · 4,818 cycles

AFTER FLAPS REACHED 45 DEGREES WE RECEIVED A FLAPS FAIL MESSAGE.REMOVED AND REPLACED FLAP PDU OPS CHECK GOOD IAW CRJ MM 27-52-01.P/N 865D100-7 S/N OFF 0831 S/N ON 0706.

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG) · airframe 5,415 hrs · 4,776 cycles

GEAR DISAGREEMENT AND NOSE DOOR WARNING INFLIGHT. WARNINGS WENT AWAY AFTER APPROX. 5 MIN. ENROUTE TO DENVER. INSTALLED SERVICEABLE PSEU IAW CRJ MM 32-61-01. OPS CHECKS GOOD.

Part: WIRE HARNESS — INOPERATIVE (CARGO DOOR) · airframe 5,415 hrs · 4,776 cycles

IN FLIGHT, RECEIVED GEAR DISAGREEMENT WARNING MSG, AND GEAR ICONS ON EDI. COMPLIED WITH QRH. DIVERTED TO TUL. REMOVED AND REPLACED CARGO DOOR WIRE HARNESS IAW CRJ MM 32-61-00. OPS CHECK GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,292 hrs · 3,739 cycles

FS 625 STR 14 LT AND 14 RT INTERCOSTAL ANGLE CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06. P/N: 601-35012-51.

Part: DRIVE SHAFT — DAMAGED (LT WING TE FLAP) · airframe 4,292 hrs · 3,739 cycles

LEFT WING NR 4 FROM INBOARD FLEXIBLE DRIVE SHAFT IS DAMAGED AT HEX END. FOUND DURING C-CHECK INSPECTION. FLEX DRIVE REPLACED IAW CRJ MM 27-53-10-400-803. P/N: 11045D100-401, S/N OFF: 4864, S/N ON: 8082.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,292 hrs · 3,739 cycles

FS 280 RBL AND LBL 9.0 INBOARD AND OUTBOARD FLOORBEAM ANGLES CRACKED. FOUND DURING C-CHECK INPSECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21 AND 51-23-00.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,292 hrs · 3,739 cycles

FS 621.0 LEFT FLOORBEAM ANGLE LBL 42 CRACKED. FOUND DURING C-CHECK INSPECTION. DAMAGED AREA REPAIRED IAW CRJ REO 601R-53-61-117.

Part: CONTROL UNIT — MALFUNCTIONED (HORZONTAL STAB) · airframe 3,935 hrs · 3,489 cycles

STAB CH 1 INOP STATUS MESSAGE. WILL NOT ENGAGE. REMOVED AND REPLACED HORIZONTAL STABILIZER MOTOR CONTROL UNIT AND TRIM ACTUATOR IAW CRJ MM 27-42-01, 27-42-05. PERFORMED OPS CHECK OF HORIZONTAL STAB TRIM SYSTEM IAW CRJ MM 27-40-00 AND 27-41-00. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 2,482 hrs · 2,211 cycles

ON FINAL APPROACH INTO LAX, SELECTED FLAPS 20 DEGREES AND FLAPS STOPPED AT 18 DEGREES. REMOVED AND REPLACED LEFT OUTBOARD NR 3 AND NR 4 FLAP ACTUATORS IAW CRJ MM 27-53-05. CYCLED FLAPS NUMEROUS TIMES. OPS CHECK GOOD ON GROUND. COMPLIED WITH AD 98-20-01.

Part: ADC — FAILED (NR 1) · airframe 1,202 hrs · 1,013 cycles

ADC NR 1 FAILED INFLIGHT. ERRATIC V/S INDICATIONS. VSI INDICATIONS HAPPENING FOR APPROXIMATELY 4 MINUTES PRIOR TO FAILURE. INSTALLED SERVICEABLE ADC 850A IAW 34-13-00. ALL CHECKS OK ON GROUND AT THIS TIME.