N909SW

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 50,287 hrs · 43,272 cycles

APU OIL TEMP CAUTION MESSAGE IN FLIGHT. RAN QRH LANDED AT NEAREST SUITABLE. (FLT 5455 FILED CLOSED)REMOVED AND REPLACED WITH SERVICEABLE THE OIL COOLER ON THE APU IN REFERENCE TO CRJ 200 AMM 49-91-07 OPS CHECKS GOOD NO LEAKS NOTED, REMOVED AND REPLACED WITH NEW THE HIGH OIL TEMP SENSOR ON THE APU IN REFERENCE TO CRJ 200 AMM 49-91-25 OPS CHECKS GOOD NO LEAKS NOTED , REMOVED AND REPLACED WITH NEW THE OIL FILTER ON THE APU IN REFERENCE TO CRJ 200 AMM 49-91-10 NO LEAKS NOTED , CHECKED OIL LEVEL OF THE APU ITS FULL NO CONTAMINATES FOUND IN THE FILTER. RAN APU IN REFENCE TO CRJ200 AMM 49-10-00 FOR 1 HOUR WITH LOAD MAX TEMP OBSERVED WAS 184C.

Part: NONE — FAILED · airframe 49,110 hrs · 42,168 cycles

R COWL ANTI ICE CAUTION ON CLIMB OUT WITH COWL ANTI ICE SELECTED OFF RAN QRH (FLIGHT #5015 FILED CLOSED) REFERENCE TO EAML 1012961 WITH THE FOLLOWING CORRECTIVE ACTION: 'REMOVED AND REPLACED RIGHT ENGINE PRESSURE RELIEF VALVE IN REFERENCE TO CRJ 200 AMM 30-22-04. OPS CHECK GOOD IN REFERENCE TO 30-22-04 AND 71-00-00. NO MESSAGES PRESENT AT THIS TIME. AIRCRAFT OK FOR RETURN TO SERVICE.

Part: NONE — FAILED · airframe 48,193 hrs · 41,346 cycles

GEAR DISAGREE AFTER T/O , RAN QRH AND GOT DOWN 3 GREEN. RETURNED TO FIELD DUE TO ICING CONDITIONS AND LANDED OVER WEIGHT 49,000. 300FT PER MIN ON TOUCHDOWN (FLIGHT 4771 - FILED CLOSED) VERIFIED WITH CREW THAT RH MLG WAS THE GEAR THAT FAILED TO FULLY RETRACT. FOUND ALL GEAR TO BE HEAVILY ICED OVER PREVENTING GEAR RETRACTION. REMOVED ICE AND PERFORMED GEAR INSPECTION AND FOUND NO DAMAGE AT THIS TIME. SWUNG GEAR MULTIPLE TIMES WITH NO FURTHER FAULTS AT THIS TIME. REF. AMM 32-30-00, 32-10-00 AND 32-20-00 PLEASE REFERENCE AML 860010 FOR OVER WEIGHT LANDING.

Part: ANGLE — CORRODED (PAX DOORWAY) · airframe 46,600 hrs · 39,883 cycles

KICK ANGLE AT PASSENGER DOOR SILL CORRODED (C-CHECK) RO 3/24/2021 REMOVED PASSENGER DOOR KICK ANGLE. REF: CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-10, CRJ200 SRM 51-42-21. - INSTALLED NEW PASSENGER DOOR LOWER KICK ANGLE P/N 601R31527-221. REV: DWG 601R31527, REV: AM. CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-13 AND CRJ200 SRM 51-42-21, RESTORED FINISH AND APPLIED CIC TO REPAIR AREA AS REQUIRED REF. CRJ 200 SRM 51-25-01 AND 51-21-11. REFERENCE THE CONTINUE CARD FOR DETAILS. COMPLIED WITH 51-900-1003-SKY

Part: FRAME — CRACKED (BS 333 S1R) · airframe 46,600 hrs · 39,883 cycles

*FS333.00 FRAME IS CRACKED AT THE STGR1R. (C-CHECK) RO 3/24/2021 REMOVED DAMAGED FRAME SECTOR AT FS333.00 FROM STGR-0 TO STGR-5R, REPLACED AND INSTALLED NEW FRAME SECTOR P/N#6001R32004-5. REF. CRJ-200 SRM 51-42-06,SRM 51-42-21 DWG#601R32004 REV. N, AND MHI REO#601R-53-21-3409 REV -- DATE 2021-03-11. PRESSURE LEAK CHECK GOOD / COMPLIED WITH 51-900-1003-SKY

Part: THRUST WASHER — BROKEN (RT WING TE FLAP) · airframe 46,600 hrs · 39,883 cycles

RH OUTBOARD (R-1) FLAP ACTUATOR FITTING THRUST WASHER BROKEN. (C-CHECK) RO 3/24/2021 REMOVED BROKEN THRUST WASHER AND INSTALLED NEW THRUST WASHER ABOVE R-4 OTBD FLAP ACTUATOR. REF. CRJ200 SRM 51-41-02.

Part: HINGE — DAMAGED (PAX DOORWAY) · airframe 46,600 hrs · 39,883 cycles

*PAX DOOR FUSELAGE SIDE HINGE HAS OBLONG HOLES ON LUGS FOR PIANO HINGE PIN (C-CHECK) RO 3/24/2021 FOUND PAX DOOR HINGE HAFT FUSELAGE SIDE OUT OF LIMIT PER REO 601R-53-21-814 REV C DATED 2017-08-02 . REMOVED AND INSTALLED NEW AIRCRAFT SIDE HINGE HALF P/N 600-31529-15, REF: CRJ200 SRM 53-21-23 AND REO 601R-53-21-656, REV: A, 2017-03-06. COMPLIED WITH 51-900-1003-SKY

Part: ANGLE — CRACKED (BS 621) · airframe 46,600 hrs · 39,883 cycles

CLIP CRACKED AT APPROXIMATELY STGR13R ON REAR Z-MEMBER FS621 REAR BULKHEAD (C-CHECK) RO 3/24/2021 REMOVED CRACKED CLIP AT STGR 13R. REF: CRJ200 SRM 51-42-06. INSTALLED NEW CLIP P/N 601R350147-1. REF: DWG 601-35012, REV: D, REF: CRJ200 SRM 51-42-06, AND DWG 601R350147, REV: --. COMPLIED WITH 51-900-1003-SKY. REFERENCE THE CONTINUE CARD FOR A DETAILED DESCRIPTION OF WORK PERFORMED. PRESSURE CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR AREA) · airframe 46,600 hrs · 39,883 cycles

FOUND DD3 INTERCOSTAL CORRODED AT THE FWD SIDE OF THE PAX DOOR (AS MARKED). (C-CHECK) RO 3/24/2021 REMOVED CORROSION ON PAX DOOR DD3 INTERCOSTAL AT FWD SIDE REF CRJ 200 SRM 51-21-06.FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 52-00-00. MEASURED THICKNESS REPAIRED DD3 INTERCOSTAL AT THE FWD SIDE OF THE PAX DOOR REF REO 601R-52-11-2856 REV-- DATE 2021-03-06. COMPLIED WITH ALL STEPS REO 601R-52-11-2856 REV-- DATE 2021-03-06. COMPLIED WITH 51-900-1003-SKY

Part: SKIN — CHAFED (SERVICE DOOR) · airframe 46,600 hrs · 39,883 cycles

SERVICE DOOR EXTERIOR SKIN CHAFFED APPROXIMATELY 2" ABOVE FWD GUIDE PIN ON EXERIOR SERVICE DOOR HANDLE (MARKED) (C-CHECK) RO 3/24/2021 BLENDED DAMAGE AREA REF CRJ200 SRM 51-12-00.FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 52-00-31.REPAIRED REF REO 601R-52-41-455 REV-- DATE 2021-03-03 . COMPLIED WITH ALL STEPS REO 601R-52-41-455 REV-- DATE 2021-03-03

Part: SKIN — CORRODED (LT WING) · airframe 46,600 hrs · 39,883 cycles

*LH WING LOWER PLANK HAS FRETTING FROM CONTACT WITH WING FAIRING 193AB AT WS 45.00L AND AFT EDGE. (C-CHECK) RO 3/24/2021 BLENDED OUT FRETTING ON LH WING LOWER PLANK AFT EDGE AT WS45 AND FOUND IN LIMITS REF REO 601R-57-21-880 REV. D, 2017/03/06 ALL STEPS COMPLIED WITH, COMPLIED WITH 51-900-1003-SKY.

Part: SKIN — CORRODED (RT WING) · airframe 46,600 hrs · 39,883 cycles

*RH WING LOWER PLANK HAS FRETTING FROM CONTACT WITH WING FAIRING 193AB AT WS 45.00R AND AFT EDGE. (C-CHECK) RO 3/24/2021 BLENDED OUT FRETTING ON RH LOWER WING PLANK WS 45 AT AFT EDGE AND FOUND IN LIMITS REF REO 601R-57-21-880 REV D 2017/03/06 ALL STEPS COMPLIED WITH, COMPLIED WITH 51-900-1003-SKY

Part: SEAT TRACK — CORRODED (BS 358-380) · airframe 46,600 hrs · 39,883 cycles

*SEAT RAIL CORRODED LBL9, S358.00 - FS380.00. (C-CHECK) RO 3/24/2021 LBL9 SEAT TRACK AT FS 358.00 TO FS 380.00 IS OUT OF LIMITS HAVING CORROSION ON MORE THEN 2 ELEMENTS REF CRJ200 SRM 53-21-49. REMOVED LBL9 SEAT TRACK AT FS 358.00 TO FS 380.00 REF CRJ200 AMM 53-01-11-000-802. REPLACED AND INSTALLED NEW SEAT TRACK FS358.00 TO FS380.00 LBL-9 REF. CRJ-200 AMM 53-01-11-400-802

Part: SEAT TRACK — CORRODED (BS 358-380) · airframe 46,600 hrs · 39,883 cycles

*SEAT RAIL CORRODED RBL9, S358.00 - FS380.00. (C-CHECK) RO 3/24/2021 RBL9 SEAT TRACK AT FS 358.00 TO FS 380.00 IS OUT OF LIMITS HAVING CORROSION ON MORE THEN 2 ELEMENTS REF CRJ200 SRM 53-21-49. REMOVED RBL9 SEAT TRACK AT FS 358.00 TO FS 380.00 REF CRJ200 AMM 53-01-11-000-802. REPLACED AND INSTALLED NEW SEAT TRACK FS358.00 TO FS380.00 RBL-9 REF. CRJ-200 AMM 53-01-11-400-802

Part: FLOOR SUPPORT — CORRODED (BS 295-310) · airframe 46,600 hrs · 39,883 cycles

* FLOOR SILL FWD OF SERVICE DOOR HAS CORROSION BETWEEN FS310.00 AND FS295.00 (MARKED). (C-CHECK) RO 3/24/2021 BLENDED OUT CORROSION ON R/H FLOOR SILL, FWD OF SERVICE DOOR BETWEEN FS295.00 AND FS310.00 REF REO 601R-53-00-530 REV-A, DATED 2014-10-07 AND DWG# 601R31148, REV-V. REMOVED AND REPLACED CORRODED ANGLE SUPPORT PLATE WITH NEW PLATE (P/N 601R38669-49) BETWEEN FS 295.00 TO FS 310.00 REF CRJ-200 SRM 51-42-06, DWG# 601R38669 REV-N. RESTORED FINISH TO REPAIR AREA REF CRJ-200 SRM 51-25-16 AND APPLIED CIC TO REPAIR AREA REF CRJ-200 SRM 51-21-11. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION FOR DETAILS.

Part: HINGE FITTING — CORRODED (CARGO DOOR) · airframe 46,600 hrs · 39,883 cycles

* FOUND COROSSION ON THE BOTTOM HINGE FITTING OF THE CARGO COMPARTMENT DOOR(AREA MARKED) (C-CHECK) RO 3/24/2021 REMOVED AND INSTALLED NEW FWD AND AFT BOTTOM HINGE FITTINGS OF THE CARGO COMPARTMENT DOOR. REF: CRJ 200 SRM 51-42-21 AND DWG 601R35027 REV Y. COMPLIED WITH SKYCARD 51-900-1003-SKY.

Part: FLOORBEAM — DAMAGED (BS 280) · airframe 46,600 hrs · 39,883 cycles

*280.00 LEFT FLOOR POST HAS A DRILL START AT THE TOP END FORWARD SIDE. (MARKED) (C-CHECK) RO 3/24/2021 REMOVED AND INSTALLED NEW LH FLOOR POST AT FS 280 LBL 9 REF CRJ 200 SRM 51-42-06 AND DRAWING# 600-34017 REV AA, AND MHIRJ REO 601R-53-11-3674 REV --, DATED 2021-03-11. COMPLIED WITH 51-900-1003-SKY

Part: DOOR SILL — CORRODED (PAX DOOR AREA) · airframe 46,600 hrs · 39,883 cycles

* PAX DOOR LOWER SILL CORRODED AROUND AFT DRAIN HOLE (MARKED). (C-CHECK) RO 3/24/2021 REMOVED CORROSION ON PAX DOOR LOWER SILL NEAR AFT DRAIN HOLE REF CRJ200 SRM 51-21-06. COMPLIED WITH REO 601R-53-21-3406 REV -- DATED 2021-02-27. COMPLIED WITH 51-900-1003-SKY

Part: FLOORBEAM — CRACKED (BS 280) · airframe 46,600 hrs · 39,883 cycles

*FLOOR MEMBER, FS280.00, FWD FLOOR ANGLE IS CRACKED OUTBOARD ENDS, LBL9 €“ RBL9. (MARKED) (C-CHECK) RO 3/24/2021 REMOVED AND REPLACED FS280.00, FWD FLOOR ANGLE LBL9 €“ RBL9 REF. CRJ 200 SRM 51-42-06 AND DWG 600-34017 REV. AD. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: BRACKET — BROKEN (BS 621 BULKHEAD) · airframe 46,600 hrs · 39,883 cycles

*AFT CARGO PRESSURE BULKHEAD FS621.0 AT RBL9 ISOLATOR BRACKET IS BROKEN. (MARKED) (C-CHECK) RO 3/24/2021 BROKEN ISOLATOR REMOVED AND REPLACED WITH FS621 BULKHEAD REINFORCEMENT ON JOB 27558105, OP 5531.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 46,600 hrs · 39,883 cycles

*FLOOR MEMBER, FS280.00, IS CRACKED OUTBOARD ENDS, LBL9 €“ RBL9. (MARKED) (C-CHECK) RO 3/24/2021 REPAIRED FS280 BULKHEAD ASSY REF. REO 601R-53-11-926 REV. -B DATED 2006-05-10 ALL STEPS COMPLIED WITH, AND REO 601R-53-11-3666 REV. -- DATED 2021-03-12 ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: SKIN — GOUGED (BS 559 S26-27R) · airframe 46,600 hrs · 39,883 cycles

*GOUGE ON INTERNAL FUSELAGE SKIN BETWEEN STGR 27 - 26R, FS 559.00+16 - 559.00+32 (C-CHECK) RO 3/24/2021 BLENDED OUT GOUGE ON INTERNAL FUSELAGE SKIN BETWEEN STGR 27 - 26R, FS559.00+16 - 559.00+32. REF: CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 53-00-31. REPAIRED INTERNAL FUSELAGE SKIN BETWEEN STGR 27 - 26R, FS559.00+16 - 559.00+32. REO 601R-53-51-564 REV-- DATE 2021-03-04. COMPLIED WITH ALL STEPS OF 601R-53-51-564 REV-- DATE 2021-03-04

Part: SEAT TRACK — CORRODED (BS 449-559) · airframe 46,600 hrs · 39,883 cycles

*MULTIPLE AREAS OF CORROSION ON FLOOR SEAT TRACK LBL9 BETWEEN FS 499.00 €“ 559.00 (C-CHECK) RO 3/24/2021 REMOVED AND INSTALLED NEW CABIN FLOOR SEAT TRACK FROM FS499.00 TO FS559.00 LBL 9 REF CRJ-200 SRM 53-01-11. SEE CONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (BS 409-499) · airframe 46,600 hrs · 39,883 cycles

*MULTIPLE AREAS OF CORROSION ON FLOOR SEAT TRACK LBL9 BETWEEN FS 409.00+128 €“ 499.00 (C-CHECK) RO 3/24/2021 REMOVED MULTIPLE AREAS OF CORROSION ON SEAT TRACK AT LBL9 BETWEEN FS409.00+128-499.00 REF: CRJ200 SRM 51-21-06 PAGE 1 (1)FS424.00(.010) (2) FS439.00-449.85 ( .012 ) (3) FS461.00 (.010) (4) FS473.15-484 (.010) (5) FS461.00 (.008) CAL:TUC8529 DUE DATE 31 AUG.2021. SEE CONTINUATION CARD

Part: PRESSURE DECK — DENTED (BS 439-449) · airframe 46,600 hrs · 39,883 cycles

*DENT ON LH PRESSURE FLOOR SILL PANEL BETWEEN FS 449.085 €“ 439.00, LBL27 -LBL45 (C-CHECK) RO 3/24/2021 DENT DIMENSIONS ARE AS FOLLOWS: WMAX=WMIN=1.0", D=0.022", T=0.080", TMAX=0.063", D/T=0.275 AND WMIN/D= 45.45 WHERE TMAX. PERMITTED FOR DENT IS 0.063" AND ACTUAL DEPHT IS 0.080", THEREFORE FOUND OUT OF LIMITS. REF: CRJ-200 SRM 53-41-45. REPAIRED REF. MHIRJ REO 601R-53-41-2876 REV-- DATED 2021-03-02. ALL STEPS COMPLIED WITH COMPLIED WITH 51-900-1003-SKY. PRESSURE CHECKS GOOD.

Part: HINGE — CHAFED (RT AILERON) · airframe 46,600 hrs · 39,883 cycles

*R/H AILERON UPPER L/E AT CENTER HINGE CHAFED. (C-CHECK) RO 3/24/2021 REMOVED AND REPLACED RH LEADING EDGE UPPER SKIN PER REFERENCE DRAWING# 601R13031 REV K AND REO 601R-57-61-773 REV --, DATED 2021-03-02 (STEPS 1, 2, AND 3) COMPLIED WITH 51-900-1003-SKY

Part: PRESSURE DECK — CORRODED (ZONE 100) · airframe 46,600 hrs · 39,883 cycles

*MULTIPLE AREAS OF CORROSION ON RH PRESSURE FLOOR SILL PANEL. AREAS MARKED. (C-CHECK) RO 3/24/2021 REPAIRED RH PRESSURE FLOOR SILL PANEL REF REO 601R-53-41-666 REV C DATED 2012-11-06 AND REO 601R-53-41-2881 REV -- DATED 2021-03-05 AND REO 601R-53-41-2883 REV-- DATED 2021-03-22. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAIL.

Part: SPRING — CORRODED (BUTTE DOOR) · airframe 46,600 hrs · 39,883 cycles

*L/H WING O/B FLAP HINGE BOXES I/B AND O/B BUTE DOOR ACTUATOR SPRINGS HAVE CORROSION. (C-CHECK) RO 3/24/2021 REMOVED 2 EA. BAD BUTE DOOR ACTUATORS AND INSTALLED 2 EA NEW ACTUATORS ON LH WING OTBD FLAP INBD AND OTBD HINGE BOXES. REF. CRJ200 AMM 27-54-25-400-801. SEE CONTINUE CARD FOR DETAILS.

Part: STRAP — CORRODED (BS 559) · airframe 46,600 hrs · 39,883 cycles

*CORROSION ON FLOOR SUPPORT STRAP BETWEEN RBL27 €“ RBL45 AT FS 559.00 (C-CHECK) RO 3/24/2021 FLOOR SUPPORT STRAP BETWEEN RBL27 €“ RBL45 AT FS559.00 HAS CORROSION ACROSS ENTIRE LENGTH. REPLACEMENT IS NECESSARY WHEN MORE THAN 30% OF ITS LENGTH IS DAMAGED. STRAP IS OUT OF LIMITS. REF: CRJ200 SRM 53-00-00. REMOVED FLOOR SUPPORT STRAP BETWEEN RBL27 €“ RBL45 AT FS 559.00. REF: CRJ200 SRM 51-42-06. - INSTALLED NEW FLOOR SUPPORT STRAP BETWEEN RBL27 - RBL45 AT FS 559.00 WITH 3EA NEW NUTPLATES AND 1EA NEW DOMENUT. REF: CRJ200 SRM 51-42-06 AND DWG 601R31025 REV N. COMPLIED WITH 51-900-1003-SKY. PRESSURE CHECKS GOOD.

Part: PRESSURE DECK — CORRODED (CABIN) · airframe 46,600 hrs · 39,883 cycles

*MULTIPLE AREAS OF CORROSION ON LH PRESSURE FLOOR SILL PANEL. AREAS MARKED. (C-CHECK) RO 3/24/2021 REPAIRED MULTIPLE AREAS OF CORROSION ON LH PRESSURE FLOOR SILL PANEL BY COMPLYING WITH REO 601R-53-41-666 REV -C DATED 2012-11-06, AND REO 601R-53-41-2881 REV-- DATED 2021-03-05. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: FLOOR SUPPORT — GOUGED (BS 559-574) · airframe 46,600 hrs · 39,883 cycles

*GOUGE ON FLOOR BEAM LBL9 OTBD FLANGE BETWEEN FS 559.00+112 €“ 574.00 (C-CHECK) RO 3/24/2021 BLENDED GOUGE ON FLOOR BEAM LBL9 OTBD FLANGE BETWEEN FS 559.00+112 €“ 574.00. WITHIN LIMITS REF REO 601R-53-51-563 REV-- DATED 2021-02-28. COMPLIED WITH 51-900-1003-SKY.

Part: INTERCOSTAL — CRACKED (BS 621 BULKHEAD) · airframe 46,600 hrs · 39,883 cycles

* REAR PRESSURE BULKHEAD AFT SIDE HAS CRACKED INTERCOSTAL ON RH SIDE (MARKED WITH ORANGE STREAMER) (C-CHECK) RO 3/24/2021 REMOVED AND REPLACED REAR PRESSURE BULKHEAD AFT SIDE CRACKED INTERCOSTAL WITH NEW P/N: 601-35012-52 ON RH SIDE. REF: , CRJ-200 SRM 51-42-06 AND DWG. 601-35012 REV D COMPLIED WITH SKYCARD 51-900-1003-SKY..

Part: VANE — WORN (RT WING TE FLAP) · airframe 46,600 hrs · 39,883 cycles

RH INBD FLAP VANE INBD LEADING EDGE SKIN WORN FROM BUMPER STOP (C-CHECK) RO 3/24/2021 COMPLIED WITH REO 601R-57-52-004 REV-D DATE 2012-12-19 REPAIRS TO LEADING EDGE SKIN - INBOARD FLAP VANE. FOUND TO BE OUT OF LIMITS, REPLACED SKIN WITH NEW P/N 601R14303-42. REF CRJ200 SRM 51-42-10 AND DWG. 601R14302 REV.E SEE CONTINUATION CARD FOR DETAILS / COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: SKIN — CHAFED (FUSELAGE) · airframe 46,600 hrs · 39,883 cycles

*SKIN AROUND APU EXHAUST HAS 2EA SMALL CHAFES AT THE AFT EDGE OF THE SKIN CUTOUT. (C-CHECK) RO 3/24/2021 BLENDED OUT CHAFES ON SKIN AROUND APU EXAUST CUTOUT REF CRJ 200 SRM 51-21-06, FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 53-00-31. MEASURED THICKNESS .055. ORIGINAL THICKNESS .058 REF CRJ 200 SRM 53-61-31. MATERAL LOSS .003 NO MATERAL LOSS ALLOWED IN AREA . COMPLIED WITH REO 601R-53-61-7590 REV -- 2021-02-28 . COMLPIED WITH 51-900-1003-SKY

Part: ACCESS PANEL — GOUGED (LT WING TE FLAP) · airframe 46,600 hrs · 39,883 cycles

GOUGE FOUND ON INBOARD FLAP ACCSS PANEL 584AB (C-CHECK) RO 3/24/2021 DAMAGE ON FLAP PANEL 584AB FOUND OUT OF LIMITS REF CRJ 200 SRM 57-52-00, RECEIVED NEW PANEL , LOCATED AND DRILLED REF CRJ 51-40-11 , INSTALLED ON MX 22298612 JOB 27558100 OP 7005.

Part: BOLT — CORRODED (LT SPOILER) · airframe 46,600 hrs · 39,883 cycles

* LH FLIGHT SPOILER ALL ATTACH, SAFETY TAB AND BONDING WIRE HARDWARE HAS CORROSION (C-CHECK) RO 3/24/2021 REPLACED LH FLIGHT SPOILER INBOARD AND OUTBOARD SAFETY TABS AND 4 BOLTS THAT HOLD THE TABS TO A/C, REPLACED BROKEN OUTBOARD BONDING WIRE AND THE 2 SCREWS AND TWO WASHERS THAT ATTACH THE BONDING WIRE TO A/C. REPLACED THE 2 SCREWS AND 2 WASHERS THAT HOLD THE INBOARD BONDING WIRE. REPLACED THE 2 NUTS AND 2 COTTER PINS ON THE 2 ACTUATOR BOLTS DUE TO CORROSION. REPLACED THE NUT AND COTTER PIN ONTHE OUTBOARD HINGE BOLT DUE TO CORROSION. REMOVED PARTS CRJ 200 AMM 27-64-05-000-801 AND INSTALLED PARTS PER CRJ 200 AMM 27-64-05-400-801 BONDING TEST GOOD

Part: BOLT — CORRODED (LT SPOILER) · airframe 46,600 hrs · 39,883 cycles

* LH OUTBD GROUND SPOILER ALL ATTACH AND PCU LINK HARDWARE HAS CORROSION (C-CHECK) RO 3/24/2021 INSTALLED NEW LH OTBD GROUND SPOILER ATTACH AND PCU LINK HARDWARE REF CRJ-200 AMM 27-65-01-400-801, OPERATIONAL TEST OF THE GROUND SPOILERS CHECKED GOOD, SEE CONTINUATION CARD FOR DETAILS.

Part: BOLT — CORRODED (RT SPOILER) · airframe 46,600 hrs · 39,883 cycles

* RH INBD GROUND SPOILER ATTACH, PCU LINK AND BONDING WIRE HARDWARE HAS CORROSION (C-CHECK) RO 3/24/2021 INSTALLED NEW RH INBD GROUND SPOILER ATTACH, PCU LINK AND BONDING WIRE HARDWARE REF CRJ-200 AMM 27-63-01-400-801, OPERATIONAL TEST OF THE GROUND SPOILERS CHECKED GOOD, SEE CONTINUATION CARD FOR DETAILS.

Part: BOLT — CORRODED (LT SPOILER) · airframe 46,600 hrs · 39,883 cycles

* LH INBD GROUND SPOILER OUTBD ATTACH HINGE AND PCU LINK HARDWARE HAS CORROSION (C-CHECK) RO 3/24/2021 INSTALLED NEW LH INBD GROUND SPOILER OUTBD ATTACH HINGE AND PCU LINK HARDWARE REF CRJ-200 AMM 27-65-01-400-801, OPERATIONAL TEST OF THE GROUND SPOILERS CHECKED GOOD, SEE CONTINUATION CARD FOR DETAILS.

Part: BOLT — CORRODED (LT SPOILERON) · airframe 46,600 hrs · 39,883 cycles

* LH SPOILERON ALL ATTACH AND SAFETY TAB HARDWARE HAS CORROSION (C-CHECK) RO 3/24/2021 REMOVED AND REPLACED ALL ATTACH AND SAFETY TAB HARDWARE THAT HAVE CORROSION WITH NEW HARDWARE IAW CRJ200 AMM 27-64-01-400-801STEP 2.B AND STEP 2.C. AND CRJ200 AMM 27-62-01-400-801 STEP 2.B.(6-7), OPERATIONAL TEST OF THE LH SPOILERON CHECKED GOOD, SEE CONTINUATION CARD FOR DETAILS.

Part: BOLT — CORRODED (RT SPOILERON) · airframe 46,600 hrs · 39,883 cycles

* RH SPOILERON ALL ATTACH AND SAFETY TAB HARDWARE HAS CORROSION (C-CHECK) RO 3/24/2021 INSTALLED NEW RH SPOILERON ATTACH AND SAFETY TAB HARDWARE REF CRJ-200 27-64-01-400-801, OPERATIONAL TEST OF THE FLIGHT SPOILER/SPOILERON CHECKED GOOD, SEE CONTINUATION CARD FOR DETAILS.

Part: BOLT — CORRODED (RT SPOILER) · airframe 46,600 hrs · 39,883 cycles

* RH OUTBD GROUND SPOILER ALL ATTACH AND PCU LINK HARDWARE HAS CORROSION (C-CHECK) RO 3/24/2021 INSTALLED NEW RH OUTBD GROUND SPOILER ATTACH AND PCU LINK HARDWARE REF CRJ-200 AMM 27-63-01-400-801, OPERATIONAL TEST CHECKED GOOD, SEE CONTINUATION CARD FOR DETAILS.

Part: BOLT — CORRODED (RT SPOILER) · airframe 46,600 hrs · 39,883 cycles

* RH FLIGHT SPOILER ALL ATTACH AND SAFETY TAB HARDWARE HAS CORROSION (C-CHECK) RO 3/24/2021 INSTALLED NEW RH FLIGHT SPOILER ATTACH AND SAFETY TAB HARDWARE REF CRJ-200 AMM 27-64-05-400-801, OPERATIONAL TEST OF THE FLIGHT SPOILER/SPOILERON CHECKED GOOD, SEE CONTINUATION CARD FOR DETAILS.

Part: FRAME — CRACKED (BS 364) · airframe 46,600 hrs · 39,883 cycles

* ACFT SIDE, FS364.00 AVIONICS FWD FRAME / LH DOOR GUIDE IS CRACKED. FLAGGED (C-CHECK) RO 3/24/2021 REMOVED AND REPLACED L/H DOOR GUIDE ON THE AVIONICS FWB FRAME IAW CRJ 200 SRM 51-41-02

Part: FRAME — CRACKED (BS 394) · airframe 46,600 hrs · 39,883 cycles

* ACFT SIDE, FS394.00 AVIONICS AFT FRAME / LH DOOR GUIDE IS CRACKED. FLAGGED (C-CHECK) RO 3/24/2021 REMOVED AND REPLACED L/H DOOR GUIDE ON THE AVIONICS AFT FRAME IAW CRJ 200 SRM 51-41-02

Part: FRAME — CRACKED (BS 394) · airframe 46,600 hrs · 39,883 cycles

* ACFT SIDE, FS394.00 AVIONICS AFT FRAME / RH DOOR GUIDE IS CRACKED. FLAGGED (C-CHECK) RO 3/24/2021 REMOVED AND REPLACED THE R/H DOOR QUIDE ON THE AVIONICS AFT FRAME IAW CRJ 200 SRM 51-41-02

Part: POWER SUPPLY — FAILED (TE FLAPS) · airframe 44,120 hrs · 37,664 cycles

FLAP FAIL ON DEPARTURE, COMPLIED WITH QRH. RETURNED TO FIELD. LANDED WITHOUT INCIDENT. (FLT#5300) CLOSED REMOVED AND REPLACED LEFT BPSU IAW AMM. OPS AND RIG CHECKS GOOD.

Part: WIRE HARNESS — FAILED (NLG) · airframe 42,648 hrs · 36,338 cycles

GEAR DISAGREE WARNING MESSAGE DURING CLIMB. REMOVED AND REPLACED THE NLG DOWNLOCK WIRE HARNESS NR 2 PS2GA IAW AMM. OPS CHECKED GOOD.

Part: SWITCH — FAILED (PITCH TRIM) · airframe 41,588 hrs · 35,368 cycles

STAB AND MACH TRIM DISENGAGED AFTER TAKE OFF, EMERGENCY DECLARED. RTF. (FLT 5118) FO: 01/02/2018 CLOSED REPLACED CAPTAINS PITCH TRIM DISCONNECT SWITCH AND HSTCU. OPS CHECK NORMAL.

Part: PROXIMITY SENSOR — OUT OF ADJUST (MLG) · airframe 41,546 hrs · 35,335 cycles

RETURNED TO FIELD DUE TO TO GEAR DISAGREE. NLG DID NOT RETRACT. ADJUSTED THE NLG PROXIMITY SENSORS, PERFORMED MULTIPLE GEAR SWINGS. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 40,609 hrs · 34,469 cycles

SMOKE TOILET CAUTION. RETURNED TO FIELD. EMERGENCY DECLARED. REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR IAW AMM. OPS CHECKED GOOD.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 38,529 hrs · 32,503 cycles

LEFT HAND I/B FLAP VANE LEADING EDGE CHAFE OUT OF LIMITS. REPLACED LEFT HAND I/B FLAP VANE LEADING IAW SRM.

Part: STRUT — UNDERSERVICED (NLG) · airframe 37,104 hrs · 31,163 cycles

CREW REPORTS NLG WOULD NOT RETRACT AFTER TAKEOFF. RETURN TO THE FIELD. PERFORMED FULL SERVICE ON NLG STRUT AND MULTIPLE GEAR SWINGS, OPS CHECK GOOD ON GROUND, WILL DO FUNCTIONAL CHECK.

Part: CONNECTOR — ARCED (WINDOW HEAT) · airframe 35,737 hrs · 29,956 cycles

DURING CRUISE, THE LT COCKPIT WINDOW BEGAN TO ARC AT THE ELECTRICAL CONNECTOR POINT ON THE UPPER PART OF THE WINDOW. THE WINDOW THEN SHATTERED AND SMOKE WAS OBSERVED IN THE FLIGHT DECK. R & R LT SIDE WINDOW, REFERENCE APPLICABLE STEPS IN AMM OPS CHECKS GOOD AT THIS TIME. LEAK CHECKS GOOD AT THIS TIME. M19:469041, PN ON: NP-139322-11, SN ON: 14323H5693, PN OFF: NP-139322-001, SN OFF: 02109H4363.

Part: PRIORITY VALVE — SLOW (NLG) · airframe 34,819 hrs · 29,171 cycles

AFTER DEPARTURE, NOSE GEAR MADE UNUSUAL NOISES, FOLLOWED BY A DELAY IN THE GEAR UP INDICATION. FOLLOWED BY A GEAR DISAGREE CAUTION MESSAGE. RAN THE APPROPRIATE QRH PROCEDURE, MESSAGES ALL CLEARED WITH GEAR DOWN AND 3 GREEN. RETURNED TO FIELD IAW QRH. R & R THE NLG PRIORITY VALVE IAW AMM, OPS CHECK AND LEAK CHECK GOOD. JACKED ACFT AND SWUNG GEAR SEVERAL TIMES IAW AMM. NO FURTHER FAULTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG) · airframe 34,811 hrs · 29,163 cycles

DURING DEPARTURE, GEAR DISAGREE WARNING MESSAGE DURING GEAR RETRACTION. RIGGED FWD NLG DOORS, AND CHECKED GAPS FOR NLG PROXIMITY SENSORS. ALL GAPS GOOD IAW AMM. PERFORMED GEAR SWING IAW AMM, OPS CHECK GOOD AT THIS TIME.

Part: BEARING — FAILED (PAX DOOR) · airframe 34,631 hrs · 29,020 cycles

CABIN DOOR WON'T OPEN. REPLACED MCD PRESSURE VALVE SPRING ROD BEARING IAW AMM.

Part: OIL COOLER — MALFUNCTIONED (APU) · airframe 33,860 hrs · 28,427 cycles

FOLLOWING A GEN 2 FAILURE, CREW COMPLIED WITH QRH AND DESCENDED TO 300FT AND STARTED APU. RECEIVED AN APU HIGH OIL TEMP. REPLACED APU OIL COOLER IAW AMM.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 33,786 hrs · 28,350 cycles

EMERGENCY EXIT SIGN ON WARDROBE INOPERATIVE. C-CHECK, R & R CONNECTORS ON EMERGENCY EXIT SIGN IAW ESPM.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 33,786 hrs · 28,350 cycles

CORROSION FOUND ON BS 349 RBL 45 FLOORBEAM. C-CHECK, REPAIRED FLOORBEAM IAW SRM.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 33,786 hrs · 28,350 cycles

SERVICE DOOR LOWER DOOR SILL STRUCTURE, FOUND CORROSION AT THE AFT LOWER LATCH FITTING AREA. C-CHECK, SERVICE DOOR LOWER SILL SURROUND STRUCTURE REPLACED IAW SRM AND AMM.

Part: STOP FITTING — CRACKED (WS 163) · airframe 33,786 hrs · 28,350 cycles

BUTTE DOOR STOP ASSY AT WS 163 IS CRACKED. C-CHECK, R & R IAW SRM.

Part: ROLLER — CHAFED (RT WING TE FLAP) · airframe 33,786 hrs · 28,350 cycles

RIGHT OTBD FLAP INBD ROLLER FITTING CHAFED FROM CONTACT WITH THE WING T/E ALIGNMENT FITTING. C-CHECK, BLENDED DAMAGED AREA, IAW REO.

Part: STIFFENER — CRACKED (BS 621 BULKHEAD) · airframe 33,786 hrs · 28,350 cycles

STIFFENER ANGLE ON FS 621 BULKHEAD AFT SIDE AT WL 79.5, OTBD OF LBL 36 FRAME, CRACKED ON INBD SIDE. C-CHECK, R & R STIFFENER ANGLE ON FS 621, BULKHEAD AFT SIDE AT WL 79.5, OTBD OF LBL 36 FRAME IAW SRM.

Part: ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 33,786 hrs · 28,350 cycles

FS 621 BULKHEAD AFT SIDE HAS CRACKED ANGLE AT S14L. C-CHECK, R & R ANGLE IAW SRM.

Part: SKIN — CORRODED (LT WING) · airframe 33,786 hrs · 28,350 cycles

LEFT WING PLANK, 540BB ACCESS HOLE HAS PITTING CORROSION AROUND RIM AT SEVERAL LOCATIONS. C-CHECK, LOWER LT WING PLANK AT PANEL LOCATION 540BB PITTING CORROSION TREATED IAW REO.

Part: ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 33,786 hrs · 28,350 cycles

BS 621 BULKHEAD AFT SIDE HAS CRACKED ANGLE AT S14R. C-CHECK, R & R ANGLE IAW SRM.

Part: SKIN — CORRODED (LT WING) · airframe 33,786 hrs · 28,350 cycles

LEFT WING PLANK, 510 AB ACCESS HOLE HAS PITTING CORROSION ON RIM. C-CHECK, LOWER LT WING PLANK AT PANEL LOCATION 510AB PITTING CORROSION TREATED IAW REO.

Part: FRAME — CHAFED (BS 280) · airframe 33,786 hrs · 28,350 cycles

CHAFE DAMAGE ON FRAME BS 280, BETWEEN S2 - 3L. C-CHECK, FABRICATED REPAIR STRAP IAW EA.

Part: SPLICE — CRACKED (BS 283) · airframe 33,786 hrs · 28,350 cycles

INBD AND OTBD SPLICE ANGLES AT BS 283, S3L CRACKED. C-CHECK, INSTALLED NEW SPLICE ANGLES IAW SRM.

Part: STRUCTURE — CORRODED (E/E BAY DOOR) · airframe 33,786 hrs · 28,350 cycles

CORROSION ON INNER SURFACE OF AVIONICS BAY DOOR CUTOUT FWD SIDE, AROUND SEAL MATING AREA. C-CHECK, BLENDED CORROSION AVIONICS BAY DOOR CUTOUT FWD SIDE IAW REO.

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 33,786 hrs · 28,350 cycles

TWO FLOORBEAM VERTICAL ATTACH ANGLES ARE CRACKED AT FS 484, LBL 28 AND LBL 36. C-CHECK, R & R ATTACH ANGLES IAW SRM.

Part: VERTICAL BEAM — CRACKED (BS 409 BULKHEAD) · airframe 33,786 hrs · 28,350 cycles

VERTICAL BEAM ON BULKHEAD BS 409+128 AT RBL 36 INBD CRACKED AT LOWER RADIUS. C-CHECK, R & R VERTICAL BEAM IAW SRM.

Part: SUPPORT — CHAFED (PAX DOOR) · airframe 33,786 hrs · 28,350 cycles

PASSENGER DOOR SUPPORT WHEEL LEG CHAFING ON HANDRAIL. C-CHECK, REPAIRED IAW EA.

Part: LEVER — CHAFED (PAX DOOR) · airframe 33,786 hrs · 28,350 cycles

PASSENGER DOOR FORWARD PULL-IN LEVER CHAFED. C-CHECK, REPAIRED LEVER IAW REO.

Part: CAP — DENTED (PAX DOOR) · airframe 33,786 hrs · 28,350 cycles

PASSENGER DOOR UPPER INTERIOR CORNER CAP DENTED. C-CHECK, REPAIRED PAX DOOR IAW REO.

Part: CAP — DENTED (PAX DOOR) · airframe 33,786 hrs · 28,350 cycles

PASSENGER DOOR UPPER FWD INTERIOR CORNER CAP DENTED. C-CHECK, REPAIRED PAX DOOR IAW REO C.

Part: SUPPORT FITTING — CHAFED (PAX DOOR HANDLE) · airframe 33,786 hrs · 28,350 cycles

PASSENGER DOOR INNER HANDLE TORQUE TUBE SUPPORT FITTING CHAFED. C-CHECK, REPAIRED PASSENGER DOOR INNER HANDLE TORQUE TUBE SUPPORT FITTING IAW EA.

Part: STRUCTURE — CHAFED (PAX DOOR) · airframe 33,786 hrs · 28,350 cycles

PASSENGER DOOR ICE BREAK CABLE CHAFING ON PRESSURE DOOR. C-CHECK, REPAIRED CHAFING IAW REO.

Part: BULKHEAD — GOUGED (BS 621) · airframe 33,786 hrs · 28,350 cycles

THREE SMALL GOUGES ON REAR PRESSURE BULKHEAD ON RT SIDE WL 103, RBL18 ,27.5 AND 36. C-CHECK, BULKHEAD REPAIRED IAW REO.

Part: SKIN — CHAFED (FUSELAGE) · airframe 33,786 hrs · 28,350 cycles

RT LOWER SKIN T/E CHAFED AT RBL 45.0. C-CHECK, REPAIRED IAW REO AND SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,786 hrs · 28,350 cycles

RIGHT WING INBD FLAP VANE L/E CHAFED OTBD OF CENTER SLIDING BEAM ACTUATOR. C-CHECK, BLENDED OUT CHAFE ON RT WING INBD FLAP VANE OTBD MID L/E SKIN IAW REO.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 33,786 hrs · 28,350 cycles

LT MLG DOOR INNER L/E SKIN CHAFED AT 10" INBD OF OTBD END. C-CHECK, CUTOUT AND REPAIRED L/E SKIN ON LT MLG DOOR IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 33,786 hrs · 28,350 cycles

RIGHT AILERON LOWER INBD L/E FIXED SHROUD SKIN CHAFED. C-CHECK, BLENDED CHAFED AREA IAW REO AND SRM.

Part: CONTROL ARM — CHAFED (RT MLG DOOR) · airframe 33,786 hrs · 28,350 cycles

RT MLG DOOR LOWER CONTROL ARM CHAFED AT INBD END. C-CHECK, BLENDED CHAFED AREAS OF RT MLG DOOR STRUT AND BELLCRANK IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,786 hrs · 28,350 cycles

RIGHT WING INBD FLAP VANE L/E CHAFED INBD OF INBD SLIDING BEAM ACTUATOR. C-CHECK, BLENDED OUT CHAFE ON RT WING INBD FLAP VANE INBD L/E SKIN IAW SRM AND REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,786 hrs · 28,350 cycles

RIGHT WING INBD FLAP VANE L/E CHAFED OTBD OF OTBD SLIDING BEAM ACTUATOR. C-CHECK, BLENDED OUT CHAFE ON RT WING INBD FLAP VANE OTBD L/E SKIN IAW SRM.

Part: SKIN — CHAFED (FUSELAGE) · airframe 33,786 hrs · 28,350 cycles

LT LOWER SKIN TRAILING EDGE CHAFED AT LBL 45.0. C-CHECK, REPAIRED IAW REO AND SRM.

Part: FITTING — CHAFED (RT WING TE FLAP) · airframe 33,786 hrs · 28,350 cycles

RIGHT WING OTBD FLAP ALIGNMENT FITTING AT WS 169.94 CHAFED. C-CHECK, REPLACEDFITTING IAW REO AND SRM.

Part: SKIN — CHAFED (RT AILERON) · airframe 33,786 hrs · 28,350 cycles

RIGHT AILERON UPPER SKIN L/E SHROUD CHAFED IN VARIOUS PLACES. C-CHECK, BLENDED CHAFED AREA IAW REO.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 33,786 hrs · 28,350 cycles

LEFT MLG DOOR INNER L/E SKIN CHAFED AT OTBD END. C-CHECK, REPAIRED LT MLG DOOR INNER L/E SKIN IAW REO.

Part: ACCESS PANEL — CHAFED (LT WING) · airframe 33,786 hrs · 28,350 cycles

LT WING ACCESS PANEL 599BB CHAFED. C-CHECK, BLENDED LT WING ACCESS PANEL 599BB IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,786 hrs · 28,350 cycles

LEFT INBD FLAP VANE L/E SKIN CHAFED NEAR OTBD END. C-CHECK, BLENDED OUT CHAFE ON LT WING INBD FLAP VANE OTBD L/E SKIN IAW SRM. AND REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,786 hrs · 28,350 cycles

LEFT INBD FLAP VANE L/E SKIN CHAFED AT CENTER. C-CHECK, BLENDED OUT CHAFING DAMAGE ON LT INBD FLAP VANE OTBD MID L/E SKIN IAW REO AND SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,786 hrs · 28,350 cycles

LEFT INBD FLAP VANE L/E SKIN CHAFED NEAR INBD END. C-CHECK, BLENDED OUT CHAFE ON LT WING INBD FLAP VANE INBD L/E SKIN IAW SRM AND REO.

Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 3) · airframe 31,420 hrs · 26,493 cycles

DURING GEAR EXTENSION, RECEIVED HYDRAULIC 3 LOW PRESSURE CAUTION MESSAGE FOLLOWED BY GEAR DISAGREE WARNING MESSAGE & NOSE DOOR WARNING MESSAGE. THESE LASTED FOR APPROXIMATELY FIVE SECONDS. THE NOSE WHEEL CAME DOWN & MESSAGES WENT AWAY. FLT#5235 BLED AIR FROM NR 3 HYDRAULIC SYSTEM, PERFORMED SEVERAL GEAR SWINGS IAW AMM. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,993 hrs · 26,173 cycles

EMERGENCY EXIT SIGN LIGHTS OVER EACH DOOR ARE BURNED OUT. RELAMPED.

Part: BALLAST — FAULTY (LAVATORY) · airframe 30,702 hrs · 25,946 cycles

LIGHT ABOVE SINK IN LAV IS DIM AND HAS A SLIGHT ELECTRICAL SMELL. (FLT 6234) REPLACED LAVATORY LIGHT BALLAST.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,199 hrs · 25,569 cycles

AFT CABIN EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 5495) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,906 hrs · 25,354 cycles

OVERHEAD EMERGENCY LIGHT NR 3 BURNED OUT. (FLT 6300) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,707 hrs · 25,205 cycles

EMERGENCY LIGHT AT FLOOR LEVEL AT MAIN CABIN DOOR IS BURNED OUT. (FLT 6419) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,630 hrs · 25,147 cycles

NR 2 CEILING LEVEL EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 6474) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,630 hrs · 25,147 cycles

NR 4 RIGHT SIDE EXTERIOR EMERGENCY LIGHT BURNED OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: STRUCTURE — CRACKED (RT WING) · airframe 29,598 hrs · 25,115 cycles

RIGHT TRUNNION LOWER PLANK HOLES CRACKED 4 EACH. (C-CHECK) REPAIRED DISCREPANT HOLES IN WING ASSEMBLY (STEEL STRAP, LOWER WING PLANK, LOWER FLANGE OF TRUNNION) AT WS 65.75 BETWEEN REAR SPAR AND AUX SPAR IAW REO.

Part: TRUNNION — CRACKED (LT MLG) · airframe 29,598 hrs · 25,115 cycles

LEFT TRUNNION LOWER PLANK HOLES CRACKED 6 EACH. (C-CHECK) REPLACED LEFT MLG TRUNNION IAW SRM.

Part: SKIN — DAMAGED (RT WING) · airframe 29,598 hrs · 25,115 cycles

FOUND 3 EACH PREVIOUSLY OVERSIZED HOLES THRU RIGHT LOWER WING PLANK. (C-CHECK) REPAIRED IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 29,598 hrs · 25,115 cycles

CRACK NOTED & MARKED ON FS 409.128 VERTICAL POST AT LBL 18.00 WL 69.00 OUTBOARD AFT RADIUS. (C-CHECK) REPLACED CRACKED FS 409+128 POST AT LBL 18 IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,430 hrs · 24,969 cycles

NUMBER 1 WHITE EMERGENCY LIGHT AT FLOOR LEVEL BY MAIN CABIN DOOR INOPERATIVE. (FLT 5556) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,575 hrs · 23,499 cycles

RIGHT WING EXTERIOR EMERGENCY EXIT LIGHT IS OUT. (FLT 5543) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,451 hrs · 23,409 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5537) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,135 hrs · 23,181 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5228) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,088 hrs · 23,149 cycles

NR 2 CEILING EMERGENCY LIGHT IS OUT. (FLT 5379) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,862 hrs · 22,963 cycles

AFT OVERHEAD EMERGENCY LIGHT WILL NOT ILLUMINATE. (FLT 6439) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,862 hrs · 22,963 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5316) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,809 hrs · 22,919 cycles

THE 2ND TO LAST OVERHEAD EMERGENCY LIGHT BURNED OUT. (FLT 6420) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,514 hrs · 22,681 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6235) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,448 hrs · 22,625 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5454) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,408 hrs · 22,598 cycles

AFT EXTERIOR EMERGENCY LIGHT ON RIGHT SIDE OF A/C BURNED OUT. (FLT 5516) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,408 hrs · 22,598 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,380 hrs · 22,577 cycles

AFT 2 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 5350) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,380 hrs · 22,577 cycles

NR 1 AND 2 OVERHEAD EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,345 hrs · 22,551 cycles

NR 1 & NR 3 CEILING EMERGENCY LIGHTS ARE OUT. (FLT 6495) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,232 hrs · 22,460 cycles

NR 3 & NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 6459) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,182 hrs · 22,412 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5635) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,182 hrs · 22,412 cycles

NR 2 AND NR 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 5470) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,133 hrs · 22,374 cycles

NR 2 CEILING EMERGENCY LIGHT IS OUT. (FLT 6393) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,054 hrs · 22,318 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5406) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,985 hrs · 22,268 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6534) RELAMPED EMERGENCY LIGHT.

Part: TIRE — BURST (MLG) · airframe 25,837 hrs · 22,153 cycles

2 MLG TIRE BLEW OUT ON TAKEOFF. (FLT 6506) REPLACED MLG WHEEL ASSEMBLY AND MLG WIRING HARNESS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,660 hrs · 22,031 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5641) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,574 hrs · 21,967 cycles

FS 559 PRESSURE BULKHEAD CRACKED AT RIGHT SIDE. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,574 hrs · 21,967 cycles

FS 559 PRESSURE BULKHEAD CRACKED AT LEFT SIDE. (C-CHECK) REPAIR PER REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 26,688 hrs · 22,816 cycles

CRACK IN THE AIRCRAFT SKIN JUST BELOW THE FORWARD CORNER OF THE AFT TRU BAY DOOR LATCH ON THE LEFT SIDE. (C-CHECK) REPLACED TRU DOOR LANDING SKIN PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 26,688 hrs · 22,816 cycles

CRACKED INTERCOSTAL LOCATED AT FRAME STA 320 DATUM 7. (C-CHECK) REPLACED PER SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 26,688 hrs · 22,816 cycles

FS 409.+128 BL 0.00 LEFT AFT RADIUS OF VERTICLE POST CRACKED. (C-CHECK) REPAIRED PER SRM.

Part: SKIN — CHAFED (FUSELAGE) · airframe 26,688 hrs · 22,816 cycles

NR 3 TRU ELECTRICAL WIRES CHAFING ON THE TRU BAY LOWER SKIN. (C-CHECK) REPAIRED PER REO.

Part: SKIN — CRACKED (PAX DOOR) · airframe 26,688 hrs · 22,816 cycles

FOUR CRACKS MARKED ON LOWER PORTION OF PAX DOOR INNER SKIN. (C-CHECK) REPAIRED PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,536 hrs · 21,933 cycles

NR 4 CEILING EMERGENCY LIGHT IS OUT. (FLT 6908) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,450 hrs · 21,856 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6360) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,287 hrs · 21,730 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6498) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,150 hrs · 21,632 cycles

NR 2 CEILING EMERGENCY LIGHT IS OUT. (FLT 6223) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,075 hrs · 21,570 cycles

EMERGENCY LIGHT FORWARD OF THE MAIN CABIN DOOR IS OUT. (FLT 6690) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,035 hrs · 21,532 cycles

NR 4 CEILING EMERGENCY LIGHT IS OUT. (FLT 6607) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,968 hrs · 21,481 cycles

RIGHT EXTERIOR OVERWING AFT EMERGENCY EXIT LIGHT IS OUT. (FLT 7005) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,633 hrs · 21,226 cycles

TWO OVERHEAD EMERGENCY LIGHTS OUT. (FLT 5801) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,576 hrs · 21,194 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6860) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,459 hrs · 21,087 cycles

RIGHT WING CENTER EMERGENCY EXIT LIGHT INOPERATIVE. (FLT 6408) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,239 hrs · 20,896 cycles

AFT CEILING EMERGENCY LIGHT IS NOT ILLUMINATED. (FLT 6656) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,625 hrs · 19,587 cycles

NR 2 CEILING EMERGENCY FLOOD LIGHT INOP. (FLT 6022) RELAMPED EMERGENCY LIGHT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 22,331 hrs · 19,330 cycles

FUSELAGE SKIN CRACKED BELOW THE FORWARD CORNER OF THE AFT TRU BAY DOOR LATCH. (SVC CHECK) COMPLIED WITH TEMPORARY REPAIR PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,151 hrs · 19,184 cycles

CABIN EMERGENCY LIGHT AT ROW 10 INOP. (FLT 6681) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,779 hrs · 18,882 cycles

NR 3 EMERGENCY CEILING LIGHT INOP. (FLT 6520) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,929 hrs · 18,208 cycles

AFT EMERGENCY LIGHT INOP. (FLT 5919)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,700 hrs · 18,028 cycles

NR 3 CEILING EMERGENCY FLOODLIGHT INOP. (FLT 6132) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,645 hrs · 17,987 cycles

EMERGENCY LIGHT INOP OVER ROW 10. (FLT 5959) RELAMPED EMERGENCY CEILING LIGHT AT ROW 10 AS REQUIRED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 20,435 hrs · 17,821 cycles

FS 484 INTERCOSTAL CLIP CRACKED. (C CHECK) REPLACED CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,428 hrs · 17,815 cycles

FS 202 BULKHEAD CRACKED. (C CHECK) REO REPAIR IN PROGRESS.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,747 hrs · 18,064 cycles

FS 202 BULKHEAD CRACKED. (C CHECK) REPAIRED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 20,747 hrs · 18,064 cycles

FS 280 CLIPS CRACKED. (C CHECK) REPLACED PER SRM.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 20,747 hrs · 18,064 cycles

FS 280 BULKHEAD GOUGED. (C CHECK) REPAIRED PER REO.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 20,747 hrs · 18,064 cycles

FS 621 BRACKET CRACKED. (C CHECK) REPLACED PER SRM.

Part: FITTING — CRACKED (CARGO BAY) · airframe 20,747 hrs · 18,064 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 20,747 hrs · 18,064 cycles

FS 484 INTERCOSTAL CLIP AT LBL 36 CRACKED. (C CHECK) REPLACED PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,368 hrs · 17,765 cycles

EMERGENCY LIGHT AT ROW 10 INOP. (FLT 6352) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 18,970 hrs · 16,671 cycles

FLT 6495 - EMERGENCY LIGHT ON CEILING AT ROW 2 INOP. RELAMPED.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 18,194 hrs · 16,071 cycles

FLT 5808 - ABORTED TAKEOFF FOR "SMOKE TOILET" CAUTION MSG. RAN ENGINES AND APU BLEEDS, OPERATED PACKS AT FULL HOT, UNABLE TO DUPLICATE.

Part: ACM — MALFUNCTIONED (RIGHT) · airframe 18,155 hrs · 16,042 cycles

ON CLIMB OUT SMOKE TOILET MESSAGE. (FLT 6752)REPLACED RIGHT ACM PN 782790-15 SN ON 200404155 SN OFF 200211021.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 18,155 hrs · 16,042 cycles

SMOKE TOILET WARNING ON TAKEOFF. (FLT 6690)REPLACED COALESCER BAGS ON LT AND RT WATER SEPARATORS. RAN ENGINES AT POWER, NO WARNINGS DISPLAYED.

Part: SMOKE WARNING — ACTIVATED (LAVATORY) · airframe 18,121 hrs · 16,019 cycles

ON CLIMB, SMOKE TOILET CAUTION MESSAGE APPEARED FOR 2-3 MINUTES (FLT 6664). ACCOMPLISHED ENGINE GROUND RUNS WITH BOTH PACKS RUNNING. NO SMOKE MESSAGES, NO SMOKE IN LAVATORY.

Part: A/C PACK — OVERHEATED (LEFT) · airframe 18,059 hrs · 15,967 cycles

FLT 6695 - LEFT PACK "HI TEMP" CAUTION ON ECS PAGE AND BURNING ODOR NOTED IN AIRCRAFT. REPLACED LEFT PACK AND LEFT PACK RAM AIR CHECK VALVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,018 hrs · 15,933 cycles

CEILING RECESSED EMERGENCY LIGHT, MOST FORWARD, INOP (FLT 6588). RELAMPED EMERGENCY LIGHT.

Part: PDU — MALFUNCTIONED (THRUST REVERSER) · airframe 16,820 hrs · 14,916 cycles

RECEIVED A "R REV UNLOCKED" CAUTION MESSAGE, FLIGHT NR 6370. REPLACED THE NR 2 THRUST REVERSER PDU IAW MM 78-32-03. OPS CHECK GOOD AT THIS TIME.

Part: EXTINGUISHER — DISCHARGED (RT ENGINE) · airframe 16,434 hrs · 14,567 cycles

RIGHT ENGINE FIRE BOTTLE DISCHARGED. REPLACED FIRE BOTTLE IAW CRJ 200 MM 26-21-07.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 16,793 hrs · 14,888 cycles

STN 280 AT LBL9.0 AND RBL9.0 UPPER FLOOR SUPPORT ANGLE IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO601R 53-11-136.

Part: MOUNT — WORN (LT ENGINE) · airframe 16,793 hrs · 14,888 cycles

LEFT ENGINE AFT MOUNT IS WORN, FOUND AT C-CHECK. REPLACED ENGINE THRUST MOUNT FITTING AND BOLTS IAW CRJ200 AMM 71-22-01-400-801.

Part: SHAFT — WORN (RT ENGINE MOUNT) · airframe 16,793 hrs · 14,888 cycles

RIGHT ENGINE AFT MOUNT THRUST SHAFT IS WORN, FOUND AT C-CHECK. REPLACED ENGINE THRUST SHAFT IAW CRJ200 AMM 71-00-00-400-801.

Part: COALESCER BAG — ODOR (CABIN AIR) · airframe 16,372 hrs · 14,509 cycles

FLT 5924 - AFTER TAKEOFF RECEIVED SMOKE TOILET CAUTION MESSAGE. REPLACED LEFT AND RIGHT COALESCER BAGS IAW AMM 21-51-13. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECK GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 16,351 hrs · 14,489 cycles

FLT 6755 - SMOKE IN CABIN AFTER TAKEOFF. INSPECTED CABIN FOR ODOR AND HEAT RELATED ISSUES. NO DEFECTS NOTED. ALL OPS CHECK GOOD.

Part: QUICK DISCONNECT — LOOSE (NR 1 BRAKE) · airframe 15,592 hrs · 13,872 cycles

ON LANDING ROLL, THE AIRPLANE SEEMED TO VEER TO THE RIGHT WHEN BRAKES WERE APPLIED, FLIGHT NR 6472. FOUND NR 1 BRAKE QUICK DISCONNECT TO BE LOOSE. SECURED THE QUICK DISCONNECT FITTING IAW CRJ 200 AMM 32-41-05. OPS CHECK GOOD.

Part: LINE — LEAKING (NR 1 HYD SYSTEM) · airframe 13,497 hrs · 12,064 cycles

HYD 1 LOW PRESSURE AT FL 190, NO QUANTITY OR PRESSURE. REPAIRED LEAK IN NR 1 PRESSURE LINE. OPERATIONAL AND LEAKS CHECKS GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 11,758 hrs · 10,573 cycles

CAPTIANS (LEFT) WINDSHIELD SHATTERED AT 17,000'. REMOVED AND REPLACED CAPTAIN'S WINDSHIELD IAW CRJ MM 56-00-00, 56-11-01, 56-12-01AND RII CARD 56-402. OPERATIONAL CHECKS GOOD,

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 11,193 hrs · 10,056 cycles

AFT OVERHEAD EMERGENCY LIGHT INOP. RELAMPED AFT OVERHEAD EMERGENCY LIGHT. OPERATIONAL TEST GOOD.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 11,193 hrs · 10,056 cycles

STALL FAIL CAUTION AND SPOILERON FAIL STATUS MSG AFTER LANDING. REPLACED RIGHT HAND SPOILERON INBOARD PCU (NR 2 HYD). OPERATIONAL CHECK GOOD IAW CRJ 200 MM 27-62-01.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 11,143 hrs · 10,016 cycles

SPOILERONS FAULT STATUS MSG. REPLACED NR 2 SECU PER MM 27-61-05. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 11,030 hrs · 9,915 cycles

FLIGHT SPOILERONS STATUS MSG. REPLACED SECU NR 1 IAW AMM 27-61-05, OPERATIONAL CHECK GOOD.

Part: WINDOW — FAILED (COCKPIT) · airframe 10,566 hrs · 9,497 cycles

RIGHT DV WINDOW SHATTERED INFLIGHT. REPLACED FO SIDE WINDOW IAW CRJ MM 56-12-01. OPERATIONAL CHECK GOOD, PN/OFF NP139322-6, SN/OFF 011-45H8597.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 9,649 hrs · 8,682 cycles

EMERGENCY LIGHT STRIP ON THE FLOOR FROM EMERGENCY EXIT ROW 8 AND BEHIND DOES NOT ILLUMINATE. RESECURED CONNECTOR AT AFT END OF CABIN TRACK. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 9,609 hrs · 8,648 cycles

STAB TRIM CH 2 WILL NOT ENGAGE. REMOVED AND REPLACED HSTCA AND MOTOR CONTROL UNIT IAW MM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD, P/N: 7062-3, S/N OFF: 9911.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 9,558 hrs · 8,604 cycles

STATUS MESSAGE STAB CH2 INOP. REPLACED HSTCU IAW CRJ 200 MM 27-41-01 AND 27-41-00. OPERATIONAL CHECK GOOD.

Part: SWITCH — MALFUNCTIONED (TRIM) · airframe 8,831 hrs · 8,000 cycles

STAB TRIM CH 2 MSG. REPLACED CAPTIANS TRIM SWITCH IAW 27-42-00, OPERATIONAL CHECK GOOD.

Part: PIVOT ASSY — WORN (RUDDER PEDALS) · airframe 8,339 hrs · 7,611 cycles

KLUNKING NOISE AND FEEL IN CAPTAINS RUDDER PEDALS. INSTALLED NEW FRONT PIVOT ASSY ON CAPT'S SIDE RUDDER PEDALS IAW AMM 27-21-05, OPERATIONAL CHECK GOOD.

Part: FRAME — CRACKED (FUSLEAGE) · airframe 7,709 hrs · 7,059 cycles

FRAME 621 RIGHT SIDE CARGO BAY IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED -2, -4, -6 REPAIR PARTS IAW REO 601R-53-5542.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 7,709 hrs · 7,059 cycles

ATTACH BRACKETS CRACKED AT FS 280 INBOARD AND OUTBOARD OF LBL 9. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED (2) EACH 601R31113-57 ANGLES PER ENG DWG 601R31113 AND SRM 51-42-06 PAGES 5, 6, AND 7.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,709 hrs · 7,059 cycles

FS 484 RIGHT SIDE, OUTBOARD INTERCOSTAL, INBOARD ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE PER REO 601R-53-0029.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 7,709 hrs · 7,059 cycles

FS 589 LEFT ATTACH CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE PER ENG DWG 601R35011 REV R.

Part: ATTACH BRACKET — CRACKED (FUSLEAGE) · airframe 7,709 hrs · 7,059 cycles

ATTACH BRACKETS CRACKED AT FS 280 INBOARD AND OUTBOARD OF RBL 9. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED (2 EA) ATTACH BRACKETS AT FS 280 INBOARD AND OUTBOARD OF RBL 9 IAW CRJ 200 SRM 51-42-21 FIG 11 AND 51-42-06 FIG 8.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 7,485 hrs · 6,858 cycles

STAB TRIM CH2 AND MACH TRIM WILL NOT ENGAGE. REPLACED HSTCU, OPERATIONAL CHECK GOOD IAW 27-41-01.

Part: PCU — OUT OF RIG (SPOILERS) · airframe 7,437 hrs · 6,822 cycles

FLT SPOILER FAULT STATUS MESSAGE APPEARS AFTER LANDING. RIGGED LEFT SPOILERONS INBOARD/OUTBOARD PCUS IAW MM 27-62-01. RIGGED LEFT AND RIGHT FLIGHT SPOILER OUTBOARD PCU IAW CRJ MM 27-62-01. REPLACED NR 1 AND NR 2 SECUS IAW CRJ MM 27-61-05. OPERATIONAL CHECK GOOD IAW CRJ 200 FIM 27-63-00. P/N 49-164-20, S/N OFF 03259, 03020, P/N OFF 49-164-05, S/N OFF 102.

Part: PCU — MALFUNCTIONED (FLIGHT SPOILER) · airframe 7,353 hrs · 6,755 cycles

ON TAXI STATUS MESSAGE FLT SPOILERS FAULT. REMOVED AND REPLACED RIGHT HAND INBOARD FLIGHT SPOILERS PCU IAW 27-62-01 CRJ MM, OPERATIONAL CHECK GOOD. P/N 27000-7, S/N OFF 5625.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 7,083 hrs · 6,525 cycles

(FLT. SPOILERS FAULT AND SPOILERONS FAULT) STATUS MESSAGES APPEARED ON TAXI-OUT. REMOVED AND REPLACED NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK OK.

Part: CONCENTRATOR — MISINSTALLED (DCU) · airframe 7,353 hrs · 6,755 cycles

INADVERTENTLY A TECHNICIAN INSTALLED A CRJ700 DCU IN A CRJ200 AND DAMAGED THE DCU. INSPECTED DCU2 RACK CONNECTION AND WIRING AS REQUIRED. NO DEFECTS NOTED. INTERNAL CORRECTIVE ACTION, EA IMPLEMENTED TO INSTALL POLORIZING KEYS IN ALL CRJ200 AIRCRAFT DCU MOUNTING RACKS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,928 hrs · 6,367 cycles

AFT CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT BULB FOR AFT CEILING EMERGENCY LIGHT CRJ AMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 6,092 hrs · 5,607 cycles

ON PUSHBACK FLIGHT SPOILER FAULT. REMOVED AND REPLACED RIGHT INBOARD SPOILERON PCU IAW CRJ MM 27-62-01 AND RIGHT SECU IAW MM 27-61-05. OPS AND LEAK CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (FLIGHT CONTROL) · airframe 5,822 hrs · 5,336 cycles

AFTER POWER UP DURING ORIGINATING CHECKS, THE YD2 INOP. MESSAGE AND FD2 FAIL MESSAGE ILLUMINATED AND COULD NOT BE REMOVED. REMOVED AND REPLACED NR 2 FCC CARD IAW AMM CHAPTER 22-12-14. OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 4,006 hrs · 3,697 cycles

AFTER TAKEOFF AND CLIMBING THROUGH 500 FT AGL, THE STAB CH1 INOP MESSAGE ILLUMINATED. RAN QRH PROCEDURE. MESSAGE PERSISTED. INSTALLED SERVICEABLE HORIZONTAL STABILIZER ACTUATOR IAW MM 27-42-01 AND RII 27-415. OPS CHECK GOOD. NO DEFECTS NOTED. ALSO INSTALLED SERVICEABLE MOTOR CONTROL UNIT IAW MM 27-42-05. OPS CHECK GOOD. NO DEFECTS NOTED. ALL PANELS CHECKED AND SECURED. MCU P/N: 706-3, S/N OFF: 218.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 4,195 hrs · 3,876 cycles

ANGLES CRACKED AT FS 280, RBL 9, INBOARD AND OUTBOARD. FOUND DURING C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-42-06 AND 51-42-21.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,195 hrs · 3,876 cycles

FS 484 LEFT AND RIGHT INTERCOSTALS OUTBOARD FLG LBL 36 CRACKED. FOUND DURING C-CHECK INSPECTION. INTERCOSTALS REPAIRED IAW CRJ REO 601R53-41-059. HFEC C/O IAW 51-20-06/REO 601R-53-41-059 ON REPAIRED AREAS AND BRACKET RADIUS. NO CRACKS NOTED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,201 hrs · 3,884 cycles

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

Part: FLEX DRIVE — BENT (TE FLAP) · airframe 4,195 hrs · 3,876 cycles

LEFT OUTBOARD FLAP FLEX DRIVE (NR 5) IS BENT AT ENDS. FOUND DURING C-CHECK INSPECTION. LEFT OUTBOARD FLEX DRIVE NR 5 HAS BEEN REPLACED IAW AMM 27-53-10.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 4,201 hrs · 3,884 cycles

FS 625.3 RIGHT ANGLE CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED FS 625.3 ANGLE IAW CRJ SRM 51-40-11 AND 51-42-06.

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM) · airframe 3,379 hrs · 3,100 cycles

STAB TRIM CHANNEL 1 INOP MESSAGE. REMOVED AND REPLACED HSTA AND MOTOR CONTROL UNIT IAW RII 27-415. OPS CHECK GOOD AT THIS TIME. HSTA PN OFF: 8396-3 SN OFF: 728.

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM) · airframe 2,456 hrs · 2,330 cycles

HYD PUMP 2B MESSAGE ILLUMINATED ON APPROACH. HYDRAULIC SYNOPTIC PAGE SHOWED 0 PERCENT FLUID, TEMP 40 DEGREES WITH HYD PSI OF 3000. REPLACED NR 2 HYD SYSTEM TUBE ASSY, CASE DRAIN AND TUBE ASSY, PUMP PRESS LINE. SERVICED NR 2 HYD SYSTEM. NO LEAKS NOTED. OPS CHECK GOOD.

Part: CONTROL PANEL — INOPERATIVE (COCKPIT) · airframe 2,119 hrs · 2,053 cycles

RUDDER TRIM ROTARY SWITCH INOP. UNABLE TO ACTIVATE TRIM NOSE RIGHT WHEN ROTATING SWITCH TO FULLY RIGHT. REPLACED RUDDER TRIM CONTROL PANEL WITH SERVICEABLE PANEL. OPS CHECK GOOD.

Part: IDG — MALFUNCTIONED (NR 1 ENGINE) · airframe 1,670 hrs · 1,633 cycles

ON TAKEOFF OUT OF 2500 FT, THE NR 1 GENERATOR WENT OFFLINE. FOLLOWED QRH, ATTEMPTED TO RESET IT AND THE ADG DEPLOYED. RETURNED TO LAX. REMOVED AND REPLACED NR 1 IDG, GCU AND SERVICED NR 2 IDG WITH OIL. GROUND RAN. OPS CHECKS GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 699 hrs · 690 cycles

AT FL350 CO-PILOT'S WINDOW CRACKED. REMOVED AND REPLACED RT SIDE WINDOW.