N498CA

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 37,013 hrs · 35,101 cycles

LEFT INBOARD FLAP LOWER SKIN HAS 3 DENTS INBOARD OF THE INBOARD HINGE ARM. (C-CHECK) RO 2/1/2021 REMOVED DAMAGED SKIN PANEL 601R-14028-45 AND INSTALLED NEW SERVICEABLE SKIN SECTION 601R-14028-45 IAW CRJ-200 SRM 51-42-13. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. AND COMPLIED WITH SKYWEST CARD 51-900-1003-SKY. 337 ATTACHED. PART FOR PART REPLACEMENT, NO WEIGHT CHANGE. REFERENCED DRAWING 601R14008 FOR FASTENER CALL OUT

Part: ANGLE — CRACKED (ZONE 200) · airframe 37,013 hrs · 35,101 cycles

ANGLE CRACKED AND SUPPORT CLIP CORRODED AT FS280 AND STGR2L (C-CHECK) RO 2/1/2021 REMOVED CLIP, REMOVED DOUBLER, REMOVED BRAACKET IAW CRJ SRM 51-42-06. REMOVED CORROSION IAW CRJ 200 SRM 51-21-06. NO CRACKS FOUND. INSTALLED DOUBLER, BRACKET AND CLIP IAW CRJ 200 SRM 51-42-06, 51-42-10

Part: ANGLE — CRACKED (FUSELAGE) · airframe 37,013 hrs · 35,101 cycles

ANGLE CRACKED AT STR 16L BETWEEN FS 621 AND FS 625 (C-CHECK) RO 2/1/2021 REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE IAW CRJ200 SRM 51-42-21, 51-40-11

Part: BOLT — CORRODED (LT WING) · airframe 37,013 hrs · 35,101 cycles

WHILE PERFORMING INSPECTION ON 57-590-600 AND 57-690-6000 FOUND THAT L/H AND R/H HINGE BOX BOLTS ON W.S. 178, 220, 264 WERE ALL CORRODED AND NEED TO BE REPLACED. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED HARDWARE ON L/H AND R/H W.S 178-.00, 220.00, AND 264.00 IAW CRJ 200 AMM 57-21-34-000-801/802/803 AND 57-21-35-400-801/802/803

Part: SKIN — CHAFED (RT WING) · airframe 37,013 hrs · 35,101 cycles

R/H CENTER WING, LOWER SKIN IS CHAFED AT B.L. 45.00 AT REAR SPAR. (C-CHECK) RO 2/1/2021 REPAIRED RH CENTER WING LOWER SKIN AT BL 45 AT REAR SPAR IAW BOMBARDIER REO 601R-57-21-880 REV D DATED 2017/03/06 ZONE A REFERENCE SKYCARD 51-900-1003-SKY (CL-600-2B19) WEIGHT AND BALANCE NOT EFFECTED SEE ATTACHED M-337

Part: SKIN — CHAFED (LT WING) · airframe 37,013 hrs · 35,101 cycles

L/H CENTER WING, LOWER SKIN IS CHAFED AT B.L. 45.00 AT AFT SPAR. (C-CHECK) RO 2/1/2021 REPAIRED LH CENTER WING LOWER SKIN AT BL 45 AT REAR SPAR IAW BOMBARDIER REO 601R-57-21-880 REV D DATED 2017/03/06 ZONE A REFERENCE SKYCARD 51-900-1003-SKY (CL-600-2B19) WEIGHT AND BALANCE NOT EFFECTED SEE ATTACHED M-337

Part: WEB — CORRODED (PAX DOOR) · airframe 37,013 hrs · 35,101 cycles

PAX DOOR AFT WEB IS CORRODED. (C-CHECK) RO 2/1/2021 REPLACED PAX DOOR AFT WEB P/N 601R317071-11 IAW CRJ 200 SRM 51-40-11 , 51-42-06 REV 38 7-1019

Part: HINGE — GOUGED (PAX DOOR) · airframe 37,013 hrs · 35,101 cycles

PAX DOOR HINGE ON THE FUSELAGE SIDE IS GOUGED ON THE 11TH, 12TH, 13TH, 14TH, 15, 16TH, 17TH, 18TH, 23RD, 24TH, 25TH AND 27TH LUG VALLEYS FROM FWD SIDE OF THE HINGE. (C-CHECK) RO 2/1/2021 REPAIRED PAX DOOR HINGE FUSELAGE SIDE IAW BOMBARDIER REO 601R-53-21-814 REV C DATED 2017-08-02 AND MHI RJ REO 601R-53-21-3377 REV-- DATED 2020-12-24. REFER TO CONTINUATION CARD FOR ALL WORK PERFORMED. COMPLIED WITH SKYCARD 51-900-1003-SKY AND FORM M-337. NO WEIGHT AND BALANCE AFFECTED.

Part: SKIN — CRACKED (LT WING) · airframe 37,013 hrs · 35,101 cycles

L/H WING STATION 200 HAS 2 CRACKS IN THE TRAILING EDGE OF THE PANEL WHERE THE SKIN IS COVERED BY THE I/B FLIGHT SPOILER (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED L/H WING TRAILING EDGE IAW CRJ 200 SRM 51-42-06 & 51-42-21

Part: FRAME — DAMAGED (ZONE 100) · airframe 37,013 hrs · 35,101 cycles

FOUND DAMAGED AREA AT FS 605 BETWEEN STRINGERS 20R AND 21R. (C-CHECK) RO 2/1/2021 COMPLIED WITH REPAIR DAMAGED AREA AT FS 605 BETWEEN STRINGERS 20R AND 21R IAW MHIRJ REO 601R-53-61-7515 REV -- DATED 2021-01-04 BY CUTTING AWAY DAMAGE, REMOVEING BURRS,VISUAL INSPECT,PERFORMING EDDY CURRENT, FABBING REPAIR PARTS,WET INSTALLING PARTS , EDGE SEALING, AND PAINT, AND SKYWEST CARD 51-900-1003-SKY, 337 ATTACHED / WEIGHT REMOVED 0.050 WEIGHT INSTALLED 0.450 TOTAL WEIGHT INSTALLED 0.400

Part: FRAME — CORRODED (PAX DOOR) · airframe 37,013 hrs · 35,101 cycles

PAX DOOR FORMER AT FS347.27 CORRODED BEYOND LIMITS. (C-CHECK) RO 2/1/2021 REMOVED DAMAGED FORMER AND INSTALLED NEW SERVICEABLE FORMER IAW CRJ 200 SRM 51-42-06, 51-40-11 AND 51-42-21 AND SKYWEST CARD 51-900-1003-SKY, 337 ATTACHED, AND NO WEIGHT CHANGE. REFERENCED DRAWING 601R31702 FOR FASTENER CALL OUT

Part: BEARING — CORRODED (PAX DOOR) · airframe 37,013 hrs · 35,101 cycles

PAX DOOR TORQUE TUBE SHAFT BEARINGS(QTY 2) RUSTED AND HAVE SIDE TO SIDE PLAY BEYOND ALLOWABLE LIMITS. REPLACE P/N'S 600-31320-73. (C-CHECK) RO 2/1/2021 LOCATED AND DRILLED 2EA NEW BEARING ASSYS P/N 600-31320-73 IAW CRJ200 SRM 51-40-11 REV38 DATED JUL 10/19. BEARING ASSYS TO BE INSTALLED ON MX TRANS 21986007 ITEM 20.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,013 hrs · 35,101 cycles

PAX DOOR INTERCOSTAL DD4 CORRODED BEYOND LIMITS. P/N 601R318081-1 (C-CHECK) RO 2/1/2021 REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW SERVICEABLE INTERCOSTAL IAW CRJ-200 SRM 51-40-11 AND 51-42-06. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. AND COMPLIED WITH SKYWEST CARD 51-900-1003-SKY. M-337 ATTACHED. / PART FOR PART REPLACEMENT, NO WEIGHT CHANGE. REFERENCED DRAWING 601R31702 FOR FASTENER CALL OUT

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,013 hrs · 35,101 cycles

PAX DOOR INTERCOSTAL DD3 CORRODED BEYOND LIMITS. P/N 601R318056-1 (C-CHECK) RO 2/1/2021 REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW SERVICEABLE INTERCOSTAL IAW CRJ-200 SRM 51-40-11 AND 51-42-06 AND SKYWEST CARD 51-900-1003-SKY, 337 ATTACHED, AND NO WEIGHT CHANGE.REFERENCED DRAWING 601R31702 FOR FASTENER CALL OUT

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,013 hrs · 35,101 cycles

PAX DOOR INTERCOSTALS 3RD AND 4TH FROM HINGE AFT SIDE CORRODED BEYOND LIMITS. P/N'S 601R31902-317 (QTY 2). (C-CHECK) RO 2/1/2021 REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW SERVICEABLE INTERCOSTAL IAW CRJ 200 SRM 51-40-11 AND 51-42-06. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.AND COMPLIED WITH SKYWEST CARD 51-900-1003-SKY. 337 ATTACHED. / PART FOR PART REPLACEMENT, NO WEIGHT CHANGE. REFERENCED DRAWING 601R31902 FOR FASTENER CALL OUT

Part: FRAME — CORRODED (ZONE 800) · airframe 37,013 hrs · 35,101 cycles

PAX DOOR FORMER AT FS311.75 CORRODED BEYOND LIMITS. (C-CHECK) RO 2/1/2021 REMOVED DAMAGED FORMER AND INSTALLED NEW SERVICEABLE FORMER IAW CRJ 200 SRM 51-42-06, 51-40-11 AND 51-42-21 AND SKYWEST CARD 51-900-1003-SKY, 337 ATTACHED, AND NO WEIGHT CHANGE.REFERENCED DRAWING 601R31702 FOR FASTENER CALL OUT

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 37,013 hrs · 35,101 cycles

LEFT FLOOR SILL ASSY LBL45 LFS513 HAS CORROSION (C-CHECK) RO 2/1/2021 REPAIRED AREA IAW REO 601R-53-41-666 REV C DATED 2012-11-06. COMPLIED WITH SKY CARD 51-900-1003-SKY AND FORM M-337. WEIGHT AND BALANCE NOT AFFECTED.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 37,013 hrs · 35,101 cycles

RIGHT FLOOR SILL ASSY RBL45 RFS505 HAS CORROSION (C-CHECK) RO 2/1/2021 COMPLIED WITH BMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06 DISPOSITION 1.2 AND SKYCARD 51-900-1003-SKY (CL600-2B19). CAL TOOLING USED WVACT3099 CAL DATE 06/15/2020 CAL DUE 06/30/21 ORIG MAT .055" MAT LOSS .002" MAT REMOAINING .053". 337 COMPLETED

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 37,013 hrs · 35,101 cycles

RIGHT FLOOR SILL ASSY RBL45 RFS499 HAS CORROSION (C-CHECK) RO 2/1/2021 COMPLIED WITH BMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06 DISPOSITION 1.2 AND SKYCARD 51-900-1003-SKY (CL600-2B19). CAL TOOLING USED WVACT3099 CAL DATE 06/15/2020 CAL DUE 06/30/21 ORIG MAT .055" MAT LOSS .008" MAT REMOAINING .047". 337 COMPLETED

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 37,013 hrs · 35,101 cycles

LEFT FLOOR SILL ASSY LBL45 LFS491 HAS CORROSION (C-CHECK) RO 2/1/2021 REPAIRED AREA IAW REO 601R-53-41-666 RERV C DATED 2012-11-06. COMPLIED WITH SKYCARD 51-900-1003-SKY AND FORM M-337. WEIGHT AND BALANCE NOT AFFECTED.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 37,013 hrs · 35,101 cycles

LEFT FLOOR SILL ASSY LBL45 LFS535 HAS CORROSION (C-CHECK) RO 2/1/2021 COMPLIED WITH BMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06 DISPOSITION 1.2 AND SKYCARD 51-900-1003-SKY (CL600-2B19). CAL TOOLING USED WVACT3099 CAL DATE 06/15/2020 CAL DUE 06/30/21 ORIG MAT .055" MAT LOSS .006" MAT REMOAINING .049". 337 COMPLETED

Part: FRAME — CORRODED (ZONE 100) · airframe 37,013 hrs · 35,101 cycles

F.S. 589 FRAME IS CORRODED IN TWO LOCATIONS. FIRST LOCATION IS BETWEEN STRG 20R TO 21R. SECOND IS AT STRG 23R AT THE TOP AND AFT SIDE. (C-CHECK) RO 2/1/2021 REMOVED DAMAGED FRAME AND INSTALLED NEW SERVICEABLE FRAME IAW CRJ-200 SRM 51-42-06, 51-42-21 AND 51-40-11. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.ALL WORK PERFORMED, AND COMPLIED WITH SKYWEST CARD 51-900-1003-SKY. 337 ATTACHED. PART FOR PART REPLACEMENT, NO WEIGHT CHANGE. REFERENCED DRAWING 601R23025 FOR FASTENER CALL OUT.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 37,013 hrs · 35,101 cycles

LEFT FLOOR SILL ASSY LBL45 LFS499 HAS CORROSION (C-CHECK) RO 2/1/2021 REPAIRED AREA IAW REO 601R-53-41-666 REV C DATED 2012-11-06. COMPLIED WITH SKYCARD 51-900-1003-SKY AND FORM 337. WEIGHT AND BALANCE NOT AFFECTED.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 37,013 hrs · 35,101 cycles

LEFT FLOOR SILL ASSY LBL41 TO LBL45 LFS560 HAS CORROSION (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED LH TENSION STRAP IAW CRJ 200 SRM 51-42-06

Part: FRAME — CORRODED (ZONE 100) · airframe 37,013 hrs · 35,101 cycles

F.S. 605 FRAME IS CORRODED IN TWO LOCATIONS. FIRST LOCATION IS BETWEEN STRG 20R TO 21R. SECOND LOCATION IS BETWEEN 26R TO 27. (C-CHECK) RO 2/1/2021 REMOVED DAMAGED FRAME AT FS605 AND INSTALLED NEW SERVICEABLE FRAME IAW CRJ-200 SRM 51-42-06 AND 51-42-21. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.ALL WORK PERFORMED, AND COMPLIED WITH SKYWEST CARD 51-900-1003-SKY. 337 ATTACHED. PART FOR PART REPLACEMENT, NO WEIGHT CHANGE. REFERENCED DRAWING 601R36026 FOR FASTENER CALL OUT.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 37,013 hrs · 35,101 cycles

LEFT FLOOR SILL ASSY LBL45 LFS529 HAS CORROSION (C-CHECK) RO 2/1/2021 REPAIRED AREA IAW REO 601R-53-41-666 REV C DATED 2012-11-06. COMPLIED WITH SKYCARD 51-900-1003-SKY AND FORM M -337. WEIGHT AND BALANCE NOT AFFECTED.

Part: FRAME — CORRODED (ZONE 100) · airframe 37,013 hrs · 35,101 cycles

FRAME AT FS333 CORRODED BETWEEN STGR21L AND STGR23L. (C-CHECK) RO 2/1/2021 REMOVED DAMAGED FRAME AND INSTALLED NEW SERVICEABLE FRAME AT FS 333 IAW CRJ-200 SRM 51-42-06, 51-40-11 AND 51-42-21 AND COMPLIED WITH SKYWEST CARD 51-900-1003-SKY. 337 ATTACHED.PART FOR PART REPLACEMENT, NO WEIGHT CHANGE. REFERENCED DRAWING 601R32004 FOR FASTENER CALL OUT.

Part: FRAME — CORRODED (ZONE 100) · airframe 37,013 hrs · 35,101 cycles

FRAME AT FS310 CORRODED BETWEEN STGR26L AND STGR26R. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED FRAME SECTOR IAW CRJ 200 SRM 51-42-06 & 51-42-21. REFER TO CONTINUATION CARD FOR ALL WORK PERFORMED, AND COMPLIED WITH SKYWEST CARD 51-900-1003-SKY. 337 ATTACHED. / PART FOR PART REPLACEMENT, NO WEIGHT CHANGE. REFERENCED DRAWING 601R32002 FOR FASTENER CALL OUT.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 37,013 hrs · 35,101 cycles

INTERCOSTAL AT STRG20L CORRODED BETWEEN FS333 AND FS349. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED INTERCOSTALAT STR21L BETWEEN FS333 AND FS349 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. REFER TO CONTINUATION CARD FOR ALL MAINTAINENCE PERFORMED. AND COMPLIED WITH SKYWEST CARD 51-900-1003-SKY. 337 ATTACHED. PART FOR PART REPLACEMENT, NO WEIGHT CHANGE. REFERENCED DRAWING 601R31527 FOR FASTENER CALL OUT

Part: FRAME — CORRODED (ZONE 100) · airframe 37,013 hrs · 35,101 cycles

FRAME AT FS310 CORRODED BETWEEN STGR20R AND STGR21R. (C-CHECK) RO 2/1/2021 REMOVED DAMAGED FRAME AND INSTALLED NEW SERVICEABLE FRAME AT FS 310 BETWEEN STGR20R AND STGR21R IAW CRJ-200 SRM 51-42-06, 51-40-11 AND 51-42-21 REV 38 DATED 10 JULY 2019 AND COMPLIED WITH SKYWEST CARD 51-900-1003-SKY. 337 ATTACHED. PART FOR PART REPLACEMENT, . REFERENCED DRAWING 601R32002 FOR FASTENER CALL OUT. NO WEIGHT CHANGE PART FOR PART REPLACEMENT.

Part: SKIN — GOUGED (ZONE 200) · airframe 37,013 hrs · 35,101 cycles

FUSELAGE SKIN IS GOUGED 4 PLACES JUST AFT OF PASSENGER DOOR HINGE BETWEEN STR 17L AND 18L. (C-CHECK) RO 2/1/2021 COMPLIED WITH REPAIR OF FUSELAGE SKIN IS GOUGES 4 PLACES JUST AFT OF PASSENGER DOOR HINGE BETWEEN STR 17L AND 18L. IAW MHIRJ REO 601R-53-21-3380 BY BLENDING,NDT, AND TOUCH UP PAINT.AND SKYWEST CARD 51-900-1003-SKY AND ATTACHED FORM 337. / NO WEIGHT CHANGE

Part: TENSION TIE — CORRODED (PAX DOOR) · airframe 37,013 hrs · 35,101 cycles

PAX DOOR FWD AND AFT TENSION TIE BAR HARDWARE CORRODED. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED CORRODED FWD AND AFT TENSION TIE BAR HARDWARE IAW CRJ200 AMM 52-11-19-400-803 REV62 DATED DEC10/20. INSTALLATION OF TENSION TIES TO BE ACCOMPLISHED ON MX TRANS #21986007 ITEM 13.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,013 hrs · 35,101 cycles

PAX DOOR DD6 INTERCOSTAL CORRODED. (C-CHECK) RO 2/1/2021 REMOVED AND INSTALLED SERVICABLE DD6 INTERCOSTAL IAW CRJ 200 SRM 51-42-06 REV 38 DATED JUL 10/19 AND SKYCARD 51-900-1003-SKY (CL600-2B19). FORM 337 COMPLETED. PART FOR PART REPLACEMENT, NO WEIGHT CHANGE. REFERENCED DRAWING 601R31702 FOR FASTENER CALL OUT.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,013 hrs · 35,101 cycles

PAX DOOR DD3 INTERCOSTAL CORRODED. (C-CHECK) RO 2/1/2021 REMOVED AND INSTALLED SERVICABLE INTERCOSTAL IAW CRJ200 SRM 51-42-06 REEV 38 DATED JUL10/19 AND SKY CARD 51-900-1003-SKY (CL600-2B19). 337 COMPLETED PART FOR PART REPLACEMENT, NO WEIGHT CHANGE. REFERENCED DRAWING 601R31702 FOR FASTENER CALL OUT.

Part: FITTING — CHAFED (PAX DOOR) · airframe 37,013 hrs · 35,101 cycles

PAX DOOR ARRESTER FITTING CHAFED (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED NEW SERVICEABLE PN 601R31722-1 IAW CRJ 200 AMM 20-21-00-910--801

Part: ANGLE — CRACKED (PRESS BULKHEAD) · airframe 37,013 hrs · 35,101 cycles

AFT BULKHEAD, AFT SIDE, RH CLIP CRACKED @ FS 621 STR 14 (C-CHECK) RO 2/1/2021 REMOVED AND LOCATED AND DRILLED, INSTALLED AND PAINTED NEW CLIP IAW CRJ 200 SRM 51-40-11,51-42-21, AND 51-25-21.

Part: BRACKET — CRACKED (PRESS BULKHEAD) · airframe 37,013 hrs · 35,101 cycles

AFT SIDE OF AFT BULKHEAD, LH SIDE @ FS625.30 STR 14, @ THREE INCHES FROM OUTBOARD SKIN, CRACKED BRACKET (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED BRACKET AFT SIDE AFT PRESSURE BULKHEAD LH SIDE @FS625.30 STR14 IAW CRJ200 SRM 51-42-21 AND 51-40-11

Part: FITTING — CRACKED (RT WINDSHIELD) · airframe 37,013 hrs · 35,101 cycles

RH WINDSHIELD SIDE POST LOWER O/B ANGLE IS CRACKED. (C-CHECK) RO 2/1/2021 REMOVED OLD UNSERVICEABLE RH WINDSHIELD SIDE POST LOWER O/B ANGLE. DRILLED, LOCATED, AND INSTALLED NEW SERVICEABLE RH WINDSHIELD SIDE POST LOWER O/B ANGLE, P/N 601R33235-4S IAW CRJ 200 SRM 51-42-21, 51-40-11, 51-23-00 AND 51-21-16.

Part: NUT — CORRODED (LT WING SPOILER) · airframe 37,013 hrs · 35,101 cycles

L/H WING FLIGHT SPOILER BOTH I/B HINGE ATTACH PIONT HARDWARE NUTS ARE CORRORDED. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED CORRODED L/H WING FLIGHT SPOILER BOTH I/B HINGE ATTACH PIONT HARDWARE NUTS IAW CRJ 200 AMM 27-64-01-946-004,

Part: ROD END — CORRODED (LT WING SPOILER) · airframe 37,013 hrs · 35,101 cycles

L/H WING I/B GROUND SPOILER ACTUATOR ROD END ATTACHMENT HARDWARE CORRODED (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED LH WING IB GROUND SPOILER ACTUATOR ROD END ATTACHMENT HARDWARE IAW CRJ 200 AMM 27-63-01-000/400-801

Part: NUT — CORRODED (RT WING SPOILER) · airframe 37,013 hrs · 35,101 cycles

R/H WING O/B GROUND SPOILER ACTUATOR ATTACHMNET NUT HARDWARE (QTY 2) IS CORRODED. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED CORRODED HARDWARE IAW CRJ 200 AMM 27-63-01-400-801 STEP 2 B. 1(D,E,F)

Part: ANGLE — CORRODED (LT WING SPOILER) · airframe 37,013 hrs · 35,101 cycles

L/H WING SPOILERON I/B HINGE BOLT STOP ANGLE HARDWARE CORRORDED. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED CORRODED L/H WING SPOILERON I/B HINGE BOLT STOP ANGLE HARDWARE IAW CRJ 200 AMM 27-64-01-420-001.

Part: PCU — CORRODED (LT WING SPOILER) · airframe 37,013 hrs · 35,101 cycles

L/H WING FLIGHT SPOILER PCU'S ( I/B AND O/B ) MOUNTNG ATTACHMENT HARDWARE NUTS ARE CORRODED. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED L/H WING FLIGHT SPOILER PCU'S ( I/B AND O/B ) MOUNTNG ATTACHMENT HARDWARE NUTS IAW CRJ 200 AMM 27-62-01-910-004.

Part: WASHER — CORRODED (RT WING SPOILER) · airframe 37,013 hrs · 35,101 cycles

R/H WING FLIGHT SPOILER O/B ACTUATOR ATTACHMNET THROUGH BOLT HARWARE CORRORDED. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED CORRODED R/H WING FLIGHT SPOILER O/B ACTUATOR ATTACHMNET THROUGH BOLT HARWARE IAW CRJ 200 AMM 27-62-01-943-003.

Part: NUT — CORRODED (LT WING SPOILER) · airframe 37,013 hrs · 35,101 cycles

L/H WING SPOILERON I/B HINGE NUT HARDWARE CORRODED. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED L/H WING SPOILERON I/B HINGE NUT HARDWARE IAW CRJ 200 AMM 27-64-01-869-001

Part: ANGLE — CORRODED (LT WING SPOILER) · airframe 37,013 hrs · 35,101 cycles

L/H WING FLIGHT SPOILER I/B HINGE BOLT STOP ANGLE HAS CORRODED HARDWARE BOLTS. ( QTY 2 ) (C-CHECK) RO 2/1/2021 REMOVED AND REPLACE CORRODED HARDWARE ON L/H WING FLIGHT SPOLIER BOLT STOP ANGLE IAW CRJ 200 AMM 27-64-01-869-001.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 37,013 hrs · 35,101 cycles

RH IB FLAP VANE LEADING EDGE IS CHAFED AT ALL 3 CONTACT POINTS (C-CHECK) RO 2/1/2021 REMOVED CHAFED DAMAGED R/H FLAP VANE LEADING EDGE SKINS. LOCATED, DRILLED, INSTALLED,ALODINED,PRIMED, AND TOPCOATED 3 NEW SERVICEABLE R/H I/B FLAP VANE LEADING EDGE SKINS IAW CRJ-200 51-40-11, 51-21-11, 51-25-01,51-25-06, 51-42-10, 51-23-00, AND 51-42-13.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 37,013 hrs · 35,101 cycles

LH IB FLAP VANE LEADING EDGE IS CHAFED AT ALL 3 CONTACT POINTS (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED LH IB FLAP VANE LEADING EDGE AT 3 CHAFED CONTACT POINTS IAW CRJ 200 SRM 51-42-10. REFER TO CONTINUATION CARD FOR DETAILED WORK PERFORMED.

Part: BUSHING — DAMAGED (RT AILERON) · airframe 37,013 hrs · 35,101 cycles

REMOVE AND REPLACE BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK) RO 2/1/2021 REMOVED R/H AILERON AFT SPAR BUSHING AND HARDWARE ANDD INSTALLED NEW SERVICEABLE BUSHINGS AND HARDWARE AT AFT SPAR IAW CRJ-200 AMM 20-26-00-910-802 , 27-15-01-400-801 AND REO 601R-57-51-015 REV NC 8/9/95. SEE SKY CARD 51-900-1003-SKY AND ATTACHED M-337. WEIGHT AND BALANCE NOT EFFECTED. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 34,592 hrs · 32,266 cycles

DENT FOUND AT APPROX. FS 700 ABOVE STGR 15L. (C-CHECK) RO: 03/02/2019 REPAIRED DENTS AT APPROX FS700 IAW REO.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 34,592 hrs · 32,266 cycles

CORROSION ON DOUBLER AT RT FS 349 ABOVE SERVICE DOOR LOWER SILL. (C-CHECK) RO: 03/02/2019 REPAIRED THE DOUBLER AT RT FS 349 ABOVE SERVICE DOOR LOWER SILL IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,592 hrs · 32,266 cycles

CORROSION ON IN BOARD LBL9 FLOORBEAM FLANGE FS570.00 €“ FS609.00. (C-CHECK) RO: 03/02/2019 REMOVED AND INSTALLED NEW FLOORBEAM CAP AT LBL 9 BETWEEN F.S 570 AND F.S 615 IAW REO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,592 hrs · 32,266 cycles

CORROSION ON FLANGE OF FRAME, FS605.00, STGR21L €“ STGR23L. (C-CHECK) RO: 03/02/2019 BLENDED/REMOVED CORROSION FROM FS605 FRAME LOWER FLANGES LOCATED BETWEEN STGR-21L & STGR-23L IAW REO. PRESSURE CHECK GOOD.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 34,592 hrs · 32,266 cycles

TWO DENTS APROX RBL6 BETWEEN STR 26 AND 27 BETWEEN FS 250 AND 265. (C-CHECK) RO: 03/02/2019 REPAIRED THE TWO DENTS APROX RBL6 BETWEEN STR 26 AND 27 BETWEEN FS 250 AND FS 265 REF REO. PRESSURE CHECKS GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,592 hrs · 32,266 cycles

THREE DENTS APPROX RBL 6 BETWEEN STRG 26 AND 27 APPROX FS 276. (C-CHECK) RO: 03/02/2019 DRESSED DISCREPANT SKIN TO ORIGINAL CONTOUR IN 3 SPOTS AND REPAIRED AREA IAW REO. PRESSURE CHECK GOOD.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 34,592 hrs · 32,266 cycles

TWO DENTS APROX LBL 8 OUTBD STR 26 APROX FS 273. (C-CHECK) RO: 03/02/2019 PERFORMED DENT REPAIR AT APPROX. FS 273 STR 26 LBL 8 IAW REO. PRESSURE CHECK GOOD.

Part: VANE — CHAFED (TE FLAP) · airframe 34,592 hrs · 32,266 cycles

RT INBOARD FLP VANE LEADING EDGE HAS CHAFING AT THE INBOARD, CENTER, AND OUTBOARD SECTIONS OF FLAP VANE. (C-CHECK) RO: 03/02/2019 REMOVED DAMAGED O/B AND I/B RT FLAP VANE LEADING EDGE CAP AND REPLACED WITH NEW CAP IAW SRM.

Part: STOP FITTING — CHAFED (FUSELAGE) · airframe 34,592 hrs · 32,266 cycles

AVIONICS BAY DOOR LT & RT STOP FITTINGS ON FUSELAGE CHAFED. (C-CHECK) RO: 03/02/2019 REMOVED AND INSTALLED NEW FWD, LT AND RT AVIONICS DOOR STOP FITTINGS AND ALL HARDWARE IAW SRM. OPERATIONAL CHECK OF THE AVIONICS DOOR GOOD IAW AMM.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 34,411 hrs · 32,061 cycles

GEAR DISAGREE ON ARRIVAL. BOTH MAIN LANDING GEAR WOULD NOT COME DOWN. PULLED THE MANUAL RELEASE HANDLE AND GEAR CAME DOWN VIA THE QRH. (FLT#7392) CLOSED REMOVED AND REPLACED THE MAIN LANDING GEAR SELECTOR VALVE IAW AMM.PERFORMED MULTIPLE SUCCESSFUL GEAR SWINGS, OPS AND LEAK CHECK GOOD.

Part: FRAME — CORRODED (BS 319) · airframe 30,997 hrs · 28,317 cycles

AVIONICS BAY BELOW FLOORBOARD AT BS 319 FRAME HAS CORROSION AT STRINGER 27. COMPLIED WITH REO, ALL STEPS COMPLETED OF PERMANENT REPAIR.

Part: SKIN — CORRODED (BS 559) · airframe 30,997 hrs · 28,317 cycles

RIGHT FUSELAGE SKIN HAS CORRODED AND GOUGED BETWEEN STRINGERS 22 AND 24R, BS 559 +96. COMPLIED WITH REO ALL STEPS COMPLETED OF PERMANENT REPAIR.

Part: SKIN — CORRODED (BS 559) · airframe 30,997 hrs · 28,317 cycles

FUSELAGE SKIN HAS CORROSION AT BS 559 TO 559 +112 STRINGER 26L TO 26R. COMPLIED WITH REO, ALL STEPS COMPLETED OF PERMANENT REPAIR.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 30,997 hrs · 28,317 cycles

LEFT INBOARD FLAP VANE CENTER SECTION HAS A DEEP CHAFE AREA. REMOVED AND REPLACED THE FLAP VANE, IAW SRM.

Part: ENGINE — FLAMED OUT (NR 2) · airframe 29,147 hrs · 26,533 cycles

NR 2 ENGINE FLAMED OUT AFTER TAKEOFF. ATTEMPTED TO RELIGHT ENGINE, UNSUCCESSFUL. CREW DECLARED AN EMERGENCY AND DIVERTED. CABIN WAS BRACED AND THE ACFT LANDED SAFELY. TAXIED TO THE GATE UNDER ITS OWN POWER. R & R RT ENGINE ASSY. OPS CHECKS AND LEAK CHECKS GOOD.

Part: SENSOR — MALFUNCTIONED (NLG DOOR) · airframe 28,990 hrs · 26,398 cycles

NOSE DOOR OPEN, NOSE GEAR DISAGREE MESSAGES RETURNED TO THE FIELD. ADJUSTED NOSE LANDING GEAR CENTERING SENSOR. OPS CHECKED GOOD.

Part: SKIN — CRACKED (LEFT SIDE) · airframe 27,095 hrs · 24,688 cycles

LEFT SIDE SKIN AT A FWD EQUIPT COMPARTMENT AFT LATCH LOCATION HAS SUSPECT CRACK. CREMOVED AND INSTALLED NEW TRU SKIN REF SRM AND STS EA COMPLIED WITH ST 51-900-1003.

Part: SHROUD — CHAFED (RT AILERON) · airframe 27,095 hrs · 24,688 cycles

RIGHT UPPER AILERON SHROUD HAS CHAFE WEAR AT APPROXIMATE LOCATION JUST OTBD OF WS 321.32. R & R RT AILERON SHROUD IAW SRM.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 27,095 hrs · 24,688 cycles

FS 484, RBL 36 UPPER ANGLE HAS CRACK AT RIVET LOCATION. C-CHECK, RO 2/8/15, PERFORMED CUTOUT OF INTERCOSTAL AT FS 484, RBL 36 AND INSTALLED -2 REPAIR ANGLE AT FS 484.0, RBL 36 IAW REO. PRESSURE LEAK CHECK GOOD REF AMM.

Part: BULKHEAD — CRACKED (BS 202) · airframe 27,095 hrs · 24,688 cycles

EMERGENCY BRAKE PASS THRU AT FS 202 CRACKED. REPAIRED FS 202 BULKHEAD WHERE EMERGENCY BRAKE, PARKING BRAKE CABLE, PASSES THROUGH THE BULKHEAD REF REO. COMPLIED WITH ST AND ALL STEPS OF REO. PRESSURE LEAK CHECK GOOD.

Part: FLOOR PANEL — CRACKED (BS 461) · airframe 27,095 hrs · 24,688 cycles

PRESSURE FLOOR AT FRAME STA 461, BL0, RBL 9 CRACKED. REPAIRED PRESSURE FLOOR AT FS 461, BL 0 - RBL 9 IAW REO. REPAIRED BY CUTTING OUT CRACKS AND INSTALLING REPAIR DOUBLERS. COMPLIED WITH ST 51-900-1003. PRESSURE LEAK CHECK OF REPAIR IS GOOD REF AMM.

Part: FLOOR PANEL — CRACKED (BS 461) · airframe 27,095 hrs · 24,688 cycles

PRESSURE FLOOR AT FRAME STA 461 BL0-LBL9 CRACKED. REPAIRED PRESSURE FLOOR AT FS 461 BL 0 - LBL 9 IAW REO. REPAIRED BY CUTTING OUT CRACKS AND INSTALLING REPAIR DOUBLERS. COMPLIED WITH ST 51-900-1003. PRESSURE LEAK CHECK OF REPAIR IS GOOD REF AMM.

Part: PROXIMITY SENSOR — FAILED (WOW) · airframe 26,115 hrs · 23,883 cycles

WOW INPUT DURING GEAR RETRACTION. R & R WOW PROXIMITY SENSOR RT INBD MLG AND UPPER SECTION HARNESS IAW AMM,

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,370 hrs · 23,292 cycles

EXTERNAL EMERGENCY LIGHT IS BURNED OUT. REPLACED THE LAMP.

Part: PROXIMITY SENSOR — FAILED (PAX DOOR) · airframe 25,322 hrs · 23,254 cycles

SERVICE DOOR CAUTION MESSAGE DURING APPROACH AND SMOKE IN THE COCKPIT FROM THE FLOOR UP. REPLACED SERVICED DOOR OUTER HANDLE PROXIMITY SENSOR.

Part: INVERTER — FAILED (CABIN) · airframe 24,284 hrs · 22,474 cycles

LT OVERWING EMERGENCY EXIT LOWER LIGHT DOES NOT ILLUMINATE. FLT 6209 REPLACED EMERGENCY LIGHT INVERTER FOR LT SIDEWALL EMERGENCY LIGHT. OPERATIONS CHECKED GOOD.

Part: SPLICE — BROKEN (CABIN) · airframe 24,259 hrs · 22,456 cycles

FLOOR LEVEL EMERGENCY EXIT AT MAIN CABIN DOOR DOES NOT ILLUMINATE. FLT 3486 REPLACED DEFECTIVE SPLICE IAW AMM. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,909 hrs · 22,178 cycles

NR 1 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#5505 RELAMPED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,870 hrs · 22,149 cycles

RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT IS BURNED OUT. FLT#5517 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,870 hrs · 22,149 cycles

NR 2 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#5327 RELAMPED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,870 hrs · 22,149 cycles

LT FWD OVERWING EXTERIOR EMERGENCY LIGHT IS BURNED OUT. SERVICE RELAMPED.

Part: CONNECTOR — LOOSE (CABIN) · airframe 23,870 hrs · 22,149 cycles

EXIT ROW 8, LT SIDE, EMERGENCY LIGHT FLOOR LEVEL DOES NOT ILLUMINATE. FLT#5361 SECURED LOOSE CONNECTOR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,955 hrs · 21,332 cycles

CARGO FLOORBEAM TOP CAP AT LBL 27 AND FS 621 HAS CORROSION. (C-CHECK) REPLACED WITH NEW CARGO FLOORBEAM AT LBL 27 FOR FS 569 TO FS 621 IAW REO.

Part: DOOR — CHAFED (LT MLG) · airframe 22,955 hrs · 21,332 cycles

LEFT MAIN LANDING GEAR DOOR HAS CHAFE ON FORWARD CORNER NEAR WHEEL BRUSH. (C-CHECK) REPAIRED LEFT MAIN LANDING GEAR DOOR CHAFE IAW REO.

Part: PLATE — CORRODED (FUSELAGE) · airframe 22,955 hrs · 21,332 cycles

CARGO LANDING PLATE HAS CORROSION ON LOWER SIDE UNDER NUT PLATES. (C-CHECK) REPLACED CARGO LANDING PLATE IAW REO AND SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,955 hrs · 21,332 cycles

FLOORBEAM CLIP AT FS 280.0 RBL 11.0 IS CRACKED. (C-CHECK) REPLACED CLIP AT FS 280.0 RBL 11.0 WITH NEW P/N 601R-53-11-171-5 AND SHIM-6 IAW REO AND SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,955 hrs · 21,332 cycles

FS 621 AFT PRESSURE BULKHEAD FORWARD SIDE CRACK INDICATION NOTED ON WEB AT AFT CARGO TRACK (UPPER). (C-CHECK) REPAIRED FS 621 AFT PRESSURE BULKHEAD FORWARD SIDE FOR CRACK NOTED ON WEB AT AFT CARGO TRACK (UPPER) IAW REO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,955 hrs · 21,332 cycles

FS 280.0 FLOORBEAM UPPER ANGLE HAS A CRACK AT RBL 10.0. (C-CHECK) REPAIRED CRACK AT FS 280.0 RBL 10.0 UPPER ANGLE IAW REO.

Part: WIRE — LOOSE (CABIN) · airframe 22,953 hrs · 21,330 cycles

A/C LEFT EMERGENCY EXIT OVERWING DOOR LOWER EXIT SIGN DOES NOT ILLUMINATE. (FLT 2959) RE-SECURED LOOSE WIRE IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,842 hrs · 21,222 cycles

REAR OVERHEAD EMERGENCY LIGHT BURNED OUT. (FLT 2977) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,622 hrs · 20,990 cycles

NR 1 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 2953) RELAMPED EMERGENCY LIGHT.

Part: FUSE — BLOWN (BATTERY CHARGER) · airframe 22,484 hrs · 20,845 cycles

LEFT OVERWING EMERGENCY EXIT LOWER SIDEWALL EXIT LIGHT DOES NOT ILLUMINATE. (FLT 2916) REPLACED FUSE ON NR 3 EMERGENCY BATTERY CHARGER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,261 hrs · 19,583 cycles

EMERGENCY LIGHT IN CENTER AISLE AT ROW 10 IS OUT. (FLT 2950) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,160 hrs · 19,479 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2879) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,983 hrs · 19,277 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7986) RELAMPED EMERGENCY LIGHT.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 20,941 hrs · 19,229 cycles

RIGHT WINDSHIELD ARCING AT ALTITUDE AND SHATTERED AFTER LANDING. (FLT 2980) REPLACED RIGHT WINDSHIELD IN REFERENCE TO AMM. PN OFF NP139321-14 SN OFF 03022H4853.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,712 hrs · 18,999 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2967) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,596 hrs · 18,889 cycles

FLT 2973, NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,401 hrs · 18,693 cycles

NR 1 AND NR 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 2921) RELAMPED EMERGENCY LIGHTS.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,224 hrs · 18,529 cycles

FLT 5544, NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,151 hrs · 18,467 cycles

NR 1 AND 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 6307) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,085 hrs · 18,410 cycles

OVERHEAD AFT EMERGENCY LIGHT IS OUT. (FLT 6478) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,911 hrs · 18,280 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6464) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,911 hrs · 18,280 cycles

GALLEY SERVICE DOOR AND FORWARD LEFT EMERGENCY EXTERIOR LIGHTS ARE OUT. (FLT 6464) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,508 hrs · 17,945 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6218) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,404 hrs · 17,858 cycles

NR 2 LEFT SIDE EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 4654) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,251 hrs · 17,736 cycles

LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6447) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,205 hrs · 17,691 cycles

NR 1 OVERHEAD EMERGENCY LIGHT BURNED OUT. (FLT 6378) RELAMPED EMERGENCY LIGHT.

Part: ENGINE — FAILED (RIGHT) · airframe 18,786 hrs · 17,358 cycles

RIGHT ENGINE FAILURE ON TAKEOFF. (FLT 5307) REPLACED RIGHT ENGINE. P/N: CF34-3B1 S/N: 807356C

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,608 hrs · 17,209 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4666) RELAMPED EMERGENCY LIGHT.

Part: MOUNT — CORRODED (RT ENGINE) · airframe 18,539 hrs · 17,143 cycles

RIGHT ENGINE FORWARD YOKE MOUNT HAS CORROSION ON SPHERICAL BUSHING. (ENGINE CHANGE) REPLACED FORWARD YOKE MOUNT ASSEMBLY ON RIGHT ENGINE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,492 hrs · 17,103 cycles

FS 559 PRESSURE BULKHEAD CRACKED ON BOTH SIDES. (C-CHECK) REPAIRED PER REO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 19,531 hrs · 17,967 cycles

FS 280 UPPER FRAME FLANGE CRACKED AT LBL 9.0 OUTBOARD UPPER AILERON PULLEY ATTACH POINT. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,271 hrs · 16,921 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 13 IS OUT. (FLT 3116) RELAMPED. EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 18,217 hrs · 16,867 cycles

ALL EMERGENCY LIGHT BATTERIES DEAD. (FLT 3077) REPLACED ALL FOUR EMERGENCY LIGHTS BATTERY PACKS.

Part: LANDING GEAR — FAILED

LANDED AT 17:10 WITH THE LT MLG UP. THE NTSB HAD RELEASED THE ACFT TO BE DISEMBARKED AND RECOVERED. NO INJURIES WERE REPORTED. THE ACFT WILL BE JACKED TO LOWER THE LT MLG AND TOWED OFF THE RUNWAY. REPAIR IN PROGRESS (FAA SDR 2010101600051/SWIA201024936).

Part: UNKNOWN — MALFUNCTIONED (LT MLG) · airframe 17,101 hrs · 15,754 cycles

(FLT 3074) GEAR DISAGREE RESULTING IN LEFT MLG NOT EXTENDING ON LANDING. REPLACED LEFT MLG ASSEMBLY, LEFT MLG UPLOCK, LEFT MLG SIDE STAY ACTUATOR, LEFT MLG SELECTOR VALVE, 3A AND 3B HYDRAULIC PUMPS, MLG PRIORITY VALVE, MLG BYPASS VALVE, SYSTEM 3 HYDRAULIC RESERVOIR, LEFT ASSIST ACTUATOR, LEFT ASSIST SELECTOR VALVE, PRESSURE RELIEF VALVE, RESTRICTOR VALVE AND PROXIMITY SENSOR ELECTRONIC UNIT WITH SERVICEABLE UNITS PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,689 hrs · 15,327 cycles

NR 3 EMERGENCY CEILING LIGHT INOP. (FLT 3045) RELAMPED EMERGENCY LIGHT.

Part: STRIP — DEFECTIVE (TE FLAP) · airframe 16,014 hrs · 14,624 cycles

AIRCRAFT ROLLED HARD RIGHT WHILE ON FINAL AT 1000FT AGL AND REQUIRED ABOUT HALF CONTROL DEFLECTION TO THE LEFT TO KEEP WINGS LEVEL WITH FLAPS AT 45 DEGREES. (FLT 3075) SANDED LEFT AND RIGHT FLAP TEFLON ABRASION STRIPS DUE TO FINDING LIP ON ABRASION PADS.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 14,421 hrs · 13,004 cycles

FLT 2716, LEFT WINDSHIELD CRACKED. REPLACED WINDSHIELD.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 14,421 hrs · 13,004 cycles

FLT 1010, EMERGENCY EXIT LIGHT INOP. OPERATIONAL CHECK NORMAL.

Part: WINDOW — CRACKED (COCKPIT) · airframe 14,415 hrs · 12,999 cycles

LEFT SIDE WINDOW CRACKED. (FLT 2556) REPLACED WINDOW.

Part: FITTING — OUT OF ADJUST (PAX DOOR) · airframe 14,178 hrs · 12,733 cycles

FLT 2526 - PASSENGER DOOR NOT OPENING AND CLOSING PROPERLY. ADJUSTED DOOR UPPER FORWARD AND AFT SPIGOT FITTINGS.

Part: PIN — LACK OF LUBE (PAX DOOR) · airframe 14,178 hrs · 12,733 cycles

FLT 2681 - MAIN DOOR HARD TO OPEN. LUBED LATCH PINS.

Part: LUG — CRACKED (TE FLAP) · airframe 14,464 hrs · 13,061 cycles

LEFT OUTBOARD FLAP HINGE BOX LUG CRACKED. (C CHECK) REPAIRED PER AMM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 14,464 hrs · 13,061 cycles

CLIP AT FS 280 CRACKED. (C CHECK) REPLACED PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 14,464 hrs · 13,061 cycles

WEB AND CLIPS CRACKED AT FS280. (C CHECK) REPAIRED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 14,464 hrs · 13,061 cycles

AFT PRESSURE BULKHEAD LINTEL FITTING CRACKED. (C CHECK) REPAIRED PER REO.

Part: DOOR — STIFF (MAIN PAX) · airframe 14,103 hrs · 12,643 cycles

FLT 2582 - MAIN CABIN DOOR DIFFICULT TO OPEN. OPERATIONAL CHECK NORMAL.

Part: DOOR — STIFF (MAIN PAX) · airframe 14,103 hrs · 12,643 cycles

FLT 2793 - MAIN CABIN DOOR HARD TO OPEN. OPERATIONAL CHECK NORMAL.

Part: MOUNT — CORRODED (RT ENGINE) · airframe 13,960 hrs · 12,493 cycles

RIGHT ENGINE THRUST MOUNT CORRODED. SB COMPLIANCE, REPLACED PER AMM.

Part: PIN — LACK OF LUBE (PAX DOOR) · airframe 12,985 hrs · 11,425 cycles

FA UNABLE TO OPEN MAIN CABIN DOOR. (FLT 2523)LUBED CABIN DOOR LATCH PINS.

Part: WHEEL — BINDING (PAX DOOR) · airframe 12,555 hrs · 10,955 cycles

FLIGHT ATTENDANT REPORTS THAT THE MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. FLIGHT 2803. INSPECTED, CLEANED AND ADJUSTED PAX DOOR SUPPORT WHEEL IAW 52-11-13. OPS CHECK GOOD.

Part: HANDLE — WORN (PAX DOOR) · airframe 12,197 hrs · 10,563 cycles

FLT 2555 - MAIN CABIN DOOR WOULD NOT OPEN. REPLACED MAIN CABIN DOOR OUTER HANDLE IAW AMM 52-11-03. OPS CHECK GOOD.

Part: LATCH — DAMAGED (PAX DOOR) · airframe 11,621 hrs · 9,993 cycles

FLIGHT ATTENDANT WAS UNABLE TO OPEN MAIN CABIN DOOR. REPLACED DOOR LATCH MECHANISM BOX PER MM 52-11-25. OPS CHECK GOOD.

Part: DOOR — OUT OF RIG (PAX DOOR) · airframe 11,542 hrs · 9,920 cycles

FLT 2640 - MAIN CABIN DOOR WOULD NOT SHUT PROPERLY. RIGGED PASSENGER DOOR ASSEMBLY IAW AMM 52-11-25. OPS CHECK GOOD.

Part: DOOR — DIRTY (MAIN PAX) · airframe 11,406 hrs · 9,805 cycles

FLT 2511 - MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. CLEANED, LUBED AND CYCLED DOOR SEVERAL TIMES IAW CRJ AMM 52-70-00. OPS CHECK GOOD.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 8,645 hrs · 7,593 cycles

FLIGHT 5312- DURING LANDING RECEIVED A FLAP FAIL CAUTION MESSAGE AT 8 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (G) 1,2,3, (A,B,C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: BPSU — FAULTY (RT WING TE FLAPS) · airframe 8,651 hrs · 7,598 cycles

FLIGHT 5245 - FLAP FAIL MESSAGE. SECOND EVENT. REMOVED AND REPLACED RIGHT BPSU.

Part: ADC — MALFUNCTIONED (AVIONICS) · airframe 7,602 hrs · 6,586 cycles

FLIGHT 9761 - EFIS COMP MON WARNING. REPLACED THE NR 2 ADC.

Part: ENGINE — FAILED (RIGHT) · airframe 7,546 hrs · 6,539 cycles

FLIGHT 5788 - FOUND RT ENGINE OIL PRESSURE WARNING. REPLACED THE RT ENGINE.

Part: RELAY — OVERHEATED (AVIONICS BAY) · airframe 7,485 hrs · 6,476 cycles

FLIGHT 5029- ENROUTE CVG-ACY CREW DETECTED AN ELECTRICAL OVERHEAT SMELL FOLLOWED BY AC BUS 1 CAUTION MESSAGE, LEFT AUTO TRANSFER FAIL, GENERATOR 1 OFF CAUTION, STAB TRIM AND MACH TRIM CAUTIONS, EFIS COMP MON WITH IAS YELLOW ON AIRSPEED AND AUTOPILOT NOSE UP TRIM CAUTION. CREW DECLARED AN EMERGENCY AND DIVERTED TO CMH, FLIGHT LANDED WITHOUT INCIDENT. (NO VISIBLE SMOKE IN COCKPIT OR CABIN). FOUND 1K4XD - AC UTILITY BUS #1 RELAY TO BE THE ROOT CAUSE OF ELECTRICAL OVERHEAT SMELL. REPLACED RELAY AND SURROUNDING ELECTRICAL COMPONENTS/WIRING.

Part: TRANSDUCER — MALFUNCTIONED (RT ENGINE) · airframe 6,286 hrs · 5,346 cycles

RT ENGINE OIL PRESSURE WARNING. REPLACED OIL PRESSURE TRANSDUCER.

Part: WARNING LIGHT — ILLUMINATED (OIL SYSTEM) · airframe 6,100 hrs · 5,279 cycles

FLIGHT 5701 - RIGHT ENGINE OIL PRESSURE WARNING. SERVICED RIGHT ENGINE WITH 3.5 QTS OIL, PERFORMED OIL CONSUMPTION RUN AND LEAK CHECK WITH SATISFACTORY RESULT.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 5,971 hrs · 5,168 cycles

OUTBOARD INTERCOSTALS CRACKED AT FS 484. REPAIRED IAW REO 601R-53-41-059.

Part: FLOOR SUPPORT — CRACKED (CARGO BAY) · airframe 5,971 hrs · 5,168 cycles

LT AND RT CARGO FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117.

Part: PUMP — FAILED (RT ENGINE) · airframe 5,732 hrs · 4,955 cycles

FLIGHT 5170 DURING CRUISE FLT (BTV/CVG) RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING, CREW DECLARED AN EMERGENCY, PERFORMED RT ENGINE IFSD PROCEDURE, DIVERTED TO BUF AND LANDED WITHOUT INCIDENT. REPLACED THE RT ENGINE LUBRICATION AND SCAVENGE PUMP ASSEMBLY.

Part: WARNING LIGHT — ILLUMINATED (OIL SYSTEM) · airframe 5,697 hrs · 4,919 cycles

FLIGHT 5837 ENGINE OIL PRESSURE WARNING. INSPECTED ENGINE OIL SYSTEM, NO DEFECTS FOUND, GROUND RIMS WERE SATISFACTORY. COULD NOT DUPLICATE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 2,551 hrs · 2,216 cycles

DAMAGED STRUCTURE ON RIGHT SIDE OF FUSELAGE AT FS 640 AND FS 672.2. REPAIRED STRUCTURE DAMAGE ON RIGHT SIDE FS 640 AND 672.2 IN ACCORDANCE WITH REO 601R-53-61-956.