N978SW

Part: APU — FAULTED (ZONE 100) · airframe 48,282 hrs · 42,144 cycles

APU OIL TEMP CAUTION AT CRUISE. (FLIGHT 5116) REF AML 1760814, REF AML 1760819, REF AML 1760821, DEFERRING APU IAW MEL 49-10-1A. REMOVED & REPLACED APU ASSY, & APU GENERATOR. OPS CHKD GOOD. APU OIL TEMP CAUTION NO LONGER DISPLAYED. DMI CLEARED AND PLACARDS REMOVED.

Part: OIL SYSTEM — WARNING MESSAGE (APU) · airframe 48,264 hrs · 42,121 cycles

APU OIL TEMP CAUTION IN CRUISE. MEL 49-10-1ACAT C, ODI EVENT, (FLIGHT 5116) REFERENCE AML 1760814, REFERENCE AML 1760819, REFERENCE AML 1760821. DEFERRING APU IAW MEL 49-10-1A. MAINTENANCE PROCEDURES COMPLIED WITH. PLACARD INSTALLED.

Part: WARNING MESSAGE — ILLUMINATED (APU OIL TEMP) · airframe 48,264 hrs · 42,121 cycles

APU OIL TEMP CAUTION AT CRUISE. (FLIGHT 5116)

Part: OIL SYSTEM — WARNING MESSAGE (APU) · airframe 48,264 hrs · 42,121 cycles

APU OIL TEMP CAUTION AT CRUISE. (FLIGHT 5116) REFERENCE AML 1760814, REFERENCE AML 1760819, REFERENCE AML 1760821. DEFERRING APU IAW MEL 49-10-1A. MAINTENANCE PROCEDURES COMPLIED WITH. PLACARD INSTALLED.

Part: OIL SYSTEM — LOW PRESSURE (LT ENGINE) · airframe 46,130 hrs · 39,804 cycles

AT CRUISE APPROX 25 MIN FROM XWA GOT L ENG OIL PRESS WARNING MESSAGE. RAN QRH. IT CALLED FOR SHUTTING THE ENGINE DOWN. RAN QRH FOR SHUTTING LEFT ENGINE DOWN. LANDED SAFELY. (FLIGHT 5461 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS

Part: OIL SYSTEM — LOW PRESSURE (LT ENGINE) · airframe 46,133 hrs · 39,806 cycles

AT CRUISE APPROX 25 MIN FROM XWA GOT L ENG OIL PRESS WARNING MESSAGE. RAN QRH. IT CALLED FOR SHUTTING THE ENGINE DOWN. RAN QRH FOR SHUTTING LEFT ENGINE DOWN. LANDED SAFELY. FLIGHT 5461. REPLACED LEFT ENGINE ATS, IDG, #6 AND #7 CARBON SEALS AND EXHAUST FRAME. PERFORMED LEFT ENGINE HOUR LONG OIL CONSUMPTION RUN REF GE MANUAL 72-00-00. NO OIL ADDED AFTER RUN. LEAK CHECK GOOD.

Part: BPSU — FAILED (TE FLAPS) · airframe 45,845 hrs · 39,498 cycles

RECEIVED FLAPS FAIL CAUTION MESSAGE AT CRUISE ALTITUDE. RAN QRH AND RETURNED TO ORD. (FLIGHT 5722 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28399576 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE CP 28400569 FOR TROUBLESHOOTING OF FLAP FAIL CAUTION AND REPLACEMENT OF THE LEFT BPSU. OPS CHECK GOOD. REFERENCE CP 28400457 FOR COMPLIANCE WITH FLAP FAIL AD 2009-06-12/09."

Part: UNKNOWN — DENTED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

RH WING LEADING EDGE PANE 620 JL HAS A SMALL DENT ON THE INBOARD SIDE (TOP) 27104415 (C-CHECK RO 9/6/2023) REPAIRED R/H WING LEADING EDGE PANEL REF REO 601R-57-41-1165 REV -- DATED 2023-09-01. COMPLIED WITH 51-900-1003-SKY AND VISUALLY INSPECT FOR ANY DAMAGE PROPAGATION AT INTERVALS NOT TO EXCEED 300 FLIGHT HOURS . SEE CONTINUATION CARD FOR DETAILS.REPAIR WAS MEASURMENT AND INSPECTION ONLY - NO MATERIAL ADDED OR REMOVED - WEIGHT IS UNCHANGED

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

*FS333.00 STRG 0 - STRG 1LH, FRAME POSSIBLY CRACKED AT LOWER MACHINE HOLE (MARKED) 26957001 (C-CHECK RO 9/6/2023) REPAIRED FS333.00 STRG 0 - STRG 1LH, FRAME REO 601R-53-21-3642 REV -- DATE 2023-08-11. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

STRINGER 3L IS CRACKED JUST FORWARD OF FRAME 379.00 AT IS CONNECTION POINT WITH THE PASSENGER DOOR UPPER SILL FITTING. (MARKED) (C-CHECK RO 9/6/2023) REPAIRED STRINGER 3L JUST FORWARD OF FRAME 379.00 REF CRJ-200-SRM 53-00-03. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

STRINGER 3L IS CRACKED JUST FORWARD OF FRAME 379.00 AT IS CONNECTION POINT WITH THE PASSENGER DOOR UPPER SILL FITTING. (MARKED) (C-CHECK RO 9/6/2023) REPAIRED STRINGER 3L JUST FORWARD OF FRAME 379.00 REF CRJ-200-SRM 53-00-03. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

FOUND CRACK ON COCKPIT FLOOR SUPPORT ANGLE ,FWD OF FS 280 FLOOR BEAM. (C-CHECK RO 9/6/2023) REPLACED CRACK COCKPIT FLOOR SUPPORT ANGLE ,FWD OF FS 280 FLOOR BEAM WITH NEW ANGLE PN 600-34017-351 PO# T-69724 REF CRJ 200 SRM 51-42-06 AND DWG 600-34017 REV AD. COMPLIED WITH SKY CARD 51-900-1003-SKY STRUCTURAL MAJOR REPAIR.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

AFTER REMOVAL OF R/H ELEVATOR FITTING AT BL15.25, FITTING WAS DIS-ASSEMBLED TO EVALUTE PRIOR TO NEW BEARING INSTALLATION AND FOUND CORROSION AND PITTING INSIDE BOTH SIDES OF BEARING BORE. (C-CHECK RO 9/6/2023) R/H ELEVATOR FITTING LOCATED AT BL 15.25 HAS BEEN REMOVED AND REPLACED W/A NEW FITTING (PN 600-24043-1) REF DWG# 601R24025, REV G. REFER TO CONTINUATION SHEET FOR DETAILS.C/W SKY CARD 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

LEFT HAND PRESSURE FLOOR SILL HAS CORROSION IN MULTIPLE AREAS BETWEEN FS409+128 TO FS559.00. (MARKED) (C-CHECK RO 9/6/2023) REPAIRED LEFT HAND PRESSURE FLOOR SILL BETWEEN FS409+128 TO FS559.00 BY COMPLYING WITH ALL STEPS OF REO 601R-53-41-666 REV -C DATED 2012-11-06. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

UPON REMOVAL ON JOB HN103215 CAMP #26917265, FOUND L/H ELEVATOR L/E HINGE FITTING ASSY P/N 600-24043-1 AT ES16.52 TO HAVE PITTING CORROSION IN BEARING BORES OF BOTH FITTING HINGE HALVES. REPLACE HINGE FITTING ASSY P/N 600-24043-1. (C-CHECK RO 9/6/2023) REMOVED L/H ELEVATOR HINGE FITTING ASSY P/N 600-24043-1 LOCATED ON ELEVATOR L/E @ ES16.52 FOR REPLACEMENT OF BEARING, AND SEPARATED FITTING ASSY INTO HINGE HALVES REF CRJ 200 SRM 51-42-06, AND CRJ 200 SRM 51-42-21. UPON REMOVAL OF BEARING, FOUND PITTING CORROSION IN BEARING BORES OF BOTH HINGE HALVES. REPLACE HINGE FITTING ASSY P/N 600-24043-1. INSTALLED 1 EA NEW L/E HINGE FITTING ASSY P/N 600-24043-1 ON L/H ELEVATOR @ ES16.52 REF BOMBARDIER DWG #601R24025 REV (G), CRJ 200 SRM 51-42-21, AND CRJ 200 SRM 51-42-06. USED TORQUE WRENCH TUC 6229 CAL DUE 31 JULY 2023.COMPLIED WITH TASK 51-900-1003-SKY AND M-337

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

FOUND 2 CRACKED AREAS AT LBL 12 AND 1 CRACKED AREA AT RBL 12.0 ON FS 280 FLOOR SUPPORT BEAM. (C-CHECK RO 9/6/2023) REPAIRED BULKHEAD WEB FS280 FLOOR SUPPORT BEAM BY COMPLYING WITH ALL STEPS OF REO 601R-53-11-926 REV -B DATED 2006/05/10. NO DEFECTS NOTED. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. STRUCTURAL MAJOR REPAIR. SEE CONTINUATION CARD FOR FURTHER DETAILS.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

FOUND 2 CRACKED AREAS AT LBL 12 AND 1 CRACKED AREA AT RBL 12.0 ON FS 280 FLOOR SUPPORT BEAM. (C-CHECK RO 9/6/2023) REPAIRED BULKHEAD WEB FS280 FLOOR SUPPORT BEAM BY COMPLYING WITH ALL STEPS OF REO 601R-53-11-926 REV -B DATED 2006/05/10. NO DEFECTS NOTED. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. STRUCTURAL MAJOR REPAIR. SEE CONTINUATION CARD FOR FURTHER DETAILS.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

LH FLOOR SILL AFT OF FS 449.85 HAS CHIPPED PAINT AND LIGHT CORROSSION AT FASTNER HOLE MARKED (C-CHECK RO 9/6/2023) REPAIRED LH FLOOR SILL AFT OF FS449.85 BY COMPLYING WITH REO 601R-53-41-666 REV -C DATED 2012-11-06. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. BLEND OUT ONLY NO WEIGHT CHANGE.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

FRAME AT FS574.0 STGR24R-STGR27 HAS AREAS OF CORROSION (C-CHECK RO 9/6/2023) INSTALLED NEW FRAME SECTOR AT FS574.00 PER CRJ200 SRM 51-42-06 AND 51-42-21 AND 51-42-22.DWG# 601R35031 REV-AG AND DWG# 601R35226 REV-P AND DWG# 601R36024 REV-N.COMPLIED WITH ALL STEPS OF REO 601R-53-61-8062 REV -A DATED 2023-08-10.COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (STRUCTURAL MAJOR REPAIR).NO DEFECTS NOTED.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

PRESSURE FLOOR FS481.00 INBOARD AFT ATTACH ANGLE ON BRACKET BETWEEN RBL27 & RBL43 IS CRACKED. (MARKED) (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED NEW ATTACH ANGLE BRACKET REF CRJ200 SRM 51-42-21 AND REO 601R-53-41-059 REV-C DATED: 2020-03-11 USED FOR FASTENER CALL OUT FOR 4 FASTENERS ONLY. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

RIGHT WING TRAILING EDGE UNDER OUTBOARD GROUND SPOILER WS137.0 CRACKED (C-CHECK RO 9/6/2023) REPAIRED CRACK TO TRAILING EDGE RIB AT WS130.10 RHS PER R.E.O. 601R-57-51-1020 REV. -- DATED 2023-07-21. COMPLIED WITH ALL APPLICABLE STEPS SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1003-SKY AND (M-337)

Part: UNKNOWN — GOUGED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

RH ELEVATOR INBD HINGE GOUGED (C-CHECK RO 9/6/2023) REMOVED GOUGE FROM RH ELEVATOR INBD HINGE, WITHIN LIMITS. RECEIVED AND COMPLIED WITH MHIRJ REO 601R-55-11-748 REV --A, DATED 2023-08-18 . SEE CONTINUATION FOR FURTHER DETAILS. COMPLIED WITH 51-900-1003-SKY.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

PAX DOOR INTERCOSTAL AT DD7 BETWEEN FS 320.10 AND FS329.50 HAS CORROSION (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD7 REF CRJ200 SRM 51-42-06 AND DWG 601R31702 REV N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — GOUGED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

*LH EMER DOOR, BOTH THE FWD AND AFT BOTTOM DOOR HOOKS (ON DOOR) ARE GOUGED AND AREAS OF ROLLED METAL (MARKED) (C-CHECK RO 9/6/2023) REPAIRED DAMAGE AT LH OVERWING EMERGENCY EXIT DOOR FWD AND AFT LOWER FITTINGS PER REO 601R-52-21-147 REV -- DATE 2023-07-23 ALL STEPS OF REO COMPLIED WITH. LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY AND M-337. SEE CONTINUE CARD FOR DETAILS

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

LEFT SIDE FS235.00 UPPER FRAME SECTOR IS CRACKED. (MARKED) SRM 53-11-15 (C-CHECK RO 9/6/2023) REPLACED LH SIDE FS235.00 UPPER FRAME SECTOR/ANGLE P/N: 601R34032-21, NEW CLIP P/N: 601R34032-31 AND NEW ATTACHMENT ANGLE P/N:601R34032-19. REF CRJ200 SRM 51-42-06, REF CRJ200 SRM 51-42-21, AND DWG 601R34032 REV-V. NO DEFECTS NOTED. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (STRUCTURAL MAJOR REPAIR).

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

FUSELAGE SKIN JUST AFT OF THE PASSENGER DOOR HINGE HAS DAMAGE. (MARKED) (C-CHECK RO 9/6/2023) REPAIRED FUSELAGE SKIN JUST AFT OF THE PASSENGER DOOR HINGE REF REO 601R-53-21-3643 REV -- DATED 2023-08-07. COMPLIED WITH 51-900-1003-SKY AND LEAK CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS. BLEND ONLY NO WEIGHT CHANGE.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

DATUM 1 INTERCOSTAL BETWEEN APPROX FS320 - FS338 HAS CORROSION (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED NEWLY DRILLED INTERCOSTAL D1 BETWEEN FS320 - FS338 REF CRJ200 SRM 51-42-06 REF CRJ200 SRM 51-42-21 AND DWG 601R31702 REV-N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — BENT (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

CARGO DOOR FORWARD TRACK SUPPORT LOWER CHANNEL IS BENT. (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED THE NEW CHANNEL AT THE AFT CARGO DOOR FORWARD TRACK SUPPORT THE LOWER CHANNEL PART # 601R35050-119 REF. CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21 AND DWG 601R35050 REV. AC. SEE CONTINUATION CARD FOR DETAILS C/W TASK CARD 51-900-1003-SKY

Part: UNKNOWN — BENT (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

CARGO DOOR FORWARD TRACK SUPPORT LOWER CHANNEL IS BENT. (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED THE NEW CHANNEL AT THE AFT CARGO DOOR FORWARD TRACK SUPPORT THE LOWER CHANNEL PART # 601R35050-119 REF. CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21 AND DWG 601R35050 REV. AC. SEE CONTINUATION CARD FOR DETAILS C/W TASK CARD 51-900-1003-SKY

Part: UNKNOWN — BENT (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

CARGO DOOR FORWARD TRACK SUPPORT UPPER CHANNEL IS BENT. (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED A NEW REPLACEMENT CARGO DOOR FORWARD TRACK SUPPORT UPPER CHANNEL (PART#601R35050-21) REF CRJ 200 SRM 51-42-06 AND DRAWING 601R35050 REV AC. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUATION FOR FURTHER DETAILS.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

DATUM 4 INTERCOSTAL BETWEEN APPROX FS338 - FS347 HAS CORROSION (C-CHECK RO 9/6/2023) REMOVED AND REPLACED INTERCOSTAL D4 BETWEEN FS338 - FS347 REF CRJ200 SRM 51-42-06 DWG 601R31702 REV-N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

DATUM 2 INTERCOSTAL BETWEEN APPROX FS338 - FS347 HAS CORROSION (C-CHECK RO 9/6/2023) REMOVED AND REPLACED INTERCOSTAL D2 BETWEEN FS338 - FS347 REF CRJ200 SRM 51-42-06 , AND DWG 601R31702 REV-N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOODS . SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

DATUM 1 INTERCOSTAL BETWEEN APPROX FS338 - FS347 HAS CORROSION (C-CHECK RO 9/6/2023) REPLACED INTERCOSTAL D1 BETWEEN FS338 - FS347 REF CRJ200 SRM 51-42-06. DWG 601R31702 REV-N. PRESSURE LEAK CHECK GOOD. SEE CONTINUE CARD FOR ALL WORK PERFORMED. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

DATUM 3 INTERCOSTAL BETWEEN APPROX FS320 - FS338 HAS CORROSION (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED NEW PAX DOOR DATUM 3 INTERCOSTAL BETWEEN FS 320 -FS338 REF CRJ-200-SRM 51-42-06, CRJ-200-SRM 51-42-21 AND DRAWING 601R31702 REV N . COMPLIEDWITH 51-900-1003-SKY AND PRESSURE CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

DATUM 5 INTERCOSTAL BETWEEN APPROX FS338 - FS347 HAS CORROSION (C-CHECK RO 9/6/2023) REMOVED AND REPLACED INTERCOSTAL D5 BETWEEN FS338 - FS347 REF CRJ200 SRM 51-42-06, DWG 601R31702 REV-N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

DATUM 4 INTERCOSTAL BETWEEN APPROX FS320 - FS338 HAS CORROSION (C-CHECK RO 9/6/2023) INSTALLED NEWLY DRILLED INTERCOSTAL D4 BETWEEN FS320 - FS338 REF CRJ200 SRM 51-42-06 REF CRJ200 SRM 51-42-21 AND DWG 601R31702 REV-N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

AFT FORMER @ APPROX. FS347 HAS CORROSION (C-CHECK RO 9/6/2023) REMOVED AND REPLACED AFT FORMER @ FS347 REF CRJ200 SRM 51-42-06 REF CRJ200 SRM 51-42-21 DWG 601R31702 REV-N. NO DEFECTS NOTED. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (STRUCTURAL MAJOR REPAIR).

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

FWD FORMER @ APPROX. FS311 HAS CORROSION (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED NEW FWD PASSENGER DOOR FORMER REF CRJ-200-SRM 51-42-06 , CRJ-200-SRM 51-42-21, AND DRAWING 601R31702 REV N . COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — WORN (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

PAX DOOR PIANO HINGE ON AIRCRAFT SIDE HAS WORN HINGE PIN HOLES (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED NEW HINGE (FUSELAGE SIDE) REF. CRJ 200 SRM 53-21-23 , DWG 601R31527 REV AM AND REO 601R-53-21-656 REV. A DATED 2017/03/06. LEAK CHECK GOOD. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CHAFED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

LEFT INBOARD FLAP VANE INBOARD LEADING EDGE PANEL IS CHAFED. (C-CHECK RO 9/6/2023) EVALUATED FOUND OUT OF LIMITS, REMOVED AND INSTALLED NEW LEFT INBOARD FLAP VANE INBOARD LEADING EDGE PANEL REF CRJ200 SRM 51-42-13 & DWG 601R14303 REV J. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. 99747

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

PAX DOOR INTERCOSTAL MID DD2 IS CORRODED(MARKED). (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED NEWLY DRILLED INTERCOSTAL D2 BETWEEN FS320 - FS338 REF CRJ200 SRM 51-42-06 REF CRJ200 SRM 51-42-21 AND DWG 601R31702 REV-N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

PAX DOOR INTERCOSTAL MID DD6 IS CORRODED(MARKED). (C-CHECK RO 9/6/2023) REMOVED AND INSTALLED NEWLY DRILLED INTERCOSTAL D6 BETWEEN FS320 - FS338 CRJ200 SRM 51-42-06 CRJ200 SRM 51-42-21 AND DWG 601R31702 REV-N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — WORN (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

RH WING AILERON HAS WEAR ON LOWER LEADING EDGE SHROUDS. MARKED. (C-CHECK RO 9/6/2023) REPLACED SHROUD AT R/H WING AILERON LWR I/B L/E WITH NEW FASTENERS REF. CRJ200 SRM 51-42-21 & BOMBARDIER DWG. CC670-1300 REV. -D AND RESTORED FINISH ON FASTENERS REF. CRJ200 SRM 51-25-16. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1003-SKY AND M-337

Part: UNKNOWN — DENTED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

LEFT INBD WING FLAP LOWER SKIN DENTED INBD SIDE MARKED. (C-CHECK RO 9/6/2023) REPAIRED LEFT INBD WING LOWER SKIN (LH INBD FLAP LOWER SKIN). REF CRJ200 SRM 57-52-00 REPAIR #3. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (STRUCTURAL MAJOR REPAIR).

Part: UNKNOWN — GOUGED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

LH WING AILERON CENTER HINGE (WING SIDE) HAS GOUGES. MARKED. (C-CHECK RO 9/6/2023) REPAIRED GOUGE ON LH WING AILERON (WING SIDE) CENTER HINGE TO A SMOOTH CONTOUR REF CRJ200 SRM 51-12-00. AND REO 601R-57-51-1018 REV--, DATED 2023-07-19 ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1003-SKY AND M-337. SEE CONTINUATION CARD FOR DETAILS.

Part: UNKNOWN — DENTED (UNKNOWN) · airframe 44,712 hrs · 38,304 cycles

BETWEEN FS409+48 AND FS409+64 BETWEEN STR 23L AND 24L. BLEND PERFORMED PER REO 601R-53-00-115 REV A. LOOKS LIKE A SMALL DENT. 2 DENTS LOCATED APPROXIMATELY BETWEEN FS409+16 AND FS409+48 AND BETWEEN STRINGERS 23L AND 24L. 2EA INDICATIONS OF DENTING DETERMINED TO BE BLENDS TO REMOVE LIGHTNING STRIKE DAMAGE. BLEND AT FS409+16, 2.10" ABOVE STGR 23L IS A PERMANENT REPAIR PER GREO 601R-53-00-115 REV A DATED 2010-09-29 AND BLEND AT 2.50" FWD OF FS409+32, 2.80" ABOVE STGR 23L IS A PERMANENT REPAIR PER REO 601R-53-00-404 REV -- DATED 2011-02-10. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK RO 9/6/2023) PERFORMED REPAIRS TO LH FUSELAGE SKIN BETWEEN FS409+16 - FS409+64 BETWEEN STGR 22L TO STGR24L BY COMPLYING WITH ALL STEPS OF REO 601R-53-31-1284 REV-- DATED 2023-07-25. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY, NO DEFECTS NOTED.

Part: NONE — DENTED · airframe 43,748 hrs · 37,409 cycles

DENT ON FUSELAGE SKIN FWD OF FS574.00 BETWEEN STGR1L AND 2L. (HAS BEEN DETEMINED TO BE A MAJOR REPAIR.) (FILED CLOSED)PERFORMED A DOUBLER REPAIR INSTALLED ON FUSELAGE SKIN FWD OF FS574.00 BETWEEN STGR1L AND 2L IN REFERENCE TO CRJ200 SRM 53-00-31, FASTENERS INSTALLED IN REFERENCE TO REO 601R-53-61-7860 REV -- DATED 2022-07-11 / ALSO SEE CP#25143120 FOR PRESSURIZATION CHECK.

Part: NONE — CRACKED · airframe 43,264 hrs · 36,955 cycles

CARGO DOOR SCUFF PLATE CRACKED AT ONE SCREW (FILED - CLOSED) REPLACED CARGO DOOR SCUFF PLATE IN REFERENCE TO RJ 200 AMM 53-60-31

Part: NONE — CRACKED · airframe 42,829 hrs · 36,559 cycles

AT CRUISE ALTITUDE R WINDSHIELD HEAT CAUTION MESSAGE AND 30 SECONDS LATER THE EXTERIOR WINDSHIELD LAYER SHATTERED (FLIGHT 5068 - FILED CLOSED) REMOVED AND REPLACED RIGHT WINDSHIELD, OPS AND LEAK CHECKS GOOD, REFERENCE AMM 56-11-04 COMPLIED WITH TASK CARD 56-220-1000-SKY

Part: PROXIMITY SENSOR — OUT OF ADJUST (MLG) · airframe 41,670 hrs · 35,521 cycles

GEAR DISAGREE ON APPROACH TO ORD. RIGHT MAIN LANDING GEAR WOULD NOT EXTEND. RAN QRH AND RESOLVED ISSUE. LANDED WITHOUT INCIDENT. (FLIGHT 5390 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22613534 WITH THE FOLLOWING CORRECTIVE ACTION: "TROUBLESHOT GEAR DISAGREE IN REFERENCE TO CRJ 200 FIM 32-60-09. FOUND THAT S33 AND S17 PROX SENSOR WERE SHOWING FAR IN THE PSEU. REDADJUSTED S33 PROX SENSOR IN REFERENCE TO CRJ 200 AMM 32-61-05. FOUND THAT S17 PROX SENSOR WAS WITHIN RIGGING LIMITS. PERFORMED MULTIPLE GEAR SWINGS IN REFERENCE TO CRJ 200 AMM 32-30-00 IN MULTIPLE CONFIGURATIONS, HYDRAULIC SYSTEM 3A ON/3B OFF, 3A OFF/3B ON AND BOTH HYDRAULIC SYSTEM 3A/B ON WITH NO DISCREPENCIES NOTED. LANDING GEAR EXTENDED AND RETRACTED AS INTENDED. OKAY FOR CONTINUED SERVICE AT THIS TIME. REFERENCE CP 22613704-1 FOR SEALANT APPLICATION ON S33 PROXIMITY SENSOR.

Part: SEAT TRACK — CORRODED (BS 605-621) · airframe 40,206 hrs · 34,146 cycles

SEAT TRACK LBL 27 REQUIRES REPLACEMENT DUE TO CORROSION FS605-FS621 (C-CHECK) RO 2/10/2020 REMOVED CORRODED SEAT TRACK AND REPLACED WITH NEW SEAT TRACK IAW CRJ-200 AMM.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 40,206 hrs · 34,146 cycles

SEAT TRACK ON TOP OF FLOOR BEAM LBL27 FS559+80-FS559+96 REQUIRES FABRICATION DUE TO CORROSION 101813 1000/0150 #7568663 (C-CHECK) RO 2/10/2020 LOCATE AND DRILL IAW CRJ 200 SRM TR 51-42 PART# 20276-288-0-0, TAG# B88014. PRIMER IAW CRJ 200 SRM TOP COAT IAW CRJ 200 SRM ALODINE IAW CRJ 200 SRM

Part: SEAT TRACK — CORRODED (BS 559) · airframe 40,206 hrs · 34,146 cycles

SEAT TRACK RBL 27 FS 559+/0 - FS 559+96 REQUIRES FABRICATION DUE TO CORROSION 1018131 1000/0153 #7568666 (C-CHECK) RO 2/10/2020 DRILLED AND LOCATED SEAT TRACK IAW CRJ-200 REO. PN: CDSP1900-509 TN:B13362 AND CRJ-200 SRM 51-40-11 TR 51-42

Part: SEAT TRACK — CORRODED (BS 449-554) · airframe 40,206 hrs · 34,146 cycles

LH SIDEWALL SEAT TRACK REQUIRES FABRICATION DUE TO CORROSION FS449-FS544 1018131 2000/0050 #7568413 (C-CHECK) RO 2/10/2020 LOCATED AND DRILLED NEW SEAT TRACK IAW REO AND CRJ-200 SRM.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 40,206 hrs · 34,146 cycles

INTERCOSTAL CRACKED AT STGR 13L RPB FS 621.0 TO FS 625.3 FRAME (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED FS 621-625.3 STR 13L INTERCOSTAL IAW CRJ 200 SRM.

Part: INTERCOSTAL — CRACKED (BS 621-623) · airframe 40,206 hrs · 34,146 cycles

INTERCOSTAL CRACKED AT STGR 14L RPB FS 621.0 TO 625.3 FRAME (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED FS 621-FS 625.3 AT STR 14L IAW CRJ 200 SRM.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 40,206 hrs · 34,146 cycles

RH SIDEWALL SEAT TRACK #3 REQUIRES FABRICATION DUE TO CORROSION FS409+16-FS409+112. 1018131 2000/0046 #7568409 (C-CHECK) RO 2/10/2020 DRILLED AND LOCATED SEAT TRACK IAW CRJ-200 REO AND CRJ-200 SRM TR 51-42 REV C 12/18/17

Part: SEAT TRACK — CORRODED (BS 549-559) · airframe 40,206 hrs · 34,146 cycles

RH SIDEWALL SEAT TRACK #7 REQUIRES FABRICATION DUE TO CORROSION FS549-FS559+80 1018131 2000/0044 #7568407 (C-CHECK) RO 2/10/2020 FABRICATED SEAT TRACK IAW CRJ-200 REO.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 40,206 hrs · 34,146 cycles

SEAT TRACK ON TOP OF FLOOR BEAM LBL27 HAS CORROSION SPOTS BETWEEN FS 559+80 THRU 559+96 IN THE CARGO BAY (C-CHECK) RO 2/10/2020 INSTALLED SEAT TRACK IAW CRJ 200 AMM. AAR527961 CAL DUE 10-02-20

Part: SEAT TRACK — CORRODED (BS 559) · airframe 40,206 hrs · 34,146 cycles

SEAT TRACK ON TOP OF FLOOR BEAM RBL 27 HAS CORROSION SPOTS BETWEEN FS 559+80 THRU FS 559+96, IN THE CARGO BAY. (C-CHECK) RO 2/10/2020 REMOVED CORRODED SEAT TRACK AND REPLACED WITH NEW SEAT TRACK IAW CRJ-200 AMM.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 40,206 hrs · 34,146 cycles

RH SIDEWALL SEAT TRACK #4 REQUIRES FABRICATION DUE TO CORROSION FS409+112-FS449+85. 1018131 2000/0041 #7568404 (C-CHECK) RO 2/10/2020 LOCATED AND DRILLED RH SIDEWALL SEAT TRACK IAW TR 51-42 P/N: 20276-288-0-0 TAG#B15445

Part: SEAT TRACK — CORRODED (BS 406-409) · airframe 40,206 hrs · 34,146 cycles

LH SIDEWALL SEAT TRACK #3 REQUIRES FABRICATION DUE TO CORROSION FS406+16-FS409+112. 1018131 2000/0047 #7568410 (C-CHECK) RO 2/10/2020 LOCATED AND DRILLED SEAT TRACK IAW CRJ-200 SRM.

Part: FLOORBEAM — CORRODED (BS 621) · airframe 40,206 hrs · 34,146 cycles

FLOOR LANDING STRIP HAS CORROSION AND BARE METAL SPOTS AT FS 621 BETWEEN RCL 27 AND THE RH FLOOR SILL, IN THE CARGO BAY. (C-CHECK) RO 2/10/2020 CORROSION FOUND TO BE OUT OF LIMITS IAW CRJ-200 SRM. REMOVED AND REPLACED REPAIR PARTS IAW BOMBARDIER GREO.

Part: FLOORBEAM — CORRODED (BS 621) · airframe 40,206 hrs · 34,146 cycles

FLOOR PANEL LANDING STRIP AT FS 621 HAS CORROSION AND BARE METAL SPOTS BETWEEN LBL 27 AND THE LH FLOOR SILL, IN THE CARGO BAY. (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED CRACKED ANGLE IAW REO.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 40,206 hrs · 34,146 cycles

SEAT TRACK ON TOP OF FLOOR BEAM LBL 9 HAS CORROSION SPOTS BETWEEN FS 559 + 80 THRU FS 559 + 96 IN THE CARGO BAY (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED SEAT TRACK IAW CRJ-200 AMM.

Part: SEAT TRACK — CORRODED (BS 406-449) · airframe 40,206 hrs · 34,146 cycles

LH SIDEWALL SEAT TRACK #4 REQUIRES FABRICATION DUE TO CORROSION FS406+112-FS449+85. 1018131 2000/0048 #7568411LOCATED AND DRILLED SEAT TRACK IAW CRJ-200 SRM TR AND REO.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 40,206 hrs · 34,146 cycles

RH SIDEWALL SEAT TRACK #5 REQUIRES FABRICATION DUE TO CORROSION FS449.85+FS499. 1018131 2000/0042 #7568405 (C-CHECK) RO 2/10/2020 DRILLED AND LOCATED NEW SEAT TRACK IAW CRJ-200, TR,AND REO.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 40,206 hrs · 34,146 cycles

SEAT TRACK ON TOP OF FLOOR BEAM RBL 9 HAS CORROSION SPOTS BETWEEN FS 559 + 80 THRU FS 559 + 96 IN THE CARGO BAY (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED SEAT TRACK IAW CRJ-200 AMM.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,206 hrs · 34,146 cycles

LH SIDEWALL SEAT TRACK STICK 2 REQUIRES FABRICATION (C-CHECK) RO 2/10/2020 FABRICATED NEW SEAT TRACK IAW CRJ-200 REO. PN:20276-288-0-0 TAG: B16466

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 40,206 hrs · 34,146 cycles

RH AISLE SEAT TRACK #1 FS364-409 REQS FAB LOCATE DRILL (C-CHECK) RO 2/10/2020 FABRICATED NEW SEAT TRACK IAW CRJ-200 SRM AND REO.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 40,206 hrs · 34,146 cycles

RH SIDEWALL SEAT TRACK STICK #2 REQUIRES FABRICATION DUE TO CORROSION FS 364-409+16 (C-CHECK) RO 2/10/2020 FABRICATED NEW SEAT TRACK IAW CRJ-200 REO. PN:20276-288-0-0 TAG: B16466

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 40,206 hrs · 34,146 cycles

FLIGHTDECK WINDOW CENTER POST LEFT LOWER ATTACH IS CRACKED VERIFIED BY HFEC (C-CHECK) RO 2/10/2020 REPLACED CRACKED ATTACH FITTING IAW CRJ200 SRM.

Part: SEAT TRACK — CORRODED (BS 499-544) · airframe 40,206 hrs · 34,146 cycles

RH SIDEWALL SEAT TRACK STICK #6 REQUIRES FABRICATION DUE TO CORROSION FS 499+544 1018131 2000/0043 #7568406 (C-CHECK) RO 2/10/2020 FABRICATED NEW SEAT TRACK IAW REO. P/N: 20276-288-0-0 TAG: B16042

Part: SEAT TRACK — CORRODED (BS 559) · airframe 40,206 hrs · 34,146 cycles

RH AISLE SEAT TRACK STICK 4 HAS CORROSION SPOTS BETWEEN FS 559 THRU FS 559+80 IN THE CABIN (C-CHECK) RO 2/10/2020 REMOVED AND INSTALLED NEW SEAT TRACK IAW CRJ-200 AMM.

Part: SEAT TRACK — CORRODED (BS 449) · airframe 40,206 hrs · 34,146 cycles

LH SIDEWALL SEAT TRACK STICK 5 REQUIRES FABRICATION DUE TO CORROSION FS449.85-449 1018131 2000/0049 #756412 (C-CHECK) RO 2/10/2020 FABRICATED LH SIDEWALL SEAT TRACK IAW CRJ-200 SRM AND REO.

Part: ATTACH ANGLE — CRACKED (BS 605) · airframe 40,206 hrs · 34,146 cycles

FLOOR SUPPORT BEAM ATTACH ANGLE BELOW FLOOR EDGE MEMBER FS605.00 CGO DOOR THRESHOLD CRACKED IN RADIUS (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED FLOOR SUPPORT BEAM ATTACH ANGLE AT FS 605 AND LBL 45 IAW CRJ 200 SRM. ADJUSTMENT VERIFICATION C/W ON CP# 20133687 W/O 1018131 8000 0010 SN 7568237

Part: SEAT TRACK — CORRODED (BS 574-605) · airframe 40,206 hrs · 34,146 cycles

SEAT RAIL BEAM AT LBL 27 CORRODED AT FLOOR BOARD LAND FASTENER LOCATIONS FS574.00 TO FS605.00 (C-CHECK) RO 2/10/2020 THE SEAT RAIL BEAM CAP WAS CORRODED AND OUT OF LIMITS. REMOVE AND REPLACED THE WHOLE SEAT RAIL BEAM CAP FROM FS574.00 - FS605.00 IAW CRJ 200 SRM.

Part: ATTACH ANGLE — CRACKED (BS 589) · airframe 40,206 hrs · 34,146 cycles

FLOOR SUPPORT BEAM ATTACH ANGLE BELOW EDGE MEMBER FS589.00 CGO DOOR THRESHOLD CRACKED IN RADIUS (C-CHECK) RO 2/10/2020 REMOVE AND REPLACED FLOOR SUPPORT BEAM ATTACH ANGLE AT FS 589 AND LBL 45 IAW CRJ 200 SRM ADJUSTMENT VERIFICATION C/W ON CP# 20133687 W/O 1018131 8000 0010 SN 7568237

Part: ATTACH FITTING — CORRODED (BS 621) · airframe 40,206 hrs · 34,146 cycles

FLOOR BEAM ATTACHMENT FITTING AT FS 621.00 BULKHEAD RBL 27 OUTB FLOOR BOARD SUPPORT FLANGE HAS CORROSION (C-CHECK) RO 2/10/2020 REPAIRED FLOOR BEAM, FLOOR BOARD SUPPORT ANGLE IAW BOMBA REO.

Part: ATTACH FITTING — CORRODED (BS 621) · airframe 40,206 hrs · 34,146 cycles

LBL 27 FLOOR BEAM ATTACH FITTING AT FS 621.00 BH HAS CORROSION AT 4EA FLOOR BOARD ATTACH NUTPLATES (C-CHECK) RO 2/10/2020 REPAIRED FLOOR BEAM AT FS 621.00 LBL 27 IAW BOMBARDIER REO.

Part: STOP FITTING — CHAFED (E/E BAY DOOR) · airframe 40,206 hrs · 34,146 cycles

FWD E&E BAY DOOR OPENING RH FWD DOOR STOP FITTING IS CHAFED (C-CHECK) RO 2/10/2020 REMOVED AND RE PLACED FWD RH E7E BAY DOOR FITTING IAW CRJ200 SRM/AMM

Part: VERTICAL BEAM — CRACKED (BS 409 BULKHEAD) · airframe 40,206 hrs · 34,146 cycles

VERTICAL BEAM AT RBL 18 AT FS409+128 IS CRACKED AT THE BOTTOM O/B SIDE AGAINST THE PRESSURE BULKHEAD IN THE FWD ECS COMPARTMENT (C-CHECK) RO 2/10/2020 PERFORMED CUT OUT DAMAGE SURFACE , FABRICATED PARTS AND INSTALLED IAW CRJ200 BOMBARDIER REO.

Part: VERTICAL BEAM — CRACKED (BS 409 BULKHEAD) · airframe 40,206 hrs · 34,146 cycles

VERTICAL BEAM AT LBL 27 AT FS409+128 IS CRACKED AT THE BOTTOM I/B SIDE AGAINST THE PRESSURE BULKHEAD IN THE FWD ECS COMPARTMENT (C-CHECK) RO 2/10/2020 PERFORMED CUT OUT DAMAGE FABRICATED PARTS AND INSTALLED IAW CRJ200 BOMBARDIER REO.

Part: VERTICAL BEAM — CRACKED (BS 409 BULKHEAD) · airframe 40,206 hrs · 34,146 cycles

VERTICAL BEAM AT RBL 27 AF FS409+128 IS CRACKED AT THE BOTTOM I/B SIDE AGAINST THE PRESSURE BULKHEAD IN THE FWD ECS COMPARTMENT (C-CHECK) RO 2/10/2020 PERFORMED CUT OUT DAMAGE, FABRICATED PARTS AND INSTALLED IAW CRJ200 BOMBARDIER REO.

Part: DRAG ANGLE — CRACKED (LT MLG WW) · airframe 40,206 hrs · 34,146 cycles

LH WING MLG W/W DRAG ANGLE AT WS 53.60 CRACKED. (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED CRACKED DRAG ANGLE AT WS 53.6 IAW CRJ 200 SRM.

Part: ATTACH BRACKET — CRACKED (LT WING MLG WW) · airframe 40,206 hrs · 34,146 cycles

LH MLG W/W HYDRAULIC PRESSURE TRANSDUCER ATTACH BRACKET AT LWR SURFACE OF PRESSURE FLOOR SKIN, BROKEN. (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED ATTACH BRACKET FOR PRESSURE TANSDUCER LH MLG W/W IAW CRJ200 SRM. P/N:MS20470AD5-6 TAG:B15674. P/N:601R75262-159 TAG:B20991

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 40,206 hrs · 34,146 cycles

RH WING AUX SPAR AREA IN MLG W/W WS48.0, INTERCOSTAL ATTACH ANGLE COMMON TO WING PLANK CRACKED. (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED ATTACH ANGLE IAW CRJ-200 SRM. P/#: 600-10204-28 / T/#: B21305

Part: ATTACH BRACKET — CRACKED (RT MLG WW) · airframe 40,206 hrs · 34,146 cycles

RH MLG W/W HYDRAULIC PRESSURE TRANSDUCER ATTACH BRACKET AT LWR SURFACE OF PRESSURE FLOOR SKIN, BROKEN. (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED ATTACH BRACKET FOR PRESSURE TRANSDUCER RH MLG W/W IAW CRJ200 SRM. P/N:MS20470AD5-6 TAG:B15674 P/N:601R75262-157 TAG:B90691

Part: DRAG ANGLE — CRACKED (RT WING) · airframe 40,206 hrs · 34,146 cycles

RH WING AUX SPAR INBD DRAG ANGLE CRACKED. (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED DRAG ANGLE IAW CRJ-200 SRM. P/#: 600-10389-2S T/#: B21306

Part: RIB — CRACKED (LT WING MLG WW) · airframe 40,206 hrs · 34,146 cycles

LH MLG W/W AUX SPAR AREA SUPPORT RIB AT WS 58.88 CRACKED. (C-CHECK) RO 2/10/2020 REPAIRED SUPPORT RIB AT WS53.60 IAW REO.

Part: RIB — CRACKED (RT MLG WW) · airframe 40,206 hrs · 34,146 cycles

RH MLG W/W AUX SPAR AREA SUPPORT RIB AT WS 58.88 CRACKED. (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED BATT RIB IAW CRJ-200 SRM 51-42-21 AND SRM. P/#: HST11AG5-4 T/#: A8479. P/#: HST11AG5-3 T/#: B11376. P/#: KFN587-08 T/#: A85270. P/#: MS20470AD5-5 T/#: B21179. P/#: MS20470AD5-6 T/#: B15674

Part: FLOORBEAM — CRACKED (BS 280) · airframe 40,206 hrs · 34,146 cycles

ANGLE CLIP IS CRACKED ON THE AFT OF BEAM 280 AND O/B SIDE OF RBL 9, IN THE CABIN BELOW THE FLOOR. (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED CRACKED CLIP IAW CRJ-200 SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 40,206 hrs · 34,146 cycles

ANGLE CLIP IS CRACKED ON THE AFT SIDE OF BEAM 280 AND O/B SIDE OF LBL 9, IN THE CABIN BELOW THE FLOOR (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED CRACKED CLIP IAW CRJ-200 SRM.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 40,206 hrs · 34,146 cycles

RH SIDEWALL SEAT TRACK STICK 5 HAS CORROSION SPOTS BETWEEN FS 449.85 THRU FS 499, IN THE CABIN. (C-CHECK) RO 2/10/2020 REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW CRJ-200 AMM.

Part: VERTICAL BEAM — CRACKED (BS 409 BULKHEAD) · airframe 40,206 hrs · 34,146 cycles

VERTICAL BEAM AT LBL 9 AT FS 409+128 IS CRACKED AT THE BOTTOM I/B SIDE AGAINST THE PRESSURE BULKHEAD, IN THE FWD ECS COMPARTMENT. (C-CHECK) RO 2/10/2020 REPAIRED FS 409+128 I/B LBL 9 VERTICAL POST IAW BOMBARDIER REO.

Part: SEAT TRACK — CORRODED (BS 544-559) · airframe 40,206 hrs · 34,146 cycles

LH SIDEWALL SEAT TRACK STICK 7 HAS CORROSION SPOTS BETWEEN FS 544 THRU FS 559+80, IN THE CABIN. (C-CHECK) RO 2/10/2020 REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW CRJ-200 AMM.

Part: SEAT TRACK — CORRODED (BS 499-544) · airframe 40,206 hrs · 34,146 cycles

RH SIDEWALL SEAT TRACK STICK 6 HAS CORROSION SPOTS BETWEEN FS 499 THRU FS 544, IN THE CABIN. (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 AMM.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 40,206 hrs · 34,146 cycles

RH SIDEWALL SEAT TRACK STICK 2 HAS CORROSION SPOTS BETWEEN FS 364 THRU FS 409+16, IN THE CABIN. (C-CHECK) RO 2/10/2020 REMOVED CORROSION SIDEWALL SEAT TRACK AND INSTALLED NEW SIDEWALL SEAT TRACK IAW CRJ-200 AMM.

Part: SEAT TRACK — CORRODED (BS 499-544) · airframe 40,206 hrs · 34,146 cycles

LH SIDEWALL SEAT TRACK STICK 6 HAS CORROSION SPOTS BETWEEN FS 499 THRU FS 544, IN THE CABIN. (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED SEAT TRACK IAW CRJ-200 AMM. P/#: 20276-288-0-0 T/#: B16042

Part: BEAM — CRACKED (BS 409) · airframe 40,206 hrs · 34,146 cycles

VERTICAL BEAM AT LBL 18 AT FS 409+128 IS CRACKED AT THE BOTTOM O/B SIDE AGAINST THE PORESSURE BULKHEAD, IN THE FWD ECS COMPARTMENT. (C-CHECK) RO 2/10/2020 PERFORMED CUT- OUT DAMAGE ,FABRICATED AND INSTALLED RAPAIR PARTS IAW CRJ200 BOBARDIER REO.

Part: SEAT TRACK — CORRODED (BS 406-409) · airframe 40,206 hrs · 34,146 cycles

RH SIDEWALL SEAT TRACK STICK 3 HAS CORROSION SPOTS BETWEEN FS 406+16 THRU FS 409+112, IN THE CABIN. (C-CHECK) RO 2/10/2020 REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW CRJ-200 AMM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 40,206 hrs · 34,146 cycles

ANGLE CLIP IS CRACKED ON THE AFT SIDE OF BEAM 280 AND I/B SIDE OF RBL 9, IN THE CABIN BELOW THE FLOOR. (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED CRACKED CLIP IAW CRJ-200 SRM.

Part: SEAT TRACK — CORRODED (BS 549-559) · airframe 40,206 hrs · 34,146 cycles

RH SIDEWALL SEAT TRACK STICK 7 HAS CORROSION SPOTS BETWEEN FS 549 THRU FS 559+80, IN THE CABIN. (C-CHECK) RO 2/10/2020 REMOVED AND INSTALLED NEW SEAT TRACK IAW CRJ-200 AMM.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 40,206 hrs · 34,146 cycles

RH SIDEWALL SEAT TRACK STICK 4 HAS CORROSION SPOTS BETWEEN FS 409+112 THRU FS 449.85, IN THE CABIN. (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED SIDEWALL SEAT TRACK IAW CRJ 200 AMM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 40,206 hrs · 34,146 cycles

FLOOR ANGLE STRIP ON THE FWD SIDE OF BEAM 280 IS CRACKED JUST I/B OF LBL 12, IN THE VERY FWD E&E BAY. (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED CRACKED ANGLE IAW CRJ-200 SRM.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 40,206 hrs · 34,146 cycles

LH SIDEWALL SEAT TRACK STICK 2 HAS CORROSION SPOTS BETWEEN FS 364 THRU FS 409+16, IN THE CABIN. (C-CHECK) RO 2/10/2020 REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW CRJ-200 AMM.

Part: STRAP — CORRODED (BS 559 FLOORBEAM) · airframe 40,206 hrs · 34,146 cycles

FLOOR STRAP AT FS 559 HAS CORROSION BETWEEN RBL 27 THRU THE RH FLOOR SILL, IN THE CABIN. (C-CHECK) RO 2/10/2020 REMOVED AND INSTALLED FABRICATED STRAP IAW CRJ-200 SRM.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 40,206 hrs · 34,146 cycles

LH SIDEWALL SEAT TRACK STICK 5 HAS CORROSION SPOTS BETWEEN FS 449.85 THRU FS 499, IN THE CABIN. (C-CHECK) RO 2/10/2020 REMOVE AND REPLACED THE CORRODED SEAT TRACK WITH A NEW ONE IAW CRJ 200 AMM. P/N SH670-33425-3 TAG # B14589

Part: SEAT TRACK — CORRODED (BS 406-409) · airframe 40,206 hrs · 34,146 cycles

LH SIDEWALL SEAT TRACK STICK 3 HAS CORROSION SPOTS BETWEEN FS 406+16 THRU FS 409+112, IN THE CABIN. (C-CHECK) RO 2/10/2020 REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW CRJ-200 AMM.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 40,206 hrs · 34,146 cycles

RH AISLE SEAT TRACK STICK 1 HAS CORROSION SPOTS BETWEEN FS 364 THRU FS 409, IN THE CABIN. (C-CHECK) RO 2/10/2020 REMOVED CORRODED SEAT TRACK AND FABRICATED AND INSTALLED NEW SEAT TRACK AND INSTALLED IAW CRJ-200 AMM.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 40,206 hrs · 34,146 cycles

SERVICE DOOR OPENING LOWER SILL LOWER LONGERON ANGLE STRIP HAS CORROSION SPOTS BETWEEN FS 319.70 THRU FS 349. (C-CHECK) RO 2/10/2020 REPLACED SERVICE DOOR LOWER SILL ANGLE IAW CRJ200 SRM. P/N-CR3523-5-3 TAG#A79034 P/N-CR3523-5-3 TAG#A84833 P/N-CR3522-5-3 TAG#A83951 P/N-CR3523-5-3 TAG#A84833 P/N-CR3522-5-4 TAG#A83069 P/N-601R-38303-253 TAG#B21493 P/N: AN3H10A TAG:B14970 T/W: AAR527961 CAL DD: 10/02/220

Part: SEAT TRACK — CORRODED (BS 406-449) · airframe 40,206 hrs · 34,146 cycles

LH SIDEWALL SEAT TRACK STICK 4 HAS CORROSION SPOTS BETWEEN FS 406+112 THRU FS 449.85, IN THE CABIN (C-CHECK) RO 2/10/2020 REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW CRJ-200 AMM.

Part: BEAM — CHAFED (RT WING TE FLAP) · airframe 40,206 hrs · 34,146 cycles

RH INBD FLAP VANE INBD ACTUATOR SLIDING BEAM CHROME SURFACE CHAFED BY CONTACT WITH ROLLER. (C-CHECK) RO 2/10/2020 RMEOVED AND REPLACED RH IB FLAP ASSY IAW CRJ200 AMM. RIG AND OPS C/W ON CP# 20005908 W/O 1018130 6000 0011 AND CP# 20005909 W/O 1018130 6000 0012. / T/W: AAR531355 CAL DD: 11/01/2020.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 40,206 hrs · 34,146 cycles

BEAM 280 PREVIOUS REPAIR IS CRACKED AND HAS A BROKEN-OFF RIVIT HEAD ALONG THE UPPER AFT SIDE JUST O/B OF RBL 9, IN THE CABIN BELOW THE FLOOR. (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED CRACKED REPAIR ANGLE IAW BOMBARDIER GREO.

Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 40,206 hrs · 34,146 cycles

RT FLIGHT SPOILER LOWER SURFACE DELAMINATED (C-CHECK) RO 2/10/2020 REPAIRED R/H FLIGHT SPOILER LOWER SURFACE DELAM IAW REO. OPS TEST GOOD IAW CRJ200 AMM. T/W 519954 CAL DD: 05-09-2020 P/N: AN320C6 TAG: A85081 P/N: MS17825-6 TAG: B21406 PN/: MS17825-5 TAG: A85957 P/N: NAS1518F3R4 TAG: B23104 P/N: R30B18 TAG: B21891

Part: ANGLE — CRACKED (EXT SERVCE PANEL) · airframe 40,206 hrs · 34,146 cycles

EXTERNAL SERVICE PANEL HAS CRACKED CLIP (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED CLIP IAW CRJ-200 SRM. P/#: 601R33003-19 T/#: B20799

Part: ATTACH BRACKET — CRACKED (RT WING-BODY) · airframe 40,206 hrs · 34,146 cycles

RT WING OVER THE WING FAIRING ATTACH BRACKET CRACKED AT FS 461 (C-CHECK) RO 2/10/2020 REMOVED DAMAGED BRACKET, FABRICATED AND INSTALLED NEW BRACKET IAW CRJ 200 SRM.

Part: ATTACH BRACKET — CRACKED (RT WING-BODY) · airframe 40,206 hrs · 34,146 cycles

RT WING OVER THE WING FAIRING ATTACH BRACKET CRACKED AT FS 473.15 (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED RH WING FAIRING ATTACH BRACKET IAW CRJ 200 SRM.

Part: SKIN — CRACKED (LT WING LE) · airframe 40,206 hrs · 34,146 cycles

LEFT WING O/B L/E CRACKED IN MIDDLE OF FWD FACE (C-CHECK) RO 2/10/2020 REPAIRED LEFT WING O/B L/E IAW REO.

Part: FRAME — CORRODED (BS 333) · airframe 40,206 hrs · 34,146 cycles

FRAME 333 HAS CORROSION SPOTS ON THE FWD SIDE BETWEEN STGR 23R THRU 22R IN THE FWD E&E BAY (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED FRAME STATION 333 FROM THE SERVICE DOOR THRESHOLD IAW CRJ-200 SRM. 601R32004-795 TAG BB5202

Part: TRUNNION — DAMAGED (MLG) · airframe 40,206 hrs · 34,146 cycles

COMPLY WITH: 601R-57-046 - WINGS - CENTER WING PRIMARY STRUCTURE - COLD WORKING OF FASTENER HOLES IN THE MAIN LANDING GEAR (MLG) TRUNNION FITTING REV C PART(S) A, B (C-CHECK) RO 2/10/2020 COMPLIED WITH WINGS - CENTER WING PRIMARY STRUCTURE - COLD WORKING OF FASTENER HOLES IN THE MAIN LANDING GEAR (MLG) TRUNNION FITTING REV C PART(S) A, B AND REO.

Part: ISOLATOR — BROKEN (FUSELAGE) · airframe 35,664 hrs · 30,182 cycles

BULKHEAD FACE HAS BROKEN ISOLATORS. (C-CHECK) RO: 1/17/2018. REPLACED ISOLATORS IAW SRM.

Part: UPLOCK ACTUATOR — FAILED (RT MLG) · airframe 32,720 hrs · 27,474 cycles

GEAR DISAGREE. RT MLG WOULD NOT RETRACT. FLT 5166, REPLACED THE RT MLG UPLOCK ACTUATOR IAW AMM. OPS CHECK GOOD.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 32,720 hrs · 27,474 cycles

GEAR DISAGREE, NLG WILL NOT RETRACT. FLUSHED THE HYD SYSTEM, REMOVED AND REPLACED FREE FALL HANDLE. REPLACED THE NLG CENTERED/EXTEND PROXIMITY SENSOR AND BRACKET IAW AMM.

Part: BULKHEAD — CRACKED (BS 202) · airframe 27,939 hrs · 23,200 cycles

FWD PRESSURE BULKHEAD CRACKED WHERE PARKING BRAKE CABLE GOES THROUGH. REPAIRED FWD PRESSURE BULKHEAD AT BS 202.75 BL 23.71 WITH REINFORCEMENT DOUBLERS IAW REO.

Part: CONTROL HANDLE — MALFUNCTIONED (MLG) · airframe 27,214 hrs · 22,658 cycles

AFTER TAKEOFF ON GEAR LEVER RETRACTION RECEIVED A/SKID INBD AND PARK BRAKE SHUTOFF VALVE CAUTION MESSAGES. GEAR DID NOT RETRACT. CYCLED GEAR NUMEROUS TIME WITH NO EFFECT. QRH DIRECTED RECYCLING PARK BRAKE WITH NO EFFECT. REPLACED LANDING GEAR CONTROL HANDLE IAW AMM.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 27,171 hrs · 22,630 cycles

BULB INSIDE THE EMERGENCY EXIT SIGN AT GALLEY SERVICE DOOR IS BURNED OUT, REPLACED THE BULB.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,106 hrs · 22,575 cycles

EXTERIOR LEFT AFT EMERGENCY LIGHT IS BURNED OUT. REPLACED THE LAMP IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 26,971 hrs · 22,463 cycles

LEFT FUSELAGE MOST AFT EMERGENCY LIGHT IS BURNED OUT. REPLACED LAMP.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 26,927 hrs · 22,422 cycles

SERVICE DOOR EMERGENCY EXIT LIGHT IS BURNED OUT. REPLACED LAMP.

Part: DOOR SILL — CORRODED (CARGO DOORWAY) · airframe 27,163 hrs · 22,625 cycles

AFT FUSE, CARGO DOOR SILL PLATE HAS CORROSION THRU THE NUTPLATES. C-CHECK. REMOVED CORRODED DOOR SILL PLATE AND INSTALLED A SERVICEABLE CARGO DOOR SILL PLATE IAW REO.

Part: STRUCTURE — MECHANIC ERROR (BS 621) · airframe 27,163 hrs · 22,625 cycles

DURING REMOVAL OF FS 621 FIREBLOCK, FOUND A DRILL START ADJACENT TO FASTENER HOLE AT LBL 33.75, WL .126 APPROX .023" DEEP. C-CHECK. REPAIRED FS 621.00 BULKHEAD WEB BETWEEN LBL 27.50 AND LBL 36.20 IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 27,163 hrs · 22,625 cycles

RIGHT AILERON UPPER L/E CHAFED IN NUMEROUS AREAS APPROXIMATELY .020" DEEP. C-CHECK. R & R UPPER LEADING EDGE SKIN4 IAW SRM.

Part: SKIN — CHAFED (LT AILERON) · airframe 27,163 hrs · 22,625 cycles

LEFT AILERON UPPER L/E CHAFED IN NUMEROUS AREAS APPROXIMATELY .015" DEEP. C-CHECK. R & R UPPER L/E SKIN IAW SRM.

Part: STIFFENER — CRACKED (BS 409) · airframe 27,163 hrs · 22,625 cycles

FOUND FS 409.00 + 128 VERTICAL POST LBL 18.0, OTBD SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS APPROX .300" LONG, 50 PERCENT FSH. C-CHECK FILE NR 2014NM060066. REMOVED OTBD SIDE STIFFENER FROM FS 409.00 + 128 LBL 18.0 VERTICAL POST AND INSTALLED NEW SERVICEABLE STIFFENER IAW REO.

Part: STIFFENER — CRACKED (BS 409) · airframe 27,163 hrs · 22,625 cycles

FOUND FS 409.00 + 128 VERTICAL POST AT BL0.0 LT AND RT SIDES HAS INDICATIONS NOTED AT AFT FLANGE RADIUS APPROXIMATELY .300" LONG 70 PERCENT FSH. C-CHECK FILE NR 2014NM060066. INSTALLED VERTICAL POST AT FS 409 + 128 BLO IAW SRM REO. LOCATED AND DRILLED NEW ANGLES -131 AND -132 IAW SRM. FABRICATED NEW WEB PN 601R32208-41 IAW SAMPLE AND SRM.

Part: POST — CRACKED (BS 409) · airframe 26,883 hrs · 22,386 cycles

BS 409.00+128 VERTICAL POST, LBL 18.0 OTBD SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS APPROXIMATELY .300 INCH LONG, 50 PERCENT FSH. C-CHECK, REPLACED STIFFENER IAW REO AND SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,826 hrs · 22,344 cycles

EMERGENCY EXIT LIGHTS ARE BURNED OUT. FLT 6415 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,342 hrs · 21,973 cycles

EMERGENCY LIGHT POD NR 3 IS BURNED OUT. FLT 6237 RELAMPED.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 25,742 hrs · 21,516 cycles

AFTER GEAR DOWN FOR LANDING, BEGAN TO SMELL A BURNED RUBBER TYPE SMELL IN FLT DECK & IN CABIN. FLT#5526 INSPECTED AFT EQUIPMENT BAY & AVIONICS BAY FOR ANY DEFECTS, NONE FOUND.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,607 hrs · 21,399 cycles

NR 2 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#6340 RELAMPED.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 25,590 hrs · 21,387 cycles

AUTOPILOT UNCOMMANDED EVENT CLIMBING IN SPEED MODE BUGGED TO 265 UNCOMMANDED CHANGE TO IAS 40. ACFT PITCHED UP TO 1800 FPM CLIMB. AUTOPILOT OPERATED NORMALLY REMAINDER OF FLIGHT. FLT 5496 NO FAULT FOUND. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,530 hrs · 21,347 cycles

AFT EMERGENCY LIGHT BURNED OUT. FLT#5319 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,530 hrs · 21,347 cycles

EXTERIOR EMERGENCY LIGHT BURNED OUT. FLT#6285 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,440 hrs · 21,267 cycles

EMERGENCY OVERHEAD LIGHTS BURNED OUT. FLT#6315 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,710 hrs · 20,696 cycles

EMERGENCY EXIT LIGHT NEXT TO GALLEY SERVICE DOOR IS BURNED OUT, RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,060 hrs · 19,417 cycles

TWO EMERGENCY EXIT LIGHT BULBS ON BULKHEAD NEXT TO MAIN CABIN DOOR INOPERATIVE. (FLT 5253) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,236 hrs · 18,790 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6245) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,868 hrs · 18,479 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6199) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,563 hrs · 18,226 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 10 IS OUT. (FLT 6453) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,383 hrs · 18,072 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5498) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,180 hrs · 17,921 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5500) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,848 hrs · 17,643 cycles

FIRST OVERHEAD EMERGENCY LIGHT DOES NOT ILLUMINATE. (FLT 5544) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,848 hrs · 17,643 cycles

AFT CEILING EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,791 hrs · 17,595 cycles

NR 3 OVERHEAD EMERGENCY LIGHT BURNT OUT. (FLT 5644) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,383 hrs · 17,294 cycles

AFT 2 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 6375) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,239 hrs · 17,172 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5631) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,173 hrs · 17,119 cycles

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

Part: MOUNT — CORRODED (LT ENGINE) · airframe 19,880 hrs · 16,891 cycles

LEFT ENGINE FORWARD YOKE MOUNT BEARINGS ARE CORRODED. (ENGINE CHANGE) INSTALLED A SERVICEABLE FORWARD YOKE MOUNT ASSEMBLY ON THE LEFT ENGINE DURING THE ENGINE CHANGE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,825 hrs · 16,847 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,778 hrs · 16,813 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5845) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,683 hrs · 15,953 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6314) RELAMPED EMERGENCY LIGHT.

Part: CARBON SEAL — DEFECTIVE (RT ENGINE) · airframe 18,620 hrs · 15,905 cycles

SMOKE TOILET CAUTION MESSAGE. (FLT 6954) REPLACED NR 1 CARBON SEAL ON THE RIGHT ENGINE.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 18,442 hrs · 15,766 cycles

RIGHT PACK CAUSES SMOKE IN CABIN. (FLT 7010) REPLACED RIGHT AIR CYCLE MACHINE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,639 hrs · 15,921 cycles

FS 559.0 PRESSURE BULKHEAD CRACKED AT LEFTSIDE CAP ANGLE RADIUS. (C-CHECK) REPAIRED PER REO.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 18,330 hrs · 15,673 cycles

FUSELAGE SKIN DAMAGE NEAR RIGHT STATIC PORT. (C-CHECK) REPAIR PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,109 hrs · 15,484 cycles

FIRST OVERHEAD EMERGENCY LIGHT OUT. (FLT 6666) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,035 hrs · 14,618 cycles

NR 3 CABIN EMERGENCY CEILING LIGHT INOP. (FLT 6746) RELAMPED EMERGENCY LIGHT.

Part: DOOR — BINDS (CABIN) · airframe 16,917 hrs · 14,524 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN FROM OUTSIDE. (FLT 6029) OPERATIONAL CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,741 hrs · 14,364 cycles

EMERGENCY EXIT LIGHT OUTSIDE OF MAIN CABIN DOOR INOP. (FLT 6370) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,741 hrs · 14,364 cycles

NR 1 CEILING EMERGENCY LIGHT INOP. (FLT 6345) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — DIRTY (FIRE BOTTLE) · airframe 16,694 hrs · 14,328 cycles

CARGO BTL LO CAUTION MESSAGE AT CRUISE. (FLT 6238) CLEANED AND RE-SECURED BOTTLE CONNECTORS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,283 hrs · 13,973 cycles

NR 3 OVERHEAD FLOOD EMERGENCY LIGHT INOP. (FLT 5850)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,077 hrs · 13,787 cycles

EMERGENCY CEILING LIGHT AT ROW 2 INOP. (FLT 6576) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,644 hrs · 13,441 cycles

NR 3 CEILING EMERGENCY LIGHT INOP. (FLT 6479) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,251 hrs · 13,113 cycles

OVERHEAD EMERGENCY CEILING LIGHT NR 3 INOP. (FLT 6394) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — BROKEN (CABIN) · airframe 14,718 hrs · 12,670 cycles

EMERGENCY EXIT LIGHT AT SERVICE DOOR BROKEN. (FLT 6518) REPLACED SIGN.

Part: ROD — OUT OF POSITION (LT COWLING) · airframe 14,718 hrs · 12,670 cycles

LEFT THRUST LEVER JAMMED AFTER TAKEOFF. (FLT 6005) RESTOWED LEFT CORE COWL HOLD OPEN ROD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,090 hrs · 12,200 cycles

CABIN CEILING EMERGENCY LIGHT INOP. (FLT 5855) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 13,975 hrs · 12,105 cycles

FS280 BULKHEAD GOUGED. (C CHECK)REPAIRED PER REO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 13,975 hrs · 12,105 cycles

FS280 ANGLE CRACKED. (C CHECK)REPAIRED PER REO.

Part: SILL — CORRODED (FUSELAGE) · airframe 13,975 hrs · 12,105 cycles

SERVICE DOOR SILL CORRODED. (C CHECK)REPLACED PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 13,975 hrs · 12,105 cycles

FS280 WEB CRACKED. (C CHECK)REPAIRED PER REO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 13,975 hrs · 12,105 cycles

FLOOR SUPPORT ANGLES CRACKED. (C CHECK)REPAIRED PER SRM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 13,064 hrs · 11,416 cycles

FLT 5862 - NR 1 CEILING EMERGENCY LIGHT INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,597 hrs · 11,046 cycles

FLT 6717 - EMERGENCY OVERHEAD LIGHT, SECOND FORM AFT, INOP. RELAMPED.

Part: BRACKET — OUT OF ADJUST (NLG) · airframe 10,303 hrs · 9,042 cycles

FLT 6384 - RECEIVED A "GEAR DISAGREE" WARNING MESSAGE AND NOSE GEAR DID NOT RETRACT. ADJUSTED THE NOSE WHEEL WEIGHT OFF WHEELS SENSOR BRACKET. OPS CHECK GOOD.

Part: BRACKET — CRACKED (TRANSDUCER) · airframe 9,251 hrs · 8,142 cycles

BRAKE TRANSDUCER IN RIGHT WHEEL WELL IS CRACKED, FOUND AT C-CHECK. INSTALLED BRAKE TRANSDUCER BRACKET PER CRJ200 SRM PGS 4-14.

Part: BRACKET — CRACKED (LT WW) · airframe 9,251 hrs · 8,142 cycles

BRAKE TRANSDUCER IN LEFT WHEEL WELL IS CRACKED, FOUND AT C-CHECK. INSTALLED BRAKE TRANSDUCER BRACKET PER CRJ200 SRM 51-42-06 PG 1-18.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 8,543 hrs · 7,553 cycles

ON GEAR EXTENSION, RECEIVED GEAR DISAGREE MESSAGE. CYCLED GEAR AND NORMAL INDICATIONS APPEARED, FLIGHT NR 5953. REPLACED LANDING GEAR SELECTOR VALVE IAW 32-33-10. GEAR SWING OPS CHECK GOOD AND VALVE LEAK CHECK GOOD.

Part: DOOR — MISSING (RT MLG) · airframe 6,923 hrs · 6,072 cycles

ON POST FLIGHT, DISCOVERED RIGHT MAIN GEAR DOOR MISSING. REPLACED RIGHT MLG DOOR IAW CRJ 200 MM 32-12-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,606 hrs · 4,955 cycles

OVERHEAD EMERGENCY LIGHT A BEAM ROW 5 INOP. RELAMPED REF 33-50-00. OPERATIONAL CHECKS GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 4,779 hrs · 4,199 cycles

EMERGENCY OVERHEAD CABIN LIGHT OUT. REPLACED CABIN OVERHEAD EMERGENCY LAMP. OPERATIONAL CHECK GOOD.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 4,574 hrs · 4,005 cycles

FOUND CARGO COMPARTMENT FS 621 LT FLOOR SUPPORT ANGLE LBL 41 CRACKED. REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV C.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 4,111 hrs · 3,620 cycles

LEFT SPOILERON STATUS MSG. REPLACED NR 3 OUTBOARD SPOILERON PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD.

Part: CONTROL LEVER — MALFUNCTIONED (TE FLAPS) · airframe 3,906 hrs · 3,426 cycles

FLAPS FAIL CAUTION; FLAPS STUCK AT 30 DEGREES. REPLACED FLAP CONTROL LEVER IAW CRJ MM 27-51-01. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 2,559 hrs · 2,264 cycles

AP PITCH TRIM MESSAGE DISPLAYED NUMEROUS TIMES DURING FLIGHT. REPLACED HSTA AND MCU IAW CRJ MM 27-42-01 AND 27-42-05. OPS CHECK GOOD, PN: 7062-3 SN OFF: 1296.

Part: CONTROL SYSTEM — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 2,523 hrs · 2,230 cycles

AP PITCH TRIM CAUTION MSG IN FLIGHT. REPLACED HSTCU WITH AS SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.

Part: SWITCH — STUCK (TRIM) · airframe 1,863 hrs · 1,659 cycles

REMOVE AND REPLACE F/O'S TRIM SWITCH DUE TO COMPLAINT OF STICKING. REPLACED F/O TRIM SWITCH AS REQUIRED PER CRJ MM 27-41-05. OPERATIONAL CHECK GOOD.

Part: SMOKE — DETECTED (COCKPIT) · airframe 1,519 hrs · 1,341 cycles

ON TAXI IN/PARKING AT GATE TRANSFERRED BLEEDS TO APU AND SMOKE BEGAN FILLING COCKPIT AND CABIN. PURGED CABIN AND COCKPIT OF SMOKE. OPERATED BOTH PACKS FOR 20 MINUTES. COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK GOOD.

Part: SWITCH — INOPERATIVE (AILERON TRIM) · airframe 834 hrs · 776 cycles

AILERON TRIM SWITCH INOPERATIVE. REPLACED AILERON TRIM/RUDDER TRIM PANEL WITH SERVICEABLE UNIT. ALL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 435 hrs · 371 cycles

MACH TRIM WILL NOT ENGAGE. REPLACED HORIZONTAL STAB TRIM CONTROL UNIT IAW CRJ MM 27-41-01, OPERATIONAL CHECK GOOD.