N965SW

Part: RIVET — DAMAGED (ZONE 200) · airframe 48,421 hrs · 41,996 cycles

FS 654.50 FRAME SPLICE AT STGR 6L HAS A RIVET HEAD POPPED OFF, POSSIBLE CORROSION (FILED CLOSED)COMPLIED WITH REO 601R-53-61-8415 REV. -, TEMPORARY REPAIR FOR BLENDED CORROSION DAMAGE TO LH & UPPER FRAME SECTORS AT FS654.50 BETWEEN STR5L - STR7L. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: FRAME SPLICE — DAMAGED (ZONE 200) · airframe 48,416 hrs · 41,991 cycles

FS654.50 FRAME SPLICE AT STGR 6L HAS A RIVET HEAD POPPED OFF/POSSIBLE CORROSION (OPEN)

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 48,421 hrs · 41,996 cycles

INTERCOSTAL LOCATED AT LT STGR 4 BETWEEN FRAMES AT FS654.50 AND FS672.20 IS CRACKED AT THE FWD LWR CORNER. REMOVED AND REPLACED INTERCOSTAL LOCATED AT LH STGR 4 BETWEEN FRAMES AT FS654.50 AND FS672.20 IN REFERENCE TO CRJ 200 SRM 51-42-06 ALSO COMPLIED WITH REO 601R-53-61-8414 REV. - DATED 2025-11-07 REPAIR FOR OVERSIZED RIVET HOLE TO STRINGER 4L BETWEEN FS654.50 - FS672.20. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: WARNING MESSAGE — ILLUMINATED (ZONE 200) · airframe 47,387 hrs · 40,911 cycles

ON DECENT RECIEVED EFIS COMP MON WITH IAS ON BOTH PFDS RAN QRH AND MSGS PERSISTEDCAPT SIDE GOT AN IAS FLAG, PITCH AND ROLL FLAG. FO SIDE GOT AN IAS FLAG, PITCH AND ROLL AND ALTITUDE FLAG. CAPT SIDE WAS COMING BACK BUT FO STILL HAD ALL THE FLAGS. DIVERED TO LAS, DECLARED EMERGENCY (DID NOT DROP OPXY MASKS) AND DID NOT LAND OVERWEIGHT. (FLIGHT 4663 - FILED CLOSED)INTERROGATED MDC FOR EFIS COMP MON PER FIM 34-22-00. NO FAULTS IN CURRENT OR FAULT HISTORY. FOR IAS FLAG, PITCH AND ROLL AND ALTITUDE FLAG, INTERROGATED MDC PER FIM 34-13-00 AND FOUND ADC 2 VAR CIRCUITRY. REMOVED AND REPLACED ADC #2 PER AMM 34-13-01. PERFORMED LEAK CHECK OF P1 AND PILOT€™S S1/COPILOT€™S S2 SYSTEM PER AMM 34-11-00. LEAK CHECK GOOD. COULD FIND NO OTHER FAULTS NOR DUPLICATE. PERFORMED CATII RETURN TO SERVICE TEST. AIRCRAFT REMAINS CATII. AIRCRAFT REMAINS RVSM.DRUCK ADTS553FSN 12933055CAL DUE 2/26

Part: SKIN — DAMAGED (ZONE 200) · airframe 47,162 hrs · 40,662 cycles

LIGHTNING STRIKE DAMAGE FOUND TO FUSELAGE SKIN BETWEEN FS625.30 AND FS654.50 AND BETWEEN STGR3R AND STGR5R. THIS REPAIR WILL BE CONSIDERED A MAJOR REPAIR PER GMM 3-26 (FILED CLOSED) COMPLIED WITH PERMANENT REPAIR ON FUSELAGE SKIN BETWEEN FS625.30 AND FS654.50 AND BETWEEN STGR3R AND STGR5R IN REFERENCE TO REO 601R-53-61-8287 REV -- DATED 2025-02-13. ALSO COMPLIED WITH TASK CARD 51-900-1003-SKY. FORM M-337 COMPLETED. **MAJOR REPAIR**

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 700) · airframe 46,927 hrs · 40,410 cycles

D: GEAR DISAGREE WARNING MESSAGE ON DEPARTURE FROM GJT.C: MEL 32-30-1CAT A DUE DATE IS 12/17/2024GEAR DISAGREE WARNING MESSAGE ON DEPARTURE FROM GJT. ON TAKEOFF UPON SELECTING GEAR UP, THE WARNING MESSAGE APPEARED. BARBER POLE NOTICED ON THE NOSE WITH BUFFETING, ALSO 2 YELLOW MAIN GEAR INDICATIONS. UPON LEVEL OFF GEAR WENT TO THE UP INDICATION AFTER HAVING PUMPS 2B AND 3B ON FOR MORE THAN 2 MINUTES. CONTINUED THE FLIGHT TO DENVER AND EXTENDED LANDING GEAR WITH NO ISSUES. (FLIGHT 4635 - FILED CLOSED) DEC 16, 2024 STATION: DEN--BEGAN TROUBLESHOOTING PER CRJ 200 FIM 32-60-07-01. FOUND NO CODES LOGGED IN THE PSEU. PERFORMED GVI OF NLG AND MLG AREAS. NO OBVIOUS DEFECTS NOTED AT THIS TIME. DEFERRED LANDING GEAR RETRACTION SYSTEM PER CRJ 200 MEL 32-30-1. ALL MX PROCEDURES COMPLIED WITH AT THIS TIME. GEAR PINS INSTALLED. CAT II STATUS DOWNGRADED AT THIS TIME. PLEASE REFERENCE AML 1493831 FOR FDR DOWNLOAD.

Part: FLAP SYSTEM — FAILED · airframe 46,210 hrs · 39,665 cycles

DUE TO FLAP FAIL AT CRUISE, COMPLY WITH FULL FLAP EVAULATION IN REF TO FIM CH 27 AND AD 2009-12-12C:MCICAT A DUE BY TAC: 39675. SMOD APPROVAL REQIRED FOR RTS. FLAP FAIL AT 15000 FT - FLAPS STUCK AT 0 DEGREES DIVERTED TO CMH. RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10 COMPLIANCE FORM. OK TO CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES. COMPLIED WITH IN ACCORDANCE WITH FIM FMRP CHAPTER 27 RESET PROCEDURES AND AD 2009-06-12 TRACKING CREATED FOR FULL AD COMPLIANCE BY MCC

Part: DUCT — WARNING MESSAGE (ANTI-ICE) · airframe 45,461 hrs · 38,835 cycles

ANTI-ICE DUCT WARNING MESSAGE DURING CLIMB. RAN QRH. MESSAGE DID NOT CLEAR ENTIRE FLIGHT. (FLIGHT 6942 FILED OPEN) PLEASE REFERENCE AML 1285266THIS IS CURRENTLY A WORK IN PROGRESS.

Part: ANTI-ICE SYSTEM — WARNING MESSAGE · airframe 45,472 hrs · 38,845 cycles

ANTI-ICE DUCT WARNING MESSAGE DURING CLIMB. RAN QRH. MESSAGE DID NOT CLEAR ENTIRE FLIGHT. (FLIGHT 6942 FILED CLOSED)TROUBLE SHOT ANTI ICE DUCT WARNING PER THE FIM 36-20-00 AND FOUND THE LT FUSELAGE NO2 FROM REAR SENSING ELEMENT FOR THE 14TH STAGE BLEED AIR TO BE KINKED/BROKEN REMOVED AND REPLACED WITH NEW THE LT FUSELAGE NO 2 FROM REAR 14TH STAGE BLEED AIR SENSOR IN REFERENCE TO CRJ 200 AMM 36-21-04 OPS CHECKS GOOD PLEASE REFERENCE AML 1285266 PLEASE REFERENCE AML 1285777 PLEASE REFERENCE AML 1285778 PLEASE REFERENCE AML 1285780 PLEASE REFERENCE AML 1286291 PLEASE REFERENCE AML 1286297

Part: UNKNOWN — FAILED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

LH ELEVATOR FAILED BACKLASH, REPLACE BEARINGS AND FITTING AS NEEDED (C-CHECK RO 7/30/2023) REMOVED & INSTALLED NEW 3 EA. BEARINGS P/N MS14103-4,MS14103-5,MS14103-6 IN L/H ELEVATOR AT HINGE 2,3, AND 4 REF. CRJ 200 AMM 20-26-00-910-808. PROOFLOAD GOOD USING TUC#9261 CAL DUE DATE 29-FEB-24, BREAKAWAY TORQUE GOOD USING TUC# 6360 CAL DUE DATE 29-FEB-24. NO DEFECTS NOTED IN BEARING BORES, SEE CONTINUE CARD FOR MORE DETAILS. FITTING REPLCED ON CAMP 26789898.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

FLOOR SUPPORT STRAP AT FS559 RBL27 TO RH FLOOR SILL HAS CORROSION (C-CHECK RO 7/30/2023) REMOVED AND REPLACED STRAP AT FS559 RBL27 REF. CRJ-200 SRM, 51-42-06 AND DWG, 601R31025 REV K. COMPLIED WITH TASK CARD 51-900-1003-SKY. PART FOR PART REPLACEMENT, NO WEIGHT CHANGE.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

CRACK ON FRAME AT FS333 STGR1L (C-CHECK RO 7/30/2023) REMOVED FS333 FRAME SECTION FROM STGR 1 TO STGR 3L. REF: CRJ200 SRM 51-42-21 AND CRJ200 SRM 51-42-06 AND INSTALLED NEW FS333 FRAME SECTION P/N 601R32004-41 FROM APROX. STGR 1 TO STGR 3. DWG 601R31016, REV: D, CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21, LEAK CHECK GOOD, COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

CRACKED CLIP ON FLOOR BEAM RBL27 FS484.0 (C-CHECK RO 7/30/2023) REMOVED, REPLACED AND INSTALLED NEW CLIP P/N 601R31171-9 ON FLOOR BEAM AT RBL 27 FS484.0 REF CRJ 200 SRM 51-42-21 AND REF REO 601R-53-41-059 REV-C DATED 2020-03-11. COMPLIED WITH TASKCARD 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

RIGHT PRESSURE FLOOR ANGLES FROM FS409+128 - FS559.0 HAVE MULTIPLE SPOTS WITH CORROSION (C-CHECK RO 7/30/2023) REPAIRED RIGHT PRESSURE FLOOR ANGLES FROM FS409+128 - FS559.0 REF. CRJ200 SRM 51-21-06, GENERIC REO 601R-53-41-666 REV-C, DATED 2012-11-06, AND REO 601R-53-41-3179 REV--, DATED 2023-06-25. LEAK CHECKS GOOD WITH NO LEAKS NOTED. SEE CONTINUE CARD FOR WORK ACCOMPLISHED. COMPLIED WITH 53-900-1003-SKY

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

CRACK AROUND FASTENER ON FRAME AT FS605.0 STGR18L (MARKED) (C-CHECK RO 7/30/2023) REMOVED CRACKED FRAME SECTION AT FS 605 BETWEEN STGR 17L - STGR 20L REF CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21 AND INSTALLED NEW FRAME SECTION P/N: 601R36026-29 AT FS 605 BETWEEN STGR 17L - STGR 20L REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG 601R36026 REV AF. REMOVED (1)EA SPLICE ANGLE AT FS 605 AND STGR 20L TO FOM REF CRJ200 SRM 51-42-06 AND INSTALLED (1)EA SPLICE ANGLE AT FS 605 AND STGR 20L REF CRJ200 SRM 51-42-06. LEAK CHECK GOOD WITH NO LEAKS NOTED.COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

LEFT PRESSURE FLOOR SILL FS409+128 - FS559.0 HAS MULTIPLE SPOTS WITH CORROSION (C-CHECK RO 7/30/2023) COMPLIED WITH REO 601R-53-41-3177 REV-- DATED 2023-06-22 STEP 1 TO 6. ENSURED BLEND OUT WAS PERFORMED PER SRM 51-21-06, ENSURED MINIMUM MATERIAL THICKNESS IS NOT LESS THAN REPORTED, ENSURED REWORKED AREAS IS CRACK FREE, RESTORED FINISH, APPLIED CIC AND ENSURED ALL OTHER REQUIREMENTS OF GENERIC REO 601R-53-41-666 REV-C DATED 2012-11-06 ARE MET COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

RIGHT PRESSURE FLOOR SILL FS409+128 - FS559.0 HAS MULTIPLE SPOTS WITH CORROSION (C-CHECK RO 7/30/2023) COMPLIED WITH REO 601R-53-41-3178 REV-- DATED 2023-06-23 STEP 1 TO 6. ENSURED BLEND OUT WAS PERFORMED PER SRM 51-21-06, ENSURED MINIMUM MATERIAL THICKNESS IS NOT LESS THAN REPORTED, REPLACED BLENDED FASTENERS, ENSURED REWORKED AREAS IS CRACK FREE, RESTORED FINISH, APPLIED CIC AND ENSURED ALL OTHER REQUIREMENTS OF GENERIC REO 601R-53-41-666 REV-C DATED 2012-11-06 ARE METREMOVED CORROSION FROM RIGHT PRESSURE FLOOR SILL FS409+128 - FS559.0 PER CRJ200 SRM 51-21-06.COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — BENT (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

CARGO DOOR SURROUND FORWARD UPPER CHANNEL BENT (MARKED) (C-CHECK RO 7/30/2023) CARGO DOOR SURROUND FWD UPPER CHANNEL DEPTH IS APPROX. 0.25" WITH SHARP CREASES. FOUND TO BE OUT OF LIMITS DUE TO LOCATION AND CONDITION(DENTS ALLOWED IN WEBS ONLY WITH NO SHARP CREASES) REF CRJ200 SRM 53-00-00. REMOVED BAD CHANNEL REF CRJ200 SRM 51-42-06. ORDERED AND RECEIVED REPLACEMENT CHANNEL PART# 601R35050-129. ORDERED AND RECEIVED REPLACEMENT FASTENERS AND INSTALLED REPLACEMENT CHANNEL WITH REPLACEMENT FASTENERS REF DRW. 601R35050 REV. Y, REF DRW. 601R35207 REV. W. AND REF CRJ200 SRM 51-42-06.COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

PAX DOOR DD8 CLIP ON THE AFT SIDE ON FRAME 320.163 IS CORRODED (C-CHECK RO 7/30/2023) REMOVED PAX DOOR DD8 CLIP ON THE AFT SIDE ON FRAME 320.163 IAW CRJ200 SRM 51-42-06 AND INSTALLED NEW PAX DOOR DD8 CLIP ON THE AFT SIDE ON FRAME 320.163 IAW CRJ200 SRM 51-42-06 AND DWG 601R31702 REV N. LEAK CHECK GOOD

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

PAX DOOR DD8 CLIP ON THE FWD SIDE ON FRAME 320.163 IS CORRODED (C-CHECK RO 7/30/2023) REMOVED PAX DOOR DD8 CLIP ON THE FWD SIDE ON FRAME 320.163 IAW CRJ200 SRM 51-42-06 AND INSTALLED NEW PAX DOOR DD8 CLIP ON THE FWD SIDE ON FRAME 320.163 IAW CRJ200 SRM 51-42-06 AND DWG 601R31702 REV N, LEAK CHECK GOOD, COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

*FS621.00 FORWARD SIDE OF AFT PRESSURE BULKHEAD HAS SCREW STRIKE DAMAGE IN NUMEROUS PLACES ON THE REPAIR STRAPS AND FASTENER HEADS (MARKED) (C-CHECK RO 7/30/2023) COMPLIED WITH REO 601R-53-61-8044 REV--, DATED 2023-06-20 ENSURED BLEND OUT WAS PERFORMED TO A SMOOTH CONTOUR TO A 20:1 TRANSITION, COMPLETE DAMAGE REMOVAL AND THAT THE MINIMUM REMAINING THICKNESS (.060") WAS NOT LESS THAN REPORTED.REMOVED AND REPLACED 7 EA. DAMAGED SOLID RIVETS WITH NEW SOLID RIVETS AT REWORK LOCATIONS ON THE FS 621.00 AFT PRESSURE BULKHEAD ON THE REPAIR STRAPS REF CRJ200 SRM 51-42-06. LEAK CHECK GOOD WITH NO LEAKS NOTED. COMPLIED WITH SKYWEST TASKCARD 51-900-1003-SKY.

Part: UNKNOWN — GOUGED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

RH WING INBD TRAILING EDGE GOUGE ON APRON SKIN WS48.0 (C-CHECK RO 7/30/2023) REPLACED THE 601R-53-41-115 (-2 ONLY) SKIN SECTION REF CRJ200 SRM 51-42-06 AND SRM 51-42-21 AND REO 601R-53-41-115 REV A DATE 2005-07-20.COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — DENTED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

DENT ON EXTERIOR FUSELAGE AT APPROX FS589 BETWEEN SGTR25L-24L (C-CHECK RO 7/30/2023) REPAIRED DENT ON EXTERIOR FUSELAGE AT APPROX FS589 BETWEEN SGTR25L-24L REF REO 601R-53-61-8042 REV -- DATE 2023-06-24 (ALL STEPS COMPLIED WITH),REO 601R-53-61-8042, REV --(P1), 2023-06-19 , GREO 601R-51-00-309 REV-A, DATED 2017-08-23 AND CRJ-200 SRM 53-00-31.LEAK CHECK GOOD, COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — WORN (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

* PASSENGER DOOR HINGE HALF ON THE FUSELAGE HAS EXCESSIVELY WORN LUGS, ALL LUGS FAIL THE GO-NO-GO GUAGE. ( TUC8495 ) (C-CHECK RO 7/30/2023) REMOVED AND REPLACED PASSENGER DOOR HINGE ON FUSELAGE REF CRJ200 SRM53-21-23 REV 39 DATED MAR 10/21, REO NO. 601R-53-21-656 REV -A DATED 2017-03-06 AND DWG 600-31527 REV A. LEAK CHECK GOOD WITH NO LEAKS NOTED. COMPLIED WITH SKY WEST TASK CARD 51-900-1003-SKY.

Part: UNKNOWN — CHAFED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

* LEFT WING INBOARD FLAP VANE, INBOARD LEADING EDGE CAP IS CHAFFED. (C-CHECK RO 7/30/2023) REMOVED AND REPLACED THE LEFT WING INBOARD FLAP VANE, INBOARD LEADING EDGE CAP (P/N 601R14303-53) REF DRW#601R14302 REV E. AND CRJ200 SRM 51-42-10. COMPLIED WITH 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIR (**RII**). SEE CONTINUATION FOR DETAILS.

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

REMOVE AND REINSTALL SERVICE DOOR TO FOM (C-CHECK RO 7/30/2023) REMOVED SERVICE DOOR TO FOM. REF CRJ200 AMM 52-41-00-000-801 AND INSTALLED NEW SERVICE DOOR REF CRJ200 AMM 52-41-00-400-801 ,FUNCTIONAL CHECK & OP TEST GOOD AT THIS TIME

Part: UNKNOWN — CHAFED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

* LEFT WING INBOARD FLAP VANE, MIDDLE LEADING EDGE CAP IS CHAFFED. (C-CHECK RO 7/30/2023) REMOVED AND REPLACED LEFT WING INBOARD FLAP VANE, MIDDLE LEADING EDGE LEADING EDGE CAP (P/N 601R14303-51) WITH NEW VANE CAP ONTO LH WING INBD FLAP VANE USING ALL NEW FASTENERS, REF CANADAIR DWG# 601R14302 REV-E AND CRJ200 SRM 51-42-13. COMPLIED WITH 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIR (**RII**). SEE CONTINUATION FOR DETAILS.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

DURING REMOVAL OF THE PAX DOOR INNER SKIN CORROSION WAS FOUND ON CLEAT AT AFT INTERCOSTAL DD6. (C-CHECK RO 7/30/2023) REMOVE NEW CLEAT AT AFT INTERCOSTAL DD5 AND INSTALLED NEW CLEAT AT AFT INTERCOSTAL DD5. REF CRJ 200 SRM 51-42-06 AND DRAWING 601R31702 REV-N, COMPLIED WITH 51-900-1003-SKY, LEAK CHECK GOOD

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

DURING REMOVAL OF THE PAX DOOR INNER SKIN CORROSION WAS FOUND ON INTERCOSTAL DD4 AFT. (C-CHECK RO 7/30/2023) REMOVED PAX DOOR DAMAGED INTERCOSTAL (DD4 AFT) REF CRJ200 SRM 51-42-06 AND INSTALLED NEW INTERCOSTAL DD4 AFT. REF CRJ 200 SRM 51-42-06 AND DRAWING 601R31702 REV-N,COMPLIED WITH 51-900-1003-SKY. LEAK CHECK GOOD

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

DURING REMOVAL OF THE PAX DOOR INNER SKIN CORROSION WAS FOUND ON INTERCOSTAL DD5 AFT. (C-CHECK RO 7/30/2023) REMOVED PAX DOOR DAMAGED INTERCOSTAL (DD5 AFT) REF CRJ200 SRM 51-42-06 AND INSTALLED NEW INTERCOSTAL DD5 REF CRJ 200 SRM 51-42-06 AND DRAWING 601R31702 REV -N, COMPLIED WITH 51-900-1003-SKY, LEAK CHECK GOOD

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

DURING REMOVAL OF THE PAX DOOR INNER SKIN CORROSION WAS FOUND ON FORMER @ FS 329.76 BETWEEN DD5 AND DD6. (C-CHECK RO 7/30/2023) REMOVED DAMAGE FORMER ON PAX DOOR AT FS 329.76 BETWEEN DD5 AND DD6 REF CRJ 200 SRM 51-42-06 AND INSTALLED NEW FORMER ON PAX DOOR AT FS 329.76 BETWEEN DD5 AND DD6 REF CRJ 200 SRM 51-42-06 , SRM 51-40-11 AND DRAWING 601R31702 REV -N, LEAK CHECK GOOD, COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

*CORROSION AROUND SEVERAL FASTENER HOLES UNDERNEATH THE SERVICE DOOR OUT PROTECTOR PLATE (MARKED (C-CHECK RO 7/30/2023) REPAIRED 3 EA. AREAS OF CORROSION AROUND SEVERAL FASTENER HOLES UNDERNEATH THE SERVICE DOOR OUT PROTECTOR PLATE REF CRJ-200 SRM 51-42-06 AND REO 601R-53-21-3638 REV--, DATED 2023-06-21, COMPLIED WITH ALL STEPS. COMPLIED WITH 51-900-1003-SKY(CL600-2B19 (**RII**). SEE CONTINUATION FOR DETAILS.BLEND ONLY NO WEIGHT CHANGE.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

DURING REMOVAL OF THE PAX DOOR INNER SKIN CORROSION WAS FOUND ON CLEAT AT AFT INTERCOSTAL DD5. (C-CHECK RO 7/30/2023) REMOVED AND INSTALLED NEW CLEAT AT AFT INTERCOSTAL DD5. REF CRJ 200 SRM 51-42-06 AND DRAWING 601R31702 REV -N, COMPLIED WITH 51-900-1003-SKY. LEAK CHECK GOOD

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

DURING REMOVAL OF THE PAX DOOR INNER SKIN CORROSION WAS FOUND ON FWD FORMER @ FS320.163. (C-CHECK RO 7/30/2023) REMOVED FWD FORMER AT FS 320.163 REF CRJ 200 SRM 51-42-06,51-42-21 AND 51-42-13 AND INSTALLED FWD FORMER AT FS 320.163 REF CRJ 200 SRM 51-42-06 AND DRAWING 601R31702 REV -N, LEAK CHECK GOOD

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

DURING REMOVAL OF THE PAX DOOR INNER SKIN CORROSION WAS FOUND ON DD5 FWD INTERCOSTAL. (C-CHECK RO 7/30/2023) REMOVED PAX DOOR DD5 FWD INTERCOSTAL. REF CRJ 200 SRM 51-42-06 AND INSTALLED PAX DOOR DD5 FWD INTERCOSTAL. REF CRJ 200 SRM 51-42-06 AND DRAWING 601R31702 REV-N AND REO601R-52-11-2982 REV -- DATE 2023-06-14, PRESSURE LEAK CHECK GOOD

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

PAX DOOR AFT FORMER CRACKED AT POWER ASSIST PULLEY BRACKET LOCATION (C-CHECK RO 7/30/2023) REMOVED PAX DOOR AFT FORMER REF CRJ200 SRM 51-41-06 AND 51-42-21 AND INSTALLED NEW AFT FORMER (PAX DOOR) REF CRJ200 SRM 51-42-06, 51-42-21 AND DWG 601R31702 REV N.LEAK CHECK GOOD COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

PAX DOOR FWD FORMER CORRODED (C-CHECK RO 7/30/2023) REMOVED PAX DOOR FWD FORMER REF CRJ 200 SRM 51-42-06 AND 51-42-21 AND INSTALLED NEW PAX DOOR FWD FORMER REF CRJ 200 SRM 51-42-06 AND 51-42-21 DRAWING 601R31702 REV -N. PERFORMED AIRCRAFT PRESSURIZATION PAX DOOR LEAK CHECK GOOD, COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

**CORROSION NOTED ON PAX DOOR MID INTERCOASTAL DD2 (MARKED) (C-CHECK RO 7/30/2023) REMOVED DAMAGED INTERCOSTAL (MID DD2) REF CRJ200 SRM 51-42-06 AND 51-42-21 AND INSTALLED NEW PAX DOOR MID INTERCOASTAL DD2 REF CRJ200SRM 51-42-06 AND DRAWING 601R31702 REV -N, COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

**CORROSION NOTED ON PAX DOOR MID INTERCOASTAL DD6 (MARKED) (C-CHECK RO 7/30/2023) REMOVED DAMAGED INTERCOSTAL ON PAX DOOR MID INTERCOASTAL DD6 REF CRJ 200 SRM 51-42-06 AND INSTALLED NEW INTERCOSTAL ON PAX DOOR MID INTERCOASTAL DD6 REF CRJ 200 SRM 51-42-06 AND DRAWING 601R31702 REV -N LEAK CHECK GOOD

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

**CORROSION NOTED ON PAX DOOR MID INTERCOASTAL DD4 (MARKED) (C-CHECK RO 7/30/2023) REMOVED INTERCOSTAL ON PAX DOOR MID DD4 REF CRJ 200 SRM 51-42-06 AND 51-42-21 AND INSTALLED NEW INTERCOSTAL ON PAX DOOR MID DD4 REF CRJ 200 SRM 51-42-06 AND 51-42-21 AND DRAWING 601R31702 REV-N. LEAK CHECK GOOD AND NO LEAKS NOTED.COMPLIED 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

*CORROSION NOTED ON PAX DOOR MID INTERCOASTAL DD1 (MARKED) (C-CHECK RO 7/30/2023) REMOVED PAX DOOR MID INTERCOASTAL DD1 REF CRJ 200 SRM 51-42-06 AND 51-42-21 AND INSTALLED PAX DOOR MID INTERCOASTAL DD1 REF CRJ 200 SRM 51-42-06 AND 51-42-21 AND DRAWING 601R31702 REV-N. LEAK CHECK GOOD AND NO LEAKS NOTED.COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

**CORROSION NOTED ON PAX DOOR MID INTERCOASTAL DD3 (MARKED) (C-CHECK RO 7/30/2023) REMOVED AND INSTALLED NEW PAX DOOR MID INTERCOASTAL DD3 REF CRJ 200 SRM 51-42-06 AND DRAWING 601R31702 REV -N, COMPLIED WITH 51-900-1003-SKY, LEAK CHECK GOOD

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 44,716 hrs · 38,064 cycles

**CORROSION NOTED ON PAX DOOR FRAME AT APPROX FS327 BETWEEN DD3-DD4 (MARKED) (C-CHECK RO 7/30/2023) REMOVED PAX DOOR FRAME AT APPROX FS327 BETWEEN DD3-DD4 REF CRJ 200 SRM 51-42-06 AND 51-42-21 AND INSTALLED NEW FRAME SECTOR AT APPROX FS 327 BETWEEN DD3-DD4 REF CRJ200 SRM 51-42-06, 51-42-21 AND DWG601R31702 REV N, COMPLIED WITH 51-900-1003-SKY, LEAK CHECK GOOD

Part: SELECTOR VALVE — FAILED (MLG) · airframe 40,148 hrs · 33,922 cycles

GEAR DISAGREE WARNING DURING APPROACH. THE RIGHT MAIN GEAR DID NOT EXTEND. DURING THE GO-AROUND THE RIGHT MAIN GEAR EXTENDED AND THE WARNING WENT AWAY. COMPLIED WITH THE QRH AND LANDED WITHOUT ANY OTHER ISSUES. REMOVED AND REPLACED MLG SELECTOR VALVE IAW AMM.

Part: SELECTOR VALVE — MALFUNCTIONED (RT MLG) · airframe 40,034 hrs · 33,825 cycles

GEAR DISAGREE ON R MAIN GEAR DURING APPROACH. THEN A THUD WAS HEARD, THE MESSAGE CLEARED, AND WE RECEIVED A DOWN AND LOCKED INDICATION. CONTINUED FOR A NORMAL LANDING. (FLT#5305) REMOVED AND REPLACED MLG SELECTOR VALVE IAW AMM. PERFORMED OPERATIONAL CHECK IAW AMM. SWUNG GEAR MULTIPLE TIMES AND PERFORMED FREE FALLS. OPS CHECK GOOD, NO LEAKS NOTED.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 36,537 hrs · 30,689 cycles

RETURNED TO THE FIELD WITH A GEAR DISAGREE. REMOVED AND REPLACED THE NLG ASSY IAW AMM. OPS AND LEAK CHECKED GOOD.

Part: WARNING MESSAGE — ACTIVATED (NLG) · airframe 35,981 hrs · 30,190 cycles

NOSE GEAR DISAGREE ON RETRACTION.

Part: SWITCH — OUT OF ADJUST (THRUST REVERSER) · airframe 35,735 hrs · 29,978 cycles

RT THRUST REVERSER UNLOCK MESSAGE DURING FLT. RT STOW SWITCH OUT OF ADJUSTMENT. ADJUSTED THE SWITCH. OPS CHECKED GOOD.

Part: CONTROL HANDLE — FAILED (LANDING GEAR) · airframe 30,931 hrs · 25,704 cycles

LANDING GEAR WOULD NOT COME DOWN, CYCLED GEAR AND GEAR CAME DOWN. REPLACED GEAR HANDLE. OPS CHECKED GOOD.

Part: CABLE — FAILED (THROTTLE) · airframe 30,695 hrs · 25,466 cycles

THE LT THRUST LEVER WOULD NOT MOVE IN FLIGHT. SHUTDOWN ENGINE. R & R LT ENGINE THROTTLE PUSH/PULL CABLE AND CONTROL GEAR BOX IAW AMM.

Part: LINE — LEAKING (APU FUEL) · airframe 29,233 hrs · 24,205 cycles

CREW REPORTED STRONG FUEL ODOR IN CABIN. TIGHTENED AND SECURED APU FUEL LINE, NO LEAKS NOTED.

Part: WINDSHIELD WIPER — LOOSE (WINDSHIELD) · airframe 29,185 hrs · 24,164 cycles

CAPTAIN'S WINDSHIELD WIPER CAME LOOSE AFTER TAKEOFF. RETURNED TO FIELD. MAINTENANCE REPLACED THE WIPER IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 28,686 hrs · 23,765 cycles

SERVICE DOOR EMERGENCY EXIT LIGHT BROKEN. R & R LIGHT IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 28,686 hrs · 23,765 cycles

PAX DOOR AREA EMERGENCY FLOOD LIGHT IS BROKEN. R & R FLOOD LIGHT IAW AMM.

Part: BUSHING — GALLED (ENGINE MOUNT) · airframe 28,353 hrs · 23,498 cycles

THE RT ENGINE YOKE LINK AND BUSHING ARE GALLED. R & R RT ENGINE UPPER YOKE LINK AND CLAMP UP BUSHING IAW AMM.

Part: RIB — CORRODED (RT PYLON) · airframe 28,353 hrs · 23,498 cycles

THE RISER OF THE RT ENGINE PYLON OTBD RIB HAS FRETTING DAMAGE. COMPLIED WITH DISPOSITION FOR FRETTING DAMAGE TO PRODUCTION RISER OF THE RT ENGINE AFT ENGINE MOUNT ENGINE PYLON OTBD RIB IAW REO.

Part: CONTROL UNIT — FAILED (SPOILERS) · airframe 28,336 hrs · 23,482 cycles

AT FL 30K WITH FLIGHT SPOILERS EXTENDED 50 PERCENT, AIRPLANE PITCHED TO RT AGGRESSIVELY. REMOVED AND REPLACED NR 1 SECU AND THE LEFT FLIGHT SPOILER OUTBOARD PCU.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,109 hrs · 23,306 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 13 IS BURNED OUT. REPLACED LAMP.

Part: TRIM SWITCH — FAILED (COCKPIT) · airframe 27,333 hrs · 22,741 cycles

STAB TRIM & MACH TRIM CAUTION MESSAGE. STAB TRIM WAS STUCK, TRIED BOTH STAB 1& 2 INDEPENDENTLY. STAB TRIM ENGAGED ON THE GND. FLT 5519 MDC FAULTS HAD BITS SET FOR FAILED FLIGHT OFFICER’S PITCH DISCONNECT SWITCH & CAPTAIN`S TRIM SWITCH. CLEANED LUBED CAPTAIN'S TRIM SWITCH AS REQUIRED. REPLACED FLIGHT OFFICER'S PITCH DISCONNECT SWITCH. OPERATIONS CHECKED GOOD.

Part: RELAY — FAULTY (ELECTRICAL SYS) · airframe 27,123 hrs · 22,572 cycles

AC ESS BUS CAUTION MESSAGE & EMERGENCY LIGHTS ON STATUS MESSAGE. FLT 5253 REPLACED AC ESS RELAY K1XD, ALL MESSAGES EXTINGUISHED, OPERATIONS CHECKED GOOD.

Part: VANE — CHAFED (TE FLAP) · airframe 26,805 hrs · 22,342 cycles

LT INBD FLAP VANE HAS CHAFE ON OTBD LE. C-CHECK BLENDED CHAFE ON LT INBD FLAP VANE OTBD LE IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,805 hrs · 22,342 cycles

FS 202 CRACKED AT PARKING BRAKE CABLE HOLE. C-CHECK REPAIRED FS 202 BULKHEAD AT PARKING BRAKE CABLE HOLE IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 26,805 hrs · 22,342 cycles

POST AT FS409+128 HAS CRACK AT LBL 27 INBD SIDE LOWER RADIUS. C-CHECK R & R FS409+128 VERTICAL POST, LBL 27 INBD SIDE IAW CRJ 200 SRM 51-40-11, 51-40-06 & EO 601R32208 SNIEO S03. LEAK CHECKED GOOD.

Part: POST — CRACKED (FUSELAGE) · airframe 26,805 hrs · 22,342 cycles

POST AT FS409+128 HAS CRACK AT RBL18 OTBD SIDE LOWER RADIUS. C-CHECK REPLACED FS409+128 VERTICAL POST, RBL18 OTBD SIDE IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 26,805 hrs · 22,342 cycles

PAX DOOR HINGE, FS SIDE, GOUGED ON LUG TOP SIDE TENTH BACK FROM FRONT. C-CHECK PAX DOOR HINGE REPAIRED IAW REO.

Part: SKIN — CRACKED (LT WING) · airframe 26,805 hrs · 22,342 cycles

LT WING LOWER PLANK WS 0.00 STRINGER 5 & 7 WING DRAIN ATTACHMENT HOLES, FWD & AFT CRACK INDICATIONS NOTED. C-CHECK SERVICE BULLETIN 601R-57-045, REVISION A, WINGS LOWER AFT WING PLANK. REMOVAL OF THE FASTENER HOLES FOR THE FUEL BOOST PUMP & THE DRAIN VALVE ASSEMBLY, PART A, & PART B INCORPORATED.

Part: POST — CRACKED (FUSELAGE) · airframe 26,805 hrs · 22,342 cycles

CRACK NOTED & MARKED IN CENTER FS409+128 VERTICAL POST BL0.0, RT C-CHANNEL IN AFT RADIUS. C-CHECK REPLACED FS409+128 VERTICAL POST, BL 0.0 RT C-CHANNEL IAW REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,805 hrs · 22,342 cycles

FS484 CLIP LT CRACKED. C-CHECK REPLACED FS 484 CLIP LT IAW REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,805 hrs · 22,342 cycles

FS 484 CLIP RT CRACKED. C-CHECK REPLACED FS 484 CLIP RT IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 26,805 hrs · 22,342 cycles

LT INBD FLAP VANE HAS CHAFES ON INBD LE. C-CHECK BLENDED CHAFE ON LT INBD FLAP VANE INBD LE IAW REO.

Part: SILL — CORRODED (FUSELAGE) · airframe 26,805 hrs · 22,342 cycles

CARGO DOOR SURROUND, LOWER SILL IS CORRODED ON UNDERSIDE, AROUND 15 EA. NUT PLATES, BETWEEN FS559.00 +112 & FS621.00. C-CHECK REMOVED CORROSION ON CARGO DOOR SILL ON UNDERSIDE BETWEEN FS559.00 +112 & FS621.00 IAW SRM & REO.

Part: POST — CRACKED (FUSELAGE) · airframe 26,805 hrs · 22,342 cycles

CRACK FOUND ON LOWER RADIUS OF FS409+128, LBL18 OTBD VERTICAL POST. C-CHECK REPLACED FS409+128 VERTICAL POST, LBL18 OTBD SIDE IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,392 hrs · 22,030 cycles

EMERGENCY OVERHEAD LIGHT NR 3 IS BURNED OUT. FLT#5420 RELAMPED

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,807 hrs · 21,552 cycles

LAST OVERHEAD EMERGENCY LIGHT IS BURNED OUT. RELAMPED.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 25,365 hrs · 21,205 cycles

CAPTAINS SIDE WINDOW ABOUT 3-4 INCHES AFT OF CHART HOLDER ALONG THE BOTTOM OF THE WINDOW LOOKED LIKE A FRAYED WIRE. (FLT 5328) REPLACED CAPTAINS SIDE WINDOW ASSEMBLY P/N ON: NP-139322-11 P/N OFF: 601R33033-19 S/N ON: 12150H9047 S/N OFF: 03177H7491

Part: PRIORITY VALVE — DEFECTIVE (NLG) · airframe 24,706 hrs · 20,652 cycles

THE NOSE GEAR WAS VERY SLOW EXTENDING, RESULTING IN A GEAR DISAGREE WARNING MESSAGE. TEN SECONDS LATER, THE GEAR WAS DOWN AND LOCKED AND THE MESSAGE EXTINGUISHED. (FLT 6337) REPLACED NLG PRIORITY VALVE IAW AMM, ALSO PERFORMED SUCCESSFUL ALTERNATE EXTENSION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,591 hrs · 20,563 cycles

NR 2 EMERGENCY OVERHEAD LIGHT IN CABIN DOES NOT ILLUMINATE. (FLT 6214) REPLACED EMERGENCY OVERHEAD LIGHT NR 2.

Part: UNKNOWN — ODOR (CABIN) · airframe 24,490 hrs · 20,495 cycles

AT GATE CONNECTED TO GROUND POWER, SMOKE STARTED TO FILL CABIN. (FLT 6207) INSPECTED CABIN, NO SMOKE FOUND. NO SMELL OF SMOKE FOUND. RAN AIRCRAFT ELECTRICAL SYSTEMS WITH GROUND POWER FOR SEVERAL HOURS IN THE HANGAR WITH NO VISIBLE SMOKE NOTED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,360 hrs · 20,402 cycles

LEFT EXTERNAL MIDDLE EMERGENCY LAMP BURNED OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,146 hrs · 20,245 cycles

SECOND EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 5351) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,000 hrs · 20,125 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4809) RELAMPED EMERGENCY LIGHT.

Part: ACTUATOR — FAILED (AUTOPILOT SYS) · airframe 23,821 hrs · 19,975 cycles

AIRCRAFT YAWED UNCOMMANDED DURING DESCENT. (FLT 6274) REPLACED NR 1 YAW DAMPER LINEAR ACTUATOR IAW AMM. P/N OFF: 622-9962-001 S/N OFF: 3662.

Part: SWITCH — FAILED (THRUST REVERSER) · airframe 23,142 hrs · 19,421 cycles

LEFT REVERSE UNLOCK MESSAGE. (FLT 5557) REPLACED LEFT THRUST REVERSER STOW MICROSWITCH IN REFERENCE TO AMM.

Part: CONTROL HANDLE — FAILED (COCKPIT) · airframe 23,045 hrs · 19,339 cycles

RECEIVED ANTISKID INBOARD MESSAGE FOLLOWED BY PARK BRAKE SOV AND ALL GEARS FAILED TO RETRACT. APPROXIMATELY A FEW MINUTES LATER ALL GEAR RETRACTED. (FLT 5597) REPLACED LANDING GEAR SELECTOR HANDLE ASSEMBLY PER CRJ AMM. P/N 601R50967-11, S/N OFF: 1498.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,608 hrs · 19,009 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6299) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,565 hrs · 18,981 cycles

FLT 6445, OVERHEAD EMERGENCY LIGHT AT ROW 10 IS OUT. RELAMPED EMERGENCY LIGHT.

Part: SERVO — FAILED (AILERONS) · airframe 22,565 hrs · 18,981 cycles

FLT 6445, AUTO PILOT UNCOMMANDED ROLL. REPLACED THE AILERON SERVO IN REFERENCE TO MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,481 hrs · 18,919 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5501) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,317 hrs · 18,793 cycles

SECOND FROM LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5417) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,300 hrs · 18,780 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5383) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,159 hrs · 18,666 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5535) RELAMPED EMERGENCY LIGHT.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 22,159 hrs · 18,666 cycles

DENT AT FS 761.00 BETWEEN STGR 14 & 15 ON LEFT SIDE. (SERVICE) COMPLIED WITH REO.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 22,159 hrs · 18,666 cycles

DENT AND SCRATCH AT FS 769.00 ABOVE STGR 14.84 LEFT SIDE. (SERVICE) COMPLIED WITH REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,109 hrs · 18,627 cycles

NR 1 OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 6275) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,059 hrs · 18,587 cycles

(C-CHECK) CRACK INDICATED ON THE LEFT SIDE FS 559.0 PRESSURE BULKHEAD. REPAIRED CRACK AT FS 559.0 PRESSURE BULLKHEAD.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,059 hrs · 18,587 cycles

(C-CHECK) CRACK AT FS 621 BULKHEAD, FORWARD FACE, ABOVE UPPER CARGO DOOR TRACK FITTING. REPAIRED CRACK AT FS 621 BULKHEAD, FORWARD FACE, ABOVE UPPER CARGO DOOR TRACK FITTING.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,039 hrs · 18,570 cycles

LEFT WING EXTERIOR EMERGENCY EXIT LIGHT IS OUT. (FLT 5630) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,039 hrs · 18,570 cycles

RIGHT WING AFT EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,836 hrs · 18,415 cycles

NR 1 EMERGENCY CEILING OVERHEAD LIGHT INOPERATIVE. (FLT 6229) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,671 hrs · 18,290 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5311) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,565 hrs · 18,209 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5555) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,450 hrs · 18,117 cycles

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

Part: SPHERICAL BEARIN — CORRODED (ENGINE MOUNT) · airframe 20,900 hrs · 17,674 cycles

RIGHT ENGINE, AFT MOUNT SPHERICAL BUSHING AND HOUSING ARE PITTED. (ENGINE CHANGE) REPLACED RIGHT ENGINE, AFT MOUNT SPHERICAL BUSHING AND HOUSING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,840 hrs · 17,627 cycles

NR 1 AND NR 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 6324) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,196 hrs · 17,115 cycles

LEFT FORWARD OVERWING EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 6537) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,023 hrs · 16,982 cycles

AFT EXTERIOR EMERGENCY LIGHTS OVER LEFT AND RIGHT WINGS ARE OUT. (FLT 6295) RELAMPED EMERGENCY LIGHTS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 19,762 hrs · 16,773 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6911) REPLACED THE NR 3 ELBP.

Part: LIGHT — UNSECURE (CABIN) · airframe 19,405 hrs · 16,475 cycles

FLOOR LEVEL EMERGENCY LIGHT NEAR MAIN CABIN DOOR INOPERATIVE. (FLT 6999) RE-ATTACHED FLOOR LEVEL EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,147 hrs · 16,253 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6416) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,016 hrs · 16,155 cycles

RIGHT FORWARD EXTERIOR EMERGENCY LIGHT OUT. (FLT 6947) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,632 hrs · 15,822 cycles

LAST OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 6765) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,632 hrs · 15,822 cycles

NR 2 OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 6899) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,963 hrs · 15,230 cycles

CEILING EMERGENCY LIGHT INOP, SECOND CEILING LIGHT FROM FRONT. (FLT 6132) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — LOOSE (CABIN) · airframe 17,877 hrs · 15,152 cycles

IN FLOOR EMERGENCY LIGHTS AT ROWS 5 TO 8 INOP. (FLT 6348) RESEATED CONNECTOR.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 17,930 hrs · 15,204 cycles

INTERCOSTAL CRACKED ON UPPER FLANGE STA 484 LBL 36.5, WL & 72 BELOW FLOOR. (C-CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,930 hrs · 15,204 cycles

CRACK NOTED & MARKED ON RT FS 559 BULKHEAD WEB, AFT FACE, INBOARD OF RBL 18 AT WL 59.1. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,430 hrs · 14,769 cycles

SECOND FROM AFT EMERGENCY LIGHT INOP. (FLT 6644) RELAMPED EMERGENCY LIGHT.

Part: TRIM PANEL — MALFUNCTIONED (RUDDER) · airframe 16,508 hrs · 14,011 cycles

ON CLIMBOUT RUDDER TRIM RAN FULL SCALE LEFT UNCOMMANDED. (FLT 5937) REPLACED RUDDER TRIM PANEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,295 hrs · 13,825 cycles

NR 3 EMERGENCY CABIN FLOOD LIGHT INOP. (FLT 5977) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,572 hrs · 13,229 cycles

OVERHEAD EMERGENCY LIGHT IN THE CABIN INOP, 3RD FROM FRONT OF A/C. (FLT 5831) REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT BULB IAW AMM 33-51-1B.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,449 hrs · 13,140 cycles

ROW 10 CEILING EMERGENCY LIGHT INOP. (FLT 6640) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,304 hrs · 13,030 cycles

NR 2 CEILING EMERGENCY LIGHT INOP. (FLT 6394) RELAMPED EMERGENCY LIGHT.

Part: BOLT — SHEARED (PAX DOOR) · airframe 15,170 hrs · 12,934 cycles

CABIN WOULD NOT PRESSURIZE. (FLT 5760) REPLACED BOLT AND BUSHING ON PASSENGER DOOR VENT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,749 hrs · 12,611 cycles

GALLEY SERVICE DOOR EMERGENCY LIGHT INOP. (FLT 5793) RELAMPED EMERGENCY LIGHT.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 14,550 hrs · 12,466 cycles

FLT 6761 - EMERGENCY EXIT LIGHT RED COVER MISSING. REPLACED LENSE.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 14,233 hrs · 12,218 cycles

FLT 6038 - CAPTAINS WINDSHIELD SHATTERED. REPLACED CAPTAINS WINDSHIELD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 13,957 hrs · 11,985 cycles

FLT 6594 - SECOND EMERGENCY POD OVERHEAD LIGHT IS BURNED OUT. RELAMPED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,432 hrs · 11,546 cycles

C-CHECK, FS 280 FLOOR SUPPORT BEAM LBL9 LOWER INBOARD AND OUTBOARD CLIPS CRACKED. REPAIRED PER REO.

Part: FITTING — CORRODED (RT ENGINE MOUNT) · airframe 13,432 hrs · 11,546 cycles

C-CHECK, RIGHT ENGINE THRUST FITTING CORRODED. REPLACED PER AMM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,432 hrs · 11,546 cycles

C-CHECK, FS 280 FLOOR SUPPORT BEAM RBL9 LOWER INBOARD AND OUTBOARD CLIPS CRACKED. REPAIRED PER REO.

Part: FITTING — CORRODED (LT ENGINE MOUNT) · airframe 13,432 hrs · 11,546 cycles

C-CHECK, LEFT ENGINE THRUST FITTING CORRODED. REPLACED PER AMM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,432 hrs · 11,546 cycles

C-CHECK, STATION 280 FLOOR SUPPORT BEAM RBL9/LBL9 CRACKED. REPAIRED PER REO.

Part: ATTACH FITTING — CRACKED (BS 625) · airframe 13,432 hrs · 11,546 cycles

C-CHECK, RIGHT AND LEFT FS 625 TIE CLIPS ON FRAME TO BULKHEAD INTERCOSTAL ARE CRACKED. REPLACED PER SRM.

Part: CONNECTOR — DIRTY (FIRE DETECTION) · airframe 12,747 hrs · 10,990 cycles

LEFT FIRE FAIL CAUTION MESSAGE IS INTERMITTENT. FLIGHT 6541. CLEANED AND RE-INSTALLED CONNECTOR PINS AND PLUG. OPS CHECK GOOD.

Part: RUDDER PEDAL — NOISY (COCKPIT) · airframe 12,436 hrs · 10,725 cycles

CREW REPORTS A THUMPING SOUND DURING FLIGHT. (FLIGHT NR 1008) RETORQUED CAPTAINS RUDDER PEDAL PIVOT BOLTS IAW RJ-SL-27-086. OPS CHECK GOOD FOR CONTINUED SERVICE.

Part: CONTROLLER — FAILED (FIRE DETECTOR) · airframe 12,300 hrs · 10,609 cycles

FLT 6150 - LEFT FIRE FAIL MESSAGE DURING TAXI OUT. REPLACED FIRE DETECTION CONTROLLER WITH A SERVICEABLE UNIT. OPS CHECK GOOD.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 11,864 hrs · 10,267 cycles

FLOOR LEVEL EMERGENCY LIGHTS ARE INOP AT ROW 5. RESECURED WIRING LIGHTING TERMINAL. OPS CHECKS GOOD.

Part: BEARING — ROUGH (YOKE) · airframe 11,233 hrs · 9,735 cycles

FLT 5802 - RESISTANCE FELT IN THE FIRST OFFICERS YOKE AILERON MOVEMENT. REPLACED THE CONTROL YOKE SHAFT SUPPORT BEARINGS IAW MM 27-11-01. OPS CHECK GOOD.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 9,998 hrs · 8,654 cycles

FLT 5892 - HYDRAULIC 2 LO PRESS CAUTION MESSAGE APPEARED. REPLACED NR 2 EDP IAW CRJ AMM 29-11-01 AND INSPECTED NR 2 HYDRAULIC SYSTEM IAW AMM 05-51-33.

Part: ADC — FAILED (NR 2) · airframe 8,560 hrs · 7,415 cycles

RECEIVED RED "IAS", "ALT" AND "V/S" FLAGS ON FO SIDE PFD IN FLIGHT. PURGED P1, P2 SYSTEMS IAW AMM 34-11-00 AND REPLACED ADC 2 IAW AMM 34-13-01.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 8,203 hrs · 7,102 cycles

AFT TWO CABIN OVERHEAD EMERGENCY LIGHTS INOP. RELAMPED OVERHEAD EMERGENCY LIGHTS IAW AMM 33-61-01. OPERATIONAL CHECKS GOOD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 8,465 hrs · 7,335 cycles

FOUND FS 280 LBL 9 1 CLIP ATTACHING TO FLOORBEAM CRACKED AND FLOOR SUPPORT ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW LBL 9 CLIP PER REO 601R 53-0054A.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 8,465 hrs · 7,335 cycles

FOUND PAX DOOR POWER ASSIST MOTOR MOUNT BRACKET (SIDE PANEL ANGLE) IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW STIFFENER PER CRJ200 SRM 51-42-06.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 8,465 hrs · 7,335 cycles

FOUND PAX DOOR OUTERHANDLE IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW OUTER HANDLE DOOR ASSY PER CRJ200 AMM 52-11-03-400-802.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 8,465 hrs · 7,335 cycles

FOUND FS 621 FLOOR SUPPORT ANGLE IS CRACKED AT LBL32, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLES AND STRAP AT FS 621 AS PER 601R-53-61-117 -1,-3 .

Part: FITTING — CRACKED (FUSELAGE) · airframe 8,465 hrs · 7,335 cycles

FOUND FS 280 RBL9 2 CLIPS ATTACHING TO FLOORBEAM CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW RBL 9 CLIP PER REO 601R 53-0054A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 8,465 hrs · 7,335 cycles

FOUND FS 280, AFT OUTBOARD CLIP AT RBL 9.00 CRACKED AT TOP RADIUS, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP/ANGLE PART 601R3113-58 PER CRJ200 SRM 51-42-21 AND 51-42-13.

Part: FITTING — CRACKED (FUSELAGE) · airframe 8,465 hrs · 7,335 cycles

FOUND CRACK IN INBOARD CLIP ON PRESSURE FLOOR SKIN AT FS 504.0 AND BL-27 RIGHT, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP PER STANDARD REPAIR 601R 53-0029B.

Part: PANEL — CRACKED (PAX DOOR) · airframe 8,465 hrs · 7,335 cycles

FOUND PAX DOOR AFT SIDE PANEL CRACKED 2 PLACES 2ND AND 3RD STEPS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER REO 601R 52-11-702.

Part: FITTING — CRACKED (FUSELAGE) · airframe 8,465 hrs · 7,335 cycles

FOUND CRACK IN CLIP ON AFT SIDE OF REAR PRESSURE BULKHEAD AT FS624.0 AND STA 15R ON RIGHT SIDE OF FUS DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP ONTO REAR PRESSURE BULKHEAD AT FS 624 AND STA 15R ON RT PER REO 601R 53-64-985.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 8,465 hrs · 7,335 cycles

FOUND PAX DOOR AFT DRAG ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER REO 601R-52-11-513.

Part: FITTING — CRACKED (FUSELAGE) · airframe 8,465 hrs · 7,335 cycles

FOUND CRACK IN CLIP ON AFT SIDE OF REAR PRESSURE BULKHEAD AT FS624.0 AND STR 15L ON LEFT SIDE OF FUS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP ONTO REAR PRESSURE BULKHEAD AT FS 624 AND STA 15L ON LT PER REO 601R 53-64-422.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 7,812 hrs · 6,762 cycles

LEFT WINDSHIELD SHATTERED INFLIGHT. DIVERTED TO SLC. REPLACED LEFT WINDSHIELD IAW AMM 56-11-01 AND RII 56-220-1000.

Part: FLUTTER DAMPER — LEAKING (AILERONS) · airframe 5,457 hrs · 4,668 cycles

INTERMITTENT FLUTTER DAMPER STATUS MESSAGE. REPLACED RT AILERON FLUTTER DAMPER IAW MM 27-15-05. OPERATIONAL CHECK GOOD.

Part: TRIM SWITCH — MALFUNCTIONED (ELEVATOR) · airframe 4,875 hrs · 4,181 cycles

CAPTAINS ELEVATOR TRIM SWITCH DOES NOT PITCH NOSE DOWN. REPLACED CAPT TRIM SWITCH REF, CRJ MM 27-41-05, OPERATIONAL CHECK GOOD.

Part: TRIM PANEL — MALFUNCTIONED (AILERON TRIM) · airframe 4,704 hrs · 4,038 cycles

AILERON TRIM DOESN'T WORK TO THE RIGHT. REPLACED FLIGHT CONTROL TRIM SWITCH PANEL. OPERATIONAL CHECK GOOD.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 4,339 hrs · 3,741 cycles

OUTER LAYER OF CAPTAIN WINDSHIELD SHATTERED. REPLACED CAPTAIN'S WINDSHIELD IAW MM 56-11-0.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 3,997 hrs · 3,461 cycles

FS 280 AT RBL 9.0 INBOARD AND OUTBOARD FLOORBEAM ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REMOVED AND REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, 51-23-00 .

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 3,997 hrs · 3,461 cycles

FS 280 AT LBL 9.0 OUTBOARD FLOORBEAM ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, 51-23-00.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 3,997 hrs · 3,461 cycles

RT FUSELAGE FLOOR SUPPORT ANGLE FS 621 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV "B" .

Part: NUT — LOOSE (CONTROL YOKE) · airframe 2,478 hrs · 2,191 cycles

F/O'S CONTROL YOKE CLICKS WHEN FULL DEFLECTION RIGHT OR LEFT AILERONS. RETORQUED NUT ON F/O'S YOKE AS REQUIRED, OPERATIONAL CHECKS GOOD.

Part: OVERHEAT LOOP — MALFUNCTIONED (LT MLG WW) · airframe 1,474 hrs · 1,328 cycles

MAIN LANDING GEAR OVERHEAT MESSAGE INFLIGHT. REPLACED LEFT MAIN LANDING GEAR BAY HARNESS OVERHEAT SENSOR LOOP. OPERATIONAL CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (AHRS) · airframe 560 hrs · 463 cycles

YAW DAMPER (YD) 1 TRIPPED OFF IN CRUISE. RESET (REPEATEDLY), GOT PROGRESSIVELY WORSE DOWN TO 2 SECONDS BETWEEN RESETS AND FAILS. ASSOCIATED: AP TRIPS OFF WITH YD1, AI NR 1 BLANKS OUT AND MAG FLAG APPEARS WITH YD1. VSI NR 1 ERRONEOUS INDICATIONS - SHOWS UP TO 1400 FPM DESCENT AND CLIMB WHILE IN LEVEL FLIGHT AND VSI NR 2 SHOWING 0 FPM UP/DOWN (IE LEVEL). STALL FAIL OCCURRED DESCENDING THROUGH 14,000 AT 3200. YD2 FAILED ON LANDING. REPLACED NR 1 AHRS COMPUTER. OPS CHECKS GOOD IAW CRJ MM 34-21-11.