N463SW

Part: UNKNOWN — SMOKE (CABIN) · airframe 43,048 hrs · 39,214 cycles

SMOKE IN THE CABIN WHILE WAITING ON TAXIWAY. HAD TO EVACUATE. (FLIGHT 5118 - FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS

Part: ACM — SMOKE (RIGHT) · airframe 43,048 hrs · 39,214 cycles

SMOKE IN THE CABIN WHILE WAITING ON TAXIWAY. HAD TO EVACUATE. (FLIGHT 5118) T/S SMOKE AND ABNORMAL SMELL/ODOR IN COCKPIT/CABIN PER FIM 21-21-00. LH ENG AND RH ENG BOROSCOPE INSPECTION. LH ENG AND RH ENG FOR ENG BOROSCOPE FINDINGS. APU BOROSCOPE INSPECTION. LH ACM AND RH ACM INSPECTION. RH ACM REPLACEMENT DUE TO EXCESSIVE OIL COMING OUT FROM RH ACM WATER SEPERATOR DRAIN. DUE TO FLIGHT CREW REPORT ABNORMAL SMELL/ODOR. REPLACEMENT OF LH AND RH PACK COALESCER BAG/SOCKS.DUE TO CABIN SMOKE EVENT, PAX EVACUATED. AIRCRAFT EMERGENCY LIGHT, FA FLASHLIGHT. BOTH OVERWING EMER DOORS NEEDS INSPECTION.

Part: RIB — DAMAGED (LT WING) · airframe 41,036 hrs · 37,098 cycles

DAMAGE FOUND ON LH WING FWD CLOSING RIB P/N 601R10854-29 AT WS389.00 IS OUT OF LIMITS AND CLASSIFIED TO BE A MAJOR REPAIR.INITIATED FORM M-337.SEE CP 27816132 FOR ORIGINAL DISCREPANCY. FILED CLOSEDREMOVED AND REPLACED LH WING FWD CLOSING RIB AT WS389.00 IAW DRAWING 601R10854 REV H AND REO 601R-57-21-3825 REV A DATED 2024-02-27. COMPLIED WITHTASK CARD 51-900-1003-SKY. COMPLETED FORM M-337. ALL WORK PERFORMED BY MHIRJ MRT REFERENCE ATTACHED STATEMENT OF WORK FOR INFORMATION.

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 40,906 hrs · 36,957 cycles

ANTI ICE DUCT WARNING MSG ON CLIMB OUT. QRH RESOLVED, WARNING EXTINGUISHED WHEN WING A/I TURNED OFF. NO WARNING WHEN WING A/I IN STBY. (FLIGHT 5018 - FILED CLOSED) SPOKE WITH PILOT AND ISOLATED ANTI-ICE DUCT WARNING MESSAGE TO RH WING. TROUBLESHOT ANTI-ICE DUCT WARNING MESSAGE REF CRJ200 FIM 36-20-00-01. USED MEGGER TO CHECK INSULATION RESISTANCE WITH RH BLCU CONNECTOR 2P1WK ON PYLON, FUSELAGE, AND RH WING SECTIONS. ALL THREE INSULATION RESISTANCE CHECKS WERE NORMAL INDICATING THERMAL SWITCHES IN RH WING ARE OPERATING NORMALLY. WHILE PERFORMING TEST OF THE BLCU SYSTEM, REF CRJ 200 AMM 36-21-10, RECEIVED CAS MISCOMP MESSAGE THAT WOULD NOT CLEAR. REMOVED AND REPLACED RH BLCU REF CRJ200 AMM 36-21-10. THEN RE-PERFORMED BLCU SYSTEM TEST MULTIPLE TIMES AND ALL TESTS WERE GOOD. PERFORMED OPERATIONAL TESTS OF WING ANTI-ICE SYSTEM REF CRJ200 AMM 30-12-00 WITH ENGINES RUNNING AT HIGH SPEED AND WING ANTI-ICE SYSTEM IN NORMAL MODE (AFTER REMOVAL AND REPLACEMENT OF RH BLCU). MULTIPLE TESTS WERE GOOD OF THE WING ANTI-ICE SYSTEM.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

SERVICE DOOR LOWER SEAL STRIKER IS CORRODED. LOWER SEAL STRIKER P/N 601R38533-9S REPLACED WITH NEW PART REF CRJ 200 SRM 51-41-02, CRJ 200 SRM 51-42-21 AND DWG 601R38340 REV. B.COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD . SEE CONTINUATION CARD FOR DETAILS.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

NLG WHEEL WELL SKIN CUT-OUT AT FS235.00 AND RBL6.0 HAS POSSIBLE CRACK IN THE SKIN (C-CHECK RO 11/21/2023) REPAIRED NLG WHEEL WELL SKIN CUT-OUT AT FS235.00 REF REO 601R-53-11-048 REV. -D DATED 2015-06-10, AND REO 601R-53-11-3896 REV. 2023-10-09. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

PAX DOOR DD3 CENTER INTERCOSTAL HAS A CRACK AT THE FWD FLANGE. (C-CHECK RO 11/21/2023) REMOVED INSTALLED NEW PAX DOOR DD3 INTERCOSTAL REF CRJ 200 SRM 51-42-06, CRJ-200 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 — CORRODED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

BAGGAGE COMPARTMENT DOOR FORWARD SEAL RETAINER HAS CORROSION (C-CHECK RO 11/21/2023) REPLACED AFT CARGO DOOR FWD SEAL RETAINER WITH NEW. REF CRJ200 SRM 51-42-06. REF CRJ200 SRM 51-42-21. DRAWING CC670-38702 REV D. LEAK CHECK GOOD. SEE CONTINUATION CARD FOR FURTHER DETAILS.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

RH FLOOR SILL AND NUTPLATES AT FS559+96- FS559+112 HAS AREAS OF CORROSION (C-CHECK RO 11/21/2023) REMOVED AND INSTALLED NEW REPLACEMENT RH FLOOR SILL AT FS559+96-FS559+112.REF CRJ200 SRM 51-42-06,SRM 51-42-21,DWG:601R31026 REV D. COMPLIED WITH 51-900--1003-SKY AND SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

SERVICE DOOR SILL FUSELAGE SIDE HAS CORROSION (C-CHECK RO 11/21/2023) REMOVED AND INSTALLED NEW SERVICE DOOR SILL BETWEEN FS 310.00 AND FS 349.00 PER CRJ 200 SRM 51-42-06, CRJ-200-SRM51-42-21 AND DWG # 601R38303 REV AR , COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

FLOOR BEAM SUPPPORT FITTING ON RBL9 FS461 IS CRACKED (C-CHECK RO 11/21/2023) REMOVED AND INSTALLED NEW FLOOR BEAM SUPPORT OUTBOARD FITTING ON RBL9 AT FS461 REF CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 WITH DRAWINGS 601R31118 REV L AND 600-31146 REV L FOR FASTENER TYPE AND SIZE.. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

PAX DR CLEAT ON LOWER CHANNEL FS320 HAS CORROSION (C-CHECK RO 11/21/2023) REMOVED AND INSTALLED NEW REPLACEMENT CLIP P/N 600-31902-276 AT PAX DOOR FRAME FS.320 & LWR CHANNEL REF. CRJ200 SRM 51-42-06 & BOMBARDIER DWG. 600-31902 REV. Y . COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD . SEE CONTINUATION CARD FOR DETAILS WEIGHT STATEMENT: PART FOR PART REPLACEMENT. NO WEIGHT CHANGE NOTED

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

PAX DR AFT INTERCOSTAL DD1 HAS CORROSION (C-CHECK RO 11/21/2023) REMOVED AND INSTALLED NEW PAX DOOR DD1 INTERCOSTAL 601R31802-318 REF CRJ 200 SRM 51-42-06 AND DWG 601R31702 REV N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD . SEE CONTINUATION FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

PAX DR AFT INTERCOSTAL DD3 HAS CORROSION (C-CHECK RO 11/21/2023) REMOVED AND INSTALLED NEW AFT DD3 INTERCOSTAL REF DWG 601R31702 REV N AND CRJ 200 SRM 51-42-06. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

PAX DR AFT INTERCOSTAL DD5 HAS CORROSION (C-CHECK RO 11/21/2023) REMOVED AND INSTALLED NEW PAX DOOR AFT INTERCOSTAL DD5 PN 601R31902-317 REF CRJ 200 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 — CORRODED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

PAX DR AFT INTERCOSTAL DD1A HAS CORROSION (C-CHECK RO 11/21/2023) REMOVED AND REPLACED INTERCOSTAL DD1A REF. DRAWING 601R31702 REV. -N AND CRJ200 SRM 51-42-06. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. NO DEFECTS NOTED.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

AFT SIDE OF THE REAR PRESSURE BULKHEAD THE CLIP ON INTERCOSTAL AT APPROXIMATELY STGR15R IS CRACKED. (MARKED) (C-CHECK RO 11/21/2023) REPLACED CRACKED FS 625 & STR 15R CLIP WITH NEW PN 601-35012-52 REF CRJ 200 SRM 51-42-06 AND DWG 601-35012 REV D. COMPLIED WITH SKY CARD 51-900-1003-SKY STRUCTURAL MAJOR REPAIR.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

AFT SIDE OF THE REAR PRESSURE BULKHEAD THE CLIP ON INTERCOSTAL AT APPROXIMATELY STGR15L IS CRACKED. (MARKED) (C-CHECK RO 11/21/2023) REPLACED FS 625 & STR 15L CLIP WITH NEW PN 601-35012-51 REF CRJ 200 SRM 51-42-06 AND DWG 601-35012 REV D. COMPLIED WITH SKY CARD 51-900-1003-SKY STRUCTURAL MAJOR REPAIR.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

CRACK ON CLIP AT STRG3L AFT OF FS280 (C-CHECK RO 11/21/2023) REMOVED AND INSTALLED STRINGER CLIP @ STR 3L AFT OF FS 280 REF DWG 600-31057 REV P , CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

LEFT WING INBOARD TRAILING EDGE RIB WS130.10 IS CRACKED AT THE AFT LOWER EDGE. (MARKED) 27189081 (C-CHECK RO 11/21/2023) REPAIRED LH WING INBD TRAILING EDGE RIB AT WS130.10 BY COMPLYING WITH ALL STEPS OF REO 601R-57-51-1029 REV-- DATED 2023-09-22. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

UPON REMOVAL ON JOB HN00112316, CAMP 27162486, FOUND R/H ELEVATOR L/E HINGE FITTING ASSY P/N 600-24043-1 LOCATED AT ES16.52 TO HAVE PITTING CORROSION IN BEARING BORES OF BOTH HINGE HALVES. REPLACE HINGE FITTING ASSY. (C-CHECK RO 11/21/2023) REMOVED AND REPALCED 1 NEW HINGE FITTING ASSEMBLY (PN 600-24043-1) ON R/H ELEVATOR AT L/E ES 16.52 REF BOMBARDIER DWG # 601R24025, REV G AND CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. COMPLIED FULLY W/SKYCARD 51-900-1003-SKY. SEE CONTINUATION SHEET FOR DETAILS.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

RIGHT WING INBOARD TRAILING EDGE RIB WS130.10 IS CRACKED AT THE AFT LOWER EDGE. (MARKED) (C-CHECK RO 11/21/2023) REPAIRED R/H WING INBOARD TRAILING EDGE RIB AT WS 130.10 REF R.E.O. 601R-57-51-1030 REV. -- DATED 2023-09-22 . COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

PAX DOOR AFT FORMER FS347.25 HAS MULTIPLE CORRODED AREAS. (C-CHECK RO 11/21/2023) REMOVED AND INSTALLED NEW PAX DOOR AFT FORMER FS347.25. REF DWG 601R31702 REV-N AND CRJ 200 SRM 51-42-06. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

PAX DOOR FWD DD5 INTERCOSTAL HAS CORROSION(MARKED). (C-CHECK RO 11/21/2023) REMOVED AND INSTALLED NEWPAX DOOR FWD DD5 INTERCOSTAL 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 — DAMAGED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

UPON REMOVAL OF BEARING FOUND BORE IN HINGE FITTING ASSY. TO BE PITTED. REPLACE HINGE FITTING ASSY. P/N 600-24043-1. (C-CHECK RO 11/21/2023) INSTALLED NEW HINGE FITTING ASSY. P/N 600-24043-1 LOCATED ON L/H ELEVATOR L/E @ ES16.52 REF CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21 AND DWG# 601R24025, REV G. COMPLED FULLY W/SKYCARD 51-900-1003-SKY. SEE CONTINUATION SHEET FOR DETAILS.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

CREW ESCAPE HATCH OUTER HANDLE INNER SPRING IN THE HOUSING IS CORRODED (C-CHECK RO 11/21/2023) REMOVED AND INSTALLED NEW CREW ESCAPE HATCH HANDLE HOUSING REF CRJ-200-SRM 51-42-06 AND DRAWING 600-33046 REV G . COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

AVIONIC DOOR AN ANGLE ON THE AFT SIDE OF THE DOOR HAS 2EA AREAS OF CORROSION (C-CHECK RO 11/21/2023) REMOVED AND INSTALLED NEW AVIONIC DOOR AN ANGLE ON THE AFT SIDE OF THE DOOR REF DRAWING CC670-38651 REV E, CRJ 200 SRM 51-42-21, AND CRJ 200 SRM 51-42-06 . COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

LH WING INBOARD FLAP CENTER VANE CAP REQUIRES REPLACEMENT DUE TO DAMAGE TO PREVIOUS REPAIR (C-CHECK RO 11/21/2023) REPLACED LH WING INBOARD FLAP, CENTER VANE CAP WITH NEW PN 601R14303-51 REF CRJ 200 SRM 51-42-13 AND DWG 601R14302 REV E . COMPLIED WITH SKY CARD 51-900-1003-SKY STRUCTURAL MAJOR REPAIR.

Part: UNKNOWN — DENTED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

EXTERNAL SKIN DENT NEAR FS265 BETWEEN STGR26L-STGR25L (C-CHECK RO 11/21/2023) REPAIRED FUSELAGE EXTERNAL SKIN NEAR FS265 BETWEEN STGR 26L AND STGR25L REF REO 601R-53-11-3890 REV -- DATED 2023-10-06. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD . SEE CONTIUNATION CARD FOR DETAILS

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 40,786 hrs · 36,828 cycles

PASSENGER DOOR SEAL STRIKER - PREVIOUS REPAIR ON THE SEAL STRIKER IS DAMAGED, FS310.00 STGR6L - 7L. (C-CHECK RO 11/21/2023) REPAIRED PASSENGER DOOR SEAL STRIKER REF REO 601R-53-22-033 REV -D DATE 2014-02-17 . COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: NONE — FAILED · airframe 39,028 hrs · 35,140 cycles

D:NOSE DISAGREE ON RETRACTION. AFTER APPROXIMATELY 30 MORE SECONDS, NOSE WHEEL SHOWED UP AND LOCKED. FOLLOWED QRH. RETURN TO FIELD. / C:MEL 32-30-1 / CAT A DUE 9/JUN/22 / NOSE DISAGREE ON RETRACTION. AFTER APPROXIMATELY 30 MORE SECONDS, NOSE WHEEL SHOWED UP AND LOCKED. FOLLOWED QRH. RETURN TO FIELD. (FLIGHT 4725 - FILED CLSOED) JUL 08, 2022 STATION: DEN--PERFORMED VISUAL INSPECTION OF NLG SENSORS FOR DAMAGE. NONE NOTED AT THIS TIME. INTERROGATED PSEU FOR FAULTS. CODES ARE AS FOLLOWS: LEG #7: S36DOWNFAR, S25DOWNFAR, S38DOWNFAR, S26DOWNFAR, S40DOWNFAR, S27DOWNFAR, S41DOWNFAR, DI16DOWNOFF, S46DOWNFAR, DI17DOWNOFF, S47DOWNFAR, S48DOWNFAR, S30DOWNFAR, S31DOWNFAR, S32DOWNFAR. LEG#10: S21DOWNNEAR, S22DOWNFAR, S35DOWNNEAR, S31DOWNFAR, S32DOWNFAR, S30DOWNFAR, DI14DOWNON. DEFERRED LANDING GEAR RETRACTION SYSTEM PER MEL 32-30-1. AUTHORIZED BY MCC. MX ACTIONS COMPLIED WITH. PLACARDS INSTALLED. AC DOWNGRADED CAT II NOT AUTHORIZED.

Part: NONE — FAILED · airframe 39,005 hrs · 35,118 cycles

D:GEAR DISAGREE WARNING MESSAGE CLIMBING THROUGH FL200. NOSE GEAR INDICATION AMBER THEN TURNED RED. COMPLETED QRH WHICH SUCCESSFULLY LOWERED THE GEAR WITH 3 GREEN INDICATIONS. DIVERTED TO KOMA WITH NIL INCIDENT. / C:MEL 32-30-1 / CAT A DUE 28/JUN/22 / ****ODI REQUIRES MANAGEMENT APPPOVAL FOR RTS****** / GEAR DISAGREE WARNING MESSAGE CLIMBING THROUGH FL200. NOSE GEAR INDICATION AMBER THEN TURNED RED. COMPLETED QRH WHICH SUCCESSFULLY LOWERED THE GEAR WITH 3 GREEN INDICATIONS. DIVERTED TO KOMA WITH NIL INCIDENT. (FLIGHT 5054 - FILED CLOSED) JUN 17, 2022 STATION: OMA--DEFERRED LANDING GEAR RETRACTION SYS IAW CRJ200 MEL 32-30-1 MX ACTION C/W PLACARD INSTALLED CAT II DOWNGRADED / JUN 20, 2022 STATION: ORD -- TROUBLESHOT GEAR DISAGREE PER CRJ 200 FIM 32-60-09. REMOVED AND REPLACED NLG UPLOCK ASSEMBLY IAW CRJ200 AMM 32-33-05. OPS CHECK GOOD. NO GEAR DISAGREE MESSAGE NOTED. DMI CLEARED. UNCOMPLIED WITH MAINTENANCE ACTION. PLACARD REMOVED.

Part: OIL COOLER — LEAKING (APU) · airframe 37,837 hrs · 34,100 cycles

ON SHORT FINAL RECEIVED SMOKE IN THE FLIGHT DECK AND CABIN AND SHORTLY AFTER RECEIVED APU OIL PRESS CAUTION MESSAGE. COMPLIED WITH QRH AND SMOKE STARTED DISSIPATING. (FLIGHT 5294 - FILED CLOSED) PERFORMED TROUBLESHOOTING IAW FIM 21-21-00. FOUND APU OIL COOLER LEAKING AND APU WITH LOW OIL, REMOVED AND REPLACED APU OIL COOLER IAW AMM 49-91-07 AND SERVICED APU WITH OIL IAW AMM 12-13-49. LEAK CHECK GOOD. REMOVED AND REPLACED BOTH LH AND RH WATER SEPARATOR COALESCERS IAW AMM 21-51-13. PERFORMED OPS CHECK OF BOTH PACKS WITH APU AND ENGINES RUNNING, NO SMOKE OR ABNORMAL SMELLS NOTICED IAW AMM 21-51-00. INSPECTED THE APU OIL MAGNETIC DRAIN PLUG FOR METAL DUE TO APU OIL PRESS CAUTION IAW AMM 49-91-15. NO METAL CONTAMINATION FOUND. REMOVED APU LCV AND INSPECTED FOR OIL CONTAMINATION ON THE LCV AND INSIDE THE APU, NO OIL CONTAMINATION NOTED. CLEANED ALL OIL FROM APU ENCLOSURE AND SURROUNDING AREAS AS REQUIRED.

Part: NONE — FAILED · airframe 37,773 hrs · 34,040 cycles

D: ON APPROACH INTO DEN WHEN LANDING GEAR LEVER WAS SELECTED DOWN, WE RECEIVED AN INTERMITTENT GEAR DISAGREE MESSAGE. AFTER APPROXIMATELY 20 SECONDS OF THIS RECURRING INTERMITTENT MESSAGE, THE GEAR INDICATED DOWN AND LOCKED AND THE MESSAGE DISAPPEARED. WE BROKE OFF THE APPROACH, REQUESTED DELAY VECTORS AND RAN QRH VOL 2 EMERGENCY 13-3 PROCEDURE. AFTER COMPLETING CHECKLIST AND SELECTING HYDRAULIC PUMP 2 AND 3B TO ON, WE REQUESTED ANOTHER APPROACH AND LANDED THE AIRCRAFT WITHOUT FURTHER INCIDENT. / C: MEL 32-30-1 / CAT: A DUE 10/06/21 / CAT: / ON APPROACH INTO DEN WHEN LANDING GEAR LEVER WAS SELECTED DOWN, WE RECEIVED AN INTERMITTENT GEAR DISAGREE MESSAGE. AFTER APPROXIMATELY 20 SECONDS OF THIS RECURRING INTERMITTENT MESSAGE, THE GEAR INDICATED DOWN AND LOCKED AND THE MESSAGE DISAPPEARED. WE BROKE OFF THE APPROACH, REQUESTED DELAY VECTORS AND RAN QRH VOL 2 EMERGENCY 13-3 PROCEDURE. AFTER COMPLETING CHECKLIST AND SELECTING HYDRAULIC PUMP 2 AND 3B TO ON, WE REQUESTED ANOTHER APPROACH AND LANDED THE AIRCRAFT WITHOUT FURTHOCT 05, 2021 STATION: DEN--DEFERRED LANDING GEAR RETRACTION SYSTEM PER MEL 32-30-1. AUTHORIZED BY MCC. MX ACTION COMPLIED WITH GEAR PINS INSTALLED. PLACARDS INSTALLED. AIRCRAFT HAS BEEN DOWNRADED FROM CATII STATUS. CATII NOT AUTHORIZED. PLACED GEAR PIN FLAGS IN COCKPIT CLOSET.

Part: ENGINE — POWER LOSS (LEFT) · airframe 36,330 hrs · 32,766 cycles

CREW REPORTS: AT APPROXIMATELY 1000 TO 2000' AGL AFTER TAKEOFF. FELT A SLIGHT SHUDDER AND LT ENGINE ITT WENT TO ROUGHLY 900C THEN NOTICED N1 SPOOLED DOWN TO ROUGHLY IDLE. LT ENGINE WAS NOT RESPONSIVE TO THRUST LEVER ADJUSTMENT AT ANY SETTING ABOVE IDLE. SECURED ENGINE PER THE QRH. TRIED RESTART OF ENGINE AND ENGINE WOULD NOT ACCELERATE ABOVE AN IDLE. EMERGENCY DECLARED. RETURNED TO BIS. NO OVERWEIGHT OR HARD LANDING. REMOVED AND REPLACED LEFT ENGINE, IN REF TO THE AMM AND TASK CARD. OPERATIONS AND LEAK CHECK GOOD. CALIBRATED TOOLS, TORQUE WENCHES S/N 0201302328, 0213500244 AND 1006200835. DYNAMOMETER S/N D34420.

Part: CARGO TRACK — CORRODED (BS 564-621) · airframe 36,152 hrs · 32,596 cycles

CARGO TIE-DOWN RAIL RBL9 FS564-FS621 HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND INSTALLED NEW CARGO TIEDOWN TRACK IAW AMM.

Part: SUPPORT ANGLE — CHAFED (PAX DOOR) · airframe 36,152 hrs · 32,596 cycles

PAX DOOR FWD SUPPORT ANGLE (UNDER FWD PULL IN LEVER) IS CHAFED. (C-CHECK) RO 8/28/2020 REMOVED CHAFFING FROM PAX DOOR FWD SUPPORT ANGLEREF CRJ 200 SRM. ORIGINAL THICKNESS OF PAX DOOR FWD SUPPORT ANGLE IS .063€? REF. CRJ200 SRM, MATERIAL REMAINING AFTER REMOVAL OF CHAFE DAMAGE IS .042€?, A MATERIAL LOSS OF .021€? OR 33%, MAKING ANGLE OUT OF LIMITS REF. CRJ200 SRM, WHICH ALLOWS MAX. MATERIAL LOSS OF 10%. REPLACE ANGLE. INSTALLED FWD. FRAME SUPPORT ANGLE ON PASSENGER DOOR. REF: CRJ-200 SRM AND DWG. PRERSSURE CHECKS GOOD.

Part: FORMER — CHAFED (BS 311) · airframe 36,152 hrs · 32,596 cycles

PAX DOOR FWD FORMER (UNDER FWD PULL IN LEVER) IS CHAFED. (C-CHECK) RO 8/28/2020 REMOVED CHAFFING FROM PAX DOOR FWD FORMER REF. CRJ 200 SRM. ORIGINAL THICKNESS OF PAX DOOR FWD FORMER IS .063€? REF. CRJ200 SRM, MATERIAL REMAINING AFTER REMOVAL OF CHAFE DAMAGE IS .040€?, A MATERIAL LOSS OF .023€? OR 37%, MAKING FORMER OUT OF LIMITS REF. CRJ200 SRM, WHICH ALLOWS MAX. MATERIAL LOSS OF 10%. REPLACE FORMER. INSTALLED FWD. FORMER ON PASSENGER DOOR. REF: CRJ-200 SRM AND DWG. COMPLIED WITH A PRESSURE LEAK CHECK. ALL CHECKS GOOD.

Part: TRUNNION — DAMAGED (RT MLG) · airframe 36,152 hrs · 32,596 cycles

WHILE COMPLYING WITH THE REPLACEMENT OF THE RHS MLG TRUNNION FITTING (REF 601R-57-21-3318) 2EA MISDRILLED HOLES (0.125" DIA) WERE FOUND IN THE LOWER AFT WING PLANK. (REF SB). NOTE 9 RIVET ARE NOT INSTALLED THROUGH THE LOWER AFT WING PLANK. (C-CHECK) RO 8/28/2020 REPAIRED MISDRILLED HOLES IN RH WING LOWER AFT PLANK PER REO.

Part: TRUNNION — WRONG PART (MLG) · airframe 36,152 hrs · 32,596 cycles

SB 601R-57-048 REV C (PART B) REQUIRED ON RHS TRUNNION DUE TO TRUNNION REPLACEMENT. REWORKED THE HOLES IN THE NEW RHS TRUNNION FITTING WEB PER REO, RIL AND IN REF ONLY TO SB REV C DATE JUN 06/2013.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 36,152 hrs · 32,596 cycles

UPON REMOVAL OF SEAT TRACK TO FOM FOR FLOOR BEAM REPLACEMENT, FOUND SEAT TRACK SECTION TO BE CORRODED FROM FS 559-94 TO FS 559+116 (C-CHECK) RO 8/28/2020 REPLACED SEAT TRACK FROM FS 559+94 TO FS 559+116. REF: CRJ-200 AMM. SEE CONTINUATION CARD FOR DETAILS.

Part: PANEL — CHAFED (RT MLG) · airframe 36,152 hrs · 32,596 cycles

R/H MLG APRON PANEL HAS DEEP LONG CHAFE DAMAGE IN LINE WITH WING UPPER PANEL SEAL FROM FS.529 TO FS.559 . (C-CHECK) RO 8/28/2020 REPAIRED THE RHS APRON ASSY SKIN PANEL REF REO.

Part: ANGLE — CRACKED (LWS 53) · airframe 36,152 hrs · 32,596 cycles

* LH FWD BATT RIB ANGLE AT WS 53.60 IS CRACKED AT TOP END. REPAIRED CRACK ON LH FWD BATT RIB ANGLE AT WS 53.60 AT TOP END PER REO. COMPLIED WITH SKY CARD.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 36,152 hrs · 32,596 cycles

FLOORBEAM ATTACHMENT CLIP AT INBOARD RBL9.0 BEAM FS280 CRACKED (C-CHECK) RO 8/28/2020 COMPLIED WITH REPAIR ON FLOOR BEAM ATTACHMENT CLIP AT FS280.00 RBL9 INBD SIDE, REF CRJ200 SRM, AND REO.

Part: FRAME — CRACKED (BS 333) · airframe 36,152 hrs · 32,596 cycles

*FS333.00 BETWEEN STRINGER 0 AND STRINGER 1L HAS A CRACK AT TOOLING HOLE. (C-CHECK) RO 8/28/2020 REMOVED FRAME AT FS 333.0 STR 1L - 5L REF CRJ 200 SRM 51-42-06. INJSTALLED NEW FRAME SECTION AT FS 333.00 STR 1L - 5L REF CRJ 200 SRM AND BOMBARDIER DWG. COMPLIED WITH PRESSURE LEAK CHECKS, ALL CHECKS GOOD.

Part: NUT — CORRODED (RT ELEVATOR) · airframe 36,152 hrs · 32,596 cycles

*RH ELEV NUTS, 4 EACH, ON THE HINGE ATTACH BOLTS ARE CORRODED (MARKED) (C-CHECK) RO 8/28/2020 REMOVED AND INSTALLED WITH 3EA NEW NUTS ON THE R/H ELEVATOR HINGE ATTACH BOLTS REF CRJ 200 AMM. OPS GOOD.

Part: ANGLE — CORRODED (BS 319) · airframe 36,152 hrs · 32,596 cycles

CLIP AT FS319 / STGR 21L HAS CORROSION. (C-CHECK) RO 8/28/2020 REMOVED CLIP AT FS319 / STGR 21L FOR CORROSION REMOVAL CRJ200 SRM. CORROSION COVERS MORE THAN 30 PERCENT OF PART. DAMAGE FOUND TO BE OUT OF LIMITS PER CRJ200 SRM. FABRICATED NEW PART USING P/N: S6144-33 PO: T55304 REF BOMBARDIER DWG. INSTALLED CLIP AT FS 319.00 IAW CRJ200 SRM.

Part: NUT — CORRODED (LT ELEVATOR) · airframe 36,152 hrs · 32,596 cycles

*LH ELEV NUTS, 4 EACH, ON THE HINGE ATTACH BOLTS ARE CORRODED (MARKED) (C-CHECK) RO 8/28/2020 REMOVED AND INSTALLED 4EA NEW NUTS ON THE L/H ELEVATOR HINGE ATTACH BOLTS REF CRJ 200 AMM. OPS GOOD

Part: INTERCOSTAL — CORRODED (BS 310-333) · airframe 36,152 hrs · 32,596 cycles

* INTERCOSTAL BETWEEN FS 310.00 AND FS 333.00 AT STGR 21L HAS CORROSION SEVERAL PLACES. (C-CHECK) RO 8/28/2020 REPLACED WITH NEW INTERCOSTAL FROM FS310.00 AND FS333.00 AT STGR21L IAW REO, CRJ 200 SRM, AND DWG. SEE CONTINUE CARD FOR DETAILS. OPERATIONAL CHECKS GOOD. PRESSURE CHECKS GOOD.

Part: BRACKET — CORRODED (DOOR SILL) · airframe 36,152 hrs · 32,596 cycles

THE PASSENGER DOOR SURROUND-STRUCTURE'S FWD AND AFT LOWER FLOOR SILL BRACKET ASSEMBLIES, WHERE THE PAX DOOR HANDRAIL ACTUATOR RODS STOW, ARE BOTH CORRODED. BLENDED CORROSION ON FWD AND AFT SILL BRACKET ASSY. IAW CRJ200 SRM. FOUND FWD SILL BRACKET TO BE IN LIMITS IAW SRM. MEASURED THICKNESS .063. ORIGINAL THICKNESS .063. NO MATERAL LOSS NOTED. DAMAGE ON AFT SILL BRACKET IS 100% MATERIAL LOSS. THE ALLOWABLE LOSS IS 10% IAW SRM, OUT OF LIMITS. INSTALLED NEW PAX DOOR SURRONDING AFT LWR SILL BRACKET ASSY. REF. SRM AND DWG.

Part: MOUNT — CORRODED (CABIN FLOOR) · airframe 36,152 hrs · 32,596 cycles

* CABIN FLOOR STRUCTURE AFT OBD MOUNT PLATE FOR WARDROBE CORRODED. MOUNTING PLATE FOUND TO BE OUT OF LIMITS REF CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILS. REMOVED AND REPLACED WITH NEW WARDROBE MOUNTING PLATE AT FS310, LBL20 REF CRJ200 SRM

Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 36,152 hrs · 32,596 cycles

* THE PASSENGER DOOR'S AFT ANCHOR FITTING IS SCRATCHED, GOUGED, AND HAS CORRODED ATTACH HARDWARE. (C-CHECK) RO 8/28/2020 REMOVED AND REPLACED PASSENGER DOOR AFT ANCHOR FITTING WITH 6EA NEW BOLS, 6EA NEW WASHERS AND 6EA NEW NUTS REF CRJ 200 AMM. ADJUSTMENT AND OPS CHECK ARE GOOD.

Part: BRACKET — CRACKED (RT MLG) · airframe 36,152 hrs · 32,596 cycles

* THE RH MLG BRAKE PRESSURE TRANSDUCER MOUNTING BRACKET AND HYDRAULIC LINE MOUNTING BRACKET, JUST FWD OF THE TRANSDUCERS, ARE BOTH CRACKED AT 3 LOCATIONS IN THE RH MLG BAY. (MARKED WITH BLACK GREASE PENCIL AND ORANGE FLAG TAPE) (C-CHECK) RO 8/28/2020 REMOVED BOTH MLG BRAKE PRESSURE TRANSDUCER MOUNTING BRACKET AND HYDRAULICLINE MOUNTUNG BRACKET IAW CRJ200 SRM, LOCATED AND DRILLED NEW BRACKETS IAW CRJ200 SRM, REMOVED ATTACHING CLAMPS ON HYDRAULIC LINES, REINSTALLED ATTACHING CLAMPS ON HYDRAULIC LINES IAW CRJ200 SRM, INSTALLED NEW BRACKETS 601R75262-157 AND 601R75262-155 IAW CRJ200 SRM. COMPLIED WITH. PERFORMED PRESSURE CHECK OF REPAIRED AREA REF. CRJ 200 AMM. CHECK GOOD.

Part: TRACK — CRACKED (CARGO DOOR) · airframe 36,152 hrs · 32,596 cycles

* CARGO DOOR FWD TRACK LOWER ATTACHMENT BRACKET CRACKED. (C-CHECK) RO 8/28/2020 REMOVED AND REPLACED CARGO DOOR FWD TRACK LOWER ATTACHMENT BRACKET CHANNEL AND RESTORED FINISH REF CRJ200 SRM

Part: FLOORBEAM — CRACKED (BS 280) · airframe 36,152 hrs · 32,596 cycles

* FLOOR BEAM ATTACHMENT CLIP AT OBD SIDE LBL 9.0 BEAM FS 280.00 CRACKED. (C-CHECK) RO 8/28/2020 REMOVED AND DISCARDED CRACKED ATTACHMENT CLIP, RECEIVED LOCATED DRILLED AND INSTALLED NEW CLIP PN# 601R31113-57, AT FS280.00 FLOOR SUPPORT LBL9. OUTBD SIDE. REF CRJ200 SRM. AND PREVIOUSLY INCORPERATED REO.

Part: ACCESS PANEL — CORRODED (COCKPIT) · airframe 36,152 hrs · 32,596 cycles

* FLIGHT COMPARTMENT CENTER FLOOR ACCESS PANEL AFT SUPPORT ANGLE AT FS 280.00 CORRODED. (C-CHECK) RO 8/28/2020 COMPLIED WITH REPAIR ON FLIGHT COMPARMENT FLOOR SUPPORT STUCTURE AFT ANGLE AT FS280.00. REF CRJ200 SRM, AND DRAWING.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 36,152 hrs · 32,596 cycles

* FLOOR BEAM ATTACHMENT CLIP AT INB SIDE LBL 9.0 BEAM FS 280.00 CRACKED. (C-CHECK) RO 8/28/2020 REMOVED AND DISCARDED DAMAGED ATTACHMENT CLIP, RECEIVED LOCATED DRILLED AND INSTALLED NEW ANGLE CLIP PN# 601R31113-57 AT FS280.00 LBL9 INBD SIDE, REF CRJ200 SRM.

Part: FLOOR SUPPORT — CORRODED (BS 353) · airframe 36,152 hrs · 32,596 cycles

* L/H CABIN FLOOR SILL HAS CORROSION AROUND SCREW HOLE AT APPROX. FS 353.00. REMOVED 2 EA NUTPLATES ON LH FLOOR SILL AT FS353. REF REO. BLENDED OUT DAMAGE AREA ON LH FLOOR SILL AT FS353. REF REO. INSTALLED 2EA NEW NUTPLATES. RESTORED THE FINISH ON BLENDED AREA OF LH CABIN FLOOR SILL SCREW HOLE AT FS 353.00 REF CRJ 200 SRM.

Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 36,152 hrs · 32,596 cycles

* THE PASSENGER DOOR'S FWD ANCHOR FITTING IS CRACKED, CORRODED, AND HAS CORRODED ATTACH HARDWARE. (C-CHECK) RO 8/28/2020 REMOVED AND REPLACED PASSENGER DOOR FWD ANCHOR FITTING WITH 6EA NEW BOLS, 6EA NEW WASHERS AND 6EA NEW NUTS REF CRJ 200 AMM.ADJUSTMENT AND OPS CHECK ARE GOOD.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 36,152 hrs · 32,596 cycles

* FLOOR BEAM ATTACHMENT CLIP AT OBD SIDE RBL 9.0 BEAM FS 280.00 CRACKED. (C-CHECK) RO 8/28/2020 COMPLIED WITH REPAIR ON FLOOR BEAM ATTACHMENT CLIPS, AT FS280.00 RBL9 OUTBD SIDE, REF REO.

Part: SEAT TRACK — CORRODED (BS 364-400) · airframe 36,152 hrs · 32,596 cycles

* CABIN FLOOR SEAT RAIL SECTION RBL 9.0 APPROX. FS 364.00 TO FS 400.00 HAS CORROSION SEVERAL PLACES. REMOVED AND REPLACED SEAT RAIL FS364-FS400 RBL9 IAW AMM 53-01-11-000-802, AND 53-01-11-400-802.

Part: SEAT TRACK — CHAFED (BS 559) · airframe 36,152 hrs · 32,596 cycles

* SIDE SEAT RAIL, L/H, HAS CHAFES AT APPROX. FS 559.00 + 22. (C-CHECK) RO 8/28/2020 REMOVED AND REPLASED L/H SIDE SEAT RAIL FS554-FS559+64 REF. CRJ 200 AMM.

Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 36,152 hrs · 32,596 cycles

* THE PASSENGER DOOR AFT ANCHOR FITTING'S SERRATED PLATE IS CORRODED. (C-CHECK) RO 8/28/2020 REMOVED AND REPLACED PASSENGER DOOR AFT ANCHOR FITTING SERRATED PLATE WITH 4EA NEW SCREWS REF CRJ 200 AMM. ADJUSTMENT AND OPS CHECK ARE GOOD.

Part: PLATE — CORRODED (PAX DOOR) · airframe 36,152 hrs · 32,596 cycles

* THE PASSENGER DOOR FWD ANCHOR FITTING'S SERRATED PLATE IS CORRODED. (C-CHECK) RO 8/28/2020 REMOVED AND INSTALLED NEW PASSENGER DOOR FWD ANCHOR FITTING SERRATED PLATE REF CRJ2000 AMM. ADJUSTMENT AND OPS CHECK ARE GOOD.

Part: ANGLE — CRACKED · airframe 36,152 hrs · 32,596 cycles

*R/H BATT RIB CAP IS CRACKED AT WS48.30. (C-CHECK) RO 8/28/2020 REMOVED AND REPLACED DAMAGED RHS BATT RIB ANGLE (P/N 600-10389-2) REF DWG, CRJ200 SRM.

Part: ANGLE — CORRODED · airframe 36,152 hrs · 32,596 cycles

*R/H ANGLE ON FWD END OF BATT RIB AT WS 53.60 IS CORRODED AROUND CANNON PLUG CONNECTERS. (C-CHECK) RO 8/28/2020 REMOVED CORROSION FROM THE RH ANGLE REF. CRJ200 SRM. ORIGINAL THICKNESS OF ANGLE = .080" REF CRJ200 SRM, MATERIAL REMAINING AFTER BLEND = .031", MATERIAL LOSS = .049", BLEND IS OUT OF LIMITS REF CRJ200 SRM. REMOVED AND REPLACED THE CORRODED RH ANGLE (P/N 601R10203-34) ON FWD END OF BATT RIB AT WS 53.60 REF DWG, AND CRJ200 SRM.

Part: ANGLE — CRACKED · airframe 36,152 hrs · 32,596 cycles

*L/H CHANNEL ON AFT END OF BATT RIB AT WS53.60 IS CRACKED AT UPPER FWD EDGE. (C-CHECK) RO 8/28/2020 REPLACED L/H CHANNEL WITH NEW ON AFT END OF BATT RIB AT WS53.60 AT UPPER FWD EDGE REF CRJ 200 SRM, CRJ 200 SRM, CRJ 200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 36,152 hrs · 32,596 cycles

*R/H PRESSURE FLOOR SILL ANGLE HAS CORROSION AT NUMEROUS LOCATINS BETWEEN FS 409+128 AND FS 559. (C-CHECK) RO 8/28/2020 BLENDED R/H PRESSURE FLOOR SILL ANGLE AT 17EA LOCATIONS, REF REO. SEE CONTINUE CARD FOR DETAILS, PRESSURE CHECK GOOD, COMPLIED WITH TASK CARD.

Part: SEAT TRACK — CORRODED (BS 574-621) · airframe 36,152 hrs · 32,596 cycles

*SEAT TRACK AT FS 574-621 LBL 9 CORRODED. INSTALLED NEW CARGO TIE-DOWN TRACK LBL9 FS574-FS621 REF. CRJ 200 AMM USING TUC8606 DUE 10/31/20.

Part: CAP — CRACKED · airframe 36,152 hrs · 32,596 cycles

*L/H BATT RIB CAP IS CRACKED AT WS48.30. (C-CHECK) RO 8/28/2020 REPLACED LH BATT RIB CAP ANGLE AT WS 48.30 WITH NEW PN 600-10389-1 REF CRJ 200 SRM AND BOMBARDIER DWG. COMPLIED WITH SKY CARD.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 36,152 hrs · 32,596 cycles

*L/H PRESSURE FLOOR SILL HAS CORROSION AT NUMEROUS LOCATINS BETWEEN FS 409+128 AND FS 559. BLENDED L/H PRESSURE FLOOR SILL AT 14EA LOCATIONS,9EA LOCATIONS IN LIMITS REF REO, 5EA LOCATIONS OUT OF LIMITS REF REO. SEE CONTINUE CARD FOR DETAILS, PRESSURE CHECK GOOD, COMPLIED WITH TASK CARD

Part: STRAP — CORRODED (BS 559) · airframe 36,152 hrs · 32,596 cycles

*FLOOR STRAP AT FS 559.0 LBL 18-27 CORRODED (C-CHECK) RO 8/28/2020 REMOVED CORROSION ON FLOOR STRAP AT FS 559.0 & LBL 27-36 REF CRJ 200 SRM. ORIGINAL THICKNESS IS 0.050" WITH REMAINING 0.042" AND MATERIAL LOSS 0.008", MAX. PERMISSIBLE IS 0.005", THEREFORE FOUND TO BE OUT OF LIMITS. REF: CRJ-200 SRM. LOCATED AND DRILLED AND INSTALLED NEW FLOOR STRAP REF CRJ 200 SRM. COMPLIED WITH. PERFORMED PRESSURE CHECK OF REPAIRED AREA REF. CRJ 200 AMM. CHECK GOOD.

Part: STRAP — CORRODED (BS 559) · airframe 36,152 hrs · 32,596 cycles

*FLOOR STRAP AT FS 559.0 RBL 18-27 CORRODED (C-CHECK) RO 8/28/2020 REMOVED CORROSION ON FLOOR STRAP AT FS 559.0 & RBL 27-36 REF CRJ 200 SRM. ORIGINAL THICKNESS IS 0.050" WITH REMAINING 0.042" AND MATERIAL LOSS 0.008", MAX. PERMISSIBLE IS 0.005", THEREFORE FOUND TO BE OUT OF LIMITS. REF: CRJ-200 SRM. LOCATED AND DRILLED NEW FLOOR STRAP REF CRJ 200 SRM. INSTALLED NEW FLOOR STRAP AT FS 559.0 RH RBL 27-36 PN 901R31025-29 REF CRJ 200 SRM FINISHED ALL FASTENERS ON FLOOR STRAP REF CRJ 200 SRM. PERFORMED PRESSURE CHECK OF REPAIRED AREA REF. CRJ 200 AMM. CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 36,152 hrs · 32,596 cycles

*R/H PRESSURE FLOOR SILL HAS CORROSION AT NUMEROUS LOCATINS BETWEEN FS 409+128 AND FS 559. (C-CHECK) RO 8/28/2020 BLENDED R/H PRESSURE FLOOR SILL AT 17EA LOCATIONS,11EA LOCATIONS IN LIMITS REF REO, 6EA LOCATIONS OUT OF LIMITS REF REO. SEE CONTINUE CARD FOR DETAILS, PRESSURE CHECK GOOD, COMPLIED WITH TASK CARD

Part: SEAT TRACK — CORRODED (BS 559) · airframe 36,152 hrs · 32,596 cycles

*SEAT TRACK AT FS 559+80- 559+112 RBL 18 CORRODED. INSTALLED NEW SEAT TRACK RBL18 FS559+80 - FS559+112 REF. CRJ 200 AMM.

Part: ANGLE — CRACKED (BS 473) · airframe 36,152 hrs · 32,596 cycles

*OTBD CLIP ON CABLE FAIRLEAD IS CRACKED. CLIP LOCATION IS FS 473 AND LBL 36. (C-CHECK) RO 8/28/2020 REMOVED CRACKED OTBD CLIP ON CABLE FAIRLEAD AND INSTALLED NEW CLIP REF REO. PRESSURE CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 36,152 hrs · 32,596 cycles

*L/H PRESSURE FLOOR SILL ANGLE HAS CORROSION AT NUMEROUS LOCATINS BETWEEN FS 409+128 AND FS 559. (C-CHECK) RO 8/28/2020 BLENDED L/H PRESSURE FLOOR SILL ANGLE AT 13EA LOCATIONS, REF REO. SEE CONTINUE CARD FOR DETAILS, PRESSURE CHECK GOOD, COMPLIED WITH TASK CARD

Part: FLOORBEAM — CORRODED (BS 559) · airframe 36,152 hrs · 32,596 cycles

*FLOOR BEAM AT FS 559+80 CORRODED ON INBD SIDE (C-CHECK) RO 8/28/2020 REPLACED FLOOR BEAM UPPER CAP ANGLE FS 559+8 TO FS 568 AND AFT. FLOOR BEAM SPLICE "U" CHANNEL AT FS 568 RBL 9. REF: CRJ-200 SRM AND REO. RESTORED FINISH . REF: CRJ-200 SRM. APPLIED CIC TO REPAIRED AREA AS REQUIRED. REF: CRJ-200 SRM. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD.

Part: TRUNNION — DEFECTIVE (MLG) · airframe 36,152 hrs · 32,596 cycles

WHILE PERFORMING SB ( MLG TRUNNION) FOUND DEFECTS IN HOLES #15,16,17,19,20, AND 21 ON THE RH MLG TRUNNION. (C-CHECK) RO 8/28/2020 REMOVED AND REPLACED RIGHT MLG TRUNNION REF REO. LEAK CHECKS GOOD.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 36,152 hrs · 32,596 cycles

* R/H INBD FLAP VANE - FLAP VANE CHAFFED AT OUTERMOST WEAR PAD LOCATION (C-CHECK) RO 8/28/2020 REMOVED AND REPLACED R/H INBD FLAP VANE REF. CRJ200 SRM AND DWG. COMPLIED WITH TASK CARD.

Part: CLEAT — CRACKED (LT WING TE FLAP) · airframe 36,152 hrs · 32,596 cycles

* THE LH INBD FLAP VANE FRONT SPAR OUTBD SIDE CLEAT IS CRACKED. (MARKED) (C-CHECK) RO 8/28/2020 REMOVED LH INBD FLAP AND INSTALLED NEW SERVICEABLE FLAP. REF CRJ 200 AMM. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 36,152 hrs · 32,596 cycles

* THE LH INBD FLAP VANE LEADING EDGE IS CHAFFED JUST OUTBD OF THE #3 FLAP VANE ACTUATOR. (MARKED) (C-CHECK) RO 8/28/2020 BLENDED OUT CHAFE DAMAGE ON THE LH INBD FLAP VANE LEADING EDGE, JUST OUTBD OF THE #3 FLAP VANE ACTUATOR REF CRJ-200 SRM. ORIGINAL THICKNESS OF LH IB FLAP VANE OB CAP IS .050" REF CRJ 200 SRM, AMOUNT REMAINING IS .027" REF NDT, REMOVED .023" AND MAX ALLOWABLE IS .020" THEREFORE OUT OF LIMITS OF REO. REMOVED AND INSTALLED A NEW L/H INBOARD FLAP LEADING EDGE SKIN VANE AT OUTBORAD LOCATION REF CRJ 200 SRM / BOMBARDIER DWG. REFERENCE THE CONTINUE CARD FOR DETAILS.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 36,152 hrs · 32,596 cycles

* THE LH INBD FLAP VANE LEADING EDGE IS CHAFFED JUST INBD OF THE #1 FLAP VANE ACTUATOR. (MARKED) (C-CHECK) RO 8/28/2020 BLENDED OUT CHAFE DAMAGE ON LH INBD FLAP VANE JUST INBD OF #1 FLAP VANE ACTUATOR IAW CRJ200 SRM. ORIGINAL THICKNESS OF LH IB FLAP VANE CAP IB END IS .050" REF CRJ 200 SRM, AMOUNT REMAINING IS .029" REF NDT, REMOVED .021" AND MAX ALLOWABLE IS .020" THEREFORE OUT OF LIMITS OF REO. REMOVED AND REPLACED AND LOCATED AND DRILLED NEW FLAP VANE CAP ON LE ON INBD FLAP NEXT TO #1 FLAP VANE ACTUATOR. IAW CRJ200 SRM. INSALLED NEW FLAP VANE LE IAW CRJ200 SRM AND DRAWING. SEALED PNL IAW CRJ200 SRM. RESTORED FINISH IAW CRJ200 SRM. WEIGHED OLD PART 0.12OZ AND NEW PART 0.12OZ NO NOTED WEIGHT CHANGE.

Part: HINGE — GOUGED (LT WING TE FLAP) · airframe 36,152 hrs · 32,596 cycles

* L/H OBD FLAP INB HINGE BOX AFT ATTACHMENT FITTING ON WING HAS INB LUGS GOUGED AT INB CORNERS. (C-CHECK) RO 8/28/2020 BLENDED OUT GOUGES ON LH OB FLAP IB HINGE BOX IB LUGS REF MHIRJ REO, ALL STEPS COMPLIED WITH AND RESTORED THE FINISH. NO WEIGHT STATEMENT REQUIRED BLEND OUT ONLY

Part: SKIN — CORRODED (BS 559) · airframe 36,152 hrs · 32,596 cycles

* EXTERNAL FUSELAGE SKIN LOWER CENTER AREA APPROX. FS 559.00 + 96 HAS CORROSION AROUND DRAIN HOLE. (C-CHECK) RO 8/28/2020 REMOVED CORROSION AROUND DRAIN HOLE AT APPROX. FS 559.00+96 EXTERNAL FUSELAGE SKIN LOWER CENTER AREA. REF: CRJ-200 SRM. ORIGINAL THICKNESS OF FUSELAGE SKIN AT 559+96 AT STRINGERS 26L TO 26R IS .063" MILLED TO .058" + OR - .002" LEAVING .056" NOMINAL REF CRJ 200 SRM, AMOUNT REMAINING IS .055" REF NDT, REMOVED .001", AND NO DAMAGE ALLOWED THIS AREA, THEREFORE OUT OF LIMITS REF CRJ 200 SRM. COMPLIED WITH MHIRJ REO. LEAK CHECK GOOD.

Part: SKIN — CORRODED (BS 559) · airframe 36,152 hrs · 32,596 cycles

* EXTERNAL FUSELAGE SKIN LOWER CENTER AREA APPROX. FS 559.00 + 16 HAS CORROSION AROUND DRAIN HOLES AND RIVETS. ( MARKED ) (C-CHECK) RO 8/28/2020 REMOVED CORROSION AT EXTERNAL FUSELAGE SKIN LOWER CENTER AREA FS 559.00+16 AROUND DRAIN HOLES AND RIVETS. REF: CRJ-200 SRM. ORIGINAL THICKNESS OF SKIN AT FS 559+16 IS .063" MILLED TO .058" + OR - .002" FOR A NOMINAL .056" REF CRJ 200 SRM, AMOUNT REMAINING IS .054" REF NDT, REMOVED .002" , BUT NO DAMAGE ALLOWED THIS AREA THEREFORE OUT OF LIMITS OF CRJ 200 SRM. COMPLIED WITH MHIRJ REO. PERFORMED PRESSURE CHECK OF REPAIRED AREA REF. CRJ 200 AMM. CHECK GOOD.

Part: STIFFENER — CRACKED (BS 621 BULKHEAD) · airframe 36,152 hrs · 32,596 cycles

FOUND CRACKED ANGLE P/N 601R36008-51 ON AFT SIDE OF FS621 BULKHEAD WHILE PERFORMING REO. (C-CHECK) RO 8/28/2020 REMOVED CRACKED ANGLE. REF: CRJ200 SRM. - INSTALLED NEW STIFFENER P/N 601R36008-51. REF: DWG. PERFORMED PRESSURE CHECK OF FASTENERS AT REPAIR AREA. ALL CHECKS GOOD.

Part: BRACKET — CRACKED (LT WING SPAR) · airframe 36,152 hrs · 32,596 cycles

*ANGLE BRACKET ON L/H WING FWD SPAR IS CRACKED AT WS139.54. FLAGGED. REMOVED AND REPLACED WITH NEW ANGLE BRACKET ON LH WING FWD SPAR AT WS139.54 REF CRJ200 SRM

Part: SKIN — CORRODED (BS 280) · airframe 36,152 hrs · 32,596 cycles

* MILD SURFACE CORROSION DETECTED ON (L & R) SIDES OF THE FWD JACKING FITTING FWD OF F.S. 280.00 IN (3EA) PLACES. (1EA) AT L/H SIDE FITTING INTERCOSTAL "FLANGE" AND F.S. 280.00 "FLANGE" INTERSECTION, (1EA) AT L/H FITTING INTERCOSTAL "FLANGE" APROX 2" FWD OF F.S. 280.00 AND (1EA) AT R/H FITTING INTERCOSTAL "FLANGE" AND F.S. 280.00 "FLANGE" INTERSECTION (MARKED). (C-CHECK) RO 8/28/2020 REMOVED CORROSION AT FWD SIDE OF FS280 ON FRAME AND INTERCOSTAL BETWEEN STGR 26L/R REF CRJ 200 SRM, BLENDED AREAS OF THE L/H SIDE OF JACK PAD FITTING INTERCOSTAL 1EA LOWER FLANGE 1EA UPPER FLANGE BETWEEN FS280.00 AND FS265.00 AT STGR27 OUT OF LIMITS REF REO. SEE CONTINUE CARD FOR DETAILS, PRESSURE CHECK GOOD, COMPLIED WITH TASK CARD

Part: MOUNT — CORRODED (SPOILER ACTUATOR) · airframe 36,152 hrs · 32,596 cycles

* RIGHT WING OUTBOARD GROUND SPOILER PANEL, CORRODED ACTUATOR MOUNT HARDWARE. BOLT, WASHER, NUT. MARKED WITH ORANGE FLAG. (C-CHECK) RO 8/28/2020 REMOVED CORRODED RH WING OTB GROUND SPOILER ACTUATOR MOUNT BOLT AND ATTACHING HARDWARE REF. CRJ200 AMM. INSTALLED NEW RH WING OTB GROUND SPOILER ACTUATOR MOUNT BOLT (1EA), WASHERS (2EA) AND NUT (1EA) REF. CRJ200 AMM. RIGGING AND OPERATIONAL CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: MOUNT — CORRODED (SPOILER ACTUATOR) · airframe 36,152 hrs · 32,596 cycles

* LEFT WING INBOARD GROUND SPOILER PANEL, CORRODED ACTUATOR MOUNT HARDWARE. MARKED. (C-CHECK) RO 8/28/2020 REMOVED AND INSTALLED NEW LH WING INB GROUND SPOILER ACTUATOR MOUNT BOLT (1EA), WASHERS (2EA) AND NUT (1EA) REF. CRJ200 AMM. OPERATIONAL TEST OF THE GROUND SPOILERS REF. CRJ200 AMM, GOOD, SEE CONTINUATION CARD FOR DETAILS.

Part: MOUNT — CORRODED (SPOILER ACTUATOR) · airframe 36,152 hrs · 32,596 cycles

* LEFT WING OUTBOARD GROUND SPOILER PANEL , CORRODED ACTUATOR MOUNT HARDWARE. MARKED ORANGE FLAG (C-CHECK) RO 8/28/2020 REMOVED CORRODED LH WING OTB GROUND SPOILER ACTUATOR MOUNT BOLT AND ATTACHING HARDWARE REF. CRJ200 AMM. INSTALLED NEW LH WING OTB GROUND SPOILER ACTUATOR MOUNT BOLT (1EA), WASHERS (2EA) AND NUT (1EA) REF. CRJ200 AMM. RIGGING AND OPERATIONAL CHECKS GOOD, SEE CONTINUATION CARD FOR DETAILS.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 36,152 hrs · 32,596 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH PARAGRAPH (J) OF AD: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER TR. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO). AND MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE, PART NUMBER: - , SERIAL NUMBER: 7820, POSITION: (C-CHECK) RO 8/28/2020 COMPLIED WITH PARAGRAPH (J) OF AD:(J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER TR. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO). AND; MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE. COMPLIED WITH SERIAL NUMBER 7820.

Part: SPHERICAL BEARIN — WORN (LT AILERON) · airframe 36,152 hrs · 32,596 cycles

REMOVE LH AILERON PCU LINKS AND REPLACE THE SPHERICAL BALLS (IAW CMM) THEN REINSTALL THE LINKS (IAW AMM) REMOVED AND INSTALLED L/H AILERON I/B AND O/B PCU OUTPUT LINKS WITH NEW SPHERICAL BEARINGS REF CRJ 200 AMM. OPS GOOD, SEE CONTINEU CARD FOR WORK PERFORMED.TASK CARD COMPLIED WITH.

Part: SPHERICAL BEARIN — WORN (RT AILERON) · airframe 36,152 hrs · 32,596 cycles

REMOVE RH AILERON PCU LINKS AND REPLACE THE SPHERICAL BALLS (IAW CMM 27-14-01) THEN REINSTALL THE LINKS (IAW AMM) (C-CHECK) RO 8/28/2020 REMOVED R/H AILERON INBOARD AND OUTBOARD PCU OUTPUT LINK SPHERICAL BEARINGS. REF. CRJ 200 CMM. REPLACED R/H AILERON INBOARD AND OUTBOARD PCU OUTPUT LINK SPHERICAL BEARINGS. REF. CRJ 200 CMM AND CRJ 200 AMM. PERFORMED AN OPERATIONAL TEST OF THE AILERON CONTROL SYSTEM. REF. CRJ 200 AMM. ALL CHECKS GOOD. TASK CARD COMPLIED WITH

Part: REINFORCEMENT — WEAK (BS 559) · airframe 36,152 hrs · 32,596 cycles

COMPLY WITH REO 601R-53-41-1116 REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS (C-CHECK) RO 8/28/2020 COMPLIED WITH REO REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS

Part: FLOOR SUPPORT — CORRODED (BS 573) · airframe 32,873 hrs · 28,889 cycles

FLOOR SUPPORT, BS 573, LBL 27 CORRODED. REPAIRED THE FLOOR SUPPORT BETWEEN BS 559.96 AND 574 IAW SRM.

Part: FLOOR SUPPORT — DAMAGED (BS 575-610) · airframe 32,873 hrs · 28,889 cycles

FLOOR SUPPORT SECTION, BS 575 - 610, LBL 27 TOP CAP DAMAGED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW REO.

Part: DOOR SILL — CORRODED (BS 532-621) · airframe 32,873 hrs · 28,889 cycles

CARGO DOOR SILL CORRODED AT LBL 43, BS 562 - 621. REPLACED THE DOOR SILL IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 32,873 hrs · 28,889 cycles

RIGHT FLAP VANE LEADING EDGE MIDDLE SECTION CHAFED. REMOVED AND REPLACED THE FLAP VANE LEADING EDGE IAW SRM.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 32,873 hrs · 28,889 cycles

LEFT INBOARD FLAP VANE LEADING EDGE SKIN CHAFED 43.5 INCHES? FROM OUTBOARD END OF VANE. INSTALLED A NEW LEFT INBOARD FLAP VANE OUTBOARD CENTER LEADING EDGE SKIN IAW SRM.

Part: HOUSING — GOUGED (CARGO DOOR) · airframe 32,873 hrs · 28,889 cycles

CARGO DOOR LATCH HANDLE HOUSING GOUGED AT TWO LOCATIONS. REMOVED AND REPLACED THE CARGO DOOR HANDLE HOUSING ASSEMBLY IAW SRM. OPS CHECKED GOOD.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 29,178 hrs · 24,809 cycles

THE LT INBD FLAP VANE L/E, CENTER VANE CAP CHAFED. REPLACED THE LT INBD FLAP VANE L/E, CENTER VANE CAP IAW SRM AND STS EA.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 29,178 hrs · 24,809 cycles

RIGHT WING INBD FLAP VANE L/E HAS 3 CHAFED AREAS. REPLACED RT WING INBD FLAP VANE L/E OTBD, INBD, CENTER VANE CAPS IAW SRM AND STS EA.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 29,178 hrs · 24,809 cycles

LEFT WING INBD FLAP VANE L/E HAS 3 CHAFED AREAS. BLENDED CHAFED AREAS OF THE LT WING INBD FLAP VANE L/E AT WS 127.25 AND WS 96.13. THE INBD AND OTBD CAPS ARE WITHIN LIMITS IAW REO AND SRM.

Part: SCUFF PLATE — DENTED (CARGO BAY) · airframe 29,178 hrs · 24,809 cycles

FOUR DENTS BELOW CARGO SCUFF PLATE APPROXIMATELY BETWEEN FS 589.00-FS 610.00 BETWEEN STR 21-23. REPAIRED DAMAGED AREA BY COLDWORKING, 3 OF THE DENTS TO ORIGINAL ACFT CONTOUR AND CUTTING OUT THE FOURTH DENT DAMAGE AND INSTALLING A REPAIR DOUBLER IAW STS EA.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 26,677 hrs · 22,298 cycles

EMERGENCY LIGHTS IN CABIN INOPERATIVE. R & R NR 4 BATTERY PACK IAW AMM 33-51-04.

Part: ACM — FAILED (RIGHT) · airframe 26,099 hrs · 21,710 cycles

SMOKE IN CABIN WITH RIGHT PACK HIGH TEMP CAUTION MESSAGE. R & R RT ACM IAW AMM.

Part: DOOR SILL — CORRODED (PAX DOORWAY) · airframe 25,651 hrs · 21,268 cycles

PAX DOOR SILL AND DOOR CUTOUT CORRODED. FOUND BEYOND LIMITS. REPLACED NEW LOWER PASSENGER DOOR SILL ASSEMBLY IAW SRM.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 25,651 hrs · 21,268 cycles

BS 349 TOP OF FLOORBEAM AT END WHERE IT MEETS LWR SILL AND FITTING THAT TIES SILLS TOGETHER HAS CORROSION ON TOP AND BETWEEN AFT SIDE OF BEAM AND SILL. C-CHECK, BLENDED AND TREATED IAW SRM AND EA.

Part: FITTING — CORRODED (BS 319) · airframe 25,651 hrs · 21,268 cycles

SERVICE DOOR FWD FRAME TO STRUCTURE FITTING AT FS 319.70 THAT ATTACHES SERVICE DOOR SILL AND SIDE SILL FWD OF SERVICE DOOR TO MAIN STRUCTURE. AT FLOOR, HAS CORROSION. C-CHECK, R & R FRAME TO STRUCTURE FITTING THAT ATTACHES SERVICE DOOR SILL AND SIDE SILL FWD OF SERVICE DOOR TO MAIN STRUCTURE AT FS 319.70 IAW SRM.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 25,651 hrs · 21,268 cycles

SEAT TRACK LBL 27, BS 559+96 - 559+112 CORRODED AROUND FASTENER LOCATIONS. C-CHECK, R & R OUT OF LIMITS SEAT TRACK IAW SRM.

Part: POST — CRACKED (BS 409) · airframe 25,651 hrs · 21,268 cycles

RBL 18 OTBD POST AT 409+128 CRACKED AT BOTTOM OF POST. C-CHECK, INSTALLED NEW POST IAW REO, AMM AND SRM.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 25,651 hrs · 21,268 cycles

SEAT TRACK LBL 9, BS 559+96 - 559+112 CORRODED. C-CHECK, REPLACED SEAT TRACK IAW REO C.

Part: SEAT TRACK — CORRODED (BS 574-617) · airframe 25,651 hrs · 21,268 cycles

SEAT TRACK LBL 9 BS 574 - 617 CORRODED. C-CHECK, REPLACED SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (BS 574-608) · airframe 25,651 hrs · 21,268 cycles

SEAT TRACK RBL 27, BS 574-608 CORRODED. C-CHECK, REMOVED OUT OF LIMITS SEAT TRACK AND REPLACED WITH NEW IAW SRM.

Part: SEAT TRACK — CORRODED (BS 574-617) · airframe 25,651 hrs · 21,268 cycles

SEAT TRACK RBL 9, BS 574 - 617 CORRODED. C-CHECK, REPLACED SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (BS 574-617) · airframe 25,651 hrs · 21,268 cycles

SEAT TRACK LBL 27, BS 574 - 617 CORRODED. C-CHECK, R & R SEAT TRACK IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 25,651 hrs · 21,268 cycles

LEFT INBD FLAP VANE L/E CHAFED AT OTBD END. C-CHECK, CHAFE REMOVED IAW REO AND SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 25,651 hrs · 21,268 cycles

RIGHT INBD FLAP VANE CHAFED ON L/E AT INBD END. C-CHECK, CHAFE BLENDED IAW REO.

Part: ANGLE — CRACKED (BS 621) · airframe 25,651 hrs · 21,268 cycles

ANGLE CRACKED RT AFT SIDE OF BS 621 INTERCOSTAL S14R. C-CHECK, REPLACED DAMAGED ANGLE IAW SRM.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 25,651 hrs · 21,268 cycles

INTERCOSTAL ON AFT LT SIDE OF BS 621 AT S13L CRACKED AT OTBD AFT CORNER. C-CHECK, R & R INTERCOSTAL IAW SRM.

Part: ATTACH FITTING — CORRODED (PAX DOOR CABLE) · airframe 25,651 hrs · 21,268 cycles

PAX DOOR FWD LOWER CABLE ATTACH FITTING AT BS 310 FLOOR LEVEL THE SERRATED PLATE UNDER THE FITTING ON THE FWD EDGE HAS CORROSION ON IT. C-CHECK, REPLACED PAX DOOR FWD LOWER CABLE ATTATCHMENT BRACKET, SERRATED PLATE, WITH NEW IAW AMM.

Part: ANGLE — CRACKED (COCKPIT) · airframe 25,651 hrs · 21,268 cycles

POSSIBLE CRACK ON WINDSHIELD CENTER POST LT LOWER ANGLE FITTING. C-CHECK, R & R LT LOWER ANGLE FITTING, IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 25,651 hrs · 21,268 cycles

RIGHT INBD FLAP VANE L/E CHAFED AT OTBD END. C-CHECK, CHAFING BLENDED IAW REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 25,651 hrs · 21,268 cycles

LEFT WING AILERON, OTBD L/E CHAFING RUB SEAL. C-CHECK, R & R LT AILERON LOWER L/E SKIN, PN CC670-13054-1 IAW SRM.

Part: HANDLE — CHAFED (PAX DOOR) · airframe 25,651 hrs · 21,268 cycles

PASSENGER DOOR FWD PULL-IN LEVER CHAFED. C-CHECK, BLENDED CHAFE IAW REO.

Part: ANGLE — CRACKED (COCKPIT) · airframe 25,651 hrs · 21,268 cycles

POSSIBLE CRACK ON WINDSHIELD CENTER POST RT LOWER ANGLE FITTING. C-CHECK, R & R RT LOWER ANGLE FITTING IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 25,651 hrs · 21,268 cycles

RIGHT INBD FLAP VANE L/E CHAFED AT CENTER. C-CHECK, CHAFING BLENDED IAW REO.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 25,651 hrs · 21,268 cycles

INTERCOSTAL ON AFT LT SIDE OF BS 621 AT S14L CRACKED AT OTBD AFT CORNER. C-CHECK, R & R INTERCOSTAL IAW SRM.

Part: ANGLE — CRACKED (BS 621) · airframe 25,651 hrs · 21,268 cycles

ANGLE CRACKED LT AFT SIDE OF BS 621 ON INTERCOSTAL AT S14L. C-CHECK, REPLACED DAMAGED ANGLE IAW SRM.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 25,651 hrs · 21,268 cycles

RIGHT INBD FLAP BONDING WIRE CHAFING INTERIOR SKIN AT MID VANE ACTUATOR. C-CHECK, REMOVED CHAFE IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 25,651 hrs · 21,268 cycles

FLOOR SUPPORT RBL 36, BS 559+80 - 621 CORRODED. C-CHECK, BLENDED CORROSION IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 25,651 hrs · 21,268 cycles

LEFT INBD FLAP VANE CHAFED ON L/E AT INBD END. C-CHECK, R & R FLAP VANE CAP IAW SRM AND REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 25,651 hrs · 21,268 cycles

LT WING AILERON L/E UPPER SKIN SHROUD HAS CHAFING. C-CHECK, REMOVED CHAFE IAW REO.

Part: INTERCOSTAL — CHAFED (BS 621) · airframe 25,651 hrs · 21,268 cycles

INTERCOSTAL ON AFT LT SIDE OF FS 621, S16L CRACKED AT OTBD AFT CORNER. C-CHECK, R & R INTERCOSTAL IAW SRM.

Part: FITTING — CORRODED (BULKHEAD) · airframe 25,651 hrs · 21,268 cycles

AFT BULKHEAD RAIL SUPPORT TO BULKHEAD FITTING HAS CORROSION AT BASE OF FITTING. C-CHECK, FITTING REMOVED AND NEW FITTING INSTALLED IAW REO.

Part: FITTING — CHAFED (WING TO BODY) · airframe 25,651 hrs · 21,268 cycles

LEFT WING TO FUSELAGE FITTING AT FS 473.15 CHAFED ON OTBD SIDE. C-CHECK, REMOVED CHAFE, FOUND TO BE WITHIN LIMITS, ROTO PEENED AND RESTORED FINISH IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 25,651 hrs · 21,268 cycles

LEFT INBD FLAP VANE L/E CHAFED AT CENTER. C-CHECK, CHAFE BLENDED IAW REO.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 25,651 hrs · 21,268 cycles

RIGHT WING INBD FLAP, UPPER SKIN IS CHAFED 45-57" AND 70" FROM INBD END OF FLAP AND 8" AFT OF L/E OF FLAP. C-CHECK, BLENDED CHAFE AND REPAIRED FLAP IAW EA.

Part: CONTROL ARM — CHAFED (RT MLG DOOR) · airframe 25,651 hrs · 21,268 cycles

RIGHT MLG DOOR LOWER CONTROL ARM CHAFED AT INBD END. C-CHECK, BLENDED CONTROL ARM CHAFE IAW REO.

Part: STRUCTURE — CORRODED (LT MLG WW) · airframe 25,651 hrs · 21,268 cycles

CORROSION ON LOWER CENTER WING, FWD OF THE OTBD FWD CORNER OF LT WHEEL WELL. C-CHECK, REMOVED CORROSION ON LOWER CENTER WING, FWD OF THE OTBD FWD CORNER OF THE LT WHEEL WELL IAW REO.

Part: STRUCTURE — CORRODED (RT MLG WW) · airframe 25,651 hrs · 21,268 cycles

CORROSION ON LOWER CENTER WING, FWD OF THE OTBD FWD CORNER OF RT WHEEL WELL. C-CHECK, BLENDED CORROSION AND FOUND WITHIN ALLOWABLE LIMITS AND REPAIRED LOWER CENTER WING, FORWARD OF THE OTBD CORNER OF RT WHEEL WELL IAW REO.

Part: ATTACH FITTING — CHAFED (RT MLG DOOR) · airframe 25,651 hrs · 21,268 cycles

RIGHT MLG DOOR LOWER CONTROL ARM ATTACHMENT LUG CHAFED. C-CHECK, THE RT MLG DOOR LOWER CONTROL ARM ATTACHMENT LUG WAS BLENDED IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,350 hrs · 20,985 cycles

EMERGENCY OVERHEAD LIGHT IN AFT CABIN IS BURNED OUT. FLT 7370 RELAMPED.

Part: A/C PACK — CONTAMINATED (AC BAY) · airframe 25,269 hrs · 20,904 cycles

BLACK BILLOWING SMOKE WITH A STRONG ODOR IN COCKPIT & CABIN, DISSIPATED ON LEVEL OFF. FLT 4476 INSPECTED AFT EQUIPMENT BAY FOUND LARGE SUMS OF GLYCOL, CLEANED AS NECESSARY. RAN BOTH PACKS WITH ENG. NO SMOKE PRESENT IAW AMM. RAN PACKS ON APU NO SMOKE PRESENT IAW AMM.

Part: FRAME — CHAFED (FUSELAGE) · airframe 25,134 hrs · 20,753 cycles

NR 2 HYDRAULIC HOSE HAS CHAFED INTO FRAME AT FS 718.00 BETWEEN STRINGER 17R & STRINGER 18R. C-CHECK REPAIRED FRAME FLANGE AT FS 718, STRINGERS 17-18 RHS IAW REO.

Part: COMPUTER — FAILED (AUTOPILOT SYS) · airframe 23,773 hrs · 19,411 cycles

YD 1 STATUS MESSAGE APPEARED AND WOULD NOT RE-ENGAGE. CONTINUOUS AIRCRAFT YAWING PULSATION IN THE RUDDER PEDALS. (FLT 7426) REPLACED NR 1 FCC IAW AMM 22-12-14. ALL FCC OPS TESTS GOOD. YAW DAMPER TEST GOOD. NO UNUSUAL RUDDER PEDAL MOVEMENTS NOTED. NO REPORT CODES PRESENT. P/N ON/OFF 622-9815-904 S/N ON 2623 S/N OFF 63XG

Part: COVER — MISSING (CABIN) · airframe 23,614 hrs · 19,244 cycles

FLOOR LEVEL EMERGENCY FLOOD LIGHT COVER ON THE WARDROBE IS MISSING. (FLT 4716) REPLACED FLOOR LEVEL EMERGENCY FLOOD LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,614 hrs · 19,244 cycles

OVERHEAD EMERGENCY LIGHT IN ROW 10 IS BURNED OUT. (FLT 7420) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,467 hrs · 19,086 cycles

GALLEY EMERGENCY EXIT FLOOD LIGHT BURNED OUT. (FLT 4645) RELAMPED EMERGENCY LIGHT.

Part: WIRE — LOOSE (CABIN) · airframe 23,467 hrs · 19,086 cycles

MAIN CABIN DOOR FLOOR LEVEL FLOOD LIGHT DOES NOT ILLUMINATE. (FLT 4645) RE-SECURED WIRE ON MAIN CABIN DOOR FLOOR FLOOD LIGHT.

Part: ACTUATOR — FAILED (TE FLAP) · airframe 23,355 hrs · 18,967 cycles

FLAP FAIL ON APPROACH. EMERGENCY DECLARED. (FLT 7378) REPLACED ALL FOUR FLAP ACTUATORS ON RIGHT WING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,084 hrs · 18,702 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4840) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,833 hrs · 18,445 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4604) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,267 hrs · 17,885 cycles

EMERGENCY LIGHT OUT ON ENTRANCE FLOORBOARD. (FLT 4451) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,267 hrs · 17,885 cycles

NR 2 AND NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4829) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,810 hrs · 17,442 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4652) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,764 hrs · 17,388 cycles

(C-CHECK) CRACK ON THE RIGHT SIDE FS 559.0 PRESSURE BULKHEAD. REPAIRED CRACK ON THE RIGHT SIDE FS 559.0 PRESSURE BULKHEAD.

Part: TIRE — BLOWN (LT MLG) · airframe 21,764 hrs · 17,388 cycles

LEFT NR 1 MAIN TIRE BLOW OUT ON LANDING. (FLT 4683) REPLACED NR 1 MLG WHEEL ASSEMBLY.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,008 hrs · 16,652 cycles

LEFT OVERWING EXTERIOR EMERGENCY EXIT LIGHTS ARE OUT. (FLT 4557) RELAMPED EMERGENCY LIGHTS.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 20,875 hrs · 16,523 cycles

GEAR DISAGREE MESSAGE ON GEAR DOWN SELECTION. (FLT 4500) REPLACED MLG SELECTOR VALVE. PN: 750005000 SN OFF: 0095T.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,886 hrs · 16,533 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4743) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,793 hrs · 16,430 cycles

ALL 3 LEFT OVERWING EMERGENCY EXIT LIGHTS ARE OUT. (FLT 4604) RELAMPED EMERGENCY LIGHT.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 20,763 hrs · 16,398 cycles

GEAR DISAGREE WITH NOSE LANDING GEAR NOT RETRACTING. (FLT 4771) REPLACED THE NLG SELECTOR VALVE. PN 750006000, SN OFF 2110.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,642 hrs · 16,280 cycles

NR 2 & 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4633) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,642 hrs · 16,280 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4633) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,578 hrs · 16,222 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4475) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,237 hrs · 15,924 cycles

NR 2 AND NR 4 CEILING EMERGENCY LIGHTS ARE OUT. (FLT 4550) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,176 hrs · 15,872 cycles

AFT OVERHEAD EMERGENCY LIGHT IS NOT WORKING. (FLT 4602) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,083 hrs · 15,790 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4448) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,985 hrs · 15,706 cycles

LEFT AFT EXTERIOR EMERGENCY OVERWING EXIT LIGHT IS OUT. (FLT 4783) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 19,915 hrs · 15,645 cycles

LAST SECTION OF THE FLOOR MOUNTED EMERGENCY LIGHTS DON'T WORK WHEN TESTED. (FLT 4602) RECONNECTED CONNECTOR AT AFT FLOOR EMERGENCY LIGHTS.

Part: SEAT BELT — DEFECTIVE (COCKPIT) · airframe 19,915 hrs · 15,645 cycles

F/O'S QUICK RELEASE SEATBELT IS HARD TO OPEN. (FLT 4795) REPLACED SEAT BELT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,887 hrs · 15,623 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4760) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,772 hrs · 15,526 cycles

MIDDLE EXTERNAL EMERGENCY LIGHT OVER RIGHT WING IS OUT. (FLT 4602) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 19,221 hrs · 15,082 cycles

LOWER RIGHT EMERGENCY LIGHT BY THE OVERWING EXIT DOOR IS INOPERATIVE. (FLT 4741) REPLACED THE NR 3 EMERGENCY LIGHT BATTERY CHARGER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,007 hrs · 14,900 cycles

RIGHT OVERHEAD EMERGENCY EXIT LIGHT IS BURNED OUT. (FLT 4847) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,129 hrs · 14,118 cycles

AFT CEILING CABIN EMERGENCY LIGHT INOP. (FLT 4490) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 17,843 hrs · 13,854 cycles

EMERGENCY LIGHTS INOP AT MIDDLE SECTION. (FLT 4617) RESEATED CONNECTOR.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,680 hrs · 13,710 cycles

FS 621 PRESSURE BULKHEAD WEB CRACKED AT LINTEL FITTING. (C CHECK) REPAIRED PER REO.

Part: SUPPORT ANGLE — CRACKED (CARGO DOOR) · airframe 17,942 hrs · 13,954 cycles

CARGO DOOR CAM TRACK SUPPORT ANGLE CRACKED. (C CHECK) REPLACED PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,942 hrs · 13,954 cycles

AFT PRESSURE BULKHEAD WEB AT FS 621 CRACKED AT AFT CARGO DOOR TRACK. (C CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,942 hrs · 13,954 cycles

AFT PRESSURE BULKHEAD FS 621 CRACKED AT LINTEL FITTING. (C CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,429 hrs · 13,495 cycles

SECOND EMERGENCY OVERHEAD FLOODLIGHT INOP. (FLT 4753) RELAMPED EMERGENCY FLOODLIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,300 hrs · 13,383 cycles

REAR OVERHEAD EMERGENCY FLOOD LIGHT INOP. (FLT 4608) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,943 hrs · 13,084 cycles

FLT 4525, NR 3 CEILING FLOOD EMERGENCY LIGHT INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,630 hrs · 12,826 cycles

OVERHEAD EMERGENCY FLOODLIGHT NR 4 INOP. (FLT 4662) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,531 hrs · 12,736 cycles

EMERGENCY EXIT SIDEWALL LIGHTING ON RIGHT SIDE INOP. (FLT 4443) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,435 hrs · 12,654 cycles

RIGHT SIDE EMERGENCY DOOR EXIT LIGHT INOP. (FLT 4611) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — LOOSE (CABIN) · airframe 16,364 hrs · 12,595 cycles

FLOOR EMERGENCY LIGHT STRIP INOP. (FLT 4570) RESEATED CONNECTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,328 hrs · 12,565 cycles

EMERGENCY FLOOD LIGHT INOP. (FLT 4625) RELAMPED EMERGENCY LIGHT.

Part: DOOR — STUCK (MAIN PAX) · airframe 15,564 hrs · 11,965 cycles

FLT 4541 - MAIN CABIN DOOR WOULD NOT OPEN ON GROUND. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,057 hrs · 11,579 cycles

FLT 4680 - AFT EMERGENCY LIGHT POD INOP. RELAMPED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 9,531 hrs · 7,364 cycles

LEFT WING CENTER EMERGENCY EXIT LIGHT INOP. REBULBED LEFT WING CENTER EMERGENCY EXIT LIGHT. OPERATIONAL HECKS GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 8,997 hrs · 6,977 cycles

RIGHT SIDE COCKPIT WINDOW CRACKED. REPLACED RIGHT SIDE COCKPIT WINDOW IAW 56-12-01 AND RII 56-220-1000.

Part: UNKNOWN — ODOR (CABIN) · airframe 8,987 hrs · 6,969 cycles

UPON LANDING OBSERVED A 'HOT ODOR'. OPERATED PACK FOR 30 MINUTES WITH NO ODORS. COULD NOT DUPLICATE DISCREPANCY.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 9,206 hrs · 7,126 cycles

STA 625 RIGHT SIDE STR 14 INTERCOSTAL CRACKED (CLIP), DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP ON RHS STR 14 STA 625 IAW CRJ 200 SRM REF 51-42-06 PG 11.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 9,206 hrs · 7,126 cycles

LBL 9 STA 280 INBD ANGLE BRACKET CRACKED AT TOP, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP IAW REO 601R-53-11-138 NC.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 9,206 hrs · 7,126 cycles

STA 625STR 14 LT SIDE INTERCOSTAL CRACKED (CLIP), DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP ON STA 625 AT STR 14 IAW CRJ 200 SRM REF 51-42-06 PG 11.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 9,206 hrs · 7,126 cycles

RBL 9 STA 280 OUTBOARD ANGLE CRACKED AT TOP, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP IAW CRJ 200 SRM 51-42-21.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 9,206 hrs · 7,126 cycles

PAX DOOR OUTER HANDLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SERVICEABLE PAX DOOR OUTER HANDLE IAW CRJ200 AMM 52-11-03-400-802. OPERATIONAL CHECKS GOOD.

Part: PANEL — CRACKED (PAX DOOR) · airframe 9,206 hrs · 7,126 cycles

PAX DOOR AFT SIDE PANEL HAS CRACK AT CORNER BETWEEN STEP THREE AND FOUR, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS ON AFT SIDE PANEL AT STEP 3, 4 AS PER REO 601R-52-11-1102.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 9,206 hrs · 7,126 cycles

FS 484 RBL 27 AND RBL 36 ANGLES CRACKED AT BOTH ENDS OF PULLEY BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLES AT FS 484, RBL 27 AND RBL 36 IAW REO 601R-53-41-059 REV A.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 9,206 hrs · 7,126 cycles

PAX DOOR - ANGLE CRACKED UPPER OUTBOARD ANGLE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW ANGLE PER CRJ 200 SRM 51-42-20 PG 23. OPERATIONAL CHECKS GOOD.

Part: WEB — CRACKED (PAX DOOR) · airframe 9,206 hrs · 7,126 cycles

PAX DOOR CRACK AT WEB BETWEEN TOP AND SECOND STEP FWD SIDE AT HANDRAIL SUPPORT FITTING, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR DOUBLER, AND ANGLES PER REO 601R-52-11-702. OPERATIONAL CHECKS GOOD.

Part: WEB — CRACKED (PAX DOOR) · airframe 9,206 hrs · 7,126 cycles

PAX DOOR CRACK AT WEB BETWEEN TOP AND SECOND STEP AFT SIDE, AT HANDRAIL SUPPORT FITTING, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR DOUBLER, AND ANGLES PER REO 601R-52-11-702. OPERATIONAL CHECKS GOOD.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 9,206 hrs · 7,126 cycles

LBL 9 STA 280 OUTBOARD ANGLE BRACKET CRACKED AT TOP, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP AT LBL 9 STA 280 OUTBOARD IAW REO 601R-53-11-138 NC.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 9,206 hrs · 7,126 cycles

LBL 10 STG 280 BELOW FORWARD WARDROBE FLOOR SUPPORT BEAM HAS CRACK COMING FROM RIVET, DISCOVERED DURING C-CHECK INSPECTION. SPLICE ANGLE INSTALLED IAW REO 601R-53-11-138NC.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 9,206 hrs · 7,126 cycles

RBL 9 STA 280 INBOARD ANGLE CRACKED AT TOP, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP AT RBL 9 STA 280 INBOARD IAW CRJ SRM 51-42-21.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,703 hrs · 6,751 cycles

FLOOR EMERGENCY LIGHTS FROM EMERGENCY EXIT TO LAV INOP. REPLACED AFT SECTION OF EMERGENCY LIGHT POWER STRIP. OPERATIONAL CHECKS GOOD, PN: 6464-5.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 7,814 hrs · 6,077 cycles

ON FINAL WHILE WINGS LEVEL, ON SPEED, FLAPS 45 DEGREES, RECEIVED STALL SHAKER. REPLACED EGPWS COMPUTER REF AMM 34-42-01. OPERATIONAL CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 7,565 hrs · 5,893 cycles

CAPT SIDE WINDOW CRACKED ON TAXI. REPLACED CAPTAINS SIDE WINDOW IAW AMM 56-12-01. P/N NP-139322-5; S/N OFF 0392H1080.

Part: ACTUATOR — MALFUNCTIONED (TE FLAP) · airframe 6,943 hrs · 5,426 cycles

ON FINAL SELECTED FLAPS 8 DEGREES. RECEIVED FLAPS FAIL MESSAGE. REPLACED FLAP ACTUATORS ON LT AND RT OUTBOARD FLAPS IAW 27-53-05. REPLACED FLEX SHAFT. REPLACED SKEW DETECTION UNIT IAW MM 27-51-15. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 6,592 hrs · 5,150 cycles

A -STAB CH 1 STATUS MESSAGE-, AFTER TAKEOFF. REPLACED HSTCU. OPERATIONAL CHECK GOOD IAW MM 27-41-01.

Part: TRIM SWITCH — INOPERATIVE (STAB TRIM) · airframe 6,214 hrs · 4,866 cycles

FO SIDE STAB TRIM INOP. REPLACED FO'S STAB TRIM SWITCH IAW 27-41-05. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 5,876 hrs · 4,606 cycles

2ND AFT OVHD EMERGENCY LIGHT INOP. RELAMPED 2ND AFT OVHD EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 5,716 hrs · 4,477 cycles

CAPT SIDE WINDSHIELD CRACKED IN FLIGHT. REPLACED CAPT SIDE WINDSHIELD IAW MM 56-00-00 AND 56-11-01, PN NR-139321-5; SN OFF 03081H9374.

Part: ACTUATOR — MALFUNCTIONED (TE FLAP) · airframe 5,100 hrs · 3,970 cycles

RECEIVED FLAPS FAIL CAUTION MSGS ON FINAL APPROACH. FAILED AT 41 DEGREES. REPLACED FLAP ACTUATORS R1, R2, R3, R4, L1, L2, L3, AND L4. OPERATIONAL CHECK GOOD AMM 27-53-01, AMM 27-53-05. P/N 852D100-19, S/N OFF 4982, 5039, 4609, 4941, P/N 853D100-20, S/N OFF 2903, P/N 854D100-20, S/N OFF 2721, P/N 853D100-19, S/N OFF 2898, P/N 854D100-19, S/N OFF 2360.

Part: CONNECTOR — CONTAMINATED (EMERGENCY LIGHT) · airframe 5,122 hrs · 3,987 cycles

FRONT SECTION OF EMERGENCY LIGHTING SYSTEM INOPERATIVE. CLEANED FORWARD EMERGENCY LIGHT STRIP CONNECTIONS OF WATER. OPERATIONAL CHECK GOOD.

Part: DETECTOR — MALFUNCTIONED (UNIT-SKEW) · airframe 4,836 hrs · 3,746 cycles

AFTER T/O, THE GEAR AND FLAP INDICATORS REMAINED ILLUMINATED ON ED1 FOR APPROX 20 MINUTES. GEAR AND FLAPS INDICATED NORMAL (UP & 0 DEGREES). REPLACED SKEW DETECTOR UNIT IAW MM 27-51-15, OPERATIONAL CHECK GOOD.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,573 hrs · 3,537 cycles

MAIN FUSELAGE FLOORBEAM AT RBL 9.0 HAS ATTACH ANGLES CRACKED AT FS 280.00. ITEM FOUND AT C-CHECK INSPECTION. ANGLES REPLACED 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 4,573 hrs · 3,537 cycles

FLOORBEAM ANGLE CRACKED AT FS 621.00 LBL 41.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE IAW CRJ REO 601R-53-61-117 REV B.

Part: FRAME — CRACKED (FUSELAGE) · airframe 4,573 hrs · 3,537 cycles

THREE SUPPORT CRACKS FOUND ON FRAME JUST AFT OF ELECTRONICS BAY DOOR, MARKED. ITEM FOUND AT C-CHECK INSPECTION. HFEC INSPECTION ON 3 SUSPECT CRACKS AS REQUESTED ON E & E BAY DOOR FRAME STRUCTURE, NO CRACKS FOUND. NDTM PT1 51-20-06.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,573 hrs · 3,537 cycles

FLOOR SUPPORT ANGLE CRACKED AT FS 621.00 RBL 41.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT IAW CRJ REO 601R-53-61-117.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,049 hrs · 3,122 cycles

2ND OVERHEAD EMERGENCY FLOOD LIGHT AND AFT OF PAX DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 3,922 hrs · 3,022 cycles

JUST AFTER TAKEOFF WITH FLAPS 20 AND TRIMS CENTERED THE AIRCRAFT ROLLS TO THE RIGHT. THIS HAPPENS IMMEDIATELY AFTER WEIGHT OFF WHEELS AND BECOMES LESS PRONOUNCED AFTER FLAP RETRACTION AND/OR INCREASE IN SPEED. SANDED ABRASION RESISTANT TEFLON FILM TO SPECIFIED LIMITS IAW CRJ MM 27-54-01-320-001.

Part: ACTUATOR — MALFUNCTIONED (STAB TRIM) · airframe 3,699 hrs · 2,844 cycles

INTERMITTENT STAB TRIM CH 1 STATUS MESSAGE. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW MM 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD. PN 4062-3 SN OFF 1102

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 2,519 hrs · 1,919 cycles

GEAR/FLAP EICAS INDICATIONS CAME ON INTERMITTANTLY FROM TAKEOFF THROUGH CLIMBOUT. REMOVED AND REPLACED FECU IAW 27-51-05. OPS CHECK GOOD AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 1,434 hrs · 1,087 cycles

FIRST CABIN CEILING EMERGENCY LIGHT IS INOP. REPLACED NR 1 ELBP IAW 33-51-04, OPS CHECK GOOD.