N446SW

Part: NOT ENTERED — WARNING MESSAGE (NOT ENTERED) · airframe 41,450 hrs · 37,814 cycles

GEAR DISAGREE WARNING MESSAGE CAME ON AFTER TAKEOFF. RIGHT MLG INDICATED UNSAFE. RAN THE QRH. MESSAGE WENT OUT. RIGHT MLG INDICATED UP. (FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26157809 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE CP 26161166, CP 26161548, CP 26158485, CP 26161533 AND CP 26161879 FOR MX ACTIONS. PERFORMED A FUNCTIONAL TEST OF THE EXTENSION AND RETRACTION SYSTEM IN REFERENCE TO CRJ 200 AMM 32-30-00, OPS CHECK GOOD AT THIS TIME, NO DEFECTS NOTED AT THIS TIME."

Part: NONE — UNCONTROLLABLE · airframe 41,222 hrs · 37,515 cycles

RUDDER LOCKED UP AT FLIGHT IDLE IN THE LANDING FLARE. NO RUDDER MOVEMENT AVAILABLE. (FLIGHT 4301 - FILED CLOSED) INSPECTED RUDDER SYSTEM CONTROL PATH REFERENCE EAMLS 1009518, 1009408, 100949 NO DEFECTS NOTED. INSPECTED POTENTIOMETER IN REFERENCE TO AMM 27-24-05 NO DEFECTS NOTED, INSPECTED RUDDER PCUS IN REFERENCE TO 27-23-01 NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECK OF RUDDER SYSTEM OPS CHECK GOOD IN REFERENCE TO AMM 27-21-00. FULL DEFLECTION OBTAINED, NO BINDING OR LOCKING. DOWNLOADED FDR REFERENCE EAML 1009408 MOVEMENT WAS OBSERVED.

Part: NONE — ODOR · airframe 40,703 hrs · 36,891 cycles

STRONG SMELL OF FUEL WHEN PACKS ARE ON WITH BOTH APU AND ENGINE BLEEDS. BOTH IN AIR AND ON GROUND. (FLIGHT 4267 - FILED CLOSED) PLEASE REFERENCE AML 898096 REMOVED AND REPLACED APU FUEL LINE REFERENCING AMM 49-31-01. OPS CHECK OF FUEL SYSTEM AND AIR CONDITIONING SYSTEM GOOD. NO LEAKS DETECTED.

Part: NONE — FAILED · airframe 39,970 hrs · 36,041 cycles

***CAT II NOT AUTHORIZED*** / D: DURING APPROACH, GEAR WAS SELECTED DOWN (180 KNOTS) AND RECEIVED A GEAR DISAGREE WARNING MESSAGE. THE NOSE DOOR OPENED BUT THE NOSE GEAR REMAINED UP (UP INDICATION). COMPLIED WITH QRH AND THE LANDING GEAR EXTENDED NORMALLY / C: MEL 32-30-1 / CAT A / EXPS 09/18/2021 / DURING APPROACH, GEAR WAS SELECTED DOWN (180 KNOTS) AND RECEIVED A GEAR DISAGREE WARNING MESSAGE. THE NOSE DOOR OPENED BUT THE NOSE GEAR REMAINED UP (UP INDICATION). COMPLIED WITH QRH AND THE LANDING GEAR EXTENDED NORMALLY. (FLIGHT 4293 - FILED CLOSED) SEP 17, 2021 STATION: CPR--DEFERRED LANDING GEAR RETRACTION SYSTEM PER MEL 32-30-1, MAINT ACTION COMPLIED, PLACARDS INSTALLED. / **ACFT DOWNGRADE FROM CAT II PER GMM CHAPTER 2 SECTION 23** / SEP 19, 2021 STATION: SLC -- REFERENCE CP 23504142 FOR NLG UPLOCK CHANGE. REFERENCE CP 23503346 FOR LANDING GEAR HEALTH CHECK. REFERENCE CP 23500511 FOR PSEU LOG READING. REFERENCE CP 23504309 FOR TROUBLESHOOTING NLG GEAR DISAGREE. REFERENCE CP 23500510 FOR FDR DOWNLOAD. SENIOR MANAGER APPROVES RTS.

Part: LANDING GEAR — FAULTED (RIGHT) · airframe 39,468 hrs · 35,456 cycles

ON APPROACH GOT GEAR DISAGREE, RIGHT MAIN. FOLLOWED QRH CYCLED GEAR AND MESSAGE CLEARED. LANDING NORMAL. ON APPROACH GOT GEAR DISAGREE, RIGHT MAIN. FOLLOWED QRH CYCLED GEAR AND MESSAGE CLEARED. LANDING NORMAL. (FLIGHT 4306) DEFERRED LANDING GEAR RETRACTION SYSTEM PER MEL 32-30-1. MAINT ACTION COMPLIED WITH. PLACARDS INSTALLED. ACFT DOWNGRADE FROM CAT II PER GMM CHAPTER 2 SECTION 23. AIRCRAFT UPGRADED TO CAT II. COMPLIED WITH TASK CARD 34-220-1021-SKY CRJ 200 CAT II RETURN TO SERVICE TEST.

Part: WIRE HARNESS — CRUSHED (RT MLG) · airframe 39,303 hrs · 35,236 cycles

D:GEAR DISAGREE WARNING MESSAGE ON APPROACH (RIGHT MAIN GEAR), LANDING GEAR LEVER WAS SELECTED UP IN THE GO-AROUND. COMPLIED WITH QRH, ALL LANDING GEAR EXTENDED NORMALLY ON SECOND ATTEMPT. / C: MEL 32-30-1 / CAT A DUE WITHIN 1 FLIGHT DAY FROM 04/04/2021 / CAT II NOT AUTHORIZED!!! / GEAR DISAGREE WARNING MESSAGE ON APPROACH (RIGHT MAIN GEAR), LANDING GEAR LEVER WAS SELECTED UP IN THE GO-AROUND. COMPLIED WITH QRH, ALL LANDING GEAR EXTENDED NORMALLY ON SECOND ATTEMPT. (FLIGHT 4317 - FILED CLOSED) APR 04, 2021 STATION: MQT--DEFERRED LANDING GEAR RETRACTION SYS PER MEL 32-30-1. MX ACTION COMPLIED WITH AND PLACARDS INSTALLED. / CAT II DOWNGRADED / APR 05, 2021 STATION: DTW -- INTEROGATED THE PSEU ON MEMORY MODE PER FIM 32-60-05 AND FOUND NO FAULTS RECORDED. PERFORMED AN EXTENSION AND RETRACTION TEST OF THE MLG SYSTEM ON SINGLE AND DUAL PUMP PER CRJ 200 AMM 32-30-00. PERFORMED A VISUAL INSPECTION OF THE RH MLG INBD HARNESS AND FOUND THE SHIELDING TO BE CRUSHED. REMOVED AND REPLACED RH MLG INBD ELECTRICAL HARNESS ASSEMBLY IN REF TO CRJ 200 AMM 32-61-20. OPS CHECK GOOD, NO DEFECTS NOTED. / COMPLIED WITH TASK CARD 34-220-1008-SKY CAT II RETURN TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 39,133 hrs · 35,021 cycles

ON DEPARTURE WHILE SELECTING FLAPS FROM 8 TO 0 HAD FLAPS FAIL CAUTION MSG. COMPLIED WITH QRH. FLIGHT 4240 - FILED CLOSED THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22314362 WITH THE FOLLOWING CORRECTIVE ACTION: "COMPLIED WITH PARAGRAPH (H)(6) OF AD 2009-06-12 AND AMOC APPROVAL LETTER LOG # 17-85 BY PERFORMING THE APPLICABLE MAINTENANCE ACTIONS SPECIFIED IN FAULT ISOLATION MANUAL (FIM) A-009, SECTION 27-50-00 OF VOLUME 1, REVISION 54, DATED NOVEMBER 10, 2017. / NOTE: IF THE LRU LOG MESSAGE INCLUDES JAM? AND THERE WAS AN OBVIOUS PHYSICAL OBSTRUCTION OF A FLAP PANEL, HINGE ARM OR BALLSCREW, AN INSPECTION OF THE AREA AND COMPONENTS AFFECTED SHOWS THAT NO DAMAGE TO COMPONENTS OR STRUCTURE RESULTED FROM THE OBSTRUCTION, AND THE FLAPS OPERATE NORMALLY, THE AIRCRAFT CAN BE RETURNED TO SERVICE WITH NO FURTHER ACTION. IN THIS CASE, INCLUDE WORDING IN THE CORRECTIVE ACTION SIMILAR TO: €ŒFOUND SNOW PACKED IN FLAP WELLS, CLEARED SNOW AND INSPECTED AREA, NO DAMAGE NOTED. OPERATED FLAPS WITH NO DEFECTS NOTED. COMPLIED WITH IN ACCORDANCE WITH FIM 27-50-00 REV. 54 AND AD 2009-06-12 AND AD CONTROL NUMBER 2009-06-12/09.€? / COMPLIED WITH SERIAL

Part: PANEL — DEBONDED (HORIZONTALS TAB) · airframe 38,764 hrs · 34,559 cycles

LT HORIZONTAL STABILIZER PANEL 333AL HAS DISBONDED UPPER AND LOWER GROUNDING PLATES. C-CHECK RO 10/29/2020. REMOVED AND REPLACED PANEL 333AL, REF AMM, CHECK OK.

Part: NUT PLATE — BROKEN (WG-BDY FAIRING) · airframe 38,764 hrs · 34,559 cycles

WING TO BODY FAIRING 195AL HAS A BROKEN NUT-PLATE, MARKED. C-CHECK RO 10/29/2020. REMOVED AND INSTALLED NEW NUT-PLATE P/N NAS1474A3 AT WING TO BODY FAIRING PANEL 195AL, REF CRJ 200 SRM.

Part: DOOR FRAME — CORRODED (BS 313) · airframe 38,764 hrs · 34,559 cycles

PAX DOOR FRAME FS 313.56 P/N 601R318086-1 CORRODED ON MULTIPLE SURFACES. C-CHECK RO 10/29/2020. FOUND PAX DOOR FRAME AT FS OH 313.56 TO BE OUT OF LIMITS, PER CRJ 200 SRM. REMOVED AND INSTALLED A NEW PAX DOOR FRAME AT FS.313.56, REF CRJ 200 AMM AND DWG. PERFORMED PRESSURE CHECK, REF CRJ 200 AMM, PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 38,764 hrs · 34,559 cycles

LT OUTBOARD FLAP, OUTBOARD HINGE ARM ASSEMBLY, AFT ATTACH BOLT CASTLE NUT APPEARS CORRODED. C-CHECK RO 10/29/2020. REPLACED LT OUTBOARD FLAP, OUTBOARD HINGE ARM ASSEMBLY, AFT ATTACH BOLT CASTLE NUT AND COTTER PIN WITH NEW PARTS (P/N: MS17825-4 AND P/N: MS24665-136), REF CRJ-200 AMM. USED TORQUE WRENCHES TUC8609 CAL DATE: 31-JUL-2021 AND TUC8619 CAL DATE: 31-OCT-2020.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,764 hrs · 34,559 cycles

PAX DOOR DD4 INTERCOSTAL (P/N 601R31902-317) HAS CORROSION. C-CHECK RO 10/29/2020. REMOVED CORROSION AND FOUND PAX DOOR INTERCOSTAL DD4 TO BE OUT OF LIMITS, REF CRJ 200 SRM. REMOVED AND INSTALLED A NEW PAX DOOR INTERCOSTAL DD4, REF CRJ 200 SRM AND DWG. PERFORMED PRESSURE CHECK, REF CRJ 200 AMM PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,764 hrs · 34,559 cycles

PAX DOOR DD6 INTERCOSTAL (P/N 601R3180571) HAS CORROSION. C-CHECK RO 10/29/2020. FOUND PAX DOOR INTERCOSTAL DD6 TO BE OUT OF LIMITS, AS PER CRJ 200 SRM. REMOVED AND INSTALLED A NEW PAX DOOR INTERCOSTAL DD6, REF CRJ 200 SRM AND DWG. COMPLIED WITH TASK CARD. PERFORMED PRESSURE CHECK, REF CRJ 200 AMM PRESSURE CHECK GOOD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: FORMER — CORRODED (PAX DOOR) · airframe 38,764 hrs · 34,559 cycles

PAX DOOR AFT FORMER AT FS 347.25 HAS CORROSION. C-CHECK RO 10/29/2020. REMOVED CORROSION ON THE PAX DOOR AFT FORMER AT FS 347.25, REF CRJ 200 SRM, FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED A NEW PAX DOOR AFT FORMER AT FS 347.25, REF CRJ 200 SRM AND DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: ATTACH ANGLE — CORRODED (BS 311) · airframe 38,764 hrs · 34,559 cycles

PAX DOOR FWD FORMER AT FS 311.75 HAS CORROSION. C-CHECK RO 10/29/2020. PAX DOOR FWD FORMER AT FS 311.75, FOUND TO BE OUT OF LIMITS, REF CRJ 200 SRM. REMOVED AND INSTALLED A NEW PAX DOOR FWD FORMER, REF CRJ 200 SRM AND DWG. COMPLIED WITH TASK CARD. PERFORMED PRESSURE CHECK, REF CRJ 200 AMM, PRESSURE CHECK GOOD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 38,764 hrs · 34,559 cycles

CARGO DOOR AFT BALANCE SPRING MOUNT STRUCTURE ON FS 621 BULKHEAD IS CRACKED. C-CHECK RO 10/29/2020. REMOVED AND REPLACED THE CARGO DOOR AFT BALANCE SPRING MOUNT BRACKET ON THE FS 621 BULKHEAD, REF CRJ 200 SRM AND DWG. PERFORMED PRESSURE CHECK, REF CRJ 200 AMM, PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 38,764 hrs · 34,559 cycles

CARGO DOOR UPPER NET SUPPORT, LOWER CLIP AT FS 621 CRACKED. C-CHECK RO 10/29/2020. REMOVED AND REPLACED CLIP P/N 601R35050-109, REF CRJ 200 SRM AND DWG.

Part: FITTING — CHAFED (CARGO DOOR LATCH) · airframe 38,764 hrs · 34,559 cycles

AFT CARGO DOOR FWD LATCH PIN FITTING ON DOOR SURROUND CHAFED, MARKED. C-CHECK RO 10/29/2020. REMOVED AND REPLACED THE CARGO DOOR FWD LATCH PIN FITTING, REF CRJ200 SRM. CHECKS ARE GOOD AT THIS TIME.

Part: STOP FITTING — CORRODED (AFT CARGO DOOR) · airframe 38,764 hrs · 34,559 cycles

AFT CARGO DOOR BOTTOM FWD STOP FITTING ON SILL CORRODED, MARKED. C-CHECK RO 10/29/2020. REMOVED AND REPLACED THE CARGO DOOR LOWER FWD STOP FITTING, REF CRJ200 SRM. CHECKS ARE GOOD AT THIS TIME.

Part: FITTING — CHAFED (CARGO DOOR LATCH) · airframe 38,764 hrs · 34,559 cycles

AFT CARGO DOOR AFT LATCH PIN FITTING ON FS 621.00 BULKHEAD CHAFED, MARKED. C-CHECK RO 10/29/2020. REMOVED AND REPLACED THE CARGO DOOR AFT LOWER CROTCH FITTING, REF CRJ200 SRM. CHECKS ARE GOOD AT THIS TIME.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 38,764 hrs · 34,559 cycles

LT & RT OUTBOARD FLAP CENTER HINGEBOX AT WS 222.00, AFT ATTACHING NUTS CORRODED, MARKED. C-CHECK RO 10/29/2020. INSTALLED 4 EA NEW AFT ATTACHING NUTS ON THE LT AND RT OUTBOARD CENTER HINGEBOX AT WS 222.00, REF CRJ200 AMM. TQ WRENCH TUC7837 NEXT CAL DUE: 30-NOV-20.

Part: STOP FITTING — CORRODED (AFT C DOOR FRAME) · airframe 38,764 hrs · 34,559 cycles

AFT CARGO DOOR BOTTOM AFT STOP FITTING ON SILL CORRODED, MARKED. C-CHECK RO 10/29/2020. REMOVED AND REPLACED THE CARGO DOOR LOWER AFT STOP FITTING, REF CRJ200 SRM. CHECKS ARE GOOD AT THIS TIME.

Part: DOUBLER — CORRODED (RT WING RIB) · airframe 38,764 hrs · 34,559 cycles

RT WS 53.60 BATT RIB CANNON PLUG DOUBLER CORRODED, MARKED. C-CHECK RO 10/29/2020. INSTALLED NEW REPLACEMENT DOUBLER ON RT WS 53.60 BATT RIB, REF CRJ200 SRM.

Part: RIB — CRACKED (RWS 48.3) · airframe 38,764 hrs · 34,559 cycles

RT WS 48.30 BATTERY RIB CAP CRACKED AT FWD/AFT ENDS, MARKED. C-CHECK RO 10/29/2020. INSTALLED NEW CAP ANGLE, PER CRJ 200 SRM AND INSTALLATION DWG.

Part: CHANNEL — CRACKED (RWS 53.6) · airframe 38,764 hrs · 34,559 cycles

RT WS 53.60 BATTERY RIB AFT CHANNEL CRACKED AT TOP, MARKED. C-CHECK RO 10/29/2020. REMOVED AND INSTALLED NEW BATTERY RIB ASSEMBLY P/N 601R10203-8, REF DWG CRJ200 SRM.

Part: ATTACH FITTING — CRACKED (AFT CARGO DOOR) · airframe 38,764 hrs · 34,559 cycles

AFT CARGO DOOR FWD UPPER ROLLER ATTACH FITTING ON DOOR CRACKED, MARKED. C-CHECK RO 10/29/2020. REMOVED AND REPLACED CARGO DOOR FITTING, REF SRM AND DWG. COMPLETED TASK CARD.

Part: DOUBLER — CORRODED (LT WING RIB) · airframe 38,764 hrs · 34,559 cycles

LT WS 53.60 BATT RIB CANNON PLUG DOUBLER CORRODED, MARKED. C-CHECK RO 10/29/2020. REMOVED CORRODED CANNON PLUG DOUBLER AND INSTALLED NEW LT WS 53.60 BATT RIB CANNON PLUG DOUBLER P/N 601R10203-33, REF CRJ 200 SRM AND DWG. SEE CONTINUATION FOR DETAILS.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 38,764 hrs · 34,559 cycles

RT INBOARD FLAP VANE ASSEMBLY INBOARD END RIB P/N 601R14304-14 AT FLAP STA 50.498 CRACKED. C-CHECK RO 10/29/2020. INSTALLED NEW END RIB PN 601R14304-14 ON RT INBOARD VANE ASSEMBLY, REF BOMBARDIER DWG AND CRJ200 SRM.

Part: GROUND STUD — CORRODED (BS 409) · airframe 38,764 hrs · 34,559 cycles

FS 409.00+80 STRG 0 CORRODED GROUND STUD HARDWARE, MARKED. C-CHECK RO 10/29/2020. REMOVED AND REPLACED STUDS, REF AMM, CHECK OK.

Part: FRAME — CRACKED (BS 333) · airframe 38,764 hrs · 34,559 cycles

FS 333.00 BETWEEN STRG 0 TO 1 LT FRAMED CRACKED, MARKED. C-CHECK RO 10/29/2020. REMOVED AND INSTALLED NEW FRAME AT FS 333.00 AT STGR 0-STGR 1L, REF CRJ200 SRM AND BOMBARDIER DRAWING. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: RIB — CRACKED (LWS 48.3) · airframe 38,764 hrs · 34,559 cycles

LT WS 48.30 BATTERY RIB CAP CRACKED AT FWD/AFT ENDS, MARKED. C-CHECK RO 10/29/2020. REMOVED AND REPLACED DAMAGED BATTERY RIB CAP ANGLE AT LT WS48.30, REF DWG AND CRJ200 SRM.

Part: STOP FITTING — GOUGED (E/E BAY DOOR) · airframe 38,764 hrs · 34,559 cycles

AVI COMPARTMENT LT FWD DOOR STOP FITTING ON SURROUND GOUGED ON UPPER EDGE, MARKED. C-CHECK RO 10/29/2020. EVAULATED AND DETERMINED DAMAGE TO BE OUT OF LIMITS. INSTALLED NEW AVIONICS COMPARTMENT LT DOOR SURROUND STOP FITTING, REF CRJ200 SRM. OPERATIONAL, RIGS, AND LEAK CHECKS ARE GOOD AT THIS TIME.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 38,764 hrs · 34,559 cycles

FS 409.00+128 TO FS 559.00 RBL 9 FLOOR BEAM CAP HAS SEVERAL AREAS OF CORROSION ON TOP, MARKED. C-CHECK RO 10/29/2020. BLENDED RBL 9 CORRODED AREAS TO A SMOOTH CONTOUR BETWEEN FS 409.00+128 AND FS 529.00, REF CRJ200 SRM. REMAINING MATERIAL IS WITHIN LIMITS. PERFORMED RBL 9 FLOOR BEAM SPLICE REPAIR BETWEEN FS 529.00 AND FS 559.00+10, REF REO. COMPLIED WITH TASK CARD. NO LEAKS NOTED.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 38,764 hrs · 34,559 cycles

FS 409.00+128-FS 559.00 LBL 9 FLOOR BEAM CAP HAS SEVERAL AREAS OF CORROSION ON TOP, MARKED. C-CHECK RO 10/29/2020. COMPLIED WITH PERMANENT REPAIR FS 409.00+128-FS 559.00 LBL 9 FLOOR BEAM CAP DAMAGE, REF REO. ALL APPLICABLE STEPS COMPLIED WITH.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 38,764 hrs · 34,559 cycles

FS 409.00+128-FS 559.00 LBL 9 FLOOR SEAT TRACK HAS SEVERAL AREAS OF CORROSION/GOUGES, MARKED. C-CHECK RO 10/29/2020. REPLACED CORRODED LBL 9 SEAT TRACK BETWEEN FS 409.00+128-FS 559.00, REF CRJ200 AMM.

Part: STOP FITTING — GOUGED (E/E BAY DOOR) · airframe 38,764 hrs · 34,559 cycles

AVI COMPARTMENT RT FWD DOOR STOP FITTING ON SURROUND GOUGED ON UPPER EDGE, MARKED. C-CHECK RO 10/29/2020. EVAAULATED AND DETERMINED DAMAGE TO BE OUT OF LIMITS. INSTALLED NEW AVIONICS DOOR COMPARTMENT RIGHT DOOR SURROUND FITTING, IAW CRJ200 SRM. OPERATIONAL, RIG, AND LEAK CHECKS ARE GOOD AT THIS TIME.

Part: ATTACH ANGLE — CRACKED (BS 621-625) · airframe 38,764 hrs · 34,559 cycles

AFT EQUIPMENT BAY, FS 621.00-FS 625.30, ATTACHING "CLIP" AT STGR 14L LEVEL CRACKED, FLAGGED. C-CHECK RO 10/29/2020. REMOVED AND REPLACED WITH NEW ATTACH CLIP AT STR 14L FS 621.0-FS 625.30, REF CRJ 200 SRM.

Part: HINGE — CHAFED (SERVICE DOOR) · airframe 38,764 hrs · 34,559 cycles

SERVICE DOOR HINGE IS CHAFED AND GOUGED IN SEVERAL LOCATIONS, MARKED. C-CHECK RO 10/29/2020. BLENDED, NO DEFECTS NOTED, EVALUATED REPAIR, FOUND OUT OF LIMITS. RECEIVED ENGINEERING REQUESTED SUPPORT REO COMPLIED WITH ALL STEPS OF REO PART IN LIMITS, ROTO PEENED REPAIRED AREA AND RESTORED THE FINISH, REF REO. COMPLIED WITH ALL STEPS OF REO.

Part: INTERCOSTAL — CORRODED (RWS 53.6) · airframe 38,764 hrs · 34,559 cycles

RT SIDE AFT SPAR INTERCOSTAL AT WS 53.60 HAS EVIDENCE OF CORROSION. C-CHECK RO 10/29/2020. REMOVED AND REPLACED RT AFT SPAR INTERCOSTAL AND SEAL AT WS 53.60. INSTALLATION COMPLETED, PER SRM AND DWG INSTALLATION. COMPLETED TASK CARD.

Part: INTERCOSTAL — CORRODED (LWS 53.6) · airframe 38,764 hrs · 34,559 cycles

LT SIDE AFT SPAR INTERCOSTAL HAS EVIDENCE OF CORROSION (AT BOTTOM) AT WS 53.60. C-CHECK RO 10/29/2020. FOUND LT SIDE AFT SPAR INTERCOSTAL CRACKED. REMOVED AND REPLACED LT SIDE AFT SPAR INTERCOSTAL (BATT RIB), REF CRJ 200 SRM, DWG. COMPLIED WITH TASK CARDS. NO LEAKS NOTED.

Part: ANGLE — CRACKED (BS 484) · airframe 38,764 hrs · 34,559 cycles

LBL 36 AT FS 484 ANGLE HAS CRACK. C-CHECK RO 10/29/2020. REMOVED AND INSTALLED A NEW ANGLE AT FS 484 LBL 36, REF REO. PERFORMED PRESSURE CHECK, REF CRJ 200 AMM, PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: FLOOR SUPPORT — CORRODED (PRESSURE DECK) · airframe 38,764 hrs · 34,559 cycles

CORROSION ON RT PRESSURE FLOOR SILL PANEL IN SEVERAL SPOTS BETWEEN FS 409+128 AND 559. C-CHECK RO 10/29/2020. REMOVED CORROSION FROM PRESSURE FLOOR SILL AT SEVERAL SPOTS PANEL BETWEEN FS 409+128 AND FS 559, REF REO. ALL SPOTS FOUND TO BE WITHIN LIMITS, AS PER REO. PERFORMED PRESSURE CHECK, REF CRJ 200 AMM, PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: STRAP — CORRODED (BS 559) · airframe 38,764 hrs · 34,559 cycles

LT FLOOR SUPPORT STRAP AT FS 559 OUTBOARD OF LBL 27 IS CORRODED. C-CHECK RO 10/29/2020. FOUND LT FLOOR SUPPORT STRAP AT FS 559 OUTBOARD OF LBL 27 TO BE OUT OF LIMITS, REF CRJ 200 SRM. REMOVED AND REPLACED FLOOR STRAP, REF CRJ200 SRM AND DWG. COMPLIED WITH TASK CARD. PERFORMED PRESSURE CHECK, REF CRJ 200 AMM, PRESSURE CHECK GOOD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: ANGLE — CRACKED (BS 605) · airframe 38,764 hrs · 34,559 cycles

AFT CARGO BAY AT FS 605.0 CLIP BELOW ENTRY WAY THRESHOLD HAS CRACK AT UPPER RADIUS. C-CHECK RO 10/29/2020. INSTALLED NEW CLIP FS 605 UNDER CARGO ENTRY WAY, REF CRJ 200 SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 38,764 hrs · 34,559 cycles

RBL 27 AT FS 484 ATTACHMENT CLIP IS CRACKED. C-CHECK RO 10/29/2020. REMOVED AND INSTALLED A NEW ATTACHMENT CLIP AT FS 484 RBL 27, REF REO AND CRJ 200 SRM. PERFORMED PRESSURE CHECK, REF CRJ 200 AMM, PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: FLOOR SUPPORT — CORRODED (PRESSURE DECK) · airframe 38,764 hrs · 34,559 cycles

CORROSION ON RT PRESSURE FLOOR ANGLE IN SEVERAL SPOTS BETWEEN FS 409+128 AND 559. C-CHECK RO 10/29/2020. REMOVED CORROSION ON THE RT PRESSURE FLOOR ANGLE BETWEEN FS 409+128 AND FS 559 AND FOUND ALL SPOTS TO BE WITHIN LIMITS, REF REO. PERFORMED PRESSURE CHECK, REF CRJ 200 AMM, PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: SEAT TRACK — CORRODED (BS 510) · airframe 38,764 hrs · 34,559 cycles

LT SIDE SEAT RAIL IS CORRODED AT APPROXIMATELY FS 510. C-CHECK RO 10/29/2020. REMOVED AND REPLACED LT SIDE SEAT RAIL FROM FS 501 TO FS 547, REF CRJ200 AMM.

Part: ANGLE — CRACKED (BS 589) · airframe 38,764 hrs · 34,559 cycles

AFT CARGO BAY AT FS 589 CLIP BELOW ENTRY WAY THRESHOLD HAS CRACK AT UPPER RADIUS. C-CHECK RO 10/29/2020. INSTALLED NEW CLIP FS 589 UNDER CARGO ENTRY WAY, REF CRJ 200 SRM AND DWG. COMPLIED WITH TASK CARD.

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 38,764 hrs · 34,559 cycles

LBL 27 AT FS 484 ATTACH ANGLE HAS CRACK. C-CHECK RO 10/29/2020. REMOVED CRACKED CLIP ON FS 484 AT LBL 27, REF CRJ 200 SRM. LOCATED AND DRILLED NEW CLIP PN: 601R31171-17, REF CRJ 200 SRM. INSTALLED NEW CLIP, REF CRJ 200 SRM AND REO FOR FASTENER IDENTIFICATION. WEIGHT STATEMENT: WEIGHT REMOVED .02LB, WEIGHT ADDED .02LB, NO WEIGHT CHANGE. TOOL TUC 1755 DUE 31-SEP-2021.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 38,764 hrs · 34,559 cycles

SEAT TRACK AT LBL 9 HAS SEVERAL SPOTS OF CORROSION FROM FS 409+64-FS 409+128. C-CHECK RO 10/29/2020. COMPLIED WITH REPLACEMENT OF SEAT TRACK RAIL, AT FS 409-00+64- FS 409+128 LBL 9, REF CRJ-200 AMM. TORQUE TUC4978 CAL DUE DATED 30-JUN-21.

Part: PUCK — CRACKED (BS 589-605) · airframe 38,764 hrs · 34,559 cycles

AFT CARGO BAY IN BETWEEN FS 589 AND FS 605.0 CARGO NET RING ATTACHMENT PAD HAS CRACK AT FWD INBOARD RADIUS. C-CHECK RO 10/29/2020. REMOVED AND REPLACED CARGO NET ATTACHMENT PAD FS 589-FS 605, REF CRJ 200 SRM AND DWG.

Part: STRAP — CORRODED (BS 559) · airframe 38,764 hrs · 34,559 cycles

RT FLOOR SUPPORT STRAP AT FS 559 OUTBOARD OF RBL 27 IS CORRODED. C-CHECK RO 10/29/2020. REMOVED DAMAGED FLOOR SUPPORT STRAP AND INSTALLED NEW STRAP P/N 601R31025-29 AT FS 559 OUTBOARD OF RBL 27, REF CRJ 200 SRM AND BOMBARDIER DWG. PERFORMED PRESSURE CHECK, REF CRJ 200 AMM, PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: FRAME — CORRODED (BS 310) · airframe 38,764 hrs · 34,559 cycles

CORROSION ON FS 310 FRAME BETWEEN STR 26L AND 27. C-CHECK RO 10/29/2020. INSTALLED NEW FRAME SECTION AT FS 310, PER CRJ200 SRM AND INSTALLATION DRAWING. INSTALLED NEW ANGLE SPLICE BRACKET, REF CRJ200 SRM AND INSTALLATION DRAWING. LEAK CHECKS ARE GOOD AT THIS TIME. COMPLIED WITH TASK CARD.

Part: FLOOR SUPPORT — CORRODED (PRESSURE DECK) · airframe 38,764 hrs · 34,559 cycles

CORROSION ON LT PRESSURE FLOOR ANGLE IN SEVERAL SPOTS BETWEEN FS 409+128 AND 559. C-CHECK RO 10/29/2020. REMOVED CORROSION ON THE LT PRESSURE FLOOR ANGLE, REF REO. FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO. PRESSURE CHECK GOOD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: FLOOR SUPPORT — CORRODED (PRESSURE DECK) · airframe 38,764 hrs · 34,559 cycles

CORROSION ON LT PRESSURE FLOOR SILL PANEL IN SEVERAL SPOTS BETWEEN FS 409+128 AND 559. C-CHECK RO 10/29/2020. REMOVED CORROSION FROM LT PRESSURE FLOOR SILL PANEL BETWEEN FS 409+128 AND FS 559.00. COMPLIED WITH ALL STEPS OF REO, LEAK CHECK GOOD, NO LEAKS FOUND AT THIS TIME.

Part: SEAT TRACK — CORRODED (BS 461-484) · airframe 38,764 hrs · 34,559 cycles

LT SIDE SEAT RAIL HAS CORROSION FROM APPROXIMATELY FS 461-FS 484. C-CHECK RO 10/29/2020. REMOVED AND REPLACED LT SIDE SEAT TRACK FROM APPROXIMATELY FS 449.85 TO FS 499.00, REF CRJ200 AMM.

Part: TRACK — WORN (CARGO DOOR) · airframe 38,764 hrs · 34,559 cycles

CARGO DOOR AFT TRACK WORN THRU AT UPPER STOP, MARKED. C-CHECK RO 10/29/2020. BLENDED OUT DAMAGE AT CARGO DOOR AFT RACK AND FOUND TO BE OUT OF LIMITS, REF REO. REMOVED AND INSTALLED A NEW CARGO DOOR AFT TRACK, REF DWG CRJ 200 SRM. PERFORMED PRESSURE CHECK, REF CRJ 200 AMM, PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: DOOR FRAME — CHAFED (PAX DOORWAY) · airframe 38,764 hrs · 34,559 cycles

PASSENGER DOOR SURROUND STRUCTURE FORWARD PULL IN LEVER FITTING STOP CHAFED, MARKED. C-CHECK RO 10/29/2020. BLENDED OUT CHAFE, NDT'ED REPAIR, EVALUATED-OUT OF LIMITS. REMOVED AND REPLACED WITH NEW DROP DOWN DOOR STOP, REF CRJ200 SRM.

Part: LUG — CHAFED (TE FLAP HINGE) · airframe 38,764 hrs · 34,559 cycles

RIGHT INBOARD FLAP, INBOARD FLAP HINGE LUG PLATES ARE CHAFED ON BOTH LOWER POSITIONS (2 EA), MARKED. C-CHECK RO 10/29/2020. COMPLIED WITH PERMANENT REPAIR RT INBOARD FLAP, INBOARD FLAP HINGE LUG, REF REO. VERIFIED ALL STEPS COMPLIED WITH.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 38,764 hrs · 34,559 cycles

RT MID FLAP VANE LEADING EDGE HAS ABRASION DAMAGE WS APPROXIMATELY 98, AS MARKED. C-CHECK RO 10/29/2020. INSTALLED NEW LEADING EDGE SKIN TO RT INBOARD VANE ASSEMBLY, REF BOMBARDIER DWG AND CRJ200 SRM.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 38,764 hrs · 34,559 cycles

RT INBOARD FLAP VANE LEADING EDGE HAS ABRASION DAMAGE WS APPROXIMATELY 60, AS MARKED. C-CHECK RO 10/29/2020. INSTALLED NEW LEADING EDGE SKIN TO RT INBOARD VANE ASSEMBLY, REF BOMBARDIER DWG AND CRJ200 SRM.

Part: LUG — CHAFED (LT WING TE FLAP) · airframe 38,764 hrs · 34,559 cycles

LT WING INBOARD FLAP HINGE LUG PLATES HAS CHAFING DAMAGE, AS MARKED. C-CHECK RO 10/29/2020. BLENDED, NO DEFECTS NOTED, EVALUATED REPAIR, FOUND OUT OF LIMITS. RECEIVED ENGINEERING REQUESTED SUPPORT REO, COMPLIED WITH ALL STEPS OF REO PART IN LIMITS. ROTO PEENED REPAIRED AREA AND RESTORED THE FINISH, REF REO. COMPLIED WITH ALL STEPS OF REO.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 38,764 hrs · 34,559 cycles

RT INBOARD FLAP VANE TRAILING EDGE HAS ABRASION DAMAGE WS APPROXIMATELY 98, AS MARKED. C-CHECK RO 10/29/2020. REPAIRED RT INBOARD FLAP VANE TRAILING EDGE, REF REO.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 38,764 hrs · 34,559 cycles

RT OUTBOARD FLAP VANE LEADING EDGE HAS ABRASION DAMAGE WS APPROXIMATELY 139, AS MARKED. C-CHECK RO 10/29/2020. INSTALLED NEW LEADING EDGE SKIN TO RT INBOARD VANE ASSEMBLY OUTBOARD END, REF BOMBARDIER DWG AND CRJ200 SRM.

Part: FASTENER — MISSING (FUSELAGE SKIN) · airframe 38,764 hrs · 34,559 cycles

FUSELAGE SKIN FASTENERS JUST FORWARD OF FS 202.75 AND BELOW WL 79.50 ON THE RT SIDE ONE (1 EA) FASTENER HEAD MISSING, THREE (3 EA) SUSPECTED TO BE LOOSE. C-CHECK RO 10/29/2020. THE LOOSE FUSELAGE SKIN RIVETS JUST FORWARD OF FS 202.75 HAVE BEEN REPLACED, REF CRJ200 SRM. THE DAMAGED RIVET BELOW WL 79.50 RT SIDE HAS BEEN REPLACED, REF CRJ200 SRM.

Part: STRIKER — DENTED (PAX DOOR) · airframe 38,764 hrs · 34,559 cycles

PREVIOUS REPAIR ON THE FS 349 PAX DOOR SEAL STRIKE FLANGE IS DENTED FROM ITS EDGE, FLAGGED. C-CHECK RO 10/29/2020. REPLACED REPAIR STRIP FROM PREVIOUS REPAIR, REF REO. COMPLIED WITH TASK CARD.

Part: SKIN — DENTED (BS 349) · airframe 38,764 hrs · 34,559 cycles

THE FUSELAGE SKIN AT APPROXIMATELY FS 349, BETWEEN STGR 3L AND STGR 11L AT THE EDGE OF THE PAX DOOR CUT-OUT HAS A DENT THAT APPEARS TO ALSO BE GOUGED UNDER A PREVIOUS TOPCOAT OF PAINT. C-CHECK RO 10/29/2020. REMOVED DAMAGED SKIN AND PERFORMED A FLUSH REPAIR. COMPLIED WITH REO. COMPLIED WITH TASK CARD. LEAK CHECK GOOD, NO LEAKS FOUND AT THIS TIME.

Part: SKIN — DENTED (AFT FUSELAGE) · airframe 38,764 hrs · 34,559 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA-THERE IS A DENT ON RIGHT SIDE OF THE AIRCRAFT BELOW AND SLIGHTLY AFT OF THE APU EXHAUST. COMPLIED WITH TEMPORARY REPAIR, PER REO. PERMANENT REPAIR DUE IN 4000 FLT HRS. DUE BY TAT 41463.9, PART NUMBER: -, SERIAL NUMBER: 7666, POSITION: C-CHECK RO 10/29/2020. APPLIED PERMANENT REPAIR TO DENT AT STR 18R AND FS 744 BY RECONTOURING DENT AND REPLACING SECTION OF STRINGER, REF REO. SEE CONTINUATION CARD FOR DETAILS.

Part: ROLLER PIN — FAILED (MLG) · airframe 37,199 hrs · 32,791 cycles

GEAR DISAGREE FOR RIGHT MAIN LANDING GEAR ON FINAL APPROACH. EXECUTED A GO AROUND AND THE GEAR POPPED DOWN. LANDED NORMALLY. (FLT#3818) CLOSED REMOVED AND REPLACED RH MLG UPLOCK ROLLER PIN IN IAW CMM. ADJUSTED RH MLG WHEEL BIN IAW AMM. PERFORMED MLG FUNCTIONAL TEST OF MLG EXTENSION AND RETRACTION IAW AMM, NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: STRUT — LOW (NLG) · airframe 36,956 hrs · 32,500 cycles

AFTER TAKEOFF RECEIVED A NOSE DOOR OPEN WARNING, GEAR DISAGREE WARNING, STEERING INOP CAUTION AND WOW INPUT CAUTION MESSAGES. RAN ALL THE QRH PROCEDURES AND RETURNED TO FIELD, NO EMERGENCY WAS DECLARED. LANDED WITHOUT INCIDENT. (FLT#4141) PERFORMED FULL SERVICE OF THE NLG STRUT IAW AMM. PERFORMED EXTENSION AND RETRACTION TEST OF THE LANDING GEAR IAW AMM. OPS CHECK GOOD. NO DEFECTS NOTICED AT THIS TIME. PERFORMED OPS TEST OF THE NWS IAW AMM. OPS TEST GOOD. NO MESSAGES SHOWING OR DEFECTS NOTED. A/C OKAY FOR SERVICE.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 35,900 hrs · 31,272 cycles

GEAR DISAGREE WARNING AFTER TAKE OFF. COMPLIED WITH QRH RESULTING IN A GEAR DOWN AND LOCKED, THREE GREEN INDICATION. RETURNED TO FIELD AND LANDING WAS NORMAL. (FLT 4445) CLOSED READJUSTED THE PROXIMITY SENSOR IAW AMM. OPS CHECK GOOD. REPLACED THE NLG SELECTOR VALVE IAW AMM, OPS CHECK GOOD , NO LEAKS NOTED. PERFORMED A PRESSURE DECAY RATE TEST IAW AMM, NO DEFECTS NOTED. ALSO PERFORMED AN EXTENSION AND RETRACTION OF THE LANDING GEAR IN IAW AMM, OPS CHECK GOOD, NO DEFECTS NOTED. A/C OK FOR SERVICE.

Part: WIRE HARNESS — FAILED (NLG DOWNLOCK) · airframe 33,728 hrs · 28,855 cycles

RETURN TO THE FIELD FOR GEAR DISAGREE DURING CLIMBOUT. REPLACED THE NLG DOWNLOCK HARNESS. OP CHECKED GOOD.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 32,016 hrs · 26,999 cycles

AFT CARGO DOOR ENTRY THRESHOLD HAS CORROSION. REPLACED CARGO DOOR ENTRY THRESHOLD FROM FS621-FS574 IAW REO.

Part: FITTING — CORRODED (FUSELAGE) · airframe 32,016 hrs · 26,999 cycles

AFT CARGO BAY AT LBL 27, AFT FLOOR SUPPORT FITTING HAS CORROSION ON UPPER CAP. INSTALLED THE REPAIR TO THE AFT CARGO BAY, LBL27 AFT FLOOR SUPPORT FITTING JUST FORWARD OF FS 621.0 IAW STS EA.

Part: CAP — WORN (TE FLAP VANE) · airframe 32,016 hrs · 26,999 cycles

RIGHT INBD FLAP VANE FWD EDGE WORN. R & R RT INBD FLAP VANE OTBD L/E CAP IAW SRM.

Part: GUIDE PLATE — CHAFED (FLAP FAIRING) · airframe 32,016 hrs · 26,999 cycles

LEFT WING FLAP FAIRING INBD GUIDE PLATE IS CHAFED UNDER PANEL 586BB. R & R LT WING FLAP FAIRING INBD GUIDE PLATE UNDER PANEL 586BB, WITH FACTORY NEW PART, PN: 601R14116-86 IAW SRM.

Part: SKIN — DENTED (FUSELAGE) · airframe 32,016 hrs · 26,999 cycles

THERE ARE 2 DENTS ABOVE THE LT PYLON BETWEEN THE APU INLET AND RAM AIR INLET. COLD WORKED, HAND DRESSED OUT THE DENT, REF STS EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,617 hrs · 25,552 cycles

EMERGENCY LIGHT INOPERATIVE. R & R NR 2 BATTERY PACK. EMERGENCY LIGHTS OPS CHECKED GOOD.

Part: DETECTOR — FAILED (CABIN AIR) · airframe 28,284 hrs · 23,188 cycles

DISPLAY COOL CAUTION MESSAGE IN FLIGHT. MESSAGE DID NOT CLEAR IN F/A OR STBY. REMOVED DISPLAY COOL LOW FLOW DETECTOR AND CLEANED DETECTOR PROBE. REINSTALLED IAW AMM.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 28,125 hrs · 23,010 cycles

EMERGENCY LIGHT CONNECTOR BROKEN FOR LOWER FLOOR EMERGENCY LIGHTS ON WARDROBE. C-CHECK, INSTALLED NEW CONNECTOR.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 28,125 hrs · 23,010 cycles

EMERGENCY LIGHT CONNECTOR BROKEN ON SIDEWALL PANEL 261BLW. C-CHECK, REPLACED CONNECTOR IAW EA.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 28,125 hrs · 23,010 cycles

RT INBD FLAP VANE OTBD CAP CHAFED, C-CHECK, BLENDED CHAFED AREA, FOUND WITHIN LIMITS IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 28,125 hrs · 23,010 cycles

RT INBD FLAP VANE CENTER OTBD CAP CHAFED, C-CHECK RO, BLENDED CHAFED AREA. OUT OF LIMITS IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 28,125 hrs · 23,010 cycles

RIGHT INBD FLAP VANE, INBD CAP CHAFED, C-CHECK, BLENDED CHAFED AREA ORIGINAL MATERIAL THICKNESS IS .050 MATERIAL REMOVED IS .016 REMAINING MATERIAL IS .034 WITIN LIMITS IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 28,125 hrs · 23,010 cycles

FOUND FWD FLOORBEAM AT BS 280 CRACKED. C-CHECK, REPLACED FWD FLOORBEAM WITH NEW IAW SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 28,125 hrs · 23,010 cycles

FOUND BS 280, RBL 9 INBD FLOORBEAM ANGLE CRACKED. C-CHECK, REPLACED FLOORBEAM ANGLE WITH NEW.

Part: STIFFENER — CRACKED (BS 409 BULKHEAD) · airframe 28,125 hrs · 23,010 cycles

INBOARD VERTICAL BEAM AT BS 409+128 BULKHEAD AND LBL 27 CRACKED AT LOWER RIVET. C-CHECK, REPLACED INBD VERTICAL BEAM AT FS 409+128 BULKHEAD AND LT BL 27.

Part: FLOOR PANEL — CRACKED · airframe 28,125 hrs · 23,010 cycles

CRACK ON TRU FLOOR UNDER BRAKE ACCUMULATOR GAUGES, C-CHECK, REPAIRED FLOOR IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 28,125 hrs · 23,010 cycles

BS 280 FLOORBEAM AT LBL 9 OTBD SIDE ANGLE CRACKED ON UPPER RADIUS. C-CHECK, REPLACED ANGLE WITH NEW, IAW SRM.

Part: SUPPORT — CRACKED (RT WINDSHIELD) · airframe 28,125 hrs · 23,010 cycles

RT WINDSHIELD SIDE POST SUPPORT CRACKED. C-CHECK, REPLACED RT SIDE WINDSHIELD SIDE POST SUPPORT IAW SRM.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 28,125 hrs · 23,010 cycles

FLOORBEAM AT BS 484 HAS CRACKED ANGLE AT RBL 27. C-CHECK, R & R ANGLE IAW SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 28,125 hrs · 23,010 cycles

BS 280 FLOORBEAM AT LBL 9 INBD SIDE ANGLE CRACKED ON UPPER RADIUS. C-CHECK, REPLACED FLOORBEAM ANGLE WITH NEW IAW SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 28,125 hrs · 23,010 cycles

BS 280 FLOORBEAM AT RBL 9 INBD SIDE ANGLE CRACKED ON UPPER RADIUS. C-CHECK, FLOORBEAM ANGLE REPLACED IAW REO.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 28,125 hrs · 23,010 cycles

FLOORBEAM AT BS 484 HAS CRACKED ANGLE AT RBL 36. C-CHECK R & R ANGLE IAW SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 28,125 hrs · 23,010 cycles

BS 280 FLOORBEAM AT RBL 9 - 15 LOWER ANGLE CRACKED. C-CHECK, REPLACED WITH NEW IAW SRM .

Part: FLOORBEAM — CRACKED (BS 280) · airframe 28,125 hrs · 23,010 cycles

BS 280 FLOORBEAM AT RBL 9 OTBD SIDE ANGLE CRACKED ON UPPER RADIUS. C-CHECK, FLOORBEAM ANGLE REPLACED IAW REO.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 28,125 hrs · 23,010 cycles

FLOORBEAM AT BS 484 HAS CRACKED ANGLE AT LBL 36. C-CHECK, R & R ANGLE IAW SRM.

Part: SKIN — GOUGED (BS 774) · airframe 28,125 hrs · 23,010 cycles

RT SIDE AFT EXTERIOR SKIN HAS A GOUGE WITH A DENT AT FS 774, 3.5" BELOW STAB BASE, C-CHECK, DAMAGE OUT OF LIMITS, CUT OUT DENT AND INSTALLED A REPAIR DOUBLER IAW SRM.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 28,125 hrs · 23,010 cycles

FLOORBEAM AT BS 484 HAS CRACKED ANGLE AT LBL 27. C-CHECK, R & R ANGLE IAW SRM.

Part: SUPPORT — CRACKED (LT WINDSHIELD) · airframe 28,125 hrs · 23,010 cycles

LEFT WINDSHIELD SIDE POST SUPPORT CRACKED. C-CHECK, R & R LT WINDSHIELD SIDE POST SUPPORT ANGLE IAW SRM.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 28,125 hrs · 23,010 cycles

PAX DOOR AFT DRAG ANGLE CRACKED AT PREVIOUS REPAIRED SPLICE. C-CHECK, REMOVED DAMAGED PAX DOOR AFT DRAG ANGLE AND INSTALLED NEW REPAIR SPLICE IAW SRM.

Part: STRIKER — GOUGED (PAX DOOR SEAL) · airframe 28,125 hrs · 23,010 cycles

PAX DOOR SEAL STRIKER, FUSELAGE SIDE, GOUGED AT FS 349 AND STGR 7L. C-CHECK, REPAIRED PAX DOOR SEAL STRIKER IAW REO.

Part: STIFFENER — CRACKED (BS 409) · airframe 28,125 hrs · 23,010 cycles

CRACK NOTED ON BS 409+128 VERTICAL POST AT BL 0, RT CHANNEL IN THE AFT RADIUS. C-CHECK, R & R THE VERTICAL POST IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 28,125 hrs · 23,010 cycles

LT INBD FLAP VANE CHAFED. C-CHECK, BLENDED CHAFE ON LT INBD FLAP CENTER VANE CAP IAW REO AND SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 28,125 hrs · 23,010 cycles

LT INBD FLAP VANE CHAFED AT OTBD LOCATION. C-CHECK, BLENDED CHAFE ON LT INBD FLAP VANE OTBD CAP IAW REO AND SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 28,125 hrs · 23,010 cycles

LEFT INBD FLAP VANE CHAFED AT INBD LOCATION. C-CHECK, BLENDED CHAFE ON LT INBD FLAP VANE AND FOUND TO BE OUT OF LIMITS, IAW REO.

Part: WIRE HARNESS — FAILED (NLG) · airframe 27,340 hrs · 22,183 cycles

NOSE GEAR DID NOT RETRACT. GEAR DISAGREE WARNING & NOSE DOOR WARNING MESSAGES. FLT 4639 REPLACED NLG CENTER EXTEND RT WOW HARNESS ASSEMBLY. CYCLED NLG, OPERATIONS CHECKED OK. PN ON OFF 17300-205, SN ON 070404001 & SN OFF 5-800.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 26,863 hrs · 21,703 cycles

DENT & GOUGE FOUND IN SKIN AT TOP OF FS 559.00+96 ADJACENT TO STRINGER 2R MEASURES OUT OF LIMITS. C-CHECK REPAIRED DAMAGE AT FS 559.00+96 ADJACENT TO STRINGER 2R, CUT OUT DAMAGED AREA & APPLIED DOUBLER IAW SRM.

Part: UPLOCK — FAILED (MLG) · airframe 26,051 hrs · 20,883 cycles

FLT 4828. GEAR DISAGREE, RT MAIN GEAR WOULD NOT DROP, AFTER FOLLOWING QRH GEAR CAME DOWN. REPLACED THE RIGHT MAIN SIDE STAY ACTUATOR. INSPECTED UPLOCK ROLLER AND HOOK ASSEMBLY, NO DEFECTS NOTED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,836 hrs · 20,659 cycles

TWO CEILING EMERGENCY LIGHTS DO NOT ILLUMINATE. (FLT 4663) REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM. P/N: 2013-1A P/N OFF: AD-2013-1A S/N ON: 112663 S/N OFF: 73207

Part: BRAKE SYS — CONTAMINATED (RIGHT) · airframe 25,684 hrs · 20,510 cycles

ON ROLL OUT WITH THRUST REVERSE FULL AND EVEN N1, AIRCRAFT KICKED TO LEFT. MAX RIGHT RUDDER WITH SLIGHT BRAKE PRESSURE TO OBTAIN CONTROLLING. (FLT 4490) TAXIED A/C, USED T/RS, T/R'S DEPLOY AND POWER UP EVENLY. FELT RIGHT BRAKES WERE LESS EFFECTIVE THAT LEFT. BLEED RIGHT I/B & O/B BRAKE. TAXIED A/C. OPS CHECK GOOD AT THIS TIME.

Part: BYPASS VALVE — FAILED (MLG) · airframe 25,537 hrs · 20,359 cycles

SELECTED THE GEAR HANDLE DOWN AND BOTH MAINS STAYED UP AND RECEIVED A GEAR DISAGREE. RAN QRH GEAR STAYED DOWN AND LOCKED WITH MANUAL EXTENSION. (FLT 4576) REPLACED MLG RUN AROUND AND BYPASS VALVE ASSEMBLY IAW AMM. P/N: 750004000-003 S/N ON: 328A S/N OFF: 797A, P/N: 750005000 S/N ON: 0994 S/N OFF: 0021

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 25,484 hrs · 20,298 cycles

F/O WINDSHIELD CRACKED. (FLT 4623) REPLACED F/O WINDSHIELD IAW AMM. P/N ON NP-139321-14 S/N ON 11048H8320 P/N OFF NP-139321-12 S/N OFF 03204H9458

Part: ACTUATOR — FAILED (TE FLAP) · airframe 25,464 hrs · 20,280 cycles

FLAPS FAIL AT 0° DURING APPROACH RETURN TO FIELD. (FLT 7381) REPLACED OF RIGHT FLAP ACTUATORS AND RIGHT BPSU.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,220 hrs · 20,061 cycles

RIGHT EMERGENCY EXTERIOR LIGHT BURNED OUT. (FLT 4778) RELAMPED EMERGENCY LIGHT.

Part: TRIM PANEL — FAILED (RUDDER SYS) · airframe 24,957 hrs · 19,826 cycles

THE RUDDER TRIM MOVED TO THE FULL LEFT POSITION, UNCOMMANDED. (FLT 4562) REPLACED RUDDER TRIM PANEL ASSEMBLY IN REFERENCE TO AMM. P/N OFF: 601R51226-235W1

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,950 hrs · 19,819 cycles

LEFT WING FORWARD EMERGENCY EXIT LIGHT IS INOPERATIVE. (FLT 4763) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,879 hrs · 19,757 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7796) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,729 hrs · 19,619 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4715) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,652 hrs · 19,543 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4538) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,032 hrs · 18,974 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4778) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,907 hrs · 18,860 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4800) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,867 hrs · 18,818 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,806 hrs · 18,753 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4570) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,551 hrs · 18,499 cycles

NR 5 EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,551 hrs · 18,499 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT4525) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,423 hrs · 18,386 cycles

SECOND TO AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4553) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,423 hrs · 18,386 cycles

LEFT FORWARD OVERWING EXTERIOR EMERGENCY EXIT LIGHT IS OUT. (FLT 4458) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,260 hrs · 18,226 cycles

NR 3 CEILING EMERGENCY LIGHT IS OUT. (FLT 4630) RELAMPED EMERGENCY LIGHT.

Part: WIRE — BROKEN (CABIN) · airframe 23,125 hrs · 18,106 cycles

LEFT WING AFT EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) FOUND CONNECTOR P4LF TO HAVE BROKEN PIN IN RECEPTACLE 21. REPAIRED WIRE AND PIN. ALSO REPLACED NR 4 ELBP BATTERY CHARGER.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,092 hrs · 18,078 cycles

RIGHT AND LEFT OVERWING MIDDLE EXTERNAL EMERGENCY LIGHTS ARE OUT. (FLT 4459) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,952 hrs · 17,952 cycles

LEFT AFT EXTERIOR OVERWING AND SERVICE DOOR EXTERIOR EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,952 hrs · 17,952 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,683 hrs · 17,702 cycles

AFT CEILING EMERGENCY LIGHT IS OUT. (FLT 4491) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,651 hrs · 17,672 cycles

FORWARD OVERHEAD EMERGENCY LIGHT IS OUT. (FLT4554) RELAMPED EMERGENCY LIGHT.

Part: BLEED AIR SYS — CONTAMINATED · airframe 21,530 hrs · 16,722 cycles

A "SMOKE TOILET" CAUTION MESSAGE WITH NO VISABLE SMOKE, BUT PASSENGERS WERE COMPLAINING ABOUT EYES BURNING. (FLT 4806) VERIFIED THAT DE-ICE FLUID CONTAMINATED THE BLEED SYSTEM. RAN APU WITH BOTH PACKS ON FOR SEVERAL HOURS AND SMELL/FUMES DISSIPATED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,588 hrs · 16,771 cycles

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

Part: ROLLER — LACK OF LUBE (SERVICE DOOR) · airframe 19,747 hrs · 15,224 cycles

GALLEY SERVICE DOOR IS HARD TO OPEN. (FLT 4536) LUBED SERVICE DOOR ROLLER AND DOOR SEAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,636 hrs · 15,136 cycles

EMERGENCY CEILING LIGHT NR 3 INOP. (FLT 4456) RELAMPED EMERGENCY LIGHT.

Part: WIRE — CHAFED (PITCH TRIM) · airframe 19,586 hrs · 15,096 cycles

PITCH TRIM INDICATION MOVING UNCOMMANDED. (FLT 4747) REPAIRED CHAFED WIRE ON NR 2 FEEDBACK RESOLVER.

Part: CONTROL UNIT — FAULTY (STAB PITCH) · airframe 19,438 hrs · 14,978 cycles

STAB TRIM MOVING UNCOMMANDED. (FLT 4685) REPLACED PITCH FEEL CONTROL UNIT AND HSTCU.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,906 hrs · 14,552 cycles

AFT EMERGENCY LIGHT INOP. (FLT 4502) RELAMPED EMERGENCY LIGHT.

Part: TRACK — DIRTY (GALLEY DOOR) · airframe 18,777 hrs · 14,446 cycles

GALLEY DOOR HARD TO OPEN FROM OUTSIDE. (FLT 4517) CLEANED DOOR FRAME ROLLER TRACKS.

Part: LENS — MISSING (CABIN) · airframe 18,362 hrs · 14,108 cycles

LENS ON EXIT ROW CEILING SIGN MISSING. (FLT 4675) INSTALLED LENS COVER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,168 hrs · 13,963 cycles

NR 3 CEILING EMERGENCY LIGHT INOP. (FLT 4500) RELAMPED EMERGENCY LIGHT.

Part: DOOR — UNKNOWN (MAIN PAX) · airframe 18,128 hrs · 13,933 cycles

FLT 4551 - MAIN CABIN DOOR IS HARD TO OPEN. OPERATION NORMAL, NO DEFECTS FOUND.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 17,626 hrs · 13,566 cycles

FLT 4810 - CABIN EMERGENCY LIGHTS, CEILING LEVEL, INOP. RELAMPED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 17,228 hrs · 13,260 cycles

C-CHECK, FS 280 INBOARD AND OUTBOARD CLIPS CRACKED. REPLACED PER SRM.

Part: MOUNT — CORRODED (RT ENGINE) · airframe 17,228 hrs · 13,260 cycles

DURING C-CHECK, RIGHT ENGINE AFT THRUST MOUNT CORRODED. REPLACED PER AMM.

Part: FITTING — CRACKED (BS 625) · airframe 17,228 hrs · 13,260 cycles

C-CHECK, UPPER LEFT FS 625 CLIP CRACKED ON PRESSURE BULKHEAD. REPLACED PER SRM.

Part: FITTING — CRACKED (BS 625) · airframe 17,228 hrs · 13,260 cycles

DURING C-CHECK, UPPER RIGHT FS 625 CLIP CRACKED ON PRESSURE BULKHEAD. REPLACED PER SRM.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 17,157 hrs · 13,203 cycles

FLT 6469 - LEFT WINDSHIELD CRACKED. REPLACED WINDSHIELD.

Part: SUPPORT BEAM — CRACKED (ENGINE) · airframe 17,091 hrs · 13,151 cycles

AD INSPECTION, ENGINE SUPPORT BEAM INSPECTION PER AD CONFIRMED CRACKS. REPAIRED PER SB 601R-53-061.

Part: CONNECTOR — ARCED · airframe 15,296 hrs · 11,755 cycles

PIN E ON J141 SHOWS SIGNS OF ARCING. REPLACED CONNECTOR. OPS CHECKS GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 13,070 hrs · 10,035 cycles

FOUND RIGHT SIDE WINDOW IS CRACKED. REPLACED RIGHT SIDE WINDOW IAW AMM 56-12-01, P/N NP139322-001, S/N 02063H9831.

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 13,001 hrs · 9,985 cycles

AFTER GEAR EXTENSION, HYD PUMP 3A CAUTION MESSAGE. HYDRAULIC SYSTEM 3 EMPTY. REPLACE O-RING ON NR 3A PRESSURE MANIFOLD. OPERATIONAL CHECK GOOD.

Part: WEB — CRACKED (PAX DOOR) · airframe 12,754 hrs · 9,801 cycles

PAX DOOR AFT WEB/CRACKED UNDER HANDRAIL, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED HANDRAIL SUPPORT FITTING FOR PAX DOOR AFT WEB PER SRM 51-42-21.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 12,754 hrs · 9,801 cycles

LBL9 STA 280 UPPER FLOOR SUPPORT HAS CRACK, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FILLER ANGLE AND REPAIR SPLICE ANGLE PER REO 601R 53-11-136 REV 'C' SHT 1-4.

Part: BRACKET — CRACKED (BRAKE TRANSDUCER) · airframe 12,754 hrs · 9,801 cycles

RT FWD BRAKE TRANSDUCER BRACKET IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW BRACKET RT SIDE PER SRM 51-42-06.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 12,754 hrs · 9,801 cycles

FWD SIDE OF PAX DOOR CRACK TOP OF DOOR OPEN BENEATH TOP FOLDING STEP, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLE AND FILLER AT PAX DOOR FWD SIDE TOP STEP PER CRJ200 REO 601R-52-11-279.

Part: WEB — CRACKED (PAX DOOR) · airframe 12,754 hrs · 9,801 cycles

PAX DOOR FWD WEB CRACKED UNDER HANDRAIL, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS TO REPAIR CRACKED PAX DOOR FWD WEB AS PER REO 601R-52-11-702 REV A.

Part: ATTACH ANGLE — CRACKED (PAX DOOR ASSIST) · airframe 12,754 hrs · 9,801 cycles

PAX DOOR ASSIST MOTOR ATTACH ANGLE/LOWER CRACKED RADIUS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW ANGLE 601R-317745-7 IAW CRJ200 SRM 51-42-06.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 12,754 hrs · 9,801 cycles

PAX DOOR HANDLE CRACKED OUTER, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED OUTER HANDLE ASSY, SPLINED SHAFT AND HANDLE FLAP IAW CRJ200 AMM 52-11-03-400-802.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 12,754 hrs · 9,801 cycles

LBL9 STA 280 LWR FLOOR SUPPORT HAS CRACK, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE, REPAIR ANGLE, CLIPS AND FILLERS PER REO 601R-53-11-171 REV C SHEET 1-2.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 12,754 hrs · 9,801 cycles

STA 484 RBL 36 INTERCOSTAL CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLE TO FS 484 INTERCOSTAL RBL36 PER CRJ200 SRM 51-42-06 PG 11 AND 51-42-21 PG 17.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 12,754 hrs · 9,801 cycles

FOUND STA 484 LBL36 AND LBL27 INTERCOSTAL CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLE TO FS 484 INTERCOSTAL RBL 36 PER CRJ200 SRM 51-42-06 PG 11 AND 51-42-21 PG 17.

Part: FRAME — CRACKED (BS 280) · airframe 12,754 hrs · 9,801 cycles

RBL9 LWR FRAME CRACKED AT FS 280, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR FILLER ANGLE AND SPLICE AT FS 280 RBL 9 AS PER REO 601R-53-11-136 REV C SHEET 1-4.

Part: BRACKET — CRACKED (BRAKE TRANSDUCER) · airframe 12,754 hrs · 9,801 cycles

LT BRAKE TRANSDUCER BRACKET CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW BRACKET LT SIDE PER SRM 51-42-06.

Part: ATTACH FITTING — CRACKED (BS 625) · airframe 12,754 hrs · 9,801 cycles

FS 625 RT SIDE CLIPS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP DW 9310 P/N 601-35012-52 P/O 72055 PER REO 601R-53-61-422.

Part: ATTACH FITTING — CRACKED (BS 625) · airframe 12,754 hrs · 9,801 cycles

FS 625 LT SIDE CLIPS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP P/N 601-35012-51 P/O 71471 PER REO 601R-53-61-422.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 12,754 hrs · 9,801 cycles

FS 280 RBL9 UPPER FLOOR SUPPORT HAS SUSPECT CRACK, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED RT I/B SUPPORT CLIP PER REO 601R-53-11-136 REV NC.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 10,533 hrs · 8,166 cycles

FLIGHT SPOILER FAULT. REPLACED NR 1 SECU IAW AMM 27-61-05. OPERATIONAL CHECKS GOOD, SN OFF: 0314.

Part: RELAY — MALFUNCTIONED (SPOILERS) · airframe 10,486 hrs · 8,126 cycles

SPOILERONS FAULT MESSAGE WOULD NOT CLEAR. REPLACED RELAY K4CN. OPERATIONAL CHECK GOOD IAW 24-01-11. SPOILERONS OPERATIONAL CHECK GOOD IAW AMM 27-61-00.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 10,279 hrs · 7,979 cycles

SPOILERONS FAULT, INBOARD GND SPOILER FAULT STATUS MSG. REPLACED RIGHT OUTBOARD SPOILERON PCU IAW 27-62-01 AND SECU NR 1 IAW MM 27-61-05, OPERATIONAL CHECK OK. P/N ON 49-164-06, S/N OFF 01598, P/N ON 270007, S/N OFF 4508.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 9,781 hrs · 7,602 cycles

"FLT SPLR" CAUTION AT THE GATE. REPLACED NR 2 SECU PER MM 27-61-05. OPERATIONAL CHECK GOOD.

Part: SUPPORT BEAM — DAMAGED (LT ENGINE) · airframe 9,668 hrs · 7,511 cycles

DAMAGE FOUND ON LT LOWER OB ENGINE SUPPORT BEAM WEB (601-35006-147/SB) UNDER FWD IB PANEL NUT PLATE FWD OF FS640.00 AFT OF FS 625.30 AND OB OF LBL36.20, IB OF WL111.09 APPROX 3 INCH LONG, ITEM FOUND AT ROUTINE INSPECTION. C/W REPAIR OF LT LOWER OB ENGINE SUPPORT BEAM IAW REO 601R-53-61-358.

Part: CONTROL UNIT — MALFUNCTIONED (MOTOR) · airframe 9,213 hrs · 7,146 cycles

STAB CH2 INOP, WILL NOT ENGAGE. REPLACED MCU IAW MM 27-42-05. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 9,213 hrs · 7,146 cycles

STAB CH2 STATUS MSG. REPLACED HSTCU IAW 27-40-00. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 9,149 hrs · 7,098 cycles

A -STAB CH 1 INOP MESSAGE- WHEN TRIMMING STAB TRIM NOSE UP. REPLACED STAB ACTUATOR AND MOTOR CONTROL UNIT IAW AMM 27-42-01 AND AMM 27-42-05. OPERATIONAL CHECK GOOD IAW AMM 27-41-00. P/N 7062-3, SN/OFF 255.

Part: CONTROL UNIT — MALFUNCTIONED (ACTUATOR) · airframe 8,650 hrs · 6,698 cycles

STAB CH 1 INOP. REPLACED MCU AND HORIZONTAL ACTUATOR. COMPLIED WITH RII 27-415 IAW MM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD. P/N 8396-3, S/N OFF 912.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,650 hrs · 6,698 cycles

REAR, LEFT SIDE EMERGENCY LIGHT INOPERATIVE. INSTALLED A NEW FLOOR LEVEL POWER STRIP IN THE AFT POSITION. OPERATIONAL CHECK GOOD.

Part: TRIM PANEL — STUCK (AILERON) · airframe 8,638 hrs · 6,688 cycles

AILERON TRIMS ONE DIRECTION. REPLACED AILERON TRIM PANEL. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED · airframe 8,543 hrs · 6,610 cycles

ON SHORT FINAL, GOT WHITE SPOILERON FAULT AND WHITE INBOARD GROUND SPOILER FAULT. REPLACED NR 2 SECU WITH A SERVICEABLE UNIT IAW 27-00-00.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 8,332 hrs · 6,435 cycles

SMOKE CARGO WARNING AT GATE WHILE LOADING BAGS. CLEARED ON ITS OWN. REPLACED NR 2 CARGO SMOKE DETECTOR IAW 26-15-01. OPERATIONAL CHECK GOOD.

Part: FLOORBEAM — CRACKED (CRACKED) · airframe 9,294 hrs · 7,215 cycles

CARGO COMPARTMENT FS 621 LHS FLOOR SUPPORT ANGLE CRACKED, ITEM FOUND AT C CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R53-61-117 REV "C".

Part: FLOORBEAM — CRACKED (BS 280) · airframe 9,294 hrs · 7,215 cycles

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

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 9,294 hrs · 7,215 cycles

FOUND FS 625 LT INTERCOSTAL ANGLE CRACKED STR 14L, ITEM FOUND AT C CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, AND 51-42-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 9,294 hrs · 7,215 cycles

FOUND FS 280 RT FLOORBEAM INBD AND OB ANGLES RBL 9.0 CRACKED, ITEM FOUND AT C CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 6,343 hrs · 4,883 cycles

(FLAPS FAIL) CAUTION MESSAGE ON APPROACH, AFTER SELECTING FLAPS 8. REPLACED LT IB NR 1 AND NR 2 FLAP ACTUATORS WITH SERVICEABLE UNITS IAW MM 27-53-01. P/N: 852D100-19, S/N OFF: 3561, P/N: 852D100-19, S/N OFF: 3612.

Part: ACTUATOR — FAILED (TE FLAP) · airframe 6,301 hrs · 4,850 cycles

FLAPS FAIL CAUTION MESSAGE ON APPROACH. FLAPS FAILED AT ZERO. REMOVED AND REPLACED NR 4 FLAP ACTUATOR IAW MM 27-53-01, 27-53-05. OPERATIONAL CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 6,157 hrs · 4,740 cycles

AFT CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED AFT CEILING LIGHT BULB AS REQUIRED. OPERATIONAL CHECK GOOD IAW MM 33-01-05.

Part: PANEL — INTERMITTENT (AILERON TRIM) · airframe 6,089 hrs · 4,686 cycles

AILERON TRIM SWITCH DOES NOT TRIM PROPERLY (INTERMITTENT). REMOVED AND REPLACED AILERON TRIM PANEL, OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 6,049 hrs · 4,656 cycles

LT SIDE EMERGENCY LIGHTS (OUTSIDE) ARE OUT. REMOVED AND REPLACED LT FORWARD EMERGENCY LIGHT LAMP. OPERATIONAL CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (SPOILERS) · airframe 4,851 hrs · 3,724 cycles

DURING TAKEOFF ATTEMPT RECEIVED CONFIG SPOILER MESSAGE, THEN INBOARD AND FLIGHT SPOILER FAULT MESSAGE. COMPLIED WITH SPOILERON SYSTEM RESET PROCEDURE AS PER AMM 27-61-05. OPERATIONAL CHECK GOOD.

Part: SHAFT — CORRODED (DOOR HANDLE) · airframe 4,557 hrs · 3,491 cycles

DISCOVERED DURING C-CHECK INSPECTION, CREW ESCAPE HATCH OUTER HANDLE SHAFT IS CORRODED. REPLACED CREW ESCAPE HATCH OUTER HANDLE IAW HARTWELL CORPORATION CMM 52-22-03. OPS CHECKS GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,557 hrs · 3,491 cycles

DISCOVERED DURING C-CHECK INSPECTION, FS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED. ANGLE AT STR 14R, FS 625 REPLACED IAW CRJ SRM 51-40-11 AND 51-42-06.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,557 hrs · 3,491 cycles

DISCOVERED DURING C-CHECK INSPECTION, FS 621 RIGHT FLOOR SUPPORT ANGLE CRACKED. REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV ''A'' AND RII 53-401.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,557 hrs · 3,491 cycles

DISCOVERED DURING C-CHECK INSPECTION, FS 280 RIGHT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21, 51-23-00 & RII 53-401.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 3,607 hrs · 2,762 cycles

SPOILER FAULT MESSAGE INBOARD GROUND SPOILERS AND FLIGHT SPOILERS. REMOVED AND REPLACED NR 2 SECU IAW 27-61-05. OPS CHECK GOOD.

Part: PCU — MALFUNCTIONED (NR 2 SPOILERON) · airframe 1,370 hrs · 1,053 cycles

CONFIG SPOILER MASTER WARNING MESSAGE CAME ON AT 70 PERCENT FOR TAKEOFF. ABORTED TAKEOFF. REMOVED AND REPLACED RIGHT SIDE SPOILERONS (BOTH) INBOARD PCU'S PER MM 27-62-01. LEAK AND OPS CHECK GOOD. MDC & SECU FLAGGED BOTH PCU'S ON TROUBLESHOOTING. AFTER PCU CHANGE, RECEIVED FLT SPOILER AND GROUND SPOILER FAULTS AND SECU NR 2 WOULD NOT RESET. REMOVED AND REPLACED NR 2 SECU PER MM 27-61-05. SYSTEM OPS CHECK GOOD. ALL SPOILER/SPOILERONS WORK PER MM. I/B PCU P/N: 27000-7, S/N OFF: 5660, O/B PCU P/N: 27000-7, S/N OFF: 5656.

Part: FLAP — BIRD STRIKE (RT WING) · airframe 427 hrs · 319 cycles

RIGHT OUTBOARD FLAP DAMAGED BY BIRD STRIKE. REMOVED AND REPLACED RIGHT WING OUTBOARD FLAP ASSEMBLY IAW 27-53-00. OPS CHECK GOOD.