N956SW

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 49,470 hrs · 42,631 cycles

AFTER EDDY CURRENT INSPECTION OF THE WINDWSHIELD CENTER POST , NR 8 ATTACH STRUCTURE CRACKS WERE FOUND IN LOWER PART. R & R WINDWSHIELD CENTER POST NR 8 ATTACH STRUCTURE IAW 00 SRM 51-24-16, SRM 51-42-21, IPC 53-11-19, PAGE 6.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 49,470 hrs · 42,631 cycles

AFT FLOOR SUPPORT, RBL 9, BTWN BS 559 +64 - 559 + 80 CORRODED. R & R THE FLOOR SUPPORT IAW SRM 51-42-21, NO FURTHER ACTION IS REQUIRED, JOB COMPLETED

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 49,470 hrs · 42,631 cycles

FWD CABIN- UNDER FLOOR FRAME FS 333.00 HAS CORROSION BETWEEN STRG 23L TO 23R. REMOVED AND REPLACED FWD CABIN- UNDER FLOOR FRAME FS 333.00 BETWEEN STRG 18LH TO 23RH IAW SRM 51-42-06, SRM 51-42-21.

Part: HYDRAULIC SYSTEM — LOW PRESSURE (ZONE 100) · airframe 49,294 hrs · 42,434 cycles

HYD 3 LO PRESS AND GEAR DISAGREE. DID MANUAL GEAR EXTENSION AND HYD 3 QRH (FLIGHT 5539 - FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS

Part: PUMP — FAULTED (ZONE 100) · airframe 49,298 hrs · 42,441 cycles

HYD 3 LO PRESS AND GEAR DISAGREE. DID MANUAL GEAR EXTENSION AND HYD 3 QRH (FLIGHT 5539 - FILED CLOSED)FOUND HYDRAULIC PUMP 3A CRACKED, REMOVED AND REPLACED HYDRAULIC PUMP 3A WITH A SERVICEABLE UNIT IN REFERENCE TO AMM 29-12-03, NO LEAKS NOTED. PLEASE REFERENCE AML 1592885 PLEASE REFERENCE AML 1592895

Part: UPLOCK HOOK — FOD (ZONE 700) · airframe 49,218 hrs · 42,321 cycles

GEAR DISAGREE WARNING ON GEAR RETRACTION AFTER TAKEOFF, LEFT MAIN INDICATING RED. WENT AWAY WITH QRH PROCEDURE, GEAR REMAINED DOWN AND LOCKED ON LANDING AT SFO. (FLIGHT 5951 - FILED CLOSED)REFERENCED FAULT ISOLATION MANUAL 32-60-07, UPON TROUBLESHOOTING FOUND FAULT CODE S20 LGUPLK STORED IN PSEU. CLEANED DEBRIS FROM UPLOCK HOOK ASSEMBLY PROX SENSOR TARGET IN REFERENCE TO AMM 32-61-05. NO OTHER DEFECTS NOTED IN LANDING GEAR RETRACTION SYSTEM. RESTORED AIRCRAFT TO NORMAL CONFIGURATION, SYSTEM OPS CHECKS GOOD.

Part: STEERING SYS — INOPERATIVE (NLG) · airframe 48,765 hrs · 41,817 cycles

CAUTION STEERING INOP ON TAKE OFF CREW REPORTED GEAR UP AT APPROX 50 FT AFTER T/O. INTERROGATED MDC FAULT HISTORY. BITS 20, 25, AND 26 SET TO 1. PER CRJ 200 FIM 32-50-01 FIGURE 103 NOTE 3: "STEERING INOP (C) NUISANCE MESSAGE ON TAKE-OFF: WHEN THE AIRCRAFT TAKE-OFF, THE NWS REMAINS ACTIVE FOR APPROXIMATELY 4 SECONDS AFTER THE NOSE WHEEL WEIGHT-ON-WHEELS (WOW) BIT FROM THE PSEU TRANSITIONS TO 0 (DO17 AND DO37). THIS IS REQUIRED TO KEEP THE STEERING ACTIVE IF THE NOSE GEAR MAKES A REBOUND DURING TAKE-OFF. IF THE LANDING GEAR CONTROL HANDLE IS SELECTEDT O THE RETRACT POSITION DURING THIS TRANSITION PERIOD, THE HYDRAULIC SUPPLY PRESSURE TO THE NWS SYSTEM IS REMOVED. THE STEERING PRESSURE SWITCH (PS1) WILL SENSE THE LOW PRESSURE CONDITION AND THE ECU WILL POST A STEERING INOP (C) MESSAGE TO INDICATE THAT THE NWS IS UNAVAILABLE . WHILE THE FAULT IS SET, THE NWS ECU MAINTENACE DISPLAY CODE WILL DISPLAY FAULT CODE "--, 5, 6" AND THE MDC FAULT HISTORY WILL INDICATE ONLY BIT 20, 25 AND 26 AS BEING SET TO 1 ON STEER-BY-WIRE LABEL 350"TAXI'D AIRCRAFT

Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 48,369 hrs · 41,387 cycles

FO SIDE WINDSHIELD HAS VERTICAL CRACK ALONG CENTER POST. (FLIGHT 4752 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28954710 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE CAMP CP28955885 FOR THE REMOVAL OF THE FO'S WINDSHIELD.INSTALLED FO SIDE WINDSHIELD IN REFERENCE TO 56-11-01 .. OPERATIONAL AND LEAK CHECK GOOD AT THIS TIME COMPLIED WITH TASK CARD 56-220-1000-SKY. "

Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 48,358 hrs · 41,376 cycles

FO SIDE WINDSHIELD HAS VERTICAL CRACK ALONG CENTER POST. (FLIGHT 4752 - FILED OPEN) PLEASE REFERENCE AML 1445552

Part: PRESSURE DECK — OUT OF LIMITS (ZONE 200) · airframe 48,362 hrs · 41,379 cycles

RH PRESSURE FLOOR SILL FS449.85 BLEND OUT IS BEYOND LIMITS OF GENERIC REO 601R-53-41-666 REV "C". (FILED CLOSED) PERFORMED REPAIR OF RH PRESSURE FLOOR SILL FS449.85 WITH REFERENCE TO REO 601R-53-41-3258 REV "--" DATED 2024-09-11. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT. SEE CHILD CAMP FOR EDDY CURRENT INSPECTION. SEE CP28799029 FOR LEAK CHECK.

Part: FLOOR SUPPORT — OUT OF LIMITS (ZONE 100) · airframe 48,323 hrs · 41,335 cycles

RH PRESSURE FLOOR SILL FS449.85 BLEND OUT IS BEYOND LIMITS OF GENERIC REO 601R-53-41-666 REV "C". (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS

Part: HINGE PIN — CORRODED (ZONE 200) · airframe 48,329 hrs · 41,343 cycles

CORROSION FOUND UNDER PANEL 141AL ON THE UPPER SURFACE UNDER THE HINGE PIN, VISIBLE WITH THE DOOR CLOSED. (FILED CLOSED) BLENDED DAMAGED AREA UNDER PANEL 141AL ON THE UPPER SURFACE UNDER THE HINGE PIN ON FUSELAGE SKIN WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE TO NDTM PART 4 51-00-001 AND FOUND TO BE STRUCTURALLY ACCEPTABLE REFERENCE REO 601R-53-21-3701 REV "--" DATED 2024-09-03. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND NDTM PART 6 53-00-096 WITH NO CRACKS FOUND. COMPLIED WITH REO 601R-53-21-3701 REV "--" DATED 2024-09-03. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT. REFERENCE CP 28754097 FOR REPAIR OF LOWER FWD OUTER PAX DOOR SKIN CORNER REPAIR.

Part: HINGE PIN — CORRODED (ZONE 200) · airframe 48,329 hrs · 41,343 cycles

CORROSION FOUND UNDER PANEL 141BL ON THE UPPER SURFACE UNDER THE HINGE PIN, VISIBLE WITH THE DOOR CLOSED. (FILED CLOSED) BLENDED DAMAGED AREA UNDER PANEL 141BL ON THE UPPER SURFACE UNDER THE HINGE PIN ON FUSELAGE SKIN WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE TO NDTM PART 4 51-00-001 AND FOUND TO BE STRUCTURALLY ACCEPTABLE REFERENCE REO 601R-53-21-3701 REV "--" DATED 2024-09-03. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND NDTM PART 6 53-00-096 WITH NO CRACKS FOUND. COMPLIED WITH REO 601R-53-21-3701 REV "--" DATED 2024-09-03. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT. REFERENCE CP 28754103 FOR REPAIR OF LOWER AFT OUTER PAX DOOR SKIN CORNER REPAIR.

Part: TRACK — DAMAGED (ZONE 800) · airframe 48,329 hrs · 41,343 cycles

FORWARD AND AFT CARGO DOOR TRACKS DAMAGED ON THE OUTSIDE OF TRACK AT THE BOTTOM WHERE CARGO DOOR PINS HAVE COME INTO CONTACT (FILED CLOSED) REMOVED AND REPLACED AFT CARGO DOOR TRACK WITH REFERENCE TO SRM 51-42-06 AND SRM 51-42-13. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. SEE CHILD CAMPS FOR LEAK CHECK (CP 28784851) AND REPLACEMENT OF FWD CARGO DOOR TRACK (CP 28739309).

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 48,329 hrs · 41,343 cycles

FOUND CORROSION ON SEVERAL AREAS OF THE LH PRESSURE FLOOR SILL. FS 409.00+128 , FS424.00 , FS439.00 , FS473.15 , 494.00 , FS513.00 , 548.00. (FILED CLOSED) BLENDED CORROSION ON THE LH PRESSURE FLOOR SILL FS 409.00+128 , FS424.00 , FS439.00 , FS473.15 , 494.00 , FS513.00 , 548.00 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE TO NDTM PART 4 51-00-001 AND FOUND TO BE ACCEPTABLE PER REO 601R-53-41-3249 REV "--" DATED 2024-08-29. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND NDTM PART 6 53-00-096 WITH NO CRACKS FOUND. COMPLIED WITH REO 601R-53-41-3249 REV "--" DATED 2024-08-29. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT. REFERNCE CHILD CAMP FOR LEAK CHECK.

Part: PRESSURE BLKHD — DAMAGED (ZONE 100) · airframe 48,329 hrs · 41,343 cycles

REAR PRESSURE BULKHEAD FORWARD FACE HAS 5 DAMAGED FASTENERS, 11 GOUGES AND ONE SCRATCH ABOUT 4 INCHES LONG (FILED CLOSED) COMPLIED WITH REO 601R-53-61-8215 DATED: 2024-08-22 REV €“ FOR THE BLENDED GOUGES ON FS 621.00 BULKHEAD AND FASTENER REPLACEMENT TO FS 621.00 BULKHEAD. REFERENCE TABLE #1 ON SHEET 4 FOR THE REWORKED LOCATIONS AND FASTENER REPLACEMENT ON THE FS 621 BULKHEAD. COMPLIED WITH TASK CARD 51-900-1003-SKY AND COMPLETED MAJOR REPAIR FORM M-337. NO DEFECTS NOTED FROM NDT.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 48,329 hrs · 41,343 cycles

FOUND CORROSION ON SEVERAL AREAS OF THE RH PRESSURE FLOOR SILL FS 424.00 , FS449.85 , FS473.15 , FS484.00 , FS513.00 , FS526.00 (FILED CLOSED) BLENDED CORROSION ON THE RH PRESSURE FLOOR SILL FS 424.00 , FS449.85 , FS473.15 , FS484.00 , FS513.00 , FS526.00 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE TO NDTM PART 4 51-00-001 AND FOUND TO BE ACCEPTABLE PER REO 601R-53-41-3249 REV "--" DATED 2024-08-29 WITH EXCEPTION OF FS 449.85. SEE CHILD CAMP FOR CONTINUATION OF REPAIR TO RH PRESSURE FLOOR SILL AT FS449.85. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND NDTM PART 6 53-00-096 WITH NO CRACKS FOUND. COMPLIED WITH REO 601R-53-41-3249 REV "--" DATED 2024-08-29. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT. REFERENCE CHILD CAMP FOR LEAK CHECK.

Part: ANGLE — CORRODED (ZONE 800) · airframe 48,329 hrs · 41,343 cycles

CORROSION FOUND IN MULTIPLE SPOTS ON THE PASSENGER DOOR ENTRANCE ANGLE JUST ABOVE STINGER 18L (FILED CLOSED) REMOVED AND REPLACED PASSENGER DOOR ENTRANCE ANGLE JUST ABOVE STR 18L WITH REFERENCE TO SRM 51-42-06 AND SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT.

Part: WIRE — LOOSE (OVERHEAT LOOP B) · airframe 47,791 hrs · 40,767 cycles

L JET OVHT FAIL CAUTION MESSAGE INTERMITTENT. RAN QRH AND IT DID NOT RETURN UNTIL WE WERE PULLING INTO THE GATE. ONLY APPEARED FOR A COUPLE SECONDS EACH TIME. (FLIGHT 5253 FILED CLOSED)INSPECTED LH JET PIPE DETECTION SYSTEM IN REFERENCE TO AMM 26-11-04. WHILE INSPECTING LH JET PIPE SENSING ELEMENT CONNECTORS AND WIRING, FOUND A WIRING CONNECTION FROM LOOP B TO BE LOOSE. RESECURED LOOSE SENSING ELEMENT WIRE CONNECTION AND PERFORMED OPERATIONAL TEST OF LH ENGINE JET PIPE FIRE DETECTION SYSTEM IN REFERENCE TO AMM 26-11-00. OPS TEST GOOD AT THIS TIME. AIRCRAFT OK FOR SERVICE.

Part: NONE — FLUCTUATES · airframe 45,479 hrs · 38,479 cycles

D: THIS IS AN **ODI EVENT** - UPPER MGMT /SMOD APPROVAL REQ'D TO RTS THIS A/C AFTER CAMPS COMPLETE / C: MCI / SEE A/C MX LOG'S 956358 & 955518 (FLIGHT 5123 - FILED CLOSED) DID OPERATIONAL CHECK OF THE STAB-TRIM SYSTEM REFERENCING THE APPLICABLE STEPS IN AMM 27-40-00. COULD NOT DUPLICATE THE DISCREPANCY. TROUBLESHOT PER FIM 27-40-00. AFTER DOING SELF TEST OF THE HSTCU FOUND THE CHANNEL B FLAGGING IN THE MDC. REMOVED AND REPLACE THE HSTCU REFERENCING THE APPLICABLE STEPS IN AMM 27-41-00. OPS CHECK GOOD AT THIS TIME. NO FURTHER MESSAGE SHOWN AT THIS TIME. COMPLIED WITH CATII RETURN TO SERVICE TASK CARD 34-220-1021-SKY.

Part: STRUT — UNDERSERVICED (NLG) · airframe 43,482 hrs · 36,698 cycles

GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF WITH NOSE DOOR OPEN WARNING MESSAGE. RETURNED TO FIELD (FLIGHT 1395 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22837592 WITH THE FOLLOWING CORRECTIVE ACTION: "JACKED THE AIRCRAFT OFF THE GROUND AND FOUND THE NOSE STRUT NOT EXTENDING. SUSPECT THAT THE STRUT WAS NOT PROPERLY SERVICED. PERFORMED A FULL NOSE STRUT SERVICE PER TASK CARD 12-710-002. JACKED THE AIRCRAFT AGAIN AND THE NOSE STRUT FULLY EXTENTED 14.5". PERFORMED A FULL GEAR SWING PER REF AMM 32-33-00. OPS CHECK GOOD."

Part: BRACKET — DAMAGED (HORIZONTAL STAB) · airframe 43,481 hrs · 36,697 cycles

RH LOWER HSTA MOTOR CONTROL UNIT MOUNT BRACKET HAS MOUNTING HOLE RIPPED OUT. (C-CHECK RO 5/20/2021) REMOVED AND REPLACED NEW LOWER HORIZONTAL STABILIZER MOTOR CONTROL UNIT MOUNT BRACKET ON RIGHTHAND SIDE IAW CRJ 200 SRM 51-42-06 AND DWG 601R92303 REV-A. (SEE CONTINUATION FOR FURTHER DETAILS). COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: CHANNEL — CRACKED (RT WING) · airframe 43,481 hrs · 36,697 cycles

WS RH 53.60 CHANNEL OUTBRD SIDE UPPER INBRD CORNER IS CRACKED. (C-CHECK RO 5/20/2021) REMOVED THE CRACKED OTBD SUPPORT CHANNEL AT RH WS.53.60 AND INSTALLED A NEW SUPPORT CHANNEL REF DWG #601R10203 REV -G, CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21, AND CRJ 200 SRM 51-45-00. COMPLIED TASK CARD 51-900-1003-SKY. SEE CONTINUATION FOR FURTHER DETAILS.

Part: PLATE — CHAFED (BS 319 S10R) · airframe 43,481 hrs · 36,697 cycles

FS 319 RH STRG RH 10 GUSSET PLATE HAS CHAFING DAMAGE UPPER SIDE AS MARKED (C-CHECK RO 5/20/2021) FS 319 RH STRG RH 10 GUSSET PLATE - REMOVED AND REPLACED WITH NEW - REF CRJ200 SRM 51-42-21, DRAWING # 601R38303 REV AR. / .COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: ANGLE — CRACKED (BS 280 LBL 9) · airframe 43,481 hrs · 36,697 cycles

CRACKED CLIP AT FS.280 ON LBL9 INBD SIDE (MARKED) (C-CHECK RO 5/20/2021) REMOVED AND INSTALLED A NEW FS.280 CLIP ON LBL9 INBD SIDE REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21 AND DWG # 601R31113 REV -M. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: ROLLER — CRACKED (BS 484 RBL 36) · airframe 43,481 hrs · 36,697 cycles

SUSPECTED CRACK ON ROLLER FAIRLEAD BRACKET ASSY ATTACHED TO RBL36.00 FLOOR BEAM AT FS 484.00 (MARKED) (C-CHECK RO 5/20/2021) REMOVED DEFECT AND INSTALLED REPAIR MATERIAL. REF REO 601R-53-41-059 REV -C DATED 2020-03-11. PRESSURE CHECKS ARE SATISFACTORY. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: FLOORBEAM — CRACKED (BS 484 LBL 9) · airframe 43,481 hrs · 36,697 cycles

SUSPECTED CRACK ON LBL9.00 PRESSURE FLOOR-SUPPORT BEAM TIE-CLIP TO CROSS-MEMBER AT FS484.00 (MARKED) (C-CHECK RO 5/20/2021) REMOVED AND INSTALLED NEW CLIP AT FS484 ON LBL9 REF DWG 601R31171 REV-B AND REO 601R-53-41-2908 REV--, DATED 2021-04-23. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: SPLICE — BROKEN (PAX DOOR) · airframe 43,481 hrs · 36,697 cycles

PAX DOOR SPLICE 131MB BROKEN (C-CHECK RO 5/20/2021) REMOVED AND REPLACED PAX DOOR SPLICE SP131MB REF ESPM 30-17-10. OPS TEST GOOD

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 43,481 hrs · 36,697 cycles

RH WINDSHIELD SIDE POST LOWER SUPPORT STRUCTURE CRACKED (MARKED-OUT OF SCOPE) (C-CHECK RO 5/20/2021) REMOVED AND REPLACED ANGLE REF CRJ200 SRM 51-42-06 & DWG 601R34032 REV -V DATED 2009-04-29. PRESSURE CHECK GOOD REF CRJ200 AMM 21-32-00-863-801. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR WORK PERFORMED

Part: FLOORBEAM — CRACKED (BS 484 LBL 36) · airframe 43,481 hrs · 36,697 cycles

SUSPECTED CRACK ON LBL36.00 FLOOR BEAM TO FLIGHT CONTROL CABLE ROLLER FAIRLEAD BRACKET ASSY CLIP AT FS484.00 (MARKED) (C-CHECK RO 5/20/2021) REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE AT LBL36.00 FS484.00 REF CRJ200 SRM 51-42-21 AND REO 601R-53-41-059 REV-C DATED: 2020-03-11 COMPLIED WITH TASK CARD 51-900-1003-SKY. PRESSURE CHECK GOOD.

Part: FLOORBEAM — CRACKED (BS 484 RBL 27) · airframe 43,481 hrs · 36,697 cycles

SUSPECTED CRACK ON RBL27.00 PRESSURE FLOOR-SUPPORT BEAM CLIP ATTACHED TO ROLLER FAIRLEAD BRACKET ASSY AT FS 484.00 (MARKED) (C-CHECK RO 5/20/2021) REMOVED CRACKED CLIP AND INSTALLED NEW CLIP REF PREVIOUSLY INCORPERATED REO 601R-53-41-059 REV-B DATED 2009-09-16 / RESTORED FINISH AT THE NEW BRACKET AREA RBL27 FS484.00 REF CRJ200 SRM 51-25-16 / . COMPLIED WITH TASK CARD 51-900-1003-SKY .SEE CONTINUE CARD FOR WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (BS 409-559 RBL9) · airframe 43,481 hrs · 36,697 cycles

RBL9.00 PRESSURE FLOOR-SUPPORT BEAM CHANNEL BETWEEN FS 409.00+128 TO FS 559.00 HAS APPROX. 71 CORROSION LOCATIONS (MARKED WITH GREASE PENCIL). (C-CHECK RO 5/20/2021) REPAIRED PRESSURE FLOOR SUPPORT BEAM CHANNEL BETWEEN FS409.00+118 TO FS559.00+10 RBL9 IAW REO 601R-53-41-2904 REV -- DATE 2021-05-05 STEPS. 1-16 ( SEE CONTINUATION FOR FURTHER DETAILS). COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: SKIN — CORRODED (PAX DOOR) · airframe 43,481 hrs · 36,697 cycles

AFTER REMOVAL OF PAX DOOR INNER SKIN FOUND SERVRE CORROSION ON INTERCOSTAL DD3 (C-CHECK RO 5/20/2021) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD3 REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21, AND DWG 601R31702 REV-N. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 43,481 hrs · 36,697 cycles

LH WINDSHIELD SIDE POST LOWER SUPPORT STRUCTURE CRACKED (MARKED-OUT OF SCOPE) (C-CHECK RO 5/20/2021) REPLACED L/H WINDSHIELD SIDE POST LWR ANGLE. REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-11, & DWG 601R34032 REV V. PRESSURE CHECK WAS SATISFACTORY. / SKYCARD 51-900-1003-SKY COMPLIED WITH

Part: FLOORBEAM — DENTED (BS 461 RBL 27) · airframe 43,481 hrs · 36,697 cycles

RBL 27.00 PRESSURE FLOOR-SUPPORT BEAM CHANNEL HAS DENT LOCATED AT APPROX. FS 461.00 (MARKED). (C-CHECK RO 5/20/2021) REPAIRED THE RBL 27.00 PRESSURE FLOOR-SUPPORT BEAM CHANNEL AT APPROX. FS 461.00 WITH REO 601R-53-41-2921 REV -- DATED 2021-05-17. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: ANGLE — CORRODED (PAX DOOR SILL) · airframe 43,481 hrs · 36,697 cycles

* PAX DOOR UPPER SILL ANGLE IS CORRODED AT THE FORWARD END. APPROX FS 310.00. (C-CHECK RO 5/20/2021) REMOVED AND REPLACED WITH NEW - BRACKET ATTACHED TO THE PAX DOOR UPPER SILL ANGLE AT/ABOUT FS310.00. REF CRJ200 SRM 51-42-06. BOMBARDIER DWG # 601R31527 REV AM. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: DOOR FRAME — CRACKED (ESCAPE HATCH) · airframe 43,481 hrs · 36,697 cycles

* CREW ESCAPE HATRCH SURROUND, ( STRUCTURAL ) DIAPHRAM AT APPROX. FS270.10 AND LBL 11.160 HAS POSSIBLE CRACK. MARKED. (C-CHECK RO 5/20/2021) REMOVED AND REPLACED CREW ESCAPE HATCH SURROUND STRUCTURAL DIAPHRAM REF CRJ200 SRM 51-42-06, DWG# 601R33048 REV- T. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: ANCHOR FITTING — CORRODED (PAX DOOR FRAME) · airframe 43,481 hrs · 36,697 cycles

* PAX DOOR FORWARD ANCHOR FITTING HARDWARE IS CORRODED. (C-CHECK RO 5/20/2021) REMOVED AND INSTALLED NEW HARDWARE ON PAX DOOR FORWARD ANCHOR FITTING. REF - CRJ 200 AMM 52-11-17-000-803 AND CRJ 200 AMM 52-11-17-400-803. / TUC8619 DUE: 10/31/2021 / 6 EACH NEW SCREWS, 4 EACH NEW BOLTS, 14 EACH NEW WASHERS, 10 EACH NEW NUTS.

Part: DOOR SILL — CORRODED (PAX DOORWAY) · airframe 43,481 hrs · 36,697 cycles

* PAX DOOR SILL FORWARD AND AFT HANDRAIL CUPS ( CLEATS ) HAVE CORROSION. (C-CHECK RO 5/20/2021) REMOVED CORROSION ON THE PAX DOOR SILL FWD AND AFT HANDRAIL CUPS REF CRJ 200 SRM 51-21-06 FOUND TO BE OUT OF LIMITS. REPLACED THE FWD AND AFT PAX DOOR SILL HANDRAIL CUPS WITH NEW SERVICEABLE CUPS REF CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-13.

Part: ANGLE — CORRODED (SERVCE DOOR SILL) · airframe 43,481 hrs · 36,697 cycles

* GALLEY SERVICE DOOR LOWER SILL ANGLE IS CORRDED AROUND FORWARD STOP FITTING. (C-CHECK RO 5/20/2021) REPLACED GALLEY SERVICE DOOR LOWER SILL ANGLE PN# 601R38303-253. REF BOMBARDIER DWG 601R38303 REV-AR, AND DWG 601R38301 REV-AD, CRJ-200 SRM 51-42-06, SRM 51-42-13, SRM 51-42-21, COMPLIED WITH SKY-51-900-1003.

Part: BRACKET — BROKEN (BS 621 BULKHEAD) · airframe 43,481 hrs · 36,697 cycles

FS.621 BULKHEAD HAS 3EA BROKEN BRACKETS @ APPROX. STRG.13-15 (MARKED) (C-CHECK RO 5/20/2021) REMOVED AND INSTALLED 3 NEW BRACKETS (PN:601R45156-75) ON THE FS.621 BULKHEAD AT APPROX STRG 13R-15R REF CRJ 200 SRM 51-42-06. LEAK CHECK GOOD.

Part: STIFFENER — CRACKED (PRESS BULKHEAD) · airframe 43,481 hrs · 36,697 cycles

FS409.00+128 PRESSURE BULKHEAD LBL 27 SUPPORT POST CRACKED AT BOTTOM INNER (MARKED - OUT OF SCOPE) (C-CHECK RO 5/20/2021) REMOVED AND INSTALLED A NEW FS.409+128 LBL 27 SUPPORT POST REF REO 601R-53-41-2909 REV -- DATED 2021-05-05 AND DWG #601R32208 REV -T. COMPLIED WITH ALL APPLICABLE STEPS OF REO 601R-53-41-2909 REV -- DATED 2021-05-05. COMPLIED WITH TASK CARD 51-900-1003-SKY. PRESSURE LEAK CHECKS GOOD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: HINGE — GOUGED (PAX DOOR) · airframe 43,481 hrs · 36,697 cycles

PAX DOOR HINGE ON FUSELAGE SIDE HAS SEVERAL WORN/EGG SHAPED LUG HOLES, ON THE FWD/AFT ENDS AND FLAT 27 IS GOUGED (MARKED) (C-CHECK RO 5/20/2021) REPLACED PAX DOOR HINGE (FUSELAGE SIDE) REF CRJ200 SRM 53-21-23 AND REO 601R-53-21-656 REV -A DATED 2017-03-06. PRESSURE CHECK GOOD REF CRJ200 AMM 21-32-00-863-801. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: STOP FITTING — CORRODED (CARGO DOOR FRAME) · airframe 43,481 hrs · 36,697 cycles

*CARGO DOOR SURROUND BOTTOM FWD STOP FITTING CHAFFED/CORRODED (MARKED) (C-CHECK RO 5/20/2021) REPLACED CARGO DOOR SURROUND LWR FWD STOP FITTING. REF CRJ200 AMM 52-31-00-820-801. ALL CHECKS GOOD

Part: STOP FITTING — CHAFED (CARGO DOORWAY) · airframe 43,481 hrs · 36,697 cycles

*CARGO DOOR SURROUND AFT CROTCH STOP FITTING CHAFFED/WORN (MARKED) (C-CHECK RO 5/20/2021) BLENDED CARGO DOOR SURROUND AFT CROTCH STOP FITTING REF CRJ200 SRM 51-12-00. FOUND OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-53-61-7637 REV-- DATED 2021-04-20. OPS TEST GOOD.

Part: FLOORBEAM — CRACKED (BS 280 RBL 9) · airframe 43,481 hrs · 36,697 cycles

FS280.00 FLOOR MEMBER IS CRACKED AT APPROX RBL9 (C-CHECK RO 5/20/2021) REMOVED AND REPLACED NEW FLOOR ANGLE PN 600-34017-351S REF CRJ200 SRM 51-41-02, SRM 51-42-06 AND SRM 41-42-21

Part: STOP FITTING — CHAFED (CARGO DOORWAY) · airframe 43,481 hrs · 36,697 cycles

*CARGO DOOR SURROUND TOP FWD STOP FITTING CHAFFED/WORN (MARKED) (C-CHECK RO 5/20/2021) REPLACED CARGO DOOR TOP FORWARD FITTING REF CRJ 200 SRM 51-41-02 TUC 4200 CAL DUE 9- 30 -2021

Part: STOP FITTING — CORRODED (CARGO DOOR FRAME) · airframe 43,481 hrs · 36,697 cycles

*CARGO DOOR BOTTOM SURROUND AFT STOP FITTING CHAFFED/CORRODED (MARKED) (C-CHECK RO 5/20/2021) REPLACED CARGO DOOR SURROUND LWR AFT STOP FITTING. REF CRJ200 AMM 52-31-00-820-801. PRESSURE CHECK GOOD.

Part: STOP FITTING — CHAFED (CARGO DOORWAY) · airframe 43,481 hrs · 36,697 cycles

*CARGO DOOR SURROUND FWD UPPER STOP FITTING CHAFFED/WORN (MARKED) (C-CHECK RO 5/20/2021) REMOVED AND REPLACED CARGO DOOR SURROUND FWD UPPER STOP FITTING IAW REO 601R-53-61-7637 REV-- DATED 2021-04-20

Part: STOP FITTING — CHAFED (CARGO DOOR FRAME) · airframe 43,481 hrs · 36,697 cycles

*CARGO DOOR SURROUND FWD CROTCH STOP FITTING CHAFFED/WORN (MARKED) (C-CHECK RO 5/20/2021) REMOVED AND REPLACED CARGO DOOR SURROUND FWD CROTCH STOP FITTING IAW REO 601R-53-61-7637 REV-- DATED 2021-04-20, & DWG 600-35072 REV -C, OPS TEST GOOD AT THIS TIME.

Part: STOP FITTING — CHAFED (CARGO DOORWAY) · airframe 43,481 hrs · 36,697 cycles

*CARGO DOOR SURROUND TOP AFT STOP FITTING CHAFFED/WORN (MARKED) (C-CHECK RO 5/20/2021) REPLACED CARGO DOOR TOP AFT FITTING REF CRJ 200 SRM 51-41-02 TUC 4200 CAL DUE 9 -30 -2021

Part: STOP FITTING — CHAFED (CARGO DOORWAY) · airframe 43,481 hrs · 36,697 cycles

*CARGO DOOR SURROUND FWD LWR STOP FITTING CHAFFED/WORN (MARKED) (C-CHECK RO 5/20/2021) REMOVED AND REPLACED CARGO DOOR SURROUND FWD LWR STOP FITTING IAW REO 601R-53-61-7637 REV-- DATED 2021-04-20

Part: ATTACH ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 43,481 hrs · 36,697 cycles

* FS 621 BULKHEAD AFT RIGHT SIDE ATTACHING CLIP AT APROX. STGR 15R IS CRACKED. (C-CHECK RO 5/20/2021) INSTALLED NEW BULKHEAD RH SIDE ATTACHING CLIP AT APPROX 15R, RESTORED FINISH TO ATTAHING CLIP. REF: CRJ200 SRM 51-42-06 AND DRAWING #601-35012 REV, -D. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: STRINGER CLIP — CRACKED (BS 280 S3L) · airframe 43,481 hrs · 36,697 cycles

LH FS 280 LH STR 3 CLIPS UPPER DOOR SILL ATTACHED CRACKED (C-CHECK RO 5/20/2021) REMOVED AND INSTALLED NEW CLIPS AT FS280 STGR 3L REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21, AND DWG 600-31057 REV-P. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: SEAT TRACK — CORRODED (BS 364-409 LBL 9) · airframe 43,481 hrs · 36,697 cycles

*MULTIPLE AREAS OF CORROSION ON SEAT TRACK LBL 9 F/S 364 TO 409 (C-CHECK RO 5/20/2021) REPLACED LBL9 SEAT TRACK BETWEEN FS364.00 & FS409.00. REF CRJ200 AMM 53-01-11-000-802 & CRJ200 AMM 53-01-11-400-802.

Part: STRAP — CORRODED (BS 559) · airframe 43,481 hrs · 36,697 cycles

LH FS 559 STRAP UNDER FLOOR PANEL LBL 27 TO 40 APPROX HAS CORROSION AS FLAGGED. (C-CHECK RO 5/20/2021) REMOVED AND REPLACED STRAP P/N 601R31025-29 REF CRJ 200 SRM 51-42-06 , 51-42-15 AND DRAWING 601R31025 REV N. SEE CONTINUATION CARD FOR DETAILS. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: SEAT TRACK — CORRODED (BS 409-559 RBL 9) · airframe 43,481 hrs · 36,697 cycles

* FLOOR SEAT TRACK RBL 9.0, BETWEEN FS 409.00 + 128 AND APPROX. FS 559.00 + 4 CORRODED SEVERAL PLACES. (C-CHECK RO 5/20/2021) REMOVED CORRODED SEAT TRACK REF CRJ200 AMM 53-01-11-000-802 / INSTALLED NEW SEAT TRACK AT RBL9 FROM FS409+128 TO FS559+4 REF CRJ200 AMM 53-01-11-400-802 / TORQUE WRENCH #TUC5659 CAL DUE:09-FEB-2022

Part: SEAT TRACK — CORRODED (BS 559 LBL 9) · airframe 43,481 hrs · 36,697 cycles

* MULTIPLE AREAS OF CORROSION ON SEAT TRACK 9L FROM FS 559 TO559+80 (C-CHECK RO 5/20/2021) REMOVED AND REPLACED RBL9 SEAT TRACK FROM FS559.00 TO FS559.00+80 REF CRJ200 AMM 53-01-11-000-802 AND AMM 53-01-11-400-802. SEE CONTINUE CARD FOR WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (PRESSURE DECK) · airframe 43,481 hrs · 36,697 cycles

RH PRESSURE FLOOR SILL HAS CORROSION FS 409+128 TO 559 AS MARKED (C-CHECK RO 5/20/2021) BLENDED CORROSION ON THE RH PRESSURE FLOOR SILL AT FS.409+128 TO FS.559 AND FOUND TO BE WITHIN LIMITS REF REO 601R-53-41-666 REV -C DATED 2012-11-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUATION FOR FURTHER DETAILS.

Part: SEAT TRACK — CORRODED (BS 409-559 LBL9) · airframe 43,481 hrs · 36,697 cycles

* FLOOR SEAT TRACK LBL 9.0, BETWEEN FS 409.00 + 128 AND APPROX. FS 559.00 + 4 CORRODED SEVERAL PLACES. (C-CHECK RO 5/20/2021) REMOVED CORROSION ON THE FLOOR SEAT TRACK ON LBL9 BETWEEN FS.409+128 TO APPROX. FS.559.00. FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 53-21-49. COMPLIED WITH REPACEMENT NEW FLOOR SEAT TRACK RAIL IN PASSENGER COMPARTMENT AT FS409.00+128 - FS559.00 LBL-9 REF CRJ 200 AMM 53-01-1-400-802 STEP 3.B. CALIBRATED TOOL USED TUC4978 CAL DUE DATE 30-JUN-.21.

Part: STRAP — CORRODED (BS 559) · airframe 43,481 hrs · 36,697 cycles

RH FS 559 STRAP UNDER FLOOR PANEL RBL 27 TO 40 APPROX HAS CORROSION AS FLAGGED. (C-CHECK RO 5/20/2021) REMOVED AND INSTALLED NEW STRAP AT FS559 RBL27 TO RBL40 REF DWG 601R31025 REV N, CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-45-00. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: FLOOR SUPPORT — CORRODED (PRESSURE DECK) · airframe 43,481 hrs · 36,697 cycles

LH PRESSURE FLOOR SILL UPPER SURFACE HAS CORROSION FS 409+128 TO 559 AS MARKED. (C-CHECK RO 5/20/2021) BLENDED CORROSION ON THE LH PRESSURE FLOOR SILL UPPER SURFACE AT FS.409+128 TO FS.559 AND FOUND TO BE WITHIN LIMITS REF REO 601R-53-41-666 REV -C DATED 2012-11-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUATION FOR FURTHER DETAILS.

Part: SEAT TRACK — CORRODED (BS 409 RBL 9) · airframe 43,481 hrs · 36,697 cycles

* CABIN FLOOR SEAT TRACK RBL9.00, FS409.00-FS409.00+128 MULTIPLE AREAS OF CORROSION (C-CHECK RO 5/20/2021) REPLACED RBL9 SEAT TRACK BETWEEN FS409.00 AND FS409.00+128. REF CRJ200 AMM 53-01-11-000-802 & CRJ200 AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409 LBL 9) · airframe 43,481 hrs · 36,697 cycles

* CABIN FLOOR SEAT TRACK LBL9.00, FS409.00-FS409.00+128 MULTIPLE AREAS OF CORROSION (C-CHECK RO 5/20/2021) REPLACED LBL9.00 FLOOR SEAT TRACK BETWEEN FS409.00 AND FS409.00+128. REF CRJ-200 AMM 53-01-11-000-802 AND CRJ-200 AMM 53-01-11-400-802. SEE CONTINUATION CARD FOR DETAILS.

Part: PLATE — CHAFED (CARGO DOOR FRAME) · airframe 43,481 hrs · 36,697 cycles

AFT BAGGAGE DOOR CUTOUT - AFT BOTTOM CORNER OF DOOR FRAME - SEALING RADIUS PLATE CHAFED AND DEFORMED FROM IMPACT - AS MARKED (C-CHECK RO 5/20/2021) REMOVED AND REPLACED AFT CARGO DOOR LOWER COMING PN:601R351602-1 REF CRJ200 SRM 51-41-02 AND 51-42-13. SEE CONTINUE CARD FOR WORK PERFORMED. PRESSURE CHECK GOOD.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 43,481 hrs · 36,697 cycles

* FOUND THE LH SIDE SEAT RAIL CORRODED AT APPROX F.S409.00+112- F.S449.85(AREA MARKED) (C-CHECK RO 5/20/2021) REMOVED CORROSION ON L/H SIDE SEAT RAIL APPROX. FS 409.00+112 - 449.85, FOUND TO BE OUT OF LIMITS, INSTALLED NEW FABRICATED LH SIDE SEAT RAIL APRROX FS409+112 TO FS449.85 REF CRJ200 AMM 53-01-11-400-802. SEE CONTINUE CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 43,481 hrs · 36,697 cycles

* FOUND THE LH SIDE FWD SEAT RAIL CORODED AT APPROX F.S409.00.(AREA MARKED) (C-CHECK RO 5/20/2021) REMOVED AND INSTALLED NEW L/H SIDE SEAT TRACK RAIL AT APPROX F.S 409, REF CRJ 200 AMM 53-01-11-000-802 & 53-01-11-944-002. TUC 5659 CAL DUE 28 FEB 2022

Part: SEAT TRACK — CORRODED (BS 439-461) · airframe 43,481 hrs · 36,697 cycles

* FOUND SURFACE COROSSION ON RH AFT SIDE SEAT RAIL AT APPROX F.S439.00- F.S461.00(AREA MARKED) (C-CHECK RO 5/20/2021) REMOVED CORROSION ON RH AFT SIDE SEAT RAIL AT APRROX FS439 TO FS461.00 REF CRJ200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. INSTALLED NEW FABRICATED SEAT TRACK REF CRJ200 AMM 53-01-11-400-802. SEE CONTINUE CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (BS 425-530) · airframe 43,481 hrs · 36,697 cycles

* FOUND MULTIPLE COROSSION SPOT ON RH FWD SIDE SEAT RAIL AT APPROX F.S425.00- -F.S530.00.(AREA MARKED) (C-CHECK RO 5/20/2021) REMOVED CORROSION ON RH SIDE SEAT RAIL AT APPROX FS425.00 TO FS530.00 REF CRJ200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. INSTALLED NEW FABRICATED SEAT TRACK REF CRJ200 AMM 53-01-11-400-802. SEE CONTINUE CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (BS 473-529) · airframe 43,481 hrs · 36,697 cycles

* FOUND THE LH SIDE SEAT RAIL CORODED AT APPROX F.S473.15-F.S529.00(AREA MARKED) (C-CHECK RO 5/20/2021) REMOVED CORROSION ON L/H SIDE SEAT RAIL APPROX. FS473.15 TO FS529.00 REF CRJ200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS, INSTALLED NEW FABRICATED LH SIDE SEAT RAIL APRROX FS473.15 TO FS529.00 REF CRJ200 AMM 53-01-11-400-802. SEE CONTINUE CARD FOR DETAILS.

Part: DOOR FRAME — CORRODED (BS 349- S25L/R) · airframe 43,481 hrs · 36,697 cycles

A BAY DOOR CUTOUT - AFT FACE OF FS 349 CORRODED BTWN STGRS 25L/25R AS MARKED (C-CHECK RO 5/20/2021) REMOVED EXFOLIATED AND INSTALLED NEW LOWER FRAME SECTION OF FS349.00 BETWEEN STGR 25L TO STGR 25R DWG 601R32005 REV-AR AND CRJ200 SRM 51-42-06. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 43,481 hrs · 36,697 cycles

* PAX DOOR INTERCOSTAL BEHIND ACCESS PANEL 832ER IS CORRODED. (C-CHECK RO 5/20/2021) REPLACED PAX DOOR DD4 AFT INTERCOSTAL. REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-13, CRJ200 SRM 51-42-21, & DWG 601R31902 REV Y. PRESSURE LEAK CHECK SATISFACTORY. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 43,481 hrs · 36,697 cycles

* PAX DOOR INTERCOSTAL BEHIND ACCESS PANEL 832BR IS CORRODED. (C-CHECK RO 5/20/2021) REMOVED AND REPLACED PAX DOOR INTERCOSTAL UNDER PANEL 832BR. REF DWG 601R31702 REV N & CRJ200 SRM 51-42-06. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 43,481 hrs · 36,697 cycles

* PAX DOOR INTERCOSTAL DD4 IS CORRODED. (C-CHECK RO 5/20/2021) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD4 REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG 601R31702 REV-N. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: HINGE — CORRODED (LT WING SPOILER) · airframe 43,481 hrs · 36,697 cycles

* LH WING INBOARD GROUND SPOILER OUTBOARD HINGE HARDWARE CORRODED (C-CHECK RO 5/20/2021) INSTALLED NEW HARDWARE ON LH WING INBOARD GROUND SPOILER OUTBOARD HINGE, REF. CRJ200 AMM 27-65-01-400-801, OPS TEST GOOD AT THIS TIME.

Part: HINGE — CORRODED (LT SPOILER) · airframe 43,481 hrs · 36,697 cycles

* LH WING SPOILERON INBOARD & OUTBOARD HINGE HARDWARE & OUTBOARD BOLT KEEPER HARDWARE CORRODED (C-CHECK RO 5/20/2021) ORDERED, RECEIVED, REMOVED, AND REPLACED LH WING SPOILERON INBOARD AND OUTBOARD KEEPER BOLTS AND HINGE NUTS REF CRJ200 AMM 27-64-01-000-801 REF CRJ200 AMM 27-64-01-400-801. OPS TEST GOOD AT THIS TIME.

Part: SKIN — CORRODED (LT AILERON LE) · airframe 43,481 hrs · 36,697 cycles

*L/H AILERON HAS AREA OF CORROSION ON LWR OTBD LEADING EDGE. (C-CHECK RO 5/20/2021) REMOVED AND REPLACED LH AILERON LOWER OUTBOARD LEADING EDGE PANEL REF SRM 51-42-21 AND SRM 51-42-06. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS

Part: HINGE — CORRODED (RT WING SPOILER) · airframe 43,481 hrs · 36,697 cycles

* RH WING FLIGHT SPOILER INBOARD & OUTBOARD HINGE HARDWARE & INBOARD BOLT KEEPER HARDWARE CORRODED (C-CHECK RO 5/20/2021) INSTALLED NEW HARDWARE ON RH WING FLIGHT SPOILER INBOARD AND OUTBOARD HINGES AND INBOARD BOLT KEEPER, REF. CRJ200 AMM 27-64-05-400-801, OPS TEST GOOD AT THIS TIME.

Part: HINGE — CORRODED (LT SPOILER) · airframe 43,481 hrs · 36,697 cycles

* LH WING OUTBOARD GROUND SPOILER INBOARD AND OUTBOARD HINGE HARDWARE CORRODED (C-CHECK RO 5/20/2021) INSTALLED NEW HARDWARE ON LH WING OUTBOARD GROUND SPOILER INBOARD AND OUTBOARD HINGES, REF. CRJ200 AMM 27-65-01-400-801, OPS TEST GOOD AT THIS TIME.

Part: HINGE — CORRODED (RT WING SPOILER) · airframe 43,481 hrs · 36,697 cycles

* RH WING OUTBOARD GROUND SPOILER OUTBOARD HINGE HARDWARE CORRODED (C-CHECK RO 5/20/2021) INSTALLED NEW HARDWARE ON RH WING OUTBOARD GROUND SPOILER OUTBOARD HINGE, REF. CRJ200 AMM 27-65-01-400-801, OPS TEST GOOD AT THIS TIME.

Part: HINGE — CORRODED (RT SPOILERON) · airframe 43,481 hrs · 36,697 cycles

* RH WING SPOILERON INBOARD & OUTBOARD HINGE HARDWARE & BOLT KEEPER HARDWARE CORRODED (C-CHECK RO 5/20/2021) INSTALLED NEW HARDWARE ON RH WING SPOILERON INBOARD AND OUTBOARD HINGES AND BOLT KEEPERS, REF. CRJ200 AMM 27-64-01-400-801, OPS TEST GOOD AT THIS TIME.

Part: HINGE — CORRODED (RT WING SPOILER) · airframe 43,481 hrs · 36,697 cycles

* RH WING INBOARD GROUND SPOILER OUTBOARD HINGE HARDWARE CORRODED (C-CHECK RO 5/20/2021) INSTALLED NEW HARDWARE ON RH WING INBOARD GROUND SPOILER, OUTBOARD HINGE, REF. CRJ200 AMM 27-65-01-400-801, OPS TEST GOOD AT THIS TIME.

Part: HINGE — CORRODED (LT SPOILER) · airframe 43,481 hrs · 36,697 cycles

* LH WING FLIGHT SPOILER INBOARD & OUTBOARD HINGE HARDWARE & BOLT KEEPER HARDWARE CORRODED (C-CHECK RO 5/20/2021) INSTALLED NEW HARDWARE ON LH WING FLIGHT SPOILER INBOARD AND OUTBOARD HINGE AND BOLT KEEPER, REF. CRJ200 AMM 27-64-05-400-801, OPS TEST GOOD AT THIS TIME.

Part: BOLT — CORRODED (RT AILERON HINGE) · airframe 43,481 hrs · 36,697 cycles

*HARDWARE SECURING HINGE BOLT RETAINERS FOR R/H AILERON ARE CORRODED. (ALL THREE HINGE LOCATIONS) (C-CHECK RO 5/20/2021) REMOVED CORRODED HINGE BOLT RETAINERS FOR R/H AILERON AND REPLACED WITH NEW HINGE RETAINER HARDWARE REF CRJ200 AMM 27-15-01-000-801 REF CRJ200 AMM 27-15-01-400-801

Part: BRACKET — CRACKED (RT WING LE) · airframe 43,481 hrs · 36,697 cycles

*ANGLE BRACKET UNDER R/H LEADING EDGE GAP PNL 620ML IS CRACKED. (BRACKET FLAGGED) (C-CHECK RO 5/20/2021) REMOVED AND REPLACED BRACKET REF. CRJ 200 SRM 51-40-11

Part: HANDLE — GOUGED (CARGO DOOR) · airframe 43,481 hrs · 36,697 cycles

CARGO DOOR HANDLE ASSY HAS GOUGE ON FWD LWR FACE OF HANDLE ASSY (MARKED) (C-CHECK RO 5/20/2021) REMOVED AND REPLACED AFT CARGO DOOR HANDLE ASSY REF CRJ200 SRM 51-42-21 AND BOMBARDIER DWG 601R35027 REV Y. PRESSURE LEAK CHECK GOOD REF CRJ200 AMM 21-32-00-863-801. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR WORK PERFORMED.

Part: BRACKET — CRACKED (LT WING LE) · airframe 43,481 hrs · 36,697 cycles

*ANGLE BRACKET UNDER L/H LEADING EDGE GAP PNL 520ML IS CRACKED. (BRACKET FLAGGED) (C-CHECK RO 5/20/2021) REMOVED AND REPLACED BRACKET REF. CRJ 200 SRM 51-40-11

Part: BOLT — CORRODED (RT WING TE FLAP) · airframe 43,481 hrs · 36,697 cycles

* RIGHT HAND WING OUTBOARD FLAP , OUTBOARD FLAP ACTUATOR MOUNT BOLT AND WASHER CORRODED. (C-CHECK RO 5/20/2021) REMOVED AND REPLACED RH OUTBOARD FLAP, OUTBOARD FLAP ACTUATOR MOUNT BOLT AND WASHER. REF: CRJ200 57-21-35-000-801 AND CRJ200 AMM 57-21-35-400-801. TQ WRECH: TUC1260 NEXT CAL DUE: 30-JUN-21

Part: FAIRING — ERODED (HORIZONTAL STAB) · airframe 43,481 hrs · 36,697 cycles

* RIGHT HORIZONTAL STABILIZER TIP FAIRING 343 AR, ERROSION AND DELAMINATION AND / BONDING PLATES CORRODED. (C-CHECK RO 5/20/2021) DRILLED AND COUNTERSUNK ALL HOLES IN NEW STAB TIP PANEL # 343 AR , COMPLIED WITH CRJ-200 SRM 51-74-00

Part: RETAINER — CORRODED (E/E DOOR SEAL) · airframe 43,481 hrs · 36,697 cycles

* AVIONICS COMPARTMENT DOOR SEAL RETAINERS HAVE CORROSION SEVERAL PLACES AROUND PERIMETER OF DOOR. (C-CHECK RO 5/20/2021) REMOVED AND REPLACED 4EA AVIONICS DOOR SEAL RETAINERS WITH NEW RETAINERS. REMOVED AND REPLACED AVONICS DOOR SEAL WITH NEW SEAL. REF: CRJ200 SRM 51-42-06 AND CRJ200 AMM 52-42-07-400-802. LEAK CHECKED GOOD.

Part: REINFORCEMENT — DAMAGED (BS 559) · airframe 43,481 hrs · 36,697 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 5/20/2021) COMPLIED WITH REO 601R-53-41-1116 REV. C DATED 2017/03/09. REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS. COMPLIED WITH TASK CARD 51-900-1003-SKY. PRESSURE CHECK GOOD.

Part: NUT PLATE — DAMAGED (WNG-BDY FAIRING) · airframe 43,481 hrs · 36,697 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA59619-REO 601R-53-31-1111 N956SW MXCODEID52094-PR - WING TO FUSELAGE PANEL 192BB HAS A NUTPLATE AT F.S. 409+96 AND 9 INCHES RIGHT OF CENTERLINE WITH ELONGATED HOLES HOLDING THE NUTPLATE BRACKET TEMPORARY REPAIR FOR ELONGATED HOLE ON FUSELAGE LOWER SKIN DOUBLER AND FRAME AT FS409.00 +96.00 STR 25R - STR 26R.IS ACCEPTABLE FOR 2500 FLIGHT HRS. NEXT C-CHECK. DUE BY TAT 45489.9, PART NUMBER: - , SERIAL NUMBER: 7825, POSITION: (C-CHECK RO 5/20/2021) REPAIRED ELONGATED HOLE AT WING TO FUSELAGE PANEL192BB NUTPLATE AT F.S. 409+96 AND 9 INCHES RIGHT OF CENTERLINE REF. REO 601R-53-31-1195 REV. -- DATED 2021-04-28. COMPLIED WITH TASK CARD 51-900-1003-SKY. PRESSURE CHECK GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,460 hrs · 33,092 cycles

FLOORBEAM FROM APPROX. FS610 TO FS621, LBL27 CORRODED. (C-CHECK) RO: 10/13/2018 REPAIRED FLOORBEAM FROM APPROX. FS610 TO FS621, LBL27 IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,460 hrs · 33,092 cycles

FLOORBEAM CAP FROM APPROX. FS559+112 TO FS569, LBL27 CORRODED. (C-CHECK) RO: 10/13/2018 REMOVED AND REPLACED FLOOR BEAM CAP FROM APPROX. FS559+112 TO FS569, LBL27 IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,460 hrs · 33,092 cycles

FLOORBEAM CAP FROM APPROX. FS569 TO FS610, LBL27 CORRODED. (C-CHECK) RO: 10/13/2018 REMOVED AND REPLACED FLOORBEAM CAP FROM APPROX. FS569 TO FS 610, LBL27 WITH NEW FLOORBEAM CAP IAW REO AND SRM.

Part: STRIKER — CHAFED (SERVICE DOOR) · airframe 39,460 hrs · 33,092 cycles

SERVICE DOOR-THE AFT AND FWD SEAL STRIKER HAS CHAFING MARKS (C-CHECK) RO: 10/13/2018 REMOVED CHAFING DAMAGE FROM SERVICE DOOR FWD AND AFT SEAL STRIKER IAW SRM. OPS TEST GOOD.

Part: SKIN — CHAFED (RT AILERON) · airframe 39,460 hrs · 33,092 cycles

RT AILERON LOWER INBOARD AND OUTBOARD FIXED LEADING EDGES HAVE CHAFING. (C-CHECK) RO: 10/13/2018 REPLACED BOTH RT I/B & O/B LOWER LEADING EDGES IAW SRM.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 39,460 hrs · 33,092 cycles

CARGO COMPARTMENT DOOR EXTERNAL SKIN AROUND THE DOOR HANDLE IS CHAFED. (C-CHECK) RO: 10/13/2018 CARGO DOOR HANDLE HOUSING REPLACED WITH NEW SERVICABLE PART IAW AMM.

Part: HOUSING — GOUGED (CARGO DOOR) · airframe 39,460 hrs · 33,092 cycles

GOUGE ON LWR FWD INNER CORNER AND UPPER AFT CORNER OF CARGO DOOR HANDLE HOUSING.(C-CHECK) RO: 10/13/2018 REPLACED CARGO DOOR HANDLE HOUSING IAW SRM. PRESSURIZED LEAK TEST OF THE CARGO DOOR HOUSING GOOD IAW AMM. NO DEFECTS NOTED.

Part: SENSOR — OUT OF RIG (NLG) · airframe 38,475 hrs · 32,196 cycles

AFTER TAKE OFF, THE NLG WOULD NOT RETRACT, NOSE DOOR OPENED AND GEAR DISAGREE WARNING MESSAGE. INTERROGATED PSEU, FOUND 523 FAR PS14GA NG OLEO CENTERING/EXTENSION. FOUND GAP ON PSI4 TO BE OUT OF RIG. ADJUSTED THE SENSOR IAW AMM. PERFORMED EXTENSION AND RETRACTION OF NLG IAW AMM AND PSEU BITE IAW AMM. OPS CHECKED GOOD.

Part: CONTROL HANDLE — FAILED (MLG) · airframe 37,130 hrs · 31,013 cycles

AFTER SELECTING GEAR UP, INBD ANTI-SKID AND PARKING BRAKE SOV MESSAGES, GEAR STAYED DOWN, AFTER APPROXIMATELY 60 SECONDS MESSAGES EXTINGUISHED AND GEAR RETRACTED. REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE IAW AMM. PERFORMED AN OPS CHECK OF LANDING GEAR, OPS CHECKED GOOD . PERFORMED OPS CHECK OF THE PARKING BRAKE SOV IAW AMM. OPS CHECKED GOOD. PERFORMED OPS CHECK OF ANTI-SKID CONTROL UNIT. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (DUCT) · airframe 36,111 hrs · 30,069 cycles

ENROUTE, LT 14TH DUCT WARNING MESSAGE INTERMITTENTLY APPEARED THROUGHOUT FLIGHT. THE DUCTING BETWEEN THE LEFT 14TH SOV AND WING ANTI ICE VALVE ILLUMINATED RED. COMPLIED WITH THE QRH, BUT MESSAGE INTERMITTENTLY PERSISTED. DECLARED EMERGENCY AND DIVERTED. PERFORMED A SYSTEM OP CHECK IAW AMM. NO FAULTS FOUND. SYSTEM OP CHECKED GOOD.

Part: SKIN — GOUGED (BS 409) · airframe 35,110 hrs · 29,095 cycles

SKIN IN THE VICINITY OF THE ADF CUTOUT NEAR BS 409+74 TO 409+64 BETWEEN STRINGER 1R AND 1L IS GOUGED AND SCRATCHED. REPAIRED THE SKIN IAW EA.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 35,110 hrs · 29,095 cycles

RIGHT INBOARD FLAP CENTER VANE CAP IS CHAFED. REMOVED AND INSTALLED A NEW FLAP VANE CAP IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 35,110 hrs · 29,095 cycles

RIGHT INBOARD FLAP OUTBOARD VANE CAP IS CHAFED. REMOVED AND INSTALLED A NEW FLAP VANE CAP IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 35,110 hrs · 29,095 cycles

RIGHT INBOARD FLAP INBOARD VANE CAP IS CHAFED. REMOVED AND INSTALLED A NEW FLAP VANE CAP IAW SRM.

Part: FRAME — CORRODED (BS 605) · airframe 35,110 hrs · 29,095 cycles

EVIDENCE OF CORROSION ON BS 605 BETWEEN STRINGER 26R & 26L. REPAIRED IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 35,110 hrs · 29,095 cycles

CORROSION ON THE FLOOR SILL FROM FS 559.00+80 TO FS 559.00+112 ON RT SIDE OF CARGO BAY. REPAIRED IAW EA.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 35,110 hrs · 29,095 cycles

PASSENGER DOOR FLOOR SUPPORT ANGLE NUTPLATE FASTENERS HAVE CORROSION. REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT TOP ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 35,110 hrs · 29,095 cycles

PASSENGER DOOR FLOOR SUPPORT ANGLE HAS CORROSION AT CONNECTOR J1MB. REMOVED AND REPLACED PASSENGER DOOR FLOOR SUPPORT TOP AND BOTTOM ANGLE IAW SRM.

Part: DOOR SILL — CORRODED · airframe 35,110 hrs · 29,095 cycles

PASSENGER DOOR LOWER SILL ANGLE HAS CORROSION AT PS9MB SENSOR. SILL ANGLE REPLACED IAW SRM.

Part: SKIN — DENTED (BS 245) · airframe 35,110 hrs · 29,095 cycles

DENT APPROX AT BS 245 AT STRINGER 21L. REPAIRED IAW EA.

Part: SKIN — DENTED (BS 240) · airframe 35,110 hrs · 29,095 cycles

DENT APPROX AT BS 240 AT STRINGER 26L. REPAIRED IAW EA.

Part: FLOOR SUPPORT — DAMAGED (CARGO BAY) · airframe 30,500 hrs · 25,072 cycles

CARGO BAY LOWER ENTRY FLOOR SUPPORT DAMAGED. FOUND OUT OF LIMITS. R & R FLOOR SUPPORT IAW REO AND SRM 51-61-23, PAGES 2-16.

Part: SHROUD — DEBONDED · airframe 30,500 hrs · 25,072 cycles

PANEL 520JL HAS SHROUD TO SKIN DEBONDING IN SERVERAL SPOTS. BONDED PANEL 520JL, SHROUD TO SKIN L/E, REF REO. (2014NM060066)

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 30,500 hrs · 25,072 cycles

LEFT INBD FLAP VANE OTBD LEADING EDGED IS CHAFED. C-CHECK, RO 9/21/14, REPLACED LT INBD FLAP, OTBD L/E FLAP VANE CAP IAW SRM 51-40-11 AND SRM 51-42-13 AND REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 30,500 hrs · 25,072 cycles

LEFT INBD FLAP VANE CENTER L/E IS CHAFED. REPAIRED LT INBD FLAP, CENTER FLAP VANE L/E IAW REO AND FOUND TO BE WITHIN LIMITS.

Part: TRUNNION — CRACKED (LT MLG) · airframe 30,500 hrs · 25,072 cycles

LEFT MLG HAS CRACK INDICATION, HOLE IS REAMED TO .330" AND 1 EACH EXISTING OVERSIZE HOLE AT APPROXIMATELY .338" WHILE TRYING TO COMPLY WITH SB. COMPLIED WITH REPAIR OF LT MLG STEEL STRAP, WING PLANK, AND TRUNNION CRACK IAW REO.

Part: TRUNNION — CRACKED (RT MLG) · airframe 30,500 hrs · 25,072 cycles

RT MLG HAS THREE CRACK INDICITATIONS. HOLES REAMED TO .330" AND EXISTING OVERSIZE HOLE AT APPROXIMATELY .338" WHILE TRYING TO COMPLY WITH WITH SB. COMPLIED WITH REPAIR OF RT MLG STEEL STRAP, WING PLANK, AND TRUNNION 3 EACH HOLES WITH CRACKS AND 1 EACH OVERSIZE HOLE REF REO. (2014NM060066)

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 30,500 hrs · 25,072 cycles

FS 621, BULKHEAD WEB HAS CRACK AT LBL 36.0 NEAR FLOOR. REPAIRED BULKHEAD WEB IAW REO. COMPLIED WITH ST 51-900-1003. PRESSURE CHECK GOOD IN REPAIR AREA IAW AMM.

Part: SUPPORT — CHAFED (PAX DOOR) · airframe 30,500 hrs · 25,072 cycles

PAX DOOR WHEEL SUPPORT ARM CHAFED FROM CONTACTING AFT HANDRAIL, BLENDED CHAFE ON PAX DOOR WHEEL SUPPORT ARM. FOUND TO BE WITHIN LIMITS IAW EA.

Part: HINGE — CHAFED (SERVICE DOOR) · airframe 30,500 hrs · 25,072 cycles

SERVICE DOOR HINGE ARM CHAFED ON TOP AND BOTTOM SIDES FROM INNER HANDLE, COMPLIED WITH PERMANENT REPAIR OF STS EA.

Part: HANDLE — CHAFED (SERVICE DOOR) · airframe 30,500 hrs · 25,072 cycles

SERVICE DOOR INNER HANDLE CHAFED ON BOTTOM SIDE FROM SERVICE DOOR HINGE ARM, C-CHECK RO 9/21/14, ORIGINAL MATERIAL THICKNESS WAS 1.700", MEASURED WITH TOOL TUC4232, DUE 28FEB2015, REMOVED 0.115" AND 0.090" NOT EXEEDING REPORTED DAMAGE DEPTH IAW STS EA. REMAINING MATERIAL THICKNESS IS 1.585", MEASURED WITH TOOL TUC4232, DUE 28FEB2015. FOUND TO BE IN LIMITS REF STS EA. PERFORMED VISUAL INSPECTION AND FOUND CHAFE WAS CAUSED DUE TO INPROPER OPERATION, NO ADJUSTMENT NECESSARY. COMMPLIED WITH STS EA. (2014NM060066)

Part: LUG — DAMAGED (RT AILERON HINGE) · airframe 30,500 hrs · 25,072 cycles

RT AILERON OTBD PCU ATTACHMENT LUGS, INBD & OTBD LUGS, BLENDED THE RT AILERON INBD & OTBD HINGE FITTING LUGS IAW REO.

Part: SKIN — DENTED (LT WING) · airframe 30,500 hrs · 25,072 cycles

LEFT WING L/E AT WS 355.848 HAS DENT APPROXIMATELY .36 WIDE AND .010 DEEP. DRESSED DENT TO ORIGINAL CONTOUR IAW REO.

Part: SKIN — DENTED (PAX DOOR) · airframe 30,500 hrs · 25,072 cycles

TOP AFT EDGE OF PAX DOOR OUTER SKIN HAS A VERY SMALL DENT. COMPLIED WITH SECTION 1-PERMANENT REPAIR TO TOP EDGE OF PAX DOOR OUTER SKIN. (2014NM060066)

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 30,270 hrs · 24,902 cycles

F/A FLASHLIGHT, LIGHT NOT BLINKING. CHARGED BATTERY IN FLASHLIGHT AT F/A'S STATION AS REQUIRED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,076 hrs · 23,985 cycles

EMERGENCY OVERHEAD LIGHT BURNED OUT, REPLACED LAMP.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 28,507 hrs · 23,559 cycles

EXIT SIGN LIGHT BULB BY SERVICE DOOR IS BURNED OUT. FLT 5380 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,436 hrs · 22,737 cycles

FIRST OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLT#6208 RELAMPED.

Part: POST — CRACKED (FUSELAGE) · airframe 26,072 hrs · 21,718 cycles

CRACK ON FS 409.0+128 VERTICAL POST INBOARD AFT RADIUS AT RBL 18.00 WL 71.00. (C-CHECK) REPLACED VERTICAL I/B POST AND STRAP COVER AT FS 409+128 RBL 18.0 IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,394 hrs · 21,201 cycles

LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5361) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,345 hrs · 21,160 cycles

AFT EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 5616) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,132 hrs · 21,002 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6241) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,991 hrs · 20,886 cycles

NR 4 RIGHT EXTERIOR OVERWING EMERGENCY EVACUATION LIGHT IS OUT. (FLT 6350) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,565 hrs · 19,719 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5407) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,565 hrs · 19,719 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6306) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,509 hrs · 19,675 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5393) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,196 hrs · 19,424 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IN CABIN IS INOPERATIVE. (FLT 5407) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,096 hrs · 19,348 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6263) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,930 hrs · 19,212 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5292) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,874 hrs · 19,155 cycles

LEFT WING EXTERIOR FORWARD EMERGENCY EXIT LIGHT IS OUT. (FLT 5439) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,786 hrs · 19,093 cycles

RIGHT NR 2 EXTERIOR OVERWING EMERGENCY LIGHT IS OUT. (FLT 5469) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,511 hrs · 18,885 cycles

NR 1 AND 2 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 5557) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,345 hrs · 18,750 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6457) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,281 hrs · 18,692 cycles

AFT OVERHEAD EMERGENCY LIGHT BURNED OUT. (FLT 5453) RELAMPED EMERGENCY LIGHT.

Part: CABLE — BROKEN (CABIN) · airframe 21,877 hrs · 18,363 cycles

FLOOR LEVEL EMERGENCY LIGHTS BETWEEN ROWS 5-8 ARE OUT. (FLT 5373) REPLACED FLOOR LEVEL EMERGENCY LIGHT WIRE STRIP CABLE.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 21,846 hrs · 18,335 cycles

FS 280 FLOORBEAM CRACKED ON AFT SIDE. (C-CHECK) REPAIR PER REO,

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,846 hrs · 18,335 cycles

FS 559 BULKHEAD CRACKED AT RIGHT SIDE. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,846 hrs · 18,335 cycles

FS 621 BULKHEAD WEB CRACKED AT LINTEL FITTING. (C-CHECK) REPAIR PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,235 hrs · 17,868 cycles

LEFT FORWARD EXTERIOR EMERGENCY EXIT LIGHT IS OUT. (FLT 6398) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,938 hrs · 17,622 cycles

FORWARD EMERGENCY LIGHT ON LEFT SIDE OF AIRCRAFT EXTERIOR IS OUT. (FLT 6841) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,875 hrs · 17,570 cycles

NR 1 CEILING EMERGENCY LIGHT IS OUT. (FLT 6361) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,438 hrs · 17,216 cycles

FORWARD EMERGENCY LIGHT ON RIGHT SIDE OF FUSELAGE IS BURNED OUT. (FLT 6464) RELAMPED EMERGENCY LIGHT.

Part: HANDLE — LACK OF LUBE (CABIN DOOR) · airframe 20,297 hrs · 17,106 cycles

MAIN CABIN DOOR DIFFICULT TO UNLATCH FROM INSIDE. (FLT 7010) LUBRICATED MAIN CABIN DOOR INNER HANDLE ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,878 hrs · 16,761 cycles

NR 1 OVERHEAD EMERGENCY LIGHT OUT. (FLT 6400) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,706 hrs · 16,625 cycles

RIGHT FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. (FLT 6593) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,041 hrs · 16,048 cycles

AFT EMERGENCY FLOODLIGHT INOP. (FLT 6657) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 18,800 hrs · 15,843 cycles

KNEE LEVEL EMERGENCY EXIT LIGHT AT GALLEY SERVICE DOOR INOP. (FLT 6330) REPLACED BATTERY CHARGER AND BATTERY PACK. P/N: AD-2013-1A, S/N OFF: 47637.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,659 hrs · 15,729 cycles

NR 1 CEILING EMERGENCY LIGHT INOP. (FLT 6870) RELAMPED EMERGENCY LIGHT.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 18,457 hrs · 15,555 cycles

FLOOR EMERGENCY LIGHTS NEAR RIGHT WING EXIT INOP. (FLT 6724) REPLACED EMERGENCY BATTERY NR 3 INVERTER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,457 hrs · 15,555 cycles

OVERWING EMERGENCY EXIT LOWER EXIT LIGHT INOP AT SEAT 8C. (FLT 6086) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,429 hrs · 15,524 cycles

NR 3 CEILING EMERGENCY LIGHT INOP. (FLT 6764)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,235 hrs · 15,369 cycles

ROW 2 OVERHEAD CABIN EMERGENCY FLOODLIGHT INOP. (FLT 5855) RELAMPED EMERGENCY LIGHT.

Part: MOUNT — CORRODED (RT ENGINE) · airframe 18,110 hrs · 15,266 cycles

RIGHT ENGINE MOUNT ASSEMBLY PITTED. (ENGINE CHG) REPLACED ENGINE MOUNT PER AMM.

Part: TURBINE CASE — CRACKED (RT ENGINE) · airframe 18,110 hrs · 15,266 cycles

RIGHT ENGINE LPT CASE CRACKED BEYOND LIMITS. (SERVICE CK) ENGINE CHANGED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,031 hrs · 15,203 cycles

NR 2 OVERHEAD EMERGENCY LIGHT INOP. (FLT 6576) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,958 hrs · 15,147 cycles

NR 1 EMERGENCY CEILING LIGHT INOP. (FLT 6059) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,680 hrs · 14,915 cycles

CABIN EMERGENCY CEILING LIGHT AT ROW 5 INOP. (FLT 6615) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,476 hrs · 14,748 cycles

FLT 6656 - NR 2 CEILING EMERGENCY LIGHT INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,324 hrs · 14,630 cycles

EMERGENCY CEILING LIGHT NR 4 INOP. (FLT 5927) RELAMPED CEILING LIGHT.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 17,044 hrs · 14,373 cycles

AFT CARGO DOOR SILL FRAMES CRACKED. (C-CHECK) REPAIRED PER REO.

Part: RAIL — CRACKED (CARGO BAY) · airframe 17,044 hrs · 14,373 cycles

AFT UPPER CARGO DOOR GUIDE RAIL CRACKED. (C CHECK)REPAIRED PER REO.

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 17,605 hrs · 14,855 cycles

AFT CARGO DOOR SILL FRAMES CRACKED. (C CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,022 hrs · 14,351 cycles

MOST AFT CEILING EMERGENCY LIGHT INOP. (FLT 5960) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,802 hrs · 14,175 cycles

OVERHEAD EMERGENCY LIGHT (POD NR 3) BURNT OUT. (FLT 5991) RELAMPED NR 3 OVERHEAD CABIN EMERGENCY FLOOD LIGHT IAW CRJ AMM 33-51-00. OPS CHECKS GOOD.

Part: SEAL — DIRTY (GALLEY DOOR) · airframe 16,718 hrs · 14,113 cycles

GALLEY SERVICE DOOR DIFFICULT TO OPEN. (FLT 6255) CLEANED DOOR SEAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 16,450 hrs · 13,906 cycles

MAIN CABIN OUTSIDE EMERGENCY LIGHT INOP. (FLT 6534) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,080 hrs · 13,639 cycles

EMERGENCY LIGHTS OVER CENTER AISLE INOP. (FLT 6189) RELAMPED EMERGENCY LIGHTS.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,973 hrs · 13,561 cycles

FLT 6015 - CEILING LEVEL EMERGENCY FLOODLIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 14,951 hrs · 12,783 cycles

FLT 6356 - CEILING LEVEL EMERGENCY FLOODLIGHT, SECOND AFT, INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 14,853 hrs · 12,711 cycles

FLT 6503 - OVERHEAD EMERGENCY LIGHT BY LAVATORY INOP. RELAMPED.

Part: INVERTER — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 14,279 hrs · 12,265 cycles

FLT 6108 - FORWARD GREEN LIGHT SECTION OF EMERGENCY FLOOR LIGHTING INOP. REPLACED NR 2 EMERGENCY LIGHTING INVERTER.

Part: CHARGER — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 14,215 hrs · 12,215 cycles

FLT 6406 - FLOOR LEVEL EMERGENCY LIGHT STRIP, FORWARD SECTION INOP. RESET BATTERY CHARGER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,116 hrs · 12,131 cycles

OVERHEAD EMERGENCY LIGHTS NR 3 AND NR 4 INOP (FLT 6504). RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,116 hrs · 12,131 cycles

SECOND AFT EMERGENCY LIGHT IN CEILING INOP (FLT 5868). RELAMPED EMERGENCY LIGHT.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 13,987 hrs · 12,031 cycles

ON APPROACH TO LANDING, RECEIVED "NOSE GEAR" DISAGREE (FLT 6541). REPLACED NLG SELCTOR VALVE. P/N 75000-6000, S/N OFF 2029.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,971 hrs · 12,019 cycles

AFT CABIN EMERGENCY CEILING FLOOD LIGHT INOP (FLT 6504). RELAMPED EMERGENCY LIGHT.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,491 hrs · 11,606 cycles

FS 280 FLOOR SUPPORT IS CRACKED ALONG THE OB SIDE OF RBL 9. (FOUND AT C-CHECK) COMPLIED WITH REPAIRS AT FS 280 AND RBL 9 IAW MFG REO 601R-53-11-171, REV. "D".

Part: FITTING — CORRODED (LT NACELLE) · airframe 13,491 hrs · 11,606 cycles

LT AND RT ENGINE AFT THRUST FITTINGS HAVE SIGNS OF CORROSION. (FOUND AT C-CHECK) REPLACED THRUST FITTINGS IAW AMM 71-22-01-400-801.

Part: HANDLE — BROKEN (PAX DOOR) · airframe 12,238 hrs · 10,531 cycles

PASSENGER DOOR HANDLE WAS BROKEN OFF, FLIGHT NR 6607. REPLACED OUTER PAX DOOR HANDLE IAW CRJ 200 52-11-03.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 10,258 hrs · 8,840 cycles

LIGHTED EMERGENCY EXIT SIGN IN GALLEY DOES NOT ILLUMINATE. RELAMPED THE EMERGENCY EXIT SIGN IAW AMM 33-51-21.

Part: HOLDER — SPARKS (COCKPIT) · airframe 8,922 hrs · 7,656 cycles

FOS CHART HOLDER SHOT OUT SPARKS AND CHART HOLDER CB 246 POPPED OUT. SECURED SCREW ON FOS CHART HOLDER. OPERATIONAL CHECKS GOOD.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 8,344 hrs · 7,172 cycles

INTERCOSTAL IN ACCESS HOLE 832AR UPPER CORNER CRACKED ON PAX DOOR, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW INTERCOSTAL PER CRJ200 SRM 51-42-13 PG 1 AND 2 AND SRM 51-42-20 PG 23.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 8,344 hrs · 7,172 cycles

FS 621 RBL 40 WL 79 FLOOR SUPPORT ANGLE IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED (2) REPAIR ANGLE SECTIONS (1 STRAP AND REPAIR ANGLE) RT SIDE 621 FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117 REV4.

Part: ANGLE — CRACKED (BS 280) · airframe 8,344 hrs · 7,172 cycles

ANGLE CRACKED AT FS 280 WL 79 LBL 9, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIP AT FS280 RBL 9.0 I/B SIDE PER CRJ200 REO 601R 53-11-136.

Part: FITTING — CRACKED (FUSELAGE) · airframe 8,344 hrs · 7,172 cycles

AFT EQUIPMENT BAY FS 625 WL.79, ANGLES CRACKED (2) AT LBL 40 7 RBL 40, DISCOVERED DURING C-CHECK INSPECTION 1. REPLACED CLIPS AT FS 625 LBL 40 AND RBL 40 IAW CRJ 200 SRM 51-42-06 PG 13 SEC A.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 8,344 hrs · 7,172 cycles

INTERCOSTAL CRACKED IN UPPER RADIUS AT ACCESS HOLE 832BR ON PAX DOOR, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW INTERCOSTAL PER SRM 51-23-00 PG 4 AND SRM 51-42-06 PG 1-18 AND SRM 51-42-21.

Part: WEB — CRACKED (BS 280) · airframe 8,344 hrs · 7,172 cycles

FS 280 WEB CRACKED O/B OF LDL9 ANGLE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR FILLER ANGLE AND 2 REPAIR SPLICE ANGLES AT FS 280 O/B OF LBL 9.0 AT FLOOR LEVEL IAW CRJ200 REO NR 601R-53-11-136.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 8,344 hrs · 7,172 cycles

ANGLE CRACKED AT FS 280 WL 79 RBL 9, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIP AT FS280 RBL 9.0 I/B SIDE PER CRJ200 REO 601R 53-11-137.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 8,344 hrs · 7,172 cycles

PAX DOOR EXTERIOR HANDLE IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW PAX DOOR OUTER HANDLE ASSEMBLY PER CRJ200 AMM 52-11-03-400-802. OPERATIONAL CHECKS GOOD.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 8,344 hrs · 7,172 cycles

PAX DOOR DOOR STEP AFT DRAG ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FABRICATED REPAIR ITEMS, -1 ANGLE SECTION, 2 SPLICE ANGLES IAW CRJ 200 REO 601R-52-11-513A NOTES 8, 9, 10.

Part: PANEL — CRACKED (PAX DOOR) · airframe 8,344 hrs · 7,172 cycles

PAX DOOR BASE OF 3RD STAIR AFT SIDE PANEL CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS IAW REO 601R-52-11-702 SHEET 3 NOTES 1 THRU 17.

Part: PANEL — CRACKED (PAX DOOR) · airframe 8,344 hrs · 7,172 cycles

PAX DOOR FWD SIDE PANEL CRACKED AT BASE OF 2ND STEP, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER AND ANGLES AS PER CRJ 200 REO 601R-52-11-702 RII 52-900-1001 AND REO 601R-52-11-702.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 6,256 hrs · 5,337 cycles

FRONT CEILING LEVEL EMERGENCY FLOODLIGHT INOP. REPLACED NR 1 BATTERY ASSY POWER SUPPLY AND FWD EMERGENCY LIGHT IAW 33-50-00. OPERATIONAL CHECK GOOD.

Part: WINDOW — FAILED (COCKPIT) · airframe 5,219 hrs · 4,448 cycles

LEFT SIDE WINDOW SHATTERED IN FLIGHT DECK. REPLACED LEFT SIDE WINDOW IAW CRJ MM 56-12-01, PN OFF: 60R33033-11 SN OFF: 03062H7719.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB) · airframe 4,285 hrs · 3,714 cycles

STAB CHANNEL 2 WILL NOT ENGAGE. REPLACED HORIZONTAL STABILIZER MOTOR CONTROL UNIT IAW AMM 27-42-05. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 4,285 hrs · 3,714 cycles

EMERGENCY EXIT LIGHTS AT ROW 8 DIM. REPLACED NR 3 POWER SUPPLY IAW MM 33-50. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 4,259 hrs · 3,687 cycles

STAB TRIM CH1 WILL NOT ENGAGE. REPLACED HSTCU. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 4,201 hrs · 3,640 cycles

SPOILERON FAULT STATUS MESSAGE DISPLAYED. REPLACED SPOILERON OUTBOARD PCU. OPERATIONAL CHECK GOOD IAW CRJ MM 27-60-00. P/N 27000-7, S/N OFF 7517.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 4,093 hrs · 3,562 cycles

CAPTAIN`S WINDSHIELD SHATTERED AT FL350. REPLACED LEFT WINDSHIELD PER AMM 56-11-01. P/N OFF 601R33033-17, S/N OFF 03091H9936.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,559 hrs · 3,939 cycles

FS 621 LT FLOORBEAM ANGLE AT LBL 41 IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE IAW CRJ REO 601R-53-61-117 REV B.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,559 hrs · 3,939 cycles

MAIN FUSELAGE; FLOORBEAM AT RBL 9.0 HAS OB ATTACH ANGLE CRACKED AT FS 280.00, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, 51-23-00.

Part: HANDLE — DIRTY (SERVICE DOOR) · airframe 2,197 hrs · 1,973 cycles

GALLEY SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. CLEANED DOOR HANDLE SHAFT OF DEBRIS AND LUBRICATED AS NEEDED. OPERATIONAL CHECK GOOD.