N937EV

Part: LANDING GEAR — WARNING MESSAGE · airframe 35,672 hrs · 34,281 cycles

D: GEAR DISAGREE AFTER SELECTING GEAR UP. NOSE GEAR DID NOT COME UP. RAN QRH AND MANUALLY RELEASED GEAR. RETURNED TO FIELD. GEAR REMAINED LOCKED AND TAXI IN AS NORMAL.C: MEL 32-30-1CAT: A DUE: 1 FLT DAY**** DUE TO ODI EVENT****MANAGEMENT APPROVAL IS REQUIRED VIA MXC SUPERVISOR PRIOR TO RETURN TO SERVICE AFTER CLEARING THIS DEFERRAL. **** (FLIGHT 5767 - FILED CLOSED) AUG 10, 2024 STATION: SDF--DEFERRED LANDING GEAR RETRACTION SYSTEM PER MEL 32-30-1. COMPLIED WITH MX ACTION. PLACARDS INSTALLED. AIRCRAFT OK FOR CONTINUED SERVICE.CAT II NOT AUTHORIZED AUG 11, 2024 STATION: ORD -- FOUND NLG WOW NO. 2 AND CENTER HARNESS ASSEMBLY DAMAGED. REMOVED AND REPLACED IN REFERENCE TO AMM 32-61-25. OPS CHECK GOOD AT THIS TIME. NO FURTHER DEFECTS FOUND AT THIS TIME. MEL CLEARED, PLACARDS REMOVED. MAINTENANCE ACTIONS REVERSED. SEE CP 28668286 FOR AIRCRAFT UPGRADING TO CAT II STATUS.

Part: NONE — FAILED · airframe 32,814 hrs · 31,479 cycles

TROUBLESHOOT R WINDOW HEAT CAUTION ON CLIMB OUT AT 3K FEET. RAN QRH AND MESSAGE CLEARED. GOT MESSAGE AGAIN DESCENDING THROUGH 5K FEET. (FILED - CLOSED) REPLACED RT SIDE WINDOW IN REFERENCE TO CRJ200 AMM 56-12-01 AND 56-220-1000-SKY. OPS CHECK GOOD. NO LEAKS NOTED. / TORQUE WRENCH: S/N 6580 CAL DATE 9/2022 / TORQUE WRENCH: S/N 1219909882 CAL DATE 12/2022 / TORQUE WRENCH: S/N 0197302061 CAL DATE 05/31/2023

Part: NONE — FAILED · airframe 32,610 hrs · 31,300 cycles

GEAR DISAGREE AFTER TAKE OFF FLOW QRH PROCEDURES THEN RTF (FLIGHT 5229 - FILED CLOSED) FDR ANALYSIS INDICATED NOSE GEAR DID NOT FULLY RETRACT WHEN COMMANDED, MAINS DID GO FULL UP AND LOCKED. WHEN GEAR COMMANDED DOWN, ALL GEAR WERE DOWN AND LOCKED, AIRCRAFT LANDED IN NORMAL CONFIGURATION NOT OVER WEIGHT. PERFORMED VISUAL INSPECTION OF NOSE GEAR FOR DAMAGE, CONDITION AND DEBRIS, FOUND REMNANTS OF TOW STRAP TANGLED WITHIN THE GEAR. PERFORMED VISUAL INSPECTION OF NOSE LANDING GEAR AND FOUND NO DAMAGE TO GEAR AT THIS TIME. TROUBLESHOT PER FIM 32-60-07, COMPLETED DISAGREE TROUBLESHOOTING HELP SHEET, PSEU INDICATED STORED FAULTS OF S22 S30 S31 S32 D114 AND DI15 ALL FAR OR OFF IN UNEXPECTED CONDITION. FDR ANALYSIS CONFIRMS PSEU FINDINGS THAT NOSE GEAR DID NOT FULLY STOW. AFTER A/C DEPARTURE GROUND CREW INFORMED MX THAT THEY WERE UNABLE TO LOCATE THE TOW STRAP. AS PREVIOUSLY MENTIONED THREAD REMNANTS OF SUSPECTED TOW STRAP WERE FOUND TANGLED IN THE GEAR AND REMOVED. SUSPECT TOW STRAP FOD WAS AT FAULT FOR GEAR DISAGREE EVENT. PERFORMED SEVERAL EXTENSION AND RETRACTION OF NOSE GEAR IN REF TO AMM 32-33-

Part: NONE — FAILED · airframe 32,548 hrs · 31,246 cycles

DURING CLIMB OUT AT FL200 GOT THE CABIN ALT CAUTION MESSAGE. RAN THE QRH AND THE MANUAL PRESSURE CONTROLLER WAS NOT STOPPING THE CABIN ALT FROM CLIMBING. GOT THE CABIN ALT WARNING AND RETURNED TO KAMA. (FLIGHT 6941 - FILED CLOSED) REMOVED AND REPLACED BOTH CABIN PRESSURE CONTROLLERS IN REF. TO AMM 21-31-16. REMOVED AND REPLACED CABIN PRESSURE SELECTOR PANEL IN REF. TO AMM 21-31-10. PERFORMED MULITPLE PRESSURIZATION TEST ON A/C WITH RIGHT PACK ONLY. OPS CHECK GOOD ON THE GROUND. A/C PRESSURE HELD AT DELTA 4.0 FOR OVER 5 MINUTES EACH TIME WITH NO NOTICIBLE ISSUES. PLEASE REFERENCE AML 873988

Part: LINE — CHAFED (HYD SYSTEM) · airframe 30,460 hrs · 29,409 cycles

FOUND STAINLESS LINE TO NR 1 HYDRAULIC ACMP RUBBING THROUGH LEFTHAND FRAME FS 718.00 BETWEEN STGR 16A AND STGR 17. DAMAGE OUT OF LIMITS AND FOUND TO BE A MAJOR REPAIR, PER GMM 3-26 FORM M-337 REQUIRED. PERFORMED TEMPORARY REPAIR NR 2, IN REFERENCE TO CRJ 200 REO.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 29,862 hrs · 28,871 cycles

RH FLOOR SUPPORT RBL 9, BS 558 TO 559+10 WAS CORRODED AROUND NUTPLATE LOCATION INBOARD AND OUTBOARD SIDES. COMPLIED WITH REPAIR IAW REO, ALL STEPS COMPLIED WITH, CHECKS OKAY, COMPLETED TASK.

Part: FLOOR SUPPORT — CORRODED (BS 409+64-96) · airframe 29,862 hrs · 28,871 cycles

FLOOR BEAM AT LBL 9.00 HAS EXFOLIATION CORROSION AROUND MULTIPLE FLOORBOARD SCREW HOLES IN SECTION APPROX. 2 IN. FORWARD OF FS409.00+64 TO APPROX. 2 IN AFT OF FS409.00+96 (C-CHECK) RO 7/18/2020 REMOVED AND INSTALLED NEW FLOOR BEAM AT LBL 9.00 AT FS 409.00+5 TO FS 409+118. REF. REO. DWG. COMPLIED WITH TASK CARD.

Part: SUPPORT ANGLE — CHAFED (PAX DOOR) · airframe 29,862 hrs · 28,871 cycles

UPON REMOVAL OF THE FWD PAX DOOR PULL IN LEVER FOUND THE FWD PAX DOOR ANGLE SUPPORT CHAFE. REPAIRED PAX DOOR FWD ANGLE SUPPORT IAW MHIRJ REO.

Part: STIFFENER — DEFECTIVE (BS 409) · airframe 29,862 hrs · 28,871 cycles

F.S 409+128 LBL 18 OTBD AFT RADIUS OF VERTICAL POST DEFECT NOTED. (C-CHECK) RO 7/18/2020 REMOVED AND REPLACED FS 409+128 POST REF DWG, AND REO, CHECKS OKAY, COMPLETED TASK CARD

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 29,862 hrs · 28,871 cycles

PAX DOOR FWD INTERCOSTAL DD5 AND BRACKET IS CRACK (C-CHECK) RO 7/18/2020 INSTALLED NEW PAX DOOR FWD INTERCOSTAL DD5 AND BRACKET, REF. CRJ200 SRM AND BOMBARDIER DWG, PRESSURE CHECK GOOD AT THIS TIME, NO LEAKS FOUND AT THIS TIME, COMPLIED WITH STRUCTURAL MAJOR REPAIR (**RII**)

Part: FORMER — CORRODED (PAX DOOR) · airframe 29,862 hrs · 28,871 cycles

PAX DOOR FWD FORMER F/S 311.75 HAS CORROSION (C-CHECK) RO 7/18/2020 DAMAGE WITHIN LIMITS REF REO, RESTORED ACCESS AND PAX DOOR FWD FORMER REF SRM AND DWG, CHECKS OKAY, COMPLETED TASK CARD

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 29,862 hrs · 28,871 cycles

PAX DOOR - AFT DD6 INTERCOSTAL HAS CORROSION. INSTALLED NEW PAX DOOR AFT DD6 INTERCOSTAL, IAW SRM AND DWG, PRESSURE CHECKED GOOD. COMPLIED WITH STRUCTURAL MAJOR REPAIR.

Part: DOOR FRAME — CORRODED (BS 347) · airframe 29,862 hrs · 28,871 cycles

PAX DOOR AFT FORMER AT FS347.27 HAS CORROSION (C-CHECK) RO 7/18/2020 REMOVED AND REPLACED PAX DOOR AFT FORMER REF SRM AND DWG, COMPLETED TASK CARD, CHECKS OKAY

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 29,862 hrs · 28,871 cycles

PAX DOOR - AFT PULL IN CAM DOUBLER IS CRACKED REMOVED AND INSTALLED NEW PAX DOOR PULL IN CAM DOUBLER IAW CRJ 200 SRM AND BOMBARDIER DWG. COMPLIED WITH SKYWEST SKYCARD COMPLETED FORM M-337

Part: FITTING — CORRODED (DOOR FRAME) · airframe 29,862 hrs · 28,871 cycles

PAX DOOR SURROUND, AFT HANDRAIL CLOSING FITTING ASSEMBLY HAS CORROSION. BLENDED OUT CORROSION ON THE PAX DOOR SURROUND, AFT HANDRAIL CLOSING FITTING WITH-IN ALLOWABLE LIMITS IAW SRM. RESTORED FINISH TO REWORK AREA IAW SRM. REMOVED AND REPLACE THREE NUTPLATES AT REWORK AREA IAW SRM.

Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 29,862 hrs · 28,871 cycles

*PAX DOOR SURROUND - FWD ANCHOR FITTING - SERRATED PLATE HAS CORROSION. PASSENGER DOOR FWD ANCHOR FITTING REMOVED AND REPLACED WITH NEW. REF AMM. FUNCTIONAL TEST CHECKED GOOD.

Part: PRESSURE PANEL — CORRODED (BS 439-499) · airframe 29,862 hrs · 28,871 cycles

* THE RH PRESSURE FLOOR SILL PANEL HAS MULTIPLE LOCATIONS OF CORROSION BETWEEN FS439.00 AND FS499.00. REMOVED CORROSION ON RH PRESSURE FLOOR SILL PANEL BETWEEN FS439.00 AND FS499.00 IN 5 LOCATIONS. ALL BLENDS WITHIN LIMITS. SEE CONTINUE CARD FOR FURTHER DETAIL. REF: REO. COMPLIED WITH TASK CARD.

Part: PRESSURE PANEL — CORRODED (BS 424-473) · airframe 29,862 hrs · 28,871 cycles

* THE LH PRESSURE FLOOR SILL PANEL HAS CORROSION BETWEEN FS424.00 AND FS473.00. (MARKED) (C-CHECK) RO 7/18/2020 REMOVED CORROSION ON LH PRESSURE FLOOR SILL PANEL BETWEEN FS424.00 AND FS473.00 IN 7 LOCATIONS. ALL BLENDS WITHIN LIMITS. SEE CONTINUE CARD FOR FURTHER DETAIL. REF: REO.

Part: FLOOR SUPPORT — CORRODED · airframe 29,862 hrs · 28,871 cycles

*PAX DOOR SURROUND - LOWER FLOOR SUPPORT ANGLE HAS CORROSION AT FASTNER HOLES. PASSENGER DOOR LOWER FLOOR SUPPORT ANGLE REMOVED AND REPLACED WITH NEW, IAW SRM AND DWG. COMPLIED WITH TASK CARD.

Part: FRAME — CRACKED (BS 333) · airframe 29,862 hrs · 28,871 cycles

FRAME SECTOR APPROX BS 333, STRINGER 1L, CRACKED AT TOOLING HOLE. REMOVED AND INSTALLED A NEW FRAME IAW DRAWING, AND SRM. COMPLIED WITH TASK CARD. ALL CHECKS GOOD.

Part: DOOR FRAME — CHAFED (CARGO BAY) · airframe 29,862 hrs · 28,871 cycles

THE CARGO DOOR CUTOUT INETRIOR SURROUND LOWER COMBING FWD SIDE IS CHAFED. REMOVED AND REPLACED CARGO DOOR COAMING REF SRM, CHECK OKAY

Part: DOOR FRAME — CHAFED (CARGO BAY) · airframe 29,862 hrs · 28,871 cycles

THE CARGO DOOR CUTOUT INTERIOR SURROUND UPPER COMBING IS CHAFFED IN THE CENTER. REMOVED AND REPLACED CARGO DOOR UPPER COAMING REF SRM, CHECK OKAY

Part: FITTING — CORRODED (DOOR HANDRAIL) · airframe 29,862 hrs · 28,871 cycles

PAX DOOR SURROUND - FWD HANDRAIL CLOSING FITTING ASSEMBLY HAS CORROSION. BLENDED OUT CORROSION ON THE PAX DOOR SURROUND - FWD HANDRAIL CLOSING FITTING (SILL CUP CLEAT) WITH-IN ALLOWABLE LIMITS IAW SRM. RESTORED FINISH TO REWORK AREA IAW SRM. REMOVED AND REPLACE 2 EA. NUTPLATES AT REWORK AREA REF IAW SRM.

Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 29,862 hrs · 28,871 cycles

*PAX DOOR SURROUND - AFT ANCHOR FITTING - LAMINATED SHIM PLATE HAS CORROSION. (C-CHECK) RO 7/18/2020 REMOVED AND REPLACED THE AFT PASSENGER DOOR ANCHOR FITTING, REF CRJ 200 AMM.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 29,862 hrs · 28,871 cycles

*PAX DOOR SURROUND - UPPER SILL ATTACH ANGLES AT STGR3L, APPROX. FS280 APPEAR CRACKED. (C-CHECK) RO 7/18/2020 REMOVED AND REPLACED STR3 CLIPS REF DWG AND SRM, CHECK OKAY, COMPLETED TASK CARD

Part: CARGO TRACK — CORRODED (BS 559) · airframe 29,862 hrs · 28,871 cycles

CARGO TRACK BETWEEN BS 559+96 AND 559+112 CORRODED. CORROSION COMPLETELY COVERS ALL 3 ANCHOR PLATES AND IS OUT OF LIMITS IAW SRM. REMOVED THE ANCHOR PLATES IAW AMM. INSTALLED THE REPLACEMENT ANCHOR PLATES IAW AMM.

Part: BRACKET — CORRODED (FLOOR SUPPORT) · airframe 29,862 hrs · 28,871 cycles

FLOOR SUPPORT STRUCTURE MIDDLE MOUNT BRACKET FOR AFT CARGO DOOR NETTING HAS CORROSION. FLOOR SUPPORT STRUCTURE MIDDLE MOUNT BRACKET FOR AFT CARGO DOOR NETTING HAS CORROSION ON MORE THAN ONE ELEMENT AND COVERS MORE THAN 30% OF PART AND IS OUT OF LIMITS REF CRJ200 SRM. REMOVED BAD PLATE FROM INTERCOSTAL REF CRJ200 SRM. ORDERED AND RECEIVED REPLACEMENT PLATE PART# 601R35031-179, 10EA. REPLACEMENT NUTPLATES PART# MS21059L3 AND REPLACEMENT FASTENERS. INSTALLED REPLACEMENT PLATE WITH REPLACEMENT FASTENERS REF CRJ200 SRM AND DRW. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD

Part: SEAT TRACK — CORRODED (BS 559) · airframe 29,862 hrs · 28,871 cycles

SEAT TRACK AT RBL 9, BETWEEN JUST AFT OF BS 559 AND TO JUST AFT OF BS 559+80 WAS CORRODED AND GOUGED. REPLACED THE SEAT TRACK.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 29,862 hrs · 28,871 cycles

FLOOR SUPPORT STRUCTURE ÂT RBL 9, ? TOP WAS CORRODED AT MULTIPLE LOCATIONS BETWEEN APPROXIMATELY BS 559+10 AND 559+80. COMPLIED WITH PERMANENT REPAIR TO THE FLOOR SUPPORT IAW SRM AND REO, ALL APPLICABLE STEPS COMPLIED WITH, COMPLETED TASK CARD.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 29,862 hrs · 28,871 cycles

*FLOOR SUPPORT STRUCTURE, AT RBL9, APPROX. FS559+80: TRACK FOR 9G/LAV MOUNT IS CORRODED. (C-CHECK) RO 7/18/2020 REMOVGED AND INSTALLED 1 EACH NEW SERVICEABLE SEAT TRACK SECTION P/N 601R38779-13 AT RBL9 AND FS559+80. REF - CRJ 200 AMM.

Part: PANEL — CRACKED (PAX DOOR) · airframe 29,862 hrs · 28,871 cycles

PASSENGER DOOR AFT WEB PANEL HAS CRACK IN LOWER CORNER. REMOVED AND INSTALLED NEW AFT STAIR WEB PANEL IAW SRM.

Part: BRACKET — CORRODED (FLOOR SUPPORT) · airframe 29,862 hrs · 28,871 cycles

*FLOOR SUPPORT STRUCTURE AFT MOUNT BRACKET FOR AFT CARGO DOOR NETTING HAS CORROSION. (C-CHECK) RO 7/18/2020 CARGO FLOOR SUPPORT STRUCTURE AFT MOUT BRACKET FOR NETTING HAS CORROSION ON MULTIPLE ELEMENTS AND IS OUT OF LIMITS. REMOVED AND REPLACED WITH NEW BRACKET P/N 601R35031-189 REF CRJ 200 SRM AND BOMBARDIER DRAWING. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 29,862 hrs · 28,871 cycles

* THE SEAT TRACK AT LBL 9.00 HAS CORROSION FROM FS364.00 TO JUST AFT FS394.00. REMOVED AND REPLACE PART - THE NEW SEAT TRACK ALONG WITH NEW FASTENERS AT LBL 9.0 AT FS364.00 - FS394.00 . REF CRJ200 AMM.

Part: FLOORBEAM — CORRODED (BS 621) · airframe 29,862 hrs · 28,871 cycles

FLOORBEAM ANGLE AT LEFT SIDE BS 621 BULKHEAD HAS CORROSION. REMOVED AND REPLACED REPAIR ANGLE IN REFERENCE TO REO AND SRM, CHECK OKAY, COMPLETED TASK CARD

Part: FITTING — CORRODED (BS 310) · airframe 29,862 hrs · 28,871 cycles

* THE WARDROBE FITTING JUST FWD OF FS310.00 AT LH FLOOR SILL HAS CORROSION. (MARKED) (C-CHECK) RO 7/18/2020 REMOVED AND REPLACED WARDROBE FITTING JUST FWD OF FS310.00 AT LH FLOOR SILL. SEE CONT CARD FOR DETAILS. REF: CRJ200 NDTM, CRJ200 SRM AND DWG

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 29,862 hrs · 28,871 cycles

THE SEAT TRACK AT RBL 9 WAS CORRODED FROM BS 364 TO JUST AFT OF BS 394. REMOVED AND REPLACED THE SEAT TRACK IAW AMM.

Part: FRAME — CORRODED (BS 605) · airframe 29,862 hrs · 28,871 cycles

*CORROSION ON FRAME AT FS 605.00 ON FWD FACE BETWEEN STRG 24R STGR 26R (C-CHECK) RO 7/18/2020 REPLACED FS605.00 FRAME BETWEEN STGR 20R AND STGR 20L. REF BOMBARDIER DWG AND CRJ 200 SRM. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 29,862 hrs · 28,871 cycles

BS 621 PRESSURE BULKHEAD, FWD FACE ABOVE FLOOR, AREA EXIBITS MANY SCREW STARTS AND GOUGES, AND SEVERAL DAMAGED RIVET HEADS. REPAIRED THE BS 621 BULKHEAD IAW REO. COMPLIED WITH TASK CARD.

Part: FLOORBEAM — CRACKED (BS 559) · airframe 29,862 hrs · 28,871 cycles

*PRESSURE FLOOR SUPPORT CENTER BEAM (BL 0.00) IS CRACKED AT FS 559.00 (C-CHECK) RO 7/18/2020 REPAIRED FLOOR BEAM BETWEEN FS529.00 & FS559.00 AND BL0.0. REF REO. ALL CHECKS GOOD.

Part: FLOORBEAM — CORRODED (BS 621) · airframe 29,862 hrs · 28,871 cycles

FLOORBEAM AT LBL 27 FOR THE FS621 BULKHEAD MOUNT WAS CORRODED. COMPLIED WITH PERMANENT REPAIR FLOOR FITTING AT BS 621 REF REO, ALL STEPS COMPLIED WITH.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 29,862 hrs · 28,871 cycles

PAX DOOR, MIDDLE INTERCOSTAL DD6 HAS SIGNS OF CORROSION AND LOSS PF PROTECTIVE COATING. REMOVED AND REPLACED PAX DOOR INTERCOSTAL IAW SRM AND DWG, COMPLETED TASK CARD, CHECKED OKAY.

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 29,862 hrs · 28,871 cycles

COPILOTS OUTBOARD SEAT TRACK HAS MISSING AND DAMAGED FASTENER HEADS FOR THE TOP CAP PLATE. PERFORMED PERMANENT REPAIR TO COPILOT'S OTBD SEAT TRACK. REF REO & DWG.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 29,862 hrs · 28,871 cycles

PAX DOOR, MIDDLE INTERCOSTAL AT DD4 WAS CORRODED. INSTALLED A NEW PAX DOOR DD4 INTERCOSTAL IAW SRM AND DWG, PRESSURE LEAK CHECKED GOOD. NO DEFECTS NOTED. COMPLIED WITH STRUCTURAL MAJOR REPAIR.

Part: BRACKET — CORRODED (BS 347) · airframe 29,862 hrs · 28,871 cycles

PAX DOOR - CLIP AT APPROX. FS347 FOR THE AFT INTERCOSTAL AT DD6 HAS CORROSION. (C-CHECK) RO 7/18/2020 INSTALLED NEW PAX DOOR CLIP COMMON TO AFT DD6 INTERCOSTAL, REF. CRJ200 SRM AND BOMBARDIER DWG, PRESSURE LEAK CHECK GOOD AT THIS TIME, NO LEAKS FOUND AT THIS TIME, COMPLIED WITH STRUCTURAL MAJOR REPAIR (**RII**)

Part: BULKHEAD — CHAFED (BS 280) · airframe 29,862 hrs · 28,871 cycles

*FS280, RIGHT SIDE BULKHEAD HAS CHAFES ON A REPAIR DOUBLER ON THE AFT SIDE. REMOVED AND REPLACED THE EXISTING CHAFED -1 DOUBLER WITH A NEW -1 DOUBLER REF PREVIOUSLY ACCOMPLISHED REO, SRM AND RESTORED FINISH TO REWORK AREA IAW SRM.

Part: ROLLER — CRACKED (GALLEY DOOR) · airframe 29,862 hrs · 28,871 cycles

SERVICE DOOR: AFT DOWN-LOCK ROLLER IS CRACKED. REMOVED AND REPLACED THE ROLLER AND PIN IAW AMM.

Part: SKIN — DENTED (BS 603) · airframe 29,862 hrs · 28,871 cycles

DENT IN AIRCRAFT SKIN BS 603, STR 18L. REPAIRED THE DENT WITH GOUGE IAW REO.

Part: HINGE FITTING — CHAFED (EMERGENCY EXIT) · airframe 29,862 hrs · 28,871 cycles

RIGHT EMERGENCY DOOR HINGE FITTINGS FWD AND AFT HAVE ABRASION DAMAGE. COMPLIED WITH PERMANENT REPAIR DOOR HINGE FITTINGS REF REO, ALL STEPS COMPLIED WITH, CHECKS OKAY, COMPLETED TASK CARD

Part: SKIN — DENTED (BS 605) · airframe 29,862 hrs · 28,871 cycles

6 EA. DENT LOCATED @ APPROX. FS605 BELOW WL 783.50 (MARKED). PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. ALL DENTS REPAIRED WITHIN ALLOWABLE LIMITS REF REO, ALL STEPS COMPLIED WITH, COMPLETED TASK CARD, CHECKS OKAY

Part: FUEL CONTROL — MALFUNCTIONED (LT ENGINE) · airframe 29,790 hrs · 28,806 cycles

ABNORMALLY HIGH LEFT ITT TEMP DURING FLIGHT FOLLOWED BY L ENG OIL PRESS WARNING ON DESCEND, ACCOMPLISHED QRH PROCEDURE ON DESCEND. FLIGHT 5303 - FILED CLOSED PERFORMED ENGINE OIL CONSUMPTION CHECK REF PPGRM TEST NUMBER 9 NO OIL NEEDED AFTER RUN. PLEASE REFERENCE AML 403732 FOR FDR DOWNLOAD REQUEST. AFTER FDR DOWNLOAD IT WAS DETERMINED THAT THE LOW OIL PRESSURE WAS CAUSED BY AN INFLIGHT SHUT DOWN. AFTER TROUBLESHOOTING IT WAS DETERMINED BY FLEET COORDINATOR THAT THE MAIN FUEL CONTROL WOULD NEED REPLACED. REMOVED AND REPLACED LEFT HAND ENGINE MAIN FUEL CONTROL WITH A SERVICEABLE UNIT WITH REFERENCE TO THE APPLICABLE STEPS IN THE CRJ200 AMM. OPS AND LEAK CHECK GOOD AT THIS TIME. COMPLIED WITH CRJ200 TASK CARD FOR INSTALLATION OF THE MAIN FUEL CONTROL. SEE ATTACHED TASK CARD AS NECESSARY. NO AUTO SHUT DOWN NOTED FOR THE LEFT ENGINE AND OIL PRESSURE INDICATION SYSTEM OPS CHECKS GOOD WITH REFERENCE TO THE APPLICABLE STEPS IN THE CRJ200AMM AND CRJ200 AMM. AIRCRAFT OKAY FOR CONTINUED SERVICE. TORQUE WRENCH S/N 0711501055 CAL DUE 11/2020. FORCE GAUGE S/N E9516A041 CAL DUE 01/31/2021

Part: PANEL — CORRODED (BS 260) · airframe 25,464 hrs · 25,040 cycles

COCKPIT, BS 260, WL 73, RBL 11 TO LBL 11 CORRODED ON THE VERTICAL PANEL. BLENDED CORROSION IAW SRM AND REO.

Part: SKIN — CORRODED (BS 409) · airframe 25,464 hrs · 25,040 cycles

LOWER EXTERNAL FUSELAGE SKIN HAS CORROSION AT MATING SURFACE FOR WING TO BODY PANEL, BS 409+96, BL 0. BLENDED CORROSION IAW SRM.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 25,464 hrs · 25,040 cycles

DENT ON THE UNDER SIDE OF LEFT OUTBOARD FLAP OUTBOARD EDGE. REPAIRED THE FLAP IAW SRM.

Part: PRESSURE DECK — CORRODED (BS 409-559) · airframe 25,464 hrs · 25,040 cycles

LEFT SIDE PRESSURE FLOOR SILL PANEL HAS CORROSION BETWEEN FS409.00+128 AND FS559.00 AT WL73.0. REMOVED CORROSION IAW SRM. PERFORMED LEAK CHECK IAW AMM. NO LEAKS NOTED.

Part: SEAT TRACK — CORRODED (BS 574-609) · airframe 25,464 hrs · 25,040 cycles

CORROSION FOUND ON THE SEAT TRACK BS 574 TO 609, LBL 27. REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK IAW REO AND SRM.

Part: SHROUD — CHAFED (RT WING AILERON) · airframe 25,464 hrs · 25,040 cycles

RIGHT WING. AILERON LOWER LEADING EDGE SHROUD CHAFED. REPLACED THE SHROUD IAW SRM.

Part: SKIN — DENTED (BS 250-265) · airframe 25,464 hrs · 25,040 cycles

DENT ON THE FUSELAGE SKIN, BS 265 - 250, STRINGERS 26 - -27R. REPAIRED IAW REO.

Part: SKIN — DENTED (BS 654-672) · airframe 25,464 hrs · 25,040 cycles

TWO SMALL DENTS ON UPPER FUSELAGE SKIN BETWEEN BS 654.5 AND 672.20, STRINGERS 8R AND 9R. REPAIRED IAW REO.

Part: SKIN — DENTED (BS 235-250) · airframe 25,464 hrs · 25,040 cycles

DENT ON THE FUSELAGE SKIN AT BS 250 - 235 , STRINGERS 25- 26R. REPAIRED IAW REO.

Part: FAIRING — GOUGED · airframe 25,464 hrs · 25,040 cycles

LOWER LEFT VISOR FAIIRING 326BL WAS GOUGED. REMOVED AND INSTALLED IAW SRM.

Part: STRIKER — DAMAGED (PAX DOOR SEAL) · airframe 25,464 hrs · 25,040 cycles

PASSENGER DOOR AFT SEAL STRIKER HAS EDGE DAMAGE. REPAIRED THE SEAL STRIKER IAW REO.

Part: SKIN — DENTED (BS 590) · airframe 25,464 hrs · 25,040 cycles

DENT FOUND ON THE RIGHT FUSELAGE SKIN, BS 590 BETWEEN STRINGERS 20R AND 21R. REPAIRED THE DENT IAW REO.

Part: SKIN — DENTED (BS 640-654) · airframe 25,464 hrs · 25,040 cycles

SMALL DENT ON UPPER FUSELAGE SKIN BETWEEN BS 640 AND 654, STRINGERS 6R AND 7R. REPAIRED IAW REO.

Part: SKIN — DENTED (BS 640) · airframe 25,464 hrs · 25,040 cycles

SMALL DENT ON UPPER FUSELAGE SKIN FWD OF BS 640, BETWEEN STRINGERS 6R AND 7R. PERFORMED CUT-OUT REPAIR IAW REO.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 24,428 hrs · 24,110 cycles

RIGHT OUTBOARD FLAP LOWER SKIN DENTED, REPAIRED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 424-513) · airframe 24,428 hrs · 24,110 cycles

LEFT PRESSURE FLOOR SUPPORT IS CORRODED BETWEEN BS 424 AND 513. REPAIRED IAW REO.

Part: FLOORBEAM — CORRODED (BS 409) · airframe 24,428 hrs · 24,110 cycles

FLOORBEAM CAP IS CORRODED RBL 9.0 BETWEEN BS 409+16 - 409.00+112. REMOVED AND REPLACE THE FLOORBEAM CAP IAW REO.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 24,428 hrs · 24,110 cycles

LEFT INBD FLAP LOWER SKIN AT INBD END HAS TWO DENTS AND GOUGES. REPAIRED IAW SRM.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 24,428 hrs · 24,110 cycles

RIGHT FLAP LOWER SKIN DENTED APPROX WS 65. REPAIRED RT FLAP SKIN IAW SRM.

Part: WARNING MESSAGE — FALSE ACTIVATION (OVERHEAT) · airframe 22,828 hrs · 22,332 cycles

PILOT REPORTED THE RT JET OVERHEAT FAIL CAUTION MESSAGE IN FLIGHT. CAME ON AND DISAPPEARED TWICE. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY IAW AMM 26-11-00, OPS CHECKED GOOD WITH NO DEFECTS NOTED. THE DISCREPANCY HAS NOT REPEATED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,557 hrs · 22,030 cycles

NR 2 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 21,893 hrs · 21,331 cycles

DENT ON RT HORIZONTAL STABILIZER L/E. COMPLIED WITH ECTC REO 601R-55-12-541 PERMANENT REPAIR. RECEIVED REO 601R-55-12-541. COMPLIED WITH REO 601R-55-12-541. EC/TC REO 601R-55-12-541 HAS BEEN COMPLIED WITH REO 601R-55-12-541, REV A HAS BEEN ACCOMPLIISHED. OUT OF SEQUENCE REMOVED RT STAB L/E IAW AMM 55-12-02-000-801. INSTALLED RT STAB L/E IAW AMM 55-12-02-400-801.

Part: SEAT TRACK — CORRODED (BS 499-544) · airframe 21,893 hrs · 21,331 cycles

LEFT SIDE SEAT TRACK AT BS 499 - 544 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 499-544) · airframe 21,893 hrs · 21,331 cycles

RIGHT SIDE SEAT TRACK AT BS 499 - 544 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-411-400-802.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 21,893 hrs · 21,331 cycles

LT SIDE SEAT TRACK AT BS 449-499 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 21,893 hrs · 21,331 cycles

LEFT SIDE SEAT TRACK IS CORRODED IN MULTIPLE AREAS AT BS 409+128 - 449. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 21,893 hrs · 21,331 cycles

RIGHT SIDE SEAT TRACK AT BS 449 - 499 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: POST — CRACKED (BS 409) · airframe 21,893 hrs · 21,331 cycles

BS 409+128, VERTICAL POST CRACKED ON AFT LT SIDE ATTACHED TO BULKHEAD AT BL 0. REMOVED VERTICAL POST L-ANGLE IAW SRM 51-42-06. INSTALLED SERVICEABLE VERTICAL POST BULKHEAD REINFORCING ANGLE AT FS 409+128, BL0 LT SIDE WL65-WL73 IAW SRM 51-42-06, 51-42-22 AND DWG 601R32208. LOCATED FASTENER HOLES IN NEW SERVICABLE BULKHEAD REINFORCING ANGLE TO MATCH EXISTING VERTICAL POST, BULKHEAD WEB FASTENER LOCATIONS AT FS 409+128/BL0, LEFT SIDE WL73-WL65 IAW SRM 51-40-11, 51-42-06. RECEIVED AND COMPLIED WITH REO 601R-53-41-2016, REV-DATED 2016-03-27 AS WRITTEN. RECEIVED AND COMPLIED WITH ECTC REO 601R-53-41-2016.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 21,893 hrs · 21,331 cycles

CORROSION FOUND ALONG LT SEAT TRACK BETWEEN BS 364 - 409+16. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 544-559) · airframe 21,893 hrs · 21,331 cycles

LEFT SIDE SEAT TRACK AT BS 544 - 559+64 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 544-559) · airframe 21,893 hrs · 21,331 cycles

RIGHT SIDE SEAT TRACK AT FS 544 - 559+64. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 21,893 hrs · 21,331 cycles

RT SIDE SEAT TRACK AT BS 409+128 - 449 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 21,574 hrs · 20,972 cycles

LEFT FRONT WINDSHIELD EXPERIENCED ELECTRICAL ARCHING AND SMOLDERING IN UPPER LT CORNER. FOLLOWED BY ENTIRE WINDSHIELD SHATTERING. R & R LT WINDSHIELD IAW AMM 56-11-01, IPC 56-11-00, FIG 1, RET 5F. OPS CHECK AND LEAK CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. ACFT OK FOR SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 20,230 hrs · 19,579 cycles

EMERGENCY LIGHT FOUND CRACKED AND DELAMINATED. REPLACED THE LIGHT TRACK.

Part: BULKHEAD WEB — CRACKED (BS 559) · airframe 20,230 hrs · 19,579 cycles

FOUND THE BS 559 BULKHEAD WEB HAS CRACK INDICATION NOTED OTBD OF RBL 9.0 APPROXIMATLEY FOUR INCHES IN LENGTH. REPAIRED IAW REO 601R-53-41-260 AND REO 601R-53-41-260, REV E.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,106 hrs · 19,449 cycles

EXTERNAL EMERGENCY LIGHT NR 3 INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-21. SYS OPS CHECKED GOOD. NO FURTHER ACTION.

Part: LIGHT — WORN (CABIN) · airframe 19,917 hrs · 19,264 cycles

EMERGENCY LIGHT WORN. R & R EMERGENCY LIGHT IAW AMM 33-51-01.

Part: COVER — BROKEN (EMERGENCY LIGHTS) · airframe 19,618 hrs · 18,960 cycles

EXIT COVER ON LOWER FWD WALL BY PASSENGER DOOR BROKEN. R & R EMERGENCY FLOOD LIGHT ASSY IAW AMM 33-51-19. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,746 hrs · 17,129 cycles

CABIN AFT MOST CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-16, OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 17,448 hrs · 16,826 cycles

RT NR 2 EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. R & R BULB IAW AMM 33-51-21. OP'S CHECKED GOOD.

Part: GLOWSTRIP — MISINSTALLED (CABIN) · airframe 17,229 hrs · 16,600 cycles

GLOWSTRIP ROWS 8 THROUGH 14 INSTALLED INCORRECTLY. REMOVED AND INSTALLED GLOWSTRIP CORRECTLY IAW AMM 33-51-01.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,229 hrs · 16,600 cycles

NR 1 CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 17,198 hrs · 16,566 cycles

FWD BULKHEAD EMERGENCY FLOOR LEVEL FLOODLIGHT COVER MISSING. REPLACED FWD BULKHEAD EMERGENCY FLOOR LEVEL FLOODLIGHT COVER IAW AMM 33-51-19.

Part: RIB — CRACKED (LT MLG WW) · airframe 17,140 hrs · 16,504 cycles

LEFT BATTERY RIB CRACKED INSIDE LT MLG WW. REPAIRED IAW REO 601R-57-51-046 PERMENENT REPAIR. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CORRODED (BS 409) · airframe 17,140 hrs · 16,504 cycles

CORROSION ON INTERNAL SKIN AROUND VHF 2 ANTENNA LOCATED AT S27 BETWEEN FRAMES 409 AND 409+16. REPAIRED IAW SRM 51-21-06.

Part: SKIN — CORRODED (RT WING) · airframe 17,140 hrs · 16,504 cycles

FOUND CORROSION ON RT LOWER WING PLANK AT FUEL PANEL 640BB ACCESS HOLE. REPAIR CLASSIFIED AS MAJOR. COMPLIED WITH ECTC EO 600-57-81 C/W AS WRITTEN.

Part: STRUCTURE — CORRODED (BS 295-333) · airframe 17,140 hrs · 16,504 cycles

CORROSION FOUND NEAR RBL 9, BETWEEN FS 295 & 333. REPAIRED IAW SRM 51-21-06 AND REO 601R-53-21-2448 IAW NDTM PART 1 51-20-06.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 17,140 hrs · 16,504 cycles

SEAT TRACK RBL 9, FS 364 & 409 CORRODED IN SEVERAL AREAS. R & R SEAT TRACK IAW AMM 53-01-11-000-802, AND 53-01-11-000-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,140 hrs · 16,504 cycles

SEAT TRACK CORRODED AT SEVERAL AREAS. R & R SEAT TRACK IAW AMM 53-01-11-000-802, 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 17,140 hrs · 16,504 cycles

SEAT TRACK ON LBL 9, BETWEEN BS 364 & 409 HAS CORROSION ON FWD EDGE. R & R SEAT TRACK IAW AMM 53-01-11-000-802, 53-01-11-400-802.

Part: ANGLE — CRACKED (BS 625 S14L) · airframe 17,140 hrs · 16,504 cycles

CRACKED ANGLE ON AFT PRESSURE BULKHEAD AT S14L AFT SIDE BS 625. REMOVED CRACKED ANGLE IAW SRM 51-42-06-00. INSTALLED ANGLE IAW SRM 51-42-21.

Part: ATTACH ANGLE — CRACKED (BS 625) · airframe 17,140 hrs · 16,504 cycles

CRACKED ANGLE ON AFT PRESSURE BULKHEAD FS 625 AFT SIDE AT S14R. REMOVED CRACKED INTERCOSTAL ANGLE IAW SRM 51-42-21. INSTALLED NEW SERVICEABLE INTERCOSTAL ANGEL IAW SRM 51-42-21 & DWG 601R350126.

Part: LIGHT — WRONG PART (CABIN) · airframe 17,140 hrs · 16,504 cycles

ACFT ARRIVED WITH IMPROPER EMERGENCY FLOOR LIGHT TRACKS GOING FORWARD, EMERG EXITS. REMOVED LIGHT IAW AMM 33-51-01-000-806 AND INSTALLED IAW AMM 33-51-01-400-806.

Part: HANDLE — DIRTY (SERVICE DOOR) · airframe 16,044 hrs · 15,344 cycles

SERVICE DOOR HANDLE WON`T POP OPEN FROM OUTSIDE. CLEANED DEBRIS OUT OUTER HANDLE PIN PRESS, AND SPRING, TRIGGER AIRSTAIR. LUBRICATED IAW AMM 12-20-52. OPS CHECK GOOD SEVERAL TIMES IAW AMM 52-41-03.

Part: DOOR — BINDING (SERVICE) · airframe 13,350 hrs · 12,397 cycles

RAMPER CANNOT OPEN SERVICE DOOR. OPS TEST OF DOOR GOOD REF AMM 52-41-00. (CLOSED)

Part: LIGHT — BROKEN (CABIN) · airframe 13,116 hrs · 12,141 cycles

BOTH WARDROBE EMERGENCY EXIT LIGHTS ARE BROKEN. REPLACED FLOOR LIGHT AND EXIT LIGHT ON WARDROBE IAW AMM 33-51-10-400-801 AND 33-51-19-400-801. INSTALLED WARDROBE EXIT LIGHT LENS COVER IAW AMM 33-51-10-400-801. EMERGENCY LIGHT OP CHECK DUE. WARDROBE EMERGENCY LIGHT OP CHECK IS GOOD IAW AMM 33-51-00-710-801.

Part: SKIN — CORRODED (FUSELAGE) · airframe 13,101 hrs · 12,126 cycles

FOUND FOR GOUGES WITH CORROSION AROUND AIR EXTERNAL CONNECTION ON SKIN/PLATING WHERE FITTING MOUNTS. REPAIRED DAMAGED AREA IAW REO 601R-53-61-4104.

Part: SILL — CORRODED (FUSELAGE) · airframe 13,101 hrs · 12,126 cycles

PAX DOOR CUTOUT SILL ANGLE IS CORRODED. INSTALLED NEW SILL ASSY IAW SRM 51-42-06, 51-42-21 & 51-42-13.

Part: SILL — CORRODED (FUSELAGE) · airframe 13,101 hrs · 12,126 cycles

PAX DOOR CUTOUT SILL ANGLE IS CORRODED. REMOVED PAX DOOR CORRODED SILL ANGLE IAW SRM 51-42-06, 51-42-10 & 51-42-21. LOCATED & DRILLED NEW SERVICEABLE SILL ANGLE IAW SRM 51-40-11, 51-22-00, 51-42-06, 51-42-10.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 13,101 hrs · 12,126 cycles

FS 280, FLOORBEAM ATTACH ANGLES AT INBD AND OTBD SIDES OF LBL 9 AND RBL 9 ARE CRACKED IN UPPER RADIUS AND TRANSVERSE BEAM IS CRACKED 1.0" IN LOWER RADIUS JUST OTBD OF RBL 9. R & R ATTACH ANGLES IAW SRM 51-42-06 AND 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 13,101 hrs · 12,126 cycles

CARGO BAY FLOOR SUPPORT OTBD FLANGE OF LBL 27 IS CORRODED AROUND NUTPLATE HOLE FROM FS 574 TO 621. REMOVED FOR REPLACED IAW SRM 51-42-06 AND SRM 51-42-21.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 13,101 hrs · 12,126 cycles

LEFT FS 484 FLOOR SUPPORT INTERCOSTAL REPAIR ANGLE CRACKED AT LBL 36. REPAIRED IAW REO 601R-53-41-059.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 13,101 hrs · 12,126 cycles

RIGHT FS 484, FLOOR SUPPORT INTERCOSTAL REPAIR ANGLE CRACKED AT RBL 27. R & R RT FLOOR SUPPORT, INTERCOSTAL IAW SRM 51-42-21.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 13,101 hrs · 12,126 cycles

LT FS 484 FLOOR SUPPORT INTERCOSTAL REPAIR ANGLE CRACKED AT LBL 27. REMOVED ANGLE AND INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-40-11 AND SRM 51-42-21.

Part: LIGHT — DAMAGED (GALLEY) · airframe 13,101 hrs · 12,126 cycles

GALLEY SIDE TRIM PANEL EXIT LIGHT IS DAMAGED. REMOVED, REPLACED AND INSTALLED SERVICEABLE GALLEY SIDE TRIM PANEL EXIT LIGHT IAW AMM 33-51-13-400-801. OPS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 12,005 hrs · 10,871 cycles

LOWER EXIT SIGN COVER IN GALLEY MISSING BY SERVICE DOOR. REPLACED GALLEY RT LOWER EXIT SIGN IAW AMM 33-51-10. OPS CK GOOD ACFT OK FOR SERVICE. (CLOSED)

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 11,793 hrs · 10,635 cycles

EMERGENCY EXIT SIGN REF CAP IN CABIN CEILING IS MISSING. REINSTALLED RED END CAP FOR EXIT SIGN REF AMM 33-51-14. (CLOSED)

Part: RELAY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 10,475 hrs · 9,087 cycles

EMERGENCY LIGHTS ON STATUS LIGHT REMAINS ON WHEN EMERGENCY LIGHT SWITCH IS SELECTED TO ARM. R & R ACCESS BUS-SENSE RELAY K1XD IAW AMM 24-51-27. OPS CHECKED IAW AMM 24-51-27. OPS CHECKED EMERGENCY LIGHTS IAW AMM 33-51-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 10,474 hrs · 9,087 cycles

R & R BATTERY PACKS NR 3 AND NR 4 IAW AMM 33-51-04. OPS CHECKED IAW AMM 33-51-04.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 10,474 hrs · 9,087 cycles

R & R BATTERY PACKS NR1 AND NR2 IAW AMM 33-51-04. OPS CHECKED IAW AMM 33-51-04.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 9,519 hrs · 8,057 cycles

PAX DOOR AFT ANCHOR FITTING CRACKED. REMOVED AND INSTALLED NEW ANCHOR FITTING IAW MM 52-11-17-400-804.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 9,519 hrs · 8,057 cycles

LEFT FS 484 FLOOR SUPPORT INTERCOSTAL ANGLE AT LBL 27 CRACKED .1 INCH LONG UNDER CABIN FLOOR PNL 261DLF. REMOVED OLD CLIP IAW SRM 51-42-06. LOCATED AND DRILLED UP NEW CLIP IAW SRM 51-40-11. INSTALLED NEW CLIP IAW REO 601R-53-41-059 & ASA EC/TC.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 9,519 hrs · 8,057 cycles

LEFT AND RIGHT OBLIQUE ANGLES AT FS 625 AFT EQUIP COMPARTMENT ARE CRACKED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,649 hrs · 5,385 cycles

AFT RIFGR EMERGENCY LIGHT BULB INOP.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 5,929 hrs · 4,759 cycles

LT OVERWING FWD EMERGENCY LIGHT BULB BURNED OUT.

Part: FLASHLIGHT — WEAK (COCKPIT) · airframe 5,618 hrs · 4,496 cycles

F/O'S YELLOW FLASHLIGHT ON C/B PANEL NR 2 BATTERY IS WEAK / UNSERVICEABLE.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 4,955 hrs · 3,960 cycles

CRACK FOUND ON CARGO DOOR STRUCTURE ANGLE AT FS 621 LBL 36.00 WL 112.00 (CARGO POST LOWER ANGLE).

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 4,957 hrs · 3,960 cycles

AT I/S 484.00 RIGHT INTERCOSTAL AND CLIP ARE CRACKED, LEFT INTERCOSTAL IS CRACKED.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 4,957 hrs · 3,960 cycles

CRACK FOUND ON PAX DOOR HANDLE. OUTER HANDLE ASSEMBLY REMOVED IAW MM 52-11-03 / TASK 52 11 03 020 07. LATCH LOCK BOX REMOVED FOR ACCESS AND INSTALLED IAW 52-11-21. LATCH LOCK BOX AND OUTER HANDLE INSTALLED IAW 32-11-03 AND 52-11-25. FUNCTIONAL TEST OF PASSENGER DOOR C/O IAW 52-11-03 720 802. SUPPLEMENTAL - SDR CLOSED 06/21/07.

Part: FLAP — FAILED (WING) · airframe 4,678 hrs · 3,736 cycles

FLAPS FAIL AT CRZ FL300 AT ZERO. EMERGENCY DECLARED.

Part: STEP — BROKEN (AIRSTAIR DOOR) · airframe 4,251 hrs · 3,409 cycles

ASD BTM STEP BROKEN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,138 hrs · 3,322 cycles

LEFT OVERWING EMERGENCY LIGHTS INOP.

Part: STEP — CRACKED (AIRSTAIR) · airframe 3,041 hrs · 2,490 cycles

ASD BOTTOM STEP CRACKED.

Part: WARNING LIGHT — ILLUMINATED (LAVATORY SMOKE) · airframe 1,932 hrs · 1,583 cycles

SMOKE TOILET CAUTION MSG IN FLT 2 TIMES. "NOTED A UNUSUAL ODOR IN CABIN" "REPEAT"

Part: COALESCER BAG — DIRTY (FUSELAGE)

DURING APPROACH, AT APPROX 5,000 FT, THE CREW SAW AND SMELLED SMOKE IN THE COCKPIT. SHORTLY AFTER, A SMOKE TOILET CAUTION MESSAGE ON THE EICAS WAS RECEIVED. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED WITH THE CREW REQUESTING THE EMERGENCY VEHICLES BE DISPATCHED. BEFORE LANDING, THE SMOKE TOILET MESSAGE EXTINGUISHED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT AND RT COALESCER BAGS AND RAN BOTH ENGINE IN ALL BLEED CONFIGURATIONS WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: UNKNOWN — UNKNOWN

DURING APPROACH, THE CREW REPORTED SMELLING SMOKE AND RECEIVING AN AMBER SMOKE LAV MESSAGE. NO VISUAL COMFIRMATION OF SMOKE. THE AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO DEFECTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: FLASHLIGHT — INOPERATIVE (COCKPIT)

DURING A GROUND INSPECTION IN ATL, THE CAPTAINS FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS FLASHLIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)