N367CA

Part: SENSOR — FAULTED (BRAKE TEMP) · airframe 47,441 hrs · 36,886 cycles

DURING CLIMB OUT AT AROUND 8000+ BRAKE OVHT WARNING MSG DISPLAYED FOR THE IB L SIDE BRAKES. FOLLOWED THE QRH. MSG WENT AWAY MOC NOTIFIED DEFERD LH IB BRAKE TEMP. INDACATION. MEL 32-46-1D CAT C MX PROCEDURES C/W. MOC NOTIFIED. 7821 PLACARD. R & R BREAK TEMP SENSOR IAW CRJ 700 AMM 32-46-01 OPS CHECK GOOD MM02 UPDATED PLACARD REMOVED.

Part: BRACKET — CRACKED (ZONE 200) · airframe 46,115 hrs · 35,501 cycles

CRACK ON FITTING OF PAD FWD UPPER AT FS310.00 PASSENGER DOOR SURROUND STRUCTURE (L1). FITTING OF PAD FWD UPPER AT FS310.00 PASSENGER DOOR SURROUND STRUCTURE (L1) WAS REPLACED PER CRJ 700 SRM 51-42-21-001-001-A01

Part: HINGE — CORRODED (ZONE 200) · airframe 46,115 hrs · 35,501 cycles

AFT LAV SERVICE POINT DOOR HINGES AND HINGE FITTINGS HAVE CORROSION AFT LAV SERVICE POINT DOOR HINGES AND HINGE FITTINGS WERE REPLACED PER CRJ-700 AMM 52-45-01 (CONFIG A01), SRM 51-41-02-001-001-A01 AND AMM 20-21-00-910-801-A01

Part: SUPPORT PLATE — CORRODED (ZONE 100) · airframe 46,115 hrs · 35,501 cycles

CORROSION ON RH/LH MLG HYDRAULIC LINES SUPPORT PLATE (IN BK, LG EXT, LG RET) ON WHEEL WELL AREA, RBL 45/LBL 45. DUE TO EXCESSIVE DAMAGE RH/LH MLG HYDRAULIC LINES SUPPORT PLATE (IN BK, LG EXT, LG RET) ON WHEEL WELL AREA, RBL 45/LBL 45 WERE REPLACED PER CRJ 700 SRM 51-10-06-001-001-A01 AND SRM 51-41-02-001-001-A01

Part: SKIN — CRACKED (ZONE 500) · airframe 46,115 hrs · 35,501 cycles

CRACK ON SLOT OF TRACK 2 OF SLAT 1 AT FIXED LEADING EDGE LH WING CRACK ON SLOT OF TRACK 2 OF SLAT 1 AT FIXED LEADING EDGE LH WING

Part: FLOOR SUPPORT — CORRODED (BS 310-349) · airframe 41,258 hrs · 30,887 cycles

MULTIPLE AREAS OF CORROSION ON PAX DOOR FLOOR SUPPORT ANGLE. - REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT AFT CAP ANGLE, FWD CAP ANGLE, MID CAP ANGLE, AFT CLOSING FITTING, FWD CLOSING FITTING, AFT HANDRAIL FITTING, FWD HANDRAIL FITTING AND KICKPLATE ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-41-00-001-001-A01, 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.

Part: FITTING — CORRODED (BS 310-349) · airframe 41,258 hrs · 30,887 cycles

MULTIPLE AREAS OF CORROSION ON PAX DOOR FLOOR SUPPORT ANGLE. - REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT AFT CAP ANGLE, FWD CAP ANGLE, MID CAP ANGLE, AFT CLOSING FITTING, FWD CLOSING FITTING, AFT HANDRAIL FITTING, FWD HANDRAIL FITTING AND KICKPLATE ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-41-00-001-001-A01, 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 310-349) · airframe 41,258 hrs · 30,887 cycles

MULTIPLE AREAS OF CORROSION ON PAX DOOR FLOOR SUPPORT ANGLE. - REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT AFT CAP ANGLE, FWD CAP ANGLE, MID CAP ANGLE, AFT CLOSING FITTING, FWD CLOSING FITTING, AFT HANDRAIL FITTING, FWD HANDRAIL FITTING AND KICKPLATE ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-41-00-001-001-A01, 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 310-349) · airframe 41,258 hrs · 30,887 cycles

MULTIPLE AREAS OF CORROSION ON PAX DOOR FLOOR SUPPORT ANGLE.- REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT AFT CAP ANGLE, FWD CAP ANGLE, MID CAP ANGLE, AFT CLOSING FITTING, FWD CLOSING FITTING, AFT HANDRAIL FITTING, FWD HANDRAIL FITTING AND KICKPLATE ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-41-00-001-001-A01, 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.

Part: FITTING — CORRODED (BS 310-349) · airframe 41,258 hrs · 30,887 cycles

MULTIPLE AREAS OF CORROSION ON PAX DOOR FLOOR SUPPORT ANGLE. - REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT AFT CAP ANGLE, FWD CAP ANGLE, MID CAP ANGLE, AFT CLOSING FITTING, FWD CLOSING FITTING, AFT HANDRAIL FITTING, FWD HANDRAIL FITTING AND KICKPLATE ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-41-00-001-001-A01, 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.

Part: FITTING — CORRODED (BS 310-349) · airframe 41,258 hrs · 30,887 cycles

MULTIPLE AREAS OF CORROSION ON PAX DOOR FLOOR SUPPORT ANGLE. - REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT AFT CAP ANGLE, FWD CAP ANGLE, MID CAP ANGLE, AFT CLOSING FITTING, FWD CLOSING FITTING, AFT HANDRAIL FITTING, FWD HANDRAIL FITTING AND KICKPLATE ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-41-00-001-001-A01, 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 310-349) · airframe 41,258 hrs · 30,887 cycles

MULTIPLE AREAS OF CORROSION ON PAX DOOR FLOOR SUPPORT ANGLE. - REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT AFT CAP ANGLE, FWD CAP ANGLE, MID CAP ANGLE, AFT CLOSING FITTING, FWD CLOSING FITTING, AFT HANDRAIL FITTING, FWD HANDRAIL FITTING AND KICKPLATE ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-41-00-001-001-A01, 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.

Part: FITTING — CORRODED (BS 310-349) · airframe 41,258 hrs · 30,887 cycles

MULTIPLE AREAS OF CORROSION ON PAX DOOR FLOOR SUPPORT ANGLE. - REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT AFT CAP ANGLE, FWD CAP ANGLE, MID CAP ANGLE, AFT CLOSING FITTING, FWD CLOSING FITTING, AFT HANDRAIL FITTING, FWD HANDRAIL FITTING AND KICKPLATE ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-41-00-001-001-A01, 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 319-349 S19R) · airframe 41,258 hrs · 30,887 cycles

SERVICE DOOR INTERCOSTAL AT STGR 19R IS CORRODED FROM FS 310 TO FS 349 - REMOVED AND REPLACED INTERCOSTAL P/N SH670-32047-1, FS 310 - FS 319 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND INTERCOSTAL P/N SH670-32004-1, FS 319 - FS 349 IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 310-319 S19R) · airframe 41,258 hrs · 30,887 cycles

SERVICE DOOR INTERCOSTAL AT STGR 19R IS CORRODED FROM FS 310 TO FS 349 - REMOVED AND REPLACED INTERCOSTAL P/N SH670-32047-1, FS 310 - FS 319 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND INTERCOSTAL P/N SH670-32004-1, FS 319 - FS 349 IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 581-677) · airframe 41,258 hrs · 30,887 cycles

FLOORBEAM AT RBL 9 FS 581 TO 677 HAS CORROSION ON TOP OF BEAM. - COMPLIED WITH MHIRJ REO #670-53-41-514 REV-- DATED 2021-04-09 FOR REPAIR TO FLOORBEAM @ RBL9 FS 581-FS 677. WVAC EMP STAMP #738 MTC

Part: FLOOR SUPPORT — CORRODED (BS 485-581) · airframe 41,258 hrs · 30,887 cycles

TOP OF FLOORBEAM AT FS 485.00 TO FS 581.00 LBL 9 IS CORRODED IN MULTIPLE LOCATIONS. - REMOVED CORRODED FLOOR BEAM FROM F.S.485 TO F.S.581, LBL9 AND INSTALLED NEW SERVICABLE FLOOR BEAM IAW CRJ 700 SRM 53-00-41-201-001-A01.

Part: SEAT TRACK — CORRODED (BS 485) · airframe 41,258 hrs · 30,887 cycles

SEAT TRACK AT RBL 9 BEGINNING AT APPROX FS 485.00 CORRODED IN SEVERAL LOCATIONS. - REMOVED & REPLACED SEAT TRACK AT RBL 9 FS 485 TO FS 581 PN SH670-33426-1 IAW CRJ 700 AMM 53-00-49-000/400-801-A17-A03. WVAC EMP STAMP #712 MTC

Part: SEAT TRACK — CORRODED (BS 581) · airframe 41,258 hrs · 30,887 cycles

SEAT TRACK AT RBL 9 BEGINNING AT APPROX FS 581.00 CORRODED IN SEVERAL LOCATIONS. - REMOVED & REPLACED SEAT TRACK AT RBL 9 FS 581 PN SH670-33425-3 IAW CRJ 700 AMM 53-00-49-000/400-801-A17-A03.WVAC EMP STAMP #712 MTC

Part: SEAT TRACK — CORRODED (BS 785) · airframe 41,258 hrs · 30,887 cycles

LH SIDE SEAT TRACK BEGINNING AT APPROX FS 785 CORRODED IN SEVERAL LOCATIONS. - REMOVED AND REPLACED TRACK IAW CRJ 700 AMM 53-00-49-400-801(A17) WVAC EMP STAMP #711 MTC

Part: SEAT TRACK — CORRODED (BS 866-969) · airframe 41,258 hrs · 30,887 cycles

LH SIDE SEAT TRACK SHORT SEGMENT AND ADJACENT TRACK BEGINNING AT APPROX FS 847.00 CORRODED IN SEVERAL LOCATIONS. - REPLACED TRACK AT FSS 866-969 LH SIDE RAIL IAW CRJ 700 AMM 53-00-49-400-801-A17. CLEANED TRACK AT 847-866 IAW CRJ 700 AMM 51-26-00-120-801-A01. NO CORROSION NOTED. WVAC EMP STAMP #711 MTC

Part: CROSSBEAM — CORRODED (BS 280) · airframe 41,258 hrs · 30,887 cycles

L/H & R/H FS 280 BEAMS ARE CORRODED. - REMOVED AND REPLACED FS 280 L/H AND R/H CROSS BEAMS PT#CC 670-34175-7 AND ""J"" ANGLE PT #CC670-33292-13 IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01. REMOVED AND REPLACED L/H AND R/H FITTINGS PT PT #BA670-30068-1 BA670-30068-2 IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01. WVAC EMP STAMP #738 MTC

Part: STRINGER — CORRODED (ZONE 100) · airframe 41,258 hrs · 30,887 cycles

STRINGER 19L IS CORRODED BETWEEN FS 333 TO FS 349. - REPAIRED STR 19L BETWEEN FS 333 AND 349 IAW ENDEAVOR AIR EA# CRJ 753-11283 DATED 3/2/21. WVAC EMP STAMP #703 MTC

Part: SEAT TRACK — CORRODED (BS 830 RBL 9) · airframe 41,258 hrs · 30,887 cycles

SEAT TRACK AT RBL 9 BEGINNING AT APPROX FS 830.00 CORRODED IN SEVERAL LOCATIONS. - INSTALLED NEW SEAT TRACK PT #SH670-37411-3 AT FS 830.00 TO FS 696+8 RBL9 IAW CRJ 700 AMM 53-00-49-400-801-A17. FIXED 3 EACH SCREWS THAT WERE NOT FULLY ENGAGED AND ATTACHED TECH DATA. WVAC EMP STAMP #738 MTC

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 41,258 hrs · 30,887 cycles

L/H FS 280 WEB IS CORRODED. - REMOVED FABRICATED, LOCATED, DRILLED AND INSTALLED FS280 LOWER WEB AN SPLICE ON LH BULKHEAD IAW CRJ 700 SRM 53-11-10-201-004-A01. 908.1 AND 303.6 ACCEPTABLE AS IS THIS IS NOT A PRESSURE BULKHEAD.

Part: SEAT TRACK — CORRODED (BS 708-763) · airframe 41,258 hrs · 30,887 cycles

RH SIDE SEAT TRACK BEGINNING AT APPROX. FS 785.00 CORRODED IN SEVERAL LOCATIONS. - LOCATED, DRILLED AND INSTALLED NEW SEAT TRACK RH SIDE FS 785.00 IAW CRJ 700 SRM 51-40-11-001-001-A01, 53-00-49-201-002-A01, REO 670-53-00-343 REV-N DATED 2019-07-16 AND CRJ 700 AMM 53-00-49-400-801-A01. WVAC EMP STAMP #738 MTC

Part: ANGLE — CORRODED (BS 280) · airframe 41,258 hrs · 30,887 cycles

UPON REMOVAL OF FS 280 L/H LOWER WEB FOUND STIFFENER ANGLE AT LBL 17.46 TO BE DAMAGED. - REMOVED,LOCATED, AND DRILLED AND INSTALLED NEW SERVICEABLE STIFFENER ANGLE AT LBL 17.46 P/N:CC670-34151-5 IAW CRJ 700 SRM 51-40-11-001-001-A01 AND SRM 51-42-06-001-001-A01. WVAC EMP STAMP #712 MTC

Part: PLATE — CORRODED (EMERGENCY EXIT) · airframe 41,258 hrs · 30,887 cycles

R/H WING EMERGENCY EXIT STEP PLATE CORRODED. - REMOVED & REPLACED RH OVERWING STEP PLATE IAW CRJ 700 SRM 51-42-02-001-001-A01.

Part: INTERCOSTAL — DAMAGED (BS 265-280) · airframe 41,258 hrs · 30,887 cycles

2 INTERCOSTALS BETWEEN FS 265-FS 280 BETWEEN LBL 18 TO LBL 27 UNDER FLIGHT COMPARTMENT FLOOR AFT HOLES ARE DAMAGED. - REPAIRED LBL 38.50 INTERCOSTAL IAW ENDEAVOR AIR ENDEAVOR AIR EA CRJ 753-11254. INSTALLED NEW SERVICEABLE FASTENER ON AFT HOLE OF LBL 27 IAW CRJ 700 SRM 51-42-06-001-001-A01. WVAC EMP #574786

Part: SEAT TRACK — CORRODED (BS 860 LBL 9) · airframe 41,258 hrs · 30,887 cycles

SEAT TRACK AT LBL 9 BEGINNING AT APPROX FS 830.00 CORRODED IN SEVERAL LOCATIONS. - REMOVED/INSTALLED SEAT TRACK AT LBL 9 FS 830+8 TO 985+3 IAW CRJ 700 AMM 53-00-49-000/400-801-A17. WVAC EMP STAMP #712 MTC

Part: FLOORBEAM — CRACKED (BS 280) · airframe 41,258 hrs · 30,887 cycles

DURING REPAIR OF R/H FLIGHT DECK DOOR POST, FOUND R/H FLIGHT DECK FLOOR BEAM ANGLE CRACKED. - REMOVED, LOCATED,DRILLED,AND INSTALLED RH FLOOR BEAM (FLIGHT DECK) ANGLE AND GUSSET P/N:CC670-33199-3,CC670-33467-2 IAW CRJ 700 SRM 57-42-06-001-001-A01,51-40-11-001-001-A01,51-42-21-001-001-A01. WVAC EMP STAMP #712 MTC

Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 41,258 hrs · 30,887 cycles

LH SIDE SEAT TRACK BEGINNING AT APPROX FS 485.00 CORRODED IN SEVERAL LOCATIONS. - INSTALLED L/H SIDE SEAT TRACK IAW CRJ 700 AMM 53-00-49-400-801-A17, SEAT TRACK P/N: SH670-32234-3. WVAC EMP STAMP #738 MTC

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 41,258 hrs · 30,887 cycles

SEAT TRACK AT LBL 27 BEGINNING AT APPROX FS 349.00 CORRODED IN SEVERAL LOCATIONS. - REMOVED AND REPLACED SEAT TRACK IAW CRJ 700 AMM 53-00-49-400-801-A17. FABBED PER REO 670-53-00-343 REV N DATED 2019-07-16. WVAC EMP STAMP #711 MTC

Part: SEAT TRACK — CORRODED (BS 677-863) · airframe 41,258 hrs · 30,887 cycles

SEAT TRACK AT RBL 9 BEGINNING AT APPROX AT RBL 9 BEGINNING AT APPROX AT RBL 9 BEGINNING AT APPROX FS 677.00 CORRODED IN SEVERAL LOCATIONS. - REMOVED AND REPLACED SEAT TRACK IAW CRJ 700 AMM 53-00-49-400-801-A17.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 41,258 hrs · 30,887 cycles

DURING REPAIR OF L/H FLIGHT DECK DOOR POST, FOUND L/H FLIGHT DECK FLOOR BEAM ANGLE CRACKED. - REMOVED LH FLIGHT DECK FLOORBEAM ANGLE IAW CRJ 700 SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE ANGLE PN CC670-33199-48 IAW CRJ 700 SRM 51-40-11-001-001-A01. LOCATED AND DRILLED NEW GUSSET PN CC670-33467-1. INSTALLED FLOORBEAM ANGLE AND GUSSETT ON LH FLIGHT DECK FLOORBEAM IAW CRJ 700 SRM 51-42-06-001-001-A01 AND SRM 57-42-21-001-001-A01. WVAC EMP STAMP #703 MTC

Part: ANGLE — CORRODED (FLOOR SILL) · airframe 41,258 hrs · 30,887 cycles

FLOOR SILL CLIP AT RBL 42 FS 319.70 IS CORRODED. - REMOVED AND REPLACED CORRODED FLOOR SILL ANGLE AT RBL 42 FS 319.70 WITH NEW SERVICEABLE ANGLE PN SH670-32177-1 IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. WVAC EMP #83534

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 41,258 hrs · 30,887 cycles

LH SIDE SEAT TRACK BEGINNING AT F.S. 579.00 CORRODED IN SEVERAL LOCATIONS. - INSTALLED L/H SIDE SEAT TRACK FROM FS 379 TO FS 485 IAW CRJ 700 AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 579) · airframe 41,258 hrs · 30,887 cycles

LH SIDE SEAT TRACK BEGINNING AT F.S. 579.00 CORRODED IN SEVERAL LOCATIONS. - INSTALLED L/H SIDE SEAT TRACK FROM FS 379 TO FS 485 IAW CRJ 700 AMM 53-00-49-400-801-A03. WVAC EMP STAMP# 780 MTC

Part: SEAT TRACK — CORRODED (BS 708) · airframe 41,258 hrs · 30,887 cycles

LH SIDE SEAT TRACK BEGINNING @ APPROX FS708 CORRODED IN SEVERAL AREAS - REMOVED AND REPLACED SEAT TRACK IAW CRJ 700 AMM 53-00-49-000/400-801-A03.

Part: SEAT TRACK — CORRODED (BS 581) · airframe 41,258 hrs · 30,887 cycles

RH SIDE SEAT TRACK BEGINNING AT APPROX FS 581.00 CORRODED IN SEVERAL LOCATIONS. - REMOVED AND REPLACED R/H SIDE SEAT TRACK BEGINNING AT APPROX. FS 581.00 IAW AMM 53-00-49-000-801 AND 53-00-49-400-801(A17). WVAC EMP #460661

Part: SEAT TRACK — CORRODED (BS 485) · airframe 41,258 hrs · 30,887 cycles

RH SIDE SEAT TRACK BEGINNING AT APPROX FS 485.00 CORRODED IN SEVERAL LOCATIONS. - INSTALLED NEW SEAT RH RAIL @ FS 483-573 R/H IAW CRJ 700 AMM 53-00-49-400-801-A17. WVAC EMP #89523

Part: SEAT TRACK — CORRODED (BS 969) · airframe 41,258 hrs · 30,887 cycles

RH SIDE SEAT TRACK BEGINNING AT APPROX FS 969.00 CORRODED. - INSTALLED RH SEAT TRACK BEGINING APPROX FS 969.00 IAW CRJ 700 AMM 53-00-49-400-801(A17.) WVAC EMP STAMP #712 MTC

Part: NUT PLATE — CORRODED (ZONE 100) · airframe 41,258 hrs · 30,887 cycles

NUTPLATE ASSY FORWARD SIDE OF FS 364 STR 27 CORRODED. - REPLACED CORRODED NUTPLATE ASSY IAW CRJ 900 SRM 51-42-06-001-001-A01 AND DRAWING #SH670-32456, 2024 T3 0.032". WVAC EMP #460661

Part: FLOOR SUPPORT — CORRODED (BS 280-319.7) · airframe 41,258 hrs · 30,887 cycles

FLOOR SILL PLATE AT RBL 42 IS CORRODED BETWEEN FS 310.00 AND FS 319.70 - REMOVED, LOCATED, DRILLED AND INSTALLED FLOOR SILL AT RBL 42 FS 280 - FS 319.70 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01,51-42-21-001-001-A01 AND 51-42-13-001-001-A01. WVAC EMP STAMP #712 MTC

Part: SEAT TRACK — CORRODED (BS 708-763) · airframe 41,258 hrs · 30,887 cycles

RH SIDE SEAT TRACK BEGINNING AT APPROX. FS 708.00 CORRODED IN SEVERAL LOCATIONS. - INSTALLED SIDEWALL SEAT RAIL @ FS 708.0-763.0 RH STR 15 IAW CRJ 700 AMM 53-00-49-400-801-A17. WVAC EMP #89351

Part: BRACKET — DENTED (R AILERON FAIRIN) · airframe 41,258 hrs · 30,887 cycles

R/H AILERON CENTER SUPPORT FAIRING BRACKET DENTED/BENT. - INSTALLED NEW RIB P/N: CC620-13022-2 ON R/H AILERON IAW CRJ 700 SRM 51-42-001-001-A01 REV.38 DATED JUL 25/2020. WVAC EMP #460661

Part: SEAT TRACK — CORRODED (BS 677) · airframe 41,258 hrs · 30,887 cycles

LH SIDE SEAT TRACK BEGINNING AT APPROX FS 677.00 CORRODED IN SEVERAL LOCATIONS. - INSTALLED SIDE WALL SEAT RAIL AT STR 15L FS 677 IAW CRJ 700 AMM 53-00-49-400-801-A17. WVAC EMP #89351

Part: SEAT TRACK — CORRODED (BS 677) · airframe 41,258 hrs · 30,887 cycles

RH SIDE SEAT TRACK BEGINNING AT FS 677.00 CORRODED IN SEVERAL LOCATIONS. - INSTALLED SIDE WALL SEAT RAIL AT FS 677-FS 730 STR 15R IAW CRJ 700 AMM 53-00-49-400-801-A17. WVAC EMP #89351

Part: SEAT TRACK — CORRODED (BS 379) · airframe 41,258 hrs · 30,887 cycles

RH SIDE SEAT RAIL BEGINNING @ FS 379 CORRODED IN SEVERAL LOCATIONS. - INSTALLED R/H SIDE SEAT RAIL AND SUPPORT STRUCTURE FROM FS 379 TO FS 483 IAW CRJ 700 AMM 53-00-49-400-801CONFIG A17). WVAC EMP STAMP #712 MTC

Part: SEAT TRACK — CORRODED (BS 581-679 LBL9) · airframe 41,258 hrs · 30,887 cycles

SEAT TRACK AT LBL 9 BEGINNING AT FS 581.00 CORRODED IN SEVERAL LOCATIONS. - REMOVED AND REPLACED SEAT TRACK AT LBL9 FS 581-677 IAW CRJ 700 AMM 53-00-400-801-A17. WVAC EMP #89351

Part: SEAT TRACK — CORRODED (BS 581) · airframe 41,258 hrs · 30,887 cycles

RH SIDE SEAT TRACK BEGINNING AT APPROX FS 581.00 CORRODED IN SEVERAL LOCATIONS. - REMOVED AND REPLACED R/H SIDE SEAT TRACK BEGINNING AT APPROX. FS 581.00 IAW AMM 53-00-49-000-801 AND 53-00-49-400-801(A17).

Part: FLOORBEAM — CORRODED (BS 280) · airframe 41,258 hrs · 30,887 cycles

FLOORBOARD SUPPORT ANGLE IS CORRODED AT F.S. 280, STGR 27. - REMOVED AND REPLACED SUPPORT ANGLE IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01. WVAC EMP STAMP# 711 MTC

Part: STRINGER — CORRODED (BS 333-349 S23L) · airframe 41,258 hrs · 30,887 cycles

STRINGER 23L IS CORRODED BETWEEN FS 333 TO FS 349. - REPAIRED STR 23L FROM FS 333-354 IAW CRJ 700 SRM 53-00-03-201-001-A01. REMOVED AND REINSTALLED IAPS CARD CAGE FOR ACCESS IAW CRJ 700 AMM 22-12-01-000/400-801-A01. PERFORMED SELF TEST OF IAPS IAW CRJ 700 AMM 22-12-00-740-801-A01. NO DEFECTS NOTED. WVAC EMP STAMP #703 MTC

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 41,258 hrs · 30,887 cycles

SERVICE DOOR UPPER FLOOR SILL ANGLE IS CORRODED ON O/B EDGE. - LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE FLOOR SILL ANGLE P/N SH670-31986-1 AND MOUNTING ANGLE P/N SH670-31996-35 IAW CRJ 700 SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01. WVAC EMP STAMP #703 MTC

Part: SEAT TRACK — CORRODED (BS 969) · airframe 41,258 hrs · 30,887 cycles

LH SIDE SEAT TRACK BEGINNING AT APPROX FS 969.00 CORRODED IN SEVERAL LOCATIONS. - REMOVED/INSTALLED LH SEAT TRACK @ FS953+7-985+3 IAW CRJ 700 AMM 53-00-49-000/400-801-A17. WVAC EMP STAMP #712 MTC

Part: ANGLE — CORRODED · airframe 41,258 hrs · 30,887 cycles

LEFT & RIGHT INTERNAL REAR SPAR (FS 693) AUX SECTION (BLOWOUT PANEL) HAS NUMEROUS CORRODED NUTPLATES IN ANGLES. L/R FWD LOWER ANGLE CORRODED. - REMOVED & REPLACED LEFT AND RIGHT TIRE BLOWOUT PANEL SUPPORT ANGLES IAW CRJ 700 SRM 51-42-21-001-001-A01.

Part: FRAME — CORRODED (BS 517 24L-25R) · airframe 41,258 hrs · 30,887 cycles

FWD CARGO COMPARTMENT FRAME AT FS 517.00 IS CORRODED BETWEEN STGR 24L AND STGR 25R. - REMOVED, LOCATED, DRILLED, AND INSTALLED FRAME AT FS 517.00 IAW CRJ 700 SRM 51-42-06-001-001-A01. WVAC EMP STAMP #712 MTC

Part: STRIKER — CORRODED (BS 310-349) · airframe 41,258 hrs · 30,887 cycles

SERVICE DOOR LOWER SEAL STRIKER HAS CORROSION AROUND FASTENER HOLES. - REMOVED/REPLACED SERVICE DOOR SEAL STRIKE IAW CRJ700 AMM 51-42-06-001-001-A01 AND INSTALLED SERVICE DOOR STOPS IAW CRJ700 AMM'S 53-21-27-400-802(A01) THEN PERFORMED LEAK/OPS CHECK IAW CRJ700 AMM 52-00-00-790-801(A01)/ 52-41-00-710-801(A01). WVAC EMP #585987

Part: INTERCOSTAL — CORRODED (FWD AVIONICS BAY) · airframe 41,258 hrs · 30,887 cycles

FWD AVIONICS BAY DOOR INTERCOSTAL IS CORRODED BETWEEN STGR 26L TO 25L. - INTERCOSTAL FOUND TO BE OUT OF LIMITS IAW CRJ 700 SRM 53-21-23-101-003-A01. LOCATED AND DRILLED SERVICEABLE INTERCOSTAL IAW CRJ 700 SRM 51- 40-11-001-001-A01. INSTALLED SERVICEABLE INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. WVAC EMP STAMP #703 MTC

Part: INTERCOSTAL — CORRODED (BS 333-349 S20L) · airframe 41,258 hrs · 30,887 cycles

PAX DOOR INTERCOSTAL BETWEEN FS 333 TO FS 349 AT STGR 20L IS CORRODED. - REMOVED UNSERVICEABLE PAX DOOR INTERCOSTAL BETWEEN FS 333 TO FS 349 AT STR 20L IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED, DRILLED AND INSTALLED A NEW SERVICEABLE INTERCOSTAL BETWEEN FS333 TO FS349 AT STR 20L P/N SH670-31823-15 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-40-41-001-001-A01 WVAC EMP STAMP #703 MTC

Part: INTERCOSTAL — CORRODED (BS 364 S26-27L) · airframe 41,258 hrs · 30,887 cycles

AVIONICS BAY DOOR FWD INTERCOSTAL IS CORRODED BETWEEN STGR 27 TO 26L. - REMOVED AND REPLACED AVIONICS BAY DOOR FWD INTERCOSTAL IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. WVAC EMP # 585987

Part: LIGHT — DETACHED (CABIN FLOOR) · airframe 40,288 hrs · 29,981 cycles

EMERGENCY FLOOR LIGHTING IS COMMING OFF THE FLOOR IN FRONT OF THE CLOSET "REPLACED EMERGENCY FLOOR LIGHTING IN FRONT OF THE CLOSET PER CMM 33-51-07 NO FURTHER DEFECTS NOTED AT THIS TIME "

Part: DOOR — DAMAGED (CABIN) · airframe 37,513 hrs · 27,424 cycles

PAX DOOR WILL NOT OPEN ALL THE WAY FERRY FLT FROM KDTW TO KSTL. REPAIRED PAX DOOR IAW REO 670-52-11-1027.

Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR) · airframe 37,346 hrs · 27,262 cycles

PAX DOOR LATCH CAUTION WITH A PAX DOOR WARNING. PERFORMED AN OPS CHECK OF THE PAX DOOR IAW AMM 52-11-00, AND PERFORMED OPS CHECK OF THE PAX DOOR WARNING INDICATION SYS IAW 52-70-04 , NO MESSAGE NOTED.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 37,338 hrs · 27,254 cycles

VERTICAL STABILIZER RT FWD AND AFT DRAG ANGLES CRACKED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-55-31-018 REV A DATED 2016-11-10, REO 670-55-31-106 REV.-- DATED 2018-06-06 AND NDTM PART1 51-20-006.

Part: ARM — GOUGED (CARGO DOOR) · airframe 37,338 hrs · 27,254 cycles

FWD CARGO FWD AND AFT COUNTER BALANCE ARMS HAVE GOUGES ON THE O/B SURFACES. CORRECTIVE ACTION: REOAIRED FWD CARGO FWD AND AFT COUNTERBALANCE ARMS IAW NDT MANUAL PART 1 51-20-006, SRM 52-35-09, 21-24-11 AND REO 670-52-35-350 REV - DATED 2018-06-12.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 37,338 hrs · 27,254 cycles

VERTICAL STABILIZER LT FWD AND AFT DRAG ANGLES ARE CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-55-31-018, REV A DATED 2016-11-10, AND REO 670-55-31-106 DATED 2018-06-06.

Part: SKIN — GOUGED (FUSELAGE) · airframe 37,338 hrs · 27,254 cycles

AFT LOWER FUSELAGE BETWEEN FS 969.00 AND 977.00 THERE ARE MULTIPLE GOUGES. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-53-00-547 DATED 2018-06-11, AND F670-53-00-547(P1) DATED 2018-06-05.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 37,338 hrs · 27,254 cycles

AFT CARGO DOOR FWD TRACK MID CHANNEL CRACKED AT FS 1000 STGR 13L. CORRECTIVE ACTION: REMOVED AND REPLACED AFT CARGO DOOR FWD TRACK MID CHANNEL AT FS 1000 STGR 13 L IAW SRM 51-42-06.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 37,338 hrs · 27,254 cycles

PASSENGER DOOR INTERCOSTAL DD6 IS CRACKED. REMOVED AND REPLACED INTERCOSTAL DD6(PN:601R-31902-485) IAW SRM 51-42-06, AND 51-40-11.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 37,338 hrs · 27,254 cycles

RIGHT HAND F.S. 280.00 CROSSBEAM IS CORRODED AND CRACKED. CORRECTIVE ACTION REMOVED AND REPLACED RT F.S. 280.00 CROSSBEAM(PN CC670-34175-7S) IAW REO 670-53-11-1398 DATED 07 JUN 2018, NDT MANUAL PART 1 51-20-006, SRM 53-11-41, 51-25-21, 51-21-11, 51-42-06, 51-42-21, 51-42-13, 51-40-11, AND AMM 20-70-00.

Part: CLEAT — CORRODED (PAX DOOR) · airframe 37,338 hrs · 27,254 cycles

PASSENGER DOOR INTERCOSTAL DD6 CLEAT IS CORRODED. REMOVED AND REPLACE CLEAT (PN:600-31902-269) IAW SRM 51-42-06, AND 51-40-11.

Part: SUPPORT BRACKET — CRACKED (LT SLAT TRACK) · airframe 37,338 hrs · 27,254 cycles

LEFT SLAT TRACK 1 - 3 HOUSING BRACKET CRACKED. REPAIRED THE LT SLAT TRACK 1-3 HOUSING BRACKET IAW REO 670-57-42-577, REV -, NDTM PART 1, 51-20-006, AND SRM 51-26-00.

Part: CLEAT — CORRODED (PAX DOOR) · airframe 37,338 hrs · 27,254 cycles

PAX DOOR INTERCOSTAL DD4 HAS AN INBOARD CLEAT SHOWING SIGNS OF CORROSION. REMOVED AND REPLACED IAW SRM 51-42-06, 51-42-21, AND 51-40-11

Part: BRACKET — CRACKED (PAX DOOR) · airframe 37,338 hrs · 27,254 cycles

UPPER BRACKETS UNDER THE COVER PLATE ON THE PAX DOOR WERE CRACKED. REMOVED AND REPLACED THE BRACKETS IAW SRM 51-41-02.

Part: ANGLE — CORRODED (BS 280 FLOORBEAM) · airframe 37,338 hrs · 27,254 cycles

FLOORBEAM ANGLE AT BS 280 HAD SIGNS OF CORROSION. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-13, 51-42-06, AND 51-42-21.

Part: SHELF — CRACKED (ZONE 200) · airframe 37,338 hrs · 27,254 cycles

JB6 MOUNTING SHELF HAD A CRACK AT THE FWD OTBD CORNER. REMOVED AND REPLACED THE MOUNTING SHELF IAW SRM 51-42-06.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,338 hrs · 27,254 cycles

PASSENGER DOOR INTERCOSTAL DD7 ANGLE CORRODED. REPLACED THE INTERCOSTAL ANGLE IAW SRM 51-40-11, AND 51-42-06.

Part: STRUCTURE — CRACKED (E/E BAY) · airframe 37,338 hrs · 27,254 cycles

FWD EQUIPMENT COMPARTMENT LOWER STUCTURE CRACKED JUST OTBD OF ADG STOWING MANIFOLD. REPAIRED IAW REO 670-53-11-509, REV D, AND REO 670-53-11-1397, REV-.

Part: RETAINER — GOUGED (FWD CARGO DOOR) · airframe 37,338 hrs · 27,254 cycles

FORWARD CARGO DOOR LOWER SEAL RETAINER WAS DENTED AND GOUGED. REPAIRED THE SEAL RETAINER IAW REO 670-52-35-127, REV --, SRM 51-21-11, 51-26-06, 51-25-16, AND NDTM, PART 1, 51-20-006.

Part: ANGLE — CORRODED (BS 939) · airframe 37,338 hrs · 27,254 cycles

AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE ANGLE AT BS 939 WAS CORRODED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06, 51-40-11, 51-45-00, AND 51-25-16.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 37,338 hrs · 27,254 cycles

FWD AND AFT PULL IN CAM DOUBLERS WERE CRACKED ON THE PAX DOOR. REMOVED AND REPLACED THE CAM DOUBLERS IAW SRM 51-40-11, 51-25-16, 51-42-06, 51-40-00, AND 51-42-21.

Part: FORMER — CORRODED (PAX DOOR) · airframe 37,338 hrs · 27,254 cycles

PASSENGER DOOR FWD FORMER AT LOWER CAM HAS SIGNS OF CORROSION. REMOVED AND REPLACED FWD FORMER FS 311.75 IAW SRM 51-42-06 AND 51-42-21.

Part: SKIN — DENTED (TE FLAP) · airframe 37,338 hrs · 27,254 cycles

RT I/B FLAP BOTTOM SURFACE HAS MULTIPLE DENTS. REPAIRED RT I/B FLAP BOTTOM SURFACE IAW REO 670-57-52-160 REV A, DATED 2016-10-21.

Part: SKIN — CORRODED (ZONE 800) · airframe 37,338 hrs · 27,254 cycles

SIGNS OF CORROSION ON INTERNAL SKIN BENEATH ACCESS PANEL 832FL. REMOVED AND REPLACED INNER SKIN IAW SRM 51-41-02, 51-42-06, 51-42-13, 51-42-21, 51-42-22 AND REO 670-52-11-1020 DATED 2018-06-05.

Part: COVER — UNSECURE (ESCAPE ROPE) · airframe 35,704 hrs · 25,746 cycles

ESCAPE HANDLE COVER AT ROW 12AB WILL NOT STAY ATTACHED. SECURED THE ESCAPE ROPE COVER IAW IAW AMM 20-51-00.

Part: DOOR SEAL — DEFECTIVE (EMERGENCY EXIT) · airframe 33,818 hrs · 24,233 cycles

EMERGENCY EXIT HISSING IN FLIGHT AT 12A. R & R THE OVERWING EMERGENCY EXIT VENT PLATE SEAL IAW AMM 52-21-03. OPS CHECK GOOD. ACFT OK FOR SERVICE.

Part: COVER — MISSING (CABIN) · airframe 33,577 hrs · 24,054 cycles

RT EMERGENCY LIGHT COVER UNDER FLASHLIGHT IN FWD GALLEY MISSING. INSTALLED COVER IAW AMM 33-51-11. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: WARNING LIGHT — FALSE INDICATION (PAX DOOR) · airframe 33,494 hrs · 23,997 cycles

INTERMITTENT PAX DOOR OUTER HANDLE LIGHT IN FLIGHT. PERFORMED OPS CHECK OF PAX DOOR OUTER HANDLE IAW 52-11-03 NO DEFECT NOTED AT THIS TIME.

Part: WARNING MESSAGE — ILLUMINATED (PAX DOOR HANDLE) · airframe 33,484 hrs · 23,989 cycles

PAX DOOR OUTER HANDLE CAUTION MESSAGE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,986 hrs · 23,614 cycles

FUSELAGE RT FRAME FS 235 HA & INDICATION OF 3 INCHES LONG PROPAGATING FROM THE RADIUS AT STRINGER 13A, FAILED NDT.

Part: DOOR — NOISY (CABIN) · airframe 32,961 hrs · 23,593 cycles

PASSENGER DOOR SQUEAL. PERFORMED PRESSURIZATION OF ACFT IAW AMM 21-31-00. OPERATIONS CHECKED GOOD. HAD MECHANIC OUTSIDE PAX DOOR TO CHECK FOR LEAKS, NONE NOTED. NO SOUNDS IN ACFT. OK FOR SERVICE. INSPECTED DOOR SEAL, NO DEFECTS NOTED.

Part: FLOOR SUPPORT — CORRODED (BS 1000-1051) · airframe 32,921 hrs · 23,569 cycles

COROSION FOUND ON FLOOR SUPPORT LBL 9.0 BETWEEN FS 1000 AND 1051. COMPLIED WITH REO 670-53-00-029.

Part: FLOOR SUPPORT — CORRODED (BS 1015-1051) · airframe 32,921 hrs · 23,569 cycles

FLOOR SUPPORT CORRODED BEYOND ALLOWABLE LIMITS AT LBL 27, BS 1015 - 1051.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 32,627 hrs · 23,359 cycles

SMELL OF SOMETHING ELECTRICALLY HOT ON THE FLIGHT DECK. INSPECTED FLIGHT DECK FOR ANY SIGNS OF ELECTRICAL OVERHEAT & ANY BURNING SMELL IAW AMM 05-21-00. NO DEFECTS NOTED AT THIS TIME.

Part: DOOR — NOISY (CABIN) · airframe 32,627 hrs · 23,359 cycles

LOUD HIGH SQUEAL FROM THE MAIN CABIN DOOR. INSPECTED MAIN DOOR & MAIN DOOR SEAL FOR PROPER OPERATION. MAIN DOOR OPENS & CLOSES NORMALLY. DETERMINED ACFT SAFE FOR A ONE TIME FERRY FLIGHT.

Part: STEP — CRACKED (PAX DOOR) · airframe 32,621 hrs · 23,355 cycles

PASSENGER DOOR BOTTOM STEP CRACKED. REMOVED, REPAIRED, & REINSTALLED PAX DOOR BOTTOM STEP IAW AMM 51-22-81 & 52-11-04.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 32,621 hrs · 23,355 cycles

FORWARD CARGO DOOR SHOWING SIGNS OF CORROSION NEAR STRINGER 22L, AT FRAME STATION 533.00. CUT OUT DAMAGED AREA, INSTALLED NEW STRINGER, PN SH670-33223-1, IAW SRM 53-00-03, 51-21-06, 53-31-06, 51-26-00, 51-25-06, 51-25-16, 53-00-00, 51-42-06, 51-42-13, 51-21-11 & AMM 51-21-01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 32,621 hrs · 23,355 cycles

INBOARD INTERCOSTAL, AT FWD MAIN AVIONICS DOOR SURROUND AT FS 364, SIGNS OF CORROSION. R & R INBD INTERCOSTAL IAW SRM 51-41-02, 51-40-11 & 51-42-21.

Part: RIB — CRACKED (LT WING) · airframe 32,621 hrs · 23,355 cycles

LEFT WING FIXED LE RIB AT STRINGER 27.75 IS CRACKED. CUT OUT DAMAGED AREA. ACCOMPLISHED REPAIR IAW REO 670-57-42-611, DATED 20 JAN 2016. WO 80364, WC 5067.

Part: DOOR — DENTED (CABIN) · airframe 32,621 hrs · 23,355 cycles

PASSENGER DOOR HAS DENT. REPAIRED PAX DOOR BY CUTTING OUT DAMAGE, FABRICATING & INSTALLING REPAIR PARTS IAW REO 670-52-11-868 DATED 21JAN 2016.

Part: ANGLE — CORRODED (ZONE 100) · airframe 32,621 hrs · 23,355 cycles

PASSENGER DOOR ENTRY FLOORBOARD MIDCAP ANGLE HAS SIGNS OF CORROSION. R & R MIDCAP ANGLE IAW AMM 21-20-00 & 51-40-11.

Part: ATTACH BRACKET — CRACKED (FAIRING)

CRACK IN ATTACH BRACKET ON AFT WING TO BODY FAIRING STRUCTURE AT FS 909.00. REPAIRED CRACK BY CUTTING OUT DAMAGE. FABRICATING REPAIR PARTS & INSTALLING IAW REO 670-53-82-478 REV A DATED 2014 11 12.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,631 hrs · 23,355 cycles

FRAME 319.70 IS CORRODED, BETWEEN STRINGER 26L & 27. REMOVED DAMAGED AREA OF FRAME & SPLICED IN NEW FRAME IAW REO 670-53-21-799 DATED 30 JAN 2012, SRM 51-42-06, 20-80-00.

Part: BEAM — CRACKED (FUSELAGE) · airframe 32,621 hrs · 23,355 cycles

LEFT & RIGHT SIDES OF FS 280.00 BEAM ARE CRACKED. R & R LT & RT SIDES OF FS 280.00 BEAM, PN CC670-34175-7S, IAW SRM 51-42-06, 51-42-13, 51-42-21, 51-40-11, 51-21-11, 51-25-16, 53-11-41 & AMM 20-70-00.

Part: COMPRESSOR BLADE — DAMAGED (NR 2 ENGINE) · airframe 32,484 hrs · 23,252 cycles

RIGHT ENG FLAME OUT ON SHORT FINAL. INSPECTED 6TH STAGE CHECK VLV, FOUND TO BE WORN. R & R CHECK VLV IAW AMM 36-11-03. BORESCOPE INSPECTION OF NR 2 ENG REQUIRED. PERFORMED BORESCOPE INSPECTION OF NR 2 ENG IAW AMM 72-32-00. FOUND DAMAGE TO 5TH STAGE COMPRESSOR BLADE. NR 2 ENG CHANGE REQUIRED. R & R NR 2 ENG IAW AMM 71-00-00. MODEL CF34-8C5B1, SN OFF E965372 & SN ON E965453.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,275 hrs · 23,092 cycles

CEILING OVERHEAD EMER LIGHT AT ROW 9 INOPERATIVE. DEFERRED EMER CEILING LIGHT AT ROW 9 IAW MEL 33-51-01B.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,336 hrs · 22,370 cycles

OVERHEAD EMER LIGHT AT ROW 15 INOPERATIVE. RELAMPED EMER FLOOD LIGHT IAW AMM 33-51-11. OPERATIONS CHECKED GOOD.

Part: DOOR — OBSTRUCTED (OVERWING EXIT) · airframe 31,297 hrs · 22,342 cycles

LEFT OVERWING EMER EXIT SQUEALS. REMOVED FOREIGN OBJECT FROM DOOR FRAME. OPERATIONS CHECKED GOOD IAW AMM 52-21-00.

Part: DOOR SEAL — OUT OF ADJUST (CABIN DOOR) · airframe 21,242 hrs · 22,296 cycles

LOUD WHISTLE COMING FROM MAIN CABIN DOOR. ADJUSTED MAIN CABIN DOOR SEAL. PERFORMED PRESSURIZATION OF ACFT IAW AMM 21-31-00. NO LOUD WHISTLE NOISE OR ANY OTHER DEFECTS NOTED AT THIS TIME. ACFT OK FOR SERVICE.

Part: DOOR — NOISY · airframe 31,242 hrs · 22,296 cycles

LOUD SQUEAL ABOVE FL 210. PERFORMED GVI & OPERATIONS CHECK OF ALL PAX & SERVICE DOORS TO ENSURE ACFT IS SAFE FOR FERRY FLIGHT. ACFT IS SAFE FOR ONE TIME FERRY FLIGHT.

Part: DOOR — NOISY (CABIN) · airframe 31,200 hrs · 22,264 cycles

LOUD WHISTLE FROM PAX DOOR IN FLIGHT. PERFORMED OPERATIONAL CHECK, NO DEFECTS NOTED. INSPECTED & FOUND SAFE FOR A ONE TIME FERRY FLIGHT.

Part: DOOR — NOISY (CABIN) · airframe 31,195 hrs · 22,261 cycles

LOUD SQUEAL FROM PAX DOOR WITH CABIN DIFFERENTIAL PRESS AT 7.2. PERFORMED PRESS CHECK IAW AMM 21-31-00. NO LEAKS NOTED.

Part: DOOR SEAL — DIRTY (PAX DOOR) · airframe 31,189 hrs · 22,258 cycles

LOUD SQUEAL FROM PAX DOOR ON DESCENT. CLEANED MAIN DOOR SEAL IAW AMM 52-11-00.

Part: DOOR — NOT CLOSED (CARGO BAY) · airframe 30,621 hrs · 21,824 cycles

CABIN ALT WARNING MSG IN FLIGHT AT 11000 FEET. UPON INSPECTION FOUND DOOR SLIGHTLY OPEN. CLOSED AFT CARGO DOOR IAW AMM 52-31-00. PRESSURIZED ACFT IAW 21-31-00. OPERATIONS CHECKED GOOD.

Part: INDICATION SYS — FALSE ACTIVATION (COCKPIT) · airframe 30,385 hrs · 21,646 cycles

LEFT EMER EXIT CAUTION. VERIFIED DOOR CLOSED, LATCHED & LOCKED. DEFERRED LT EMER EXIT DOOR INDICATION SYS IAW MEL 52-70-03 CAT C.

Part: DOOR — NOT SEATED (EMERGENCY EXIT) · airframe 30,380 hrs · 21,640 cycles

LT OVERWING EMER EXIT DOOR CAUTION MSG. RE RACKED LT EMER DOOR IAW AMM 52-21-00. OPERATIONS CHECKED GOOD.

Part: INDICATION SYS — FALSE ACTIVATION (COCKPIT) · airframe 30,271 hrs · 21,559 cycles

LEFT EMER EXIT CAUTION MSG ON TAKEOFF. DEFERRED LT EMER EXIT DOOR INDICATION IAW MEL 52-70-03 CAT C.

Part: COVER — UNSECURE (EMERGENCY EXIT) · airframe 28,095 hrs · 20,613 cycles

LEFT EMER HANDLE COVER HAS FALLEN OFF. SECURED COVER ON LT EMER EXIT DOOR IAW AMM 52-22-61. NO OTHER EFFECTS NOTED.

Part: DOOR — FAULTED (EMERGENCY EXIT) · airframe 30,234 hrs · 21,530 cycles

LEFT EMER EXIT CAUTION MSG. REMOVED & REINSTALLED LT OVERWING EMER DOOR IAW AMM 52-70-10. NO MSG AT THIS TIME.

Part: LANYARD — FRAYED (PAX DOOR) · airframe 30,150 hrs · 21,464 cycles

FORWARD PAX DOOR HANDRAIL LOCK PIN LANYARD FRAYED. SECURED PAX DOOR PIN LANYARD & DEFERRED IAW MEL 52-00-05 CAT C.

Part: TRIM PANEL — BROKEN (SERVICE DOOR) · airframe 29,851 hrs · 21,230 cycles

SERVICE DOOR HANDLE TRIM BROKEN, HARD TO CLOSE. DEFERRED SERVICE DOOR PULL HANDLE IAW NEF 25-999-1 CAT 1.

Part: INDICATION SYS — FALSE ACTIVATION (COCKPIT) · airframe 29,851 hrs · 21,230 cycles

SERVICE DOOR CAUTION MSG IN FLIGHT. DEFERRED SERVICE DOOR INDICATION IAW MEL 52-70-05 CAT C.

Part: HANDLE — NOT SEATED (SERVICE DOOR) · airframe 29,512 hrs · 20,964 cycles

SERVICE DOOR CAUTION MSG ON GND WITH DOOR CLOSED & OUTER HANDLE NOT FLUSH. SERVICE DOOR OPERATIONS CHECKED GOOD IAW AMM 52-41-01.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 29,486 hrs · 20,942 cycles

PAX DOOR OUTER HANDLE MSG. DEFERRED PAX DOOR INDICATION IAW MEL 52-70-01 CAT A.

Part: CONNECTOR — DIRTY (PAX DOOR) · airframe 29,480 hrs · 20,937 cycles

PAX DOOR OUTER HANDLE CAUTION MSG. CLEANED & SECURED PAX DOOR HARNESS CONNECTOR IAW ESPM 20-20-26. OPERATIONS CHECK COMPLIED WITH, NO FAULTS NOTED AT THIS TIME.

Part: HANDLE — OUT OF ADJUST (PAX DOOR) · airframe 29,344 hrs · 20,825 cycles

PAX DOOR OUTER HANDLE CAUTION MSG. ADJUSTED DOOR HANDLE IAW AMM 52-70-04. OPERATIONS CHECKED GOOD, OK FOR SERVICE.

Part: PANEL — LOOSE (SERVICE DOOR) · airframe 29,264 hrs · 20,758 cycles

WALL PANEL IN GALLEY LOOSE BY SERVICE DOOR. SECURED SERVICE DOOR WALL PANEL IAW 52-41-00.

Part: PLACARD — WORN (PAX DOOR) · airframe 28,741 hrs · 20,346 cycles

PAX DOOR LIFT HANDLE TO OPEN PLACARD WORN. R & R LIFT HANDLE TO OPEN PLACARD IAW AMM 20-60-04.

Part: PLACARD — WORN (PAX DOOR) · airframe 28,741 hrs · 20,346 cycles

PAX DOOR EXIT PLACARD IS WORN. R & R EXIT PLACARD IAW AMM 20-60-04.

Part: FASTENER — ABNORMAL (PAX DOOR) · airframe 28,741 hrs · 20,346 cycles

PAX DOOR STEPS HAVE MISSING & LOOSE HARDWARE. REPLACED MISSING HARDWARE & TIGHTENED LOOSE HARDWARE IAW AMM 20-21-00.

Part: SEALANT — MISSING (PAX DOOR) · airframe 28,735 hrs · 20,341 cycles

PAX DOOR WARNING ON EICAS & PX 107 MISSING SEALANT. VERIFIED PAX DOOR CLOSES & LOCKS NORMALLY WITH GREEN WITNESS MARKS ALIGNED & DEACTIVATED GND VLV IAW AMM 21-24-18. VERIFIED PX 107 SECURE, ACFT IS SAFE FOR A ONE TIME FERRY FLIGHT FROM BOS TO STL.

Part: PROXIMITY SENSOR — OUT OF ADJUST (CABIN DOOR) · airframe 28,735 hrs · 20,341 cycles

MAIN CABIN DOOR WILL NOT CLOSE. FOUND INTERMITTENT FIT BETWEEN PX 107 & OUTER DOOR HANDLE. ADJUSTED PX107 IAW AMM 52-70-04. OPERATIONS CHECKED GOOD IAW AMM 52-11-00, OPERATIONS CHECKED GOOD ON PX107, SEALANT NOT INSTALLED.

Part: INDICATOR — FADED (PAX DOOR) · airframe 26,774 hrs · 19,561 cycles

GREEN PIN INDICATOR MARKS ON MAIN DOOR FADED. DEFERRED GREEN WITNESS MARKS ON PAX DOOR IAW NEF 25-999-1 CAT 1.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,702 hrs · 20,314 cycles

STAIR LIGHTS INOPERATIVE. DEFERRED STAIR LIGHTS IAW MEL 33-21-02 CAT D.

Part: CHARGER — FAILED (CABIN) · airframe 28,689 hrs · 20,304 cycles

THE EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACKS NR 1 & NR 2 ARE INOPERATIVE. REMOVED & INSTALLED SERVICEABLE BATTERY CHARGER ASSEMBLIES NR 1 & NR 2 IAW AMM 33-51-17. OPERATIONAL CHECK GOOD IAW AMM 33-51-17 & 33-51-00.

Part: SEAL — TORN (EMERGENCY EXIT) · airframe 28,689 hrs · 20,304 cycles

RIGHT OVERWING EMERGENCY EXIT PRESS SEAL TORN. R & R RT OVERWING EMERGENCY EXIT PRESS SEAL IAW AMM 52-21-07.

Part: RETAINER — DAMAGED (PAX DOOR) · airframe 28,689 hrs · 20,304 cycles

PAX DOOR SEAL RETAINER DAMAGED. REPAIRED PAX DOOR SEAL RETAINER IAW REO 670-53-22-001 REV H DATED JUNE 10 2013.

Part: SILL — CORRODED (FUSELAGE) · airframe 28,689 hrs · 20,304 cycles

LEFT SILL FWD OF PAX DOOR AT FS 280.00 CROSSBEAM CORRODED. R & R LT SILL FWD OF PAX DOOR AT FS 280.00-310.00 IAW SRM 51-42-10, 51-42-21 & 51-42-06.

Part: PROXIMITY SWITCH — OUT OF ADJUST (EMERGENCY EXIT) · airframe 28,689 hrs · 20,304 cycles

LEFT OVERWING EMERGENCY EXIT DOOR LIGHT DOESN'T TURN AMBER WHEN OPENED. ADJUSTED LT OVERWING EMERGENCY EXIT PROXIMITY SWITCH IAW AMM 52-70-10, OPERATIONS CHECKED GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 28,689 hrs · 20,304 cycles

FUSELAGE FRAME AT FS 310 & STRINGER 25R HAS CORROSION ON FACE & BOTTOM FLANGE. CUT OUT & REMOVED DAMAGED FRAME SECTION. FABRICATED SPLICE, STRINGER CLEATS & SHIM. INSTALLED REPAIR PARTS WITH NEW FRAME SECTOR IAW REO 670-53-21-799, DATED 30 JAN 2012.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 28,689 hrs · 20,304 cycles

LEFT OTBD INTERCOSTAL FWD OF FS 369.00 CORRODED. R & R LT OTBD INTERCOSTAL FWD OF FS 369.00 IAW SRM 51-42-21.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 28,689 hrs · 20,304 cycles

RIGHT INBD INTERCOSTAL FWD OF FS 369.00 CORRODED. R & R RT INBD INTERCOSTAL FWD OF FS 369.00 IAW SRM 51-42-21.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 28,689 hrs · 20,304 cycles

NR 3 LINTEL STRINGER CRACKED. REPAIRED LINTEL NR 3 STRINGER IAW SB 670BA-53-040 DATED 11 NOV2011 & REO 670-53-21-493 REV C DATED 08 DEC 2011.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 28,689 hrs · 20,304 cycles

LEFT INBD INTERCOSTAL FWD OF FS 369.00 CORRODED. R & R LT INBD INTERCOSTAL FWD OF FS 369.00 IAW SRM 51-42-21.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 28,689 hrs · 20,304 cycles

RIGHT OTBD INTERCOSTAL FWD OF FS 369.00 CORRODED. R & R RT OTBD INTERCOSTAL FWD OF FS 369.00 IAW SRM 51-42-21.

Part: PLATE — CORRODED (SERVICE DOOR) · airframe 28,689 hrs · 20,304 cycles

SERVICE DOOR FWD FLOOR PROTECTOR PLATE CORRODED. R & R SERVICE DOOR FWD PROTECTOR PLATE IAW SRM 51-42-06.

Part: CAP — CORRODED (PAX DOOR) · airframe 28,689 hrs · 20,304 cycles

PAX DOOR MID CAP CORRODED. R & R PAX DOOR MID CAP IAW SRM 51-41-02 & 51-42-06.

Part: BRACKET — CORRODED (SERVICE DOOR) · airframe 28,689 hrs · 20,304 cycles

SERVICE DOOR 2 FWD FLOOR PROTECTOR L BRACKETS CORRODED. R & R 2 SERVICE DOOR FWD FLOOR PROTECTOR L BRACKETS IAW SRM 51-42-06, 51-25-16 & 51-21-11.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 28,689 hrs · 20,304 cycles

SERVICE DOOR SEAL STRIKER CORRODED. R & R SERVICE DOOR SEAL STRIKER IAW SRM 51-42-06, 51-25-16 & 51-21-11.

Part: SILL — CORRODED (FUSELAGE) · airframe 28,689 hrs · 20,304 cycles

RIGHT SILL FWD OF SERVICE DOOR CORRODED. R & R RT FWD SILL FWD OF SERVICE DOOR IAW SRM 51-42-13, 51-42-06, 51-40-11, 51-21-11, 51-25-16 & AMM 20-70-00.

Part: BEAM — CORRODED (FUSELAGE) · airframe 28,689 hrs · 20,304 cycles

LT & RT 280 BEAM CORRODED. R & R FS 280.00 BEAM LT & RT IAW SRM 51-42-06, 51-42-21 & 51-42-13.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 28,689 hrs · 20,304 cycles

SERVICE DOOR KICK ANGLE CORRODED. R & R SERVICE DOOR KICK ANGLE IAW SRM 51-42-06.

Part: WEB — CORRODED (FUSELAGE) · airframe 28,689 hrs · 20,304 cycles

RIGHT WEB AT FS 280.00 CROSSBEAM CORRODED. REPAIRED RT WEB AT 280.00 CROSSBEAM IAW 670-53-11-594 DATED 4/27/2011 REV.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 28,689 hrs · 20,304 cycles

PAX DOOR KICK ANGLE CORRODED. R & R PAX DOOR KICK ANGLE IAW SRM 51-42-06 & 51-42-21.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,689 hrs · 20,304 cycles

AVIONICS CRAWLWAY FLOORBOARD FWD MOUNT ANGLE AT FS 280.00 CORRODED. R & R AVIONICS CRAWLWAY FLOORBOARD FWD MOUNT IAW SRM 51-25-06, 51-42-10, 51-42-21, 51-42-06, 51-40-11, 51-25-16 & 51-21-00.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 28,689 hrs · 20,304 cycles

TCAS MOUNTING CHANNEL CORRODED. R & R TCAS MOUNTING CHANNEL IAW SRM 51-25-06, 51-40-11, 51-42-06, 51-42-11 & 51-42-21.

Part: WEB — CORRODED (FUSELAGE) · airframe 28,689 hrs · 20,304 cycles

LEFT WEB AT FS 280.00 CROSSBEAM CORRODED. REPAIRED LT WEB AT FS 280.00 IAW 670-53-11-594 DATED 04/27/2011 REV.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,689 hrs · 20,304 cycles

RIGHT FLOOR SEAT RAIL TRACK CORRODED AT FS 364.00. R & R RT FLOOR SEAT RAIL FROM FS 350.00 TO FS 485.00 IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,689 hrs · 20,304 cycles

LEFT FLOOR SEAT RAIL TRACK CORRODED FROM FS 364 TO FS 453. R & R FLOOR SEAT TRACK IAW AMM 53-00-49.

Part: MOUNT FITTING — CORRODED (GALLEY) · airframe 28,689 hrs · 20,304 cycles

ALL FIVE MOUNTING FITTINGS HAVE SIGNS OF CORROSION. R & R ALL FIVE MOUNT FITTINGS IAW CMM 25-33-42. PARTS INSTALLED, CDSP2019-7C-760, CDSP2019-7C-620, 9331091-3, & A661091-1.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 28,689 hrs · 20,304 cycles

PASSENGER DOOR HAS CORROSION AROUND FASTENER HOLES. REMOVED NUTPLATES, BLENDED CORROSION, INSTALLED NUTPLATES IAW SRM 52-00-01, 52-21-11, 51-25-06, 51-42-06 & 51-25-16.

Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 3) · airframe 28,430 hrs · 20,115 cycles

GEAR DISAGREE WARNING MESSAGE. PERFORMED BLEEDING OF THE NR 3 HYD SYS IAW AMM 29-10-00. SERVICED NR 3 HYD SYS IAW AMM 12-12-29. PERFORMED THE EXTENTION & RETRACTION OF THE LG IAW AMM 32-30-00. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: CABLE — BROKEN (PAX DOOR) · airframe 28,223 hrs · 19,959 cycles

MAIN PAX DOOR SUPPORT WHEEL CABLE BROKEN. INSPECTED DOOR & FOUND CABLE NOT TO BE BROKEN, FOUND FO RESTRICTING MOVEMENT, REMOVED FO & PERFORMED OPERATIONAL CHECK IAW CRJ700 AMM 52-11-00, OPERATIONS CHECKED GOOD AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,923 hrs · 18,939 cycles

EMERGENCY CEILING FLOOD LIGHT ROW 15, INOPERATIVE. R & R BULB IAW AMM 33-51-09. OP'S CHECKED GOOD.

Part: DOOR — UNKNOWN (EMERGENCY EXIT) · airframe 26,826 hrs · 18,869 cycles

WATER LEAKING IN FROM ESCAPE HATCH. PERFORMED INSPECTION/CHECK OF CREW EMERGECNCY ESCAPE HATCH IAW AMM 52-22-00, NO DEFECTS NOTED.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 26,809 hrs · 18,853 cycles

FOWARD GALLEY EMERGENCY LIGHTS INOPERATIVE, TWO ON CIELING AND ALSO LIGHT BY SERVICE DOOR AND BY F/A FLASHLIGHT HOLDER. INSPECTED AND FOUND LOOSE CONNECTOR ON EPSU NR 1. RECONNECTED AS REQUIRED IAW AMM 33-51-17. OP'S CHECKED GOOD AT THIS TIME.

Part: CABLE — FRAYED (PAX DOOR) · airframe 26,785 hrs · 18,837 cycles

PAX DOOR CABLE FRAYED.

Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR) · airframe 26,220 hrs · 18,424 cycles

PAX DOOR LATCH CAUTION MESSAGE AND PROXIMITY SYS FAULT 1 STATUS MESSAGE IN FLIGHT. PERFORMED OPS CHECK OF PAX DOOR IAW AMM 52-11-00, OPS CHECK GOOD, NO MESSAGE NOTED AT THIS TIME.

Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR) · airframe 26,208 hrs · 18,412 cycles

PAX DOOR WARNING MESSAGE ON TAXI FROM GATE. VERIFIED PAX DOOR CLOSES AND LOCKS NORMALLY, VISUAL INSPECTION OF INDICATORS SHOWS LOCKED IAW AMM 52-11-00.

Part: WIRE — BROKEN (DOOR SENSOR) · airframe 26,208 hrs · 18,412 cycles

PAX DOOR WARNING MESSAGE. INSPECTED AND FOUND BROKEN WIRE TO SENSOR PX 101. REPAIRED BROKEN WIRE IAW ESPM 20-33-00, NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,010 hrs · 18,260 cycles

EMERGENCY LIGHT AT ROW 15 IS OUT. REPLACED LAMP IAW AMM 33-51-09, OP'S CHECKED GOOD AT THIS TIME.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,906 hrs · 18,189 cycles

EMERGENCY CEILING FLOOD LIGHT OVER ROW 9, INOPERATIVE. LAMPED EMERGENCY FLOOD LIGHT OVER ROW 9 IAW AMM 33-51-09.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,146 hrs · 17,660 cycles

ROW 10 CEILING FLOOD LIGHT INOPERATIVE.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 24,927 hrs · 17,495 cycles

MAIN CABIN DOOR EMERGENCY EXIT LENS NOT SECURE. SECURED MAIN CABIN EMERGENCY LIGHT LENS IAW AMM 33-51-05.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 24,921 hrs · 17,489 cycles

EMERGENCY LIGHTS WON'T COME ON. OPS CHECK OF EMERGENCY LIGHTS GOOD AT THIS TIME IAW 33-55-00.

Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 24,827 hrs · 17,413 cycles

EMERGENCY EXIT DOOR COVER LOOSE, RT -PLACED ON NEF RT EMERGENCY EXIT HANDLE COVER CONTROL NR 12406 IAW NEF 25-100-6, CAT 5.

Part: WARNING MESSAGE — ILLUMINATED (EMERGENCY EXIT) · airframe 24,485 hrs · 17,177 cycles

LEFT EMERGENCY DOOR CAUTION MESSAGE ON LANDING.

Part: PROXIMITY SENSOR — FAULTY (PAX DOOR) · airframe 24,485 hrs · 17,177 cycles

PROX SYSTEM FAULT 2 STATUS MESSAGE POSTED ON ED2. VERIFIED PAX DOOR IS CLOSED, LATCHED, AND LOCKED PRIOR TO DEPARTURE AND FERRY FLIGHT. R & R PROX SWITCH PX-25 IAW AMM 52-70-04.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 24,413 hrs · 17,124 cycles

LEFT OVERWING EXIT MASTER CAUTION. CYCLED LT WING EMERGENCY EXIT DOOR IAW AMM 52-21-00. NO MESSAGES NOTED ON EICAS.

Part: SKIN — DENTED (PAX DOOR) · airframe 24,347 hrs · 17,076 cycles

SMALL DENT DISCOVERED ON MAIN PAX DOOR MIDDLE PORTION OF AFT SECTION. INSPECTED DENT AND FOUND TO BE WITHIN LIMITS IAW SRM 52-11-01

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,194 hrs · 16,968 cycles

EMERGENCY CABIN LIGHT IS INOPERATIVE. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 23,915 hrs · 16,755 cycles

LEFT OVERWING EXIT COVER UNSECURED. RESECURED COVER IAW AMM 52-21-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,712 hrs · 16,596 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4565) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,346 hrs · 16,348 cycles

EMERGENCY LIGHTS WILL NOT STAY ILLUMINATED WHEN SELECTED ON. (FLT 4558) REPLACED ALL 4 ELBPS. P/N AD-2013-1A; S/N OFF 68997; S/N OFF 67791; S/N OFF 81445; S/N OFF 64825.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,291 hrs · 16,318 cycles

LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4567) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,228 hrs · 16,289 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4518) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,956 hrs · 16,108 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4565) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,458 hrs · 15,778 cycles

AFT OVERHEAD EMERGENCY LIGHT BURNED OUT. (FLT 4650) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,426 hrs · 15,754 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4536) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,228 hrs · 15,613 cycles

NR 5 OVERHEAD EMERGENCY LIGHT BURNED OUT. (FLT 4722) RELAMPED EMERGENCY LIGHT.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 19,091 hrs · 13,560 cycles

SMOKE REPORTED IN AFT CABIN. REPLACED RIGHT ACM. (FLT 4574) P/N OFF: GG670-95009-1, S/N OFF: 00748.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,956 hrs · 13,456 cycles

LEFT AFT EMERGENCY LIGHT INOP AND LENS BROKEN. (FLT 4457) RELAMPED AND REPLACED LENS.

Part: BEAM — CORRODED (FUSELAGE) · airframe 18,884 hrs · 13,408 cycles

FS 280 BEAM CORRODED. (C CHECK) REPLACED BEAM PER REO.

Part: WEB — CORRODED (FUSELAGE) · airframe 19,178 hrs · 13,624 cycles

LEFT LOWER WEB AT FS 280 CORRODED. (C CHECK) INSTALLED NEW WEB PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,755 hrs · 13,304 cycles

THE REAR CABIN EMERGENCY CEILING LEVEL FLOODLIGHT INOP. (FLT 4703) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 18,755 hrs · 13,304 cycles

NR 2 AND NR 3 EMERGENCY OVERHEAD FLOODLIGHTS INOP. (FLT 4692) EMERGENCY LIGHTS CHECK NORMAL.

Part: SIGN — MALFUNCTIONED (CABIN) · airframe 18,730 hrs · 13,285 cycles

TWO OVERHEAD EMERGENCY FLOOD LIGHTS AND ONE CEILING EXIT SIGN INOP. (FLT 4627) OPERATIONAL CHECK NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 18,598 hrs · 13,197 cycles

FLT 4549 - EMERGENCY LIGHT IN CEILING NEAR EXIT ROW INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,504 hrs · 13,125 cycles

NR 4 EMERGENCY CEILING FLOODLIGHT INOP. (FLT 4535) RELAMPED EMERGENCY LIGHT.

Part: TORQUE TUBE — CORRODED (NLG) · airframe 18,289 hrs · 12,984 cycles

NOSE LANDING GEAR TORQUE TUBE INNER SURFACE CORRODED. (FLT 4862)REPLACED TORQUE TUBE AND UPPER TORQUE ARM PER CMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,017 hrs · 12,785 cycles

NR 4 EMERGENCY CEILING LIGHT INOP. (FLT 4543) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,987 hrs · 12,765 cycles

OVERHEAD EMERGENCY LIGHT INOP. (FLT 4503) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,188 hrs · 12,190 cycles

CEILING EMERGENCY FLOOD LIGHT INOP. (FLT 4811)RELAMPED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 17,089 hrs · 12,124 cycles

SVC CHECK, FIRST OFFICERS WINDSHIELD CRACKED. REPLACED WINDSHIELD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 16,421 hrs · 11,630 cycles

FLT 4853 - AT TOP OF DESCENT FIRST OFFICER'S SIDE WINDOW CRACKED. REPLACED SIDE WINDOW.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,052 hrs · 11,389 cycles

FLT 4583 - NR 4 EMERGENCY FLOODLIGHT INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,514 hrs · 11,001 cycles

EMERGENCY LIGHT THIRD FROM FRONT OF CABIN IS INOP. (FLT 3837) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,397 hrs · 10,931 cycles

CEILING EMERGENCY FLOOD LIGHT FORWARD OF AFT LAV INOP. RELAMPED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,567 hrs · 11,039 cycles

STA 280 COCKPIT FLOOR SUPPORT HEAVILY CORRODED (C-CHECK). REPLACED SUPPORT PER SRM.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 15,567 hrs · 11,039 cycles

STA 280 CROSSBEAM IS CRACKED AT LBL 9 AND RBL 9 (C-CHECK). REPAIRED PER REO.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 15,567 hrs · 11,039 cycles

STA 280 LOWER BULKHEAD WEB IS CORRODED (C-CHECK). REPLACED LOWER WEB PER REO.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 13,437 hrs · 9,655 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED NEAR CABLE PULLEY BRACKET. REPAIRED CRACK IAW REO 670-52-11-0054.

Part: ENGINE — LEAKING (COMPRESSOR) · airframe 13,165 hrs · 9,496 cycles

FLT 4082 - ON TAKEOFF ROLL, RECEIVED MASTER WARNING "SMOKE FWD LAV" AND "SMOKE AFT LAV." FOUND OIL MIGRATING INTO COMPRESSOR AND BLEED SYSTEM. REPLACED RIGHT ENGINE ASSEMBLY IAW 71-00-00, P/N CF34-BC5B1, S/N OFF 965366.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 12,741 hrs · 9,236 cycles

LEFT WINDSHIELD CRACKED ON CLIMB OUT, FLIGHT NR 4003. REPLACED LEFT WINDSHIELD IAW AMM 56-11-01, P/N NP-139321-13, S/N OFF 02122H5460.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 12,488 hrs · 9,071 cycles

AFT CEILING EMERGENCY EXIT LIGHT IS INOP, FLIGHT NR 1001. RELAMPED AS REQUIRED. OPS CHECK GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 12,470 hrs · 9,061 cycles

PAX O2 MASK IN FORWARD LAV DEPLOYED. RESTOWED OXYGEN MASK IN FORWARD LAV.

Part: LEVER — OUT OF ADJUST (CABIN DOOR) · airframe 12,043 hrs · 8,788 cycles

CABIN DOOR IS HARD TO OPEN FROM THE GROUND. ADJUSTED SWIVEL LEVERS, ADJUSTMENT BOLTS AND STOPS IAW 52-11-17. OPS CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 11,877 hrs · 8,697 cycles

EMERGENCY CEILING POD LIGHT INOP. REPLACED LAMP IN EMERGENCY CEILING POD LIGHT, PN: 1317.

Part: STRUT — CORRODED (NLG) · airframe 10,987 hrs · 8,121 cycles

NLG AXLE/PISTON ASSEMBLY, CORROSION IN BOTH TORQUE LINK ATTACH BORES. REPLACED NLG ASSEMBLY IAW AMM 32-21-01.

Part: STRUT — CORRODED (RT MLG) · corrosion level 3 · airframe 10,987 hrs · 8,121 cycles

RIGHT MLG I/B UPPER TORQUE LINK ATTACH LUG HAS INTERNAL PITTING CORROSION. REPAIRED IAW BF GOODRICH CONSESSION SCR0073-06 REV A.

Part: SENSING ELEMENT — FAILED (LT MLG OVERHEAT) · airframe 10,767 hrs · 7,961 cycles

FLIGHT 5340 - AFTER TAKEOFF RECEIVED BRAKE OVERHEAT WARNING FOR LEFT OUTBOARD MLG. AIRCRAFT RETURNED TO GSO AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED BRAKE TEMP SENSOR.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 9,029 hrs · 6,830 cycles

FLIGHT 5365 - EMERGENCY LIGHT IN GALLEY CEILING INOPERATIVE. REPLACED EMERGENCY BATTERY PACK.

Part: PANEL — UNSECURE (CABIN) · airframe 9,031 hrs · 6,831 cycles

FLIGHT 5365 - EN ROUTE PBI-CVG PART OF THE GALLEY CEILING PANEL CAME UNSECURE, FLIGHT DIVERTED TO SAV. SECURED CEILING PANEL IN PLACE WITH SPEED TAPE AND DEFERRED PER GMM.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 7,872 hrs · 6,090 cycles

FS 280 TRANSVERSE BEAM CORRODED BETWEEN LBL 36 TO RBL 36. REPAIRED IAW BOMBARDIER REO 670-53-11-047 REV C.

Part: BULKHEAD — CORRODED (FS 280) · corrosion level 2 · airframe 7,872 hrs · 6,090 cycles

THE LT AND RT LOWER BULKHEAD WEBS AT FS 280 ARE CORRODED FROM LBL 36 TO RBL 36. REMOVED THE CORRODED WEBS AND INSTALLED NEW WEBS IAW REO 670-53-11-052 REV A.

Part: CROSSBEAM — CORRODED (FS 280) · corrosion level 2 · airframe 7,872 hrs · 6,090 cycles

THE TRANSVERSE BEAM AT FS 280 IS CORRODED FROM LBL 36 TO RBL 36. THE CORRODED TRANSVERSE BEAM WAS REMOVED. A NEW TRANSVERSE BEAM WILL BE INSTALLED IAW REO 670-53-11-047 REV C.

Part: SEAT TRACK — CORRODED (BS 374-485) · corrosion level 2 · airframe 7,872 hrs · 6,090 cycles

FLOOR SEAT TRACK RAIL AT LBL 9 FS 374 TO 485 HAS CORROSION. DEPTH IS .025 INCH AROUND BOLT HOLE. INSTALLED NEW SEAT RAIL IAW BRAS EO 601R-53-4713 AND IAW CRJ700 AMM TASK 53-00-49-400-801-A03.

Part: APU — FAULTY (EMPENNAGE) · airframe 7,869 hrs · 6,084 cycles

FLIGHT 4989 - RECEIVED A FORWARD LAVATORY SMOKE WARNING MESSAGE DURING TAKEOFF ROLL, FLIGHT RETURNED TO GATE. REPLACED THE APU.

Part: SELECTOR VALVE — INOPERATIVE (MLG) · airframe 6,917 hrs · 5,339 cycles

FLIGHT 5296 - GEAR DISAGREE WARNING. REPLACED THE LANDING GEAR SELECTOR VALVE.

Part: OVERHEAT LOOP — OUT OF ADJUST (RT ENGINE) · airframe 5,652 hrs · 4,365 cycles

FLIGHT 5474 RT ENGINE BLEED CAUTION. COULD NOT DUPLICATE. ADJUSTED BLEED SENSOR LOOPS.

Part: FAN BLADE — VIBRATES (RT ENGINE) · airframe 4,103 hrs · 3,124 cycles

FLIGHT 5672 NR 2 ENGINE FAN VIBE INDICATES 2.4. REPLACED THE RT ENGINE FAN BLADES.

Part: HINGE FITTING — CRACKED (SPOILER) · airframe 3,932 hrs · 2,989 cycles

RIGHT INBOARD MULTI FUNCTION SPOILER SHROUD FITTING P/N CC670-17083-5 IS CRACKED. REMOVED CRACKED FITTING AND INSTALLED NEW SERVICEABLE FITTING P/N CC670-17083-5 IAW BOMBARDIER REGIONAL AIRCRAFT SERVICES EO 601R-57-4910.

Part: ACCELEROMETER — FAULTY (LT ENGINE) · airframe 2,747 hrs · 2,093 cycles

FLIGHT 5043) DURING CRUISE FLIGHT THE LT ENGINE FAN VIBRATION ENTERED THE AMBER CAUTION RANGE REACHING 2.1. AIRCRAFT RETURNED TO THE DEPARTING CITY (CVG). REPLACED THE LT ENGINE VIBRATION/ACCELEROMETER.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 2,508 hrs · 1,907 cycles

WHILE ACCOMPLISHING EO 55-009 THE INSTALLATION OF RAIN GUTTER ON STRINGERS 10L AND 10R AT WL 109-673 BETWEEN MID SPAR DATUM 43.750 PERCENT TO 55.625 PERCENT THE FASTENER HOLES WERE ELONGATED DURING THE DRILLING PROCESS. PERFORMED A MAJOR REPAIR BY REAMING HOLES TO REMOVE DAMAGE, FABRICATING AND INSTALLING FREEZE PLUGS IAW WVAC EO 601R-53-4345.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 2,508 hrs · 1,907 cycles

FS 1098.20 BULKHEAD RIGHT WEB BETWEEN STRINGERS 8R AND 9R IS CRACKED. REPAIRED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B.

Part: SLEEVE — BROKEN (RT MLG T LINK) · airframe 2,019 hrs · 1,535 cycles

RT MLG LOWER TORQUE LINK ASSY HAS BROKEN LOCKING SLEEVE. REMOVED BROKEN SLEEVE AND INSTALLED A SERVICEABLE ONE.