N340CA

Part: OXYGEN MASK — NO DEPLOY (ZONE 200) · airframe 47,444 hrs · 37,020 cycles

DURING CRUISE CREW REPORTED R BLEED DUCT WARNING WITH CABIN DEPRESSURIZATION. FOLLOWING QRH PROCEDURES THE DESCENDED AND DECLARED EMERGENCY. PASSENGER OXYGEN MASKS WERE DEPLOYED WITH A FEW NOT DEPLOYED, ROWS 7 C7D AND 16 A&B. INSPECTED SEAT 7 C/D AND 16 A/B OXYGEN MASKS WITH NO DEFECTS NOTED. RESTOWED IAW AMM 35-21-03. PERFORMED OPERATIONAL CHECK IAW AMM 35-20-00. OPERATIONAL CHECK GOOD.

Part: HINGE FITTING — CHAFED (ZONE 300) · airframe 47,073 hrs · 36,626 cycles

VERTICAL STABILIZER MID LOWER HINGE ASSY., LOWER HINGE HALF P/N AV670-21140-001 HAS AN EXCESSIVELY WORN BEARING LANDING. COMPLIED WITH MHIRJ REO 670-55-31-192 REV-- DATED 2025-06-20. INSTALLED NEW SERVICABLE LOWER HINGE P/N AV670-21081-013.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 47,073 hrs · 36,626 cycles

FS333 FLOOR CROSSBEAM IS CORRODED BETWEEN LBL9 AND LBL24. REPAIRED F.S.333 FLOOR CROSSBEAM BETWEEN LBL9 AND LBL24 IAW MHIRJ REO 670-53-21-2630 REV -- DATED 2025-06-16.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 47,073 hrs · 36,626 cycles

FOUND THE R/H F.S. 280 CROSSBEAM TO HAVE MULTIPLE SPOTS OF CORROSION. REMOVED R/H FS 280 CROSSBEAM IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-13-- 001-0010A01, 51-42-21-001-001-A01, 51-40-11-- 001-001-A01. REF. BARCODE IDENTIFIER HN00243776 FOR COMPLETION OF BOMBARDIER REO# 670-53-11-579 REV. B, DATED 2013/05/01. LINE ITEM 6A FOR FABRICATION OF REPAIR ITEMS -3, -4, -5, -6, -7, -8, -9, -21, -22,-31 & -32. LINE ITEM 5A FOR INSTILLATION OF REPAIR ITEMS-3, -4, -5, -6, -7, -8, -9, -21, -22, -31 & -32. REPAIRED R/H F.S. 280 CROSSBEAM IAW REO 670-53-11-579 REV. B, DATED 2013/05/01

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 47,073 hrs · 36,626 cycles

"LH F.S.280 CROSSBEAM HAS MULTIPLE AREAS OF CORROSION. UPON FURTHER EVALUATION FOUND L/H FS280.00 CROSSBEAM TO BE OUT OF LIMITS DUE TO 100% MATERIAL LOSS. FABRICATED LOCATED AND DRILLED REPAIR ITEMS -3, -4, -5, -6, -7, -8, -9, -21, -22, -31, -32 IAW BOMBARDIER REO# 670-53-11-579 REV. B, DATED 2013/05/01. ITEMS -3, -4, -5, -6 MADE FROM S6144-17 (CERT ATTACHED), ITEM -8 MADE FROM S6144-32 (CERT ATTACHED), ITEM -9 MADE FROM S6144-14 (CERT ATTACHED), ITEM -7 MADE FROM 2024-T3 0.040"" PO# 5-22986, ITEM -21 & -22 MADE FROM 2024-T3 0.090"" PO# 5-13710, ITEM -31 & -32 MADE FROM 2024-T3 0.063"" PO# 5-58493. REPAIRED FS280.00 CROSSBEAM IAW REO 670-53-11-579 REV. B, DATED 2013/05/01."

Part: FAN — INOPERATIVE (LAV EXHAUST) · airframe 46,185 hrs · 35,682 cycles

AFTER TAKEOFF, AT APPROX 500 FT ALTITUDE, CREW REPORTED SMOKE SMELL IN CABIN. RETURNED TO ATL. R&R GALLEY/LAV EXHAUST FAN IAW CRJ 700 AMM 21-23-93. OPS CHECK GOOD AT THIS TIME.

Part: ANGLE — CORRODED · airframe 42,602 hrs · 32,226 cycles

RH MLG WHEEL WELL BLOW OUT PNL ATTACHING ANGLES ARE CORRODED. - REMOVED & REPLACED ANGLE IAW CRJ 700 SRM 51-42-210-001-001-A01. CURE CHECK OF SEALANT IN FUEL TANK GOOD. POINTED FASTENERS IAW CRJ 700 SRM 51-25-00-001-001-A01. LEAK CHECK OF REPAIR AREA PERFORMED IAW CRJ 700 AMM 28-11-00-790-801-A01. LEAK CHECK GOOD. REMOVED & REINSTALLED FUEL PANEL 611BB IAW CRJ 700 SRM 28-11-01-000/400-802-A01 LEAK CHECK GOOD. WVAC EMP STAMP #774 MTC

Part: BUSHING — WORN · airframe 42,602 hrs · 32,226 cycles

UPON REMOBAL OF RH MLG SIDE FOUND IN BOARD PINTLE PIN BUSHING BORE TO BE OUT OF TOLERANCE. - COMPLIED WITH REPAIR OF R/H MLH SIDE STAY PINTLE PIN BUSHING BORE IAW MHIRJ REO 670-57-11-186 REV--DATE 2021-12-01.

Part: NONE — CORRODED · airframe 42,602 hrs · 32,226 cycles

RH MLG SIDE STAY IS CORRODED AT HINGE JOINT AND ALONG LWR AFT EDGE OF UPPER BEAM. - REMOVED APEX BOLT AND STOP COMMON TO OLD SIDE STAY IAW CMM GOODRICH 32-11-12 REMOVED AND REPLACED R/H MLG SIDE STAY IAW CRJ 700 AMM 32-11-12-000/400-801-A01 BLEED LEAK AND OPS ARE GOOD AT THIS TIME.

Part: ANGLE — CORRODED · airframe 42,602 hrs · 32,226 cycles

SERVICE DOOR LOWER SILL MOUNTING ANGLE IS CORRODED - PLACED EWIS PROTECTION IAW CRJ 700 AMM 20-70-00-910-801-A01 REMOVED AND INSTALLED DOOR SILL ATTACHED BRACKETS IAW CRJ 700 51-42-06-001-001-A01 REMOVED AND INSTALLED DOOR SILL ATTACHED ANGLE IAW CRJ700 SRM 51-42-06-001-001-A01 LOCATED AND RILLED IAW SRM 51-40-11-001-001-A01 WVAC EMP # 7358

Part: NONE — CORRODED · airframe 42,602 hrs · 32,226 cycles

RH FLOOR SILL BETWEEN FS 280 AND FS 319 IS CORRODED IN MULTIPLE PLACES. - REMOVED AND INSTALLED RH FLOOR SILL BETWEEN FS 280 TO FS 319 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-001-001-A01 AND LOCATED AND DRILLED NEW RH FLOOR SILL FROM FS 280 TO FS 319 IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED SPLICE ANGLE IAW CRJ 700 SRM 51-42-13-001-001-A01 AND 51-42-06-001-001-A01. WVAC EMP #7358

Part: STRINGER — CORRODED · airframe 42,602 hrs · 32,226 cycles

STRINGER 24L CORRODED BETWEEN FS 585.00 AND FS 613.00 - REPAIRED STRINGER 24L BETWEEN F.S. 585.00 & F.S. 613.00 IAW ENDEAVOR AIR EA# CK5753-12504 DATED 12-2-21 REV IR WVAC EMP STAMP # 722 MTC

Part: STRINGER — CORRODED · airframe 42,602 hrs · 32,226 cycles

STRINGER 26L CORRODED AT FS 453.00 TO FS 469.00 - REMOVED AND REPLACED FASTENERS ON STR 26L FROM FS 453.00-469 IAW CJR 700 SRM 51-42-06-0901-001-A01. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT O LIMITS. REPAIRED IAW ENDEAVOR AIR EA CRJ 753-12462. WVAC EMP # 56399

Part: STRINGER — CORRODED · airframe 42,602 hrs · 32,226 cycles

STRINGER 24L CORRODED BETWEEN FS 517.00 AND FS 533.00 - REPAIRED STRINGER 24L BETWEEN FS 517.00 TO 533.00 IAW ENDEAVOR AIR EA# CRJ753-12503 DATED 12-2-21 REV IR WVAC EMP STAMP # 722 MTC

Part: SKIN — CHAFED · airframe 42,602 hrs · 32,226 cycles

EXTERNAL FUSELAGE SKIN BETWEEN FS 977.50 AND FS 985 HAS A CHAFE MEAS. 3"L. - REPAIRED AREA OF EXTERNAL SKIN FS. 977.5-985 IAW EA CRJ753-12527 REV.IR DATED 12/17/2021. WVAC EMP STAMP # 711 MTC

Part: SEAT TRACK — CORRODED · airframe 42,602 hrs · 32,226 cycles

L/H SIDE SEAT RAIL IS CORRODED FROM FS 675 TO FS 713. - FABRICATED AND REPLACED LH SIDE SEAT RAIL FS 675-713 IAW CRJ 900 SRM 51-40-11-001-001-A01, 53-00-49-201-002-A01 AND AMM 53-00-49-400-801-A1

Part: STRINGER — CORRODED · airframe 42,602 hrs · 32,226 cycles

STGR 26R CORRODED BETWEEN FS 517.00 AND FS 533.00 - REPAIRED STRINGER 26R BETWEEN FS 517 AND FS 533 IAW ENDEAVOR EA# CRJ 753-12505 REV IR DATED 12/2/21 REMOVED TAPE. COMPLIED WITH EA CRJ 753-12505 REV IR DATED 12/2/21 WVAC EMP STAMP # 711 MTC

Part: BUSHING — NONE · airframe 42,602 hrs · 32,226 cycles

RH AILERON BUSHING LUG MARKED C IS DAMAGED AND OVERSIZED. - REPAIRED LUG AND REPLACED BUSHING IAW REO 670-57-61-107 REV B DATED 2019-01-14.

Part: CHANNEL — CRACKED · airframe 42,602 hrs · 32,226 cycles

L/H SIDE SEAT RAIL CHANNEL CRACKED BETWEEN FS 477.00 AND FS 573.00. - REPLACED SEAT TRACK RETAINER AND INSTALLED SEAT TRACK IAW CRJ 700 AMM 53-00-49-400-801-A03.

Part: STRINGER — CORRODED · airframe 42,602 hrs · 32,226 cycles

STR 22R JUST FORWARD OF FS 349 IS CORRODED. - FOUND STRINGER 22R OUT OF LIMITS R/R UNSERVICEABLE STRINGER 22R WITH A SERVICEABLE STRINGER IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01 AND 51-23-00-001-001-A01. WVAC EMP STAMP #722 MTC

Part: FRAME — CORRODED · airframe 42,602 hrs · 32,226 cycles

FRAME FS 333 IS CORRODED AT LOWER FLANGE AND WEB BETWEEN STR 26L TO STR 27 IN AVIONICS BAY. TCI 53-20-320. - REMOVED CORROSION ON FRAME FS 333 BETWEEN STR 26L AND STR 27 IAW CRJ 700 SRM 51-21-06-001-001-A01. NO DAMAGE ALLOWED PER CRJ 700 SRM 53-21-00-101-002-A01. NDT NOT REQUIRED DUE TO 100% MATERIAL LOSS REPAIRED CORRODED LOWER FLANGE AND WEB BETWEEN STR 26L TO STR 27 FS 333.00 IAW SRM 53-00-06-201-006-A01. REMOVED AND REINSTALLED CRAWL WAY FLOOR BRACKET IAW CRJ700 SRM 51-42-06-001-001-A01 COMPLIED WITH NDT OF CUT LINES IAW SRM 53-00-06-201-006-A01. DISPLACED AND RECONNECTED DRAIN ON L/H SIDE IAW CRJ 700 SRM 51-41-02-001-001-A01. DISCONNECTED AND RECONNECTED L/H AND R/H ANTENNA ON CABLE ON AVIONCS BAY IAW CRJ 700 AMM 51-54-001-400-801-A01. REMOVED STRINGER CLIPS BETWEEN STR 25R AND 25L AT FS 333 IAW CRJ700 SRM 51-42-06-001-001-A01. LOCATED AND DRILLED FS 333 FRAMER SPLIC AT STR 25R & 25L IAW CRJ 700 SRM 53-00-06-201-006-A01. TRIMMED FRAME SPLICE AT FS 333 ON STR 25L AND 25R IAW CRJ700 SRM 53-00-06-201-006-A01 AND IAW 53-00-06-201-006-A01 & 51-25-00-001-001-A01.

Part: STRINGER — CORRODED · airframe 42,602 hrs · 32,226 cycles

STR 22R JUST FORWARD OF FS 349 IS CORRODED. - FOUND STRINGER 22R OUT OF LIMITS R/R UNSERVICEABLE STRINGER 22R WITH A SERVICEABLE STRINGER IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01 AND 51-23-00-001-001-A01. WVAC EMP STAMP #722 MTC

Part: ANGLE — CORRODED · airframe 42,602 hrs · 32,226 cycles

LIGHTENING DIVERTER ATTATCHING ANGLE BRACKET AT RBL 27.00 FROM FS 310 - FS 333 IS BENT AND REQUIRES REPLACEMENT. - REPLACED ATACHING ANGLE BRACKET @ RBL 27.00 FROM FS 310 - FS 333 WITH A SERVICEABLE ANGLE AND 2 EA CLIPS IAW CRJ 700 SRM 51-42-06-001-001(A01) AND BLEDNED CORROSION IAW EA # CRJ 753-12448 & CRJ 753-12447 REV IR DATED 11-28-21. ANGLE BRACKET DRILLED & LOCATED IAW CRJ 700 SRM 51-40-11-001-001(A01). WVAC EMP STAMP #722 MTC.

Part: STRAP — CORRODED · airframe 42,602 hrs · 32,226 cycles

PANEL 196DR STRAP HAS MULTIPLE SPOTS OF CORROSION. - LOCATED AND DRILLED AFT AND FWD C CHANNELS AND STRAP IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED C CHANNELS TO STRAP IAW CRJ 700 SRM 51-42-13-001-001-A01 AND SRM 51-25-00-001-001-A01. INSTALLED ASSY TO PANEL 195DR IAW CRJ 700 AMM 53-82-83-400-803-A01. WVAC EMP #56399

Part: BRACKET — CORRODED · airframe 42,602 hrs · 32,226 cycles

MACHINED BRACKET AT FS 581.00 BETWEEN STGR 26L AND STGR 27 IS CORRODED - REMOVED AND REPLACED MACHINED BRACKET AT FS 581.00 BETWEEN STR 26L AND 27 IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED · airframe 42,602 hrs · 32,226 cycles

SEAT TRACK AT LBL 9 FROM APPROX FS 830 TO FS 985 IS CORRODED IN MULTIPLE SPOTS. - AFTER FURTHER EVALUATION CORROSION EXISTS IN MORE THAN ONE CROSS SECTIONAL AREA MAKING SEAT TRACK OUT OF LIMITS IAW CRJ 700 SRM 53-51-49-101-001-A01. LOCATED, DRILLED AND INSTALLED SEAT TRACK P/N 20276- 288-0-DA ON FS 830 TO FS 985 LBL9 IAW CRJ 700 SRM 51-40-11-001-001-A01 AND CRJ 700 AMM 53-00-49-000/400-801-A17.

Part: SEAT TRACK — CORRODED · airframe 42,602 hrs · 32,226 cycles

RH SIDE SEAT RAIL CORRODED BETWEEN FS 857 AND FS 961 - REMOVED AND REPLACED SEAT TRACK ON RH SIDE BETWEEN FS 857-961 IAW CRJ 700 AMM 53-00-49-000/400-801-A17.

Part: BRACKET — CORRODED · airframe 42,602 hrs · 32,226 cycles

MACHINED BRACKET AT FS 533.00 BETWEEN STGR 26L AND STGR 27 IS CORRODED - REMOVED AND INSTALLED NEW SERVICEABLE MACHINED BRACKET P/N: SH670-33389-1 AT FS 333 BETWEEN STR 26L AND STR 27 IAW CRJ 700 SRM 51-42-21-001-001-A01. WVAC EMP #89190

Part: PLATE — CORRODED · airframe 42,602 hrs · 32,226 cycles

LH OVERWING EXIT SILL STEP PLATE HAS CORROSION BETWEEN FS 761.85-785.15, PON SH670-36552-7. - REMOVED STEP PLATE IAW CRJ 700 SRM 51-41-02-001-001-A01, CORROSION FOUND TO BE OUT OF LIMITS IAW CRJ 700 SRM 53-41-23-101-001-A01. DAMAGE THROUGH PART, INSTALLED NEW STEP PLATE LH OVERWING EXIT IAW CRJ 700 SRM 51-41-02-001-001-A01, NEW PLATE INSTALLED P/N SH670-365521

Part: SEAT TRACK — CORRODED · airframe 42,602 hrs · 32,226 cycles

LH SIDE SEAT RAIL CORRODED BETWEEN FS 379 AND FS 483. - REMOVED & REPLACED L/H SIDE SEAT RAIL AT FS 379 TO 483 IAW CRJ 700 AMM 53-00-49-000/400-801(A17).

Part: SEAT TRACK — CORRODED · airframe 42,602 hrs · 32,226 cycles

LH SIDE SEAT RAIL CORRODED BETWEEN FS 787 AND FS 857. - AFTER FURTHER EVALUATION, CORROSION EXISTS ON MORE THAN ONE CROSS SECTIONAL AREA MAKING SLAT TRACK OUT OF LIMITS IAW CRJ700 SRM 53-41-49-101-001-A01. REMOVED AND REPLACED SLAT TRACK RAIL ON LH BETWEEN FS 787 AND FS 857 IAW CRJ700 AMM 53-00-49-000/400-801-A17.

Part: SEAT TRACK — CORRODED · airframe 42,602 hrs · 32,226 cycles

RBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 581 TO F.S. 677. - REMOVED CORROSION FLOOR SLAT TRACK RBL 9 BETWEEN FS 581 TO 677 IN MORE THAN ONE CROSS-SECTIONAL AREA. FOUND TO BE OUT OF LIMITS IAW CRJ SRM 51-21-06-001-001-A01 AND SRM 53-31-49-101-001-A01. REMOVED AND RE-PLACED SLAT TRACK IAW CRJ700 AMM 53-00-49-000/400-801-A17.

Part: SEAT TRACK — CORRODED · airframe 42,602 hrs · 32,226 cycles

LH SIDE SEAT RAIL CORRODED BETWEEN FS 713 AND FS 763. - REMOVED AND REPLACED L/H SIDE SEAT RAIL BETWEEN FS 713 AND FS 763 IAW CRJ700 AMM 53-00-49-000/400-801-A17. WVAC EMP STAMP # 703 MTC

Part: SEAT TRACK — CORRODED · airframe 42,602 hrs · 32,226 cycles

RH SIDE SEAT RAIL CORRODED BETWEEN FS 787 AND FS 857. - AFTER FURTHER EVALUATION, CORROSION EXISTS ON MORE THAN ONE CROSS-SECTIONAL AREA MAKING SLAT TRACK OUT OF LIMITS IAW CRJ700 SRM 53-42-49-101-001-A01. REMOVED AND REPLACED SLAT TRACK ON RH AT FS 787 AND FS 857 IAW CRJ700 AMM 53-00-49-000/400-801-A17.

Part: SEAT TRACK — CORRODED · airframe 42,602 hrs · 32,226 cycles

LBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN FS 581 TO FS 677. - REMOVED CORROSION AT FLOOR SEAT TRACK LBL 9 BETWEEN FS 581 TO 677 MORE THAN ONE CROSS SECTIONAL AREA FOUND SEAT TRACK OUT OF LIMITS IAW CRJ 700 SRM 51-21-06-001-001-A01 AND SRM 53-31-49-101-001-A01. REMOVED REPLACED FLOOR SEAT TRACK LBL 9 BETWEEN FS 581 AND FS 677 IAW CRJ 700 53-00-49-000/400-801-A17.

Part: SEAT TRACK — CORRODED · airframe 42,602 hrs · 32,226 cycles

RH SIDE SEAT RAIL CORRODED BETWEEN FS 573 AND FS 675. - AFTER FURTHER EVALUATION CORROSION EXISTS ON MORE THAN ONE CROSS SECTION AND AREA THEREFORE SEAT TRACK IS OUT OF LIMITS. IAW CRJ 700 SRM 53-31-49-101-001-A01. REMOVED AND REPLACED SEAT TRACK P/N 670-3358670-3358-3 ON RH SIDE BETWEEN FS 573 AND FS 675 IAW CRJ 700 AMM 53-00-49-000/400-801-A01.

Part: SEAT TRACK — CORRODED · airframe 42,602 hrs · 32,226 cycles

LH SIDE SEAT RAIL CORRODED BETWEEN FS 857 AND FS 961. - REMOVED AND REPLACED SEAT TRACK P/N: SH670-37543-3 ON LH SIDE FS 857 TO FS 961 IAW CRJ 700 AMM 53-00-49-000/400-801-A17.

Part: SEAT TRACK — CORRODED · airframe 42,602 hrs · 32,226 cycles

LBL 9 SEAT TRACK FROM FS 379 TO FS 485 IS CORRODED - AFTER FURTHER EVALUATION, CORROSION EXISTS IN MORE THAN ONE CROSS SECTIONAL AREA MAKING SEAT TRACK OUT OF LIMITS IAW CRJ700 SRM 53-21-49-101-001-A01. REMOVED AND REPLACED SEAT TRACK P/N SH670-32249-3 AT FS 379 TO FS 485 LBL9 IAW CRJ700 AMM 53-00-49-000/400-801-A17. WVAC EMP STAMP # 703 MTC

Part: SEAT TRACK — CORRODED · airframe 42,602 hrs · 32,226 cycles

RH SIDE SEAT RAIL CORRODED BETWEEN FS 378 AND FS 483 - REMOVED & REPLACED R/H SEAT RAIL BETWEEN F.S. 378 TO 483 IAW CRJ700 AMM 53-00-49-000/400-801(A17) WVAC EMP # 56399

Part: SEAT TRACK — CORRODED · airframe 42,602 hrs · 32,226 cycles

SEAT TRACK AT RBL 9 FROM APPROX FS 830 TO FS 978 IS CORRODED IN MULTIPLE SPOTS. - AFTER FURTHER INVESTIGATION SEAT TRACK IS OUT OF LIMITS IAW CRJ 700 SRM 53-51-49-101-001-A01 DUE TO CORROSION IN MORE THAN ONE CROSS SECTIONAL AREA REMOVED AND REPLACED SEAT TRACK P/N: SH670-37411-3 IAW CRJ 700 AMM 53-00-49-000/400-801-A17. WVAC EMP STAMP #703 MTC

Part: SEAT TRACK — CORRODED · airframe 42,602 hrs · 32,226 cycles

LH SIDE SEAT RAIL CORRODED BETWEEN FS 573 AND FS 675. - INSTALLED NEW SEAT TRACK RAIL PN SH670-33558-3 ON LH SIDE FS 573 TO FS 675 IAW CRJ 700 AMM 53-00-49-400-801-A17.

Part: PLATE — CORRODED · airframe 42,602 hrs · 32,226 cycles

SUPPORT PLATE AT FS 533.00 STGR 25R IS CORRODED. - REMOVED AND REPLACED CORRODED SUPPORT PLATE AT FS 533.00 STR 25R IAW CRJ 700 SRM 51-42-06-001-001-A01 AND SRM 51-42-15-001-001-A0

Part: SEAT TRACK — CORRODED · airframe 42,602 hrs · 32,226 cycles

LH SIDE SEAT REAIL CORRODED BETWEEN FS 483 AND FS 573. - BLENDED CORROSION AT LH SIDE SEAT RAIL AT FS 483 ADN FS 571 IAW CRJ 700 SRM 53-00-101-001-A01. BLENDED AREAS TO BE OUT OF LIMITS IAW CRJ 700 SRM 53-31-49-101-001-A01. REMOVED AND REPLACED L/H SEAT SIDE RAIL FS 483 TO FS 573 IAW CRJ 700 AMM 53-00-49-000/400-801-A17.

Part: SEAT TRACK — CORRODED · airframe 42,602 hrs · 32,226 cycles

RH SIDE SEAT RAIL CORRODED BETWEEN FS 48 AND FS 573. - AFTER FURTHER EVALUATION, CORROSION EXISTS IN MORE THAN ONE CROSS-SECTIONAL AREA THEREFORE SEAT TRACK IS OUT OF LIMITS IAW CRJ 700 SRM 53-31-49-101-001-A01. REMOVED AND REPLACED RH SIDE SEAT RAIL FS 483-573 IAW CRJ 700 AMM 53-00-49-000/400-801-A17.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 36,380 hrs · 27,767 cycles

LH F.S. 280.00 FLOOR BEAM CORRODED AND RH F.S. 280.00 FLOOR BEAM CRACKED AND CORRODED. CORRECTIVE ACTION TO BE ACCOMPLISHED AVMAX W/O 80799 W/C 1126.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 40,783 hrs · 30,489 cycles

LH FWD AND AFT VERTICAL STAB DRAG ANDGLES CRACKED. CORRECTIVE ACTION: REPAIRED LH FWD AND AFT DRAG ANGLE IAW BOMBARDIER REO# 670-55-31-018 REV A DATED 2016-11-10, BOMBARDIER REO# 670-55-31-128 DATED 2020-01-29 AND GOJET EO C700-55MR-001O DATED 11-24-2018.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 40,783 hrs · 30,489 cycles

R/H BULKHEAD WEB AT F.S. 280.00 CORRODED. CORRECTIVE ACTION: REPAIRED R/H BULKHEAD WEB AT F.S. 280.00 BY REMOVING CORREDED BULKHEAD WEB, FABRICATING AND INSTALLING NEW BULKHEAD WEB IAW BOMBARDIER REO# 670-53-11-594 REV A DATED: 2015/06/26

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 40,783 hrs · 30,489 cycles

RH INBRD FLAP DENTED ON LOWER SKIN AND RIB BETWEEN FLS. 30.00 AND 36.00 APPOXIMATLEY 9.1 INCHES FROM TRAILING EDGE . CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR TO RH INBRD FLAP LOWER SKIN BY CUTTING OUT DAMAGED SKIN, FABRICATING AND INSTALLING REPPAIR PARTS IAW CRJ 700 SRM 57-52-01, TYPE IV REPAIR PERFROMED.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 40,783 hrs · 30,489 cycles

RH FWD AND AFT VERTICAL STABILIZER DRAG ANGLES CRACKED. CORRECTIVE ACTION: REPAIRED RH FWD AND AFT DRAG ANGLES IAW BOMBARDIER REO# 670-55-31-018 REV A DTED 2019-11-10, BOMBARDIER REO# 670-55-31-128 DATED 2020-01-29, AND GOJET EO C700-55MR -001-O DATED 11-24-2018.

Part: SUPPORT — CRACKED (BS 793) · airframe 40,783 hrs · 30,489 cycles

LH ANGLE ON FRAME SUPPORT CRACKED AT F.S.793.00 CORRECTIVE ACTION: REMOVED DAMAGED AREA BY CUTTING OUT DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW REO670-53-82-478 REV:A DATED 2014/11/12, CRJ 700 SRM 51-42-06, 51-42-21, 51-21-11, 51-25-06, 51-25-16 TR 51-0065, AND NDTM PART01 51-20-006.

Part: ANGLE — CORRODED (ZONE 100) · airframe 40,783 hrs · 30,489 cycles

FLOOR RAIL AND FWD PAX DOOR ARM CUT OUT PLATE HAVE SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPALCED KICK PLATE ANGLE(P/N:SH670-31875-3S), MID CAP ANGLE(P/N:SH670-31825-9SS), AND FITTING (P/N:SH670-31840-3) IAW CRJ700 AMM 52-70-04, CRJ700 SRM 51-41-02, 53-21-23, 51-21-11, 51-25-06, 51-25-16 TR 51-0065, 51-40-11, 51-42-06, AND 51-42-21.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 40,783 hrs · 30,489 cycles

RH SIDE SEAT RAIL BETWEEN F.S.708.00 TO F.S.761.OO HAS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED RH SIDE SEAT RAIL FROM F.S.703.00 TO F.S.761.00(P/N: SH670-37509-1) IAW CRJ700 AMM 53-00-49 AND CRJ 700 SRM 53-41-49.

Part: STAND OFF — CRACKED (RT NACELLE) · airframe 40,783 hrs · 30,489 cycles

R/H LOWER TRANS COWL INBD ANGLE WEDGE CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED R/H LOWER TRANSCOWL I/B STANDOFF (P/N: 624-2082-201) IAW CRJ700 SRM 51-42-13 AND 51-42-22.

Part: FLOOR PANEL — DAMAGED (E/E BAY) · airframe 40,783 hrs · 30,489 cycles

FORWARD EQUIPMENT COMPARTMENT R/H SIDE FLOOR CRACKED AT APPROX F.S. 195.00. CORRECTIVE ACTION: REPAIRED FWD EQUIPMENT COMPARTMENT R/H FLOOR BY CUTTING OUT DAMAGE, FABRICATING REPAIR PARTS, AND INSTALLING REPAIR PARTS IAW BOMBARDIER REO 67-53-11-1572 DATED 2020-02-01, BOMBARDIER REO 670-53-11-509 REV E DATED 2018-02-08, AND CRJ 700 AMM 20-70-00. NDT PERFORMED BY BARON NDT, LLC FAA CRS#5NDR545D REPORT# M013020-3, P.O.#152607, DATED 30JAN2020 NO DEFECTS NOTED AT THIS TIME AND REPORT# S012520-1, P.O.# 152530, DATED 25JAN2020 NO DEFECTS NOTED AT THIS TIME.

Part: DOOR SEAL — DIRTY (SERVICE DOOR) · airframe 39,592 hrs · 29,368 cycles

SERVICE DOOR CAUTION MSG APPEARS IN FLIGHT AND LOUD HISSING NOISE FROM DOOR. DEFERRED SERVICE DOOR CAUTION MSG PER MEL 52-70-05 CAT C OC#70056400 C/P/T 06/09/19 AUTH BY MXC, CLEANED SERVICE DOOR SEAL WORK PERFORMED IAW AMM 51-26-00.

Part: STEP — DETACHED (PAX DOOR) · airframe 38,624 hrs · 28,496 cycles

PAX DOOR TOP STEP DETACHED FROM ACFT. R/R HORIZONTAL UPPER STAIRS PANEL HINGE IAW CRJ 700 AMM 52-11-04 A/C OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG STEERING) · airframe 36,669 hrs · 26,648 cycles

NOSE WHEEL STEERING INOPERATIVE CAUTION MESSAGE ILLUMINATED IN FLIGHT. OPS CHECK OF THE NOSE WHEEL STEERING IAW AMM 32-51-00, OPS CHECKED GOOD.

Part: UNKNOWN — UNKNOWN (PAX DOOR) · airframe 36,629 hrs · 26,605 cycles

MAIN PAX DOOR WILL NOT OPEN FROM OUTSIDE OR INSIDE AIRCRAFT. PERFORMED OPS CHECK OF PAX DOOR IAW CJR 700 AMM 52-11-00 OPS CHEKC GOOD AT THIS TIME.

Part: DOOR SEAL — DAMAGED (PAX DOOR) · airframe 35,500 hrs · 25,594 cycles

PASSENGER DOOR SEAL DAMAGED. REMOVED AND REPLACED PASSENGER DOOR SEAL IAW AMM 52-11-07.

Part: DOOR FRAME — CORRODED (PAX DOORWAY) · airframe 35,500 hrs · 25,594 cycles

PASSENGER DOOR FWD FRAME ACCESS PANEL 832CL HAS SIGNS OF CORROSION ON UPPER INTERNAL FOOT (FORMER). CORRECTIVE ACTION: CLEANED AND EVALUATED FORMER AND FOUND DAMAGE TO BE OUT OF LIMITS IAW CRJ700 SRM 51-26-00/53-00-00. REMOVED AND REPLACED FWD FORMER IAW CRJ700 SRM 51-42-06/51-42-21/51-25-06/51-40-11/51-25-16

Part: FORMER — CRACKED (PAX DOOR) · airframe 35,500 hrs · 25,594 cycles

PASSENGER DOOR AFT EDGE MEMBER (FORMER) CRACKED ON TOP FLANGE. REMOVED AND REPLACED AFT EDGE MEMBER IAW SRM 51-42-06/52-11-06/52-11-07/51-42-21/51-40-11.

Part: ATTACH ANGLE — CRACKED (PAX DOOR) · airframe 35,500 hrs · 25,594 cycles

PASSENGER DOOR RT LOWER ATTACH ANGLE CRACKED. REMOVED AND REPLACED RT LOWER ATTACH ANGLE IAW SRM 51-40-11, 51-42-06.

Part: RETAINER — CORRODED (PAX DOOR SEAL) · airframe 35,500 hrs · 25,594 cycles

PAX DOOR LOWER AFT CORNER SEAL RETAINER IS DAMAGED. REMOVED AND REPLACED LOWER AFT CORNER SEAL RETAINER IAW SRM, 51-40-11, 51-25-16, AND 51-42-06

Part: RETAINER — CORRODED (PAX DOOR SEAL) · airframe 35,500 hrs · 25,594 cycles

PAX DOOR FORWARD SEAL RETAINER IS CORRODED. REMOVED AND REPLACED THE FORWARD SEAL RETAINER IAW SRM 51-42-06, & 51-40-11

Part: MOUNT — CRACKED (PAX DOOR ASSIST) · airframe 35,500 hrs · 25,594 cycles

PAX DOOR POWER ASSIST MOTOR MOUNT IS CRACKED ON UPPER SIDE. REMOVED AND REPLACED MOUNT IAW SRM 51-42-06, AND 51-40-11.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 35,500 hrs · 25,594 cycles

PAX DOOR MID INTERCOSTAL SHOWS SIGNS OF CORROSION. REMOVED AND REPLACED MID INTERCOSTAL IAW SRM 51-42-06, 51-26-00, AND 51-40-11

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 35,524 hrs · 25,610 cycles

PAX DOOR WON'T CLOSE. LUBRICATED AND ADJUSTED THE DOOR, OPS CHECKED GOOD IAW AMM 52-11-00.

Part: FITTING — CRACKED (DOOR CAM) · airframe 35,500 hrs · 25,594 cycles

PAX DOOR UPPER AFT CAM FITTING IS CRACKED. REMOVED AND REPLACED AFT UPPER PAX DOOR CAM FITTING IAW SRM 51-42-21, AND 51-25-16.

Part: RETAINER — CORRODED (CARGO DOOR) · airframe 35,500 hrs · 25,594 cycles

FWD CARGO DOOR SEAL RETAINERS(3) ARE CORRODED. REMOVED AND REPLACED FWD CARGO DOOR SEAL RETAINERS (3-PNS: CC670-38663-5, CC670-38674-3, CC670-38675-3) IAW SRM 51-42-06, 51-21-11, 51-25-06, AND 51-42-13.

Part: DOOR SILL — CORRODED (CARGO DOORWAY) · airframe 35,500 hrs · 25,594 cycles

AFT CARGO DOOR SILL IS CORRODED. REMOVED AND REPLACED AFT CARGO DOOR SILL IAW SRM 51-42-06, 51-42-13, 53-61-23, 51-40-11, 51-25-16, 52-32-00, 51-31-00, AND AMM 51-42-13

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 35,500 hrs · 25,594 cycles

PAX DOOR INTERIOR INTERCOSTAL LOWER AFT, IS CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, 51-42-21, AND 51-40-11

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,500 hrs · 25,594 cycles

CORROSION ON RT SEAT TRACK AT FS 349 AND BETWEEN FS 421 AND FS 469 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED RT SEAT TRACK FROM FS 349 TO FS 485 IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,500 hrs · 25,594 cycles

RT CENTER SEAT TRACK CORROSION OUT OF LIMITS AT FS 677. REPLACED RT CENTER SEAT TRACK FROM FS 581-677 IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,500 hrs · 25,594 cycles

LT CENTER SEAT TRACKS CORROSION AND GOUGES FOUND TO BE OUT OF LIMITS BETWEEN FS 581-677. REPLACED LT CENTER SEAT TRACK AT FS 581-677 IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,500 hrs · 25,594 cycles

LT CENTER SEAT TRACK CORRODED BETWEEN FS 517.00 AND FS 533.00. REPLACED LT CENTER SEAT RAIL FROM FS 485.00 TO FS 581.00 IAW AMM 53-00-49.

Part: AXLE — CORRODED (MLG) · airframe 35,500 hrs · 25,594 cycles

CORROSION FOUND ON INBD AND OTBD LT AXLES. PERFORMED SB 49200-32-95 IAW SB 670BA-32-048 AND REO 670-32-11-361, NDT PERFORMED, NO DEFECTS NOTED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,500 hrs · 25,594 cycles

FRAME 333 AT RT BETWEEN STR 0 TO STR 1R HAS A CRACK. REMOVED AND REPLACED FRAME 333 IAW SRM 51-42-06, 51-42-21, 51-40-11, 51-23-00, 51-25-16, 51-21-11.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 35,500 hrs · 25,594 cycles

STRINGER 26R BETWEEN FRAME 333.00 AND FRAME 349.00 HAS SIGNS OF CORROSION. REMOVED AND REPLACED STRINGER 26R BETWEEN FRAME 333.00 AND FRAME 349.00 IAW SRM53-21-03, 51-42-21, 51-42-06, 51-40-11, 51-25-16, AND 51-21-11.

Part: CROSSBEAM — CORRODED (BS 1000-1015) · airframe 33,264 hrs · 23,871 cycles

CORROSION FOUND ON RT SIDE BEAM, AT FS 1000-1015 STR 17R.

Part: FLOOR SUPPORT — CORRODED (BS 1015-1031) · airframe 33,264 hrs · 23,871 cycles

SIDE FLOOR SUPPORT CORRODED BEYOND ALLOWABLE LIMITS AT BS 1015-1031, STR 17.

Part: FLOOR SUPPORT — CORRODED (BS 1031-1040) · airframe 33,264 hrs · 23,871 cycles

CORROSION FOUND ON FLOOR SUPPORT AT LBL 9.0 FROM FS 1031-1040.

Part: LIGHT — UNSECURE (CABIN) · airframe 33,010 hrs · 23,680 cycles

RIGHT SIDE EMER EXIT ROW FLOOR ILLUMINATION STRIP IS UNGLUED. GLUED RT SIDE EMER FLOOR ILLUMINATION STRIP IAW AMM 33-51-01. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: BOLT — DEFECTIVE (PAX DOOR) · airframe 32,792 hrs · 23,522 cycles

PASSENGER DOOR HANDRAIL INOPERATIVE. R & R BOLT FOR PAX DOOR HANDRAIL IAW AMM 52-11-05. OPERATIONS CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,706 hrs · 23,460 cycles

EMERGENCY LIGHT ON CAPTAINS SIDE, EXIT ROW HAS ONE BULB OUT OF 5 NOT WORKING. RELAMPED EMER LIGHT IAW AMM 33-51-05. OPERATIONS CHECKED GOOD AT THIS TIME. OK FOR SERVICE.

Part: MARKER — DEFECTIVE (CABIN DOOR) · airframe 32,374 hrs · 23,209 cycles

MAIN CABIN DOOR BOTTOM RT, ALIGNMENT MARK UNREADABLE. RE-APPLIED INDICATION MARK IAW AMM 51-22-81. PERFORMED INSPECTION OF MAIN PAX DOOR WITNESS MARKS IAW AMM 52-11-00.

Part: SPRING — MISINSTALLED (PAX DOOR) · airframe 32,345 hrs · 23,188 cycles

PASSENGER DOOR SUPPORT WHEEL DID NOT DEPLOY, DOOR CONTACTED GND. FOUND PAX DOOR SUPPORT WHEEL SPRING NOT INSTALLED CORRECTLY. REMOVED & REINSTALLED PAX DOOR SUPPORT WHEEL SPRING CORRECTLY & REPOSITIONED CABLE BACK ON TO PULLEYS IAW AMM 52-11-13. OPERATIONS CHECKED GOOD.

Part: SPRING — DEFECTIVE (PAX DOOR) · airframe 32,246 hrs · 23,111 cycles

PASSENGER DOOR SUPPORT WHEEL DID NOT DEPLOY. R & R PAX DOOR SUPPORT WHEEL TORSION SPRING IAW AMM 52-11-12.

Part: SUPPORT — BROKEN (PAX DOOR) · airframe 31,963 hrs · 22,893 cycles

SUPPORT BAR FOR PAX DOOR HANDRAIL BROKE OFF. REMOVED PAX DOOR FWD & AFT HANDRAIL ACTUATOR ASSEMBLIES. SECURED PAX DOOR HANDRAIL IN THE STOWED POSITION. VERIFIED PAX DOOR OPENS & CLOSES WITHOUT IMPEDANCE. PERFORMED GVI OF ACFT, FOUND SAFE FOR A ONE TIME FERRY FIGHT.

Part: SKIN — GOUGED (FUSELAGE) · airframe 31,478 hrs · 22,517 cycles

RIGHT AFT FUSELAGE HAS A GOUGE & DENTED BETWEEN FS 1144 & 1162. CUT OUT DAMAGE & REPAIRED IAW REO 670-53-61-1125, DATED 07 MAY 2015. WO 80286 & WC 1170.

Part: POST — CORRODED (FUSELAGE) · airframe 31,478 hrs · 22,517 cycles

RIGHT FLOOR POST AT RBL 11.16, FS 280.0 IS CORRODED. REPAIRED RT FLOOR POST AT RBL 11.16 & FS 280.0 IAW REO 670-53-11-1049 DATED 25 APRIL 2015. NDT PERFORMED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,478 hrs · 22,517 cycles

LEFT & RIGHT FLOORBEAM AT FS 280 IS CORRODED. R & R FLOORBEAM IAW AMM 53-11-41 & SB 670BA-53-026.

Part: STRAP — BROKEN (FUSELAGE) · airframe 31,478 hrs · 22,517 cycles

AFT BODY FAIRING CTR SUPPORT STRAP BROKEN. FABRICATED NEW STRAP IAW DWG CC670-9171 REV NC DATED APRIL 1998.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,478 hrs · 22,517 cycles

LEFT & RIGHT SIDE SEAT RAILS HAVE SPOTS OF CORROSION FROM FS 669.40 TO 977.0. EVALUATED & FOUND TO BE OUT OF LIMITS. REPLACED LT NR 5 & 6 RAIL SECTIONS & REPLACED RT NR 4 & 6 RAIL SECTIONS IAW AMM 53-00-49 & REO 670-53-00-013 REV J DATED 22 OCT 2014. PN'S SH670-36255-3, SH670-37509-1 & SH670-36260-5. WO 80286 & WC 2194.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,478 hrs · 22,517 cycles

1/4 TURN FLOOR SUPPORT ANGLE AT FS 280.00 IS CORRODED. R & R 1/4 TURN FLOOR SUPPORT ANGLE IAW SRM 51-42-06 & 51-42-13.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 31,478 hrs · 22,517 cycles

RIGHT FLOOR SILL AT FS 280.00 IS CORRODED. R &R RT FLOOR SILL, PN SH670-3212-3, AT FS 280.00 IAW SRM 20-70-00, 51-42-06, 51-40-11, 51-21-11 & 51-25-21.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 31,478 hrs · 22,517 cycles

LEFT FLOOR SEAT TRACK FROM BS 477 - 639 IS CORRODED. R & R SEAT TRACK IAW AMM 53-00-49 & REO 670-53-00-013 REV J .

Part: HOUSING — GOUGED (PAX DOOR) · airframe 31,478 hrs · 22,517 cycles

PASSENGER DOOR POWER ASSIST PULLY HOUSING IS GOUGED. R & R PAX DOOR POWER ASSIST PULLY HOUSING, PN 601R317107-17, IAW AMM 52-11-08.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 31,478 hrs · 22,517 cycles

PASSENGER DOOR KICK ANGLE IS CORRODED. R & R PAX DOOR KICK ANGLE, PN SH67031875-35, IAW SRM 51-42-06 & 51-40-11.

Part: CAP — CORRODED (PAX DOOR) · airframe 31,478 hrs · 22,517 cycles

PASSENGER DOOR FWD & AFT ANGLE CAPS ARE CORRODED. R & R PAX DOOR FWD ANGLE CAP, PN SH670-31821-5, & AFT ANGLE CAP, PN:SH670-31821-6, IAW SRM 51-42-21.

Part: CAP — CORRODED (PAX DOOR) · airframe 31,478 hrs · 22,517 cycles

PASSENGER DOOR MID CAP CORRODED. R & R PAX DOOR MID CAP, PN SH670-31825-05, IAW SRM 51-41-02 & 51-40-11.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 31,478 hrs · 22,517 cycles

AFT FUSELAGE FAIRING SUPPORT AT FS 950.0 IS CORRODED. R & R AFT FUSELAGE FAIRING SUPPORT, PN SH670-39189-1, AT FS 950.0 IAW SRM 51-42-06 & 51-45-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,478 hrs · 22,517 cycles

AFT CARGO FLOORBEAM LBL AT 27.00 & FS 1031.00 IS CORRODED. REPAIRED AFT CARGO FLOORBEAM, PN 670-53-00-029-16, AT LBL 27.00 & FS 1031.00 BY CUTTING OUT CORRODED AREA FROM FS 1000.00 TO FS 1051 IAW REO 670-53-00-029 REV A DATED 31 AUG 2010. NDT PERFORMED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,478 hrs · 22,517 cycles

LEFT & RIGHT SIDE SEAT RAILS CORRODED IN MULTIPLE AREAS FROM FS 379.00 - 645.00. REPLACED CORRODED RAILS LT & RT SIDE SEAT IAW AMM 53-00-49.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 31,478 hrs · 22,517 cycles

MAIN AVIONICS COMPARTMENT T CAS ANTENNA MOUNT CORRODED. R & R T CAS CHANNEL IAW SRM 51-42-05 & 51-42-21.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 31,478 hrs · 22,517 cycles

LEFT & RIGHT BULKHEAD WEBS AT FS 280 HAVE CORROSION. R & R LT & RT BULKHEAD WEBS AT FS 280 IAW REO 670-53-11-594 REV DATE 04 27 2011 & SRM 51-42-06, 51-25-16 & 51-21-11.

Part: LENS — MISSING (CABIN) · airframe 31,178 hrs · 22,303 cycles

EMERGENCY FLOOR FLOODLIGHT IN GALLEY IS MISSING LENS & ONE BLUB OUT. PLACED MISSING EMER FLOODLIGHT LENS ON NEF 25-100-12. RELAMPED BULB, OPERATIONS CHECKED GOOD.

Part: PROXIMITY SWITCH — OUT OF ADJUST (NLG) · airframe 29,788 hrs · 21,234 cycles

LANDING GEAR DID NOT RETRACT ON CLIMB OUT. ADJUSTED NLG WOW PROX SWITCHES PX03 & PX11 IAW AMM 32-61-05. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.

Part: COVER — DETACHED (EMERGENCY EXIT) · airframe 29,593 hrs · 21,082 cycles

RIGHT EMER OVERWING EXIT HANDLE COVER DETACHED. SECURED RT OVERWING EMER EXIT COVER IAW AMM 52-21-02.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 29,593 hrs · 210,820 cycles

CREW REPORTS PAX DOOR HARD TO CLOSE. LUBED DOOR IAW 12-20-52. PERFORMED OPERATIONS CHECK OF PAX DOOR IAW AMM 52-11-00. OPERATIONS CHECK GOOD AT THIS TIME.

Part: HINGE PIN — MIGRATED (PAX DOOR) · airframe 29,353 hrs · 20,890 cycles

TOP PAX STEP HINGE PIN IS MIGRATING. REPOSITIONED PAX DOOR TOP STEP HINGE PIN IAW 52-11-04.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 29,163 hrs · 20,734 cycles

PAX DOOR OUT HANDLE CAUTION LIGHT IN FLIGHT. PAX DOOR WARNING SYS OPERATIONS CHECKED GOOD THIS TIME IAW 52-70-04.

Part: SCREW — LOOSE (EXIT SIGN) · airframe 28,345 hrs · 20,117 cycles

EMERGENCY EXIT SIGN ABOVE SERVICE DOOR IS FALLING OFF. SECURED LOOSE SCREW IAW CRJ700 AMM 33-51-05.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,043 hrs · 19,876 cycles

EMERGENCY LIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,716 hrs · 19,627 cycles

CEILING EMERGENCY LIGHT INOPERATIVE, ROW 9 & 10.

Part: SEAL — OBSTRUCTED (ESCAPE HATCH) · airframe 27,333 hrs · 19,335 cycles

CREW ESCAPE HATCH LEAKS WATER ON GROUND. REMOVED DEBRIS FROM ESCAPE HATCH SEAL. OP'S CHECKED ESCAPE HATCH IAW AMM 52-72-00, OP'S CHECKED GOOD.

Part: SEAL — LEAKING (ESCAPE HATCH) · airframe 27,288 hrs · 19,298 cycles

FLIGHT DECK ESCAPE HATCH LEAKING. LUBRICATED FLIGHT DECK ESCAPE HATCH SEAL IAW AMM 12-20-52, NO LEAKS AT THIS TIME.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 27,214 hrs · 19,239 cycles

FLAPS HALFSPEED STATUS MESSAGE. CLEARED INHIBITS AND PERFORMED OPS CHECK OF SFECU IAW AMM 27-51-05. OP'S CHECK GOOD AT THIS TIME.

Part: HOOK AND LOOP — MISSING (EMERGENCY EXIT) · airframe 27,131 hrs · 19,170 cycles

SEAT 12D HOOK AND LOOP MISSING FROM EMERGENCY DOOR PANEL. REPLACED HOOK AND LOOP AS REQUIRED IAW AMM 51-22=31.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 26,836 hrs · 18,950 cycles

LEFT EMERGENCY EXIT COVER IS LOOSE. RESECURED LT EMERGENCY EXIT COVER AS REQUIRED IAW 33-51-10.

Part: GCU — INOPERATIVE (NR 2) · airframe 26,655 hrs · 18,819 cycles

GENERATOR NR 2 OFF CAUTION MESSAGE IN FLIGHT WITH APU DEFERED. SWAPPED GCU NR 2 AND GCU NR 3 FOR TROUBLESHOOTING, IAW AMM 24-11-07 AND 24-22-03. GCU NR 2 OPS CHECK GOOD AT THIS TIME IAW AMM 24-11-01.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 26,519 hrs · 18,717 cycles

PAX DOOR LINTAL STRINGER 3 CRACKED AT FS 280.00. REPAIRED LINTAL STRINGER IAW SB 670BA-53-040 AND REO 670-53-21-493.

Part: LINER — DAMAGED (SERVICE DOOR) · airframe 26,519 hrs · 18,717 cycles

SERVICE DOOR LOWER LINER BOTTOM EDGE DAMAGED. R & R SERVICE DOOR LINER IAW AMM 25-26-07.

Part: ATTACH BRACKET — LOOSE (SERVICE DOOR) · airframe 26,519 hrs · 18,717 cycles

SERVICE DOOR LATCH ATTACH BRACKET LOOSE. REPLACED RIVETS IN BRACKET IAW SRM 51-42-10.

Part: ROLLER — WORN (SERVICE DOOR) · airframe 26,519 hrs · 18,717 cycles

SERVICE DOOR FWD AND AFT BOTTOM DOOR ROLLERS ARE WORN. R & R SERVICE DOOR ROLLERS IAW AMM 52-41-02.

Part: SUPPORT ANGLE — CORRODED (BS 280) · airframe 26,519 hrs · 18,717 cycles

CENTER CRAWLWAY FLOORBOARD SUPPORT ANGLE AT FS 280, CORRODED. R & R ANGLE IAW SRM 51-42-06.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 26,519 hrs · 18,717 cycles

COCKPIT FLOORBEAM AT FS 280, CORRRODED. R & R COCKPIT FLOORBEAM IAW SRM 51-42-06.

Part: SILL — CORRODED (SERVICE DOORWAY) · airframe 26,519 hrs · 18,717 cycles

SERVICE DOOR SILL SHOWS SIGNS OF CORROSION. R & R DOOR SILL IAW SRM 53-21-45.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 26,519 hrs · 18,717 cycles

RT FLOOR SUPPORT FROM FS 280-FS319 HAS CORRODED. R & R RT FLOOR SUPPORT IAW SRM 51-42-01 AND 51-42-11.

Part: RIVET — WORN (PAX DOOR) · airframe 26,519 hrs · 18,717 cycles

PAX DOOR FWD AND AFT CLOSING PLATES HAVE WORN RIVETS. R & R PAX DOOR FWD AND AFT CLOSING PLATES RIVETS IAW SRM 51-42-13.

Part: SEAT TRACK — CORRODED (BS 597) · airframe 26,519 hrs · 18,717 cycles

SEAT TRACK HAS CORROSION AT FS 597. R & R RT SEAT TRACK FROM FS 581 TO 677, IAW SRM 53-00-49.

Part: SEAT TRACK — CORRODED (BS 700) · airframe 26,519 hrs · 18,717 cycles

SEAT TRACK HAS CORROSION AT FS 700. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.

Part: CROSSBEAM — CORRODED · airframe 26,519 hrs · 18,717 cycles

FS 280, CROSSBEAM CORRODED. R & R FS 280 CROSSBEAM IAW REO 670-53-11-047.

Part: LINER — DAMAGED (SERVICE DOOR) · airframe 26,519 hrs · 18,717 cycles

SERVICE DOOR LOWER LINER BOTTOM EDGE DAMAGED. REMOVED AND INSTALLED SERVICE DOOR LINER IAW AMM 25-26-07.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 26,295 hrs · 185,565 cycles

RIGHT ENGINE DEGRADED, CAUTION MESSAGE ON TAKEOFF. PERFORMED 3 ENGINE STARTS AND CLEARED FAULTS IAW AMM 72-00-00.

Part: SEAL — OBSTRUCTED (EMERGENCY EXIT) · airframe 26,221 hrs · 18,500 cycles

ESCAPE HATCH LEAKING. REMOVED DEBRIS FROM DOOR SEAL AND STRIKER, INSPECTED AROUND HATCH & SEAL WITH NO DAMAGE NOTED IAW AMM 52-22-00. NO LEAKS DEFECTED AT THIS TIME.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 26,053 hrs · 18,376 cycles

CABIN PRESSURE APPEARED ABNORMAL AFTER AFT CARGO DOOR MESSAGE CAME ON. FOUND CABIN PRESSURE CONTROLLER NR 1 AUTO MODE FAILED.

Part: PIN — MISSING (DOOR HANDRAIL) · airframe 25,531 hrs · 17,993 cycles

DMI 33679, PIN MISSING FROM CABIN DOOR RAILING. CLEARED DMI 33679 WITH CLOSING CONTROL NR 233. INSTALLED MAIN DOOR RAILING PIN IAW AMM 52-11-05.

Part: BULB — BURNED OUT (CABIN) · airframe 24,996 hrs · 17,580 cycles

NR 4 CEILING EMERGENCY LIGHT INOPERATIVE. R & R BULB AT NR 4 CEILING EMERGENCY LIGHT. OPS CHECK GOOD IAW AMM 33-51-09

Part: SNAP RING — MISSING (EMERGENCY EXIT) · airframe 24,818 hrs · 17,449 cycles

SNAP RING ON RT LIFE LINE MISSING. INSTALLED SNAP RING ON RT LIFE LINE IAW AMM 25-63-04.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,803 hrs · 17,437 cycles

EMERGENCY LIGHT AT ROW 4 INOPERATIVE. R & R EMERGENCY LIGHT BULB AT ROW 4 IAW AMM 33-51-09.

Part: WARNING MESSAGE — ILLUMINATED (PAX DOOR) · airframe 24,782 hrs · 17,442 cycles

PAX DOOR OUTER HANDLE CAUTION MESSAGE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,110 hrs · 16,945 cycles

NR 5 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4451) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,508 hrs · 16,516 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4811) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,391 hrs · 16,444 cycles

NR 4 OVERHEAD EMERGENCY CEILING LIGHT IS OUT. (FLT 4806) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,970 hrs · 16,148 cycles

FORWARD OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4811) RELAMPED EMERGENCY LIGHT.

Part: BEAM — CORRODED (FUSELAGE) · airframe 22,990 hrs · 16,162 cycles

FS 280 BEAM CORRODED ON LEFT AND RIGHT SIDES. (C-CHECK) REPLACED FS 280 BEAM PER SRM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 21,849 hrs · 15,392 cycles

EMERGENCY LIGHTS OVER FORWARD F/A STATION DO NOT ILLUMINATE. (FLT 4695) REPLACED NR 1 ELBP POWER SUPPLY. P/N AD-2013-1A, S/N OFF 23380.

Part: CHARGER — FAILED (CABIN) · airframe 20,739 hrs · 14,685 cycles

NR 1 EMERGENCY BATTERY CHARGER WILL NOT CHARGE BATTERY. (FLT 4607) REPLACED NR 1 EMERGENCY BATTERY CHARGER PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 20,739 hrs · 14,685 cycles

EMERGENCY LIGHTS INOPERATIVE. (FLT 4607) REPLACED EMERGENCY LIGHT BATTERY PACKS AT POSITIONS 1-4 PER AMM.

Part: FITTING — CORRODED (RT ENGINE) · airframe 20,216 hrs · 14,328 cycles

RIGHT ENGINE AFT THRUST FITTING PITTED. (ENG CHANGE) REPLACED RIGHT ENGINE AFT THRUST FITTING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,778 hrs · 14,039 cycles

AFT OVERHEAD EMERGENCY LIGHT INOP. (FLT 4591) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,488 hrs · 13,056 cycles

ONE EMERGENCY LIGHT INOP. (FLT 4883) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,308 hrs · 12,926 cycles

AFT CEILING EMERGENCY LIGHT INOP. (FLT 4537) RELAMPED EMERGENCY LIGHT.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 17,446 hrs · 12,273 cycles

FLOOR LEVEL EMERGENCY EXIT SIGN AT MAIN CABIN ENTRANCE INOP. (FLT 4563) REPLACED NR 1 EMERGENCY BATTERY POWER SUPPLY.

Part: BEAM — CORRODED (FUSELAGE) · airframe 17,724 hrs · 12,478 cycles

FS 280 BEAM CORRODED. (C CHECK) REPAIRED PER SRM.

Part: FRAME — CORRODED (PYLON) · airframe 17,724 hrs · 12,478 cycles

ENGINE PYLONS K-FRAME MOUNTS CORRODED. (C CHECK) REPLACED PER AMM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 17,724 hrs · 12,478 cycles

FS 280 BEAM CRACKED. (C CHECK) REPAIRED PER REO.

Part: SILL — CORRODED (PAX DOOR) · airframe 17,724 hrs · 12,478 cycles

PASSENGER DOOR SILL CORRODED. (C CHECK) REPLACED PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 17,724 hrs · 12,478 cycles

FS 280 STIFFENERS CRACKED. (C CHECK) REPLACED PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,724 hrs · 12,478 cycles

LOWER FUSELAGE CLIPS CRACKED IN AREA OF FS 300-400. (C CHECK) REPLACED PER SRM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 17,329 hrs · 12,195 cycles

FLT 4853 - ONE OVERHEAD EMERGENCY CEILING FLOODLIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,174 hrs · 12,089 cycles

FLT 4770 - FORWARD MOST CEILING EMERGENCY FLOODLIGHT INOP. RELAMPED.

Part: LIGHT — NOT SEATED (CABIN) · airframe 17,084 hrs · 12,015 cycles

FLT 4716 - LIGHT BULB IN EMERGENCY LIGHT BURNED OUT. RESEATED LAMP IN FIXTURE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 17,053 hrs · 11,995 cycles

FLT 4718 - DAMAGE TO FUSELAGE SKIN, RIGHT SIDE OF AIRCRAFT AFT OF SERVICE DOOR. REPAIRED PER REO.

Part: WINDOW — CRACKED (COCKPIT) · airframe 16,800 hrs · 11,796 cycles

FLT 4863 - ON APPROACH, RIGHT SIDE WINDOW CRACKED. REPLACED WINDOW.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 16,685 hrs · 11,721 cycles

FLT 4719 - FWD CEILING EMERGENCY LIGHT INOP. RELAMPED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 16,479 hrs · 11,576 cycles

AFT CEILING OVERWING EMERGENCY LIGHT INOP (FLT 4399). REPLACED NR 3 BATTERY CHARGER AND BATTERY. P/N: AD-2013-1A, S/N ON: 11467, S/N OFF: 83440.

Part: O-RING — LEAKING (NR 1 HYD SYSTEM) · airframe 15,229 hrs · 10,710 cycles

HYDRAULIC SYSTEM NR 1 QUANTITY INDICATION DECREASED TO 0% WITH AN EDP NR 1 CAUTION MESSAGE. (FLT 3898) REPLACED O-RING ON THE QUICK CONNECT COUPLING IN THE PYLON FOR THE LT THRUST REVERSER. OPS CHECK GOOD.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,907 hrs · 10,501 cycles

FS 280 BEAM IS CRACKED AND CORRODED AT RBL9, FOUND AT C-CHECK. COMPLIED WITH REQUIRED REPAIRS PER CRJ700/900 SRM 51-42-06.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,907 hrs · 10,501 cycles

COCKPIT FLOOR SUPPORT AT FS280 IS CRACKED AND CORRODED AT RBL9, FOUND AT C-CHECK. REPAIRED COCKPIT FLOOR SUPPORT PER CRJ700/900 SRM 51-42-06.

Part: LIGHT — BROKEN (CABIN) · airframe 13,956 hrs · 9,878 cycles

SERVICE DOOR OVERHEAD EMERGENCY LIGHT IS BROKEN. REPLACED LIGHT ASSEMBLY.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 13,765 hrs · 9,762 cycles

FLT 4035 - HYDRAULIC SYSTEM NR 2 QUANTITY INDICATION SHOWS 0 PERCENT. REPLACED NR 2 ENGINE DRIVEN PUMP IAW AMM 29-11-01.

Part: WINDOW — CRACKED (COCKPIT) · airframe 13,625 hrs · 9,675 cycles

FLT 4011 - CAPTAINS SIDE WINDOW CRACKED. REPLACED CAPTAINS SIDE WINDOW IAW 56-12-01 P/N: NP-139322-11, S/N OFF: 02098H3465.

Part: MOUNT — CORRODED (RT ENGINE) · airframe 13,613 hrs · 9,669 cycles

RIGHT ENGINE, FORWARD ENGINE MOUNT LINK ASSEMBLY LOWER BUSHING AND THROUGH BUSHING IS CORRODED. REPLACED FORWARD MOUNT LINK AND BUSHING IAW 71-23-01.

Part: WINDOW — CRACKED (COCKPIT) · airframe 13,326 hrs · 9,476 cycles

RIGHT WINDOW CRACKED WHILE AT ALTITUDE. REPLACED RIGHT SIDE WINDOW IAW 56-12-01. OPS CHECK GOOD, P/N OFF NP-139322-001, S/N 02070H1423.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 12,436 hrs · 8,941 cycles

LEFT WINDSHIELD CRACKED ON CLIMB-OUT, RETURNED TO SLC. LEFT WINDSHIELD WAS REPLACED IAW MM 56-11-01, P/N OFF: NP-139321-003 S/N OFF: 02085H2662.

Part: OXYGEN MASK — UNWANTED DEPLOY (LAVATORY) · airframe 12,370 hrs · 8,903 cycles

FORWARD LAV 02 MASK WAS FOUND DEPLOYED. RESTOWED 02 MASKS IN FORWARD LAV.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 12,141 hrs · 8,782 cycles

RIGHT FRONT WINDSHIELD CRACKED IN FLIGHT. REPLACED RIGHT WINDSHIELD IAW MM 56-11-01.

Part: COMPUTER — MALFUNCTIONED (FUEL SYSTEM) · airframe 11,379 hrs · 8,266 cycles

FLIGHT 5440 - FUEL CHANNEL 1/2 CAUTION AND AUTO CROSSFLOW INHIBIT CAUTION MESSAGES. CENTER TANK AND TOTAL FUEL INDICATIONS BLANK. DECLARED EMERGENCY, RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. RESET NR 1 AND NR 2 FUEL COMPUTER.

Part: INLET — DENTED (RT NACELLE) · airframe 11,050 hrs · 5,591 cycles

RIGHT ENGINE LOWER FAN COWL IS DENTED. REPAIRED RT LOWER COWL IAW REO 670-54-16-694.

Part: FAN BLADE — OUT OF BALANCE (RT ENGINE) · airframe 5,537 hrs · 4,061 cycles

FLIGHT 5232 - EN ROUTE CVG-STL F/A REPORTS SIGNIFICANT VIBRATION IN THE CABIN, FLIGHT RETURNED TO CVG. REPLACED THE RIGHT ENGINE FAN BLADE NR 6.

Part: FAN BLADE — OUT OF BALANCE (RT ENGINE) · airframe 5,537 hrs · 4,061 cycles

FLIGHT 5232 - EN ROUTE CVG-STL F/A REPORTS SIGNIFICANT VIBRATION IN THE CABIN, FLIGHT RETURNED TO CVG. REPLACED THE RIGHT ENGINE FAN BLADE NR 7.

Part: FAN BLADE — OUT OF BALANCE (RT ENGINE) · airframe 5,537 hrs · 4,061 cycles

FLIGHT 5232 - EN ROUTE CVG-STL F/A REPORTS SIGNIFICANT VIBRATION IN THE CABIN, FLIGHT RETURNED TO CVG. REPLACED THE RIGHT ENGINE FAN BLADE NR 8.

Part: FAN BLADE — OUT OF BALANCE (RT ENGINE) · airframe 5,537 hrs · 4,061 cycles

FLIGHT 5232 - EN ROUTE CVG-STL F/A REPORTS SIGNIFICANT VIBRATION IN THE CABIN, FLIGHT RETURNED TO CVG. REPLACED THE RIGHT ENGINE FAN BLADE NR 20.

Part: FAN BLADE — OUT OF BALANCE (RT ENGINE) · airframe 5,537 hrs · 4,061 cycles

FLIGHT 5232 EN ROUTE CVG-STL F/A REPORTS SIGNIFICANT VIBRATION IN THE CABIN, FLIGHT RETURNED TO CVG. REPLACED THE RIGHT ENGINE FAN BLADE NR 21.

Part: FAN BLADE — OUT OF BALANCE (RT ENGINE) · airframe 5,537 hrs · 4,061 cycles

FLIGHT 5232 - EN ROUTE CVG-STL F/A REPORTS SIGNIFICANT VIBRATION IN THE CABIN, FLIGHT RETURNED TO CVG. REPLACED THE RIGHT ENGINE FAN BLADE NR 22.

Part: OVERHEAT SENSOR — MALFUNCTIONED (E/E BAY) · airframe 9,906 hrs · 7,332 cycles

FLIGHT 5131 - EN ROUTE IAD-DCA RECEIVED A BLEED DUCT WARNING MESSAGE, FLIGHT RETURNED TO THE FIELD. REPOSITIONED LEFT SENSING ELEMENTS IN AFT EQUIPMENT BAY THAT MAY HAVE BEEN TOUCHING EACH OTHER.

Part: RELAY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 7,465 hrs · 5,627 cycles

CABIN EMERGENCY LIGHTS FLICKER ON AND OFF. REPLACED RELAY K135.

Part: VANE — CRACKED (TE FLAPS) · airframe 7,435 hrs · 5,601 cycles

RT OUTBOARD FLAP VANE IS CRACKED. REPAIRED RT OUTBOARD FLAP VANE UPPER SKIN IAW BRAS EO 601R-52-6696.

Part: VANE — CRACKED (RT OB FLAP) · airframe 7,435 hrs · 5,601 cycles

RT OUTBOARD FLAP VANE HAS 0.5 INCH CRACK ON UPPER SKIN APPROX 24 INCHES FROM INBOARD EDGE. CUT OFF INBOARD END OF SKIN PANEL TO REMOVE DAMAGE. FABRICATED AND INSTALLED REPAIR SKIN AND INTERNAL SPLICE DOUBLER (2024-13-040) IAW BRAS EO 601R-52-6696.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,435 hrs · 5,601 cycles

LT AND RT LOWER WEBS BELOW FLOOR AT FS 280 ARE CORRODED FROM LBL36 TO RBL36. REMOVED CORRODED WEBS AND INSTALLED NEW WEBS IAW REO 6670-53-11-052 REV A.

Part: HINGE FITTING — CRACKED (SPOILERS) · airframe 7,435 hrs · 5,601 cycles

RT MULTI-FUNCTION SPOILER CENTER HINGE FITTING CRACKED IN HALF. REMOVED CRACKED FITTING AND INSTALLED NEW FITTING P/N CC670-17113-5 IAW CRJ AMM 57-73-27-400-801-A01.

Part: SKIN — CORRODED (FUSELAGE) · airframe 7,435 hrs · 5,601 cycles

CORROSION ON INNER SIDE OF SKIN ON FWD SIDE BL 10R TO 10L AND AFT SIDE BL 0 TO 10R OF AVIONICS BAY CUTOUT. REMOVED CORROSION AT AVIONICS BAY DOOR CUTOUT IAW BOMBARDIER EO 601R-53-6614.

Part: BULKHEAD — CORRODED (FUSLEAGE) · airframe 7,435 hrs · 5,601 cycles

FS 280 BULKHEAD LOWER WEBS ARE CORRODED BEYOND LIMITS FROM LBL 36 TO RBL 36. REPLACED THE FS 280 BULKHEAD LOWER WEBS IAW BOMBARDIER REO 670-53-11-052 REV A REPAIR 2.

Part: CYLINDER — CORRODED (NLG) · airframe 7,435 hrs · 5,601 cycles

NLG OUTER CYLINDER P/N 52101-1, S/N BA0025 CORRODED. CORROSION REPAIRED IAW BOMBARDIER REO 670-32-21-058, GOODRICH SCR 0008-04 REV C, BOMBARDIER REO 670-32-21-0030 AND GOODRICH SCR 0001-005.

Part: CYLINDER — DAMAGED (NLG) · airframe 7,435 hrs · 5,601 cycles

NLG OUTER CYLINDER P/N 52101-1, S/N BA0025 HAS HOLE IN THE CHROME BAND. REPAIR NLG OUTER CYLINDER IAW BOMBARDIER REO 670-32-21-0059 AND GOODRICH SCR 0024-05.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,435 hrs · 5,601 cycles

TRANSVERSE BEAM AT FS 280 FROM LBL 36 TO RBL 36 CORRODED ALONG UPPER AND LOWER EDGES. REPLACED THE TRANSVERSE BEAM AT FS 280 IAW BOMBARDIER REO 670-53-11-047 REV C.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 7,435 hrs · 5,601 cycles

CORROSION FOUND NEAR POTABLE WATER DOOR AT FS 364 APPROXIMATELY 3 INCHES LONG, 700 INCHES WIDE AND BETWEEN .005 AND .007 INCHES DEEP. REMOVED CORROSION AT POTABLE WATER DOOR SURROUND AREA IAW BOMBARDIER EO 601R-53-6620.

Part: ODOR — DETECTED (COCKPIT) · airframe 1,762 hrs · 1,392 cycles

FLIGHT 5887 DURING CLIMBOUT OF CVG, SMOKE (ODOR) WAS NOTED IN CABIN AND COCKPIT, CREW DECLARED AN EMERGENCY, RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. PERFORMED A VISUAL INSPECTION OF CABIN LIGHTING, OPERATED APU AND AIR CONDITIONING PACKS. DISCREPANCY COULD NOT BE DUPLICATED.

Part: HYDRAULIC LINE — CHAFED (HYDRAULIC SYS) · airframe 6,147 hrs · 4,633 cycles

FLIGHT 5048, EDP 2A FAILED AND LOSS OF FLUID QUANTITY. REPLACED SECTION OF HYDRAULIC TUBING WHICH HAD CHAFED THRU IN THE AFT EQUIPMENT BAY.

Part: CONTROL HANDLE — FAULTY (COCKPIT) · airframe 4,411 hrs · 3,282 cycles

FLIGHT 5287 GEAR DISAGREE WARNING. REPLACED THE GEAR SELECTOR LEVER.

Part: FAN BLADE — DAMAGED (RT ENGINE) · airframe 3,286 hrs · 2,439 cycles

FLIGHT 5646 RIGHT ENGINE VIBRATION 1.5 TO 2.1. REPLACED ALL 28 FAN BLADES.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 2,931 hrs · 2,174 cycles

PRESSURE BULKHEAD WEB AT FS 1098 STR 8L - 9L IS CRACKED AT NR 4 HYD LINE CONNECTION. PERFORMED MAJOR REPAIR IN ACCORDANCE WITH CANADAIR REO 670-53-61-034 REV B AND DEVIATION ENG ORDER (WVAC) 601R-53-4406.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 2,931 hrs · 2,174 cycles

PRESSURE BULKHEAD WEB AT FS 1098 STR 8R, 9R IS CRACKED AT NR 4 HYD LINE CONNECTION. PERFORMED MAJOR REPAIR IN ACCORDANCE WITH CANADAIR REO 670-53-61-034 REV B.

Part: CONTROL COLUMN — BINDING (COCKPIT) · airframe 2,767 hrs · 2,042 cycles

FLIGHT 5877 AILERON CONTROLS WERE BINDING DURING FLIGHT. LOOSENED AND THEN RETORQUED CO-PILOTS CONTROL YOKE. NO DEFECTS NOTED.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 1,583 hrs · 1,155 cycles

FLIGHT 5207 GEAR DISAGREE WARNING DURING RETRACTION. REPLACED THE LANDING GEAR SELECTOR VALVE.

Part: SERVICE DOOR · airframe 1,014 hrs · 728 cycles

FLIGHT 5936 EXTERNAL POWER PANEL LEFT OPEN.INSPECTED EXTERNAL POWER DOOR FOR DAMAGE, AND SECURED DOOR CLOSED.

Part: CONTROLLER — INOPERATIVE (AUTOCOARSEN)

PILOT REPORTED THAT THE AUTOCOARSEN SYSTEM WOULD NOT ARM DURING TAKEOFF ROLL. TAKEOFF WAS ABORTED.