N614QX

Service difficulty reports · 465

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N614QX' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR QXEA2010041500268Striker · corrodedC-CHECK SERVICE DOOR STRIKER SEAL HAS CORROSION. REMOVED CORROSION IAW CXRJ700 SRM 51-21-06-001-001-A01. PERFORMED LPI IAW NDTM LPI 51-20-008-230-A01. STRIKER SEAL FOUND TO BE OUT OF LIMITS OF SRM 53-21-23-101-001-A01. REMOVED SERVICE DOOR STRIKER SEAL ANDApr 14, 2010 · N614QX · Cndair CL6002C10 · Service DoorsSDR QXEA2010041500267Fitting · corrodedC-CHECK FOUND CORROSION ON FWD JACK FITTING BETWEEN FS 265-FS280 AND STRINGER 26L AND 26R. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDED CORROSION BETWEEN FS265-FS280 ON FWD JACK FITTING IAW SRM 51-21-06-001-001-A01. BLENDED CORRODION BETWEEN FS 2Apr 14, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, StructureSDR QXEA2010041500266Strap · corrodedC-CHECK DURING INSP FOUND CORRODED ON FS 280 JOINT STRAP AT STRINGER 27RBL 3". REMOVED 2 RIVETS AND BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDED AREA IS A NO-DAMAGE ALLOWED AREA IAW SRM 53-21-01-101-002-A01. PERFORMED ECI ON BLENDED AREA . NO CApr 14, 2010 · N614QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR QXEA2010041500265Seat Track · corrodedC-CHECK SUSPECT CORROSION ON LT SIDE SEAT TRACK FS379-485. BLENDED CORROSION FOUND TO BE OUT OF LIMITS IAW REO 670-53-03-013. REMOVED LT SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW LT SEAT TRACK IAW AMM53-00-49-400-801.Apr 14, 2010 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010041500263Attach Angle · corrodedC-CHECK ATTACHED ANGLE CORRODED IN AVIONICS BAY UNDER FLOORBOARDS 141ALF. REMOVED ANGLE IAW SRM 51-42-06-001-001-A01. FOUND OUT OF LIMITS IAW SRM 53-00-00-001-A01. LOCATED HOLES IN NEW ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED NEW ANGLE IAW SRM 51-42-0Apr 13, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR QXEA2010041500260Stringer · corrodedC-CHECK - DURING INSP FOUND CORROSION ON STR 26 RT JUST AFT OF FS 280 JOINT STRAP ON STRINGER ATTACH FLANGE. BLENDED AREA OF CORROSION ON STRINGER IAW SRM 51-21-06-001-001-A01. BLENDED AREA FOUND TO BE A "NO DAMAGE ALLOWED" AREA IAW SRM 53-21-03-101-002-A01Apr 13, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR QXEA2010041500264Skin · corrodedRFD C-CHECK INNER SIDE OF FUSELAGE SKIN AROUND AVIONICS DOOR CUT-OUT HAS CORROSION. REMOVED CORROSION IAW REO670-53-21-242. PERFORMED LPI. NO CRACKS OR CORROSION FOUND IAW NDTM LPI-51-20-008-230-A01, REO670-53-21-242. COMPLETED REPAIR IAW SRM 51-21-16-001-Apr 12, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR QXEA2010041500261Seat Track · corrodedC-CHECK EVIDENCE OF CORROSION ON RT SIDE SEAT TRACK FROM FS 784 TO FS 863. FOUND CORROSION OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801A2. INSTALLED SEAT TRACK IAW RJ700 AMM 53-00-49-400-801-A02.Apr 12, 2010 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010041200254Sill · chafedC-CHECK DURING INSP FOUND AFT CARGO DOOR SILL TO BE CHAFED AND CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED ECI IAW NDTM ECI 51-20-006. FOUND BLEND OUT OF LIMITS SENT TO ENGINEERING TREATED AND PRIMED AND PAINTED AS REQUIRED IAW REO 6Apr 12, 2010 · N614QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR QXEA2010041500262Attach Angle · corrodedC-CHECK DURING INSP, FOUND CORROSION ON ATTACH ANGLE 26R FWD OF FS364 ON ITS OTBD SIDE. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-12-00-001-001 AND SRM 53-21-23-101-001-A01. LOCATED HOLES IN NEW ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED NEWApr 11, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR QXEA2010041300257Angle · corrodedC-CHECK SERVICE DOOR MID CAP ANGLE HAS CORROSION. REMOVED CORROSION IAW SRM 51-12-001-001-A01 AND 53-21-23-101-002-A01. REMOVED MID CAP ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED , DRILLED, AND DE-BURRED NEW MID CAP-ANGLE IAW SRM 51-40-11-001-001-A01. INSApr 11, 2010 · N614QX · Cndair CL6002C10 · Service DoorsSDR QXEA2010041200256Seat Track · corrodedRFD C-CHECK EVIDENCE OF CORROSION ON RT SEAT TRACK FROM FS 708 TO FS 762. BLENDED OUT CORROSION FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED RT SEAT TRACK IAW AMM 53-00-49-000-801-A02. INSTALLED NEW SEAT TRACKS IAW AMM 53-00-49-000-801-A02.Apr 9, 2010 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010041200255Seat Track · corrodedRFD C-CHECK EVIDENCE OF CORROSION ON LT SIDE SEAT TRACK FROM FS 677 TO FS 708. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED LT SIDE SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW LT SIDE SEAT TRACK FROM 677 TO 708 IAW AApr 9, 2010 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010041200253Seat Track · corrodedC-CHECK CORROSION FOUND ON SECTION OF THE LT FLOOR SEAT TRACK FROM FS379 TO FS485. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK FROM FS 379 TO 485 IAW AMM 53-00-49-000-801. INSTALLED NEApr 9, 2010 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010041200252Skin · damagedC-CHECK. COMPLY WITH HORIZON TASK CARD REO 670-57-52-134/3. DRILLED OUT ALL BLIND RIVETS IAW REO 670-57-52-134. REMOVED DAMAGED SKIN IAW REO 670-57-52-138. PERFORMED LPI ON CUT LINES. NO CRACKS FOUND. IAW NDTM LPI 51-20-008-230-A01. REO 670-57-52-138. Apr 9, 2010 · N614QX · Cndair CL6002C10 · Wing, Plate/SkinSDR QXEA2010041200247Angle · corrodedC-CHECK. DURING INSP FOUND CORRODED ANGLE FWD CAP AT PAX DOOR. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. INSTALLED NEW ANGLE IAW SRM 51-42-06-001-001-A01.Apr 9, 2010 · N614QX · Cndair CL6002C10 · Passenger/Crew DoorsSDR QXEA2010041200245Sill · corrodedC-CHECK-PAX DOOR LOWER SILL HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. REMOVED DOOR SILL IAW SRM 51-42-06-001-001-A01. INSTALLED NEW SILL IAW SRM 51-42-06-001-001-A01.Apr 9, 2010 · N614QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR QXEA2010040900244Skin · corrodedC-CHECK CORROSION ON BELLY SKIN LOCATED WHERE ADF ANTENNA IS LOCATED. BLENDED AREAS IAW SRM 51-21-06-001-001-A01. FOUND BLEND OUT OF LIMITS IAW SRM 53-31-01-101-003. PERFORMED ECI, NO CRACKS OR CORROSION FOUND AT THIS TIME IAW NDTM ECI 51-20-006-250-A01 ANDApr 9, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR QXEA2010040900243Panel · chafedC-CHECK CHAFE ON L/E OF FLAP PANEL 584EB. BLENDED CHAFED DAMAGE IAW SRM 51-12-00-001-001-A01. FOUND BLEND TO BE OUT OF LIMITS IAW SRM 57-52-01-101-001-A01. TREATED, PRIMED, TOP-COATED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, 51-25-16-001-001-A01.Apr 8, 2010 · N614QX · Cndair CL6002C10 · Leading Edge DevicesSDR QXEA2010040900242Seat Track · corrodedC-CHECK CORROSION FOUND ON SECTION OF RT FLOOR SEAT TRACK FROM FS 349 TO FS 485. BLENDED CORROSION, FOUND BLEND OUT OF LIMITS IAW REO 670-53-00-13. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A02. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A02.Apr 8, 2010 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2011004090024Seat Track · corrodedC-CHECK EVIDENCE OF CORROSION ON LT SIDE SEAT TRACK FROM FS 708 TO FS 762. BLENDED CORROSION, FOUND BLEND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A02. DRILL HOLES AND COUNTERSUNK NEW TRACK IAW SRM 51-40-11-001-Apr 8, 2010 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010040900236Seat Track · corrodedC-CHECK - SUSPECT CORROSION ON LT SIDE SEAT TRACK FROM FS 572 TO 669.40. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.Apr 8, 2010 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010040900240Floorbeam · corrodedC CHECK- COCKPIT PANEL FLOOR SUPPORT ANGLE AT FS 280 SHOWS SIGNS OF CORROSION. BLENDED CORROSION, FOUND CORROSION OUT OF LIMITS IAW SRM5300-00-001-A01 PAGE 3. LOCATED FASTENER HOLE IN NEW ANGLE IAW SRM51-40-11-001-001-A01. INSTALLED NEW A IAW SRM 51-42-21-Apr 7, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR QXEA2010040900239Floorbeam · corrodedC CHECK -LT AND RT SIDE OF 280 BEAM SHOWS SIGNS OF CORROSION. BLENDED CORROSION RT 280 BEAM IAW SRM 51-11-00-001-001-A01. FOUND BEAM TO BE CRACKED. REMOVED BEAM IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. CUT NEW 280 BEAM. PERFORMED LPI ON CUTLIApr 7, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR QXEA2010040900238Web · corrodedC-CHECK - CORROSION FOUND ON R/H WEB AT FS 280.00. BLENDED CORROSION, FOUND BLENDS TO BE OUT OF LIMITS IAW SRM 53-11-10-991-805. REMOVED WEB IAW SRM 57-42-06-001-001-A01 AND 51-42-13-001-001-A01. LOCATED ALL FASTENER HOLES IN NEW WEB IAW SRM 51-40-11-001-0Apr 7, 2010 · N614QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR QXEA2010040900237Frame · corrodedC-CHECK - CORROSION FOUND ON FWD WEB SIDE OF FRAME 295.00 AROUND STGR 26R CUTOUT. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, BLENDS WITHIN LIMITS IAW SRM 53-21-06-101-002-A01. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-21-06-001-001-AApr 7, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, FrameSDR QXEA2010040800235Frame · corrodedC-CHECK - CORROSION ON THE ATTACH FLANGE AT FRAME FS 549.00 BETWEEN STR 27 AND 26L. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. REMAINING MATERIAL THICKNESS IS .059" AND WITHIN LIMITS OF SRM 53-31-06-101-003-A01. TREATED AND PRIMED IAW SRM 51-21-11-001Apr 7, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, FrameSDR QXEA2010040800234Frame · corrodedC CHECK - CORROSION ON THE ATTACH FLANGE AT FRAME FS 517.00 BETWEEN STR 27 AND 26R. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. REMAINING MATERIAL THICKNESS IS .045" AND WITHIN LIMITS OF SRM 53-31-06-101-003-A01. TREATED AND PRIMED IAW SRM 51-21-11-001Apr 7, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, FrameSDR QXEA2010040800233Frame · corrodedC CHECK - CORROSION ON THE ATTACH FLANGE AT FRAME FS 517.00 BETWEEN STR 27 AND 26L. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. REMAINING MATERIAL THICKNESS IS .068" AND WITHIN LIMITS OF SRM 53-31-06-101-003-A01. TREATED AND PRIMED IAW SRM 51-21-11-001Apr 7, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, FrameSDR QXEA2010040800232Frame · corrodedC CHECK - CORROSION ON THE ATTACH FLANGE AT FRAME FS 517.00 BETWEEN STR 26L AND 25L. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. REMAINING MATERIAL THICKNESS IS .067" AND WITHIN LIMITS OF SRM 53-31-06-101-003-A01. TREATED AND PRIMED IAW SRM 51-21-11-001Apr 7, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, FrameSDR QXEA2010040800231Frame · corrodedC CHECK -CORROSION ON THE ATTACH FLANGE AT FRAME FS 517.00 BETWEEN STR 23L AND 22L. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. REMAINING MATERIAL THICKNESS IS .069" AND WITHIN LIMITS OF SRM 53-31-06-101-003-A01. TREATED AND PRIMED IAW SRM 51-21-11-00Apr 7, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, FrameSDR QXEA2010040800230Frame · corrodedC CHECK -CORROSION ON THE FWD FREE FLANGE ON FRAME FS 517.00 BETWEEN STR 26L AND 26R. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. REMAINING MATERIAL THICKNESS IS .048" AND WITHIN LIMITS OR SRM 53-31-06-101-003-A01. TREATED AND PRIMED IAW SRM 51-21-11-Apr 7, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, FrameSDR QXEA2010040800229Frame · corrodedC-CHECK - CORROSION ON THE ATTACH FLANGE OF FRAME FS 629.00 BETWEEN STR 27 AND 26R. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED .003", REMAINING MATERIAL THICKNESS IS .060" AND WITHIN LIMITS OR SRM 53-31-06-101-003-A01. ALODINED IAW 51-21-11-00Apr 7, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, FrameSDR QXEA2010040700227Structure · chafedC CHECK - CHAFING AT STR 27 FS 977.00 UNDER PANEL DL. BLENDED OUT DAMAGED AREA IAW SRM 51-12-00-001-001-A01. BLEND FOUND TO BE WITHIN LIMITS IAW REO 670-53-00-14. PERFORMED LPI IAW NDTM LPI 51-20-008-230-A01. ETCHED AND ALODINED IAW SRM 51-21-11-001-001-A0Apr 6, 2010 · N614QX · Cndair CL6002C10 · Fuselage Main, StructureSDR QXEA2010040700225Seat Track · corrodedC CHECK - EVIDENCE OF CORROSION ON LT SIDE SEAT TRACK FROM FS 784.00 TO FS 863.00. BLENDED OUT ALL CORROSION AND FOUND TO BE WITHIN LIMITS OF REO 670-53-00-13. ETCHED AND ALODINED LT SIDE SEAT TRACK IAW SRM 51-21-11-001-001-A01.Apr 6, 2010 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010040700224Seat Track · corrodedC CHECK - EVIDENCE OF CORROSION ON RT SIDE SEAT TRACK FROM FS 677.00 TO FS 708.00. BLENDED OUT ALL CORROSION AND FOUND TO BE WITHIN LIMITS OF REO 670-53-00-13. TREATED IAW REO 670-53-00-13.Apr 6, 2010 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010040700223Seat Track · corrodedC CHECK - SUSPECT CORROSION ON SIDE SEAT TRACK RT FROM FS 572-669.4. BLENDED OUT ALL CORROSION FOUND TO BE WITHIN LIMITS IAW REO 670-53-00-13. TREATED IAW REO 670-53-00-13.Apr 5, 2010 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010040600220Seat Track · corrodedC-CHECK - SUSPECT CORROSION ON LT SIDE SEAT TRACK FROM FS 485 TO 572. BLENDED LT SIDE SEAT TRACK FS 485 TO 572 CORROSION. ORIGINAL THICKNESS .110, BLENDED .020 MAX ALLOWABLE .035", REMAINING MATERIAL .090" FOUND TO BE WITHIN LIMITS IAW REO 670-53-00-013. EApr 5, 2010 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010040600221Seat Track · corrodedC-CHECK - SUSPECT CORROSION ON SIDE SEAT TRACK FROM FS 379 TO 485 FURTHER INVESTIGATION REQUIRED ON RT SIDE. BLENDED OUTT ALL CORROSION TO .031" DEEP BY 1.0" WIDE BY 1.0" LONG. ORIGINAL MATERIAL THICKNESS IS .105" REMAINING MATERIAL AFTER BLAND .074" CORROSApr 5, 2010 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010040600222Seat Track · corrodedC-CHECK - SUSPECT CORROSION ON SIDE SEAT TRACK FROM FS 485 TO 572 FURTHER INVESTIGATION REQUIRED ON RT SIDE. BLENDED OUT ALL CORROSION TO .024" DEEP BY .375 WIDE BY 2" LONG. ORIGINAL MATERIAL THICKNESS IS .105", REMAINING MATERIAL AFTER BLENDING .081" CORROSApr 5, 2010 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010040600215Skin · chafedC-CHECK - RT LOWER L/E OF AILERON HAS CHAFING ON SKIN. BLENDED DAMAGE ON THE RT LOWER L/E SKIN AT AILS 330.68 AND AILS 370.66 TO A SMOOTH AND DAMAGE FREE CONDITION IAW SRM 51-12-00-001-001-A01. ALL BLENDS ARE WITHIN LIMITS IAW SRM 57-61-01-101-001-A01. ETCApr 4, 2010 · N614QX · Cndair CL6002C10 · AileronsSDR QXEA2010040600214Skin · chafedC-CHECK - LT UPPER L/E OF AILERON HAS CHAFING ON SKIN. BLENDED CHAFE DAMAGE ON UPPER L/E AT AILS 365.00 IAW SRM 51-12-00-001-001-A01. BLEND IS A MAX 2.0 INCH LONG AND .75 INCH WIDE. REMAINDER MAX OF .005 OUT OF ORIGINAL .090. BLEND IS WITHIN LIMITS IAW SRApr 4, 2010 · N614QX · Cndair CL6002C10 · AileronsSDR QXEA2010022500145Panel · hotPASSENGER COMPLAINS THAT THE SIDEWALL AT ROW 18E WAS TO HOT TO TOUCH DURING APPROACH. FOUND SIDEWALL TEMP AT ROW 18AB & 18DE BOTH FOLLOW DEMAND TEMPERATURE, AIR CONDITIONING DUCTS RUN BEHIND SIDEWALL IN THAT LOCATION. NO DEFECTS FOUND AIR FLOW TO GASPERS IS NFeb 21, 2010 · N614QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR QXEA2009101900825Controller · malfunctionedINBD GROUND SPOILER FAULT STATUS MESSAGE AFTER LIFTOFF. RETURNED TO FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. INTERROGATED MDC, FOUND FAULT IN HISTORY, "SSCU 1/NO ASCU-1, BUS INPUT". C/W FIM ISOLATION IAW FIM 27-61-05-810-839-A02. REMOVED AND REPLACED ANOct 15, 2009 · N614QX · Cndair CL6002C10 · Brake Anti-Skid SectionSDR QXEA2009100600762Wire Harness · malfunctionedWHILE AT CRUISE "AFT CARGO FOOR" CAUTION AND "PROX SYS FAULT2" STATUS MESSAGE. DIVERTED AND ACCOMPLISHED A UNEVENTFUL LANDING. INSPECTED AFT CARGO DOOR UPON ARRIVAL AT GATE, FOUND DOOR CLOSED AND LOCKED. INSPECTED MDC MESSAGE - AFT CARGO DOOR COVER, INPECTED Oct 2, 2009 · N614QX · Cndair CL6002C10 · Door System WiringSDR QXEA2009033000200Transducer · failedPDX - RIGHT AFTER T/O STALL FAIL CAUTION LIGHT CAME ON. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. IN MDC HISTORY FOUND "SPC L/R AOA DISAGREE". PERFORMED FUNCTIONAL TEST OF STALL PROTECTION COMPUTER PER CRJ700 AMM TASKS 27-35-01-720-801, FMar 24, 2009 · N614QX · Cndair CL6002C10 · Stall Warning SystemSDR QXEA2008110601169Wire Harness · chafedPDX - WIRE HARNESS TO STATIC INVERTER ON AFT RT SIDE OF REAR PRESSURE HAS CHAFED THRU HYDRAULIC LINE AND DAMAGED WIRES TO STATIC INVERTER. REPAIRED WIRE RHB0878-20 AT STATIC INVERTER BY SPLICING IAW CRJ 700 WM 74-00-01. INSTALLED STATIC INVERTER WITH A SERVINov 2, 2008 · N614QX · Cndair CL6002C10 · Ignition System WiringSDR QXEA200800689Floorbeam · corrodedRFD C4 CHECK LT SECTION OF THE 280 CROSSBEAM IS CORRODED. BLENDED CORROSION FROM LT FS 280 CROSSBEAM. .020 MATERIAL REMOVED, BLEND IS OUT OF LIMITS IAW REO 670-53-11-046. REMOVED LT SECTION OF 280 CROSSBEAM IAW CRJ 700 SRM 51-42-06. CUT NEW CROSSBEAM IAW RJun 12, 2008 · N614QX · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR QXEA200800688Sill · corrodedRFD C4 CHECK FOUND CORROSION ON SILL OF AFT CARGO BAY DOOR. BLENDED IAW REO 670-53-61-373, .002 MATERIAL REMOVED. PERFORMED ECI IAW REO 670-53-61-373 NO DEFECTS NOTED. TREATED, PRIMED AND PAINTED IAW REO 670-53-61-373.Jun 12, 2008 · N614QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR QXEA200800687Seat Track · corrodedRFD C4 CHECK NUMEROUS CORROSION SPOTS ON LT SIDE SEAT RAIL FS 379 TO FS 483. REMOVED CORROSION FROM SEAT TRACK AT FS 379 TO FS 483. .015 MATERIAL REMOVED TREATED IAW REO 670-53-00-013 AND SRM 51-21-16.Jun 12, 2008 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
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