GE CF34-8C1

Service difficulty reports · 1,415

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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 engine_model_key = 'CF348C1'
  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 QXEA2010022200111Seat Track · corrodedC-CHECK - LT FLOOR SEAT TRACK FROM FS 185.00 TO FS 581.00 IS CORRODED. FOUND SEAT TRACK TO BE BEYOND LIMITS IAW REO 670-53-00-013. REMOVED TRACK IAW AMM 53-00-49-000-801-A02. INSTALLED NEW TRACK IAW AMM TASK 53-00-49-400-801.Feb 19, 2010 · N612QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010022200113Striker · corrodedC CHECK - PAX DOOR STRIKER ANGLE IS CORRODED. FOUND STRIKER ANGLE TO BE CORRODED THROUGHOUT AND IS BEYOND LIMITS IAW SRM 53-21-23-001-001-A01 PAGE 101. REMOVED STRIKER ANGLE, LOCATED AND DRILLED NEW ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED STRIKER ANGLFeb 19, 2010 · N612QX · Cndair CL6002C10 · Door Warning SystemSDR QXEA2010022200116Seat Track · corrodedC-CHECK - LT SIDE SEAT TRACK FROM FS 863.00 TO 969.00 HAS NUMEROUS SPOTS OF CORROSION. EVALUATED LT SIDE SEAT TRACK, FOUND CORROSION ON SEAT TRACK SCREW COUNTERSINK. COUNTERSINK IS A NO ALLOWABLE DAMAGE AREA IAW REO 670-53-00-013. REMOVED LT SIDE SEAT TRACFeb 19, 2010 · N612QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010022200119Seat Track · corrodedC-CHECK - RT SIDE SEAT TRACK FROM FS 677.00 TO 711.00 HAS NUMEROUS SPOTS OF CORROSION. EVALUATED RT SIDE SEAT TRACK, FOUND CORROSION ON SEAT TRACK SCREW COUNTERSINK. COUNTERSINK IS A NO ALLOWABLE DAMAGE AREA IAW REO 670-53-00-013. REMOVED RT SIDE SEAT TRACFeb 19, 2010 · N612QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010022200120Seat Track · corrodedC-CHECK - LT SIDE SEAT TRACK FROM FS 570.00 TO 677.00 HAS NUMEROUS SPOTS OF CORROSION. EVALUATED LT SIDE SEAT TRACK FROM FS 570.00 TO 677.00, FOUND CORROSION ON SEAT TRACK SCREW COUNTERSINK. COUNTERSINK IS A NO ALLOWABLE DAMAGE AREA IAW REO 670-53-00-013. Feb 19, 2010 · N612QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010022200123Seat Track · corrodedC-CHECK - LT SIDE SEAT TRACK FROM FS 863.00 TO 969.00 HAS NUMEROUS SPOTS OF CORROSION. EVALUATED LT SIDE SEAT TRACK, FOUND CORROSION ON SEAT TRACK SCREW COUNTERSINK. COUNTERSINK IS A NO ALLOWABLE DAMAGE AREA IAW REO 670-53-00-013. REMOVED LT SIDE SEAT TRACKFeb 19, 2010 · N612QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010022200117Attach Bracket · gougedC CHECK - DURING INSP FOUND GOUGES ON LT LOWER CASCADE ATTACHMENT BRACKET. BLENDED 2 GOUGES SMOOTH IAW SRM 51-12-00-001-001-A01. PERFORMED LPI ON BLENDS, NO CRACKS NOTED AT THIS TIME IAW NDTM LPI 51-20-008. TREATED, PRIMED IAW SRM 51-21-11-001-001-A01 AND 5Feb 19, 2010 · N612QX · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR QXEA2010022200100Skin · chafedC-CHECK- 2 BELLY SKINS CHAFED AT FS 977 FROM PANELS 195DL/196DR. BLENDED CHAFED AREA IAW REO 670-53-00-014. PERFORMED LPI ON BLENDED AREAS, NO CRACKS NOTED AT THIS TIME, IAW REO 670-53-00-014 NDTM 51-20-08. ALL BLENDED AREAS ARE WITHIN LIMITS IAW REO 670-53Feb 18, 2010 · N612QX · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR QXEA2010022200101Fitting · damagedC-CHECK -LT MLG SIDE STAY FITTING DAMAGED AT UPPER OTBD FLANGE EDGE. BLENDED OUT DAMAGE AND WITHIN LIMITS IAW REO 670-57-11-043. PERFORMED LPI ON BLENDED AREAS, NO CRACKS NOTED AT THIS TIME, IAW LPI NDTM 51-20-08, REO 670-57-11-043. PERFORMED ROTO PEEN IAW Feb 18, 2010 · N612QX · Cndair CL6002C10 · Main Landing GearSDR QXEA2010022200102Fitting · damagedC-CHECK - RT MLG SIDE STAY FITTING DAMAGED 2 PLACES ON OTBD UPPER FLANGE. BLENDED OUT DAMAGE AND WITHIN LIMITS IAW REO 670-57-11-043. PERFORMED LPI ON BLENDED AREAS, NO CRACKS NOTED AT THIS TIME, IAW LPI NDTM 51-20-08, REO 670-57-11-043. PERFORMED ROTO PEENFeb 18, 2010 · N612QX · Cndair CL6002C10 · Main Landing GearSDR QXEA2010022200103Door Frame · damagedC CHECK - FWD CARGO BAY DOOR SURROUND STRUCTURE HAS GOUGES IN FWD LOWER CORNER AND AFT LOWER CORNER OF STRIKER SEAL. REMOVED DAMAGE IAW SRM 51-12-00-001-001-A01. BLENDED AREAS ARE WITHIN LIMITS IAW SRM 53-31-23-101-001-A01 AND 53-00-00-101-001-A01. TREATED,Feb 18, 2010 · N612QX · Cndair CL6002C10 · Fuselage Main, StructureSDR QXEA2010022200104Door Frame · gougedC-CHECK - FWD CARGO BAY DOOR SURROUND STRUCTURE HAS GOUGES IN FWD LOWER CORNER AND AFT LOWER CORNER OF SEAL RETAINER. DAMAGE FOUND TO BE DENTS NOT GOUGES. REMOVED DAMAGE IAW SRM 51-12-00-001-001-A01. BLENDED AREAS ARE WITHIN LIMITS IAW REO 670-52-35-127. Feb 18, 2010 · N612QX · Cndair CL6002C10 · Fuselage Main, StructureSDR QXEA2010022200105Structure · damagedC-CHECK - CHAFE DAMAGE FOUND ON RT ENG LOWER TRANSCOWL SLIDER INBD. BLENDED DAMAGED AREA IAW AND WITHIN TOLERANCE OF REO 670-78-34-384. TREATED AND PRIMED IAW SRM 51-21-11-001-001, 51-25-06-001-001. ALL WORK WAS PERFORMED IAW REO 670-78-34-384.Feb 18, 2010 · N612QX · Cndair CL6002C10 · Engine Thrust ReverserSDR QXEA2010021800093Seat Track · corrodedC CHECK -CORROSION ON LT FLOOR SEAT TRACK FROM FS 349.00 TO FS 485.00. FOUND CORROSION TO BE BEYOND LIMITS IAW REO 670-53-00-013. REMOVED LT FLOOR TRACK IAW AMM 53-00-49-000-801. PREPARED NEW SEAT TRACK IAW SRM 51-40-11-001-001-A01, TREATED IAW SRM 51-21-11Feb 17, 2010 · N612QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010021800094Seat Track · corrodedC-CHECK - CORROSION ON RT FLOOR SEAT TRACK FROM FS 349.00 TO FS 485. FOUND CORROSION TO BE BEYOND LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801, PREPPED NEW TRACK FOR INSTALL IAW SRM 51-40-11-001-001-A01, TREATED TRACK IAW SRM 51-Feb 17, 2010 · N612QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010021800095Seat Track · corrodedC-CHECK - CORROSION ON RT FLOOR SEAT TRACK FROM FS 581.00 TO FS 691.50. FOUND CORROSION TO BE BEYOND LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A01, PREPPED NEW TRACK FOR INSTALL IAW SRM 51-40-11-001-001, ETCHED AND ALODINED TRFeb 17, 2010 · N612QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010021800096Seat Track · corrodedC CHECK - NUMEROUS SPOT OF CORROSION ON LT FLOOR SEAT TRACK FROM FS 485.00 TO FS 570. FOUND CORROSION TO BE BEYOND LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801, DRILLED NEW TRACK FOR INSTALL IAW SRM 51-40-11-001-001, ETCHED AND AFeb 17, 2010 · N612QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010022200129Spring · failedBRAKE PEDALS, ESPECIALLY LT, DO NOT MOVE SMOOTHLY. BRAKES THEMSELVES ARE OK AS ARE RUDDER PEDALS. FOUND RETURN SPRING ON DUAL BRAKE RETURN VALVE FAILED. REPLACED WITH SERVICEABLE SPRING, OPS CHECKED WITH ACFT STATIONARY AND IN MOVEMENT. OPS CHECKED GOOD, OPENEFeb 16, 2010 · N610QX · Cndair CL6002C10 · Landing Gear Brake SystemSDR QXEA2010021800088Floorbeam · corrodedC-CHECK -SURFACE CORROSION FOUND ON TOP FLANGE OF FS 280.0 BEAM. BLENDED SURFACE CORROSION, REMOVED .002" MATERIAL IAW SRM 53-21-43-101-001-A01. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, 51-25-06-001-001-A01. APPLIED CFeb 15, 2010 · N612QX · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR QXEA2010021800089Floorbeam · corrodedC-CHECK -FLOORBEAM ANGLE ON FWD SIDE OF 280.0 IS CORRODED. REMOVED FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED NEW ANGLE IAW SRM 51-42-21-001-001-A01. INSTALLED NEW NUTPLATES USING CR3214-4 FASTENERS, ALL WORK IAW SRM 51-42-13-001-001-A01. APPLFeb 15, 2010 · N612QX · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR MASA2010020900135Fan Blade · lack of lubeRIGHT ENGINE VIB AT 1.8. C/W FAN BLADE LUBE.Feb 9, 2010 · N505MJ · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR CA091206002Actuator · failed(CAN) FLT CREW REPORTED A SLAT FAIL CAUTION MSG IN FLIGHT. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MX REPORTED THAT 2 TORQUE INDICATORS WERE TRIPPED ON THE RT WING AND ONE ON THE LT WING. RT WING, OTBD SLAT, INBD ACTUATOR REPLACED ANNov 24, 2009 · Cndair CL6002C10 · Leading Edge Slat ActuatorSDR MASA2009111400333O-Ring · defectiveASH FLT 7277 IND-ORD. FLIGHT DIVERTED, AN EMERGENCY DECLARED DUE TO LEFT ENGINE OIL PRESSURE WAS BELOW 25 PSI. MX INSTALLED O-RINGS ON STARTER.Nov 14, 2009 · N509MJ · Cndair CL6002C10 · Turbine Engine Oil SystemSDR QXEA2009102000828Duct · contaminatedRECEIVED SMOKE AFT LAVATORY WARNING LIGHT AFTER TAKEOFF. FA REPORTED SMELLING UNUSUAL ODOR. LIGHT WENT OUT. RETURNED TO FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. LANDING WAS ESTIMATED AT 69,500 LBS WITH A DESCENT RATE OF 100-200 FPM. DRIED INTERNAL ENGOct 16, 2009 · N610QX · Cndair CL6002C10 · Engine Cooling SystemSDR QXEA2009082400626Fadec · malfunctionedPDX - "L FADEC" CAUTION MSG. ALL ENGINE INDICATIONS NORMAL. RETURNED TO THE FIELD. LANDED BELOW MAX LANDING WEIGHT. MDC MESSAGE L FADEC FAILED SWITCH VERSION - DISAGREE SOFTWARE CHECK SUMS (A+B) DISAGREE. LABEL BIT 355A - 23 (BUILT IN TEST) FLAGGED WITH OAug 18, 2009 · N600QX · Cndair CL6002C10 · Fuel Control/Turbine EnginesSDR CA090521002Aileron · contaminated(CAN) CREW DECLARED EMERGENCY DUE TO LWD CAUTION AT FL 270 (RT AILERON JAMMED) FLIGHT DIVERTED BECAUSE OF AN AILERON JAM. DURING CLIMB TO FL270 MESSAGE "AP LWD" APPEARED - DISAPPEARED AND APPEARED SHORTLY AFTER AGAIN. CREW DISCONNECTED AUTOPILOT FOR CHECK OFMay 19, 2009 · Cndair CL6002C10 · Aileron Control SystemSDR CA090502001Circuit Breaker · failed(CAN) NR 2 ENG STARTED NORMALLY, DURING NR 1 START, EXPERIENCED A ENG HOT ICON WITH FADEC ABORT OF START. LOST AC ELECTRICAL POWER. NR 2 ENG & APU SHUTDOWN. ACFT TOWED BACK TO GATE. ACFT POWER SHUTDOWN. CREW REPORTED SYNOPTIC PAGE INDICATED AC BUSS 1 FAULTEDApr 25, 2009 · Cndair CL6002D24 · Electrical Power System WiringSDR CA090407020Window · cracked(CAN) THE F/O WINDSHIELD CRACKED ON TAKEOFF. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. REMOVED AND REPLACE THE F/O WINDSHIELD REFERENCE AMM 56-11-01.Apr 4, 2009 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA090326018Handle · defective(CAN) FLT 2233, FLT CREW REPORTED NO GEAR MOVEMENT WHEN GEAR SELECTED UP. QRH FOLLOWED AND ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED LANDING GEAR SELECTOR HANDLE AND OPS CHECKED GEAR RETRACTION SYS SERVICEABLE. Mar 12, 2009 · Cndair CL6002C10 · Landing Gear SelectorSDR QXEA2009011200009Valve · leakingONT - LEFT NR 1 ENGINE LEAKED FUEL ON SHUTDOWN. C/W VISUAL INSPECTION OF MASTER AND SLAVE VG ACTUATORS DRAINS FOR FUEL LEAKAGE. NO LEAKS NOTED. INSPECTED AND FOUND FUEL LEAKING AT OBV DRAIN. REMOVED AND REPLACED OPERABILITY VALVE IAW CRJ 700 AMM TASK 75-31Jan 5, 2009 · N611QX · Cndair CL6002C10 · Compressor Bleed ControlSDR QXEA2009011200008Unknown · leakingBUR - FUEL LEAKING FROM LEFT ENGINE WITH BOOST PUMPS ON. INSPECTED NR 1 ENGINE FOR LEAKS FROM DRAIN MAST WITH BOOST PUMPS RUNNING. NO LEAKS NOTED. GROUND RAN ENGINE WITH MULTIPLE STARTS AND STOPS TOTALING 30+ MINUTES. C/W INSPECTION. NO LEAKS NOTED. C/W Jan 4, 2009 · N611QX · Cndair CL6002C10 · Engine Fuel DistributionSDR COMA2008111970002Fan Blade · defectiveEN ROUTE ATL-MKE THE LEFT ENGINE VIBRATION INDICATION REACHED 1.8 AMBER, REDUCED THRUST TO INDICATE GREEN. CREW DIVERTED TO MKE AND LANDED WITHOUT INCIDENT. REPLACED ALL FAN BLADES ON THE LEFT ENGINE.Nov 19, 2008 · N369CA · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR COMA0870028Engine · vibrationLT ENGINE N2 VIB ON CLIMBOUT FROM CVG. ACFT RETURNED TO CVG. LANDED SAFELY. R&R LT ENGINE.Oct 26, 2008 · N371CA · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR CA080930001Door · missing(CAN) DURING THE WALKAROUND THE CREW NOTICED THE LT MLG DOOR WAS MISSING. THE DOOR SEPARATED FROM ACFT DURING THE FLIGHT. THE PRELIMINARY ASSESSMENT FROM PICTURES SHOWS THE HINGE FITTINGS CRACKED AND THE ROD END SNAPPED ON THE DOOR ATTACHMENT POINT. LAST SSep 28, 2008 · Cndair CL6002C10 · Landing Gear DoorsSDR COMA0870026Engine · vibrationFLIGHT NR 6421 DURING CLIMBOUT FROM CVG NR 1 ENGINE N1 VIB INCREASED TO 1.8 YELLOW, IN CRUISE VIB WENT TO 2.4 YELLOW. SHUT DOWN ENGINE, RESTARTED ENGINE AND VIB WENT AWAY. EMERGENCY DECLARED. A/C CONTINUED TO MSP AND LANDED SAFELY. INSPECTED NR 1 ENGINE FASep 27, 2008 · N374CA · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR TRAX200801123Fadec · malfunctionedDURING DESCENT FROM 22500 TO 12000 @ 300KIAS GOT R FADEC MSG RAN QRH & MONITORED ENGINE INDICATIONS. R ITT WENT TO 932 C. SHUTDOWN R ENGINE. RAN SINGLE ENGINE PROCEDURES CHECK AND LANDED WITH ALL CHECK LIST NO HOT ICON GAUGE TURNED RED. EMERGENCY DECLARED.Sep 7, 2008 · N761ND · Cndair CL6002C10 · Fuel Control/Turbine EnginesSDR VNAA0808015Antenna · unserviceableDURING SCHEDULED MX DAMAGE CAUSED BY POSSIBLE LIGHTNING STRIKE WAS NOTED. DME ANT WAS R&R ALONG WITH DAMAGE TO FUSELAGE REPAIRED. NO OTHER DAMAGE WAS NOTED AND THE ACFT WAS RELEASED FOR SERVICE.Aug 26, 2008 · N703PS · Cndair CL6002C10 · DME/TACAN SystemSDR VNAA0808006Warning System · false activationCREW REPORTED A RED WARNING "L BLEED DUCT" CAS MESSAGE IN FLIGHT. CREW ELECTED TO DIVERT TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ACFT AND FOUND NO DEFECTS. ACFT WAS RELEASED FOR SERVICE. (S)Aug 8, 2008 · N712PS · Cndair CL6002C10 · Central WarningSDR VNAA0808003Door · openCREW ELECTED TO RETURN TO CLT FOR GROUND POWER DOOR LEFT OPEN. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ACFT WITH NO DEFECTS NOTED. ACFT WAS RELEASED FOR SERVICE. (S)Aug 4, 2008 · N718PS · Cndair CL6002C10 · DoorsSDR VNAA0808002Door · openCREW ELECTED TO RETURN TO MSY FOR GROUND POWER DOOR LEFT OPEN. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ACFT WITH NO DEFECTS NOTED. ACFT WAS RELEASED FOR SERVICE. (S)Aug 1, 2008 · N705PS · Cndair CL6002C10 · DoorsSDR VNAA0808001Door · openCREW ELECTED TO RETURN TO CLT FOR COM DOOR LEFT OPEN. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ACFT WITH NO DEFECTS NOTED. ACFT WAS RELEASED FOR SERVICE. (S)Aug 1, 2008 · N706PS · Cndair CL6002C10 · DoorsSDR VNAA0807013Door · openCREW REPORTED HIGH PITCHED NOISE IN FLIGHT AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE MAINTENANCE SERVICE DOOR OPEN. MAINTENANCE INSPECTED AND SECURED THE DOOR WITH NO DEFECTS. AIRCRAFT WAS REJul 22, 2008 · N723PS · Cndair CL6002C10 · Service DoorsSDR VNAA0807003None · noneCREW REPORTED A GROUND POWER DOOR LEFT OPEN. CREW RETURNED TO HSV AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. MAINTENANCE SECURED THE DOOR CLOSED. AIRCRAFT WAS RELEASED FOR SERVICE. (A)Jul 11, 2008 · N705PS · Cndair CL6002C10 · Standard Practices/StructuresSDR SWIA200819856Controller · failedLT BLEED DUCT MESSAGE ON CLIMB OUT WITH A LOSS OF PRESSURIZATION. (FLIGHT NR 6116) REPLACED ANTI ICE LEAK CONTROLLER AND PERFORMED FLIGHT TEST. ALL CHECKS OK. P/N GG670-80012-3, S/N OFF: 00452. Jul 9, 2008 · N728SK · Cndair CL6002C10 · Airfoil Anti/De-ice SystemSDR VNA2008F00003Door · openCREW REPORTED AN EXTERNAL SERVICE DOOR LEFT OPEN AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINT INSPECTED AND FOUND THE EXTERNAL POWER DOOR OPEN. NO DEFECTS OR DAMAGE FOUND. MAINTENANCE SECURED THE DOOR CLOSED. AIRCRAFT WAJun 30, 2008 · N712PS · Cndair CL6002C10 · Service DoorsSDR VNA2008F00001Door · openCREW REPORTED THE GROUND POWER DOOR LEFT OPEN AFTER TAKEOFF. CREW ELECTED TO RETURN TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINT INSPECTED AND FOUND DEFECTS. OPS CHECK GOOD AT THIS TIME. MAINT SECURED THE DOOR CLOSED. AC WAS RELEASED FOR SERVICE. (K)Jun 24, 2008 · N712PS · Cndair CL6002C10 · DoorsSDR VNAA0806005Door · openCREW REPORTED AN EXTERNAL GROUND POWER DOOR LEFT OPEN AFTER TAKEOFF. THE CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NO DAMAGE OR DEFECTS. MAINTENANCE SECURED THE DOOR CLOSED. ACFT WAS RELEASED FOR SERVICE. (Jun 7, 2008 · N708PS · Cndair CL6002C10 · Service DoorsSDR VNAA0805022Proximity Sensor · malfunctionedCREW REPORTED AN INTERMITTANT SERVICE DOOR EICAS MESSAGE AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REMOVED THE INNER HANDLE. MAINTENANCE PERFORMED A DETAILED INSPECTION OF THE HANDLE ASSEMBLY. NO DEMay 18, 2008 · N706PS · Cndair CL6002B19 · Door Warning SystemSDR VNAA0805019Latch · brokenCREW REPORTED AFTER TAKEOFF HEARD A WHINING NOISE COMING FROM THE NOSE OF THE AIRCRAFT. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE COMM PANEL LATCH WAS BROKEN. MAINTENANCE REMOVED AND REPLACED THE LATCH INMay 14, 2008 · N706PS · Cndair CL6002B19 · Accessory Compartment DoorsSDR VNAA0805015Door · openCREW REPORTED A SERVICE PANEL DOOR LEFT OPEN. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE SERVICE PANEL DOOR OPEN. MAINTENANCE SECURED THE DOOR CLOSED. NO DEFECTS OR DAMAGE AT THIS TIME. AIRCRAFT WAS RELEMay 12, 2008 · N702PS · Cndair CL6002B19 · Fluid Service Doors
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