GE CF34-3B1

Service difficulty reports · 5,402

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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 engine_model_key = 'CF343B1'
  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 CA120906002Panel · damaged(CAN) SEVERAL INSERTS INSTALLED IN PSU PANELS WERE FOUND TO BE DETACHING FROM INSTALLED LOCATIONS DURING SCHEDULED MAINTENANCE. PSU PANELS WERE MFG UNDER STC: C-LSA10-014/D RDA APPROVAL BEING INITIATED WITH ENGINEERING COMPANY.Sep 6, 2012 · Cndair CL6002B19 · Passenger Compartment EquipmentSDR CA120907003Panel · failed(CAN) SEVERAL INSERTS INSTALLED IN PSU PANELS WERE FOUND TO BE DETACHING FROM INSTALLED LOCATIONS DURING MAINTENANCE. PSU PANELS WERE UNDER STC: SA08-66, ISSUE 3. RDA APPROVAL IS BEING INITIATED WITH ENGINEERING COMPANY.Sep 6, 2012 · Cndair CL6002B19 · Passenger Compartment EquipmentSDR ASOA2012090702169Bulb · burned outRT CENTER OVERWING EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT BULB IAW AMM 33-51-21, OPS CHECKED GOOD.Sep 5, 2012 · N882AS · Cndair CL6002B19 · Emergency LightingSDR VNAA2012090500004Carbon Seal · leakingCREW REPORTED SMOKE / TOILET CAS MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED NUMBER 1 AND NUMBER 3 CARBON SEALS FOR RIGHT ENGINE (DUE TO LEAKING) AND PERFORMED CHECKS USING AIRCRAFT AND ENSep 5, 2012 · N218PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA120906008Shutoff Valve · failed(CAN) RT 14TH DUCT WARNING MESSAGE. INFLIGHT RETURN, WITH RT ENGINE AT IDLE IAW QRH, MESSAGE DISAPPEARED. GROUND RUNS C/O. RAN N1 AT 90 PERCENT FOR APPROXIMATELY 5 MINS THEN SWITCHED ON THE WING ANTI-ICE AND COWL ANTI-ICE. 14TH STAGE DUCT OVERHEAT MESSAGE CASep 3, 2012 · Cndair CL6002B19 · Pneumatic Distribution SystemSDR A6WA201240822Unknown · odorEXCESSIVE FUEL VAPORS IN CABIN WHILE REFUELING. CREW REPORTED FUEL VAPOR ODOR EITHER APU BLEED OR GROUND AIR ONLY-WITH APU AND ENGINES NOT RUNNING. INSPECTED FOR LEAKS-NO LEAKS NOTED AT THIS TIME.Aug 31, 2012 · N441ZW · Cndair CL6002B19 · Air Distribution SystemSDR ASOA2012083102160Battery · dischargedEMERGENCY LIGHT ON F/A PANEL ON POSITION EMERGENCY LIGHT ARE NOT OPERATING. CHARGED BATTERY SUPPLY IAW AMM 33-51-00 AND OPS CHECKED GOOD.Aug 30, 2012 · N828AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2012091202195Seat Track · corrodedSEAT TRACK FROM FS 409.128 TO 559.16 CORRODED. REMOVED CORROSION IAW SRM 51-21-06, MAX MATERIAL REMOVED AT LOCATION R3, FIG 101, .012 DEEP. MATERIAL REMOVED WITHIN LIMITS OF SRM 53-21-49. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-000-802.Aug 30, 2012 · N903EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR CA120829001Pdu · seized(CAN) ON APPROACH THE CREW SELECTED FLAP 45 & RECEIVED FLAP FAIL LIGHT AT FLAP 30. MAINTENANCE FOUND POWER DRIVE UNIT, PDU, SEIZED REPLACED SAME IAW AMM 27-52-01. RIGGING OF FLAPS CARRIED OUT AND OPS CHECK PERFORMED. NO FAULT FOUND.Aug 29, 2012 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA2012083102157Flashlight · inoperativeF/A FLASHLIGHT INOPERATIVE. REPAIRED F/A FLASHLIGHT IAW AMM 25-61-02. OPS CHECKED GOOD, OK FOR SERVICE.Aug 28, 2012 · N872AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA2012083102158Flashlight · inoperativeCAPTAIN'S FLASHLIGHT INOPERATIVE. REPAIRED IAW AMM 25-61-02. OPS CHECKED GOOD. AC OK FOR SERVICE.Aug 28, 2012 · N975EV · Cndair CL6002B19 · Emergency EquipmentSDR TCJA201209100001Apu · failedAPPROXIMATELY FIVE MINUTES INTO GROUND RUN IN PREPARATION FOR A FLIGHT, APU EXHIBITED A LOUD SCREECHING OR GRINDING NOISE FOLLOWED BY TWO LOUD "POPS". HEAVY OIL SMOKE IMMEDIATELY BEGAN EXITING CABIN AND COCKPIT AIR CONDITIONING DUCTING. APU SHUTDOWN WAS INITAug 28, 2012 · N529DM · Cndair CL6002B16 · APU Core EngineSDR A6WA201240826Sill · corrodedPAX DOOR SILL HAS CORROSION. FOUND CORROSION TO BE 100 PERCENT MATERIAL LOSS. REMOVED, FABRICATED, AND INSTALLED NEW SERVICEABLE SILL IAW SRM 51-42-06, 51-42-13, 51-42-21 AND 51-24-16.Aug 28, 2012 · N407AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA120828001Angle · cracked(CAN) WHILE PERFORMING AN INTERNAL ZONAL INSPECTION OF THE CENTER WING SECTION IAW TASKS RJ2-57-510-502 AND RJ2-57-900-320, THERE WERE CRACKS FOUND IN THE CENTER WING TANKS FWD OF THE COLLECTOR TANKS. CRACKS WERE FOUND AT INSIDE FUEL PANEL LOCATION 510AB LT SAug 27, 2012 · Cndair CL6002B19 · Wing Miscellaneous StructureSDR ASOA2012083002139Lens · missingRT SIDE EXTERIOR EMERGENCY LIGHT LENS POPPED OUT. RESECURED RT 3 EMERGENCY LIGHT LENS ASSY. IAW AMM 33-51-21, OPS CHECKED GOOD, ACFT OK FOR SERVICE.Aug 26, 2012 · N971EV · Cndair CL6002B19 · Emergency LightingSDR A6WA201240828Roller · chafedLEFT OTBD FLAP ROLLER FITTING CHAFED. PERFORMED REPAIR OF LT OTBD FLAP INBD ROLLER FITTING IAW REO 601R-57-53-943.Aug 25, 2012 · N407AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201240815Door · chafedRIGHT MLG DOOR CHAFED ON LOWER L/E. REPLACED FILLER ON LOWER L/E ON RIGHT MLG DOOR IAW REO 601R-52-82-034.Aug 23, 2012 · N407AW · Cndair CL6002B19 · Landing Gear DoorsSDR ASOA2012091802227Drag Angle · crackedPAX DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED PAX DOOR AFT DRAG ANGLE IAW EC/TC REO 601R-52-11-513.Aug 23, 2012 · N970EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201240827Cargo Track · corrodedTHREE CARGO TRACKS ON LBL AND RBL 9 HAS CORROSION IN CARGO AREA. REMOVED AND INSTALLED SERVICEABLE CARGO TRACKS IAW AMM 53-01-11.Aug 23, 2012 · N407AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201240806Escape Hatch · unsecureCREW HATCH POPPED OPEN FROM REAR OF HATCH ABOUT 1 INCH. ABORTED TO AT 100 KNOTS. MAX BTMS 5,6,7,6. HES STOP INSP NOT REQUIRED IAW MXCTL.Aug 22, 2012 · N419AW · Cndair CL6002B19 · Emergency ExitsSDR A6WA201240812Seat Track · gougedRT SIDE SEAT TRACK NR 3 GOUGED BEYOND LIMITS. R & R SEAT TRACK SECTION.Aug 22, 2012 · N407AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201240813Post · gougedAFT PRESSURE BULKHEAD CENTER POST IS GOUGED AT TOP. REPAIRED AFT PRESSURE BULKHEAD CENTER POST FS 621 TO DEPTH. .055 AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW REO 601R-53-61-4636.Aug 22, 2012 · N407AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2012082702107Bulkhead · crackedBS 202 BULKHEAD CRACKED AT PARKING BRAKE CABLE. CRACK HAS BEEN VERFIED BY NDT FABRICATED FILLERS AND DOUBLER. FABRICATED REINFORCEMENT DOUBLER. PREPARED AND INSTALLED PARTS AND FASTENERS, RESTORED FINISH AND APPLIED CIC. REF. 601R-53-11-563 REV. B. REPAIR TAug 21, 2012 · N980EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201240817Structure · corrodedTOP OF PAX DOOR STAIR STRUCTURE HAS CORROSION. REMOVED OLD PAX DOOR EDGE MEMBER DUE THE CRACKS FOUND WHILE CLEANING CORROSION FABRICATED NEW EDGE MEMBER IAW SRMS 51-24-19, 51-42-06, 51-42-13.Aug 21, 2012 · N407AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR 2012FA0000580Skin · crackedA 1 INCH PRESSURE SKIN CRACK WAS FOUND BETWEEN THE LOWER BEACON AND THE NR 2 VHF ANTENNA. LOCATED AT FS 409+32, STR 26L TO STR 26R. REPAIRED WITH REO 601R-53-31-759.Aug 20, 2012 · N591ML · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2012082002081Connector · disconnectedWARDROBE AND GALLEY EMERGENCY LIGHTS ARE INOPERATIVE. TROUBLESHOT EMERGENCY LIGHTS IAW WDM 33-51-00. FOUND FOUR QUICK DISCONNECT CONNECTORS DISCONNECTED. SWAPED AT LT FWD FLOOR LEVEL EXIST FLOODLIGHT (DS9LY) AND FWD EXIT SIGN (DS10LY). CONNECTED IS9LY AND DSAug 20, 2012 · N880AS · Cndair CL6002B19 · Light System WiringSDR REXA2012082001280Relay · failedRIGHT THRUST REVERSER WILL NOT DEPLOY PAST IDLE, FEELS LIKE LEVER GETS STUCK. REMOVED AND REPLACED RELAY 2K5KE IN JB 3 IAW ESPM 20-22-00. OPS CHECKED GOOD OF RIGHT THRUST REVERSER IAW AMM 78-30-00.Aug 20, 2012 · N824AY · Cndair CL6002B19 · Engine Thrust ReverserSDR ASOA2012082402095Fan · failedDISPLAY COOL CAUTION MESSAGE IN FLIGHT. FOLLOWED QRH. WHEN SWITCHING FROM NORMAL TO FLIGHT ALTERNATE SMELLED ELECTRICAL BURNING ODOR FOR 10 SECONDS. RECEIVED ODOR TWICE MORE FOR SHORT DURATION OF TIME (DISPLAY COOLING FANS) R & R DISPLAY FAN IAW AMM 21-24-1Aug 20, 2012 · N832AS · Cndair CL6002B19 · Air Distribution FanSDR ASOA2012082302090Detector · failedFLAPS FAIL MESSAGE AT 18000FT. NEVER WENT AWAY. LANDED FLAPS ZERO. EMERGENCY DECLARED AS A PRECAUTION, TOWER HAD EQUIPMENT STANDING BY. R & R SKEW DETECTION UNIT IAW AMM 27-51-15. CLEARED. SDR CLOSED.Aug 19, 2012 · N900EV · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR REXA2012081901279Oil System · low pressureON FLIGHT 3952, THE CREW PERFORMED A RIGHT ENGINE SHUTDOWN DUE TO LOW ENGINE OIL PRESSURE (5PSI) AFTER TAKEOFF FROM FNT. CREW DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED RIGHT ENGINE IAW AMM 71-00-00 AND CHECKLIST PROVIDED. ALAug 19, 2012 · N8560F · Cndair CL6002B19 · Engine Oil PressureSDR A6WA201240802Engine · malfunctionedAT 1000 FT, FELT AND HEARD BANG AND SHUTTER RT EGT SHOT INTO RED HIGH 900'S REDUCED THRUST ON RT ENG EGT RETURNED TO GREEN VIB ICON ON N2 EVEN AT IDLE, PERFORMED PRECAUTIONARY SHUTDOWN IAW GRH. ALL PARAMETERS NORMAL ENGINE WAS NOT WINDMILLING. REMOVED AND REPAug 18, 2012 · N434AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR REXA2012081801274Gearbox · malfunctionedRIGHT THRUST LEVER BINDS AT HIGH THRUST SETTING, WOULDN'T ALLOW CLIMB THRUST TO BE SET AT HIGHEST N1 SETTING. CARAT INDICATED 95.0 SHOULD BE SET AND COULD ONLY SET 94.2. REMOVED AND REPLACED RIGHT THROTTLE GEARBOX IAW AMM 76-11-17. CHECKED RIGGING ON POWER Aug 18, 2012 · N8696C · Cndair CL6002B19 · Power LeverSDR ASOA2012082202088Bulb · burned outRT AFT EXTERNAL EMERGENCY LIGHT IS INOP. R & R RT AFT EXTERNAL EMERGENCY LIGHT BULB. OP'S CHECKED GOOD. R & R RT AFT EXTERNAL EMERGENCY LIGHT BULB. AMM 33-51-21. OP'S CHECKED GOOD.Aug 18, 2012 · N877AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2012082202089Battery · dischargedF/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT BATTERIES, IAW AMM 25-61-00. OPS CHECKED GOOD.Aug 18, 2012 · N981EV · Cndair CL6002B19 · Emergency EquipmentSDR A6WA201240807Sill · corrodedPAX DOOR CUT OUT LOWER SILL CORRODED AROUND SWITCH AND ANGLE. REMOVED CORRODED ON AREA IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED UNSERVICEABLE LOWER SILL AND REPLACED WITH SERVICEABLE LOWER SILL.Aug 18, 2012 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012082102083Lamp · burned outEMERGENCY LIGHT INOPERATIVE. RELAMPED OVER WING EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.Aug 17, 2012 · N916EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2012082102084Isolator · brokenONE ISOLATOR BROKEN IN CARGO COMPATMENT AFT BULKHEAD LT SIDE BOTTOM. R & R 1 BROKEN ISOLATOR IN CARGO COMPATMENT AFT BULKHEAD LEFT SIDE BOTTOM IAW SRM 51-42-13.Aug 17, 2012 · N921EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2012081601266Gearbox · restrictedRIGHT THRUST LEVER QUADRANT HAS LOT OF FRICTION IN HIGHER TRUST SETTINGS. HARD TO SET TRUST AT HIGHER LEVELS. REMOVED AND REPLACED RIGHT ENGINE THROTTLE CONTROL GEARBOX PER AMM 76-11-17. RIQ CHECKS, FRICTION TEST, AND FUNCTIONAL CHECKS ARE GOOD PER AMM 76-11Aug 16, 2012 · N8696C · Cndair CL6002B19 · Power LeverSDR ASOA2012081702079Latch · lack of lubeUNABLE TO OPEN GALLEY SERVICE DOOR FROM OUTSIDE - OPENS FINE FROM THE INSIDE. CLEANED SILL AND LUBED LATCHES AND HANDLE. CHECKED OPS IAW AMM 52-41-00. OPS CK OK. SDR CLOSED.Aug 16, 2012 · N836AS · Cndair CL6002B19 · Service DoorsSDR CA120820004Actuator · failed(CAN) IN FLIGHT THE ACFT YAWS BY ITSELF WITH THE AP ENGAGED OR DISENGAGED. THE RUDDER INDICATOR ON EICAS IS ALSO MOVING BACK AND FORTH SLIGHTLY. EXTENSIVE T/S WITH WIRING AND SYS CHECKS WAS CARRIED OUT, FINALLY BOTH YAW DAMPER ACTUATORS WERE REPLACED AND THEAug 16, 2012 · Cndair CL6002B19 · Rudder Control SystemSDR A6WA201240774Warning Message · illuminatedON TAKE OFF ROLL, RECEIVED IDG 1 CAUTION MESSAGE. SERVICED NR 1 IDG WITH 11 PUMPS IAW AMM 12-23-01. RAN NR 1 ENGINE. OPS CHECKED GOOD.Aug 15, 2012 · N420AW · Cndair CL6002B19 · AC Generator-AlternatorSDR A6WA201240777Structure · damagedELONGATED HOLE ON LT FWD AVIONICS FLIGHT CONTROL ACCESS AT 12 O`CLOCK. FASTENER HOLE FWD MFG AND INSTALL FREEZE PLUG IAW REO 601R-53-11-162, REV B.Aug 15, 2012 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240778Hinge · corrodedPAX DOOR UPPER STEP HINGE CORRODED. REMOVED DAMAGED HINGE AND REPLACED WITH NEW SERVICEABLE HINGE IAW SRM 51-41-02.Aug 15, 2012 · N450AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR VNAA2012081700011Carbon Seal · damagedCREW REPORTED LOW OIL PRESSURE ON THE LEFT ENGINE. AIRCRAFT DIVERTED AND LANDED SAFELY. MAINTENANCE TROUBLESHOT AND REPLACED THE LEFT ENGINE AGB CARBON SEALS MATING RINGS. OPERATIONAL CHECKS WERE PERFORMED USING THE AIRCRAFT MAINTENANCE MANUALS. THE AIRCRAug 14, 2012 · N207PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA201240772Bpsu · failedFLAPS FAILED IN FLT AT 20 DEGREES WHEN 30 DEGREES WAS SELECTED. PERFORMED FLAP RESET PROCEDURE IAW SUPPLEMENT 98-18E BOX 12, FLAPS RESET. FOUND REPEAT BPSU FAULT CODES IN FECU, REPLACED LT BPSU IAW AMM 27-51. OPS CK GOOD.Aug 14, 2012 · N406AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA201240801Skin · chafedLT AILERON UPPER L/E CHAFED. BLENDED CHAFED AREAS IAW SRM 51-12-00. MEASURED, FOUND TO BE WITHIN LIMITS IAW REO 601R-57-61-437.Aug 14, 2012 · N450AW · Cndair CL6002B19 · AileronsSDR A6WA201240781Mount Bracket · crackedPAX DOOR PWR ASSIST MOTOR MOUNTING BRACKET CRACKED. REMOVED CRACKED MOUNTING BRACKET AND REPLACED WITH NEW SERVICEABLE BRACKET, PN 601R3177457 IAW SRM 51-42-06.Aug 14, 2012 · N450AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012091202194Beam · corrodedFS 349.00 TRANSVERSE BEAM HAS CORROSION AT RBL 40. FROM AFDL 400640: FS 349.00 TRANSVERSE BEAM IS CORRODED BEYOND 10 PERCENT LIMITS AT RBL 40 IAW SRM 53-00-00-01, T/R 53-27, FIG 102, SHEET 2. REPAIRED FS 349.00 TRANSVERSE BEAM AT RBL 49 IAW REO 601R-53-21-Aug 14, 2012 · N903EV · Cndair CL6002B19 · Fuselage Main, StructureSDR CA120817002Actuator · sticking(CAN) ON ROTATION, THE F/O NOTED THAT THE ELEVATOR CONTROL WAS STICKY. IT WAS HARDER THAN NORMAL AND ON IT`S OWN, WOULD NOT RETURN TO THE NEUTRAL POSITION. CREW ELECTED TO RETURN. MAINTENANCE PERSONNEL FOUND THAT THE CAPTAIN AND SERVO ACTUATOR AT FAULT. BOTAug 14, 2012 · Cndair CL6002B19 · Elevator Control SystemSDR TRBA20120811001Bulb · inoperativeFOUND MAIN CABIN DOOR EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. REPOSITIONED MAIN CABIN DOOR EMERGENCY LIGHT BULB. OPS CHECK IAW MM 33-50-00 OK. ACFT RETURN TO SERVICE.Aug 13, 2012 · N431 · Aerosp ATR72 · Emergency Lighting
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