GE CF34-3B1

Service difficulty reports · 5,402

Newest first. General aviation reporting is voluntary.

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 ASOA2012081002049Valve · failed"GEAR DISAGREE "MASTER WARNING COMPLIED WITH QRH CYCLED GEAR TOOK APPROX 60 SEC FOR GEAR TO COME UP RT MAIN WAS SLOW TO COME DOWN HDY 3 PRESSURE WAS 2700PSI. EMERGENCY DECLARED AS A PRECAUTION. R & R PRIORITY VALVE IAW AMM 32-32-15 IPC REF 32-32-10 ITEM 205 Aug 6, 2012 · N820AS · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA2012082902124Angle · crackedAFT EQUIPMENT BAY, LT SIDE 621 -625 OBLIQUE ANGLE CRACKED. REMOVED LT SIDE OBLIQUE ANGLE REPLACED WITH SERVICEABLE OBLIQUE ANGLE IAW SRM 51-42-21. PAINT TOUCH UP ANGLE IN AFT EQUIP BAY LT SIDE IAW SRM 51-25-01. SDR CLOSED.Aug 6, 2012 · N846AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012091202192Floor Support · crackedRT FLOOR SUPPORT ANGLE CRACKED AT FS 484 RBL 27. R & R RT FLOOR SUPPORT ANGLE AT FS 484, RBL 27 IAW SRM 51-42-21.Aug 6, 2012 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012091202193Post · crackedFS 409+128 VERTICAL POST AT RBL 18 FAILS NDT WITH AN INDICATION ON INBD AFT RADIUS ON UPPER POST GREATER THAN 50 PERCENT SCREEN HEIGHT. REMOVED POST IAW SRM 51-42-06 7 51-42-22. INSTALLED NEW POST ASSY IAW SRM 51-42-06, 51-42-22 & REO 601R-53-41-889.Aug 6, 2012 · N903EV · Cndair CL6002B19 · Fuselage Main, StructureSDR CA120809004Switch · failed(CAN) IN THE CLIMB THE RT THRUST REVERSER UNLOCKED MESSAGE CAME UP INTERMITTENTLY. THE ACFT RETURNED TO THE DEPARTURE AIRPORT AND LANDED UNEVENTFULLY. MAINTENANCE T/S FOUND THE RT T/R THROTTLE LOCKOUT SWITCH AT FAULT. THE SWITCH WAS REPLACED AND FUNCTION CHAug 5, 2012 · Cndair CL6002B19 · Engine Thrust ReverserSDR REXA2012080401224Engine · odorDURING CLIMB-OUT, FLIGHT 4416, FLIGHT ATTENDANT NOTICED POSSIBLE SMOKE IN CABIN. SMOKE ODOR IN COCKPIT. NO FIRE INDICATIONS. AIR RETURNED TO DEPARTURE. FLIGHT ATTENDANT STATED THAT IS SEEMED TO COME FROM THE FLOOR VENTS. REMOVED AND REPLACED RIGHT ENGIAug 4, 2012 · N8390A · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA2012080802039Strut · underservicedAFTER TAKEOFF, WOW AND STEERING INOPERATIVE MESSAGE. WHEN GEAR SELECTED UP, MASTER WARNING, NOSE GEAR DISAGREE. EMERGENCY DECLARED, RETURNED TO DEPARTURE. R & R AIR STARTER VALVE IAW CMM 32-20-04. PERFORMED FULL SERVICE TO NLG STRUT IAW AMM 12-12-32. Aug 4, 2012 · N920EV · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR A6WA201240761Tube · dentedRT FLAP CENTER & INBD VANE ACTUATOR TUBES HAVE INDENTATIONS FROM THE ROLLERS. REPAIRED IAW REO 601R-57-52-1544, REV A.Aug 4, 2012 · N447AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201240760Engine · malfunctionedAPPLICATION OF TAKE OFF POWER, FELT VIBRATION IN AIRFRAME FOLLOWED BY LT ENGINE LOW OIL PRESSURE CAS MESSAGE. ABORTED TAKE OFF AT LESS THAN 20 KTS. PULLED ACFT OFF RUNWAY, NOTICED ITT WAS FULL SCALE AND N1 AND N2 VIB MESSAGES APPEARED. LEFT ENGINE REPLACEMEAug 3, 2012 · N423AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA2012091202191Light · brokenTHE RT SIDE AISLE EMERGENCY LIGHT BROKEN AND PIECED TOGETHER. ON REPAIR OF RT EMERGENCY LIGHT, FOUND LT SIDE TO ALSO BE DAMAGED. REPAIRED LT AND RT EMERGENCY LIGHTS IAW AMM SUPPLEMENT AND AMM 33-51-01-400-805.Aug 3, 2012 · N903EV · Cndair CL6002B19 · Emergency LightingSDR A6WA201240759Warning Message · illuminatedLEFT WINDOW HEAT CAUTION MESSAGE, COMPLIED WITH FIM RESET MESSAGE CLEARED. ABORTED TAKE OFF.Aug 2, 2012 · N458AW · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR ASOA2012080302035Handle · lack of lubePAX OUTER HANDLE HARD TO PUSH OPEN. PAX OUTER HANDLE LUBRICATED IAW AMM 52-11-03. OPS CHECKED GOOD.Aug 1, 2012 · N824AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012081602074Attach Fitting · corrodedPAX DOOR UPPER HINGE SECTION AT FS 320.10 & FS 338.00 BOTH FWD 7 AFT CLEAT CORRODED BEYOND LIMITS. REMOVED CORRODED CLEAT. FITTED, DRILLED & INSTALLED NEW CLEAT IAW SRM 51-42-06 & 51-42-13.Aug 1, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA201240740Skin · dentedLT LOWER CORE COWL INNER SKIN DENTED IN MULTIPLE SPOTS. 10 DENTS LOCATIONS ON LT LOWER CORE COWL. INNER SKIN WITH FOUR REQUIRED AND 6 FOUND TO BE WITHIN ALLOWABLE DAMAGE REO.Aug 1, 2012 · N447AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201240804Skin · gougedLT LOWER CORE COWL INNER SKIN GOUGED 3 SPOTS, 10 GOUGED LOCATIONS ON LT LOWER CORE COWL INNER SKIN 4 FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS AND TO 6 AREAS. REPAIRED IAW REO 601R-71-12-4122.Aug 1, 2012 · N447AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR ASOA2012080302031Battery Pack · failedNR 7 AND NR 8 EMERGENCY LIGHTS AND THE SECOND FROM FWD AND MOST AFT CENTER CEILING EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPS CHECKED GOOD.Jul 31, 2012 · N884AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2012080302032Lamp · burned outNR 5 EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.Jul 31, 2012 · N925EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2012080302033Bpsu · failedAFTER TAKEOFF, FLAPS FAILED AT 8 DEGREES. COMPLIED WITH QRH. EMERGENCY DECLARED, ACFT RETURNED TO DEPARTURE. R & R RT BPSU IAW AMM 27-51-10. R & R FECU IAW AMM 27-51-05. OPS CHECKED GOODJul 31, 2012 · N976EV · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA2012081602072Attach Angle · crackedCLIP, ON FWD OF ENGINE SUPPORT BEAM AT FS 635.30 BL, RBL 18.00 HAS A .5" CRACK IN LOWER CORNER. FAILED VISUAL NDT INSPECTION. REMOVED CRACKED CLIP AT FS 635.30 BL, RBL 18.00 IAW SRM 51-42-21. REPLACED CRACKED WITH NEW CLIP IAW SRM 51-42-21.Jul 31, 2012 · N880AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2012081602073Attach Angle · crackedATTACH ANGLE ON FWD OF ENGINE SUPPORT BEAM AT FS 635.30 BL, RBL 27.50 HAS A .3" CRACK IN LOWER CORNER. FAILED VISUAL NDT INSPECTION. REMOVED CRACKED ATTACH ANGEL FWD OF ENGINE SUPPORT BEAM IAW SRM 51-42-06 AND 51-42-21. REPLACED CRACKED ATTACH ANGLE IAW SRM Jul 31, 2012 · N880AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201240742Skin · gougedGOUGED ON FUSELAGE AT FS 559 FROM CONTACT WITH RT STUB FAIRING COMPLIED WITH REO 601R-53-41-610.Jul 31, 2012 · N447AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2012080302028Inverter · inoperativeLEFT EMERGENCY EXIT FLOOR LEVEL EXIT SIGN INOPERATIVE. R & R NR 2 INVERTER IAW AMM 33-51-07. OP CHECKED GOOD.Jul 30, 2012 · N836AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2012080302029Control Unit · failedFLAPS FAILED AT 0 ON APPROACH, SKEW DETECTION SYS DEACTIVATED. EMERGENCY DECLARED. REMOVED AND REPLACED RT BPSU AND FECU. OPS CHECKED GOOD.Jul 30, 2012 · N976EV · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA201240746Fitting · crackedFITTING CRACKED OUT APPROX FS 461, RBL 9. REMOVED CRACKED FITTING AT FS 461, RBL 9. INSTALLED NEW SERVICEABLE FITTING PN 600-31068-19.Jul 30, 2012 · N447AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201240747Skin · gougedPANEL 445AB HAS NUMEROUS SMALL DENTS AND GOUGES ON INNER SKIN. REPAIR IAW REO 601R-71-12-4124.Jul 30, 2012 · N447AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201240748Beam · damagedLT INBD FLAP VANE ACTUATORS SLIDING BEAMS HAVE DAMAGE ON UPPER AND LOWER SURFACES FROM ROLLERS. REPAIRED BY BLENDING IAW REO 601R-57-52-1942.Jul 30, 2012 · N447AW · Cndair CL6002B19 · Wing Main, Frame StructureSDR ASOA2012080202026Bulb · burned outLEFT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED BULB AND INSTALLED A NEW BULB IAW AMM 33-51-20. OPS CHECKED GOOD.Jul 29, 2012 · N975EV · Cndair CL6002B19 · Emergency LightingSDR A6WA201240733Stall Warning · intermittentSTALL FAIL ON ROTATION- COMPLIED WITH QRH, RETURNED TO DEPARTURE, COMPLIED WITH FIM RESET PROCEDURES. NO DEFECTS NOTED AT THIS TIME. NOTED.Jul 29, 2012 · N464AW · Cndair CL6002B19 · Stall Warning SystemSDR A6WA201240734Control Cable · failedON DESCENT, LT THRUST LEVER STUCK AT AROUND 82 PERCENT, N1. COMPLIED WITH QRH, SHUTDOWN NR 1 ENGINE IN FLIGHT, ALL ENGINE PARAMETERS NORMAL. R & R LT ENGINE THROTTLE CONTROL CABLE IAW AMM 76, OPS CHECKED GOOD.Jul 29, 2012 · N449AW · Cndair CL6002B19 · Power LeverSDR A6WA201240745Floor Support · corrodedCORROSION ON FLOOR SUPPORT STRUCTURE FS 621 & LBL 31 AT NUTPLATE HOLE BLENDED CORROSION ON FLOOR STRUCTURE. FOUND TO BE WITHIN LIMITS IAW REO 601R-53-61-4600.Jul 29, 2012 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240744Floor Support · corrodedCORROSION AT FLOOR SUPPORT STRUCTURE FS 621 & LBL14 NUTPLATE HOLE. REMOVED CORROSION, MEASURED & FOUND IT TO BE WITHIN ALLOWABLE LIMITS, DEPTH .012" WITH .05" LENGTH 0.7" IAW REO 601R-53-61-4600.Jul 29, 2012 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240735Monitor · malfunctionedREJECTED TAKE OFF AT 58 KTS FOR EFIS COMP MON HEADING, BTMS READS 4, 4, 3, 3. PERFORMED OPS TEST OF AHRS IAW AMM 34-21-01. OPS CHECKED GOOD.Jul 29, 2012 · N455AW · Cndair CL6002B19 · Attitude Gyro and Indicating SystemSDR A6WA201240736Fan · contaminatedDISPLAY COOL CAUTION MESSAGE IN FLIGHT, WOULD NOT CLEAR WHEN STANDBY FAN SELECTED. MESSAGE CLEARED IN STBY WHEN DESCENDING THROUGH 8000`. FOUND DEBRIS INSIDE NR 2 DISPLAY FAN, CLEANED DEBRIS. INSTALLED FAN. OPS CHECKED GOOD AT THIS TIME. NO MESSAGE NOTEDJul 29, 2012 · N422AW · Cndair CL6002B19 · Air Distribution FanSDR ASOA2012080102009Sign · missingLIGHTED EXIT SIGN NEAR SERVICE DOOR MISSING. INSTALLED LIGHTED EXIT SIGN NEAR SERVICE DOOR IAW AMM 33-51-10.Jul 28, 2012 · N846AS · Cndair CL6002B19 · Emergency LightingSDR A6WA201240732Proximity Sensor · out of adjustPAX DOOR WARNING IN FLIGHT AT 7 PSID. C/W QRH, WITNESS MARKS APPEARED NORMAL. ADJUSTED PAX DOOR CAN 1 PROXIMITY SENSOR IAW AMM 52-70-04. OPS CHECKED GOOD.Jul 28, 2012 · N448AW · Cndair CL6002B19 · Door Warning SystemSDR A6WA201240731Shaft · crackedSERVICE DOOR OUTER HANDLE WILL NOT STOW FROM OUTSIDE OR INSIDE. INSPECTED SERVICE DOOR FOUND OUTER HANDLE SHAFT CRACKED. DOOR OPERATES PROPERLY FORM INSIDE REF LP 228429/4 FOR MEL.Jul 28, 2012 · N423AW · Cndair CL6002B19 · Service DoorsSDR A6WA201240737Mount Bracket · crackedSYS 3 BROKEN ACCUMULATOR FWD MOUNTING BRACKET CRACKED. REMOVED UNSERVICEABLE BRACKET AND REPLACED WITH SERVICEABLE BRACKET, PN 601R75250-25, IAW AWC SRM 51-42-06, 51-40-11 AND 51-42-21.Jul 28, 2012 · N447AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR REXA2012072701202Carbon Seal · leakingSMOKE TOILET CAUTION MESSAGE AFTER TAKEOFF. FLIGHT ATTENDANT CALLED AND ADVISED FLIGHT CREW CABIN WAS FILLING UP WITH SMOKE. SMELLED LIKE BURNT RUBBER, ACCORDING TO FLIGHT ATTENDANT. REMOVED AND REPLACED RT ENGINE NR 1 CARBON SEAL IAW MM 72-00-00. ENGINE Jul 27, 2012 · N8718E · Cndair CL6002B19 · Turbine Engine Oil SystemSDR ASOA2012080102022Attach Bracket · crackedCARGO BAY, AFT BRACKET AT FS 621 CRACKED WHERE BRACKET ATTACHES TO CROSSMEMBER CARGO DOOR. R & R CARGO BAY AFT BRACKET IAW SRM 51-42-21-00.Jul 27, 2012 · N880AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201240749Bulkhead · damagedDOUBLE DRILLED HOLE ON FS 559 BULKHEAD AT RBL 18. DURING INCORPORATION OF GREO 601R-53-41-1116, REV B. CW REO 601R-53-41-1594 BY CUTTING OUT DAMAGED REINFORCING ANGLE STEPPING UP HOLES, AND INSTALLING FREEZE PLUGS AND A FILLER.Jul 27, 2012 · N447AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR CA120801009Adc · failed(CAN) IN THE CLIMB THE CAPTAIN WAS NOT ABLE TO ADJUST HIS BAROMETRIC SETTING FOR HIS ALTIMETER. THE ACFT RETURNED TO THE DEPARTURE AIRPORT. MAINTENANCE REPLACED THE LT AIR DATA COMPUTER AND RETURNED THE ACFT TO SERVICE. PN 822-0372-445, SN 1L59R. PART TSR 67Jul 27, 2012 · Cndair CL6002B19 · Air Data ComputerSDR ASOA2012072701991Charger · failedEMERGENCY LIGHTS (FWD) ARE INOPERATIVE. R & R BATTERY CHARGER ASSY NR 1 IAW AMM 33-51-05. R & R FUSES AT BATTERY PACK NR 2 IAW VCMM 33-22-11.Jul 26, 2012 · N914EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2012072701992Light · inoperativeEMERGENCY EXIT LIGHT INOPERATIVE IAW AMM 33-51-21. R & R EMERGENCY EXIT LIGHT ASSY IAW AMM 33-51-21, OPS CHECKED GOOD.Jul 26, 2012 · N914EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2012072701993Bulb · burned outOVERWING INTERIOR EMERGENCY LIGHT OUT. R & R INTERIOR EMERGENCY EXIT LIGHT BULB IAW AMM 33-51-14.Jul 26, 2012 · N931EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2012072701994Battery Pack · failedLT AND RT TOP OVERWING EMERGENCY LIGHTS OUT. R & R NR 2 EMERGENCY BATTERY PACK IAW AMM 33-51-04. OPS CHECKED GOOD.Jul 26, 2012 · N931EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2012073001999Angle · crackedPASSENGER COMPARTMENT FLOOR STRUCTURE AT FS 484.00, LBL 27.00, ATTACHMENT ANGLE IS CRACKED. REMOVED ANGLE IAW SRM 51-42-21. REPLACED CRACKED ANGLE AT FS 494.00, LBL 27.00 IAW SRM 51-42-21 AND SRM 51-42-06 PN 601R31171-17. TJul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012073002000Frame · crackedFS 718 FRAME, CRACKED JUST BELOW STRINGER 11 RT. REMOVED DAMAGE IAW REO 601R-53-61-193. PERFORMED LPI CUT LINE IAW NDTM 51-10-08. NO INDICATIONS NOTED.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2012080102013Seat Track · corrodedIN PASSENGER COMPARTMENT RT SIDEWALL SEAT TRACK AT FS 409+8 CORRODED. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-055. RII FOUND TO BE SATISFACTORY.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012080102015Seat Track · corrodedIN PASSENGER COMPARTMENT RT SIDE SEAT TRACK AFT OF FS 409+128 IS CORRODED AT SEVERAL LOCATIONS. COMPLIED WITH EC/TC REO 601R-53-00-55 AND REO 601R-53-00-055, REV A.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012080102017Seat Track · corrodedIN PASSENGER COMPARTMENT, RBL 9.900 BETWEEN FS 364 TO 399, SEAT TRACK IS CORRODED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 51-21-49. REMOVED SEAT TRACK AND INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802.Jul 26, 2012 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
Back to GE CF34-3B1