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 ASOA201000893Angle · crackedFOUND FS 559 LT CAP ANGLE HAS INDICATION NOTED, APPROX .3" IN LENGTH 60 PERCENT FSH AT LBL 18.0 AND FS 559 RT. BULKHEAD WEB HAS INDICATIONS NOTED APPROX .3" IN LENGTH 50 PERCENT FSH INBD OF RBL 18.0 WL 59.10. BOTH FAILED NDT INSPECTION. COMPLIED WITH EC/TC Jun 11, 2010 · N684BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000894Seat Track · corrodedCARGO COMPARTMENT SEAT RAIL AT RBL 27 FS 559.00+80 TO 559.00+96 IS CORRODED. R & R SEAT RAIL IAW SRM 51-41-02.Jun 11, 2010 · N684BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000895Seat Track · corrodedCARGO COMPARTMENT SEAT RAILS AT LBL 27 BETWEEN FS 559+80 AND 567.00 ARE CORRODED. R & R SEAT RAILS IAW SRM 51-41-02.Jun 11, 2010 · N684BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000896Seat Track · corrodedCARGO COMPARTMENT SEAT RAILS AT LBL 9 BETWEEN FS 559+91 AND FS 617.00 ARE CORRODED. R & R SEAT RAILS AND ANCHOR PLATES IAW SRM 51-41-02.Jun 11, 2010 · N684BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000897Seat Track · corrodedCARGO COMPARTMENT SEAT RAILS AT RBL 9 BETWEEN FS 559.00+80 AND FS 569.00 ARE CORRODED. REPLACED SEAT RAILS IAW SRM 51-41-02. FOUND FITTING BROKEN ON SEAT TRACK 601R38727-13. REPLACED FITTING IAW SRM 51-41-02.Jun 11, 2010 · N684BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000898Floor Support · corrodedCARGO COMPARTMENT FLOOR SUPPORT CAP IS CORRODED BEYOND REPAIR AT LBL 27 FROM FS 569.00 TO FS 621.00. REMOVED CARGO COMPARTMENT FLOOR SUPPORT CAP IAW SRM 51-42-21 & 51-42-06. LOCATED AND DRILLED NEW FITTING & FLOOR SUPPORT CAP IAW SRM 51-40-11. COUNTERSUNK & Jun 11, 2010 · N684BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000900Placard · tornPAX DOOR STEPS ARROW, EXIT AND OPEN PLACARDS ARE TORN. R & R ARROW, EXIT, AND OPEN PLACARDS ON PAX DOOR STEPS IAW AMM 11-20-00-000-801 AND 11-20-00-400-801.Jun 11, 2010 · N860AS · Cndair CL6002B19 · Placards and MarkingsSDR ASOA201000901Floor Support · corrodedFLOOR SUPPORT CAP AT LBL 27 FS 621 TO FS 574 HAS CORROSION. REMOVED FLOOR SUPPORT CAP IAW SRM 51-42-05, 51-42-21 AND 51-42-13. INSTALLED NEW SERVICEABLE FLOOR SUPPORT CAP IAW SRM 51-30-11, 51-42-21 & 51-42-22. ALSO COMPLIED WITH STEPS 1 THRU 7 OF REO 601RJun 11, 2010 · N860AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000902Sill · corrodedRIGHT FUSELAGE FLOOR SUPPORT SILL AT LBL 36 FASTENER HOLES HAVE CORROSION FROM FS 589 TO 559+112. AFTER CLEANING AREA FOUND NO CORROSION. RETREATED AREA IAW SRM 51-21-11. REMOVED FLOOR SILL IAW SRM 51-42-06 AND 51-42-21. FABRICATED REPLACEMENT LIPPED PLATE FJun 11, 2010 · N860AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000903Floor Support · crackedFS 280 FLOOR SUPPORT CLIP AT RBL 18 INBD IS CRACKED. AFTER CLEANING AREA FOUND NO CORROSION. RETREATED AREA IAW SRM 51-21-11.Jun 11, 2010 · N860AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000905Lamp · inoperativeCABIN CEILING CURVED EMERGENCY EXIT SIGN FWD LAMP INOP. (RESOLVED ON W/O: 162971, TASKCARD: N/R-00007 ) R & R CABIN CEILING CURVED EMERGENCY EXIT SWD LAMP IAW AMM 33-51-14. OPS CHECK GOOD. R & R CABIN CEILING CURVED EMERGENCY EXIT SWD LAMP IAW AMM 33-51-14. OJun 11, 2010 · N930EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201000887Channel · crackedINDICATION NOTES AT FS 409+128 RBL 18 WL 69.0 IN RADIUS OF OTBD U CHANNEL OF THE BULKHEAD BEAM APPROX .30" LONG 50 PERCENT FULL SCREEN HEIGHT. REMOVED RBL 18 VERTICAL POST ASSY & SEPARATED INBD & OTBD HALVES IAW SRM 51-42-06. LOCATED & DRILLED NEW SERVICEABLJun 10, 2010 · N684BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000888Channel · crackedINDICATION NOTED AT FS 409+128 RBL 18 WL 69.00 VERTICAL POST OUTBD U-CHANNEL IN RADIUS VERTICALLY APPROX .30 IN LENGTH 55 PERCENT FSH. REMOVED OTBD POST IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW OTBD POST IAW SRM 51-40-11. ASSEMBLED NEW OTBD POJun 10, 2010 · N860AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000889Bulkhead · crackedFOUND FS 559 RT BULKHEAD WEB HAS INDICATION NOTED OTBD OF RBL 9.0 WL 54.10 APPROX .4" IN LENGTH 80 PERCENT FSH. FAILED NDT INSPECTION. C/W EC/TC REO 601R-57-41-260 IAW REO 601R-53-41-260 REV D.Jun 10, 2010 · N860AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201000890Seat Track · corrodedAFT CARGO COMPARTMENT SEAT RAILS AT LBL 9 BETWEEN FS 559+110 AND FS 569.00 BETWEEN FS 612.00 AND FS 617.00 ARE CORRODED. REMOVED AFT CARGO COMPARTMENT SEAT RAILS AT LBL 9 BETWEEN FS 559+110 AND 569.00, FS 612 - FS 617.00 AND INSTALLED SERVICEABLE SEAT RAILS BJun 10, 2010 · N860AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000892Seat Track · corrodedAFT CARGO COMPARTMENT SEAT RAILS AT RBL 27 BETWEEN FS 559+80 AND FS 559+96 IS CORRODED. REMOVED AFT CARGO COMPARTMENT SEAT RAIL AT RBL 27 BETWEEN FS 559+80 AND FS 559+96. DRILLED AND COUNTERSUNK SCREW HOLES IN SERVICEABLE RAIL IAW SRM 51-40-11 AND INSTALLEJun 10, 2010 · N860AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201040605Strip · chafedLT UPPER NOSE COWL T/E CHAFED. REPLACED AFT EDGE STRIP PN 228-50080-107 IAW CMM 71-14-01-300-814-A01 REPAIR NR SRS091.Jun 10, 2010 · N406AW · Cndair CL6002B19 · Engine Air Intake SystemSDR CA100615005Cell · leakingUPON BATTERY COMING IN FOR INSP, IT WAS FOUND THAT 9 CELLS WERE LEAKING AT SEAMS ALONG THE CELL EDGES, ACCORDING TO SHOP PERSONEL, THIS IS THE USUAL AREA FOR THE CELLS TO LEAK FROM, DUE TO THE AMOUNT OF CELLS FOUND LEAKING, THE BATTERY WAS DETERMINED TO BE BADJun 10, 2010 · Cndair CL6002B19 · Battery/Charger SystemSDR ASOA201000876Lamp · inoperativeNR 2 CEILING EMERGENCY LIGHT INOP. RELAMPED NR 2 CEILING EMERGENCY LIGHT IAW IAW AMM 33-51-16 / ITEM: 1. RELAMPED NR 2 CEILING EMERGENCY LIGHT IAW AMM 33-51-16.Jun 9, 2010 · N451CA · Cndair CL6002B19 · Emergency LightingSDR ASOA201000877Seat Track · corrodedLEFT AND RT FWD FLOOR SEAT TRACK SEGMENT IN CABIN ARE CORRODED AT THE FWD ENDS. REMOVED LT AND RT FWD SEAT TRACKS IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACKS LT AND RT FWD SECTION IAW AMM 53-01-11-400-802.Jun 9, 2010 · N684BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000886Circuit Breaker · odorIN FLIGHT HEAVY ELECTRICAL OZONE SMELL. ODOR LASTED 5-10 SECONDS DID NOT RETURN NO CIRCUIT BREAKERS WERE POPPED ALL SYSTEMS NORMAL. R & R HYD PUMP NR 2 C/B AND TRU NR 1 C/B IAW AMM 20-23-00. OPS CK GOOD.Jun 9, 2010 · N838AS · Cndair CL6002B19 · Hydraulic Power System WiringSDR A6WA201040599Floorbeam · crackedINBD CLIP ON RBL 9 AT FS 280 IS CRACKED. R & R CLIP AT FS 280, INBD SIDE OF RBL 9.0 IAW SRM 51-42-21.Jun 6, 2010 · N406AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR CA100607004Bpsu · failedON APPROACH THE FLAPS FAILED AT ZERO DEGREES. AN EMERGENCY WAS DECLARED AND THE ACFT CARRIED OUT AN UNEVENTFUL FLAP ZERO LANDING. FECU CODES 12 & 13 WERE POSTED FOR THE LT BPSU. THE LT BPSU WAS REPLACED, MANUAL TORQUE TEST WAS CARRIED OUT WITH NO FAULTS, SOMJun 5, 2010 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA201000865Bulb · inoperativeAFT CABIN AND RT NR 2 OUTSIDE EMERG LIGHTS DO NOT OPERATE. REMOVED THE AFT CABIN EMERGENCY LIGHT LENS. R & R THE BULB AND REINSTALLED THE LENS. REMOVED THE 4 SCREWS OF THE RT NR 2 OUTSIDE EMERGENCY LIGHT. R & R THE BULB AND INSTALLLED THE 4 SCREWS OF THE RT Jun 4, 2010 · N907EV · Cndair CL6002B19 · Emergency LightingSDR A6WA201040571Bracket · crackedLT JET PIPE PANEL 436BR NUT PLATE BRACKET IS CRACKED IN HALF XN 221.0. R & R BRACKET IAW SRM 51-42-06, 51-40-11.Jun 4, 2010 · N438AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR ASOA201000864Post · crackedFOUND FS 409+128 VERTICAL POST BL 0.0 LT SIDE HAS INDICATION NOTED APPROX .3 IN LENGTH 80 PERCENT FSH AT WL 60.0 AFT FLANGE RADIUS. FAILED NDT INSP. COMPLIED WITH EC/TC REO 601R-53-41-1213 AND REO 601R-53-41-1213 REV A DATED 05/18/2010 AS WRITTEN.Jun 3, 2010 · N824AS · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA201040563Access Panel · crackedTAILCONE ACCESS DOOR 361AB HAS A CRACKED LOUVER REPAIRED TAILCONE ACCESS DOOR CRACKED LOUVERS IN (2) LOCATIONS IAW REO 601R-53-84-012.Jun 1, 2010 · N438AW · Cndair CL6002B19 · Aerodynamic FairingsSDR CA100604002Skin · damaged(CAN) WHILE ON FINAL, ACFT SUFFERED FROM A BIRD STRIKE. DURING POST FLIGHT INSP CREW REPORTED A SIGNIFICANT STRUCTURAL DAMAGE ABOVE THE RADOME BELLOW THE LT WINDSCREEN. MX WAS DISPATCHED ON SITE AND CONFIRMED STRUCTURAL DAMAGE AT FUSELAGE STATION (FS)193.00 May 29, 2010 · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA201000082Pump · wornAT CRUISE ALTITUDE OF FL330 ON A REVENUE FLIGHT FROM KAUS TO KMEM, THE R ENG OIL PRESS WARNING MESSAGE ILLUMINATED. THE FLIGHT CREW COMPLETED THE QRH AND CONTACTED COMPANY DISPATCH AND MAINTENANCE. BECAUSE OF PREVIOUS OIL PRESSURE FLUCTUATION WRITE UPS ON THMay 23, 2010 · N8908D · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA201040369Fitting · crackedBATHTUB FITTING AT FS 484, RBL 9 CRACKED. FLAGGED R & R WITH SERVICEABLE BATHTUB FITTING PN 600-31068-19 AT FS 484, RBL9 ALL WORK DONE IAW SRM 51-42-06, 51-42-21, 51-21-11.May 23, 2010 · N437AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201040491Strip · chafedLT UPPER NOSE COWL AFT EDGE STRIP IS CHAFED. R & R STRIP ON LT ENGINE UPPER NOSE COWL AFT EDGE IAW BOM CMM 71-14-01.May 22, 2010 · N422AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA201040494Skin · erodedRT ENGINE NOSE INLET COWL L/E OUTER SKIN HAS EROSION DAMAGE. REPAIRED THE RT ENGINE NOSE INLET COWL L/E OUTER SKIN EROSION DAMAGE.May 21, 2010 · N442AW · Cndair CL6002B19 · Engine Air Intake SystemSDR A6WA201040493Skin · erodedLT ENGINE INLET L/E OUTER SKIN HAS EROSION DAMAGE. REPAIRED THE LT ENGINE INLET L/E OUTER SKIN EROSION DAMAGE.May 21, 2010 · N442AW · Cndair CL6002B19 · Engine Air Intake SystemSDR MALA100075Lamp · inoperativeLEFT EXTERNAL EMERGENCY LIGHT FWD OF WING L/E INOP. RELAMPED LT EXTERNAL EMERGENCY LIGHT IAW AMM CH 33-50. OPS CHECK NORMAL PN 1317.May 18, 2010 · N477CA · Cndair CL6002B19 · Emergency LightingSDR REXA201000080Warning Message · false activationAS THE THRUST LEVERS WERE ADVANCED FOR TAKEOFF, THE L REV UNLOCK CAUTION MESSAGE ILLUMINATED. THE FLIGHT CREW ELECTED TO ABORT THE TAKEOFF AND PULL OFF THE RUNWAY. THIS ACFT HAD A PREVIOUSLY DEFERRED LT THRUST REVERSER. DUE TO THE MEL REQUIREMENT TO REMOVE May 18, 2010 · N8907A · Cndair CL6002B19 · Engine Thrust ReverserSDR REXA201000081Oil System · fluctuatesAFTER REACHING CRUISE ALTITUDE OF FL330 ENROUTE, CAPTAIN OBSERVED RT ENGINE OIL PRESSURE FLUCTUATING FROM 42 TO 27 PSI. FLT CREW PERFORMED QRH & REDUCED THRUST ON RT ENGINE. JUST AS THE THRUST REDUCED, RT ENG LOW OIL PRESSURE MESSAGE ILLUMINATED FOR ABOUT 2May 18, 2010 · N8877A · Cndair CL6002B19 · Engine Oil Indicating SystemSDR ASOA201000866Windshield · crackedIN FLT AT 250FL CAPT'S SIDE WINDSCREEN FORMED A CRACK. ALSO, RECEIVED LT WINDSCREEN HEAT CAUTION MSG. R & R CAPTS WINDSHIELD IAW AMM 56-11-01. (CLOSED)May 18, 2010 · N977EV · Cndair CL6002B19 · Flight Compartment WindowsSDR ASOA201000786Placard · tornPAX DOOR EXIT PLACARD TORN. REMOVED TORN "EXIT" PLACARD IAW AMM TASK 11-30-00-000-801 & INSTALLED NEW PLACARD S1574-18 TO PAX DOOR STEP IAW AMM TASK 11-30-00-400-801.May 15, 2010 · N907EV · Cndair CL6002B19 · Placards and MarkingsSDR A6WA201040357Lug · gougedLT INBD FLAP AFT LUG FOR INBD HINGE ARM HAS DEEP GOUGE SCRATCH ON INBD SIDE. REPAIRED LT INBD FLAP AFT INBD LUG IAW REO 601R-57-52-1536.May 15, 2010 · N442AW · Cndair CL6002B19 · Trailing Edge FlapsSDR ASOA201000737Floorbeam · corrodedBULKHEAD FITTING ON FLOORBEAM CAP RBL 9 AT FS 621 CORRODED. REMOVED BULKHEAD FITTING ON FLOORBEAM CAP IAW SRM 51-42-21. DRILLED AND LOCATED NEW SERVICEABLE FITTING IAW SRM 51-40-11. INSTALLED FITTING AT FLOORBEAM CAP IAW SRM 51-41-02 AND REO 601R-53-61-3679May 14, 2010 · N824AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201000738Bulkhead · crackedFOUND FS 559 BULKHEAD WEB RT SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 60 PERCENT FSH OTBD OF RBL 9.0, WL 58.70. FAILED NDT INSPECTION. C/W ECTC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV D.May 14, 2010 · N907EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201000739Post · crackedFOUND FS 409.0+128 VERTICAL POST RBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .3" IN LENGTH 60 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSP. REMOVED ADEL CLAMPS TO ACCESS POST IAW THE SRM 51-41-02. REMOVED THE POST IAW THE SRM 51-42-06. INSMay 14, 2010 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000740Post · crackedJOB 8764825 /OPERATION 99. FOUND FS 409.0+128 VERTICAL POST BL 0.0 LT SIDE HAS INDICATION NOTED APPROX .3" IN LENGTH 80 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSPECTION. REMOVED VERTICAL POST COMMON TO FS 409+128 BL0 IAW 51-42-06. DRILLED UP May 14, 2010 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000742Stringer · crackedFOUND VISUAL EVIDENCE OF CRACK RADIATING FROM RIVET AT FS 718.00 UPPER SIDE OF STRINGER 10 LT CORNER OF STR 10 LT AND FS 718 (MARKED WITH YELLOW TAPE). PERFORMED EDDY CURRENT INSP ON NOTED AREA IAW NDTM 51-20-06. NO INDICATIONS NOTED (REMOVED YELLOW TAPE).May 14, 2010 · N907EV · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR ASOA201000744Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED APPROX .3" IN LENGTH 50 PERCENT FSH AT LBL 27.50, WL 130 LOCATED TOP OF AFT CARGO DOOR TRACK. FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-61-1541 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-May 14, 2010 · N907EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201000745Support Beam · crackedFOUND CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE HAS A CRACK IN RADIUS APPROX .5" IN LENGTH. REMOVED ANGLE IAW SRM 51-42-21. REINSTALL ANGLE AFTER REAR PRESSURE BULKHEAD REPAIR HAS BEEN COMPLETED4. INSTALLED NEW ANGLE ON CARGO DOOR SUPPORT BEAM AFT LOWER IAW SRMay 14, 2010 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040359Strip · chafedRT ENGINE LOWER NOSE COWL AFT EDGE STRAP IS CHAFED, SHORTS IPC 71-14-01, FIG 2, ITEM 105. R & R WITH SERVICEABLE AFT EDGE STRIP PN 228-50081-108 AT RT ENGINE LOWER NOSE COWL WORN DOWN IAW SRM 51-21-11, 51-25-06, 57-25-18.May 14, 2010 · N437AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201040361Strip · chafedRT ENGINE UPPER NOSE COWL AFT EDGE STRIP IS CHAFED, SHORTS IPS 71-14-01, FIG 1, ITEM 45. R & R WITH SERVICEABLE AFT EDGE STRIP PN 228-50080-108 AT RT ENGINE UPPER NOSE COWL ALL WORK DONE IAW CMM 71-14-01, SRM 51-21-11, 51-25-06, 51-25-16.May 14, 2010 · N437AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR ASOA201000731Light · looseBURNING SMELL FROM OVER HEAD ON ROW EIGHT. INSPECTED ACFT , NO SMELL NOTED. FOUND CEILING LIGHT AT ROW 8AB LOOSE, REINSTALLED AND FOUND BULBS INOP. REF AMM 33-21-01, REFER TO AFDL 535230-1.May 13, 2010 · N860AS · Cndair CL6002B19 · Passenger Compartment LightingSDR REXA201000078Warning Light · false activationAT CRUISE ALTITUDE, ENROUTE, THE R REV UNLOCK MESSAGE ILLUMINATED. THE FLIGHT CREW COMPLETED THE QRH AND DETERMINED THAT THE THRUST REVERSER WAS NOT ACTUALLY DEPLOYED. FLIGHT CREW ELECTED TO PERFORM AN AIR RETURN. AN OTHERWISE NORMAL APPROACH AND LANDING WEMay 13, 2010 · N827AY · Cndair CL6002B19 · Engine Thrust Reverser
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