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 ASOA201001107Light · burned outSECOND FROM FRONT, EMERGENCY CEILING FLOOD LIGHT IS OUT. RELAMPED SECOND FROM FRONT EMERGENCY CEILING FLOOD LAMP WITH SERVICEABLE BULB AND OPS CHECK GOOD IAW AMM 33-51-06. ACFT OK FOR SERVICE. (CLOSED)Aug 13, 2010 · N978EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201001114Seat Track · corrodedCARGO BAY SEAT TRACK CORRODED AT FS 559+80 TO FS 559+112, LBL 9, 2EA. REMOVED SEAT TRACKS IAW SRM 51-41-02. RECEIVED SERVICEABLE SEAT TRACKS FROM STORES. LOCATED AND INSTALLED SEAT TRACKS IAW SRM 51-41-02.Aug 13, 2010 · N921EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001115Seat Track · corrodedCARGO BAY SEAT TRACK CORRODED AT FS 559+80 TO FS 559+112, RBL 9, 2EA.Aug 13, 2010 · N921EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001117Web · crackedFS 280, WEB CRACKED BELOW FLOOR OTBD OF RBL 9 AND OTBD LBL 9, CORRODED AT FLOOR BETWEEN RBL 9 AND LBL 9. C/W EC/TC REO 601R-53-11-926 IAW REO 601R-53-11-926 REV B.Aug 13, 2010 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001116Seat Track · corrodedCARGO SEAT TRACK CORRODED AT FS 559, RBL 27. REMOVED SEAT TRACKS AND FITTING IAW AMM 51-41-02. RECEIVED SERVICEABLE SEAT TRACK & FITTING FROM STORES, LOCATED AND INSTALLED IAW SRM 51-41-02.Aug 13, 2010 · N921EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001118Floorbeam · corrodedFWD FLOOR ANGLE AT FS 280 IS CORRODED AND REQUIRES REPLACEMENT. REMOVED AND REPLACED FWD FLOOR ANGLE AT STA 280 IAW SRM 51-42-06 AND 51-42-21.Aug 13, 2010 · N921EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201040622Shield · gougedRT ENGINE JET PIPE FAIRING FIRE LOOP SHIELD IS COUGED. R & R IAW SRM 51-42-02.Aug 12, 2010 · N446AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA201040727Shield · gougedLT ENGINE JET PIPE FAIRING (436AL) FIRE LOOP SHIELD IS GOUGED. R & R IAW CMM 78-11-00.Aug 12, 2010 · N446AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR ASOA201001110Angle · crackedFS 621-FS 625 OBLIQUE ANGLES LT CRACKED. REMOVED AND INSTALLED OBLIQUE ANGLE AT FS 621-FS 625 IAW SRM 51-42-21. PAINT REQUIRED. PAINTED REPAIRED AREA IAW SRM 51-25-16.Aug 11, 2010 · N889AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001111Floorbeam · crackedSUPPORT CLIPS AT FS 280, RBL 9.0 ARE CRACKED. REPLACEMENT OF SUPPORT CLIP AT FS 280, RBL 9.0 IAW REO 601R-53-11-926, REV B.Aug 11, 2010 · N921EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001092Bulkhead · crackedPERFORMED EDDY CURRENT INSP OF FWD PRESSURE BULKHEAD WEB AT FS 202.75 AT BRAKE CABLE ATTACH POINT IAW NDT INSP PROCEDURE ET.2. FWD PRESSURE BULKHEAD WEB IS CONFIRMED CRACKED AT THE 8 O'CLOCK AND 11 O'CLOCK POSITIONS LOOKING AFT AT BULKHEAD. BOTH INDICATIONS AAug 10, 2010 · N926EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040592Blocker Door · chafedLEFT THRUST REVERSER BLOCKER DOORS 1-10 CHAFED ON BACKSIDE FROM STOPS. REPAIRED IAW CMM 78-30-00. REPAIR NR SRS100.Aug 10, 2010 · N446AW · Cndair CL6002B19 · Engine Thrust ReverserSDR ASOA201001089Floor Support · crackedFLOOR SUPPORT CRACKED IN CARGO COMPARTMENT AT AFT PRESSURE BULKHEAD UNDER PANEL 281LLF. REMOVED LT FS 621 FLOOR SUPPORT ANGLE LT SIDE REF SRM 51-42-06 AND 51-42-21. DRILLED COUNTERSUNK AND TRIMMED NEW FLOOR SUPPORT ANGLE REF SRM 51-40-11. STARTED INSTALLINGAug 9, 2010 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001108Seat Track · corrodedSEAT TRACK HAS MINOR CORROSION, RBL 9.00 AT FS 559+80. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW AMM 20-21-00-910-004.Aug 9, 2010 · N926EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001109Seat Track · corrodedSEAT TRACK HAS MINOR CORROSION RBL9.00 AT FS 559 + 92. (APPX). REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW AMM 20-21-00-910-004.Aug 9, 2010 · N926EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201040593Bracket · crackedLT NOSE INLET MOUNTING FLANGE WIRE HARNESS BRACKET IS CRACKED AT 8 O`CLOCK POSITION. REPLACE BRACKET IAW SRM. REO`S REMOVAL OF INLET TO ACCOMPLISH REPLACEMENT.Aug 9, 2010 · N446AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR ASOA201001161Skin · corrodedBELLY CORROSION JUST FWD OF FRAME 319.17 BETWEEN 26L AND 26R. REMOVED 6 EA FASTENERS FROM 319 FRAME BETWEEN 26L & 26R IAW SRM 51-42-06. REMOVED CORROSION IAW SRM 51-21-06. AREA REQUIRES NDT TO DETERMINE MATERIAL REMOVED. PERFORMED UT THICKNESS INSP OF BLEND Aug 9, 2010 · N926EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201040744Angle · crackedRT INBD FLAP HINGE OTBD FAIRING ANGLE ON INBD HINGE CRACKED REF 16 SRM 57-21-55. R & R WITH DUPLICATED PART IAW SRM.Aug 9, 2010 · N445AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR REXA201000101Engine · failedDURING CLIMBOUT FROM KIND, AT 4000 FEET, THE AIRCRAFT EXPERIENCED A LEFT ENGINE FAILURE. ALL INDICATIONS WERE NORMAL UNTIL THE FAILURE. THE FLIGHT CREW COMPLETED THE QRH AND NOTIFIED ATC. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS VECTORED BACK TO KIND. Aug 6, 2010 · N8721B · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA201001073Indicator · false indicationCARGO BOTTLE LOW CAUTION MESSAGE IN FLT COMPLIED WITH QRH (ENROUTE, ACFT DIVERTED DUE TO MX - EMERGENCY EQUIPMENT DID RESPOND) INSPECTED BOTH CARGO FIRE BOTTLE PRESSURE GAUGES IAW AMM CH 26-25-01 AND PERFORMED OPS TEST IAW AMM CH 26-25-00. NO DEFECTS FOUND. AAug 4, 2010 · N857AS · Cndair CL6002B19 · Extinguishing SystemSDR CA100806002Actuator · failedFLIGHT CREW REPORTED THAT AN EXCESSIVE FORCE WAS REQUIRED WHEN TURNING THE AILERON CONTROL WHEEL AFTER THE AUTOPILOT HAD BEEN DISCONNECTED. MX WAS DISPATCHED TO THE ACFT AND FOUND THE AILERON SERVO ACTUATOR AT FAULT. THE AILERON SERVO ACTUATOR IS EQUIPPED WITAug 3, 2010 · Cndair CL6002B19 · Aileron Control SystemSDR CA100806014Priority Valve · failedGEAR DISAGREE ON TAKEOFF, 2 MAIN SHOWING AMBER, NOSE GREEN (LANDING GEAR RETRACTION SYS) AFTER TAKEOFF, CREW SELECTED GEAR UP. WHEN GEAR WAS ALMOST UP IN THE WHEEL WELLS, THEY GOT THE GEAR DISAGREE WARNING ALONG WITH THE 2 MAINS INDICATING AMBER. CREW REPORJul 29, 2010 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA201001044Door · bindingPAX DOOR HARD TO OPEN. REMOVED AND REPLACED RT EMERGENCY FLOOR LEVEL EXIT PANEL IAW CRJ 200 AMM 33-51-10 OPS CHECK GOOD NO DEFECTS AT THIS TIME. [SDR CLOSED]Jul 28, 2010 · N857AS · Cndair CL6002B19 · Emergency ExitsSDR ASOA201001046Cover · missingGALLEY SERVICE DOOR FLOOR EMERGENCY EXIT SIGN LIGHT COVER MISSING. (RESOLVED ON W/O: 168315/ TASKCARD: N/R-00004) REPLACED GALLEY SERVICE DOOR FLOOR EMERGENCY FLOOD LIGHT COVER IAW CMM 33-21-58. REPLACED GALLEY SERVICE DOOR FLOOR EMERGENCY FLOOD LIGHT COVER IJul 28, 2010 · N901EV · Cndair CL6002B19 · Emergency LightingSDR A6WA201040576Skin · puncturedRT WING FLIGHT SPOILER LOWER SURFACE DENTED/PUNCTURED REPAIRED IAW REO 601R-57-73-126.Jul 27, 2010 · N449AW · Cndair CL6002B19 · SpoilersSDR CA100716005Cap · corrodedTHE LIGHTNING PROTECTION END CAPS (P/N DSC740067-1 AND -2) ON THE LEFT AND RIGHT WERE FOUND DISBONDED FROM THE HORIZONTAL STABILIZER. THE ADHESIVE BETWEEN THE LIGHTNING PROTECTION STRAPS AND HORIZONTAL STABILIZER HAD BECOME BRITTLE OVER TIME AND THE EDGES HAD Jul 15, 2010 · Cndair CL6002B19 · Horizontal Stabilizer Miscellaneous StructureSDR ASOA201001005Angle · corrodedASD THRESHOLD ANGLE CORRODED. DISCONNECTED HANDRAIL ACTUATOR ROD FROM FITTINGS & REMOVED CORRODED ANGLE AND CAPS SRM 51-41-02, 51-42-06, 51-42-11, AND 51-42-21. STARTED INSTALLING ASD THRESHOLD ANGLE EXCEPT FOR NUTPLATES & FLOOR SUPPORT ANGLE IAW SRM 51-42-06Jul 13, 2010 · N683BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000994Lamp · inoperativeCABIN CEILING EMERGENCY LIGHT AT SEAT 4AB INOP. R & R CABIN CEILING EMERGENCY FLOOD LIGHT LAMP AT SEAT 4AB IAW AMM TASK 33-51-16-400-801, TESTED EMERGENCY LIGHTS IAW AMM 33-51-00-710-801 NO DEFECTS FOUND.Jul 8, 2010 · N977EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201000995Light · inoperativeEMERGENCY LIGHT (VERTICAL) AT PAX DOOR AND BOTH EMERGENCY LIGHTS AT SERVICE DOOR ARE INOP. TROUBLESHOT, FOUND EMERGENCY LIGHT WIRING SWAPPED FWD OF SERVICE DOOR OUTBD OF GALLEY. INSTALLED WIRING CORRECTLY IAW WDM 33-51-00 AND COMPLIED WITH OPS TEST OF THE EMJul 8, 2010 · N977EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201001002Cargo Track · corrodedBAGGAGE RAILS AND ANCHOR PLATES ARE SEVERLY CORRODED AND REQUIRE REPLACEMENT FROM FS 559+112 TO FS 621.00, LBL 9. REMOVED (2 EA) BAGGAGE RAILS AND (2 EA) ANCHOR PLATES FROM LBL 9 FS 559+112 TO FS 621.00 AND DRILLED TO FINAL SIZE. (2 EA) NEW SERVICEABLE BAGGAJul 8, 2010 · N861AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000992Isolator · crackedCARGO BAY AFT BULKHEAD MOUNT ISOLATOR IS CRACKED AT LBL 27, 2ND UP FROM FLOOR. (RESOLVED ON W/O: 164029 TASKCARD: N/R-00472 ) R & R CARGO BAY AFT BULKHEAD MOUNT ISOLATOR AT LBL 27 2ND UP FROM FLOOR IAW SRM 51-42-06. (CLOSED)Jul 7, 2010 · N930EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201000973Cover · crackedEXIT SIGN COVER CRACKED ON PANEL 231BLC. REMOVED EXIT SIGN COVER ON PANEL 231BLC IAW AMM 33-51-14-000-801 STEP 3,A,1 & INSTALLED NEW SERVICEABLE EXIT SIGN COVER ON PANEL 231BLC IAW AMM 33-51-14-400-801 STEP 3,A,1.Jul 2, 2010 · N861AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201000974Drag Angle · crackedPAX DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED PAX DOOR AFT DRAG ANGLE IAW EC/TC REO 601R-52-11-513 AND ALL REQUIREMENTS OF REO 601R-52-11-513 ARE MET.Jul 2, 2010 · N861AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201000975Seat Track · chafedLT & RT FLOOR LEVEL SEAT TRACKS FROM FS 409 TO FS 409+128 ARE CHAFED AND CORRODED AT SEVERAL LOCATIONS. REMOVED FLOOR SEAT TRACK AT LBL 9.0 IAW AMM 53-01-11-000-802. LOCATED AND DRILLED FASTENER HOLES IN FLOOR SEAT TRACK IAW SRM 51-40-11. PARTIALLY INSTALLEJul 2, 2010 · N861AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000971Receptacle · shortedIN FLIGHT HAS AN UNIDENTIFIED BAD ODOR ON FLIGHT DECK. FOUND GALLEY LIGHT RECEPTACLE BURNING AND MELTING . R & R GALLEY LIGHT ASSY IAW AMM 33-26-01 ACFT OK FOR SERVICE.Jul 1, 2010 · N840AS · Cndair CL6002B19 · Passenger Compartment LightingSDR ASOA201000972Angle · crackedLT & RT FS 621-FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED CRACKED OBLIQUE ANGLES, LT & RT AT FS 621- FS 625 IAW SRM 51-42-21. FABRICATED NEW OBLIQUE ANGLES ON RT AT FS 621 - FS 625 IAW REPAIR EO 601R-53-61-100. INSTALLED NEW OBLIQUE ANGLES LT & RT AT FS621-FSJul 1, 2010 · N861AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040518Structure · crackedRT ENG THRUST REVERSER 12 O`CLOCK POSITION CASCADE CRACKED AT 3 LOCATIONS. REPLACED 12 O`CLOCK POSITION CASCADE ON RT ENG IAW AMM78-33-01.Jul 1, 2010 · N402AW · Cndair CL6002B19 · Engine Thrust ReverserSDR SWIA201024459Combustion Liner · crackedLEFT ENGINE COMBUSTION LINER CRACKED BEYOND LIMITS. (BOROSCOPE INSP) REPLACED ENGINE.Jun 27, 2010 · N432SW · Cndair CL6002B19 · Turbine Engine Combustion SectionSDR A6WA201040480Blocker Door · chafedLT ENG T/R BLOCKER DOOR 1 THRU 5 HAVE CHAFE DAMAGE AT STOPS. REPAIRED LT ENG T/R BLOCKER DOORS 1 THRU 5 AT STOPS IAW CMM 78-30-00-300-8720-A. REPAIR NO SRS.Jun 27, 2010 · N402AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201040479Blocker Door · chafedLT ENGINE T/R BLOCKER DOORS 6 THRU 10 CHAFED AT STOPS. REPAIRED LT ENG T/R BLOCKER DOORS 6 THRU 10 AT STOPS IAW B/A CMM 78-30-300-820-A01, REPAIR NR SRS100.Jun 27, 2010 · N402AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201040573Cam · wornRT OTBD FLAP, FLAP VANES CAMS WORN MEASURED RT OTBD FLAP VANE CAMS AND FOUND CAMS TO BE IN SERVICEABLE LIMITS IAW REO 601R-57-53-195.Jun 23, 2010 · N438AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040639Rib · crackedBATT RIB IN LT MLG WW IS CRACKED, 601R107091-REF. REPAIRED CRACKED BATT RIB IAW REO 601R-57-51-046, REV B, REPAIR NR 2.Jun 23, 2010 · N402AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR ASOA201000931Lamp · inoperativeAFT EMERGENCY LIGHT OVERWING ON LT & RT SIDE INOP. R & R AFT EMERGENCY LIGHT LAMPS RT & LT SIDE IAW AMM 33-51-21-400-801, OPS CK'S GOOD.Jun 21, 2010 · N924EV · Cndair CL6002B19 · Emergency LightingSDR A6WA201040452Pdu · malfunctionedLEFT THRUST REVERSER UNLOCKED MESSAGE IN FLIGHT. DEACTIVATED LT THRUST REVERSER IAW AMM TASK 78-30-00-040802, R & R LT THRUST REVERSER PDU REF AMM 78-32-03, OPS CHECKED GOOD. REMOVED PLACARD AND REMOVED FROM MEL.Jun 21, 2010 · N449AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201040448Structure · crackedT/E RT THRUST REVERSER IS CRACKED AT THE 5:30 AND 6:30 POSITIONS. REMOVED DAMAGE AND INSTALLED DOUBLERS IAW REO 601R-78-30-3999.Jun 17, 2010 · N406AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201040434Fitting · chafedLT OTBD FLAP GUIDE ROLLER FITTING CHAFED. REPAIRED IAW REO 601R-57-53-809.Jun 16, 2010 · N438AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040608Rib · crackedBATT RIB CRACKED IN RT WW CUTOUT DAMAGE & INSTALL DOUBLER IAW REO 601R-57-51-046.Jun 16, 2010 · N406AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA201040432Strip · chafedLT ENGINE LOWER NOSE COWL AFT EDGE STRIP IS CHAFED. R & R UNSERVICEABLE LT ENGINE LOWER NOSE COWL AFT EDGE STRIP AND INSTALLED SERVICEABLE AFT EDGE STRIP IAW CMM 71-14-10.Jun 15, 2010 · N438AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201040607Skin · dentedC/W AWAC CARD 4DMI13898, REPAIR LT WING L/E DENT ( C-CHECK) SRM 57-41-31. REMOVED DAMAGED LT CTR L/E SKIN BETWEEN WS 149.58 & WS 247.95, & INSTALLED SERVICEABLE LT CTR L/E SKIN (PN 601R12057-3) IAW SRM 51-42-06, 51-40-11, 51-42-13.Jun 14, 2010 · N406AW · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA201000911Engine · failedLEFT ENGINE EXPERIENCED SEVERE DAMAGE DURING THE DEPARTURE PHASE OF FLIGHT. AROUND 3,000 FT, HEARD A LOUD BANG AND EXPERIENCED YAW. POWER WAS SET AROUND 88 PERCENT "N". (EMERGENCY DECLARED - A/C RETURNED TO DEPARTURE AFTER T/O) LT ENGINE ASSY WAS REPLACED.Jun 13, 2010 · N837AS · Cndair CL6002B19 · Engine (Turbine/Turboprop)
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