GE CF34-3B1

Service difficulty reports · 5,402

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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 = '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 VNAA2010122200010Engine · vibrationCREW REPORTED THE RIGHT ENGINE MADE A NOISE AND INDICATED A VIBRATION 3.8. AIRCRAFT RETURNED TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE USING THE AIRCRAFT MAINTENANCE MANUALS COULD NOT DUPLICATE PROBLEM. AIRCRAFT WAS RELEASED FOR SERVICE.Dec 16, 2010 · N262PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA201040962Wire · sparksWHILE GETTING DE-ICED, PILOTS HEARD STRANGE SOUND IN COCKPIT, GOT UP FROM SEAT, SAW WIRES FROM CB PANEL 2 GLOWING AND SPARKING. HAD F/O TURN NR 2 GEN OFF, SELECTED AUTO TRANSFER SWITCH OFF, GRABBED COCKPIT FIRE EXTINGUISHER, PUT GLOWING AND SPARKED WIRES (REFDec 16, 2010 · N431AW · Cndair CL6002B19 · Electrical Power System WiringSDR A6WA201040963Cover · crackedAPU ENCLOSURE COVER CRACKED, TOP CTR. REPAIRED APU ENCLOSURE DOOR 311BS BY WELDING IAW REO 601R-49-11-070, REV A.Dec 16, 2010 · N457AW · Cndair CL6002B19 · APU Cowling/ContainmentSDR MALA100201Insulation · frozenRT OVERWING EMERGENCY EXIT DOOR HARD TO REMOVE FROM ACFT DUE TO FROZEN INSULATION BRICK BEHIND DOOR HANDLE, WHILE PERFORMING JOB CARD 52-840-603. REMOVED WET/FROZEN INSULATION BRICKS IN RT OVERWING EXIT DOOR - AREA FOUND TO BE CORROSION FREE - ACFT ACCEPTABLE Dec 15, 2010 · N831AY · Cndair CL6002B19 · Emergency ExitsSDR ASOA201001972Floor Support · corrodedCARGO BAY FLOOR SUPPORT CAP AT LBL 27 FS 621 TO 574 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. INSTALLED NEW FLOOR SUPPORT IAW REO 601R-53-61-3778 AND SRM 51-42-06.Dec 15, 2010 · N882AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001973Cargo Track · corrodedCARGO TRACK IS CORRODED. LOCATED, DRILLED 7 COUNTERSUNK HOLES IN NEW CARGO TRACK IAW SRM 51-41-02. INSTALLED NEW SERVICEABLE CARGO TRACKS IAW AMM 53-01-11-400-802. MINOR REPAIR.Dec 15, 2010 · N882AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201040956Hinge Fitting · nickedUPPER CTR RUDDER HINGE PITTING ARM ON VERTICAL STAB HAS MINOR NICK ON AFT EDGE. REPAIRED IAW REO 601R-55-31-204.Dec 15, 2010 · N457AW · Cndair CL6002B19 · Rudder StructureSDR A6WA201040964Controller · inoperativeLT WINDSHIELD HEAT CAUTION MSG IN FLIGHT. COMPLIED WITH QRH AND MESSAGE PERSISTS. R & R LT WINDSHIELD CONTROLLER AND ANTI-ICE CONTROL PANEL IAW AMM 30-41-01 AND OPS TEST IAW AMM 30-12-21. M/C WINDSHIELD HEAT CONTROL SWITCH WAS BAD.Dec 15, 2010 · N446AW · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR A6WA201040958Skin · erodedLT ENGINE INLET LIP SKIN HAS EROSION DAMAGE. LT ENGINE INLET LIPSKIN HAS CORROSION AT 315 AREA, SANDED LIPSKIN REMAINING .003 MATERIAL WITH .060 MATERIAL. REMAINING AREA IS WITHIN LIMITS IAW CMM 71-61-01, FIG 5003N.Dec 14, 2010 · N454AW · Cndair CL6002B19 · Engine Air Intake SystemSDR A6WA201040959Skin · corrodedRT ENG INLET LIP SKIN PITTED. REMOVED LIGHT PITTING ON RT ENG INLET LIP SKIN BY SANDING. REMOVING .004 MATERIAL WITH .059 MATERIAL REMAINING, THE LIPSKIN IS WITHIN LIMITS IAW CMM 71-61-01, FIG 5003 LIGHT.Dec 14, 2010 · N454AW · Cndair CL6002B19 · Engine Air Intake SystemSDR A6WA201040957Skin · gougedSERVICE DOOR EXTERIOR HANDLE CUT OUT HAS 5 SMALL AREAS WITH MINOR DAMAGE. REPAIRED SERVICE DOOR SKIN AND DOUBLER AROUND EXTERIOR HANDLE CUT OUT IAW REO 601R-52-41-159, DATED 2010-12-12.Dec 13, 2010 · N457AW · Cndair CL6002B19 · Galley DoorsSDR ASOA201001933Sign · inoperativeFWD LT FLOOR LEVEL EXIT SIGN INOP. R & R LT FWD FLOOR LEVEL EXIT SIGN ASSY IAW AMM 33-51-10. OPS CHECK GOOD.Dec 12, 2010 · N923EV · Cndair CL6002B19 · Emergency LightingSDR A6WA201040938Duct · disconnectedRT 10TH STAGE DUCT WARNING MESSAGE. CLEARED WHEN TURNING OFF RT PACK. INSP AND FOUND DISCONNECTED DUCT BETWEEN PRECOOLER AND HEAT EXCHANGER ON RT PACK. REPLACED SEAT AND CLAMP IAW AMM 21-51-07. OPS CK GOOD.Dec 12, 2010 · N445AW · Cndair CL6002B19 · Pneumatic Distribution SystemSDR ASOA201001931Unknown · odorFAINT ELECTRICAL BURNING ODOR EMANATING OCCASSIONALLY FOR BREIF PERIODS BY FOS DCU SWITCHES. INSPECTED WIRING AND ALL ELECTRICAL COMPONENTS IN THE FOS AREA AND FOUND NO DEFECTS OR EVIDENCE THERE OF IAW ESPM 20-12-00.Dec 11, 2010 · N861AS · Cndair CL6002B19 · Air Distribution SystemSDR ASOA201001932Floorbeam · corrodedRT CABIN FLOOR SUPPORT STRUCTURE CORRODED AT FS 349.00, RBL 36. REMOVED LIGHT CORROSION FROM RT CABIN FLOOR SUPPORT STRUCTURE AT FS 349.00 RBL 36 IAW SRM 51-21-06, STEP 3. .004" OF MATERIAL REMOVED. TREATED AREA IAW 52-21-11 AND APPLIED PRIMER AND PAINT IAW Dec 9, 2010 · N867AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001911Nut Plate · brokenAFT CARGO AFT PRESSURE BULKHEAD HAS NUTPLATE BROKEN AT CTR ROW, 2ND ROW UP FROM FLOOR (ISOLATOR). REMOVED BROKEN ISOLATOR MOUNT ON AFT PRESS BULKHEAD & INSTALLED NEW ISOLATOR MOUNT IAW SRM 51-42-13 THIS IS A MINOR REPAIR.Dec 8, 2010 · N848AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201001912Ecu · inoperativeASCENDING THROUGH 10-11K RECEIVED NWS INOP CAUTION COULD NOT EXTINGUISH. RETURN TO DEPARTURE. (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED) PERFORMED OPS CHECK OF NWS ECU IAW AMM 32-51-10-05. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. (CLDec 8, 2010 · N934EV · Cndair CL6002B19 · Landing Gear Steering SystemSDR A6WA201040935Control Column · bindingAILERONS BINDING AND AUDIBLE SNAP SOUND DURING FLIGHT CONTROL CHECK. BOTH CONTROL COLUMNS AND BOTH DIRECTIONS. LT COLUMN BINDING AT LT DEFLECTION, RT COLUMN BINDING MID AND 1/2 DEFLECTION. C/W PARA 4 OF GREO 601R-27-11-031 "DISPOSITION FOR ACFT DISPATCH. RDec 8, 2010 · N405AW · Cndair CL6002B19 · Control Column SectionSDR A6WA201040936Pdu · malfunctionedWHILE CLIMBING THRU FLIGHT LEVEL 255. RECEIVED R-REV UNLOCK CAUTION MESSAGE. BOTH REVERSER DISARM AT THE TIME MESSAGE RECEIVED. MESSAGE PERSISTED UNTIL ENGINE SHUTDOWN AT GATE C/W QRH. DIVERTED. R & R RT T/R PDU IAW AMM 78-32-03. OPS CHECKED GOOD, REMOVEDec 8, 2010 · N408AW · Cndair CL6002B19 · Engine Thrust ReverserSDR ASOA201001871Glowstrip · missingPHOTOLUMINSCENT STRIP MISSING ON AFT SIDE OF SERVICE DOOR. INSTALLED PHOTOLUMINSCENT MISSING STRIP ON AFT SIDE OF SERVICE DOOR IAW AMM, CH 11-30-00. INSTALLED PHOTOLUMINSCENT MISSING STRIP ON AFT SIDE OF SERVICE DOOR IAW AMM CH. 11-30-00.Dec 6, 2010 · N854AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA201001872Bulb · burned outAFT EMERGENCY CEILING LIGHT IS INOP. R & R AFT EMERGENCY CEILING LIGHT BULB IAW AMM 33-51-16. OPS CHECKED GOOD/ITEM: 1/ R & R AFT EMERGENCY CEILING LIGHT BULB IAW AMM 33-51-16. OPS CHECKED GOOD.Dec 6, 2010 · N858AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001873Seat Track · corrodedLT AND RT FWD FLOOR SEAT TRACKS ARE CORRODED. INSTALLED A NEW SERVICEABLE LT AND RT FWD FLOOR SEAT TRACKS IAW AMM 53-01-11-400-802.Dec 6, 2010 · N867AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001874Drag Angle · crackedPAX DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED IAW REO 601R-52-11-513.Dec 6, 2010 · N867AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001875Inverter · inoperativeRT OVERWING FLOOR LEVEL EXIT ID INOPERATIVE. R & R NR3 EMERGENCY LIGHT INVERTER IAW MM 33-51-07-000-801 & -400-801. EMERGENCY LIGHTS OPS CK OK IAW MM 33-51-00-710-801.Dec 6, 2010 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201001867Light · damagedFLOOR EMERGENCY LIGHT BY PAX ENTRY WAY BACKING/HSG DAMAGED. R & R FLOOR EMERGENCY BY PAX DOOR ENTRY WAY BASE IAW AMM 33-51-19. OPS CHECK GOOD. R & R FLOOR EMERGENCY BY PAX DOOR ENTRY WAY BASE IAW AMM 33-51-19. OPS CHECK GOOD. (CLOSED)Dec 5, 2010 · N846AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001868Light · inoperativeEXTERIOR RT AFT FUSELAGE EMERGENCY (OVER WING) LIGHT IN-OP. R & R RT AFT FUSELAGE EXTERIOR LIGHT IAW AMM 33-51-21. OP CKS GOOD.Dec 5, 2010 · N929EV · Cndair CL6002B19 · Emergency LightingSDR MALA100184Relay · malfunctionedDURING FLIGHT RECEIVED "EMERGENCY LIGHTS ON" STATUS MESSAGE WITH SWITCH IN THE ARM POSITION. F/A REPORTED NUMEROUS BUT NOT ALL OF THE EMERGENCY LIGHTS ILLUMINATED IN THE CABIN. R & R K1XD SENSE RELAY. OPS CHECKS GOOD W/REF TO AMM 33-51.Dec 4, 2010 · N8948B · Cndair CL6002B19 · Emergency LightingSDR CA101213002Element · failed(CAN) DURING THE CLIMB OUT THE CREW RECEIVED A "R 10TH STAGE DUCT" MASTER WARNING MESSAGE. THE QRH CHECKLIST REQUIRED THE CREW TO RETARD THE RT THRUST LEVER TO IDLE. A SINGLE ENGINE APPROACH AND LANDING WERE COMPLETED WITHOUT FURTHER INCIDENT. MAINTENANCE INVEDec 4, 2010 · Cndair CL6002B19 · Overheat DetectionSDR A6WA201040961Fitting · chafedOTBD FLAP ROLLER GUIDE FITTING (RT SIDE) HAS CHAFING DAMAGE, BLENDED CHAFED AREA AT RT OTBD FLAP GUIDE FITTING, REMOVING .028 OF MATERIAL WITHIN LIMITS IAW REO 601R-57-51-1453.Dec 2, 2010 · N457AW · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA201000284Pan · damagedTHE GROUND POWER UNIT (GPU) ACCESS POWER RECEPTACLE WAS DAMAGED. THE DAMAGE CONSISTS OF THE POWER RECEPTACLE BEING PULLED FROM THE INSTALLED POSITION IN THE RECESSED PAN AREA. TEMPORARY REPAIR IAW STS EA 1-2010-207. REPEAT INSPECT DAILY, FLY ON FOR 10 DAYS WIDec 1, 2010 · N8506C · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA201040880Coalescer Bag · odorAFTER STARTING ENGINES, CABIN AND COCKPIT WAS ENGULFED WITH THE ODOR OF OIL. R & R LT PACK COALSER BAG, RAN BOTH APU AND ENG AIR NO OIL SMELL NOTED.Dec 1, 2010 · N402AW · Cndair CL6002B19 · Humidity Control SystemSDR REXA201000280Skin · dentedA SINGLE INDENTATION WAS FOUND ON THE RT WING OTBD GROUND SPOILER UPPER SURFACE. THE DAMAGE IS RECORDED AS 0.049 INCH DIAMETER AND A MAXIMUM DEPTH OF 0.006 INCH AND IS LOCATED 3.7 INCHES AFT OF THE L/E AND 7.68 INCHES FROM THE OTBD EDGE. TEMPORARY REPAIR IAW SNov 29, 2010 · N801AY · Cndair CL6002B19 · SpoilersSDR MALA100179Light · malfunctionedEMER LTS ON STATUS MESSAGE. EMERGENCY LIGHTS CAME ON INTERMITTENTLY WITH SWITCH IN ARMED POSITION. HALF OF THE EMERGENCY LIGHT - LT WINDOW EXIT SIGN, MAIN PAX DOOR EXIT SIGNS - ILLUMINATE. DEFERRED CABIN EMERGENCY LIGHTS IAW MEL 33-51-1-7 ENTERED IN MM02 MXC NNov 29, 2010 · N8948B · Cndair CL6002B19 · Emergency LightingSDR CA101201001Window · crackedREF DEFECT-953421 LP-540409 CAPT SIDE WINDOW CRACKING. PIREP- "WHILE ON DECENT INTO THE YVR TERMINAL AREA THE CAPTAIN`S SIDE WINDOW DEVELOPED A CRACK FROM THE FRONT TO BACK SIDES OF THE WINDOW. IN UNDER A FEW MINUTES TWO ADDITIONAL CRACKS DEVELOPED OF SIMILANov 29, 2010 · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA201040879Warning Light · illuminatedDC EMERGENCY BUSS CAUTION MESSAGE ENROUTE. FOUND CBP1-R7 POSER SENSE TO BE POPPED. RESET BREAKER MESSAGES CLEARED. C/W OPS CHECK OF LT AND RT FIRE EXT IAW AMM 26-11-00, APU EXT IAW AMM 26-12-11, AND RT FUEL SOV IAW AMM 28-21-36, BATT DIRECT FEED IAW AMM 24Nov 28, 2010 · N407AW · Cndair CL6002B19 · DC Power Distribution SystemSDR A6WA201040874Skin · chafedL/E OF FLAP FAIRING 697BB IS CHAFED. BLENDED AREA IAW SRM 51-12-00.Nov 28, 2010 · N414ZW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040875Skin · gougedLT INBD FLAP L/E PANELS 584AB AND 584BB ARE GOUGED, BLENDED OUT GOUGES ON FLAP PANELS IAW SRM 51-21-00.Nov 28, 2010 · N414ZW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040876Hinge · chafedFUSELAGE HALF OF PAX DOOR PIANO HINGE IS CHAFED ON AFT END ON THE LAND OF THE HINGE. REPAIRED DAMAGED HINGE IAW REO 406R-53-21-814 TYPE IV REPAIR.Nov 28, 2010 · N414ZW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA201040878Frame · corrodedFRAME STATION 349, CORRODED ON FWD & AFT FACE 6 O`CLOCK POSITION SECTION. REMOVED CORROSION ON FWD AND AFT FACE OF FRAME AT FS 349 IAW SRM 51-21-06 AND REPAIRED FUSELAGE STRUCTURE FS 349 AND STR 26L IAW REO 601R-53-21-1200.Nov 24, 2010 · N421ZW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA201040873Skin · chafedLT LOWER CORE COWL CHAFED FROM BLOCKER DOOR NEXT TO FWD LATCHES BLENDED DAMAGE IAW REO 601R-71-12-232, REV D AND WAS FOUND TO BE WITHIN ALLOWABLE LIMITS. DAMAGE MEASURES 4.00 LONG, 0.25 WIDE AND .007 DEEP. TREATED AREA IAW CMM 20-01-11 AND SRM 51-25-06.Nov 23, 2010 · N414ZW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201040863Torque Box · crackedLT LOWER CORE COWL CHAFED FROM BLOCKER DOOR NEXT TO FWD LATCHES. BLENDED DAMAGE IAW REO 601R-71-12-232, REV D AND WAS FOUND TO BE WITHIN ALLOWABLE LIMITS DAMAGE MEASURES 4.00 LONG, 0.25 WIDE AND .007 DEEP TREATED AREA IAW CMM 200 AND SRM 51-25-06.Nov 23, 2010 · N421ZW · Cndair CL6002B19 · Engine Thrust ReverserSDR CA101202002Flap System · failed(CAN) ON DESCENT INTO CALGARY COMING FROM WINNIPEG DURING EXTREME COLD CONDITIONS, WHEN THE PILOTS SELECTED 8 FLAPS THE EICAS REGISTERED A FLAP FAIL CAUTION MESSAGE (AMBER). THE FLAPS DID NOT MOVE AND WERE STILL AT 0. AS PER EMERGENCY CHECKLIST THE AIRCRAFT PNov 23, 2010 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA201001865Anchor Fitting · crackedPAX DOOR ANCHOR FITTING CRACKED. REPLACED AFT PAX DOOR ANCHOR FITTING IAW AMM 52-11-17-000-804 AND 52-11-17-400-804. PAX DOOR OP'S CHECK GOOD RII ACCOMPLISHED ON LISTED WVAC NRI BY INSPECTOR.Nov 22, 2010 · N927EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040877Sill · corrodedRT FLOOR SILL CORRODED AFT OF FS 349. REPAIRED RT FLOOR SILL BETWEEN FS 349 AND FS 379 AT WL 73.10 IAW REO 601R-53-21-326.Nov 22, 2010 · N421ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040872Bulkhead · chafedAFT SIDE OF RT 280 BULKHEAD CHAFED FROM GALLEY ACCESS DOOR. CUT OUT DAMAGE FROM AFT RT SIDE 280 BULKHEAD, BLENDED CHAFED AREA ON CHANNEL IAW REO 601R-53-11-1727 FAB, WEB FILLER AND WEB DOUBLER PRIMED TOP COAT INSTALLED PART IAW REO 601R-11-1727, REV D.Nov 21, 2010 · N414ZW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR CA101123006Actuator · damagedON NR 1 ENGINE, 7 O`CLOCK POSITION THRUST REVERSER ACTUATOR FORK END BROKEN. ACTUATOR REPLACED IAW 78-32-01 AMM. FUNCTIONAL CHECKS COMPLETED.Nov 21, 2010 · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201040865Vane · chafedRT INBD FLAP ON L/E HAS CHAFING DAMAGE IN 3 PLACES. REMOVED AND INSTALLED NEW SERVICEABLE TITANIUM CAPS ON RT INBD FLAP VANE L/E IAW SB 601R-57-022, REV B.Nov 20, 2010 · N421ZW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040905Angle · gougedANGLE ON AFT PRESSURE BULKHEAD 621.0 BETWEEN CARGO NET SUPPORT AND CONNECTOR PLUGS IS GOUGED. REPAIRED AND REINSTALLED ANGLE HORIZ FLANGE IAW REO AND 601R-53-61-109, REV NC.Nov 19, 2010 · N421ZW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040906Bulkhead · chafedRT AFT 280 BULKHEAD CHAFED FROM GALLEY DOOR. REMOVED CHAFING BY CUTTING OUT THE DAMAGED AREA ON RT AFT 280 BULKHEAD AND INSTALLING WEB DOUBLER, WEB FILLER IAW REO 601R-53-11-1727.Nov 19, 2010 · N421ZW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040869Bonding · corrodedLT UPPER PYLON T/E HAS 2 EA BONDING PLATES PN 601-37012-33 CORRODED. R & R LT UPPER PYLON T/E BONDING PLATES PN 601-37012-33 SRM 51-22-00.Nov 18, 2010 · N421ZW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
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