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 A6WA20104870Skin · chafedUPPER AND LOWER L/E OF LT AILERONS IS CHAFED. BLENDED OUT LOWER SKIN WITH .040 MATERIAL REMAINING FOUND TO BE WITHIN LIMITS IAW REO 601R-57-60-020, REV NC. UPPER SKIN FOUND TO BE OUT OF LIMITS. DRILLED AND INSTALLED NEW SERVICEABLE UPPER SKIN IAW SRM 51-40-Nov 18, 2010 · N421ZW · Cndair CL6002B19 · AileronsSDR A6WA201040868Plate · corrodedRT UPPER PYLON T/E HAS 2 EA BONDING PLATES (PN 601-37012-33) CORRODED. R & R RT UPPER PYLON T/E BONDING PLATES PN 601-37012-33 IAW SRM 51-22-00.Nov 18, 2010 · N421ZW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201040858Wire Harness · damagedOVERBOARD COOL FAIL MESSAGE AFTER T/O, C/W QRH, ACFT DID NOT PRESSURIZE. R & R OVERBOARD EXHAUST VALVE AND REPLACED SERVICE DOOR HARNESS AND 3 SERV PROX SENSORS. PRESSURIZED ACFT ON GROUND IAW AMM 21-31-00. OPS CHECKS GOOD.Nov 17, 2010 · N418AW · Cndair CL6002B19 · Door System WiringSDR A6WA201040852Apu · odorSTRONG FUEL ODOR IN COCKPIT. ISOLATED FUEL ODOR TO THE AUTO SHUTDOWN OF APU AT PREVIOUS STATION. APU IS ON MEL. RAN BOTH ENGINES WITH PACKS TO FULL HOT FOR 5 MINUTES. ODOR HAS DISSAPATED. REF 214540/3 FOR NEW DISCREPANCY.Nov 17, 2010 · N459AW · Cndair CL6002B19 · APU Engine Fuel and ControlSDR A6WA201040871Skin · chafedLT INBD FLAP INNER SKIN AT CENTER FLAP VANE ACTUATOR CARRIAGE CHAFED FROM BONDING JUMPER. REPAIRED LT INBD INNER SKIN AT CENTER FLAP VANE ACTUATOR CARRIAGE IAW REO 601R-57-52-1665 REV, NC.Nov 17, 2010 · N421ZW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040819Unknown · odorAPU WOULD NOT START IN FLIGHT. AFTER LANDING APU STARTED & FUEL ODOR NOTED IN CABIN RT AFTER START, THEN DISSAPATED SHORTLY AFTERWARDS. INSPECTED APU, FOUND NO FUEL LEAKS. RAN APU FOR 20 MINUTES, NO ODOR NOTED. OK FOR SERVICE.Nov 15, 2010 · N462AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA201040864Seat Track · corrodedNR 1 SEAT TRACKS ON RBL AND LBL 9 HAVE CORROSION. REMOVED OLD SEAT TRACKS IAW AMM 53-01-11. INSTALLED NEW SEAT TRACKS PN 126-2075 IAW AMM 53-01-11.Nov 11, 2010 · N421ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201040937Transmitter · malfunctionedAT FL340 AT 300 KIAS, DURING INITIAL DESCENT, ACFT ABRUPTLY NOSED DOWN. NOTICED GEAR AND FLAP INDICATION ON EDI, FLAPS SHOWED EXTEND TO 5 DEG AND RETURNED TO ZERO DISCONNECTED A/P. FLAP HANDLE NEVER MOVED FORM ZERO POSITION. REPLACED FAULTY LT FLAP POSITIONNov 11, 2010 · N451AW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR ASOA201001735Flashlight · intermittentF/O FLASHLIGHT FLASHES AND DIM. R & R F/O'S FLASHLIGHT IAW AMM 25-61-00. OPS CK GOOD.Nov 6, 2010 · N906EV · Cndair CL6002B19 · Emergency EquipmentSDR ASOA201001728Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .1" IN LENGTH 50 PERCENT FSH FAILED NDT INSP. REPAIRED PER EC/TC REO 601R-53-61-1230 AND REPAIR C/W REQUIREMENTS OF EC/TC AND REO 601R-53-61-1230 REV D.Nov 5, 2010 · N927EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201001729Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROX .2" IN LENGTH 60 PERCENT FSH LOCATED AT TOP OF AFT CARGO DOOR TRACK FAILED NDT INSP. COMPLIED WITH EC/TC REO 601R-53-61-1541 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-1541Nov 5, 2010 · N927EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201001730Cover · missingLOWER EXIT SIGN COVER IN GALLEY MISSING BY SERVICE DOOR. REPLACED GALLEY RT LOWER EXIT SIGN IAW AMM 33-51-10. OPS CK GOOD ACFT OK FOR SERVICE. (CLOSED)Nov 5, 2010 · N937EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201001724Bulkhead Web · crackedFOUND FS 559 RT BULKHEAD WEB HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT WL 59-10 INBD OF RBL 18.0, FAILED NDT INSP. REPAIRED PRESSURE BULKHEAD WEB AND CAP ANGLES7 IAW REO 601R-53-41-260, REV E.Nov 4, 2010 · N927EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201001720Floorbeam · corrodedFLOORBEAM CAP AT LBL 9 FS 605 IS CORRODED. REPAIRED FLOORBEAM.Nov 3, 2010 · N868AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR CA101109013Indicator · failed(CAN) ON APPROACH TO RWY18, THEIR FLAPS GOT STUCK AT 8 DEGREES. THE CREW EXECUTED A MISSED APPROACH CONSULTED DISPATCH AND MTC AND LANDED SAFELY AFTERWARDS. THEY DID NOT DECLARE AN EMERGENCY. NO ADVERSE PASSENGER REACTION REPORTED. FLAP FAIL MESSAGE, GEAR Nov 3, 2010 · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR ASOA201001718Lamp · burned outLT SIDE NR2 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LT SIDE NR 2 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CK GOOD.Nov 2, 2010 · N870AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001719Battery Pack · inoperativeEMERGENCY LIGHT NOT FUNCTIONING WHEN SELECTED ON. R & R EMERGENCY LIGHT BATTERY PACK, OPS CK GOOD. AMM 33-51-04-000-801-802.Nov 2, 2010 · N926EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201001710Battery · inoperativeF/A FLASHLIGHT INOP. R & R BATTERIES IAW AMM 25-60-00. OPS CK GOOD. (CLOSED)Nov 1, 2010 · N835AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA201001711Angle · crackedLT SIDE OBLIQUE ANGLE FROM FS 625 IS CRACKED. REMOVED ANGLE IAW SRM 51-42-21. INSTALLED NEW ANGLE IAW REO 601R-53-61-100 & SRM 51-42-21.Nov 1, 2010 · N868AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001712Angle · crackedFS 559.0, LBL 18 CRACK INDICATED ON CAP ANGLE. COMPLIED WITH EC/TC REO 601R-53-41-260 AND REO 601R-53-41-260 REV E.Nov 1, 2010 · N886AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040952Skin · gougedTOP OF RT FLIGHT SPOILER AT CTR T/E IS GOUGED. REPAIRED RT FLIGHT SPOILER UPPER SKIN BETWEEN SPOILER STA 195.3603 AND SPOILER STA 204.3603 IAW REO 601R-57-73-133.Nov 1, 2010 · N448AW · Cndair CL6002B19 · SpoilersSDR REXA201000235Engine · shutdownUPON LANDING AT KORF, THE LT ENGINE SHUTDOWN FOR NO APPARENT REASON. THE FLIGHT CREW REPORTED THAT THE THRUST LEVER WAS ABOVE THE IDLE GATE AT ALL TIMES AND THAT THE OCCURRENCE HAPPENED ALMOST SIMULTANEOUS WITH THE TOUCHDOWN OF THE MAIN WHEELS ONTO THE RUNWAYOct 31, 2010 · N8623A · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA201001694Bleed Air Sys · odorON APPROACH, HAD A BURNING ODOR IN FRONT OF ACFT. SWAPED BLEEDS TO APU ODOR WAS DIMINISHED IMMEDIATELY. C/W OPS CHECK OF BOTH ENGINES IAW AMM 71-00-00. OPS CK GOOD. NO DEFECTS NOTED. (CLOSED)Oct 31, 2010 · N972EV · Cndair CL6002B19 · Engine Bleed Air SystemSDR CA101102008Skin · dented(CAN) DURING OVERNIGHT AT MAINTENANCE BASE, NOTICE DAMAGE TO RT WING LEADING EDGE AT WS380 CAUSED BY BIRD STRIKE. SUSPECT THAT HAPPEN ON LAST FLIGHT OF THE DAY. AFTER FURTHER INSPECTION FOUND DENTED BEYOND LIMITS, DEFECT 947790 RAISED. TEMPORARY REPAIR C/OUOct 31, 2010 · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA201040953Skin · crackedAFT PAX DOOR AIRSTAIR SKIN CRACKED UNDER STEP 832DT. REPAIRED AFT SKIN UNDER STEP 832DT IAW REO 601R-52-11-702, REV C.Oct 29, 2010 · N448AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040943Track · chafedRT THRUST REVERSER UPPER PYLON TRACK CHAFED. BLENDED OUT CHAFE AREA TO SMOOTH CONTOUR IAW SRM 51-12-00, NOT EXCEDING REPORTED DEPTH EDDY CURRENT INSPECTED, RESTORED FINISH IAW CMM 20-21-11.Oct 29, 2010 · N448AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201040944Fitting · chafedLT OTBD FLAP INBD ROLLER FITTING BENEATH ROLLER IS CHAFED. BLENDED OUT DAMAGE TO A SMOOTH CONTOUR IAW SRM 51-12-00, EDDY CURRENT INSPECTED IAW 51-20-06 SHOT PEEN IAW SRM 51-24-11. RESTORED PROCTINO FINISH IAW SRM 51-21-16.Oct 29, 2010 · N448AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040951Fitting · chafedRT OTBD FLAP INBD ROLLER FITTING BENEATH ROLLER CHAFED. BLENDED OUT CHAFED AREA IAW SRM 51-12-00, EDDY CURRENT INSPECT IAW NDTM 51-20-06, ROTOPEEN IAW SRM 51-24-11.Oct 29, 2010 · N448AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040949Fitting · chafedRT OTBD FLAP INBD ROLLER GUIDE FITTING CHAFED. BLENDED OUT DAMAGE IAW SRM 51-12-00, EDDY CURRENT INSPECTION IAW NDTM 51-20-06. ROTO PEEN REWORKED AREA SRM 51-24-11.Oct 29, 2010 · N448AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040948Rib · crackedLT WING BATT RIB IS CRACKED. REPAIRED LT WING BATT RIB AT WS 53.60 IAW REO 601R-57-51-046, REV B, REPAIR NR 2.Oct 28, 2010 · N448AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR MALA100161Acm · odorDURING SHORT FINAL F/A AND CREW NOTICED A BURNING ODOR COMING THROUGH THE ECS SYS, NO SMOKE OR HEAT DETECTED BY F/A OR CREW. ENGINE AIR WAS SOURCE FOR BLEED AIR. DEFERRED RT IAW MEL 21-51-1-1, C RAM AIR SOV VERIFIED OPERATIVE MX NOTIFIED 8483 ENTERED INTO MMO2Oct 26, 2010 · N8943A · Cndair CL6002B19 · Cabin Cooling SystemSDR CA101028002Element · shorted(CAN) SHORTLY AFTER DEPARTURE THE FLIGHT CREW RECEIVED AN ANTI-ICE DUCT WARNING MESSAGE, THE LT FUSELAGE FLOW BAR WAS RED. AS THERE WERE ICING CONDITIONS ENROUTE, THEY RETURNED TO YYZ. MTC INVESTIGATION FOUND SENSE ELEMENT A15WK CRACKED AND SHORTING TO GROUNOct 26, 2010 · Cndair CL6002B19 · Ice DetectionSDR A6WA201040950Plate · chafedRT INBD FLAP INBD OF LUG PLATE HAS CHAFE DAMAGE WS 80.50. REPAIRED IAW REO 601R-57-52-1536, TYPE I.Oct 25, 2010 · N448AW · Cndair CL6002B19 · Trailing Edge FlapsSDR ASOA201001646Handle · bindingSERVICE DOOR OUTER HANDLE WILL NOT TURN. LUBED SERVICE DOOR IAW AMM 12-50-52. OP CK GOOD, ACFT OK FOR SERVICE. (CLOSED)Oct 24, 2010 · N922EV · Cndair CL6002B19 · Service DoorsSDR A6WA201040798Angle · crackedFOUND INBD CAP ANGLE AY FS559 & RBL 9 CRACKED. REPAIRED CRACKED CAP ANGLE AT FS 559 & RBL 9 BY FULL INCORPORATION OF REO 601R-53-41-260, REV E. INCLUDING DEVIATION REO 601R-53-41-609, REV B DEVIATION E TO THE FS 559 PRESSURE BULKHEAD LT & RT SIDES FROM LBL 27Oct 23, 2010 · N453AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001638Unknown · odorCREW REPORTS AFTER TAKEOFF THEY RECIEVED SMOKE TOILET MESSAGE AND REPORTS OF SMOKE ODOR IN CABIN AND FLIGHT DECK. ACFT PERFORMED AN AIR RETURN WITH NO OTHER PROBLEMS. SMOKE ODOR HAD DISSIPATED AFTER 10 MINUTES. ACFT RETURNED TO DEPARTURE AFTER T/O. WITH ALLOct 22, 2010 · N667BR · Cndair CL6002B19 · Air Distribution SystemSDR ASOA201001640Bracket · crackedRT ENGINE INLET COWL HAS A CRACKED BRACKET ON AFT SIDE OF BULKHEAD AT 5 O'CLOCK POSITION. C/W REO 601R-71-61-3415 REV NC.Oct 22, 2010 · N868AS · Cndair CL6002B19 · Engine Air Intake SystemSDR ASOA201001641Unknown · odorF/A SMELLED HOT RUBBER ODOR FROM AREA OF ROW 7 DURING CLIMB AND DESCENT. INSPECTED CABIN AREA NEAR ROW 7, NO DEFECTS NOTED. INSPECTED AVIONICS BAY AREA, NO DEFECTS NOTED. PERFORMED OPS CHECK OF AIR CONDITIONING SYS IAW AMM 21-50-00, NO DEFECTS NOTED. ACFT OOct 22, 2010 · N873AS · Cndair CL6002B19 · Air Distribution SystemSDR ASOA201001642Battery Pack · dischargedNR 3 AND NR 4 EMERGENCY LIGHT BATTERY PACKS NO CHARGE. R & R NR3 AND NR4 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04-000-801 (REMOVAL) AND AMM 33-51-04-400-801 (INSTALLATION) OPS TEST GOOD IAW SUB TASK 33-51-04-740-005 NO OTHER DEFECTS NOTED.Oct 22, 2010 · N980EV · Cndair CL6002B19 · Emergency LightingSDR A6WA201040796Pressure Panel · gougedRT FUSELAGE PRESSURE PANEL CUT OUT HAS TOOLING MARKS AROUND A HOLE LOCATED AT THE 3 O`CLOCK POSITION. BLENDED OUT TOOL MARKS AROUND A HOLE LOCATED AT THE 3 O`CLOCK POSITION ON RT PRESSURE PANEL (132AL) OPENING IAW REO 601R-53-11-2002.Oct 22, 2010 · N453AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040797Floorbeam · crackedINBD FLOORBEAM CLIP ON LBL 9 AT FS 280 IS CRACKED. R & R PN 601R31113-57 AT OTBD LBL FS 280 IAW SRM 51-42-21.Oct 22, 2010 · N453AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001636Flashlight · brokenF/O'S FLASHLIGHT BROKEN. R & R FLASHLIGHT IAW AMM 25-60-01. (CLOSED)Oct 21, 2010 · N930EV · Cndair CL6002B19 · Emergency EquipmentSDR ASOA201001637Light · inoperativeTHE WARDROBE FLOOR LEVEL EMERGENCY FLOODLIGHT IS INOP. REMOVED THE WARDROBE FLOOR LEVEL EMERGENCY FLOOD LIGHT IAW AMM 33-51-19-000-801. THE WARDROBE FLOOR LEVEL EMER FLOOD LIGHT REINSTALLATION AND EMERGENCY LIGHT OPS CHECK IS DUE. INSTALLED A NEW FLOOR LEVELOct 21, 2010 · N905EV · Cndair CL6002B19 · Emergency LightingSDR A6WA201040792Angle · crackedLT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED UNSERVICEABLE OBLIQUE ANGLE FROM LT FS 625 AND INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-21 AND REO 601R-53-61-985.Oct 20, 2010 · N453AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040793Skin · chafedSKIN ON FUSELAGE AT RT STUB FAIRING IS CHAFED. REPAIRED DAMAGE AREA IAW REO 601R-53-41-341, REV C.Oct 20, 2010 · N453AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR CA101026005Control Unit · failed(CAN) DURING A 100 HR IN-HANGAR INSPECTION, THE AIRCRAFT PITCH TRIM OPS CHECK FAILED, AS FOLLOWS: WITH BOTH CHANNELS ENGAGED, STAB TRIM EICAS INDICATION DOES NOT AGREE WITH ACTUAL STABILIZER POSITION. EICAS INDICATION OF 3.0 WITH STAB AT FULL DEFLECTION, EICOct 20, 2010 · Cndair CL6002B19 · Stabilizer Control SystemSDR ASOA201001631Seat Track · corrodedNR 1 AND 2 LT SEAT TRACKS ARE CORRODED. REMOVED CORRODED SEAT TRACKS AND INSTALLED DUPLICATED TRACKS IAW AMM 53-01-11, SRM 51-25-06, 51-25-16, 51-21-11, 51-40-11.Oct 19, 2010 · N971EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001632Seat Track · corrodedNR 1 AND 2 RT SEAT TRACKS ARE CORRODED. REMOVED SEAT TRACK, LOCATED DRILLED AND COUNTERSUNK NEW SEAT TRACK, TORQUED SCREWS IAW AMM 53-01-11.Oct 19, 2010 · N971EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201040794Skin · chafedENTIRE TOP SIDE OF LT AILERON L/E IS CHAFED. REPAIRED THE CHAFED ON ENTIRE TOP SIDE OF LT AILERON L/E IAW MFG 601R-57-60-013 REV NC.Oct 19, 2010 · N453AW · Cndair CL6002B19 · AileronsSDR ASOA201001614Wire · damagedRT EMERGENCY EXIT SIGN AT ROW 8CD INOP. REPAIRED DEFECTIVE SPLICE ON RT EMERGENCY EXIT SIGN FIXTURE AT ROW 8CD IAW ESPM 20-17-10, OPS CHECK GOOD. REPAIRED DEFECTIVE SPLICE ON RT EMERGENCY EXIT SIGN FIXTURE AT ROW 8CD IAW ESPM 20-17-10, OPS CHECK GOOD. (CLOSEOct 18, 2010 · N872AS · Cndair CL6002B19 · Light System Wiring
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