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 ASOA201000603Seat Track · corrodedSEAT RAILS BETWEEN FS 559.00+110 AND FS 568.00 LBL 9 AND RBL 9 ARE CORRODED. R & R SEAT RAILS BETWEEN FS 559.00+110 & FS 568.00 LBL 9 AND RBL 9 IAW AMM 53-01-11-000-802. PROCEDURE SUBTASK 53-01-11-020-002 B1-3 & 53-01-11-420--001 B1-8. AMM 53-01-110-400-802.Apr 20, 2010 · N859AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000604Seat Track · corrodedSEAT RAILS BETWEEN FS 559.00+80 AND RBL 27 ARE CORRODED. R & R SEAT RAILS IAW AMM 53-01-11-000-802 SUBTASK PROC 53-10-11-020-002 B1-3 & 53-01-11-420-001 B1-8.Apr 20, 2010 · N859AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000605Lamp · inoperativeLT EXTERIOR NR 2 EMERGENCY LIGHT INOP. (RESOLVED ON W/O: 154976 TASKCARD: N/R-00002 ) RELAMPED LT EXTERIOR NR 2 EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD. RELAMPED LT EXTERIOR NR 2 EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD. (CLOSED)Apr 20, 2010 · N908EV · Cndair CL6002B19 · Emergency LightingSDR MASA2010041900367Oil System · overservicedLEFT ENGINE HIGH OIL TEMP IN FLIGHT. ENGINE SHUT DOWN. FOUND OIL OVER SERVICED.Apr 19, 2010 · N17358 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR ASOA201000590Bulkhead · crackedCRACK INDICATION FOUND AT AFT PRESSURE BULKHEAD LOCATED AT THE TOP OF THE LINTEL ATTACH POINT. AREA IS MARKED. REPAIRED IAW EC/TC REO 601R53-61-1230.Apr 19, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201000591Bulkhead · crackedCRACK INDICATION FOUND ON AFT PRESSURE BULKHEAD LOCATED AT THE TOP OF THE AFT CARGO DOOR TRACK. AREA IS MARKED. PERFORMED CUT OUT ON AFT PRESSURE BULKHEAD AND FABRICATED FILLER AND DOUBLES IAW REO 601R-53-61-1541. NDT REQUIRED OF CUT LINE. PERFORMED ET INSApr 19, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201000592Bracket · crackedBRACKET CRACKED AT FS 469.63 BELOW RT WING EMERGENCY EXIT THAT THE FUSELAGE OVERWING PANEL 162EL ATTACHES TO RT 161728. REMOVED CRACKED ANGLE IAW SRM 51-42-06. INSTALLED NEW ANGLE ALL WORK DONE IAW SRM 51-42-06 AND SRM 51-42-21.Apr 19, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201000593Bracket · crackedBRACKET CRACKED AT FS 449.85 BELOW RT WING EMERGENCY EXIT THAT THE FUSELAGE OVERWING PANEL 162DL ATTACHES TO RJ161728. REMOVED CRACKED ANGLE IAW SRM 51-42-06. INSTALLED NEW ANGLE IAW SRM 51-42-06 AND SRM 51-42-21.Apr 19, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201000594Bracket · crackedBRACKET CRACKED AT FS 449.85 BELOW LT WING EMERGENCY EXIT THAT THE FUSELAGE OVER WING PANEL 161DL ATTACHES TO RT 161728. (RESOLVED ON W/O: 155601 TASKCARD: N/R-00369 ) JOB 8732425 /OPERATION 186/ BRACKET CRACKED AT FS 449.85 BELOW LT WING EMERGENCY EXIT THAT TApr 19, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201000595Bracket · crackedBRACKET CRACKED AT FS469.63 BELOW LT WING ENERGENCY EXIT THAT THE FUSELAGE OVERWING PANEL 161DL ATTACHES TO RT 161728. (RESOLVED ON W/O: 155601 TASKCARD: N/R-00370 ) JOB 8732425 /OPERATION / REMOVED CRACKED ANGLE AT FS 469.93 JUST BELOW LT WING EMERGENCY EXIApr 19, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201000597Stringer · corrodedCORROSION FOUND ON STR 26R 3" AFT OF FS 333. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. STARTED SPLICE REPAIR FOR STRG 26R IAW SRM 53-00-03. PERFORMED ET INSPECTION OF CUT LINES IAW SRM 53-00-03 PARA.4.(5) IAW NDTM PART 1, 51-20-06. NO INDICATIONS NOTED. CApr 19, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR ASOA201000598Bracket · crackedCARGO DOOR SUPPORT BEAM HAS CRACKED BRACKET WHERE IT MAKE TO 621.00 BULKHEAD. (LT 04/18/10) (RESOLVED ON W/O: 155601 TASKCARD: N/R-00390 ) JOB 8732425 /OPERATION 207/ REMOVED CRACKED BRACKET FOR CARGO DOOR SUPPORT BEAM AT FS 621.00 BULKHEAD IAW SRM 51-42-21. Apr 19, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201000596Skin · corrodedCORROSION FOUND ON SKIN SPLICE AT FS 333 BETWEEN STR 27 AND 26. REPAIRED IAW REO 601R-53-21-1125.Apr 19, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA201000635Water Heater · contaminatedFA REPORTS CHEMICAL ODOR/ TASTE FROM POTABLE WATER. ALSO REPORTED BY PASSENGERS. DRAINED FWD POTABLE WATER AND SERVICED IAW AMM 12-18-38. (SDR CLOSED)Apr 18, 2010 · N980EV · Cndair CL6002B19 · Potable Water SystemSDR SWIA201024102Liner · missingFOUND RIGHT ENGINE CONTAINMENT CASE LINING MISSING. (FLT 1054) REPLACED CONTAINMENT CASE.Apr 13, 2010 · N961SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA2010041600008Screen · obstructedCREW REPORTED LEFT ENGINE OIL TEMPERATURE HIGH AND OIL PRESSURE LOW ON CLIMBOUT FROM CAK EN ROUTE TO CLT. AIRCRAFT DIVERTED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, CLEANED DEBRIS FROM THE LEFT ENGINE LUBE AND SCAVENGE PUMP SApr 12, 2010 · N230PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA2010041600007Carbon Seal · damagedCREW REPORTED A LEFT ENGINE OIL PRESSURE WARNING IN FLIGHT EN ROUTE FROM CLT TO CAK. AIRCRAFT LANDED IN CAK WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LEFT ENGINE’S CARBON SEALS FOR THE INTEGRATED DRIVE GENERATOR (IDG),Apr 11, 2010 · N230PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR ASOA201000534Battery · inoperativeC/A & F/O FLASHILGHT INOP. REPLACED BATTERIES CA/FO FLASHLIGHTS IAW AMM 25-60-00. (CLOSED)Apr 10, 2010 · N682BR · Cndair CL6002B19 · Emergency EquipmentSDR ASOA201000535Light · inoperativeAFT CEILING EMERGENCY LIGHT OUT. (RESOLVED ON W/O: 155136 TASKCARD: N/R-00049) R & R AFT CEILING EMERGENCY LIGHT IAW AMM 33-51-16-400-801. OPS TEST OF EMERGENCY LIGHTS GOOD IAW AMM 33-51-00-710-801. (CLOSED)Apr 10, 2010 · N971EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201000526Support Angle · crackedRT BATT RIB IS CRACKED AT WS 53.60. REMOVED BATT RIB SUPPORT ANGLE, COVER PANEL AND CONNECTORS J410 & J412 IAW SRM 51-41-02. REO REPAIR FOR BATT RIB NEEDS ACCOMPLISHED. COMPLIED WITH ASA REO NR 601R-57-51-046 REPAIR NR 2. REINSTALLED SUPPORT ANGLE AND COVERApr 9, 2010 · N920EV · Cndair CL6002B19 · Wing, Rib/BulkheadSDR ASOA201000527Seat Track · corrodedSEAT TRACK CORRODED CARGO COMPARTMENT FS 570 LBL 9. REMOVED 12 EA SCREWS W/EZ OUT. REMOVED OLD RTV AND PROTECTIVE FILM. CLEANED FLOORBEAM AND REAPPLIED MYLAR FILM. SKIM COATED MYLAR W/RTV 157 AND INSTALLED SERVICEABLE SEAT TRACK RAIL AND SCREWS W/MASTINOX AApr 9, 2010 · N920EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000528Seat Track · corrodedSEAT TRACK CORRODED IN CARGO COMPARTMENT FS 570, RBL 9. REMOVED 11 EA SCREWS W/EZ OUT. REMOVED OLD RTV AND PROTECTIVE FILM. CLEANED FLOORBEAM, REAPPLIED MYLAR FILM TO BEAM. SKIM COATED MYLAR FILM W/RTV 157 AND INSTALLED SERVICEABLE SEAT TRACK RAIL AND SCREWApr 9, 2010 · N920EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000530Floor Support · crackedFS 460, RBL 9 OTBD SIDE FLOOR SUPPORT CRACKED. REMOVED DAMAGED SUPPORT FITTING AT FS 460 RBL 9 OTBD SIDE AND REPLACED W/NEW SERVICEABLE FITTING IAW SRM 51-40-11, 51-42-06 AND 51-42-21.Apr 9, 2010 · N920EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040281Thrust Reverser · malfunctionedRT REV UNLOCK CAUTION MSG IN FLT. AFTER T/R`S HAD BEEN SELECTED OFF. RT THRUST REVERSER REMOVED ALONG WITH RT ENGINE CHANGE NEW THRUST REVERSER OP CHECKS GOOD AT THIS TIME.Apr 9, 2010 · N439AW · Cndair CL6002B19 · Engine Thrust ReverserSDR ASOA201000511Oxygen Bottle · lowUSED PORTABLE O2 BOTTLE TO BELOW LIMITS, 2ND BOTTLE WOULD NOT WORK. SERVICED BOTH PORTABLE O2 BOTTLES IAW CMM 35-31-01. OK FOR SERVICE.Apr 8, 2010 · N867AS · Cndair CL6002B19 · Portable Oxygen SystemSDR ASOA201000512Attach Angle · crackedAT FS 280.0, WL 72.0, RBL 9 ATTACH ANGLE CRACKED IN RADIUS (OTBD ANGLE). INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-21 AND 51-40-11. REMOVED ANGLE IAW SRM 51-42-21.Apr 8, 2010 · N919EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201000513Intercostal · crackedFS 621 TO FS 625 INTERCOSTAL CRACKED LT & RT SIDE. REMOVED INTERCOSTALS RT & LT FS 621 TO FS 625 IAW SRM 51-42-21. LT & RT INTERCOSTALS REQUIRE NEW PARTS TO INSTALL. INSTALLED INTERCOSTALS RT & LT FS 621 TO FS 625 IAW SRM 51-42-06. REQUIRE PAINT TOUCH UP. PApr 8, 2010 · N920EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000498Lamp · burned outSERVICE DOOR FLOOR EMERGENCY EXIT SIGN HAS SEVERAL LAMPS INOP. RELAMPED G1 FLOOR LEVEL EMERGENCY EXIT SIGN FLOODLIGHT. OPS CHECK GOOD. RELAMPED G1 FLOOR LEVEL EMERGENCY EXIT SIGN FLOODLIGHT. OPS CHECK GOOD.Apr 7, 2010 · N924EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201000499Lamp · burned outAFT CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED AFT CEILING EMERGENCY FLOOD LIGHT LAMP IAW AMM 33-51-16. OPS CK GOOD. RELAMPED AFT CEILING EMERGENCY FLOOD LIGHT LAMP IAW AMM 33-51-16. OPS CHK GOOD.Apr 7, 2010 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201000501Placard · deteriorated(CREW ESCAPE HATCH) EMERGENCY EXIT PLACARD IS DETERIORATED. APPLIED EMERGENCY EXIT SILKSCREEN ON 831 IAW MM 11-10-03-400-801.Apr 7, 2010 · N842AS · Cndair CL6002B19 · Placards and MarkingsSDR ASOA201000502Light · brokenLEFT EXIT LIGHT ASSY IS BROKEN. R & R LT EXIT LIGHT ASSY ON WINDSCREEN IAW MM 33-51-13-000-801 AND 33-51-13-400-801. OPS TEST DUE. OPS TEST OF THE LT WINDSCREEN EMERGENCY EXIT LIGHT IS GOOD IAW AMM 33-51-00-710-810.Apr 7, 2010 · N842AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201000503Floor Support · crackedCRACK IN CARGO FLOOR SUPPORT STRUCTURE AT FS 621 RT SIDE WL 73.50. COMPLIED TO PERMANENT REPAIR TO CARGO FLOOR SUPPORT STRUCTURE AT FS 621, RBL 28 TO RBL 40.5, WL 73.5 IAW REO 601R-53-61-117. EC/TC NOT REQUIRED. COMPLIANCE ALREADY TAKEN IN TRAX IAW AS ENGINApr 7, 2010 · N919EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000504Seat Track · corrodedCARGO COMPARTMENT FLOOR SEAT TRACK CORRODED AT FS 570 RBL 9. REMOVED CARGO COMPARTMENT FLOOR SEAT TRACK IAW SRM 51-41-04. SEAT TRACK NEEDS DRILLING & INSTALLATION. DRILLED, COUNTERSUNK AND INSTALLED SEAT TRACK AT FS 570 RBL 9 IAW SRM 51-41-00.Apr 7, 2010 · N919EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000505Seat Track · corrodedCARGO COMPARTMENT SEAT TRACK CORRODED AT FS 570 LBL 9. REMOVED CARGO COMPARTMENT FLOOR SEAT TRACK IAW SRM 51-41-04. SEAT TRACK NEEDS DRILLING & INSTALLATION. DRILLED, COUNTERSUNK AND INSTALLED SEAT TRACK AT FS 570 LBL 9 IAW SRM 51-41-00.Apr 7, 2010 · N919EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000506Seat Track · corrodedCARGO COMPARTMENT SEAT TRACK CORRODED AT FS 559+80 RBL 9. REMOVED CARGO COMPARTMENT SEAT TRACK IAW SRM 51-41-04. SEAT TRACK NEEDS DRILLING & INSTALLATION. DRILLED, COUNTERSUNK AND INSTALLED SEAT TRACK AT FS 559+80 RBL 9 IAW SRM 51-41-00.Apr 7, 2010 · N919EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000507Seat Track · corrodedCARGO COMPARTMENT SEAT TRACK CORRODED AT FS 559+80 RBL 27. REMOVED CARGO COMPARTMENT SEAT TRACK IAW SRM 51-41-04. SEAT TRACK NEEDS DRILLING & INSTALLATION. DRILLED, COUNTERSUNK AND INSTALLED SEAT TRACK AT FS 559+80, RBL 27 IAW SRM 51-41-00.Apr 7, 2010 · N919EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000508Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT TOP OF CARGO DOOR AFT TRACK LBL 27.50 WL 130 APPROX .2" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-61-1541 AND MET ALL OF THE REQUIREMENTS OF REO 601R-53-61-1541 REApr 7, 2010 · N919EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201000509Intercostal · crackedTHE CLIP AT LBL 27.0 ON THE INTERCOSTAL AT FS 484.0 HAS A .250" LONG CRACK AT THE RADIUS. REMOVED OLD BRACKET CLIP IAW SRM 51-40-11. RECEIVED NEW BRACKET CLIP & LOCATED THEN DRILLED IAW SRM 51-40-11. NEW CLIP REQUIRES INSTALLATION. REPAIR TO THE INTERCOSTAL AApr 7, 2010 · N919EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000536Pump · defectiveHYD 2 LOW PRESSURE IN FLIGHT WITH FLUID QUANITY 0 PERCENT (EMERGENCY DECLARED -- EMERGENCY PERSONNEL WERE STANDING BY) R & R EDP ON ENGINE 2 ALSO R & R THE RETURN LINE FROM THE EDP TO THE HARD LINE. OPS CHECK GOOD NO DEFECT NOTED IAW AMM 29-11-01. (CLOSED)Apr 7, 2010 · N833AS · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR A6WA201040347Skin · chafedTOP SIDE OF LT AILERON L/T IS CHAFED. REPAIRED LT AILERON UPPER L/E SKIN IAW REO 601R-57-60-013 AND REO 601R-57-60-071.Apr 7, 2010 · N440AW · Cndair CL6002B19 · AileronsSDR ASOA201000497Fairing · crackedSTANG FAIRING 444BT IS CRACKED AND FASTENER HOLES ARE ENLARGED. RECEIVED SERVICEABLE STANG FAIRING FROM STORES. LOCATED AND INSTALLED FAIRING BRACKETS IAW SRM 51-42-06. REQUIRES PAINT ON FAIRING ASSY. REF MASTER PANEL BOOK FOR INSTALLATION OF STANG FAIRING. Apr 6, 2010 · N920EV · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR VNAA2010041300002Engine · failedCREW REPORTED A LEFT ENGINE FAILURE ON CLIMBOUT FROM CLT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED THE LEFT ENGINE. MAINTENANCE ALSO REMOVED AND REPLACED DAMAGED CORE COWLS AND TRANSLATING COWLS.Apr 6, 2010 · N244PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA201000523Bulkhead · crackedFS 202.75 BULKHEAD AT PACKING BRAKE CABLE PASS THRU HAS A SUSPECTED CRACK AT THE 11 O'CLOCK POSITION. PERFORMED EDDY CURRENT INSP ON SUSPECTED AREA IAW NDTM 51-20-06. INDICATION FOUND ON UPPER SIDE OF HOLE MEASURES FULL SCREEN HEIGHT APPROX .4 LONG, FAILS NDTApr 6, 2010 · N919EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201000524Sign · crackedSERVICE DOOR INNER HANDLE "EXIT" BETA SIGN IS CRACKED. R & R SERVICE DOOR BETA LIGHT IAW AMM 33-51-09-000-802 AND 33-51-09-400-802. OPS CHECK GOOD.Apr 6, 2010 · N919EV · Cndair CL6002B19 · Emergency LightingSDR A6WA201040271Cowling · chafedLT LOWER CORE COWL CHAFED IN CTR APPROX 6 " FROM DOME. REPAIRED IAW CMM 71-12-01, REPAIR NO SRS064 & REO 601R-71-12-3976.Apr 6, 2010 · N440AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201040272Cowling · puncturedLT LOWER CORE COWL INNER SKIN PUNCTURED IN CTR REPAIRED BY CUTOUT FILLER AND DOUBLER IAW CMM 71-12-01. REPAIR SRS046 AND REO 601R-71-12-3976, REV A.Apr 6, 2010 · N440AW · Cndair CL6002B19 · Engine Cowling SystemSDR A6WA201040270Cowling · puncturedL/N LOWER CORE COWL INNER SKIN PUNCTURED AT 6" INBD OF FWD HINGE. REPAIRED LT LOWER CORE COWL INNER SKIN, 6" INBD OF FWD HINGE IAW CMM 71-12-01, REPAIR NR SRS046.Apr 6, 2010 · N440AW · Cndair CL6002B19 · Engine Cowling SystemSDR A6WA201040348Skin · chafedRT AILERON UPPER SKIN L/E CHAFED. REPAIRED CHAFE DAMAGE IAW REO 601R-57-60-013, REV NC AND REO 601R-57-60-072 REV. ORIGINAL.Apr 6, 2010 · N440AW · Cndair CL6002B19 · AileronsSDR ASOA201000493Priority Valve · failedAFTER TAKEOFF, RECEIVED A GEAR DISAGREE MSG ALONG WITH VIOLENT SHAKING IN COCKPIT THAT FELT LIKE WAKE TURBULENCE. COMPLIED W/ QRH, DECLARED AN EMERGENCY AND LANDED W/O INCIDENT.Apr 5, 2010 · N681BR · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA201000520Placard · missingCREW ESCAPE HATCH EMERG EXIT DECAL MISSING. APPLIED SILKSCREEN PRINT ON CREW ESCAPE HATCH "EMERGENCY EXIT" PLACARD IA AMM 11-10-03-400-801. (CLOSED)Apr 5, 2010 · N919EV · Cndair CL6002B19 · Placards and Markings
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