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 ASOA201000521Angle · crackedLT & RT FS 621.00 TO 625.00 ANGLES AT STRINGERS 15L AND 15R ARE CRACKED 1" LONG IN FWD RADIUS. REMOVED & DRILLED NEW SERVICEABLE 625.00 ANGLES FOR LT & RT AND INSTALLED NEW SRM 51-42-21.Apr 5, 2010 · N919EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000522Lens · crackedEXIT LENS IS CRACKED. (RESOLVED ON W/O: 154347 TASKCARD: N/R-00331 ) REMOVED CRACKED EXIT LENS FROM PNL 232DZ IAW AMM TASK 33-51-13-000-801, SUBTASK 33-51-13-020-801 STEP 3A(1). INSTALLED NEW EXIT LENS TO PNL 232DZ IAW AMM TASK 33-51-13-400-801, SUBTASK 33-5Apr 5, 2010 · N919EV · Cndair CL6002B19 · Emergency LightingSDR SWIA201023965Turbine Case · crackedRIGHT ENGINE LPT CASE CRACKED BEYOND LIMITS. (SERVICE CK) ENGINE CHANGED.Apr 3, 2010 · N956SW · Cndair CL6002B19 · Turbine SectionSDR SWIA201023966Mount · corrodedRIGHT ENGINE MOUNT ASSEMBLY PITTED. (ENGINE CHG) REPLACED ENGINE MOUNT PER AMM.Apr 3, 2010 · N956SW · Cndair CL6002B19 · Engine Mount SectionSDR A6WA201040278Switch · malfunctionedR & R REV UNLOCK MESSAGE CLIMBING THROUGH 15,000 FT, COMPLIED WITH QRH. REF LOG: 202457/2 - REPLACED RT T/R STOW SWITCH IAW AMM 78-37-01. OPS CHECKS AT THIS TIME. REMOVED PLACARD, REMOVED FROM MEL.Apr 3, 2010 · N439AW · Cndair CL6002B19 · Engine Thrust ReverserSDR ASOA201000485Control Unit · defectiveFLIGHT SPOILERS & SPOILERONS MSG ON DOWNWIND. COMPLIED WITH QRH. OBSERVED SPOILERS DEPLOY GREEN ADVISORY MSG ON TOUCHDOWN. OTHER MSG'S CLEARED AFTER TOUCHDOWN (EMERGENCY DECLARED). R & R NR 1 SPOILER ELECTRONIC CONTROL UNIT, OPS TEST GOOD REF IAW AMM 27-61-Apr 2, 2010 · N932EV · Cndair CL6002B19 · Drag Control SystemSDR ASOA201000473Light · inoperativeRT WING EMERGENCY EXIT (2) LIGHTS INOP FWD OF OVERWING EXIT. REPLACED BULBS (2) CK OK IAW AMM 53-12-10.Apr 1, 2010 · N447CA · Cndair CL6002B19 · Emergency LightingSDR ASOA201000474Light · no testEMERGENCY LIGHTS FAILED OP'S CHECK. WW 161790 03/31/10. FOUND BROKEN WIRE LY15A22 TO FLOOR PROX EXIT SIGN LT OVERWING SPLICED IAW ESPM 20-16-10. FOUND NR 2 BATTERY PACK BAD ORDERED PART PN 2013-1A NR 2 BATTERY PACK NEEDS REPLACED. R & R NR 2 BATTERY PACK IAApr 1, 2010 · N916EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201000480Attach Fitting · crackedBS 280 FRAME CLIP AT RBL9 IS CRACKED. REMOVED CRACKED FRAME CLIP & REPLACED WITH NEW AT STA 280, RBL 9, IAW SRM 53-21-43.Apr 1, 2010 · N972EV · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201000491Frame · crackedSTA 718 BETWEEN STR 10 AND 11 RT, FRAME FLANGE IS CRACKED. REPAIR TO BE C/W ON CARD S/B 601R-53-055.Apr 1, 2010 · N972EV · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201000514Floor Support · corrodedNR 1 FLOOR TRACK IN AFT CARGO AREA HAS SPOTS OF CORROSION. R & R NR 1 FLOOR TRACK CORRODED SECTION IAW AMM 53-01-11. (SDR CLOSED)Apr 1, 2010 · N972EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000515Cargo Track · corrodedNR 1 FLOOR TRACK PUCS IN AFT CARGO AREA HAS SPOTS OF CORROSION. R & R PUCKS IAW SRM 51-40-00.Apr 1, 2010 · N972EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000516Cargo Track · corrodedNR 2 FLOOR TRACK IN AFT CARGO AREA HAS SPOTS OF CORROSION. R & R CORRODED SECTIONS OF NR 2 CARGO FLOOR TRACK IAW AMM 53-01-11. (CLOSED)Apr 1, 2010 · N972EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000517Cargo Track · corrodedNR 2 FLOOR TRACK PUCS IN AFT CARGO AREA HAS SPOTS OF CORROSION. R & R BULKHEAD ATTACH FITTING IAW AMM 53-01-11.Apr 1, 2010 · N972EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000519Cargo Track · corrodedNR 4 FLOOR TRACK IN AFT CARGO AREA HAS SPOTS OF CORROSION. R & R NR 4 FLOOR TRACK CORRODED SECTION IAW AMM 53-01-11. (CLOSED)Apr 1, 2010 · N972EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000461Lens · crackedEMERGENCY EXIT LENS COVER ON LT WINDSCREEN IS CRACKED. REMOVED CRACKED EXIT LENS COVER FROM LT WINDSCREEN. INSTALLED NEW EXIT LENS COVER ON LT WINDSCREEN IAW AMM 33-51-13-400-801 STEP 3A (4).Mar 31, 2010 · N917EV · Cndair CL6002B19 · Emergency LightingSDR A6WA201040330Panel · damagedFUEL PANEL 640BB HAS GRINDING MARKS IN THE RED SEAL AREA. REPAIRED FUEL PANEL 640BB IAW REO 601R-52-21-1263.Mar 31, 2010 · N403AW · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA201000459Battery Pack · inoperativeBOTH RT AND LT AFT EXTERIOR EMERGENCY LIGHTS INOP. R & R THE NR 4 BATTERY PACK (EMERGENCY LIGHT) REF: AMM TASK 33-51-04-000-801 AND TASK 33-51 04 400-801 OPS CHECKED GOOD.Mar 30, 2010 · N858AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201000444Door · lack of lubeSERVICE DOOR COULD NOT BE OPENED FROM OUTSIDE HANDLE, JAMS HALF-WAY THROUGH TRAVEL. LUBED OUTER HANDLE IAW AMM 52-40-01. OPS GOOD.Mar 27, 2010 · N839AS · Cndair CL6002B19 · Service DoorsSDR ASOA201000435Floorbeam · cracked(3 EA) FLOOR SUPPORT CLIPS CRACKED AT FS 280 2 ON LT SIDE AND 1 ON RT SIDE COCKPIT ENTRY WAY. REMOVED CRACKED CLIPS AND INSTALLED NEW SERVICEABLE CLIP IAW SRM 51-42-21 AND 51-21-16.Mar 26, 2010 · N916EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR MASA2010032500235Probe · contaminatedNR 1 ENGINE N2 ZERO ON TAKEOFF. FOUND OIL CONTAMINATION IN PROBE, CONNECTOR CLEANED AND OPS GOOD.Mar 25, 2010 · N7305V · Cndair CL6002B19 · Turbine Engine Air Inlet SectionSDR ASOA201000427Frame · corrodedFRAME CORRODED AT FS 319 STG-26R FWD SIDE. UPON FURTHER INVESTIGATION FOUND FRAME AT FS 319, STA 26R FWD SIDE TO BE OUT OF LIMITS WITH .008 MATERIAL LOSS BEFORE CORROSION WAS REMOVED IAW SRM 51-21-15 AND 53-00-00. FRAME AT FS 319, STR 26R, REQUIRES REPLACEMEMar 25, 2010 · N825AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201000428Frame · corrodedFRAME CORRODED AT FS 364 STG 26R FWD SIDE. REMOVED CORROSION FROM FRAME FS 364, STR 26R ON FWD SIDE IAW SRM 51-21-06. REMOVING ONE BOLT TO ACCESS CORROSION IAW SRM 51-41-02 AND FOUND TO BE WITHIN LIMITS WITH OEM 0.080 AND MATERIAL LOSS TO BE 0.006 IAW SRM 53Mar 25, 2010 · N825AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201000430Post · crackedFOUND FS 409+128 VERTICAL POST RBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .3" IN LENGTH 80 PERCENT FSH AT WL 64.0 AFT FLANGE RADIUS. FAILED NDT INSPECTION. LOOSENED HYD LIEN ADEL CLAMPS AT 6 LOCATIONS, ADJACENT TO FS 409+128 RBL 18 POST FOR ACCESS IAW SRMar 25, 2010 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000431Post · crackedFOUND FS 409+128 VERTICAL POST LBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT WL 64.0 AFT FLANGE RADIUS. FAILED NDT INSPECTION. DISCONNECTED A/C CABIN AIR DUCT. REMOVED INBD AND OTBD POST. LOCATED & DRILLED OTBD POST IAW SRM Mar 25, 2010 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000448Finger Doubler · corrodedMAIN CABIN BETWEEN FS 409+128 AND FS 559.00 PRESSURE FLOOR SILL AND FINGER DOUBLER HAVE CORROSION IN NUMEROUS AREAS ON LT SIDE. (OPEN)Mar 25, 2010 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000450Floorbeam · crackedJOB 8720721, OPERATION 374 / FS 280 FLOOR SUPOORT ANGLE AT LBL 9 OTBD UNDER ALTERNET EXTENSION PULLEY BRACKET CRACKED TOP AND BOTTOM. (OPEN)Mar 25, 2010 · N825AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201024008Case · crackedLEFT ENGINE LPT CASE CRACKED AT 3 O'CLOCK POSITION, OUT OF LIMITS. (C CHECK) REPLACED ENGINE.Mar 25, 2010 · N961SW · Cndair CL6002B19 · Turbine SectionSDR ASOA201000423Light · inoperativeMIDDLE LEFT EXTERIOR EMERGENCY LIGHT INOP. R & R MIDDLE LT EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS GOOD.Mar 24, 2010 · N876AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201000424Bulkhead · crackedREAR PRESSURE BULKHEAD IS CRACKED AT LINTEL FITTING. ACCOMPLISHED LINTEL FITTING/ AFT PRESSURE BULKHEAD REPAIR IAW PL601R-53-61-1230, C/W RII OF REAR PRESSURE BULKHEAD LINTEL FITTING.Mar 24, 2010 · N972EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201023887Yoke · corrodedLEFT ENGINE FORWARD MOUNT YOKE LINK ASSEMBLY WORN AND CORRODED. (ENG CHANGE) REPLACED PER AMM.Mar 23, 2010 · N915SW · Cndair CL6002B19 · Engine Mount SectionSDR ASOA201000420Door · out of adjustRIGHT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST. ADJUSTED RT OVERWING EMERGENCY EXIT IAW AMM 52-21-00-820-801. RT OVERWING EMER EXIT FUNCTIONAL TEST GOOD IAW AMM 52-21-00-720-801. STESP 4A(4-6) ON AMM 52-21-00-720-801. PRESSURIZED ACFT IAW MM 21-32-00-86Mar 23, 2010 · N825AS · Cndair CL6002B19 · Emergency ExitsSDR ASOA201000421Door · no testLEFT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST & IS CONTACTING UPPER LATCH PIN FITTING. ADJUSTED LT OVERWING EMER EXIT IAW AMM 52-21-00-820-801. LT OVERWING EMERGENCY EXIT FUNCTIONAL TEST GOOD IAW AMM 52-21-00-720-801. PRESSURIZED ACFT IAW MM 21-32-00-Mar 23, 2010 · N825AS · Cndair CL6002B19 · Emergency ExitsSDR ASOA201000426Proximity Sensor · malfunctionedON DEPARTURE GEAR UP DISAGREE WARNING. NOSE DOOR OPEN MSG RAN QRH GEAR DOWN & LOCKED RESULTED. GEAR PINNED AT THE GATE ALL 3 IAW MX REQUEST. (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED) ADJUSTED NLG CENTERED EXTENDED PROXIMITY SENSOR IAW AMar 23, 2010 · N977EV · Cndair CL6002B19 · Landing Gear Position and WarningSDR ASOA201000439A/C Pack · odorAT LOWER ALTITUDES, PACKS PRODUCE MOLDY ODOR MAKING IT DIFFICULT TO BREATH. THIS OCCURS AT HIGHER POWER SETTINGS. PERFORMED OPEATIONAL CHECK OF LEFT & RIGHT PACKS AT LOW & HIGH TEMPS. ALL CHECKS NORMAL. NO DEFECTS NOTED AT THIS TIME, IAW AMM 21-51-00.Mar 23, 2010 · N884AS · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA201040235Lug · gougedRT T/R LOWER INBD ATTACH LUGS FOR SLIDER TRACK ARE GOUGED 0.055" DEEP. R & R RT TR LOWER INBD ATTACH LUG FOR SLIDER TRACK.Mar 23, 2010 · N439AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201040234Track · gougedRT THRUST REVERSER LOWER INBD SLIDE TRACK IS GOUGED ON AFT ATTACH LUG, R&R RT THRUST REVERSER LOWER INBD SLIDER TRACK IAW SHORTS CMM 78-34-11.Mar 23, 2010 · N439AW · Cndair CL6002B19 · Engine Thrust ReverserSDR REXA201000049Bearing · crackedDURING ENGINE REMOVAL FOR 18K LLP SHOP VISIT, MAINTENANCE DISCOVERED WHAT APPEARED TO BE A CRACK IN A FORWARD ENGINE MOUNT YOKE BEARING. THE MOUNT YOKE WAS REMOVED FROM SERVICE AND SENT OUT FOR REPAIR. THE REPAIR VENDOR CONFIRMED THE BEARING RACE TO BE CRACKMar 23, 2010 · N8412F · Cndair CL6002B19 · Engine Mount SectionSDR ASOA201000414Bulkhead · crackedBS 202.75 PRESSURE BULKHEAD CRACKED AT BRAKE CABLE FEED THROUGH HOLE. C/W EC/TC REO 601R-53-11-563 AND REO 601R-53-11-563 REV.Mar 22, 2010 · N681BR · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201000416Intercostal · crackedUPON DISASSEMBLY OF PREVIOUSLY REWORKED EXTERNAL POWER RECEPTACLE SUPPORT MEMBER, FOUND AFT INTERCOSTAL PN 600-33283-35 TO BE CRACKED INBD TOP FASTENER HOLE. DRILLED OFF, REMOVED OLD EXTERNAL POWER RECEPTACLE SUPPORT MEMBER AFT INTERCOSTAL PART NR 600-33283-Mar 22, 2010 · N681BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000417Lamp · inoperativeNR 2 INTERIOR CEILING EMERGENCY LIGHT IS INOP. RELAMPED NR 2 INTERIOR CEILING EMERGENCY LIGHT IAW AMM 33-51-16, OP'S CHECK GOODMar 22, 2010 · N823AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201000415Bulkhead · corrodedFS 621.00, PRESSURE BULKHEAD WEB FWD FACE HAS A 90 PERCENT FSH HFEC INDICATION NOTED APPROX 0.2" LONG AT THE BOTTOM INBD CORNER OF THE LINTEL FITTING. FAILS NDT AT THIS TIME. REPAIR PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETE AND THE REPAIR C/W THE REQUMar 22, 2010 · N681BR · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201000495Placard · missingEXIT PLACARD MISSING ON PAX AIRSTAIR DOOR. INSTALLED PLACARD IAW AMM 11-30-02.Mar 22, 2010 · N971EV · Cndair CL6002B19 · Placards and MarkingsSDR VNAA2010032500011Engine · vibrationCREW REPORTED VIBRATION FROM RIGHT ENGINE ON CLIMBOUT FROM CLT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED CHECKS AND GROUND RAN THE ENGINE USING THE AIRCRAFT MAINTENANCE MANUALS. VIBRATION READINGS WERE WITHIN LIMITS. AIRCMar 21, 2010 · N209PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA201000425Seat Track · corrodedLAV WALL SEAT TRACK FITTINGS ARE CORRODED. R & R SERVICEABLE SEAT TRACK FITTINGS IAW AMM TASK 25-52-01-000-802.Mar 19, 2010 · N916EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201040331Rib · crackedRT BATT RIB CRACKED IN RT WHEEL WELL. REPAIRED IAW REO 601R-57-51-046.Mar 19, 2010 · N403AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR ASOA201000400AController · uncontrollableR & R NR 2 CABIN PRESS CONTROLLER IAW AMM 21-31-16. (CLOSED)Mar 18, 2010 · N681BR · Cndair CL6002B19 · Cabin Pressure ControllerSDR A6WA201040228Sense Line · brokenRT ENGINE OIL PRESSURE MESSAGE INFLIGHT, ENG SHUTDOWN BY CREW AND COMPLIED WITH QRH. FOUND P3 SENSE LINE BROKEN, R & R P3 LINE IAW AMM 75-30, PERFORMED POWER ASSURANCE RUNS, NO DEFECTS NOTED, THROTTLE RESPONSE NORMAL.Mar 17, 2010 · N442AW · Cndair CL6002B19 · Engine Oil Indicating SystemSDR ASOA201000397Support Beam · crackedFOUND CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IS CRACKED APPROX .4" IN LENGTH. R & R CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IAW SRM 51-42-21.Mar 16, 2010 · N917EV · Cndair CL6002B19 · Fuselage Main, StructureSDR MASA2010031500210Fcu · faultyATO / RTG NR 1 ENG WOULD NOT MAKE T/O POWER. REPLACED THE FCU.Mar 15, 2010 · N77260 · Cndair CL6002B19 · Fuel Control/Turbine Engines
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