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 ASOA2012081702076Switch · illuminatedLEFT THRUST REVERSER UNLOCK MESSAGE. EMERGENCY DECLARED. R & R STOW SWITCH IAW AMM 78-37-01. OPS CHECKED GOOD.Aug 13, 2012 · N528CA · Cndair CL6002B19 · Engine Thrust ReverserSDR ASOA2012081702077Pump · malfunctionedHYD SYS 3 INDICATED 20 PERCENT, SELECTED HANDLE DOWN, RECEIVED NOSE GEAR GROUND INDICATION, THEN RECEIVED MAIN DISAGREE MSG. PERFORMED LANDING GEAR MANUAL EXT EMERGENCY DECLARED AS A PRECAUTION. R & R 3A HYD PUMP IAW AMM 29-12-03. R & R NLG SELECTOR VALVE IAug 13, 2012 · N879AS · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR A6WA201240769Lever · looseFUEL SHUTOFF LEVER ON LT THRUST LEVER IS VERY LOOSE. R & R THROTTLE QUADRANT IAW 76-11-01.Aug 13, 2012 · N446AW · Cndair CL6002B19 · Power LeverSDR REXA2012081301263Relay · failedLEFT THRUST REVERSER INOPERATIVE. REMOVED AND REPLACED RELAY 1K2KE AT JB-10 IAW WM 91-32-10. OPS CHECKED GOOD. OK FOR SERVICE.Aug 13, 2012 · N8543F · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201240784Fairing · chafedLEFT STUB FAIRING IS CHAFED. R & R LT STUB FAIRING, IAW SRM 51-24-36 AND 51-42-06.Aug 13, 2012 · N450AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR ASOA2012091002187Angle · corrodedFS 605 LOWER FRAME REINFORCING ANGLE IS CORRODED. REMOVED AND INSTALLED REINFORCING ANGLE IAW SRM 51-42-06.Aug 13, 2012 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240825Bushing · gougedRIGHT MLG SIDE STAY BUSHING GOUGED. REPAIRED IAW REO 601R-32-11-1240.Aug 13, 2012 · N450AW · Cndair CL6002B19 · Main Landing Gear Attach SectionSDR ASOA2012081402065Lamp · burned outEXTERIOR EMERGENCY LIGHT FWD OF LT OVERWING DOOR IS OUT. RELAMPED EXT EMERGENCY LIGHT NR 5 IAW AMM 33-51-21, OP'S CHECKED GOOD.Aug 12, 2012 · N884AS · Cndair CL6002B19 · Emergency LightingSDR A6WA201240782Sill · corrodedCARGO BAY DOOR SILL CORRODED AROUND NUT PLATES FLAGGED. REMOVED UNSERVICEABLE SECTION OF CARGO BAY FLOOR SILL AND INSTALLED SERVICEABLE SECTION OF CARGO BAY FLOOR SILL IAW REO 601R-53-61-690, REV D, SRM 51-42-06, 51-42-13, 51-42-21.Aug 12, 2012 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240792Cargo Track · corrodedCARGO TRACK AT LBL9 & FS 559+96 IS CORRODED. R & R SEAT TRACK, IAW SRM 51-41-02.Aug 12, 2012 · N450AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201240793Cargo Track · corrodedCARGO TRACK AT RBL 9, FS 559+96 IS CORRODED. R & R SEAT TRACK, IAW SRM 51-41-02.Aug 12, 2012 · N450AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201240763Bleed Valve · failedFLIGHT LEVEL 250, RT PACK WENT OFF LINE AND RT 10TH STAGE SHUTOFF VALVE WOULD NOT OPEN. DESCENDED TO 10,000 FT AND TRANSFERRED RT PACK TO APU. EMERGENCY DECLARED.Aug 11, 2012 · N415AW · Cndair CL6002B19 · Compressor Bleed ValveSDR A6WA201240798Attach Fitting · wornLT ELEVATOR CENTER PCU ATTACH FITTING WORN. BLENDED AREA ON LT ELEVATOR CENTER PCU ATTACH FITTING TRREATED AREA IAW REO 601R-55-11-426.Aug 11, 2012 · N450AW · Cndair CL6002B19 · Horizontal Stabilizer, Attach FittingsSDR A6WA201240799Attach Fitting · wornLT ELEVATOR OTBD PCU ATTACH FITTING WORN. BLENDED DAMAGED AREA ON LT ELEVATOR OTBD PCU ATTACH FITTING TREATED AREA IAW REO 601R-55-11-426.Aug 11, 2012 · N450AW · Cndair CL6002B19 · Horizontal Stabilizer, Attach FittingsSDR A6WA201240800Attach Fitting · wornRT ELEVATOR OTBD ATTACH FITTING WORN. BLENDED DAMAGE EVEN ON RT ELEVATOR OTBD PCU ATTACH FITTING AREA IAW REO 601R-55-11-426.Aug 11, 2012 · N450AW · Cndair CL6002B19 · Horizontal Stabilizer, Attach FittingsSDR A6WA201240783Hinge Bracket · gougedGOUGE IN LT OTBD FLAP, OTBD HINGE BOX AT FLAP HINGE FAIRING FWD OTBD ATTACH POINT REPAIRED DAMAGE ON LT OTBD FLAP HINGE BOX AT ES 264 IAW REO 601R-57-21-1727.Aug 11, 2012 · N450AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201240797Attach Fitting · wornRT ELEVATOR CENTER PCU ATTACH FITTING WORN. BLENDED DAMAGE AREA ON RT ELEVATOR CENTER PCU ATTACH FITTING TREATED AREA IAW REO 601R-55-11-426.Aug 11, 2012 · N450AW · Cndair CL6002B19 · Elevator StructureSDR A6WA201240785Floor Support · corrodedLBL 27 FLOOR SUPPORT HAS CORROSION AROUND NUTPLATE HOLES FROM FS 589.00-621.00. BLENDED OUT CORROSION IN SOME AREAS AND PERFORMED CUTOUT AND REPAIR IN ONE AREA IAW SRM 53-00-43 AND REO 601R-53-00-005, REV B.Aug 11, 2012 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240764Unknown · odorHOT ELECTRICAL ODOR DETECTED BY ALL CREW STRONGEST PRESCENCE HEAD LEVEL AND NEAR CPB1, 3 APU WAS RUNNING WITH GENERATOR ON AND BLEEDS ENG-OFF ODOR IN COCKPIT FIRST THEN GALLEY APU RUN TIME 40 MINS ODOR LINGERED 3-5 MIN AFTER SHUTDOWN. OPERATED APU WITH PACKS Aug 10, 2012 · N469AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA201240765Coalescer Bag · odorNOXIOUS ODOR IN ACFT WITH BOTH PACKS ON AND APU RUNNING. PILOT REPORTED ODOR LIKE BURNED PLASTIC. R & R LT AND RT WATER SEPARATOR COALESCER BAGS IAW AMM 21-51-13. OPS CHECKED GOOD. NO ODOR AT THIS TIME.Aug 10, 2012 · N469AW · Cndair CL6002B19 · Humidity Control SystemSDR ASOA2012082902134Attach Fitting · corrodedSERVICE DOOR LWR SILL ATTACHMENT CLIP LOCATED AT FS 349 IS CORRODED BEYOND LIMITS IAW TASK 000-53-900-509. REMOVED SERVICE DOOR LOWER SILL ATTACHMENT CLIP IAW SRM 51-42-06 & SRM 51-42-21. LOCATED & DRILLED SERVICE DOOR LOWER SILL ATTACHMENT CLIP IAW SRM 51-40Aug 10, 2012 · N846AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2012082902135Tee Fitting · corrodedFWD AND AFT TEE FITTINGS AT SERVICE DOOR ENTRANCE ARE CORRODED BEYOND LIMITS, LOCATED AT FS 319 AND FS 349 WL 73.5 IAW TASK 000-53-900-509. REMOVED CORRODED T FITTING AT FS 349, WL 73.5 IAW SRM 51-42-21. LOCATED AND DRILLED NEW T-FITTING AT FS 349, WL 73.5 IAug 10, 2012 · N846AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2012082902136Floor Support · corrodedFWD FLOOR SUPPORT AND GALLEY SUPPORT PLATE LOCATED AT RBL 35 FROM FS 295 TO FS 319 IS CORRODED BEYOND LIMITS IAW TASK 000-53-900-509. REMOVED CORRODED FLOOR SUPPORT & GALLEY SUPPORT PLATE FROM FS 310 TO FS 319, RBL 36 AND REPLACED WITH SERVICEABLE FLOOR SUPPOAug 10, 2012 · N846AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012082902137Floorbeam · corrodedFLOORBEAM AT FS 349.0 WL 73.5 CORRODED BEYOND LIMITS FROM RBL 27 TO RBL 36 IAW TASK 000-53-900-509. REPAIRED IAW REO 601R-53-21-2342.Aug 10, 2012 · N846AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2012083002151Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROX .3" IN LENGTH 100 PERCENT FSH. LOCATION TOP OF CARGO DOOR AFT TRACK. FAILED NDT INSPECTION. COMPLIED WITH REO 601R-53-61-1541, REV D,Aug 10, 2012 · N846AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201240794Trunnion · damagedFOUND THREE OVERSIZED HOLES IN MLG TRUNNION LOWER FLANGE 1 EA LT AND 2 EA RT SIDES DURING COLD WORKING. REPAIRED 3EA OVERSIZED HOLES IN LOWER MLG TRUNNION FLANGE 1 EA LT AND 2 EA RT IAW REO 601R-57-21-1728, REV.Aug 10, 2012 · N450AW · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR A6WA201240786Seat Track · corrodedCARGO SEAT TRACK AT LBL9 FS 559+112 IS CORRODED. R & R SEAT TRACK IAW SRM 53-41-02.Aug 10, 2012 · N450AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201240787Seat Track · corrodedCARGO SEAT TRACK AT LBL9 FS 559+112 IS CORRODED. R & R SEAT TRACK IAW SRM 51-41-02.Aug 10, 2012 · N450AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201240790Cargo Track · corrodedCARGO TRACK AT RBL9, FS 559+96 IS CORRODED. R & R CARGO TRACK IAW SRM 51-41-02.Aug 9, 2012 · N450AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201240791Bulkhead · damagedBULKHEAD DAMAGED. REPAIRED ON BS 280 BULKHEAD IAW REO 601R-53-11-1727 AND SRM 51-42-06.Aug 9, 2012 · N450AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201240789Cargo Track · corrodedCARGO TRACK AT LBL9, FS 599+96 IS CORRODED. R & R CARGO TRACK IAW SRM 51-41-02.Aug 9, 2012 · N450AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012082902126Attach Angle · crackedLEFT UPPER WING UNDER FUSELAGE TO WING ACCESS PANEL 161EL VERTICAL ATTACHMENT ANGLE IS CRACKED. LOCATED & DRILLED NEW SERVICEABLE VERTICAL ATTACHMENT BRACKET IAW SRM 51-40-11, INSTALLED NEW SERVICEABLE VERTICAL ATTACHMENT BRACKET UNDER ACCESS PANEL 161EL ON LAug 8, 2012 · N846AS · Cndair CL6002B19 · Wing, Attach FittingsSDR ASOA2012082902127Attach Angle · crackedRIGHT UPPER WING UNDER FUSELAGE TO WING ACCESS PANEL 162EL VERTICAL ATTACHMENT ANGLE IS CRACKED FS 469.53. REMOVED DAMAGED RT UPPER WING VERTICAL ATTACHMENT ANGLE & REPLACED W/NEW SERVICEABLE ANGLE PN IAW SRM 51-42-13 & 51-42-06.Aug 8, 2012 · N846AS · Cndair CL6002B19 · Wing, Attach FittingsSDR ASOA2012082902128Angle · crackedRIGHT FS 484.00 INTERCOSTAL ANGLE AT RBL 27 IS CRACKED .5" LONG IN UPPER RADIUS. REMOVED CRACKED ANGLE AT RBL 27 & REPLACED W/NEW SERVICEABLE ANGLE PN 601R31171-9 IAW SRM 51-42-21. TOUCHED UP REPAIR FASTENERS IAW SRM 51-25-01. APPLIED WATER DISPLACING CORROAug 8, 2012 · N846AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012082902129Angle · crackedLT FS 484.00 INTERCOSTAL ANGLE AT LBL 27 IS CRACKED .5 INCHES LONG IN UPPER RADIUS. REMOVED CRACKED ANGLE AT LBL 27 & REPLACED W/NEW SERVICEABLE ANGLE PN 601R31171-17 IAW SRM 51-42-21. PAINTED FASTENERS ON REPAIRED AREA IAW SRM 51-25-01, APPLIED WATER DISPLAAug 8, 2012 · N846AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012082902130Intercostal · crackedLEFT FS 460.00 INTERCOSTAL IS CRACKED AT LBL 9 SECOND RIVET DOWN .5" LONG. CUT AWAY DAMAGE ON INTERCOSTAL WEB AS SHOWN IN REO 601R-53-41-1600 FIG 2 SHEET 2 TO STEP 1 & 2. FABRICATED DOUBLER & FILLER IAW REO 601R-53-41-1600 IAW SRM 51-21-16 TO STEPS 4 OF REO. Aug 8, 2012 · N846AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012082902131Angle · crackedLEFT FS 484.00 INTERCOSTAL ANGLE AT LBL 9 IS CRACKED .5" LONG IN UPPER RADIUS. INSTALLED A NEW ANGLE 601R31171-27 PO W17821 IAW AMM 51-42-21.Aug 8, 2012 · N846AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012082902132Isolator · crackedFS 621.00 REAR PRESSURE BULKHEAD HAS AN ISOLATOR BROKEN. REMOVED ISOLATOR, LOCATED HOLES IN NEW BRACKET AND INSTALLED USING MS20470AD5-5. ALL WORK PERFORMED IAW SRM 51-42-06.Aug 8, 2012 · N846AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2012082902133Floorbeam · crackedIN PASSENGER COMPARTMENT BELOW FLOOR AT FS 280.00 ON RBL 9.00 AND LBL 9.00, INBD ATTACHMENT ANGLES ARE CRACKED. REMOVED THE CRACKED ATTACHMENT ANGLE AT FS 280.00 ON RBL 9.00 IAW SRM 51-42-21. INSTALLED NEW SERVICEABLE ATTACHMENT ANGLE (PN 601R31113-58) AT FAug 8, 2012 · N846AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2012081002053Latch · contaminatedF/A UNABLE TO OPEN MAIN PAX DOOR. FOUND DEBRIS IN LATCH ON MECHANISM CLEANED OUT AND LUBRICATED IAW AMM 52-11-03. ALL ROLL FITTINGS ACFT OK FOR SERVICE.Aug 7, 2012 · N824AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012081002055Lamp · burned outNR 3 CABIN CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED NR 3 CABIN EMERGENCY FLOOD LIGHT IAW AMM 33-51-16, OPS CHECKED GOOD.Aug 7, 2012 · N972EV · Cndair CL6002B19 · Emergency LightingSDR A6WA201240770Flap System · failedFLAP FAIL AT 15 DEGREES AFTER TAKEOFF. RETURNED TO LAND AT 46600 LBS. FPM DESCENT RATE AT TOUCHDOWN APPROX 400 FPM. PERFORMED FLAP RESET PROCEDURE IAW SUP 98-18E, BOX 12. FLAPS RESET. REF TO MX WO 189963 FOR ACCOMPLISHED JOB. R & R RT BPSU. OPS CHECK GOAug 7, 2012 · N417AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA2012082902125Plate · corrodedSERVICE DOOR STEP PLATE HAS MAJOR CORROSION. NEW SERVICE DOOR STEP PLATE DRILLED IAW SRM 51-41-04. INSTALLED PLATE IAW AMM 25-33-01-400-802, STEP 3A(8).Aug 7, 2012 · N846AS · Cndair CL6002B19 · Service DoorsSDR ASOA2012083002140Skin · crackedLT WING LOWER PLANK IS CRACKED .235" LONG OTBD OF JACK PAD PLUG AT WS 148.019 T/E. COMPLIED WITH EC/TC REO 601R-57-21-131 AND REO 601R-57-21-131, REV A DATED 08/29/2011 AS WRITTEN. COMPLIED WITH EC/TC REO 601R-57-21-130 AND GENERIC REO 601R-57-21-130 REV.J.Aug 7, 2012 · N846AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2012083002141Skin · crackedEXTERIOR SURFACE OF LOWER RT WING PLANK T/E AT WS 148.019 IS CRACKED APPROX 1.0 LONG. COMPLIED WITH EC/TC REO 601R-57-21-131 AND REO 601R-57-21-131 REV A.Aug 7, 2012 · N846AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2012091002180Skin · corrodedRT LOWER WING PLANK ACCESS HOLE NR 10 AT WS 188.040, 650BB HAS CORROSION AT INBD END MEASURING APPROX 1.4" LONG X .10" WIDE X .003" DEEP. COMPLIED WITH ECTC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV H.Aug 7, 2012 · N903EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2012091002182Skin · corrodedLEFT LOWER WING PLANK ACESS HOLE NR 5 AT WS 76.161, 540CB HAS CORROSION AT OTBD END MEASURING APPROX 1.3" LONG X .10" WIDE X .002" DEEP. COMPLIED WITH ECTC EO 600-57-81 & REO 601R-57-21-030, REV H.Aug 7, 2012 · N903EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2012091002183Skin · corrodedLEFT LOWER WING PLANK ACCESS HOLE 8 AT WS 136.676, 540FB HAS CORROSION AT INBD, OTBD ENDS AND 2 PLACES ON AFT EDGE. INBD CORROSION MEASURES APPROX 2" LONG X .12" WIDE X .002" DEEP. OTBD CORROSION MEASURES APPROX 4.7" LONG X .11" WIDE X .002" DEEP. CORROSION ONAug 7, 2012 · N903EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2012091002184Skin · corrodedLEFT LOWER WING PLANK ACCESS HOLE NR 10 AT WS 188.040, 550BB HAS CORROSION AT INBD AND OTBD ENDS. INBD CORROSION MEASURES APPROX 1.3" LONG X .10" WIDE X .002" DEEP. OTBD CORROSION MEASURES APPROX 1.5" LONG X .11" WIDE X .002" DEEP. COMPLIED WITH ECTC EO 600-Aug 7, 2012 · N903EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2012091002186Skin · corrodedLEFT LOWER WING PLANK ACCESS HOLE NR 15 AT WS 294.048, 550GB HAS CORROSION MEASURING APPROX 1.3" LONG X 1.0" WIDE X .002" DEEP. COMPLIED WITH ECTC EO 600-57-81 & REO 601R-57-21-030, REV H.Aug 7, 2012 · N903EV · Cndair CL6002B19 · Wing, Plate/Skin
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