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 ASOA201001438Web · crackedPAX DOOR AFT WEB IS CRACKED AT FASTENER HOLE FOR DRAG ANGLE AND STIFFENER. REMOVED CRACKED AFT WEB FROOM PAX DOOR. REMOVED ASSOCIATED STIFFENERS AND ANGLES. FIT, DRILLED AND INSTALLED SAME SERVICEABLE STIFFENERS AND ANGLES ONTO NEW WEB IAW SRM 51-42-06 ANDSep 23, 2010 · N970EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001437Floor Support · corrodedCONTINUATION OF MWC 347. FLOOR SUPPORT OTBD OF RBL 36 IS CORRODED FROM FS 621.00 TO FS 559.00+80. 26 EA NUTPLATES NEED INSTALLED. REINSTALLED 26 EA NUTPLATES IAW SRM 51-42-10.Sep 22, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001449Support · crackedCARGO DOOR STEP PLATE SUPPORT IS CRACKED. REMOVED CARGO DOOR STEP PLATE SUPPORT FROM FLOORBOARD 281LLF BY REMOVING 13 SCREWS. SUPPORT REQUIRES INSTALL. INSTALLED NEW SERVICEABLE CARGO DOOR STEP PLATE SUPPORT FLOORBOARD 281LLF BY PLACING INTO POSITION AND INSep 20, 2010 · N846AS · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA201040721Rib · crackedLT WHEEL WELL BATTERY RIB CRACKED AT WS 53.60. TRIMMED OUT DAMAGED AREA AND REPAIRED IAW REO 601R-57-51-046, REV B.Sep 20, 2010 · N451AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR ASOA201001410Light · no testRT SIDE DOORS ( SERVICE AND EMERGENCY EXITS ) BETA LIGHTS FAILED FUNCTIONAL CHECK. R & R RT SIDE DOORS (SERVICE AND EMERGENCY EXITS & BETA LIGHTS IAW AMM CH 33-51-09-400-801. COMPLIED WITH FUNCTI0NAL TEST OF THE DOOR EXIT SIGN BETA-LIGHTS ON THE RT SERVICE DSep 19, 2010 · N828AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001411Light · inoperativeLT SIDE DOORS (ASD AND EMERGENCY EXIT) BETA LIGHTS FAILED FUNCTIONAL CHECK. R & R ASD DOOR EXIT BETA LIGHT IAW AMM 11-30-02-00, 33-51-09-000-801, AND 33-51-09-400-801. FUNCTIONAL TEST OF ASD BETA LIGHT GOOD IAW AMM 33-51-09-720-801. EMERGENCY EXIT DOOR STILL Sep 19, 2010 · N828AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001412Seat Track · corrodedLT AND RT FLOOR SEAT TRACKS CORRODED FROM FS 364.00 TO FS 394.00. REMOVED LT AND RT SEAT RAILS AT FS 364.00 TO FS 394.00 IAW AMM TASK 53-01-11-000-802. INSTALLED NEW LT AND RT FLOOR SEATS TRACKS FORM FS 364.00 TO FS 394.00 IAW AMM 53-01-11-400-802. (CLOSED)Sep 19, 2010 · N828AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001413Floorbeam · crackedFS280 BEAM CRACKED ON LT SIDE, LT OF PULLEY BRACKET AT LBL9. REPAIRED FS 280 BEAM IAW EC/TC REO 601R-53-11-171 AND REO 601R-53-11-171. (CLOSED)Sep 19, 2010 · N828AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001401Floorbeam · crackedFS 280 OTBD OF LBL 9, WL 73 FLOOR SUPPORT J-ANGLE CRACKED AT ALTERNATE EXTENTION PULLEY BRACKET. COMPLIED WITH EC/TC REO 601R-53-11-926 IAW REO 601R-53-11-926, REV B.Sep 18, 2010 · N970EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001404Seat Track · corrodedCARGO BAY FLOOR SEAT RAILS AT LBL 27 FS 559.00+80 TO 559.00+96, 559.00+104, 559.00+110, AND 567.00 ARE CORRODED. REMOVED AND INSTALLED SERVICEABLE SEAT RAILS IAW 51-41-02 SRM.Sep 18, 2010 · N970EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001405Seat Track · corrodedCARGO BAY FLOOR SEAT RAILS AT LBL 9 FS 559.00+91 TO 559.00+96, FS 559.00+110 TO 569.00, FS 583, FS 600.00, AND FS 612.00 TO 617.00 ARE CORRODED. R & R SEAT RAIL AT LBL 9 BETWEEN FS 559.00+110 & FS 569 IAW SRM CH 51-41-02.Sep 18, 2010 · N970EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001406Seat Track · corrodedCARO BAY FLOOR SEAT RAILS AT RBL 9 FS 559.00+91 TO 559.00+96 AND FS 559.00+110 TO 569.00 ARE CORRODED. REMOVED SEAT RAILS IN CARGO COMPARTMENT. REF AMM 53-01-11-000-802 & INSTALLED NEW SERVICEABLE RAILS AT SAME LOCATIONS, REF AMM 53-01-11-400-802.Sep 18, 2010 · N970EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001407Seat Track · corrodedCARGO BAY FLOOR SEAT RAIL AT RBL 27 FS 559.00+80 TO FS 559.00+96 IS CORRODED. REMOVED SEAT TRACK IN CARGO BAY REF AMM 53-01-11-000-802 & INSTALLED NEW SERVICEABLE TRACK IAW AMM 53-01-11-400-802.Sep 18, 2010 · N970EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA201024923Engine · malfunctionedVIB CAUTION MESSAGE ON N2 OF LEFT ENGINE FOLLOWED BY HOT ITT FOLLOWED BY OIL PRESSURE LOSS. (FLT 4719) REPLACED LEFT ENGINE ASSEMBLY WITH A SERVICEABLE UNIT PER AMM.Sep 18, 2010 · N445SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA201001436Isolator · brokenREAR PRESSURE BULKHEAD HAS 5 BROKEN ISOLATORS. REMOVED 5 BROKEN MOUNT ISOLATORS FROM 621 BULKHEAD BY DRILLING RIVETS FROM ISOLATORS AND MOUNT BRACKETS. INSTALLED FIVE NEW SERVICEABLE ISOLATOR MOUNTS BY INSTALLING ISOLATORS ON BRACKETS WITH RIVETS IAW SRM 51-Sep 18, 2010 · N970EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201001395Handle · dirtyMAIN PAX DOOR HANDLE IS HARD TO MOVE/OPEN. INSP LINKAGE AND REMOVED DEBRIS. LUBE DOOR AND ROLLERS. OPS CHECKS GOOD WITH NO DEFECTS NOTED. REF AMM 52-11-02. (CLOSED)Sep 17, 2010 · N824AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001396Post · crackedFOUND FS 409.0+128, RBL 18.0 OTBD VERTICAL POST HAS INDICATION NOTED APPROX .3" IN LENGTH 50 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS, FAILED NDT INSP. REMOVED BOTH POST INBD AND OTBD IAW SRM 51-42-06. DRILLED & LOCATED FASTENER HOLES IAW SRM 51-40-06. INSSep 17, 2010 · N970EV · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201001435Placard · wornPAX DOOR ARROW DOWN AND EXIT PLACARDS WORN ON 5TH AND 3RD STEPS. R & R PAX DOOR ARROW AND EXIT PLACARDS IAW AMM 11-30-00-000-801 AND 11-30-00-400-801.Sep 16, 2010 · N970EV · Cndair CL6002B19 · Placards and MarkingsSDR ASOA201001484Sill · corrodedRT CABIN SIDE SILL CORROSION AT FS 578.00 EXCEEDED ALLOWABLE BLENDING LIMITS 1.0" WIDE, 1.1" LONG, .040 DEEP AROUND NUTPLATE HOLE. C/W STEPS 1, 2, 4, 5 AND 6 OF REO 601R-53-00-383. C/W REO 601R-53-00-383A. PERFORMED EDDY CURRENT OF RT CABIN FLOOR SIDE SILL.Sep 15, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040785Skin · chafedRT MLG DOOR HAS CHAFE DAMAGE AT FWD AND AFT LOWER INBD EDGES COMPLIED WITH REO 601R-52-82-033, REV A, REO 601R-52-82-034, REV NC, REO 601R-52-82-290 REV NC TO REPAIR CHAFE DAMAGE.Sep 14, 2010 · N407AW · Cndair CL6002B19 · Landing Gear DoorsSDR MALA100128Lamp · inoperativeDURING ROUTINE CHECK NOTED EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT IAW REF 33-51-21 PN ON/OFF 1317.Sep 13, 2010 · N840AY · Cndair CL6002B19 · Emergency LightingSDR CA100916003Hose · leakingDURING THE ROUTINE MX, THE AIR DRIVEN GENERATOR (ADG) WAS DEPLOYED IN ORDER TO COMPLETE A FUNCTION CHECK. AFTER THE TEST, DURING THE STOWING OF THE ADG A HYD LEAK APPEARED IN THE PRESSURE LINE (24-23-00, FIG 1, ITEM 50, PN AE1000884G0122), THIS LINE DID NOT ASep 13, 2010 · Cndair CL6002B19 · AC Generation SystemSDR ASOA201001309Valve · failedUPON T/O & RETRACTING GEAR NOSE GEAR DOORS WOULD NOT CLOSE. RECEIVED NOSE GEAR OPEN MASTER WANING . CYCLED GEAR ONCE. LANDED UNDER 47. DOOR REMAINED OPEN ALL THE WAY INTO THE GATE. ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY EQUIPMENT STANDING BY AS A PSep 12, 2010 · N686BR · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA201001310Support Angle · corrodedSUPPORT ANGLE FOR RT WARDROBE FITTING AT FS 349 BETWEEN BL 36-42R IS CORRODED. REMOVED SUPPORT ANGLE IAW SRM 51-42-06. CORRODED SUPPORT ANGLE IS BEYOND REPAIRABLE LIMITS IAW SRM 53-00-00, FIG 102, SHEET 2, LOCATED, DRILLED UP NEW SERVICEABLE SUPPORT ANGLE ISep 12, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001311Support · corrodedTHE SILL SUPPORT JUST IN FRONT OF SVC DOOR FS 310-319 IS CORRODED. REMOVED SILL PLATE IAW SRM 51-42-06. SILL PLATE REQUIRES INSTALLATION. INSTALLED NEW SERVICEABLE SILL PLATE IAW SRM 51-42-06. APPLIED PROTECTIVE TREATMENT IAW SRM 51-25-01.Sep 12, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001312Floor Support · corrodedCLIP ON THE AFT SIDE OF FLOOR SUPPORT CROSSMEMBER AT FS 349, RBL 42 IS CORRODED. REMOVED AFT CLIP IAW SRM 51-42-06 AND 51-42-21. CLIP REQUIRES REPLACED. REPLACED DAMAGED CLIP WITH SERVICEABLE CLIP IAW SRM 51-42-21. PAINTED IAW SRM 51-25-01.Sep 12, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001313Floor Support · corrodedCLIP ON FWD SIDE OF FLOOR SUPPORT CROSSMEMBER AT FS 349, RBL 42 IS CORRODED. REMOVED FWD CLIP IAW SRM 51-42-06 AND 51-42-21. LOCATED AND INSTALLED SERVICEABLE CLIP AT FS 349, RBL 42 IAW SRM 51-42-06.Sep 12, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001314Floor Support · corrodedTHE FLOOR SUPPORT CROSSMEMBER IS CORRODED AT THE RT END AT FS 349.Sep 12, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001315Floor Support · corrodedCLIP ON AFT SIDE OF FLOOR SUPPORT CROSSMEMBER AT 319.70 RBL 42 CORRODED. REMOVED CLIP ON AFT SIDE OF FLOOR SUPPORT IAW SRM 51-42-06, 51-42-26. REMOVED CORROSION ON CLIP IAW SRM 51-21-06 AREA ON CLIP WITHIN LIMITS IAW SRM 53-00-00, MATERIAL REMOVED .003, REMAISep 12, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001316Fitting · corrodedSERVICE DOOR SILL FITTING AT FS 319.70, RBL 42 CORRODED. REMOVED SILL FITTING IAW SRM 51-42-21. DRILLED & LOCATED NEW SERVICEABLE STRAP BRACKET IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE STRAP BRACKET IAW SRM 51-42-21. APPLIED PROTECTIVE PAINT IAW SRM 51-2Sep 12, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001317Battery Pack · inoperativeEXTERIOR EMERGENCY LIGHTS 7 AND 8 INOP. R & R NR4 EMERGENCY BATTERY PACK FOR LIGHTS IAW AMM 33-51-04. OPS CHECKS GOOD. NO DEFECTS NOTED. PLACARD REMOVED. DMIL CLEARED.Sep 12, 2010 · N902EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201001318Control Unit · failed"SPOILERONS" MESSAGE IN FLIGHT(EMERGENCY DECLARED). R & R NR 2 SECU IAW AMM 27-61-05. OPS CHECK GOOD, NO DEFECT NOTED AT THIS TIME. (CLOSED)Sep 12, 2010 · N976EV · Cndair CL6002B19 · Drag Control SystemSDR MALA100120Lamp · inoperativeNOTED EXTERIOR EMERGENCY LIGHT 1 INOP. RELAMPED EXTERIOR EMERGENCY LIGHT 1 IAW AMM 33-51-21 OP CHECKED IAW TASK 33-51-00-710-801.Sep 11, 2010 · N8976E · Cndair CL6002B19 · Emergency LightingSDR ASOA201001307Light · inoperativeNR 1 POSITION EXTERIOR EMERGENCY LIGHT INOP. R & R NR1 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. R & R NR1 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.Sep 11, 2010 · N824AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001304Sign · unknownREPLACED COVER EXIT SIGN OVER SERVICE DOOR, OPS OK IAW AMM 33-50-00 NEF CLEARED. (CLOSED)Sep 10, 2010 · N842AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001295Bulb · burned outTHE LT FWD OVERWING EMERGENCY LIGHT IS INOP. REPLACED LIGHT BULB FOR LT FWD OVERWING EMERGENCY LIGHT. OPS CHECKED GOOD. WORK DONE IAW AMM CHAPTER 33-51-21.Sep 9, 2010 · N926EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201001298Stringer · corrodedSTRINGER 27 CORRODED BETWEEN FS 319.00 AND FS 349.00. CUT STRINGER 27 AT FS 325 AND REMOVED AFT CORRODED SECTION IAW REO 601R-53-21-1183 REV & SRM 53-00-03. CUT EDGES OF STR 27 AFT FS 325. COMPLIED WITH SRM 53-00-03. PERFORMED EDDY CURRENT OF CUT EDGES IAW NSep 9, 2010 · N823AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR ASOA201001299Skin · corrodedSKIN CORRODED BETWEEN FS 409+16 AND 409+32 AT STR 27 AROUND STROBE LIGHT. REMOVED BEACON LIGHT REINFORCEMENT ANGLE CHANNEL IAW SRM 51-42-06. LOCATED BETWEEN FS 409+16 AND 409+32 FOUND SKIN UNDER CHANNEL TO BE FREE OF CORROSION. CHANNEL IS CORRODED BEYOND RESep 9, 2010 · N823AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA201001300Intercostal · corrodedINTERCOSTAL AT FS 559.00+80 BETWEEN RBL 9 AND RBL 27 IS CORRODED. REMOVED CAP STRIP AT FS 559.00+80 INTERCOSTAL BETWEEN RBL 9-27 IAW SRM 51-42-06 AND 51-42-10. AFTER FURTHER INVESTIGATION OF DAMAGE AT FS 559.00+80 BETWEEN RBL 9 AND RBL 27, FOUND DAMAGE TO BSep 9, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001301Frame · corrodedFRAME SECTION AT FS 349.00 IS CORRODED AT STRINGER 27. REMOVED CORROSION FROM FRAME FS 349.00 STRINGER 27 IAW SRM 51-21-06. AREA OF CORROSION REMOVED WITHIN LIMITS IAW SRM 53-00-00, FIG 102 (SHEET 2). MATERIAL REMOVED .002, REMAINING MATERIAL .061. PAINTSep 9, 2010 · N923EV · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201001302Frame · corrodedFRAME SECTION AT FS 333.00 FROM STRINGER 25L TO 25R IS CORRODED. REMOVED FASTENERS FROM FRAME SECTION AT FS 333, FROM STR 23L TO 23R IAW SRM 51-42-06 AND 51-42-21. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-15 AND 53-00-00. REMOVED FRAME SECTION FROSep 9, 2010 · N923EV · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201001303Beam · crackedTRANSVERSE BEAM IS CRACKED OTBD OF ALTERNATE EXTENSION CABLE PULLEY ON RT SIDE APPROX 1" LONG. REPAIRED FS 280 TRANSVERSE BEAM IAW EC/TC REO 601R-53-11-138.Sep 9, 2010 · N923EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001305Uplock · failedGEAR UP DISAGREE MSG RT MAIN GEAR (A/C RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED] R & R RT MLG UPLOCK ASSY IAW AMM 32-32-05. LEAK AND OPS CHECK GOOD. (CLOSED)Sep 9, 2010 · N860AS · Cndair CL6002B19 · Landing Gear Position and WarningSDR ASOA201001293Bulb · burned outRT EMERGENCY LIGHT INOP FWD OF EMERGENCY DOOR EXIT. R & R RT EMERGENCY LIGHT BULB FWD OF EMERGENCY DOOR EXIT IAW AMM 33-50-01 OPS CK GOOD.Sep 8, 2010 · N883AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001297Battery Pack · dischargedEMERGENCY BATTERY PACK NR2 IS DEAD. R & R SERVICEABLE PART IAW AMM 33-1-04-000-801 AND 33-51-04-400-801. OPS CHECK OF PACK GOOD. (CLOSED)Sep 8, 2010 · N686BR · Cndair CL6002B19 · Emergency LightingSDR ASOA201001283Post · crackedFOUND FS 409.0+128, RBL 18.0 INBD SIDE VERT POST HAS INDICATION NOTED APPROX .3" IN LENGTH 60 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSP. REMOVED INBD AND OTBD POSTS AT FS 409, RBL 18 IAW SRM 51-42-06. DRILLED SERVICEABLE INBD POST IAW SRM 51Sep 5, 2010 · N823AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201001284Angle · corrodedANGLE AT CARGO DOOR SILL PLATE IS CORRODED. REMOVED ANGLE, LOCATED, DRILLED, AND DEBURRED NEW IAW SRM 51-42-06 AND 51-40-11. INSTALLED ANGLE IAW SRM 51-42-06 & 51-42-21.Sep 5, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001285Fitting · crackedFITTING AT LOWER LT 621 BULKHEAD OTBD IS CRACKED. FOUND TO BE CRACKED, LT FS 621 BULKHEAD FLOOR SUPPORT ANGLE. REMOVED CRACKED LT FS 621 FLOOR SUPPORT ANGLE AND FOUND TO BE PREVIOUSLY REPAIRED IAW REO 601R-53-61-117 AND FOUND 11EA ELONGATED FASTENER HOLES THROSep 5, 2010 · N823AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201001286Battery Pack · inoperativeOVERHEAD EMERGENCY LIGHTS INOP. R & R NR 4 BATTERY PACK IAW AMM 33-51-04. OPS CK GOOD. R & R NR 4 BATTERY PACK IAW AMM 33-51-04, OPS CK GOOD.Sep 5, 2010 · N836AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001287Floorbeam · corrodedFS 559+80 FLOOR SUPPORT CAP STRIP BET RBL 9 - RBL 27 CORRODED. REMOVED FLOOR SUPPOR TCAP STRIP IAW SRM 51-42-06. INSTALLED NEW CAP STRIP IAW SRM 51-42-06 & 51-45-00.Sep 5, 2010 · N846AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
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