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 ASOA201001508Light · damagedWARDROBE FLOOR EMERGENCY FLOOD LIGHT DAMAGED. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHT ON WARDROBE IAW AMM 33-51-19. OPS CHECK GOOD. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHT ON WARDROBE IAW AMM 33-51-19. OPS CHECK GOOD.Oct 6, 2010 · N932EV · Cndair CL6002B19 · Emergency LightingSDR CA101018009Plate · wornMID CABIN RT EMERG EXIT DOOR WILL NOT OPEN. RT OVERWING EMERG EXIT REMOVED. SEEMS TO BE CATCHING ON THE UPPER SILL AND REQUIRES EXCESSIVE FORCE TO OPEN. DOOR SEAL FOUND DAMAGED. SEAL REPLACED. FABRICATED NEW RT EMERGENCY EXIT DOOR SLIDER PLATE IAW DWG-601Oct 6, 2010 · Cndair CL6002B19 · Emergency ExitsSDR A6WA201040774Switch · defectiveDURING CLIMB OUT AND AFTER T/R WAS DISARMED RECEIVED GREEN THRUST REVERSER ICON IN LT N1 GUAGE, NO ABNORMAL THRUST INDICATION THRUST LEVER SETTING WERE NOTED. R & R LT T/R DEPLOY SWITCH IAW AMM 78-37-01. OPS CHECK OK. LT T/R SYS GOOD AT THIS TIME. REMOVED Oct 5, 2010 · N428AW · Cndair CL6002B19 · Engine Thrust ReverserSDR MASA2010100601081Fuel Control · out of rigLT ENG ITT 905 AT TAKEOFF POWER, CREW ABORTED TAKEOFF. MX RIGGED FUEL CONTROL UNIT, OPS GOOD.Oct 4, 2010 · N17358 · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR MASA2010100601086Fan · out of balanceNR 1 ENGINE FAN VIBE REACHES 1.2MILS. MX REPLACED 28 WEIGHTS TO 4160T045P01, CHANGED 1 WEIGHT TO P06. FAN VIBE [NOW] .6 AT TAKEOFF POWER.Oct 4, 2010 · N7264V · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR A6WA201040753Bracket · crackedRT ENG JETPIPE NUTPLATE BRACKET PN 228-50181-833 UNDER PANEL 446BL IS CRACKED. REMOVED CRACKED BRACKET ASSY PN 228-50181-833. LOCATE AND INSTALLED NEW SERVICEABLE BRACKET ASSY PN 228-550181-833 UNDER PANEL 446BL, R JET PIPE.Oct 4, 2010 · N451AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA201040752Compressor · damagedAFTER T/O WITH CLIMB POWER SET, LT ENGINE LOUD NOISE & SHOOK, ITT WENT RED FOR APPROX 3 SECONDS, ACCOMPANIED BY BURNED ODOR IN COCKPIT. C/W QRH, PULLED LT THROTTLE BACK AND AT THAT POINT AMBER VIBE ICON ON LT ENG NR 2, RETURNED TO DEPARTURE, DID NOT LAND OVEROct 4, 2010 · N469AW · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR ASOA201001496Bulb · burned outSERVICE DOOR LWR EMERGENCY EXIT SIGN HAS 2 BURNED OUT BULBS. R & R INOP BULBS FROM SVC DOOR LWR EMERGENCY EXIT SIGN IAW AMM 33-51-14.OPS CHECKED GOOD. R & R INOPERATIVE BULBS FROM SERVICE DOOR LWR EMERGENCY EXIT SIGN IAW AMM 33-51-14. OPS CHECKED GOOD.Oct 3, 2010 · N845AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001492Pressure Panel · crackedFOUND FS 460 PRESSURE FLOOR HAS 2 INDICATIONS NOTED. 1 BETWEEN BL 0 AND RBL 9.0 2.8" LENGTH 50 PERCENT FSH AND 2ND BETWEEN BL 0.0 AND RBL 9.0 2.8" LENGTH 50 PERCENT FSH. FAILED NDT INSP. REO 601R-53-41-1279 REV. HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEOct 2, 2010 · N823AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201001488Lamp · burned outRT FWD EXTERNAL EMERGENCY LIGHT IS INOP. RELAMPED RT FWD EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21.OPS CHECK GOOD. RELAMPED RT FWD EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.Oct 1, 2010 · N857AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001478Floorbeam · corrodedCORROSION OF FLOORBEAMS AFT OF SPLICE AT FS 570 LBL9 - RBL9, REPAIRED IAW REO 670-53-21-591.Sep 30, 2010 · N710EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001481Fitting · corrodedLT OVERWING EXIT CORROSION AT LOWER LATCH FITTING. THIS ITEM IS INCORPORATED UNDER NEW EC/TC REO 601R-52-21-057 THIS CLEARS MCO 528892-2 REF TO AFDL 528987-3 FOR NEW MCO.Sep 30, 2010 · N821AS · Cndair CL6002B19 · Emergency ExitsSDR ASOA201001482Fitting · corrodedLT OVERWING EMERGENCY EXIT HAS CORROSION ON LOWER LATCH FITTING REF TO OLD MCO 528892-2. REPAIRED IAW REO 601R-53-21-057 REV C.Sep 30, 2010 · N821AS · Cndair CL6002B19 · Emergency ExitsSDR ASOA201001483Battery · inoperativeCAPTAINS FLASHLIGHT INOP. R & R CAPTAINS FLASHLIGHT BATTERYS IAW AMM 25-61-00. OPS CHK GOOD. OPS CHK GOOD. (CLOSED)Sep 30, 2010 · N884AS · Cndair CL6002B19 · Emergency EquipmentSDR A6WA201040720Skin · scoredSCRIBE MARK ON UNDERSIDE OF RT WING AT WS389 JUST AFT OF THE L/E. DEPTH OF SCRIBE MARK MEASURED 0.002" BLENDED SCRIBE MARK AREA TO REMOVE MARK, NOT EXCEEDING ORIGINAL DEPTH OF 0.002". PERFORMED NDT OF AREA, PERFORMED ROTO PEEN OF AREA THEN REAPPLIED FINISH ISep 30, 2010 · N451AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA201040722Rib · crackedRT WW BATT RIB CRACKED AT WS 53.60. TRIMMED OUT DAMAGED AREA AND REPAIRED IAW REO 601R-57-51-046, REV B.Sep 30, 2010 · N451AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR MASA2010093001058Gearbox · overservicedUNCONTROLLABLY HIGH OIL TEMP ON R ENGINE. CREW SHUT DOWN ENGINE AND RTF. MX FOUND AGB OVER SERVICED WITH OIL AND DRAINED TO PROPER LEVEL, OPS CHECKS WERE GOOD.Sep 29, 2010 · N17275 · Cndair CL6002B19 · Turbine Engine Accessory DriveSDR ASOA201001474Fitting · corrodedRT OVERWING EMERGENCY EXIT HAS CORROSION AT LWR LATCH FITTING. FOUND CORROSION ON LT WING EMERGENCY EXIT DOOR PN 601R30000-957, SN SB/RU/391. NOT THE RT EMERGENCY EXIT DOOR AS PREVIOUSLY REPORTED. FOUND LT AND RT OVERWING EMERGENCY EXITS WERE SWAPPED. SWAPSep 29, 2010 · N821AS · Cndair CL6002B19 · Emergency ExitsSDR ASOA201001475Skin · crackedCRACK IN SKIN AT AFT RT SIDE OF NLG DOOR CUT OUT AT FS 235 AT STR 26R.Sep 29, 2010 · N832AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA201001476Seat Track · corrodedSEAT RAIL BEAM CAP AT FS 610-589, LBL 27 HAS CORROSION AT 4 EA LOCATIONS. REMOVED SEAT RAIL CAP AT FS 569-610 IAW SRM 51-42-06, 51-42-21. LOCATED, DRILLED NEW SEAT RAIL CAP IAW SRM 51-42-06, 51-42-21. NEW SEAT RAIL CAP REQUIRES INSTALLATION. INSTALLED NEW SESep 29, 2010 · N923EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001477Battery Pack · inoperativeRIGHT EXIT EMERGENCY EXIT INDENTIFICATION SIGN INOP. R & R NR 4 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD.Sep 29, 2010 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201001471Line · leakingHYD SYS 2 FAILURE IN FLIGHT PRESSURE AND QTY INDICATE 0. (EMERGENCY DECLARED -- ENROUTE TO IAD ACFT DIVERTED DUE TO MX) FOUND HYD SYS NR 2 PRESSURE LINE ON BRAKE CONTROL VALVE LEAKING. R & R HYD LINE IAW AMM 20-22-01 LEAK CHECK GOOD. (CLOSED)Sep 28, 2010 · N830AS · Cndair CL6002B19 · Hydraulic System, MainSDR ASOA201001472Bulb · inoperativeNR 7 EXTERIOR EMERGENCY LIGHT INOP. PERFORMED OPS CHK OF LT NR7 EXT EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHK GOOD, NO DEFECTS NOTED. PERFORMED OPS CHK OF LT NR 7 EXT EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHK GOOD, NO DEFECTS NOTED. (CLOSED)Sep 28, 2010 · N906EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201001451Lens · missingFLOOD LIGHT LENS MISSING AT FLOOR LEVEL ON FWD BULKHEAD AT ASD. R & R FLOOD LIGHT ASSY IAW AMM 33-51-19. (CLOSED)Sep 27, 2010 · N686BR · Cndair CL6002B19 · Emergency LightingSDR ASOA201001455Stringer · corrodedSTRINGER 26L BETWEEN FS 349 AND 333 HAS MATERIAL LOSS OF 50 PERCENT FROM CORROSION. TOP COAT REQUIRES TO BE APPLIED TO EXTERIOR SIDE OF REPAIR AT FS 299.306, STR 26L RIVET HEADS. PAINTED IAW SRM 51-25-01.Sep 27, 2010 · N846AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR ASOA201001456Angle · crackedLT 621-625 OBLIQUE ANGLE IS CRACKED. REMOVED AND INSTALLED NEW ANGLE IAW SRM 51-42-21. PAINTED ANGLE IAW SRM 51-25-16.Sep 27, 2010 · N905EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001457Cap · missingEMERGENCY EXIT SIGN REF CAP IN CABIN CEILING IS MISSING. REINSTALLED RED END CAP FOR EXIT SIGN REF AMM 33-51-14. (CLOSED)Sep 27, 2010 · N937EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201001458Angle · crackedLT ANGLE UNDER CARGO DOOR SILL AT FS 605.00, LBL 43, HAS CRACK IN RADIUS. REMOVED LT ANGLE AT FS 605.00 IAW SRM 51-42. LT ANGLE REQUIRES LOCATING, DRILLING OF HOLES AND INSTALL. ANGLE BRACKET, PN 601R35011-13 AT FS 605.0 LBL 43 LOCATED, DRILLED AND INSTALLSep 27, 2010 · N970EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001459Floorbeam · crackedFOUND CRACK ON FLOORBEAM UPPER FLANGE LAST OTBD FASTENER HOLE AT FS 574.00 LBL 45. REPAIRED IAW REO 601R-53-61-3846.Sep 27, 2010 · N970EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001460Floorbeam · corrodedCARGO BAY FLOORBEAM CAP AT LBL 27 OTBD FROM FS 574 TO FS 621 HAS CORROSION AROUND NUTPLATES.Sep 27, 2010 · N970EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001461Web · crackedPAX DOOR FWD WEB HAS CRACK APPROX .4" FROM EDGE TO CTR OF RADIUS ON VERTICAL SURFACE, UNDER FIRST FIXED STEP APPROX 2.1" FROM INNER DOOR SKIN SURFACE. COMPLIED WITH STEPS 1 AND 2 OF REO 601R-52-11-1873. CUT OUT DAMAGED AREAS PAX DOOR FWD SIDE PANEL BOTTOM STSep 27, 2010 · N970EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001462Lamp · burned outRT NR2 EXTERNAL EMERGENCY LIGHT INOP. RELAMPED RT NR2 EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD. RELAMPED RT NR 2 EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD.Sep 27, 2010 · N979EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201001463Sill · crackedCLIP CRACKED UNDER CARGO DOOR SILL AT FS 605.0. REMOVED DAMAGED CLIP AT FS 6050 AND DRILLED UP NEW SERVICEABLE PART IAW SRM 51-42-21 AND 51-42-06. INSTALLED NEW CLIP AT FS 605.0 IAW SRM 51-42-21.Sep 27, 2010 · N980EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001464Sill · crackedCLIP CRACKED UNDER CARGO DOOR SILL AT FS 589.0. REMOVED DAMAGED CLIP AT FS 589 AND DRILLED UP NEW SERVICEABLE PART IAW SRM 51-42-20 AND 51-42-06. INSTALLED NEW CLIP AT FS 589.0 IAW SRM 51-42-21.Sep 27, 2010 · N980EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001465Seat Track · corrodedCARGO SEAT RAIL AT FUSELAGE STA 559+80 AND LBL 27 HAS CORROSION. REMOVED AND INSTALLED NEW TRACK SEGMENT AT STA 559 + 80 IAW AMM 53-01-11.Sep 27, 2010 · N980EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001466Seat Track · corrodedCARGO COMPT SEAT RAIL JUST AFT OF FUSELAGE STA 559+80 AT LBL 9 HAS CORROSION. EVALUATED, FOUND CORROSION OUT OF LIMITS IAW SRM 53-21-49 AND 53-61-49. R & R SEAT RAIL SECTION IAW AMM 53-01-11.Sep 27, 2010 · N980EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001467Seat Track · corrodedCARGO COMPT SEAT RAIL JUST AFT OF FUS STA 559+80 AT RBL 9 HAS CORROSION. FOUND CORROSION OUT OF LIMITS IAW SRM 53-21-49 AND 53-61-49. R & R SEAT RAIL SECTION IAW AMM 53-01-11.Sep 27, 2010 · N980EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001468Seat Track · corrodedCARGO COMPT SEAT RAIL JUST AFT OF FS 559+80 RBL 27 HAS CORROSION. DRILLED NEW SEAT TRACK & INSTALLED IAW AMM 53-01-11-400-802 M1417. INSTALLED FITTING IAW AMM TASK 25-41-01-400-806, SUBTASK 25-41-01-869-007.Sep 27, 2010 · N980EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001469Seat Track · corrodedCARGO COMPT SEAT RAIL AT STA 559+112 LBL 9 HAS CORROSION. FOUND CORROSION OUT OF LIMITS IAW SRM 53-21-49 AND 53-61-49. R & R SEAT RAIL SECTION IAW AMM 53-01-11.Sep 27, 2010 · N980EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001486Seat Track · corrodedALL 6 CARGO BAY SEAT TRACKS ARE CORRODED. TREAT, PRIME, PAINT AND INSTALL TRACKS -49 AND -5 REQUIRED. TREATED PARTS IAW SRM 51-21-11, PRIMED PARTS IAW SRM 51-21-06, TOPCOAT PART IAW SRM 51-25-16 & INSTALLED -49 AND -5 PARTS IAW AMM 20-21-00-910-801 & REO 601Sep 27, 2010 · N823AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001516Floor Support · corrodedFLOORBEAM HAS MINOR CORROSION AT LBL 27 BETWEEN FS 574.0 AND FS 621.0 AS MARKED. REMOVED NUT PLATES FROM FLOORBEAM CAP AT LBL27 AND FS576. 579, 585, 591, 597, 603,609 BLENDED CORROSION OUT OF LIMITS AT 5 LOCATIONS REF SRM 51-21-06. REPLACED LBL27 FLOORBEAM CSep 27, 2010 · N980EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001448Bulb · burned outREFR TO DMIL 560491-3 LIGHT BULB BURNED OUT IN EMERGENCY LIGHT FLOOD FIXTURE BY CABIN DOOR. R & R EMERGENCY FLOOD LIGHT BULB IAW AMM 33-51-01, DMIL CLEARED, PLACARD REMOVED.Sep 25, 2010 · N852AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001439Lamp · brokenRT EXTERIOR NR 2 EMERGENCY LIGHT INOP. RELAMPED RT EXTERIOR NR2 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. RELAMPED RT EXTERIOR NR2 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.Sep 24, 2010 · N684BR · Cndair CL6002B19 · Emergency LightingSDR ASOA201001440Floorbeam · crackedFS 280, AFT FLOOR SUPPORT ANGLE IS CRACKED OTBD OF RBL 9 AND LBL 9 & CORRODED ON TOP SIDE ALONG BULKHEAD AT RBL 9 AND LBL 9. FS 280 BULKHEAD WEB IS CRACKED BELOW FLOOR OTBD OF RBL 9 AND LBL 9. FS 280 FLOOR SUPPORT CLIPS ARE CRACKED INBD AND OTBD AT LBL 9 ANSep 24, 2010 · N970EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001442Bulb · burned outLIGHT BULB BURNED OUT IN EMERGENCY LIGHT FLOOD FIXTURE BY CABIN DOOR ( CABIN EMERGENCY LIGHTS: FLOOR LEVEL EMERGENCY FLOODLIGHTS (ACFT WITH PHOTOLUMINESCENT FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYS STRIP/TAPE) R & R EMERGENCY FLOOD LIGHT BULB IAW AMMSep 24, 2010 · N852AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001443Attach Fitting · corrodedCLIP AT FS 336 ON BOTTOM OF PAX DOOR IS CORRODED. R & R CORRODED CLIP IAW SRM 51-40-11, 51-42-06, AND 51-42-21 SEE FORM 412 FOR FABRICATION AND INSTALLATION DETAILS.Sep 24, 2010 · N925EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001445Attach Fitting · corrodedCLIP AT FS 321 ON BOTTOM OF PAX DOOR IS CORRODED. R & R CORRODED CLIP IAW SRM 51-40-11, 51-42-06, AND 51-42-21. SEE FORM 412 FOR FABRICATION AND INSTALLATION DETAILS.Sep 24, 2010 · N925EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001446Intercostal · crackedINTERCOSTAL CRACKED RT OVERWING BELOW EMERGENCY EXIT FWD SIDE RT. REMOVED INTERCOSTAL AT FS 449.85 BELOW RT EMERGENCY EXIT IAW SRM 51-42-06. DRILL AND INSTALL NEW SERVICEABLE INTERCOSTAL. FABRICATED NEW PART FROM S6144-33. EXTRUDED ANDGLE IAW STEP 1 OF RE0 6Sep 24, 2010 · N980EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001485Stringer · corrodedSTRINGER 26L BETWEEN FS 349 AND 333 HAS HAS MATERIAL LOSS OF 50 PERCENT FROM CORROSION. RT SPLICE REQUIRES LOCATE/DRILL AND BOTH LT AND RT SPLICE ANGLES REQUIRE INSTALL. PERFORMED EDDY CURRENT INSP ON THE CUT LINES OF STRINGER 26L AT FS 302.5. NO INDICATIONSep 24, 2010 · N846AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR REXA201000157Step · puncturedPUNCTURE IN THE PASSENGER STEP SURFACE WAS FOUND ON THE SECOND STEP FROM THE TOP (WITH DOOR IN OPEN POSITION). THE PENETRATION MEASURES APPROX 0.50 INCH DIAMETER AND IS LOCATED AT THE INBD EDGE OF THE STEP 4.75 INCHES FWD OF THE AFT EDGE. A VISUAL CHECK FROM TSep 23, 2010 · N801AY · Cndair CL6002B19 · Passenger/Crew Doors
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