GE CF34 series

Service difficulty reports · 1,368

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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 = 'CF34'
  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 ASOA201001657Sill · corrodedRT FLOOR SUPPORT SILL CORRODED AT AFT OF FS 349.00. REMOVED CORROSION ON SILL IAW SRM 51-21-06. FOUND WITHIN LIMITS IAW SRM 53-00-00.Oct 25, 2010 · N868AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001658Floorbeam · crackedFS 280, RBL 9, OTBD FLOOR SUPPORT ANGLE CRACKED. FLOOR ANGLE REPLACED ON MWC 8747421.Oct 25, 2010 · N868AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001659Floorbeam · crackedFS 280, RBL 9 INBD FLOOR SUPPORT CLIP CRACKED. REPLACED ON MWC 8747421 OP 356.Oct 25, 2010 · N868AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001660Floorbeam · crackedFS 280, LBL 9, INBD FLOOR SUPPORT CLIP CRACKED. FLOOR SUPPORT CLIP REPLACED ON MWC 8747421 OP 356.Oct 25, 2010 · N868AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001661Floorbeam · crackedFS 280, LBL 9, OTBD FLOOR SUPPORT CLIP CRACKED. FLOOR SUPPORT CLIP REPLACED ON MWC 8747421 OP 356.Oct 25, 2010 · N868AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001662Angle · corrodedFS 280, J-ANGLE PREVIOUS REPAIR BETWEEN LBL 9 AND RBL 9 CORRODED. REPLACED FS 280 J-ANGLE ON MWC 8747421 OP 356.Oct 25, 2010 · N868AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001663Floor Support · corrodedFLOOR SUPPORT ANGLE AT FS 319.70 JUST INBD OF FWD SERVICE DOOR LWR CORNER CORRODED. REMOVED CORROSION IAW SRM 51-21-06, FOUND WITHIN LIMITS IAW SRM 53-00-00.Oct 25, 2010 · N868AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001664Skin · crackedFUSELAGE SKIN ON RT SIDE FOR NLG SPADE DOOR IS CRACKED IN CORNER. COMPLIED WITH EC/TC REO 601R-53-11-0048 IAW REO 601R-53-11-0048, REV FOUND TO BE SATISFACTORY.Oct 25, 2010 · N868AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA201001665Floor Support · corrodedFLOORBEAM CAP AT LBL 27 FROM FS 621 TO 574 IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06 AND 53-00-00. LOCATED AND DRILLED IAW SRM 51-42-06, 51-42-21 AND REO 601R-53-61-3778.Oct 25, 2010 · N868AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001666Intercostal · corrodedINTERCOSTAL CAP AT FS 589 BETWEEN LBL 18 & 27 IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06 AND 253-00-00. INTERCOSTAL CAP REQUIRES REPLACEMENT. REMOVED INTERCOSTAL CAP IAW SRM 51-42-06 AND 51-42-21. INTERCOSTAL CAP REQUIREOct 25, 2010 · N868AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001667Floorbeam · corrodedFLOORBEAM CAP AT LBL 9, FS 605 IS CORRODED. REMOVED CORROSION FROM FLOORBEAM CAP. DEEPEST MATERIAL LOSS AT 0.012 DEEP X 0.75" W X 0.50" L AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06, 53-00-00, 53-61-43. REMOVED FLOORBEAM CAP BETWEEN FS 570 AND FS 621 IAW SOct 25, 2010 · N868AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001668Floor Support · corrodedFLOOR SUPPORT OTBD OF RBL 36 IS CORRODED FROM FS 621 TO 559+80. BLENDED CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, FIG 102. REMOVED FLOOR SUPPORT. LOCATED NEW . INSTALLED IAW SRM 51-42-06 AND 51-42-21.Oct 25, 2010 · N868AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040942Bearing · out of toleranceREPLACE MIDDLE (UPPER & LOWER) RUDDER HINGE BEARINGS ON ACFT WITH RUDDER PN 601R22014-1. R & R BEARINGS.Oct 24, 2010 · N448AW · Cndair CL6002B19 · Rudder StructureSDR ASOA201001644Door · bindingSERVICE DOOR CAN NOT BE OPENED FROM OUTSIDE, REPORTED BY RAMP AGENT. INSPECTED & C/W OPS CK OF SERVICE DOOR NO DEFECTS FOUND IN REF TO AMM CHAP 52-41-00.Oct 23, 2010 · N823AS · Cndair CL6002B19 · Service DoorsSDR A6WA201040795Fire · detectedAPU FIRE AT GATE FIRE BOTTLE. APU DID NOT FIRE IN THE CONTAINMENT AREA THIS FIRE WAS BY GROUND CREW FROM EXHAUST NO FIRE WARNING OCCURRED FOR INSP, MEL.Oct 23, 2010 · N427ZW · Cndair CL6002B19 · APU Core EngineSDR A6WA201040855Shaft · dentedLT INBD VANE ACTUATOR SHAFT DENTED FROM ROLLERS. EXCESSIVELY BLENDED ACTUATOR SHAFT FOUND TO BE WITHIN LIMITS IAW BA REO 601R-57-52-1640.Oct 23, 2010 · N453AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA201040783Pdu · malfunctioned"LT REV UNLOCKED" CAUTION MSG IN FLIGHT. FOLLOWED QRH PROCEDURES. NO CHANGE TO AC HANDLING CHARACTERISTICS. DID NOT SHUTDOWN ENGINE. DIVERTED. IN FLT LANDING WEIGHT CALCULATED AT 46990. R & R LT THRUST REVERSER PDU IAW AMM 78-32-03. OPS CHECK GOOD, REMOOct 23, 2010 · N413AW · Cndair CL6002B19 · Engine Thrust ReverserSDR QXEA2010102100662Floorbeam · corrodedC4 CHECK - AVIONICS FLOORBOARD SUPPORT ANGLE AT FS 280.00 IS CORRODED. REMOVED CORRODED FLOORBOARD SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. ANGLE CORRODED THROUGHOUT. LOCATED HOLES IN NEW FLOORBOARD SUPPORT ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED Oct 21, 2010 · N617QX · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR A6WA201040859Fitting · crackedBATHTUB FITTING AT RBL9, FS 461 CRACKED PN 600-31068-19. REPLACED BATHTUB FITTING WITH SERVICEABLE FITTING IAW SRM 51-42-21, 51-42-06.Oct 21, 2010 · N453AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR QXEA2010102100659Buttstrap · corrodedC4 CHECK - DURING INSP FOUND CORROSION ALONG FS 280 BUTTSTRAP BETWEEN STR 26L AND 26R. REMOVED FASTENERS FOM IAW SRM 51-42-06-001-001-A01. BLENDED CORROSION BETWEEN STRINGERS, ORIGINAL THICKNESS .100, BLENDED .008 MATERIAL FROM STRAP, REMAINING MATERIAL THICOct 20, 2010 · N617QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR A6WA201040860Attach Fitting · crackedLT OTBD 484.00 CLIP CRACKED. FATRICATED CLIP AND INSTALLED SERVICEABLE CLIP IAW REO 601R-53-41-059, REV B.Oct 20, 2010 · N453AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR V0XR413Y101910002Angle · corrodedPASSENGER DOOR MID CAP ANGLE AT STR 18L IS CORRODED BEYOND LIMITS. R & R PASSENGER DOOR MID CAP ANGLE STR 18L IAW SRM 51-41-02.Oct 19, 2010 · N152GJ · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XR413Y101910003Gusset · corrodedMAIN CABIN RT FUS FLOOR LEVEL STA 280 GUSSET IS CORRODED OUT OF LIMITS. R & R RT GUSSET AT 280 RT SIDE IAW SRM 51-42-6.Oct 19, 2010 · N152GJ · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XR413Y101910004Crossbeam · crackedBS 280 CROSSBEAM CRACKED. REPLACED CROSSBEAM STA 280 IAW REO 670-53-11-047, REV E.Oct 19, 2010 · N152GJ · Cndair CL6002C10 · Fuselage Main, StructureSDR A6WA201040854Intercostal · crackedUPPER AFT INTERCOSTAL ON PAX DOOR IS CRACKED. REPLACED CRACKED INTERCOSTAL DOUBLER WITH NEW SERVICEABLE PN 601R318094-2, IAW SRM 51-40-11, 51-42-06.Oct 19, 2010 · N453AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR QXEA2010101900638Attach Angle · corrodedC4 CHECK - DURING INSP, FOUND CORROSION ON STR 26R ATTACH FLANGE JUST AFT OF FS 333.00. REMOVED CORROSION ON STR 26R EXTENSION ANGLE ATTACH FLANGE IAW SRM 51-21-06-001-001-A01. NO MATERIAL REMAIN AFTER BLENDING OF CORROSION. REMOVED RIVETS IN THE EXTENSION Oct 18, 2010 · N617QX · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR QXEA2010101900639Frame · corrodedC4 CHECK - CORROSION FOUND ON FRAME AT FS 310.00 BETWEEN STR 27 AND 26R. REMOVED FASTENERS FOM IAW SRM 51-42-06-001-001-A01. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. AREA WITHIN LIMITS IAW SRM 53-21-06-101-002-A01. PERFORMED ECI ON BLENDED AREA , NO Oct 18, 2010 · N617QX · Cndair CL6002C10 · Fuselage Main, FrameSDR QXEA2010102200666Hinge · crackedDURING INSP OF LT MLG INBD DOOR FOUND CRACK IN FWD HINGE AREA. (MLG INBD DR PN CC670-10520 ). PLACED ON CDL C-32-12A. RETURNED TO SERVICE.Oct 18, 2010 · N601QX · Cndair CL6002C10 · Landing Gear DoorsSDR QXEA2010101900640Skin · gougedC4 CHECK - RT INBD SLAT HAS 2 GOUGES ON LOWER T/E. BLENDED INBD GOUGE AT WS 68.00 AND OTBD GOUGE AT WS 78.00 IAW SRM 51-12-00-001-001-A01. INBD GOUGE MEASURES 2.154"L X .151"W X .031"D, OTBD GOUGE MEASURES 1.981"L X .134"W X .021"D. REMAINING MATERIAL FOR IOct 16, 2010 · N617QX · Cndair CL6002C10 · Leading Edge DevicesSDR ASOA201001579Cover · crackedEMERGENCY EXIT LIGHT COVER CRACKED AT SERVICE DOOR (GALLEY ACCESS PANEL). (OPEN)Oct 15, 2010 · N709EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201001580Lens · crackedBOTH EMERGENCY EXIT LIGHT LENS COVERS CRACKED ON WARDROBE AT ASD ENTRANCE. ( OPEN )Oct 15, 2010 · N709EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201001581Cover · brokenEMERGENCY LIGHT COVER ON WALL NEAR MAIN DOOR BROKEN. REPLACED EMERGENCY FLOOR LEVEL LIGHT ASSY IAW AMM 33-51-19. OP'S CHECKS GOOD. (CLOSED)Oct 15, 2010 · N837AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001582Floorbeam · crackedFS 280, CLIPS AT RBL 9 AT INBD AND OTBD SIDE OF THE FLOORBEAM ARE CRACKED. REMOVED 2 EA CLIPS AT RBL 9 INBD AND OTBD SIDE OF FLOORBEAM AND REPLACED WITH NEW SERVICEABLE ONES IAW SRM 51-42-06 AND 51-42-21. (CLOSED)Oct 15, 2010 · N934EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001583Attach Angle · crackedFAIRLEAD INTERCOSTAL CLIP AT RBL 27 FS 484.00 IS CRACKED. REPAIRED PANEL 282AZ IAW MM 25-52-21, STEPS B1-8. NEEDS 1559A/B APPLIED. APPLIED 1559A/B IAW CMM 25-52-21 STEPS 9 AND 10. (CLOSED)Oct 15, 2010 · N934EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201001584Bulkhead · cracked2 EA CRACKS 1.5" LONG ON FS 280 BULKHEAD 3' FROM FLOOR STRUCTURE. (OPEN)Oct 15, 2010 · N934EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201001585Placard · tornPAX DOOR OPEN/EXIT, AND ASSIST PLACARDS ARE TORN. (OPEN)Oct 15, 2010 · N971EV · Cndair CL6002B19 · Placards and MarkingsSDR QXEA2010101900624Sill · damagedC4 CHECK - DURING INSP FOUND CORROSION AND RUB MARKS ON AFT BAGGAGE BAY DOOR OPENING LOWER SILL IN NUMEROUS AREAS FROM FS 1000-1047.00. CLEANED AND BLENDED AREAS WITH CORROSION AND RUB MARKS IAW SRM 51-21-06-001-001-A01 AND 51-12-00-001-001-A01. FOUND TO BE Oct 15, 2010 · N617QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR QXEA2010101900654Unknown · unknownCLIMBING THROUGH 25,500 WITH SPEED AT 290 KTS. SELECTED, THE SELECTED SPEED ROLLED BACK TO 270K. RETURNED TO THE FIELD, LANDING UNEVENTFUL. COMPLIED WITH SL REV E. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.Oct 15, 2010 · N606QX · Cndair CL6002C10 · Auto Flight SystemSDR ASOA201001570Bulkhead · crackedWHILE PERFORMING AWL2 53-41-124, FOUND A SUSPECT CRACK LOCATED AT FS 409+128 PRESSURE BULKHEAD FWD FACE COMING FROM LOWER EDGE OF THE INBD U CHANNEL AT LBL 27.00. CRACK GOES UP AND PAST FIRST LOWEST FASTENER HOLE (BUT NOT PAST THE NEXT FASTENER HOLE UP) THAT AOct 14, 2010 · N881AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR QXEA2010101500616Seat Track · corrodedC4 CHECK - DURING INSP FOUND CORROSION ON RT FLOOR SEAT TRACK AT FS 349-485. CORROSION FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED BAD SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.Oct 14, 2010 · N617QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2010101500617Seat Track · corrodedC4 CHECK -DURING INSP FOUND CORROSION ON LT FLOOR SEAT TRACK AT FS 597-677.00. CORROSION FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED BAD SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.Oct 14, 2010 · N617QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001577Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE IS CRACKED. (OPEN)Oct 14, 2010 · N934EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR N6WA20101001Crossbeam · crackedFS280 CROSSBEAM IS CRACKED. REPAIRED CROSSBEAM 280.00 IAW REO 670-53-11-047, REV E.Oct 13, 2010 · N152GJ · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201001574Angle · corrodedPAX DOOR SILL IS CORRODED ADJACENT TO CONNECTOR J1MB, FLANGES ON HANDRAIL SUPPORT STOW CUPS AND AROUND NUT CLIPS. REMOVED PAX DOOR SILL CTR CAP ANGLE IAW SRM 51-42-12. REMOVED SILL ANGLE PN 601R31527-221 IAW SRM 51-41-02, 51-42-06, 51-42-13, AND 51-42-21. LOOct 13, 2010 · N905EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001572Placard · wornPAX DOOR "EXIT", "OPEN" & DIRECTIONAL PLACARDS WORN. (OPEN)Oct 12, 2010 · N981EV · Cndair CL6002B19 · Placards and MarkingsSDR ASOA201001573Seat Track · corrodedALL 7 CARGO SEAT TRACKS HAVE CORROSION. REMOVED DISCREPANT CARGO SEAT TRACKS AND INSTALLED NEW SERVICEABLE SEAT TRACKS IAW SRM 51-41-04. (CLOSED)Oct 12, 2010 · N981EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001733Floorbeam · corrodedFS 349.00 BETWEEN RBL 9.00 AND RBL 18.00 FLOORBEAM HAS 1EA BROKEN AND CORRODED SCREW. R & R NUTPLATE AND SCREW IAW SRM CH 51-42-15-001-001. (CLOSED)Oct 12, 2010 · N709EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR A6WA201040853Panel · crackedLEFT THRUST REVERSER 4 O`CLOCK SAM PANEL SUPPORT ON TORQUE BOX CRACKED AT MOUNTING FLANGE. REPAIRED CRACKED FLANGE ON LT T/R AT 4 O`CLOCK POSITION BY REMOVING DAMAGED PORTION, FABRICATING & INSTALLING REPAIR DOUBLER AND FILLER IAW REO 601R-78-30-4013.Oct 12, 2010 · N451AW · Cndair CL6002B19 · Engine Thrust ReverserSDR ASOA201001643Stringer Splice · corrodedREMOVED STRINGER SPLICE 25R AT FS 333 IAW SRM 51-42-06-001-001-A01. SPLICE WAS REMOVED AND FOUND TO BE CORRODED A SPLICE ORDERED AND RECEIVED. LOCATED AND DRILLED EXISTING HOLES IN NEW STRINGER SPLICE. INSTALLED NEW STRINGE SPLICE WET IAW SRM 51-42-06-00Oct 11, 2010 · N709EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201001731Floorbeam · corrodedLIGHT CORROSION ON THE FLOOR SUPPORT CHANNEL WHICH IS MOUNTED TO FS 280 FRAME BETWEEN STGR 26L AND 26R. R & R FLOORBOARD SUPPORT ANGLE AT FS280 BETWEEN STGR 26L AND 26RT PN CC670-34-256-3 IAW SRM 53-11-10-991-803 AND 51-42-06-001-001-A01 AND REAPPLIED A023 FIOct 11, 2010 · N709EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
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