GE CF6-50C2

Service difficulty reports · 719

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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 = 'CF650C2'
  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 WRLA2006059Floor Support · corrodedITEM: DURING "C" IN GSO FOUND FLOOR SUPPORT IN MAIN CABIN HAS CORROSION AT STA 879 RBL60. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-31-01 VOL II.Aug 4, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006040Floor Support · corrodedITEM: DURING "C" CHECK IN GSO FOUND MAIN CABIN FLOOR PANEL NR 224AF SUPPORT CORRODED BEYOND LIMITS. REMOVED AND REPLACED SUPPORT IAW WITH SRM 51-31-01 VOL II.Aug 3, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006046Longeron · corrodedITEM: DURING "C" CHECK FOUND AT STA 1521 LONGERON 46L HAS EXFOLIATION AND HEAVY PITTING CORROSION. FABRICATED NEW REPAIR ANGLE AND CHANNEL, INSTALLED PER SRM CHAP 51 VOL II.Aug 3, 2006 · N14075 · Doug DC1030 · Fuselage Main, Longeron/StringerSDR WRLA2006047Floor Support · corrodedITEM: DURING "C" IN GSO FOUND MAIN CABIN BETWEEN STA 808 TO 899 FLOOR SUPPORT AT APPROX RBL 46 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-31-01 VOL I.Aug 3, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20060019Blades · brokenDURING TAKEOFF ROLL NR 3 ENGINE EGT INDICATOR SHOWS RAPID EGT RISE AT TEMP 945 DEGREES AMBER LIGHT CAME ON AND TEMP EXCEEDED 950 DEGREES AND KEPT RISING. F/E REDUCED THRUST NR 3 ENGINE TO PREVENT OVERTEMP AND WHEN DIFFERENCE BETWEEN N1, NR3 ENGINE AND OTHERS RAug 3, 2006 · N270AX · Doug DC1030 · Turbine SectionSDR XN0A1347Engine · unknownFLIGHT LEVEL 290 MACH .75 COULD NOT MAINTAIN SPEED OR FLIGHT LEVEL, ENGINE AI WAS ON. AC SHOULD BE ABLE TO MAINTAIN MACH .78 WITH N1 OF 98.4 FLIGHT LEVEL 280 M72. TAT 05 SAT-31. LOOKED OUT BOTH OVERWING WINDOWS AND NO ICE NOTED. PERFORMED ENGINE IDLE RUN NR 1Aug 2, 2006 · N473AS · Airbus A300B4203 · Engine (Turbine/Turboprop)SDR WRLA2006049Floor Support · corrodedITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT CHANNEL HAS SURFACE CORROSION AT STA 1887 RBL50. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-33-01 VOL II.Aug 2, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006051Floor Support · corrodedITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT CHANNEL HAS SURFACE CORROSION AT STA 1900 LBL28-LBL53. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-33-01 VOL II.Aug 2, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006052Floor Support · corrodedITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT CHANNEL HAS SURFACE CORROSION AROUND NUT PLATE CLIP HOLES AT STA 1900 LBL22-RBL22. REMOVED AND REPLACED FLOOR SUPPORT CHANNELS IAW SRM 51-31-01 VOL II.Aug 2, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006058Floor Support · corrodedITEM: DURING "C" IN GSO FOUND FLOOR SUPPORT IN MAIN CABIN HAS SURFACE CORROSION AT STA899 RBL60. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-31-01 VOL II.Aug 2, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006060Floor Support · corrodedITEM: DURING "C" IN GSO FOUND FLOOR SUPPORT IN MAIN CABIN HAS CORROSION AT STA 824 RBL60. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-31-01 VOL II.Aug 2, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20060018Manifold · crackedDURING THE TAKEOFF ROLL NR 3 ENG EGT BEGAN TO CLIMB ABOVE 950 DEGREES. THE ENGINEER PULLED NR 3 THROTTLE BACK ATTEMPTING TO BRING NR 3 EGT INTO LIMITS, THE CORRESPONDING DROP IN N1 WAS ALREADY AT 5 PERCENT LESS THAN THE N1 LIMIT AND THE EGT WAS STILL EXCEEDINAug 2, 2006 · N270AX · Doug DC1030 · Engine Cooling SystemSDR ARWA20060801Pump · unknownNR 2 ENGINE WOULD NOT SPOOL UP ON THE RUNWAY. REMOVED AND REPLACED NR 2 ENGINE MEC/FUEL PUMP PACKAGE IN ACCORDANCE WITH M/M 73-45-01 AND M/M 73-20-01; FOUND NORMAL ON ENGINE RUN-UP IN ACCORDANCE WITH M/M 71-00-00.Aug 2, 2006 · N68041 · Doug DC1010 · Fuel Control/Turbine EnginesSDR WRLA2006017Spar Cap · damagedDURING "C" CHECK IN SAT, AIRCRAFT SUSTAINED AN IMPACT DAMAGE TO LT HORIZONTAL STAB FWD SPAR CAP UPPER CHORD AREA, DIRECTLY ABOVE THE FOURTH (FROM INBD) ACCESS HOLE IN FWD SPAR. DAMAGE LENGTH IS APPROX 11.0" LONG. REMOVED DAMAGE FROM HORIZONTAL STAB FWD SPAR Aug 1, 2006 · N303 · Doug DC1030F · Horizontal Stabilizer, Spar/RibSDR WRLA2006045Frame · corrodedITEM: DURING "C" CHECK IN GSO FOUND LEFT WHEEL WELL STA 1510 FRAME CORRODED ON LOWER LEG. FORMED NEW FRAME IAW DAC DWG AEA7165 REV K. INSTALLED NEW FRAME SECTION IAW SRM 53-00-01 VOL I.Aug 1, 2006 · N14075 · Doug DC1030 · Fuselage Main, FrameSDR WRLA2006018Skin · damagedDURING "C" CHECK IN SAT, CENTER CARGO DOOR CUTOUT AT FS 1781 BELOW STR 42 AT EXISTING REPAIR DOUBLER AND EXISTING A/C SKIN STRUCTURE HIT AND PUSHED INTO FRAME 1781 (LOWER T/E OF DOOR CUTOUT). REMOVED HEATER TUBES FROM AFT TQ BOX FS 1781-1787 BETWEEN 538R-542RJul 31, 2006 · N303 · Doug DC1030F · Fuselage Main, Plate/SkinSDR WRLA2006035Floorbeam · corrodedDURING "C" CHECK IN SAT FOUND EXFOLIATED CORROSION AT FLOOR BEAM IN STA 1781 RBL 57 (CORROSION ON AFT WEB OF BEAM). FABRICATED BEAM REPAIR SECTION. TREATED,PRIMED AND INSTALLED REPAIR PARTS IAW SRM 53-00-01 FIG 9.Jul 31, 2006 · N303 · Doug DC1030F · Fuselage Main, Floor BeamSDR WRLA2006055Floor Support · corrodedITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT ANGLE HAS SURFACE CORROSION AT STA 1986 LBL14. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-31-01 VOL II.Jul 28, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006025Doubler · corrodedDURING C3 CK, FOUND CORROSION ON DOUBLER IN RT WHEEL WELL STA 1520-1500. FAB NEW DOUBLER.Jul 26, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006026Fitting · corrodedDURING C3 CK, FOUND CORROSION ON RT W/W FITTING, STA 1505 B/N LONG 44 AND 45. REPLACE SUPPORT FITTING.Jul 26, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006032Plate · corrodedDURING "C" CHECK IN SAT FOUND NR 1 ENG LEFT FAN COWL CENTER U BOLT PLATE HAS FRETTING CORROSION. REMOVED CORROSION FROM BOLT PLATE, MATERIAL LOSS WAS 0.030 FOUND TO BE OUT OF LIMITS IAW DC10 SRM 51-00-01 FIG 1A. FABRICATED NEW BOLT PLATE, TREATED AND PRIMED. Jul 26, 2006 · N303 · Doug DC1030F · Nacelle/Pylon, Main FrameSDR WRLA2006057Floor Support · corrodedITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT CHANNEL HAS CORROSION AT STA 1913 - 2007 LBL24. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT CHANNEL IAW SRM 51-31-01 VOL II.Jul 26, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006021Support · corrodedDURING C3 CK IN GSO, FOUND CORROSION R MLG MOST AFT ACCESS SUPPORT IS CORRODED. SPLICE NEW EXT ANGLE REPAIR.Jul 25, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006022Bulkhead · corrodedDURING C3 CK, FOUND CORROSION IN MAIN CABIN AFT PRESSURE BULKHEAD UNDER SPLICE ANGLE LOWER CORD. REMOVED AND REPLACED T CHORD DC10 SRM 51-31-01 VOL II.Jul 25, 2006 · N14075 · Doug DC1030 · Fuselage Main, BulkheadSDR WRLA2006036Repair · misinstalledLEFT FUSELAGE SKIN BETWEEN STA 515-535 LONG 28 TO LONG 32 HAS A SKIN SPLICE REPAIR WITH 3EA FREEZ PLUGS INSTALLED, REQUEST TO INSTALL EXTERNAL REPAIR DOUBLER THAT WAS REMOVED, MATERIAL THIKNESS .090. FABRICATED DOUBLER PER EA 010-5320-11-A0302. TREATED, PRIMEJul 24, 2006 · N303 · Doug DC1030F · Standard Practices/StructuresSDR WRLA2006033Rub Strip · corrodedDURING "C" CHECK IN SAT FOUND NR 1 ENG LT CORE COWL FWD RUB STRIP AND RH CORE COWL AFT RUB STRIP HAVE CORROSION. REMOVED & REPLACED NR 1 ENG LT CORE COWL FWD RUB STRIP FROM 6 TO 12 O'CLOCK POSITION AND REMOVED & REPLACED RT CORE COWL AFT RUB STRIP FROM 3 TO 6Jul 23, 2006 · N303 · Doug DC1030F · Nacelle/Pylon, Main FrameSDR WRLA2006034Access Panel · corrodedDURING "C" CHECK IN SAT FOUND LEFT WING I/B T/E ACCESS PANEL 541CR HAS THREE AREAS OF CORROSION. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01 IN ALL THREE AREAS. FABRICATED REPAIR DOUBLERS AND BONDED THE 3 AREAS IAW SRM 51-71-00. SEALED AND PRIMED REPJul 23, 2006 · N303 · Doug DC1030F · Wing, Plate/SkinSDR WRLA2006044Support Channel · corrodedITEM: DURING "C" CHECK IN GSO FOUND LAV SUPPORT CHANNEL CORRODED ON UPPER SURFACE STA 859 LBL70. CORROSION FOUND TO BE OUT OF LIMITS, REMOVED & REPLACED SUPPORT CHANNEL IAW DC10 SRM.Jul 23, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006030Skin · corrodedDURING "C" CHECK IN SAT FOUND RIGHT WING NR 4 SPOILER HAS LIGHT CORROSION IN SEVERAL AREAS ON UPPER SURFACE. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01 FIG 1A, REMOVED DAMAGED AREA AND CLEANED SURFACE IAW SRM 51-71-00 PAR 4, FABRICATED REPAIR PARTS, Jul 22, 2006 · N303 · Doug DC1030F · SpoilersSDR WRLA2006027Fitting · corrodedDURING C3 CK, FOUND CORROSION ON LT WHEEL WELL AT STA 1509 INBOARD FITTING. REMOVE AND REPLACE FITTING.Jul 21, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006031Nose Cowl · crackedDURING "C" CHECK IN SAT FOUND NR 1 ENG NOSE COWL UPPER RH INNER ACOUSTICAL PANEL LOWER FWD CORNER HAS A COMBINATIONOF CRACK .7" CIRCUMFERENTIAL THAT EXTENDS BEYOND 2 FASTNERS AND .6" LONGITUDINAL AND CORROSION. DAMAGE FOUND TO BE TOO EXCESSIVE PER DC10 SRM VOLJul 21, 2006 · N303 · Doug DC1030F · Nacelle/Pylon, Main FrameSDR WRLA2006023Tee Fitting · corrodedDURING C3 CK, FOUND CORROSION ON TEE CHORD AT L43 LT WHEEL WELL, STA 1521. REMOVE CORROSION AND REEVALUATE, AND GENERATE RFTS FOR REPAIR. FASTENERS REQ'D REMOVAL.Jul 20, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006067Floor Support · corrodedDURING C-CHECK IN GSO FOUND MAIN CABIN AT APPROX STA 430, AT RBL 10, FLOOR SUPPORT CORRODED. RECEIVED FLOOR SUPPORT P/N ABA8225-503 PO 541338, REMOVED OLD SUPPORT. LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-31-01 VOL II. INSTALLED FLOOR SUPPORT AND DOOR JAMJul 18, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006068Floorbeam · corrodedDURING C-CK IN GSO FOUND FLOORBOARD ATTACH ANGLE CORRODED IN MAIN CABIN AT STA 395 BELOW THE COCKPIT DOOR. FLOORBOARD ATTACH ANGLE REMOVED AND REPLACED WITH NEW P/N BAC1503-4162 EXTRUSION 7075-T6105111 (PO 541368.1) IAW DC 10 SRM 51-31-01 VOL II.Jul 18, 2006 · N14075 · Doug DC1030 · Fuselage Main, Floor BeamSDR WRLA2006069Floorbeam · corrodedDURING C-CK IN GSO FOUND FLOORBEAM CORRODED IN MAIN CABIN AT STA 495 AT APPROX RBL 56. REPLACED FLOOR SUPPORT IAW CAB DWG ACA 7364 AND DC10 SRM 51-31-01 VOL II AND DC10 SRM 51-33-01 VOL II.Jul 18, 2006 · N14075 · Doug DC1030 · Fuselage Main, Floor BeamSDR WRLA2006070Floor Support · corrodedDURING C-CK IN GSO FOUND FLOOR SUPPORT CORRODED IN MAIN CABIN B/N STA 879-755 AT APPROX LBL 46. RECEIVED NEW PART P/N ADA 7327-1 PO 540808-12; INSTALLED NEW FLOOR SUPPORT AIW DC10 SRM 51-31-01 VOL II.Jul 16, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006065Seat Track · corrodedDURING C-CK IN GSO AT STA 1960, FOUND RT O/B TRACK AND LAV MOUNT CORRODED. BLEND OUT CORROSION IN SEAT TRACK.Jul 14, 2006 · N14075 · Doug DC1030 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2006066Seat Track · corrodedDURING C-CK IN GSO FOUND RIGHT O/B SEAT TRACK AND LAV MOUNT CORRODED AT STA 1909-1913. BLENDED AREA IN ELECTRIC SEAT TRACK. FABRICATED STRAP.Jul 14, 2006 · N14075 · Doug DC1030 · Fuselage, Seat/Cargo Attach FittingsSDR XN0A1344Unknown · unknownDURING TAKE-OFF ROLL, N1 COMPUTER TARGET 115.1, THROTTLES AND N1 STABILIZED AT 115.0, BOTH ENGINES EGT EXCEEDED 960 DEGEES, NR 1 WENT TO 970 DEGREES AND NR 2 WENT TO 968 DEGREES, TAKE-OFF ABORTED. VISUALLY INSPECTED NR 1 AND NR 2 ENGINES INLET AND EXHAUST AREJul 12, 2006 · N474AS · Airbus A300B4203 · Engine (Turbine/Turboprop)SDR WRLA2006029Support · corrodedDURING CARGO MOD FOUND CABIN SEAT TRACK REF STA 392-421 CHANNEL SUPPORT P/N NBA 6000-926 CORRODED. REPLACED CABIN SEAT TRACK SUPPORT WITH P/N ABA8225-503 IAW DWG SP11530511-7025.Jul 11, 2006 · N279 · Doug MD11 · Fuselage Miscellaneous StructureSDR WRLA2006062Seat Track · corrodedDURING C-CHECK IN NAP FOUND CORROSION ON THE CHANNEL SUPPORT PN NBA6000-926 ON CABIN SEAT TRACK. REPLACED PN ABA8225-503 SUPPORT AND REWORK IAW DWG SP11530511-7025Jul 11, 2006 · N279 · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRNA200600029Connector · damagedON TAKEOFF ROLL, ENGINE NR 1 LOOP-B ON MWP AND FLIGHT ENGINEERS PANEL ILLUMINATED. ABORTED TAKEOFF, PERFORMED CHECKLIST AND RETURNED TO GATE. INSPECTED ENGINE AND FIRE LOOP, CHECKED GOOD. PLACED ON MEL 26-12-01 CAT-B, RELEASED AIRCRAFT TO SERVICE. REPAIREDJul 10, 2006 · N501TR · Airbus A300B4203 · Fire DetectionSDR WRLA2006020Bulkhead · corrodedDURING C3 CHECK, FOUND CORROSION IN LT MAIN GEAR WHEEL WELL AFT PRESSURE BULKHEAD, STA 1521, VERTICAL STIFFENER LOWER SUPPORT WEB AND ASSOCIATED ANGLES. REMOVED CORROSION AND REPLACED STIFFENER, WEB, AND ANGLES PER SRM PROCEDURES.Jul 9, 2006 · N14075 · Doug DC1030 · Fuselage Main, BulkheadSDR WRLA2006024Stiffener · corrodedDURING C3 CK, FOUND CORROSION IN LT MAIN GEAR WELL AFT PRESSURE BULKHEAD, STA 1521, ON THE VERTICAL STIFFENER (LWR AFT AREA). REMOVED CORROSION AND REPLACED STIFFENER.Jul 9, 2006 · N14075 · Doug DC1030 · Fuselage Main, BulkheadSDR WRNA200600027Clamp · brokenAFTER TAKEOFF NR 2 ENGINE FIRE LIGHT AND BELL CAME ON, REDUCED POWER, LIGHT WENT OUT. RETURNED TO FIELD AND MADE A SAFE LANDING. REPLACED BROKEN CLAMP ON 14TH STAGE BLEED MANIFOLD IAW 36-00-00 PAGE 425, LEAK CHECKED OK IAW AMM 71-00-00 PAGE 501. OPS CHECK, Jun 22, 2006 · N821SC · Airbus A300B4203 · Pneumatic Distribution SystemSDR WRLA2006061Cargo Track · corrodedDURING ACCOMP OF CARGO MOD J/C SP11530505-7014-1F, FOUND TRACK P/N AFA7795-11 MADE FROM P/N SG9291-47 CORRODED (REF STA 1811-1871). REPLACED AFFECTED TRACK WITH NEW TRACK P/N WSP0826-527 IAW DWG SP 11530505-7013.Jun 8, 2006 · N279 · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR XN0A1324Warning Light · illuminatedDURING CLIMBOUT NR 1 BLEED LIGHT ON, NO PRESSURIZATION ACCOMPANIED BY REGULATOR FAULT LIGHT. NR 2 BLEED HIGH TEMP LIGHT ACCOMPANIED BY BLEED FAULT LIGHT. REMOVED AND REPLACED NR 1 ENGINE IAW ENA EO 008-08 AND A300 AMM CHAPTER 71-00-00 PAGES 401 THRU 448. GRApr 30, 2006 · N473AS · Airbus A300B4203 · Engine Bleed Air SystemSDR ARWA20060402Compressor · dirtyBETWEEN 50 AND 60 PERCENT N1 NR 3 ENGINE HEAVY VIBRATION. REMOVED, CLEANED, LUBRICATED AND RE-INSTALLED FIRST STAGE FAN ROTOR BLADES IN ACCORDANCE WITH DC-10 A/M/M PAGE 811, M/M 72-21-00; RAN NR 3 ENGINE AT IDLE P/P AND MAX. NO EVIDENCE OF VIBRATION AT ANY SApr 28, 2006 · N478CT · Doug DC1030F · Turbine Engine Compressor SectionSDR WRNA200600012Flange · crackedNR 1 ENGINE OIL QUANTITY WENT TO (0), OIL PRESSURE FLUCTUATED AT 10 PSI WITH LOW OIL PRESSURE LIGHT ILLUMINATED ON MASTER WARNING PANEL AND HIGH OIL TEMPERATURE. ENGINE WAS SHUTDOWN, AIRCRAFT MADE A SAFE LANDING AT BDL. LEAK CHECK OF ENGINE REVELED OIL LEAKApr 27, 2006 · N820SC · Airbus A300B4203 · Turbine Engine Oil SystemSDR XN0A1319Shaft · shearedAFTER BLOCK OUT, DURING CROSS START- NR 2 ENGINE WOULD NOT START. NO N1 OR N2 INDICATIONS. START VALVE OPEN LIGHT CAME ON BUT NO START. FOUND STARTER SHAFT SHEARED, REMOVED AND REPLACED NR 2 ENGINE STARTER ASSY AS REQUIRED IAW A300 AMM CHAPTER 80-10-00, OPEApr 19, 2006 · N472AS · Airbus A300B4203 · Engine Starter
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