GE CF6-80C2B6F

Service difficulty reports · 1,456

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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 = 'CF680C2B6F'
  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 IPXA10659038Structure · crackedINSPECTION TYPE:C, LT WING NR 4 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT OTBD AREA AT OSS641.9 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, ORG MATL IS CLAD7075T6-0.063" CRK LENGTH IS 0.13" DAMAGED CUTOUT IS 8.875" X 7.25" THIS REPMar 30, 2010 · N326UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10659039Structure · crackedINSP TYPE:C, LT WING NR 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT INBD AREA AT OSS572.5 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201. ORG MATL IS CLAD7075T6-0.063" CRK LENGTH IS 0.12" DAMAGED CUTOUT IS 8.875" X 7.375" THIS REPAIR IMar 30, 2010 · N326UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10659040Skin · crackedINSPECTION TYPE:C, LTW NR 3 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED LT WING NR 3 SLAT INBD AREA AT OSS723.9 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201, ORG MATL IS CLAD7075T6-0.063" CRK LENGTH IS 0.12" DAMAGED CUTOUT IS 8.875" X 7.125" THIS REPAMar 30, 2010 · N326UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10659090Floor Panel · gougedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND DEEP AND LONG GOUGE AT STN 731 TO STN 833. RBL 11" TO RBL 33". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Mar 30, 2010 · N326UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659123Panel · crackedINSP TYPE:C EMP - LT INBD ELEVATOR T/E AREA CRACK COMPOSITE WET LAY UP. REPAIR CARRIED OUT IAW RS R55-23-36680 REV A.Mar 30, 2010 · N326UP · Boeing 76734AF · Elevator StructureSDR IPXA10659144Attach Fitting · crackedINSPECTION TYPE:C, AFT CARGO COMPT STA1087 BELOW FLOOR ATT CLIP FOUND CRACKED AT RBL25". AFT CARGO COMPT STA1087 RBL25" BELOW FLOOR ATT CLIP REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 46.Mar 30, 2010 · N326UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA10659145Attach Fitting · crackedINSPECTION TYPE:C AFT CARGO COMPT STA1087 BELOW FLOOR ATT CLIP FOUND CRACKED AT LBL25". AFT CARGO COMPT STA1087 LBL25" BELOW FLOOR ATT CLIP REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02, REV 46.Mar 30, 2010 · N326UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA10659155Spar · crackedINSPECTION TYPE:6C, LT WING L/E LES675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP FOUND CRACK. LT WIING L/E LES675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 46.Mar 30, 2010 · N326UP · Boeing 76734AF · Wing SparSDR IPXA10659157Skin · delaminatedINSP TYPE:C, LT OTBD ELEVATOR UPPER SKIN PANEL INBD AFT CORNER DELAMINATION COMPOSITE WET LAY UP. REPAIR CARRIED OUT IAW EO B767-5520-37266-A REFER RS R55-20-36688, REV A.Mar 30, 2010 · N326UP · Boeing 76734AF · Elevator, Plate/SkinSDR IPXA10659163Skin · misrepairedINSP TYPE:C, SURVEY SEQUENCE NR 326-F1-06 FUSELAGE BETWEEN BS 604 TO BS 628 STR 1R TO STR 4R EXISTING REPAIR WAS FOUND. BETWEEN BS604-628 STR1R-4R SKIN IAW R53-31-36683A MAT'L 2024T3 SKIN 0.093"-0.056" AT CUTOUT AREA WITH CUTOUT SIZE 4.18"X5.5". MAJOR REPAIRMar 30, 2010 · N326UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA10658998Skin · dented6 SKIN DENTS AT STA 450 JUST FWD OF LWR FWD CARGO DOOR CUTOUT. DENTS ARE IN CLOSE PROX TO EACH OTHER. REPAIRED IAW EO B767-5330-36821-B.Mar 29, 2010 · N310UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA10659082Floor Panel · puncturedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND PUNCTURED AT STN 932 TO STA 985, RBL 77" TO RBL 88". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659083Floor Panel · puncturedINSPECTION TYPE:6C MCD FLOOR PANEL FOUND PUNTURED AT STN 833 TO STN 930, LBL 33" TO LBL 55". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659091Floor Panel · puncturedINSP TYPE:6C, MCD FLOOR PANEL FOUND PUNCTURED AT STN 833 TO STN 930, LBL 11" TO RBL 11". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659097Floor Panel · puncturedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND SEVERAL PUNCTURES AT STN 1370 TO STN 1480, RBL 77" TO RBL 88". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALL IAW AMM 53-01-01.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659098Floor Panel · puncturedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND PUNCTURED AT STN 1344 TO STN 1425, RBL 55" TO RBL 77". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659100Floor Panel · puncturedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND PUNCTURED AT STN 540 TO STN 654+22, LBL 11" TO RBL 11". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALL IAW AMM 53-01-01.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659101Floor Panel · puncturedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND PUNCTURED AT STN 1041 TO STN 1114, RBL 33" TO RBL 55". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALL IAW AMM 53-01-01.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659115Stiffener · crackedINSPECTION TYPE:C WING CTR SECTION FRONT SPAR VERTICAL STIFFENER FOUND CRACKED JUST AT STA785.9 RBL10.94. WING CTR SECT FRONT SPAR AT STA785.9 RBL10.94 VERT STIFFENER REPAIRED IAW RS R57-00-36677 ORG MATL IS BAC1518-749-2024T3511 CRK LENGTH IS 3" CUT OFF LENGMar 29, 2010 · N326UP · Boeing 76734AF · Wing, Center BoxSDR IPXA10659139Floorbeam · crackedINSP TYPE:6C, AFT BULK CARGO COMPT MAIN DECK FLOORBEAM ATT ANGLE FOUND CRACKED AT STA 1581, RBL70". AFT BULK CARGO COMPT MAIN DECK FLOORBEAM ATT ANGLE REPLACED AND INSTALLED AT STA 1581 RBL 70" IAW SRM 51-10-02 AND 51-40-02 REV46.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA10659142Floorbeam · crackedINSPECTION TYPE:C, AFT BULK CARGO COMPT MAIN DECK FLOORBEAM ATT ANGLE FOUND CRACK AT STA1581 LBL70". AFT BULK CARGO COMPT MAIN DECK FLOORBEAM ATT ANGLE REPLACED AND INSTALLED AT STA1581 LBL70" IAW SRM 51-10-02 AND 51-40-02, REV 46.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA10659143Floorbeam · crackedINSPECTION TYPE:C FX STA246 MAIN DECK FLOORBEAM ATT CLIP FOUND CRACK AT RBL10". FX STA 246 MAIN DECK FLOORBEAM ATT CLIP AT RBL10" AREA REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02, REV 46.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA10659156Skin · misrepairedINSPECTION TYPE:C, SURVEY SEQUENCE NR 326-F1-01 FUSELAGE BETWEEN BS443-461 & S22R-26R EXISTING REPAIR DOES NOT CORRELATE TO A SRM. SURVEY SEQ NR 326-F1-01 FX BTN BS443-461 & STR22R-26R EXISTING REPAIR ADD FASTENERS ARE ADDED AND INSTALLED COMMON TO REPAIR DOMar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA10659160Skin · misrepairedINSP TYPE:C, SURVEY SEQUENCE NR 326-F1-02 BULK CARGO DOOR AT BETWEEN STA 1430-1439 STR 26L-27L AREA EXISTING REPAIR DOES NOT CORRELATE TO A SRM. BETWEEN STA 1426-1456 STR 25L-28L AREA SKIN REPAIRED RS R52-00-36681A ORG MAT'L IS 2024T3 .050" CHEM-MILLED SKIN.Mar 29, 2010 · N326UP · Boeing 76734AF · Cargo/Baggage DoorsSDR IPXA10658991Skin · dented6 SKIN DENTS AT STA 450 JUST FWD OF LWR FWD CARGO DOOR CUTOUT. DENTS ARE IN CLOSE PROX TO ONE ANOTHER. COMPLETED REPAIR IAW EO B767-5330-36821-B.Mar 28, 2010 · N310UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA10659000Floor Panel · damagedMAIN DECK FLOOR PANEL HAS HOLE. FABRICATED NEW FLOOR PANEL IAW STANDARD REPAIR EO B767-5320-9693-G.Mar 28, 2010 · N303UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659001Floor Panel · damagedFLOOR PANEL AT POS 5/6L HAS NUMEROUS HOLES. FABRICATED NEW FLOOR PANELS IAW STANDARD REPAIR EO B767-5320-9693-G.Mar 28, 2010 · N303UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658845Floor Panel · damaged3.5 X1.5 CUTOUT IN MAIN DECK FLOOR POS 10L, REPAIRED IAW SRM 53-00-50-2R.Mar 15, 2010 · N334UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658846Floor Panel · damagedFLOOR PANEL AT POS 10R DAMAGED. REPAIRED REF 767, SRM 53-00-50-2R.Mar 15, 2010 · N334UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658840Floor Panel · damagedPOS 13R OB FWD FLOOR PANEL HAS A .5 DIA HOLE. REPAIRED IAW SRM 767-300F 53-00-50-2R.Mar 14, 2010 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659035Skin · crackedINSPECTION TYPE:C, RT WING NR 10 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACK RT WING NR 10 SLAT INBD AREA AT OSS723.9 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201. ORG MATL IS CLAD7075T6-0.063" CRK LENGTH IS 0.14" DAMAGED CUTOUT IS 8.875" X 7.125". THISMar 10, 2010 · N326UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658772Seal · deterioratedFL 320 LOUD THUD FOLLOWED BY DEAFENING LOUD HOWL. INCREASING & DECREASING PSI, CHANGED ALTITUDE, NOISE DID NOT CHANGE. DIFFICULT TO COMMUNICATE WITH EACH OTHER AND AR DUE TO NOISE. NOISE STOPPED AS DESCENDING THRU FL220. CHECKED FLT COMPT FOR AIR LEAK, FOUNDMar 6, 2010 · N327UP · Boeing 76734AF · Flight Compartment WindowsSDR IPXA10658747Fairing · delaminatedINSP TYPE:C - RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-03 PAR 5A (1) FIG 5 REV 46.Mar 1, 2010 · N313UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10658748Fairing · delaminatedINSP TYPE:C- LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-03 PAR 5A (1) FIG 5 REV 46.Mar 1, 2010 · N313UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10658814Stiffener · crackedINSPECTION TYPE:C, RT WING - L/E OFSS821 FRONT SPAR STIFFENER FOUND CRACKED. RT WING L/E OFSS821 FRONT SPAR STIFFENER REPLACED AND INSTALLED IAW RS R57-00-36628. ORG MAT'L IS BAC1503-100631-7075T6511 EXTRUSION CRACK LENGTH IS .3750". THIS REPAIR IS CLASSIFMar 1, 2010 · N313UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA10658749Floor Panel · puncturedINSP TYPE:C -MCD FLOOR PANEL, FOUND SEVERAL PUNCTURED HOLES AT STA 412 TO 540 L11 TO R11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658750Floor Panel · puncturedINSP TYPE:C- MCD FLOOR PANEL, FOUND SEVERAL PUNCTURED HOLES AT STA 654+22 TO 696 R77 TO R88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658751Floor Panel · puncturedINSPECTION TYPE:C- MCD FLOOR PANEL, FOUND SEVERAL PUNCTURED HOLES AT STA 580 TO 654+22 R77 TO R88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658752Floor Panel · puncturedINSPECTION TYPE:C MCD FLOOR PANEL FOUND SEVERAL PUNCTURED HOLES AT STA731-833 R33 TO R55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658753Floor Panel · puncturedINSPECTION TYPE:C -MCD FLOOR PANEL FOUND SEVERAL PUCNTURED HOLES AT STA 690 TO 764 L77 TO L88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658754Floor Panel · puncturedINSPECTION TYPE:C- MCD FLOOR PANEL FOUND SEVERAL PUNCTURED HOLES AT STA 654+22 TO 690 R33 TO R55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658755Floor Panel · puncturedINSP TYPE:C -MCD FLOOR PANEL FOUND SEVERAL PUNCTURED HOLES AT STA 1344 TO 1480 L33 TO L55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658756Floor Panel · puncturedINSP TYPE:C - MCD FLOOR PANEL FOUND SEVERAL PUNCTURED HOLES AT STA 1197+22 TO 1207 R11 TO R33. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658757Floor Panel · puncturedINSPECTION TYPE:C- MCD FLOOR PANEL, FOUND SEVERAL PUNCTURED HOLES AT STA 654+22 TO 690 R11 TO R33. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658758Floor Panel · puncturedINSP TYPE:C -MCD FLOOR PANEL FOUND SEVERAL PUNCTURED HOLES AT STA 1207 TO 1344 L33 TO L55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658759Floor Panel · puncturedINSP TYPE:C -MCD FLOOR PANEL FOUND SEVERAL PUNCTURED HOLES AT STA 879 TO 933 L77 TO L88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658760Floor Panel · puncturedINSPECTION TYPE:C - MCD FLOOR PANEL FOUND SEVERAL PUNCTURED HOLES AT STA 731 TO 833 L11 TO R11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658761Floor Panel · puncturedINSPECTION TYPE:C- MCD FLOOR PANEL FOUND SEVERAL PUNCTURED HOLES AT STA 833 TO 930 L11 TO R11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658762Floor Panel · puncturedINSP TYPE:C -MCD FLOOR PANEL FOUND SEVERAL PUNCTURED HOLES AT STA 412 TO 540 L33 TO L55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658764Floor Panel · puncturedINSP TYPE:C- MCD FLOOR PANEL FOUND SEVERAL PUNCTURED HOLES AT STA1480 TO 1598 L11 TO R11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor Panel
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