Boeing 767-232

Service difficulty reports · 2,991

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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 aircraft_model_key = '767232'
  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 IXXA20170414236Keelbeam · corrodedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. UPPER KEEL WEB IN THE RIGHT MAIN LANDING GEAR WHEEL WELL HAS AREAS OF CORROSION IN THE FORWARD PASS THROUGH LOCATION. BLENDED CORROSION ON RIGHT MAIN LANDING GEAR WHEEL WELL STATION 970 RIGHT BUTT LINE 5 FOUND TO BE OUTMar 17, 2017 · N763CX · Boeing 767232 · Fuselage Main, KeelSDR IXXA20170412228Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER HORIZONTAL FLANGE LOWER SURFACE BS 303, LBL 54 AROUND NUTPLATE. REMOVED DAMAGED ON FLOORBEAM UPPER FLANGE LOWER SURFACE. PERFORMED REPAIR IAW SRM 51-20-01.Mar 17, 2017 · N739AX · Boeing 767232 · Fuselage Main, Floor BeamSDR IXXA20170414237Frame · crackedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. STATION 859.5 LEFT BUTT LINE 89 BELOW WATER LINE 200, FRAME INNER CHORD TRANSITION RADIUS CRACKED .25" APPROXIMATELY. REMOVED FASTENERS PER JOB CARD ENGINEERING ORDER 53-767-5352 FOR HIGH FREQUENCY EDDY CURRENT. COMPLIEMar 16, 2017 · N763CX · Boeing 767232 · Fuselage Main, FrameSDR IXXA20170412229Strap · corrodedBULK CARGO BS 1480, STRINGER 23L INTERCOSTAL INBOARD STRAP CORRODED. REMOVED AND REPLACED THE STRAP IAW SRM 51-40-02, AND ED 47221FAB88.Mar 16, 2017 · N739AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR IXXA20170412231Skin · corrodedLEFT OTBD AILERON HAS AREAS OF CORROSION ON THE SKIN AROUND THE BALANCE WEIGHT. REMOVED AND REPLACED THE AILERON IAW AMM 27-11-02, PARAGRAPH 3G.Mar 15, 2017 · N739AX · Boeing 767232 · AileronsSDR IXXA20170412230Floor Support · corrodedUPPER CARGO OUTER FLOOR SUPPORT CORRODED BS 1483-1610. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, AND ED 47224FAB08, AND 47224FAB51.Mar 15, 2017 · N739AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR IXXA20170412211Web · corrodedR2 DOOR SILL CORRODED. BLENDED AREA IAW 53-00-15 DETAIL XII PAGE 113. FOUND TO BE OUT OF LIMITS. FABRICATED A NEW DOOR SILL WEB IAW DRAWING 146T8310,Mar 14, 2017 · N739AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR IXXA20170412235Support · corrodedLEFT REAR SPAR SUPPORT IS CORRODED AT BOTH ENDS, LWS 853. REMOVED AND REPLACED THE SUPPORT STIFFENER IAW SRM 51-40-02. LEAK CHECKED IAW AMM 28-11-00. CHECKED GOOD.Mar 13, 2017 · N739AX · Boeing 767232 · Wing Miscellaneous StructureSDR IXXA20170412234Floorbeam · corrodedRBL 35 - 44, BS 1220 FLOORBEAM HAS CORROSION AROUND THE NUTPLATE. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-40-01, SECTION 9.Mar 13, 2017 · N739AX · Boeing 767232 · Fuselage Main, Floor BeamSDR IXXA20170412233Floorbeam · corrodedCORROSION ON THE FLOORBEAM UPPER HORIZONTAL FLANGE LOWER SURFACE BS 287 LBL 45 - 54. REMOVED AND REPAIRED THE DAMAGED AREA IAW SRM 53-00-51, AND DRAWING 141T5111.Mar 13, 2017 · N739AX · Boeing 767232 · Fuselage Main, Floor BeamSDR IXXA20170412232Bear Strap · corrodedTHE BEAR STRAP WAS CORRODED BS 1263-1274, BETWEEN STRINGERS 34 - 35R. THE BEAR STRAP WAS FOUND OUT OF LIMITS IAW SRM 51-10-02. FABRICATED AND INSTALLED A DOUBLER AND TRIPLE IAW SRM 53-00-01, AND ED 47224REA44.Mar 13, 2017 · N739AX · Boeing 767232 · Fuselage Main, Plate/SkinSDR IXXA20170320157Stringer · corrodedCORROSION OTBD OF RIB 2L, FORWARD LOWER EDGE OF LOWER STRINGER 8. CORROSION OUT OF LIMITS IAW SRM 55-10-02. PERFORM SPLICE REPAIR ON STRINGER 8 IAW SRM 55-16-02, REPAIR 1.Mar 9, 2017 · N739AX · Boeing 767232 · Fuselage Main, Longeron/StringerSDR IXXA20170320160Floor Support · corrodedAFT LOWER CARGO FLOOR SUPPORT CORRODED AT LBL 12, BS 1307-1329. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.Mar 8, 2017 · N739AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR IXXA20170320159Floorbeam · corrodedAFT LOWER CARGO FLOORBEAM CORRODED BS 1311, RBL 5 - LBL 20. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-40-02.Mar 8, 2017 · N739AX · Boeing 767232 · Fuselage Main, Floor BeamSDR IXXA20170320158Floorbeam · corrodedBS 1410 UPPER FLOOR SUPPORT CORRODED AROUND ALL NUT PLATES LBL 54 THROUGH RBL 54. REMOVED SURFACE DAMAGE IAW SRM 53-00-51-1A-1. REMOVED AND REPLACED THE NUT PLATES IAW SRM 51-40-02.Mar 8, 2017 · N739AX · Boeing 767232 · Fuselage Main, Floor BeamSDR IXXA20170320162Floor Support · corrodedUPPER CARGO FLOOR SUPPORT CORRODED AT BS 1395-1415, LBL 24. FABRICATED A NEW FLOOR SUPPORT IAW DRAWING 452T3252. REMOVED & REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.Mar 7, 2017 · N739AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR IXXA20170320161Stringer · corrodedCORROSION INBD OF RIB 2R LOWER STRINGER 5, VERTICAL LEG FORWARD AND AFT. CORROSION OUT OF LIMITS IAW SRM 55-10-02, FIGURE 101, DETAIL II. REMOVED AND REPLACED THE STRINGER IAW SRM 55-10-03, REPAIR 1, AND DRAWING 181T4000.Mar 7, 2017 · N739AX · Boeing 767232 · Fuselage Main, Longeron/StringerSDR IXXA20170320166Shear Tie · corrodedSHEAR TIE CORRODED AT BS 1480 BETWEEN STRINGERS 38L-39R. BLENDED AND FOUND TO BE OUT OF LIMITS. REPLACED THE SHEAR TIE IAW DRAWINGS 146T1219, AND 146T3240.Mar 2, 2017 · N739AX · Boeing 767232 · Fuselage Internal Mounting StructureSDR IXXA20170320165Angle · corrodedTWO ANGLES AT BS 977 CORRODED. REPAIRED IAW ED 47224REA51, AND 47224REA52.Mar 2, 2017 · N739AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR IXXA20170320164Strap · corrodedFLOOR PLATE STRAP LBL 70 BS 1483 CORRODED. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIGURE 101, DETAIL II. FABRICATED A NEW STRAP IAW DRAWING 368-53-16-94372.Mar 2, 2017 · N739AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR IXXA20170320163Failsafe · corrodedCORROSION FOUND ON THE TERMINAL FITTING AT RBL 97 BS 955. REMOVED AND REPLACED THE FAILSAFE.Mar 2, 2017 · N739AX · Boeing 767232 · Fuselage Main, StructureSDR IXXA20170320167Floorbeam · corrodedFLOORBEAM AT BS 1153 FROM LBL 36 - 48 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. REPLACED IAW SRM 51-40-02.Mar 1, 2017 · N739AX · Boeing 767232 · Fuselage Main, Floor BeamSDR IXXA20170320168Stringer · corrodedSTRINGER 33L, BETWEEN BS 1540 - 1562 IS CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-02 & DOCUMENT 146T8240.Feb 28, 2017 · N739AX · Boeing 767232 · Fuselage Main, Longeron/StringerSDR IXXA20170320171Link · corrodedLEFT MLG WW, SHEAR LINK IS CORRODED. REMOVED AND REPLACED THE SHEAR LINK ASSEMBLY.Feb 24, 2017 · N739AX · Boeing 767232 · Main Landing GearSDR IXXA20170320170Angle · corrodedBS 1373 LBL 54 FLOOR SUPPORT ANGLE CORRODED. BLENDED TO 100% MATERIAL LOSS. FABRICATED AND INSTALLED NEW ANGLE IAW DRAWING 453T1031.Feb 24, 2017 · N739AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR IXXA20170320169Fork · corrodedCORROSION ON THE UPPER FLANGE OF FORK AND ATTACH FITTING, IN THE UPPER FORWARD OUTBOARD CORNER OF THE LEFT WHEEL WELL. REMOVED AND REPLACED THE FORK AND SHEAR LINK.Feb 24, 2017 · N739AX · Boeing 767232 · Fuselage Main, StructureSDR IXXA20170320174Fitting · corrodedLEFT MLG WW, FORWARD SHEAR LINK FITTING IS CORRODED. REMOVED AND REPLACED SHEAR LINK ASSEMBLY.Feb 23, 2017 · N739AX · Boeing 767232 · Fuselage Main, Attach FittingsSDR IXXA20170320173Spar Cap · corrodedCORROSION ON RIGHT WING FRONT SPAR LOWER CAP UPPER SURFACE AT LEADING EDGE WS 1011. BLENDED OUT CORROSION TO 100% MATERIAL LOSS. CUT OUT DAMAGED SECTION, AND INSTALLED IAW ED 47224REA49.Feb 23, 2017 · N739AX · Boeing 767232 · Wing SparSDR IXXA20170320172Stringer · corrodedSTRINGER 13L CRACKED ON END AFT OF BS 676. REMOVED AND REPLACED THE STRINGER IAW SRM 53-00-03, FIGURE 201, REPAIR 1 AND SERVICE BULLETIN 368-53-041 REV 2.Feb 23, 2017 · N739AX · Boeing 767232 · Fuselage Main, Longeron/StringerSDR IXXA20170320175Support · corrodedFORWARD CARGO BAY LEFT UPPER OTBD CEILING SUPPORT IS CORRODED BETWEEN BS 500 - 522. REMOVED AND REPLACED SUPPORT IAW SRM 51-40-02, SECTION 9.Feb 22, 2017 · N739AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR IXXA20170320176Shear Tie · corrodedSHEAR TIE CORRODED AT BS 1395 BETWEEN STRINGERS 37 - 38L. FABRICATED AND INSTALLED A NEW SHEAR TIE IAW SRM 51-40-02 AND DRAWING 140T2102.Feb 21, 2017 · N739AX · Boeing 767232 · Fuselage Internal Mounting StructureSDR IXXA20170320177Intercostal · corrodedUPPER CARGO BS 1120 BETWEEN LBL 88 & RBL 88 DRAIN INTERCOSTALS CORRODED. REMOVED AND REPLACED THE DRAIN PAN INTERCOSTALS IAW DRAWING 368-53-13-90988.Feb 20, 2017 · N739AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR IXXA20170320178Rib · corrodedLEFT WING LEADING EDGE STRUT CORRODED AT WS 1030. REMOVED AND REPLACED RIB AND DOUBLER IAW SRM 57-41-09. CORROSION FOUND TO BE OUT OF LIMITS.Feb 16, 2017 · N739AX · Boeing 767232 · Wing, Rib/BulkheadSDR IXXA20170320179Floor Support · corrodedFORWARD TIP OF BULK FLOOR SUPPORT AT LBL 29 IS CORRODED. BLENDED CORROSION. LOST 100% OF MATERIAL. FOUND TO BE OUT OF LIMITS. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02.Feb 9, 2017 · N739AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR IXXA20170320183Stringer Clip · corrodedSTRINGER CLIP 3R, BS 1678 BULKHEAD CRACKED. THE STRINGER CLIP WAS FABRICATED IAW DRAWING 148T2120, STRINGER CLIP AND HEAT TREATED IAW 5602 REVISION AF, 5946 REVISION AF. THE STRINGER CLIP WAS INSTALLED IAW SRM 51-40-02.Feb 3, 2017 · N739AX · Boeing 767232 · Fuselage Main, Attach FittingsSDR IXXA20170320182Floorbeam · corrodedFLOORBEAM BS 1263 LBS 33 - 40 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-07, REPLACED THE FLOORBEAM ANGLE.Feb 3, 2017 · N739AX · Boeing 767232 · Fuselage Main, Floor BeamSDR IXXA20170320181Skin · corrodedSKIN CORRODED BS 1241 JUST BELOW STRINGER 34R. CORROSION ON SKIN WAS FOUND TO BE OUT LIMITS. SKIN THICKNESS OF .210, REMAINING THICKNESS .100 IN ACCORDANCE WITH B767 SRM 51-00-01 TABLE I DETAIL II. REPAIRED PER AMES ENGINEERING DOCUMENT 47224REA44 REV A.Feb 3, 2017 · N739AX · Boeing 767232 · Fuselage Main, Plate/SkinSDR IXXA20170320180Structure · corrodedRIGHT WHEEL WELL OUTBOARD LONGERON CORRODED AFT END BS 1050 RIGHT BUTT LINE 90 UPPER SIDE OF HORIZONTAL WEB. UPON FURTHER INVESTIGATION LONGERON TO BE OUT OF LIMITS IAW SRM 53-50-05. REMOVED AND REPLACED LONGERON IAW SRM 51-40-02.Feb 3, 2017 · N739AX · Boeing 767232 · Fuselage Structure (General)SDR IXXA20170320188Skin · corrodedSKIN BETWEEN STRINGERS 36 - 37R CORRODED AT BS 1170-1175. REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-01-2R-12.Feb 2, 2017 · N739AX · Boeing 767232 · Fuselage Main, Plate/SkinSDR IXXA20170320187Angle · corrodedCORROSION ON STRINGER 23R AT BS 1461. REMOVED AND REPLACED IAW SRM 51-40-02 PAGE 4 PARAGRAPH 7 AND PAGE 2 PARAGRAPH 4.Feb 2, 2017 · N739AX · Boeing 767232 · Fuselage Main, Longeron/StringerSDR IXXA20170320185Skin · corrodedAFT LOWER CARGO BS 1175-1197 STRINGER 36R TO 37R SKIN CORRODED. REMOVED DAMAGE AREA AND REPAIRED IAW SRM 53-00-01-2R-12.Feb 2, 2017 · N739AX · Boeing 767232 · Fuselage Main, Plate/SkinSDR IXXA20170320184Splice Plate · corrodedRIGHT WING LEADING EDGE SPLICE PLATE CORRODED WS 482. THE SPLICE PLATE WAS REPAIRED IAW ENGINEERING DOCUMENT 47224REA35.Feb 2, 2017 · N739AX · Boeing 767232 · Wing Main, Frame StructureSDR IXXA20170320189Stiffener · corrodedMAIN DECK FLOORBEAM HORIZONTAL STIFFENER IS CORRODED AT BS 522 RBL 42-55 . REMOVED AND REPLACED THE STIFFENER IAW SRM 51-40-02 SECTION 9 AND ENGINEERING DOCUMENT 47224FAB76.Feb 1, 2017 · N739AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR IXXA20170320192Stringer · corrodedSTRINGER 36R JUST AFT OF BS 1131 IS CORRODED ON OTBD SIDE. REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM 53-00-03 AND SRM 51-40-02.Jan 31, 2017 · N739AX · Boeing 767232 · Fuselage Main, Longeron/StringerSDR IXXA20170320191Frame · corrodedFORWARD LOWER CARGO INTERNAL FRAME AT BS 676, LBL 40 HAS CORROSION. REMOVED AND REPLACED IAW SRM 51-40-02.Jan 31, 2017 · N739AX · Boeing 767232 · Fuselage Main, FrameSDR IXXA20170320190Bear Strap · corrodedAFTER REMOVING THE FORWARD LOWER CORNER SEAL DEPRESSOR ON THE FORWARD LOWER CARGO DOOR, FOUND CORROSION ON THE BEAR STRAP COMMON TO THE SEAL DEPRESSOR. BLENDED CORROSION IAW SRM 53-00-15. BLEND WAS OUT OF LIMITS. REPAIRED IAW ENGINEERING DOCUMENT 47224REA12 RJan 31, 2017 · N739AX · Boeing 767232 · Fuselage Main, Plate/SkinSDR IXXA20170320195Pressure Deck · corrodedPRESSURE DECK BETWEEN BS 1263 - 1285, LBL 10 IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-00, FIGURE 101. FABRICATED A NEW PRESSURE DECK AND INSTALLED.Jan 30, 2017 · N739AX · Boeing 767232 · Fuselage Floor PanelSDR IXXA20170320194Skin · corrodedRIGHT MLG UPLOCK TORSION BOX, UPPER OTBD, AFT MOUNTING FLANGE SHIM HAS CORROSION AND A SUPPORT ANGLE IS BENT. REWORKED SUPPORT ANGLE, FABRICATED A SHIM IAW DRAWING 149T6972.Jan 30, 2017 · N739AX · Boeing 767232 · Main Landing GearSDR IXXA20170320193Skin · corrodedCORROSION ON STRINGER 29R AND ON THE INTERIOR SKIN BS 1085. BLENDED THE CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-00-01, FIGURE 101. REMOVED AND REPLACED UPPER AND LOWER SHEAR TIE IAW SRM 51-40-02 SECTION 7.Jan 30, 2017 · N739AX · Boeing 767232 · Fuselage Main, Plate/SkinSDR IXXA20170320196Stringer · corrodedSTRINGER 35L CORRODED BETWEEN BS 1395 - 1417. REPAIRED THE STRINGER IAW SRM 53-00-03, FIGURE 201, REPAIR 2.Jan 26, 2017 · N739AX · Boeing 767232 · Fuselage Main, Longeron/Stringer
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