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"

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SDR IXXA201309270047Failsafe · corrodedDURING HEAVY MX VISIT, MX AND ENGINEERING REPORTED AN AREA OF CORROSION ON THE FAILSAFE STRAP, BS 1348 FRAME S21-22R. CORROSION REMOVED. HFEC OPEN-HOLE INSPECTION AND SURFACE SCAN INSPECTIONS WERE ACCOMPLISHED AND CRACK INDICATIONS WERE DISCOVERED IN THREE ESep 9, 2013 · N762CX · Boeing 767232 · Fuselage Main, StructureSDR IXXA201309270048Angle · corrodedDURING HEAVY MX VISIT, MX AND ENGINEERING DISCOVERED MINOR CORROSION ON THE OUTER ANGLE OF THE LOWER DOOR JAMB FORWARD CORNER OF THE FORWARD LOWER CARGO DOOR. CORROSION REMOVED, BLENDED AREA WAS HFEC INSPECTED. SPOTFACED ALL OPEN FASTENER LOCATIONS IN BLENDSep 9, 2013 · N762CX · Boeing 767232 · Fuselage Main, StructureSDR IXXA201309270049Angle · corrodedDURING HEAVY MX VISIT, MX AND ENGINEERING DISCOVERED MINOR CORROSION ON THE OUTER ANGLE OF THE LOWER DOOR FRAME AFT CORNER OF THE FWD LOWER CARGO DOOR. CORROSION WAS REMOVED. AREA HFEC INSPECTED, NO ADDITIONAL DEFECTS WERE NOTED.Sep 9, 2013 · N762CX · Boeing 767232 · Fuselage Main, StructureSDR IXXA201309270050Angle · corrodedDURING HEAVY MX VISIT, MX AND ENGINEERING DISCOVERED CORROSION AROUND A FASTENER HOLE, BENEATH THE NUTPLATE ON THE FWD LOWER CARGO DOOR ON THE UPPER ANGLE OF THE THIRD HORIZONTAL BEAM FROM THE TOP OF THE DOOR JUST AFT OF THE ACTUATOR BRACKET. THE NUTPLATE WASSep 9, 2013 · N762CX · Boeing 767232 · Fuselage Miscellaneous StructureSDR IXXA201309270051Floorbeam · corrodedDURING HEAVY MX VISIT, MX AND ENGINEERING DISCOVERED THAT THE UPPER CAP OF THE FLOORBEAM HAS CORROSION AT BS 1395, LBL 42. R & R FLOORBEAM CAP IAW DWG 146T1215 AND SRM 51-40-02.Sep 9, 2013 · N762CX · Boeing 767232 · Fuselage Main, Floor BeamSDR IXXA201309270052Support Bracket · crackedDURING HEAVY MX VISIT, MX AND ENGINEERING DISCOVERED THE SUPPORT BRACKET FOR THE LT WING UPPER BONDED PANEL IS CRACKED AT WING STA 798.2. R & R THE SUPPORT BRACKET IAW SRM 51-40-02.Sep 9, 2013 · N762CX · Boeing 767232 · Wing Miscellaneous StructureSDR IXXA201309270053Skin · corrodedDURING HEAVY MX VISIT, MX AND ENGINEERING DISCOVERED AN ISOLATED AREA OF CORROSION ON LT WING UPPER SKIN PANEL CORROSION WAS REMOVED BY BLENDING. HFEC INSPECTED IAW NDT MANUAL, PART 6, 51-00-19. NO ADDITIONAL DEFECTS NOTED. REWORKED AREA WAS ROTO-PEENED ANDSep 9, 2013 · N762CX · Boeing 767232 · Wing, Plate/SkinSDR IXXA201309270054Angle · crackedDURING HEAVY MX VISIT, MX AND ENGINEERING DISCOVERED VERTICAL ANGLE AT BS 287, LBL 25 IN NOSE WHEEL WELL CRACKED. REPAIRED VERTICLE ANGLE IAW SRM 53-10-14, FIG NR 2 AND SRM 51-70-12, FIG NR 1.Sep 9, 2013 · N762CX · Boeing 767232 · Fuselage Main, BulkheadSDR IXXA201309270055Support Bracket · crackedLT WING FWD SPAR RIB SUPPORT BRACKET AT WBL 103 CRACKED. R & R BRACKET IAW DWG 114T1305 AND SRM 51-40-02.Sep 9, 2013 · N762CX · Boeing 767232 · Wing Miscellaneous StructureSDR IXXA2013092700056Rib · crackedVERTICAL STABILIZER ACCESS 324CLX, LOWER BOX INTERNAL LT FWD LOWER RIB CRACKED. R & R FWD LOWER RIB IAW SRM 51-40-02.Sep 9, 2013 · N762CX · Boeing 767232 · Vertical Stabilizer, Spar/RibSDR IXXA201309270057Skin · wornVERTICAL STABILIZER ACCESS 324AL, FUSELAGE MOUNTED TRIANGLE PANEL UPPER MATING SURFACE WORN. R & R FORWARD FAIRING SKIN PANEL IAW SRM 51-40-02.Sep 9, 2013 · N762CX · Boeing 767232 · Vertical Stabilizer, Plate/SkinSDR IXXA20130927058Stringer Splice · crackedSTRINGER SPLICE IN AFT LOWER COMPARTMENT AT FS1535 S39L CRACKED. R & R STRINGER 39L IAW SRM 51-40-02 AND 53-00, FIG 201, SHEET 4.Sep 9, 2013 · N762CX · Boeing 767232 · Fuselage Main, Longeron/StringerSDR IXXA20130927059Support · crackedNR 2 PYLON PANEL ACCESS PANEL 442FR, MID SUPPORT UPPER INBD RIB SUPPORT CRACKED. R & R RIB SUPPORT IAW SRM 51-40-02.Sep 9, 2013 · N762CX · Boeing 767232 · Nacelle/Pylon Miscellaneous StructureSDR IXXA2013092700060Floor Support · corrodedFORWARD LOWER COMPARTMENT FLOOR SUPPORT FWD OF AIR MIXER AT BS 742 CORRODED. R & R FLOOR SUPPORT IAW SRM 51-40-02.Sep 9, 2013 · N762CX · Boeing 767232 · Fuselage Miscellaneous StructureSDR IXXA2013092700061Nut Plate · missingAFT LOWER COMPARTMENT FLOOR NUTPLATE MISSING AT STATION 1153. REPLACED NUT PLATE IAW SRM 51-40-02.Sep 9, 2013 · N762CX · Boeing 767232 · Fuselage Miscellaneous StructureSDR IXXA130909ILN062SNut Plate · missingAFT LOWER COMPARTMENT NUT PLATE LT SIDE ROLLER TRACK MISSING AT BS 1197. REPLACED NUT PLATE, CORROSION WAS FOUND ON UPPER ANGLE. R & R UPPER ANGLE AND REPLACED NUT PLATE IAW SRM 51-40-02.Sep 9, 2013 · N762CX · Boeing 767232 · Cargo CompartmentsSDR IXXA201309270063Stringer · corrodedAFT LOWER COMPARTMENT STRINGER 36R AT BS 1225, CORRODED. R & R STRINGER 36R IAW SRM 53-00-03, REPAIR 2.Sep 9, 2013 · N762CX · Boeing 767232 · Fuselage Main, Longeron/StringerSDR IXXA20130927064Floorbeam · corrodedCORROSION WAS FOUND AROUND THE NUT PLATE ON THE HORIZONTAL FLANGE OF THE FLOOR FRAME AT BS 1175, BL0 TO BL45. R & R THE UPPER CHORD IAW SRM 51-40-02.Sep 9, 2013 · N762CX · Boeing 767232 · Fuselage Main, Floor BeamSDR IXXA130909ILN065SBeam · crackedINBD BEAM INSIDE OF THE NR 1 PYLON HYD BAY DOOR IS CRACKED AT FWD END. R & R BEAM IAW SRM 51-40-02.Sep 9, 2013 · N762CX · Boeing 767232 · Nacelle/Pylon, Main FrameSDR ABXA20130906592Mount · corrodedNR 2 ENGINE LT SIDE OF AFT MOUNT HAS MINOR CORROSION AND LT SIDE LINK HAS PITTING. R & R NR 2 ENGINE AFT MOUNT AS REQUIRED, WITH A NEW ENGINE MOUNT, IAW AMM 71-21-02-4. CORROSION, PN: 310T1020-3, MOUNT, AFT ENG, SN: 48. NAC 308.50. ACFT WAS GROUNDED.Sep 6, 2013 · N745AX · Boeing 767232 · Engine Mount SectionSDR ABXA20130906562Shear Web · corrodedSHEAR WEB BS 488, CORRODED UNDER 232G AND 232E. R & R SHEAR WEB BS 475-525, RBL 11-33- & 55-77 IAW SRM 51-40-02, PG 4, PAR7 & IAI DWG 368-53-13-95590. ACFT WAS GROUNDED.Sep 6, 2013 · N742AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA20130906559Cargo Track · corrodedUPPER CARGO, BS 355, RBL 11, CARGO TRACK AND UPPER SURFACE OF SPLICE IS CORRODED. R & R CARGO TRACK AND PLATE AT BS 347-445 IAW REA B653-60668-MR, B653-60687-MR, SRM 51-40-02, PG 4, PAR 7, IAI DWG'S 368-25-16 90621 & 368- 53-11-90590. ACFT WAS GROUNDED.Sep 6, 2013 · N742AX · Boeing 767232 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA20130906557Stringer · corrodedAFT LOWER CARGO STRINGER 39L BETWEEN BS 1197 & 1129 CORRODED. R & R STRINGER BS 1197 TO 1219 IAW SRM 53-00-03. REPAIR 2. ACFT WAS GROUNDED.Sep 6, 2013 · N742AX · Boeing 767232 · Fuselage Main, Longeron/StringerSDR ABXA20130905601Angle · corrodedCEILING PANEL ATTACH ANGLE CORROSION AT BS 1351. R & R CEILING SUPPORT ANGLES IAW SRM 51-40-02. ACFT WAS GROUNDED.Sep 5, 2013 · N745AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA20130905600Angle · corrodedCEILING PANEL ATTACH ANGLES CORRODED AT STA 1263. R & R ANGLES LBL27-RBL40 IAW SRM 51-40-02 CLEANED TREATED AND PRIMED CORROSION ON ANGLE RBL 40 & RBL 66 IAW SRM 53-00-51, FIG 101. FOUND TO BE WITHIN LIMITS. ACFT WAS GROUNDED.Sep 5, 2013 · N745AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA20130905565Seat Track · corrodedSTAINLESS ANGLE AT BOTTOM OF BACK WALL IN UPPER CARGO HAS CORROSION UNDER IT ON FLOORBEAM, APPROXIMATELY AROUND BS 1556. REMOVED & REINSTALLED STAINLESS ANGLE AT BACK WALL IN UPPER CARGO, REMOVED CORROSION & R & R SEAT TRACKS IAW SRM 51-40-02, PG 4, PAR 7, 53Sep 5, 2013 · N742AX · Boeing 767232 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA20130904566Seat Track · corrodedSEAT TRACK AT BS 1461-1502 INBD OF L2 DOOR, FOUND TO BE CORRODED BEYOND LIMITS. R & R SEAT TRACK IAW REA NR B653-60673-MR, DWG 146T0051 & SRM 51-40-02 PAR 7, PG 4. ACFT WAS GROUNDED.Sep 4, 2013 · N742AX · Boeing 767232 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA2013100200554Support · corrodedBULK CARGO CEILING LT SIDE AT ZONE 161 JUST AFT OF FLOOR SUPPORT BEAM AT STA 1540 THERE IS A CORRODED MAIN CARGO FLOOR SUPPORT. R & R FLOOR SUPPORT TEE (BEAM) AT STA 1540 IAW DWG 146T0051 & SRM 51-40-02, PG 4, PAR 7. ACFT WAS GROUNDED.Sep 4, 2013 · N742AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA2013100200553Support · corrodedAFT LOWER CARGO CEILING BETWEEN STA 1395, 1417 ON LT SIDE IS A MOUNT/SUPPORT FOR THE BULK CARGO BARRIER DOOR FWD ATTACH POINT THAT IS CORRODED. R & R MOUNT/SUPPORT FOR BULK CARGO BARRIER DOOR FWD ATTACH POINT. IAW SRM 51-40-02, STEPS 4 AND 7D. CORROSION, SUPPSep 4, 2013 · N742AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA2013100200552Strut · corrodedNR 8 SLAT, INBD AUX TRACK, INBD UPPER STRUT CORRODED AT FWD LOWER END. REMOVED NR 8 SLAT INBD UPPER RIB AT AUX TRACK DUE TO CORROSION. INSTALLED NEW SERVICEABLE UPPER RIB AS REQUESTED IAW SRM 51-40-02. CORRODED 114T2200-18 RIB, FROM L/E 436.00 TO ROW L/GE. Sep 4, 2013 · N742AX · Boeing 767232 · Leading Edge DevicesSDR ABXA20131002547Rib · corrodedRT WING L/E RIB HAS CORROSION JUST OTBD OF NR 9 SLAT INBD AUX TRACK. FOUND TO BE OUT OF LIMITS. FABRICATED NEW RIB IAW REA B657-60644. INSTALLED IAW SRM 51-40-02. ACFT WAS GROUNDED.Sep 4, 2013 · N742AX · Boeing 767232 · Wing, Rib/BulkheadSDR ABXA20130903560Angle · crackedLT ANGLE HAS HFEC DEFECT INDICATIONS IN THREE AREAS, NDTM PN 6 53-80-04, FIG 1. REPAIRED DAMAGE BY REPLACING ANGLE, UPPER AND LOWER TENSION FITTINGS, SPLICE FITTING AND SKIN REPAIR IAW SRM 53-80-01. ACFT WAS GROUNDED.Sep 3, 2013 · N742AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA2013100200551Rib · corrodedNR 11 SLAT OTBD AUX TRACK OTBD LOWER STRUT HAS CORROSION UNDER NUTPLATES. INSTALLED A NEW STRUT RIB, PN: 114T2224-8 IAW SRM 51-40-02 PARA 4 & 7 AND REA-B657-60625-. ACFT WAS GROUNDED.Sep 3, 2013 · N742AX · Boeing 767232 · Wing, Rib/BulkheadSDR ABXA20130902564Floor Support · corrodedFLOOR SUPPORT FROM BS 610 - 632 LBL 8 CORRODED AROUND NUTPLATES. R & R FLOOR SUPPORT IAW SRM 51-40-02.Sep 2, 2013 · N742AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA20130902561Stiffener · crackedUPPER CARGO FLOORBEAM, SECTION 41, CRACKED AT UNDERSIDE, BENEATH PANEL 221G JUST AFT OF ENTRYWAY FLOOR HATCH. R & R UPPER WEB STIFFENER AT STA 325-355, LBL40 BELOW PANEL 221G IAW DWG 141T5140 & SRM 51-40-02, PAR 7, PG 4, PN 141T5140-109 STIFFENER CRACKED .5" Sep 2, 2013 · N742AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA20131002550Skin · corrodedUPPER AREA FORWARD OF FRONT SPAR, AFT OF NR 12 SLAT AT WING LES 960 CORRODED. REMOVED CORROSION IAW SRM 57-20-01. SKIN BLEND-OUT AND SPLICE PLATE REPAIR WERE ACCOMPLISHED ON REA B657-60655. ACFT GROUNDED.Sep 2, 2013 · N742AX · Boeing 767232 · Wing, Plate/SkinSDR ABXA20131002549Strut · corrodedNR 4 SLAT OTBD AUX TRACK INBD LOWER STRUT CORRODED AND FASTENERS MISSING AT FORWARD END. R & R STRUT ON NR 4 SLAT OTBD AUX TRACK INBD. STRUT IAW SRM 51-40-023 & 51-40-05. ACFT WAS GROUNDED.Sep 2, 2013 · N742AX · Boeing 767232 · Leading Edge DevicesSDR ABXA2013100200555Fitting · corrodedRUDDER LT SIDE 8 INCHES BELOW TIP, 4 INCHES FWD OF T/E FASTENER HEAD POPPED, POSSIBLE DELAMINATED. REMOVED RUDDER TIP PANEL, REPLACED RUDDER TIP FITTING, REPLACED RUDDER TIP PANEL IAW SRM 51-40-02 AND SEALED IAW 51-20-5. ACFT WAS GROUNDED.Aug 31, 2013 · N742AX · Boeing 767232 · Rudder StructureSDR ABXA20130830567Stringer · corrodedAFT LOWER CARGO AREA BETWEEN BS 1502 & 1506 STRINGER 26L IS CORRODED. REMOVED DAMAGED SECTION & REPAIRED IAW SRM 53-00-03, REPAIR 2. ACFT WAS GROUNDED.Aug 30, 2013 · N742AX · Boeing 767232 · Fuselage Main, Longeron/StringerSDR ABXA20130830563Floorbeam · corrodedCORROSION UNDER NUTPLATES ON FLOORBEAM UPPER TEE BS 610, RBL 18 - 30. R & R UPPER TEE IAW SRM 51-40-02. ACFT WAS GROUNDED.Aug 30, 2013 · N742AX · Boeing 767232 · Fuselage Main, Floor BeamSDR ABXA20130911001Channel · corrodedBULK CARGO , AFT DOOR FRAME, TOP CORNER IS A CORRODED STRINGER TIE. R & R STRINGER TIE, END FITTING IAW SRM 51-40-02 AND DWG 146T3007. PN 146T3007, CHANNEL, SKIN PANEL, CORRODED BS1461, STR 24; ACFT WAS GROUNDED.Aug 28, 2013 · N742AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA20130827556Stringer · corrodedAFT LOWER CARGO BAY STRINGER 35R JUST FWD OF BS 1263 WAS CORRODED. R & R CORRODED STRINGER FROM BS 1254 TO 1259 IAW SRM 53-00-03. ACFT WAS GROUNDED.Aug 27, 2013 · N742AX · Boeing 767232 · Fuselage Main, Longeron/StringerSDR ABXA20130827536Seat Track · corrodedUPPER CARGO, BS 355, LEFT BL33, SEAT TRACK IS CORRODED. R & R SEAT TRACK IAW IA DWG 36853-16-90621, SF SRM 51-40-02 PG 7, SH 4 & REA NR B653-60668-MR. ACFT WAS GROUNDED.Aug 27, 2013 · N742AX · Boeing 767232 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA20130827518Skin · debondedLT HORIZONTAL STAB UPPER SKIN HONEYCOMB DISBONDED FROM SKIN AUX SPAR STA 127-157, VIEWED FROM INSIDE L/E AUX SPAR. REMOVED LT HORZ STAB UPPER SKIN, SENT OUT FOR REPAIR ON R501623345, REINSTALLED LT HORIZONTAL STABILIZER UPPER SKIN AT STA 127 TO 157 IAW SRM 51Aug 27, 2013 · N742AX · Boeing 767232 · Horizontal Stabilizer, Plate/SkinSDR ABXA20130826520Door Frame · corrodedBS 1461 S32L WL 133, AFT LOWER CORNER OF BULK CARGO DOOR CUTOUT IS CORROSION . REPAIRED IAW SRM 50-70-13. ACFT WAS GROUNDED.Aug 26, 2013 · N742AX · Boeing 767232 · Fuselage Main, StructureSDR ABXA20130823537Beam · damagedR1 DOOR BS 841 INTERIOR BEAM SECOND FROM TOP, AFT AREA. REMOVED & REPLACED BEAM IAW SRM 51-10-02. ACFT WAS GROUNDED.Aug 23, 2013 · N742AX · Boeing 767232 · Fuselage Main, StructureSDR ABXA20130823533Stringer · corrodedAFT LOWER CARGO STRINGER 37R BETWEEN BS 1197 & 1219 CORRODED. REMOVED CORRODED SECTION OF STRINGER 37R, SPLICED IN NEW STRINGER SECTION IAW SRM 53-00-03, FIG 201 REPAIR 2. ACFT WAS GROUNDED.Aug 23, 2013 · N742AX · Boeing 767232 · Fuselage Main, Longeron/StringerSDR ABXA20130822532Stringer · corrodedAFT LOWER CARGO STRINGER 39R BETWEEN BS 1197 & 1219 CORRODED. R & R CORRODED STRINGER IAW SRM 53-00-03. ACFT WAS GROUNDED.Aug 22, 2013 · N742AX · Boeing 767232 · Fuselage Main, Longeron/StringerSDR ABXA20130821541Web · corrodedSEVERAL AREAS OF WEB CORROSION IN THE BALLMAT AREA. R & R WEB 5, BS 1263-1285 & 1285 -1329 IAW SRM 51-40-02 AND 53-60-53. PANEL, PN: 451T2504, LOC: FS1285-FS1329/RBL 24.92-33.15. ACFT WAS GROUNDED.Aug 21, 2013 · N742AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA20130821531Stringer · corrodedFS 412 - 434, STRINGER 34R CORRODED INCLUDING SPLICE WITH RIVETS PULLING THROUGH. INSTALLED NEW SECTION OF STRINGER FROM BS 412 TO 434 IAW SRM 51-40-02. ACFT WAS GROUNDED.Aug 21, 2013 · N742AX · Boeing 767232 · Fuselage Main, Longeron/Stringer
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