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 IXXA20161111087Keelbeam · corrodedCORROSION ON LOWER KEEL BEAM AT BS 808 RBL 9. BLENDED AREA IAW SRM 53-50-12. PERFORMED ULTRASONIC INSPECTION IAW NDTM PART 4 51-00-10 PARAGRAPH 2. HIGH FREQUENCY EDDY CURRENT SCAN IAW NDTM PART 6 51-00-19, NO CORROSION INDICATION FOUND IAW REA 47224REA09. GESep 7, 2016 · N739AX · Boeing 767232 · Fuselage Main, KeelSDR IXXA20161111086Keelbeam · corrodedCORROSION UNDER NUTPLATE ON KEEL BEAM AT BS 790 RBL 9. BLENDED AREA IAW SRM 53-50-12. PERFORMED ULTRASONIC INSPECTION IAW NDTM PART 4. 51-00-10 PROCEDURE 2. HIGH FREQUENCY EDDY CURRENT IAW SRM NDTM PART 6. 51-00-19. NO CORROSION INDICATION IAW REA 47224REA09 GSep 7, 2016 · N739AX · Boeing 767232 · Fuselage Main, KeelSDR IXXA20170320207Hinge · corrodedHORIZONTAL STAB RIGHT PIVOT PIN HINGE FITTING INBD AND OTBD BUSHINGS ARE CORRODED. REPAIRED THE FITTINGS IAW ED 47224REA08.Sep 6, 2016 · N739AX · Boeing 767232 · Horizontal Stabilizer StructureSDR IXXA20170320206Hinge · corrodedHORIZONTAL STAB LT PIVOT PIN HINGE FITTING INBD AND OTBD BUSHINGS ARE CORRODED. REMOVED AND REINSTALLED THE HORIZONTAL STAB PIVOT PIN FITTING IAW SRM 51-40-02 AND DRAWING 148T2740.Sep 6, 2016 · N739AX · Boeing 767232 · Horizontal Stabilizer StructureSDR IXXA20161117115Floor Support · corrodedCORROSION AROUND NUTPLATES ON THE LEFT SLOPING FLOOR SUPPORT AT FORWARD WALL BS 1087. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS FABRICATED A NEW FLOOR SUPPORT AND REPLACED IAW SRM 51-40-02, 53-00-53, AND DRAWING 453T1719. AIRCRAFT GROUNDEDSep 6, 2016 · N739AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR IXXA20161117110Support · corrodedLEFT WING TRAILING EDGE PANEL SUPPORT HAS CORROSION AND IS LOOSE. AIRCRAFT GROUNDED. REMOVED AND REPLACED THE PANEL SUPPORT IAW SRM 51-40-02 PARAGRAPH 7D AND 9B.Sep 6, 2016 · N739AX · Boeing 767232 · Trailing Edge FlapsSDR IXXA20161007079Pivot · corrodedHORIZONTAL STAB RIGHT PIVOT PIN HINGE FITTING INBOARD AND OUTBOARD BUSHINGS ARE CORRODED. REPAIRED THE FITTINGS IAW ENGINEERING DOCUMENT 47224REA08. ACFT GROUNDED.Sep 6, 2016 · N739AX · Boeing 767232 · Horizontal Stabilizer StructureSDR IXXA20161007078Pivot · corrodedHORIZONTAL STAB LEFT PIVOT PIN HINGE FITTING INBOARD AND OUTBOARD BUSHINGS ARE CORRODED. REMOVED AND REINSTALLED THE PIVOT FITTING AFTER REWORK WAS COMPLETED IAW SRM 51-40-02 AND DWG 148T2740. ACFT GROUNDED.Sep 6, 2016 · N739AX · Boeing 767232 · Horizontal Stabilizer StructureSDR IXXA20161111103Angle · corrodedAFT LOWER CARGO BS 1540 STRINGER 31L FRAME ANGLE FORWARD OF OUTFLOW VALVE IS CORRODED. FOUND TO BE OUT OF LIMITS. FABRICATED A NEW FRAME ANGLE IAW DRAWING 146T50002. INSTALLED A NEW FRAME ANGLE IAW SRM 51-40-02 PARAGRAPH 7.Aug 31, 2016 · N739AX · Boeing 767232 · Fuselage Main, FrameSDR IXXA20161117138Skin Panel · corrodedFOUND CORROSION UNDER TRAILING EDGE SKIN PANEL AT WS 432 ON TOP OF WING. REMOVED CORROSION, REPAIRED AREA IAW REA 47224REA07. AIRCRAFT GROUNDED.Aug 25, 2016 · N739AX · Boeing 767232 · Wing, Plate/SkinSDR ABXA20160824142Plate · corrodedLEFT REAR SPAR OF CENTER WING BOX HAS CORROSION AT THE BEARING PLATE. REMOVED AND INSTALLED SERVICEABLE LT REAR SPAR BEARING PLATE IAW ARM 51-40-02. SDR INFORMATION: CORRODED LEVEL 2, PN: 111T1008-1, BEARING PLATE, EXACT FS/BS LOCATION ON ACFT: FROM FS 955 TAug 24, 2016 · N750AX · Boeing 767232 · Fuselage Main, Attach FittingsSDR ABXA20160823136Skin · corrodedCORROSION FOUND ON INTERNAL LEFT BS 955 FUSELAGE SKIN. REPAIRED THE SKIN. AIRCRAFT WAS GROUNDED.Aug 23, 2016 · N750AX · Boeing 767232 · Fuselage Main, Plate/SkinSDR ABXA20160823129Doubler · corrodedRIGHT PRESSURE DECK DOUBLER, PN 145T8754-26 IS CORRODED, FS 976. FABRICATED NEW DOUBLER IAW B653-62149-MR. DOUBLER WILL BE INSTALLED ON EA5300014-003. CORRODED LEVEL 2, PN 145T8754-26, DOUBLER, FS/BS LOCATION, FS 976, STR/WS LOCATION, RBL 97-98. ACFT WAS GAug 23, 2016 · N750AX · Boeing 767232 · Fuselage Main, BulkheadSDR IXXA20161111089Bracket · corrodedRIGHT OUTBOARD AILERON POSITION TRANSMITTER MOUNTING BRACKET HAS AREA OF CORROSION. FABRICATED AND INSTALLED MOUNTING BRACKET IAW DWG 251T1011 AND ENGINEERING DOCUMENT 47224FAB01.Aug 19, 2016 · N739AX · Boeing 767232 · Wing, Attach FittingsSDR ABXA20160816130Skin · corrodedCORROSION FOUND AROUND FASTENER HOLES ON INTERNAL SKIN BS 955. REPAIRED IAW REA B653-62159-MR. THE AIRCRAFT WAS GROUNDED.Aug 16, 2016 · N750AX · Boeing 767232 · Fuselage Main, Plate/SkinSDR ABXA20160812131Failsafe · corrodedCORROSION AND CRACKS FOUND AROUND FASTENER HOLES ON LEFT FAIL SAFE STRAP BS 955. A NEW FAIL SAFE STRAP WAS INSTALLED. THE AIRCRAFT WAS GROUNDED.Aug 12, 2016 · N750AX · Boeing 767232 · Fuselage Main, StructureSDR ABXA20160811143Pressure Deck · corrodedLEFT PRESSURE DECK WEB IS CORRODED. FABRICATED NEW LT PRESSURE WEB FROM 2024-T3 0.125, PO 0085417 IAW DWG 145T8752 AND IAW SAMPLE. 2 EA WEB EDGES OF WEB WERE MILLED IAW SAMPLE. TREATED AND PRIMED WEB IAW SOPM 20-41-02, AND PAINTED WEB IAW AMM 51-21-02. CORAug 11, 2016 · N750AX · Boeing 767232 · Fuselage Main, BulkheadSDR ABXA20160811135Skin · corrodedCORROSION FOUND ON INTERNAL BS 955 SKIN. REPAIRED IAW EA 5300013-004 AND 47008ORD09. AIRCRAFT WAS GROUNDED.Aug 11, 2016 · Boeing 767232 · Fuselage Main, Plate/SkinSDR ABXA20160810134Failsafe · corrodedFAILSAFE STRAP HAS CORROSION OUTSIDE THE TRIMABLE AREA. A NEW FAILSAFE STRAP INSTALLED IAW EA 5350013-007. THE AIRCRAFT WAS GROUNDED.Aug 10, 2016 · N750AX · Boeing 767232 · Fuselage Main, FrameSDR ABXA20160810128Pressure Deck · corrodedRIGHT PRESSURE DECK WEB IS CORRODED. NEW WEB WAS FABRICATED FROM 2024-T3 .125 CLAD ALUMINUM PO 0085417, 2 EA EDGES WERE MACHINED IAW SAMPLE, AND WEB WAS TREATED PRIMED AND PAINTED IAW DWG 145T8752 AND AMM 51-21-02. TO BE INSTALLED ON DOC 47008ORD04. CORRODEAug 10, 2016 · N750AX · Boeing 767232 · Fuselage Main, BulkheadSDR SPUY201608100009Skin · corrodedAFT CARGO BAY INTERNAL SKIN CORRODED BS 1351 STRINGER 29R.Aug 10, 2016 · N741AX · Boeing 767232 · Fuselage Main, Plate/SkinSDR SPUY201608090008Skin · crackedLOWER FUSELAGE SKIN CRACKED BS 1562 - 1640, STRINGER 24L.Aug 9, 2016 · N741AX · Boeing 767232 · Fuselage Main, Plate/SkinSDR SPUY201608090007Structure · corrodedBULK CARGO DOOR CORRODED BS 1461, S30 - 31L.Aug 9, 2016 · N741AX · Boeing 767232 · Cargo/Baggage DoorsSDR IXXA20170320208Skin · corrodedBS 1582, STRINGER 10R SKIN IS CORRODED. REPAIRED IAW SRM 53-00-01, REPAIR 1 AND ED 47224REA06.Aug 8, 2016 · N739AX · Boeing 767232 · Fuselage Main, Plate/SkinSDR IXXA20161007080Skin · corrodedBS 1582 AT STRINGER 10R SKIN IS CORRODED. REPAIRED IAW SRM 53-00-1 REPAIR 1 AND ENGINEERING DOCUMENT REA 47224REA06, AIRCRAFT GROUNDED.Aug 8, 2016 · N739AX · Boeing 767232 · Fuselage Main, Plate/SkinSDR ABXA20160729127Longeron · corrodedCORROSION ON OTBD CHORD OF RT LONGERON COMMON TO THE ATTACH POINT FOR THE SHEAR LINK AT FS 965. REMOVED CORROSION FROM OTBD CHORD OF RT LONGERON COMMON TO THE ATTACH POINT FOR THE LINK AT FS 964. REPAIRED IAW REA NR B653-62145-MR. CORRODED LEVEL 2, PN 145T8Jul 29, 2016 · N750AX · Boeing 767232 · Fuselage Main, Longeron/StringerSDR IXXA20161117116Sidewall Support · corrodedCORROSION ON AFT LOWER CARGO FORWARD WALL, CENTER AND CENTER RIGHT WALL SUPPORTS AND ANGLE BRACKET AT THE BOTTOM. FABRICATED NEW LOWER FORWARD LINE CLAMP IAW 272T4515 ASSEMBLY-7. . INSTALLED IAW SRM 51-40-02.Jul 27, 2016 · N739AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR IXXA20161111091Doubler · corrodedLEFT STABILIZER TRAILING EDGE AT OUTBOARD END HAS DOUBLER CORRODED. FOUND OUT OF LIMITS. FABRICATED A NEW DOUBLER, AND REPLACED IAW SRM 55-10-13, 51-40-02, DWG 18371700.Jul 25, 2016 · N739AX · Boeing 767232 · Horizontal Stabilizer, Plate/SkinSDR PCSA2016062001A/C Pack · fumesAIR CONDITIONING PACKS EMITTING FUMES INTO COCKPIT DURING CLIMB, CRUISE AND DESCENT.Jun 18, 2016 · N739AX · Boeing 767232 · Air Distribution SystemSDR IXXA20160420019Skin · corrodedTHE FOLLOWING WORK WAS ACCOMPLISHED DURING VISIT BY MX & ENGINEERING SERVICES. FUSELAGE SKIN, PN 146T3531-3, CORRODED AT STATION 1414, STRINGER 35R INBD OF AFT DRAIN MAST AT SKIN LAP. THE FUSELAGE SKIN WAS REPAIRED IAW SRM 53-00-01 REPAIR 12 FIGURE 201 & 469Apr 20, 2016 · N762CX · Boeing 767232 · Fuselage Main, Plate/SkinSDR IXXA2016041300099Hose · blownEICAS MESSAGE "C HYD QTY", LOSS OF ALL QTY LEADING TO C HYD FAILURE. FOUND HOSE BLOWN.Apr 13, 2016 · N762CX · Boeing 767232 · Hydraulic System, MainSDR IXXA20160429018Shear Tie · crackedDURING MX VISIT ACCOMPLISHED PERMANENT REPAIR FOR THE SHEAR TIE ATTACHED TO THE LT LONGERON LOCATED AT STATION 1746.25 & WL 258.44. WORK WAS ACCOMPLISHED IAW ENGINEERING DOCUMENT 53-767-5445 DATED 04 08 16 REV 3, NR0001, APPROVED REPAIR ON 8110-3.Apr 9, 2016 · N763CX · Boeing 767232 · Fuselage Internal Mounting StructureSDR ABXA2016225005Torque Tube · crackedDURING PREPARATION OF FLAP REMOVAL, WHILE INSTALLING NR 3 SPOILER LOCK, FOUND ACTUATOR TO WING OTBD ATTACH LUG BROKEN OFF & INBD LUG BADLY WORN. R & R NR 3 SPOILER ACTUATOR TORQUE TUBE IAW AMM 27-61-01, & 27-61-02. SDR CRACK 3 INCHES, PN 1134T1440-1, SN NSN,Feb 25, 2016 · N744AX · Boeing 767232 · Drag Control SystemSDR ABXA2016217003Software · defectiveTHE LT & RT PRIMARY FLIGHT DISPLAYS FLASHED NUMEROUS TIMES THEN BOTH FAILED. THE LT & RT NAVIGATIONAL DISPLAYS FLASHED & FAILED INTERMITTENTLY. REPLACED THE CTR & RT DATA CONCENTRATOR UNITS. THE CAUSE OF THE DISPLAY UNITS FLASHING & FAILING WAS INCOMPATIBLEFeb 17, 2016 · N740AX · Boeing 767232 · Flight Management Computing Software SystemSDR IXXA20160219004faultyEMERGENCY LIGHT UNARMED. R & R DRAWER ASSEMBLY & BULBS. OPERATIONAL CHECKED SATISFACTORY IAW AMM 33-13-01.Feb 13, 2016 · N762CX · Boeing 767232 · Emergency LightingSDR IXXA20151107118Skin · crackedSKIN CRACK & PROBABLE CORROSION AT APPROX FS 1339, LONGERON 35L. REMOVED DAMAGED AREA, FABRICATED FILLER & DOUBLER, INSTALLED REPAIRED PARTS IAW SRM 51-30-01. COMPLIED WITH HFEC OF AREA WHERE DAMAGE WAS REMOVED IAW NDT PART 6 51-00-19. NO DEFECTS NOTED.Nov 7, 2015 · N763CX · Boeing 767232 · Fuselage Main, Plate/SkinSDR PCSA2015092302Circuit Breaker · poppedLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF.Sep 22, 2015 · N739AX · Boeing 767232 · Landing Gear Retraction/Extension SystemSDR ABXA20150826150Skin · corrodedCOMPLIED WITH DETAILED INSPECTION OF SURFACE OF SKIN AT STATION 955 FAIL-SAFE CUT OUT. FOUND CORROSION & MINOR TOOLING MARKS. REMOVED & SPOT FACED SKIN CORROSION IAW REA B653-61707-MR & 47008ORD10. SDR INFO CORRODED, PN 145T3420, SN NSN, PART NAME RT SKIN, Aug 26, 2015 · N745AX · Boeing 767232 · Fuselage Main, Plate/SkinSDR ABXA20150825145Doubler · corrodedLEFT PRESS DECK FWD DOUBLER IS CORRODED BEYOND LIMITS. REFERENCE DWG 145T8752. NEW FWD LT PRESS DECK FWD DOUBLER, PN 145T8754-33 INSTALLED ON JC 53500013-003 & DOCUMENT 47008ORD03, TAG 1409197. SDR INFO CORRODED, PN 14578754-33, PART NAME DOUBLER, SN NSN, FAug 25, 2015 · N745AX · Boeing 767232 · Fuselage Main, BulkheadSDR IXXA20150826078Light · inoperativeEMERGENCY LIGHT ASSEMBLY AT L1 DOOR IS INOPERABLE. RELAMPED EMER LIGHT JUST OUTSIDE L1 DOOR AREA. OPERATIONAL CHECKED SATISFACTORY IAW AMM 33-51-06. ACFT RELEASED TO SERVICE.Aug 25, 2015 · N762CX · Boeing 767232 · Emergency LightingSDR ABXA20150821146Stringer · corrodedLEFT FWD I BEAM STRINGER AT LBL 85.90 IS CORRODED BEYOND LIMITS. REFERENCE DWG 145T8752. FABRICATED NEW SECTION OF I BEAM FROM BAC 1518-751 2024-73511, PO 0037419 IAW REA B653-61698. SDR INFO CORRODED, PN 14578752-37, SN NSN, PART NAME STRINGER, FROM STATIOAug 21, 2015 · N745AX · Boeing 767232 · Fuselage Main, Longeron/StringerSDR ABXA20150821144Pressure Deck · corrodedLEFT PRESS DECK WEB IS CORRODED BEYOND LIMITS IAW DWG 145T8752. FABRICATED NEW WEB FROM 2024-T3 .125" PO 0057631. MACHINED EDGES ANODIZED, PRIMED & PAINTED IAW DWG 145T8752 & MIL-A-8625 TYPE I CLASS 1 & SRM 51-40-05. SDR INFO CORRODED L2, PN 14578752-235, PAug 21, 2015 · N745AX · Boeing 767232 · Fuselage Main, BulkheadSDR ABXA20150820124Angle · corrodedFOUND FWD LT BILGE PANEL, AFT MOUNT ANGLE CORRODED & NUTPLATES CORRODED. R & R UPPER CHORD ASSEMBLY AT STATION 544 IAW SRM 51-40-02 PAR 4B 1-5 & SRM 51-40-02 PARA 4 & PARA 7, SOPM 20-50-01, AMM 25-53-03 4, THROUGH COMP AMM 53-01-05 3C 3 TO 3C 4 & AMM 25-53-01Aug 20, 2015 · N745AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA20150817143Web · corrodedFLOOR WEBBING AT FS 550, RBL 36 HAS A HOLE CORRODED THROUGH WEB, WEB IS APPROX 5 FEET IN LENGTH. R & R FLOOR WEB AT FS 550, RBL 36 IN FLC IAW SRM 51-40-02. SDR INFO CORRODED LEVEL 2, PN 451T2504-17, NAME PANEL, FS & BS FS 522 - 642, EXACT STRINGER & WS RBL 3Aug 17, 2015 · N745AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA20150815148Strap · corrodedDURING DETAILED VISUAL INSPECTION OBSERVED CORROSION & CRACKS AROUND HOLES COMMON TO FAILSAFE STRAP & T FITTING. PREVIOUSLY MENTIONED ON NON-ROUTINE 1369. TRIMMED OUT CRACKED & CORRODED AREA OF FAILSAFE STRAP AS WRITTEN IAW EA 53500013-003 & DOCUMENT 47008ORAug 15, 2015 · N745AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA20150815147Strap · crackedDURING ROTARY HOLE SCAN, FOUND 2 CRACKS IN HOLES COMMON TO THE FAIL SAFE STRAP. ACCOMPLISHED TRIM OUT IAW EA5350013-003 & DOCUMENT 47008ORD03. CRACKED 1/4", PN 145T2524, PART NAME, LEFT FAIL SAFE STRAP, SN NSN, FS & BS LOCATION STATION 955. ACFT WAS GNDED.Aug 15, 2015 · N745AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA20150814149Strap · crackedDURING HFEC SURFACE SCAN FOUND END OF CRACKS MENTIONED ON NON-ROUTINE 1369 & MARKED END OF CRACK LOCATIONS WITHIN TRIM OUT LIMITS. ACCOMPLISHED TRIM OUT OF FAIL-SAFE IAW EA 53500013-003 & DOCUMENT 47008ORD03. SDR INFO 1/4" CRACKED, PN 145T2524, PART NAME, LEAug 14, 2015 · N745AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA20150803125Skin · damagedSKIN HAS A LARGE CREASE GOING THROUGH LAP SPLICE AT LT FS 1395, STRINGER 36L. REPAIRED LAP SPLICE CREASE IAW REA B653-61583-MR & SRM 53-00-21. SDR INFO, PN 146T3240 & 146T3230, SN N/A, PART NAME FUSELAGE SKINS, FS & BS LOCATION ON ACFT FS 1395 TO 1417, STRINAug 3, 2015 · N745AX · Boeing 767232 · Fuselage Main, Plate/SkinSDR ABXA20150731131Skin · corrodedDDR ITEM NR 21, REINFORCED REPAIR DOUBLER FOUND ON LT FUSELAGE, STATION 1654, STRINGER 33L - 34L. REPAIRED DAMAGED SKIN IAW SRM 53-00-01 REPAIR 29. SDR, CORRODED, PN 148T3211, PART NAME SKIN, SN NSN, FS & BS LOCATION 1651 TO 1661, STRINGER & WS LOCATION, STRJul 31, 2015 · N745AX · Boeing 767232 · Fuselage Main, Plate/SkinSDR ABXA20150731130Skin · corrodedDDR ITEM NR 8, REINFORCED DOUBLER REPAIR FOUND ON LT FUSELAGE, STATION 441 - 451, STRINGER 32L. DDR NR 8 DOC REPAIR LT FUSELAGE HAS BEEN COMPLIED WITH IAW REA B653-61674-MR. CORRODED LEVEL 2, PN 143T3210-1, PART NAME SKIN, SN N/A, FS & BS FROM 442 TO 453, STJul 31, 2015 · N745AX · Boeing 767232 · Fuselage Main, Plate/Skin
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