Boeing 767-281
Service difficulty reports · 1,831
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '767281' 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.
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 = '767281' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UIEA2015081400432Strap · corrodedCORROSION ON STRAP ON FLC DOOR CUT OUT UNDER SLOPING PANEL, UPPER ATTACH BRACKET. REMOVED CORROSION IAW REA 47169REA10.SDR ABXA20150730089Angle · crackedFRONT SPAR TO LE ANGLE, ABOVE & AFT OF SLAT PDU CRACKED AT LOWER END. REMOVED & INSTALLED SERVICEABLE LOWER FRONT SPAR TO LE ANGLE ABOVE & AFT OF SLAT PDU IAW SRM 51-40-02 PARA 7, NO LEAKS NOTED. CRACKED 2 INCHES, PN 14T1342U105, PART NAME ANGLE, WING LE, SNSDR ABXA20150729110Support Beam · corrodedRIGHT WING UPPER TE PANEL SUPPORT BEAM AT WS 349 - 325 HAS A HOLE CORRODED THRU AT A NUTPLATE. R & R RT WING TE PANEL SUPPORT BEAM AT WS 349 - 325 IAW SRM 51-40-02 PARA 7 D. CORRODED L2, PN 113T1632-70AX, SN N/A, PART NAME SUPPORT, STR & WS LOCATION ON ACFT SDR ABXA20150729108Structure · corrodedSMALL AREA OF CORROSION ON UPPER TE PANEL ATTACH CHORD ON INBD END AS SEEN THRU PANEL 552AB OPENING. R & R ATTACH CHORD SECTION IAW SRM 57-51-02. CORRODED L2, PN 113T1406-5, SN N/A, PART NAME CHORD, WS LOCATION ON ACFT WS 280 - 298, ACFT WAS GNDED.SDR ABXA20150728109Support Beam · corrodedRIGHT WING, TE UPPER CHORD OF THE INBD SPOILER SUPPORT BEAM IS CORRODED AT WS 365 - 370. INSTALLED NEW CHORD PART 113T1406-6 IAW REA B657-61649MR & SRM 51-40-02. CORRODED L2, PN 113T1406-6, SN N/A, PART NAME CHORD, FS & BS LOCATION ON ACFT RT WING TO TE, STRSDR ABXA20150728098Support · corrodedREAR SPAR TO TE UPPER PANEL, ATTACH CHORD AT WS 360, CORRODED AROUND NUTPLATES AT AFT END. R & R REAR SPAR TO TE UPPER PANEL ATTACH CHORD AT WS 360 IAW DWG 113T1626 & REA B657-61627. CORRODED L2, PN 113T1626-44, SN NONE, PART NAME CHORD, UPPER SUPPORT, STRINSDR UIEA2015072900378D-Ring · missingDESCENT, HARNESS IN FLIGHT DECK UPPER STORAGE POUCH OUTBOARD HARNESS DOES NOT HAVE A D RING. INSTALLED D RING CARABINEER ON SAFETY HARNESS IAW AMM 25-61-03.SDR ABXA20150724119Longeron · crackedUPPER LONGERON WEB HAS A 2 INCH CRACK AT FS 1800 - 1806. INSTALLED NEW WEB & BRACKETS IAW SRM 51-40-02. SDR INFO, CRACK 2 INCHES, PART NUMBER 148T9120-11, PART NAME LONGERON WEB, SN NA, EXACT FS & BS LOCATION ON ACFT 1800 TO 1806. ACFT WAS GNDED.SDR ABXA20150724096Structure · corrodedWING TE LOWER PANEL ATTACH CHORD, 32 INCHES FROM REAR SPAR & 25 INCHES FROM OTBD SIDE OF INBD FLAP, OTBD HINGE PARALLEL TO REAR SPAR SPLIT ON EDGE. R & R PANEL ATTACH CHORD FOR PANEL 652JB IAW SRM 51-40-02 & REA B657-61646-MR. CORRODED LEVEL 2, PN 113T1407-2SDR ABXA20150723107Channel · corrodedALL THREE HYD LINE CLAMP BLOCKS CORRODED AT BRACKET ATTACH POINT AS SEEN THRU PANEL 552AB OPENING. REMOVED, FABRICATED & REPLACED THREE HYD LINE CLAMP BOCKS INSIDE PANEL 552AB OPENING IAW DWG 113T1101 & SRM 51-40-02. CORRODED L2, PN 65B80254-304, SN N/A, PARSDR ABXA20150722101Structure · crackedLEFT 1809 OUTER CHORD SHOWS A CRACK INDICATION, AT 3 EACH FASTENERS IN AREA 3, ON THE AFT SIDE OF CHORD. REPLACE LT 1809-5 CHORD SECTION, PN 015T1059-3 IAW REA B653-61651-MR. SDR INFO CRACKED 1/8", NO CRACK HOLES WERE ELONGATED. PN 015T1059-3, SN NA, PART NASDR ABXA20150722097Support Rib · corrodedWING REAR SPAR TO TE PANEL ATTACH BEAM FWD OF HINGED ACCESS PANEL 651YBX, SPLIT ON EDGE. REMOVED PANEL 651YBX. R & R PANEL ATTACH BEAM IAW SRM 51-40-02 PARA 7D & REA B657-61642. RE-INSTALLED PANEL 651YBX IAW SRM 51-40-02 PARA 7D. CORRODED LEVEL 2, PN 113T1SDR ABXA20150721100Panel Support · corrodedLOWER WING TE PANEL ATTACH CHORD AT WS 1054, SPLIT ON EDGE INBD OF AUX TANK VENT. R & R LT WING TE PANEL SUPPORT CHORD WS 1054 IAW SRM 51-40-02 & REA B657-61637. CORRODED L2, PN 113T1676-19, SN NSN, PART NAME PANEL SUPPORT CHORD, STRINGER & WS LOCATION ON ACSDR ABXA20150721099Panel Support · corrodedLOWER TE PANEL, ATTACH CHORD AT WS 827, CORRODED AROUND NUTPLATE. R & R LT WING TE PANEL SUPPORT CHORD IAW SRM 51-40-02, EA B657-61631. CORRODED L2, PN 113T1672-5, SN NSN, PART NAME PANEL SUPPORT, STRINGER & WS LOCATION ON ACFT WS 827. ACFT WAS GNDED.SDR ABXA20150721094Panel Support · corrodedREAR SPAR TO WING TE LOWER PANEL ATTACH CHORD SPLIT ON EDGE, AT WS 930. R & R RT WING TE LOWER PANEL ATTACH CHORD AT WS 930 IAW SRM 51-40-02 & REA B657-61634. CORRODED L2, PN 113T1683-28, SN N/A, PART NAME PANEL SUPPORT, STRINGER & WS LOCATION ON ACFT WS 930SDR ABXA20150721093Panel Support · corrodedREAR SPAR TO TE LOWER PANEL ATTACH CHORD SPLIT ON EDGE, AT WS 944. R & R RT WING TE LOWER PANEL ATTACH CHORD, AT WS 9644 IAW SRM 51-40-02 & REA B657-61636. CORRODED L2, PN 113T1675-22, SN N/A, PART NAME PANEL SUPPORT, STRINGER & WS LOCATION ON ACFT WS 944. SDR ABXA20150721092Panel Support · corrodedREAR SPAR TO TE LOWER PANEL ATTACH CHORD SPLIT ON EDGE, AT WS 1054, AT AUX TANK VENT. R & R RT WING TE LOWER PANEL ATTACH CHORD WING STATION 1054 IAW 51-40-02 & REA B657-61635. CORRODED L2, PN 113T1676-22, SN NA, PART NAME PANEL SUPPORT, STRINGER & WS LOCATIOSDR ABXA20150720102Beam · corrodedREAR SPAR TO TE PANEL, ATTACH BEAM UPPER CHORD EXFOLIATED AROUND OTBD NUTPLATES AT STATION 288, INBD OF GEAR TRUNNION. REMOVED PANELS FOR ACCESS, REMOVED CORRODED UPPER CHORD. INSTALLED NEW UPPER CHORD, PN 113T1623-125, RE-INSTALLED, REMOVED PANELS, PANELS TSDR ABXA20150717095Structure · corrodedUPPER CHORD SPLIT ON EDGE & CORRODED AROUND NUTPLATES ON REAR SPAR TO TE BEAM, AT WS 285, 14 INCHES FROM REAR SPAR M, INBD OF GEAR TRUNNION. REMOVED RT WING UPPER TE PANELS. R & R TE UPPER CHORD AT WW 285.14 IAW SRM 51-40-02 PARA 4.6 & 7D. INSTALLED PANEL ASDR ABXA20150715104Angle · corrodedLOWER ANGLE AT KEEL TO STATION 999 BULKHEAD CORRODED. REMOVED PANEL 149AL FOR ACCESS. REMOVED LOWER ANGLE, FOUND OUT OF LIMITS. REPLACED LOWER ANGLE IAW DWG 145T8610, INSTALLED LOWER ANGLE IAW SRM 51-40-02. INSTALLED PANEL 149 AL IAW SRM 51-40-02. CORRODESDR ABXA20150713120Stiffener · corrodedLEFT WING TE PANEL SUPPORT AT WS 280 HAS A CORRODED T STIFFENER, 31" AFT OF THE WING SKIN TE, PN 113T1623-19. REMOVED CORRODED STIFFENER, FABRICATED NEW FROM & 10136-2001 PO 0020699, TAG 1386185 IAW DWG 113T1623. INSTALLED NEW STIFFENER IAW SRM 51-40-02. SDSDR ABXA20150710091Strut · corrodedNUMBER 2 SLAT OTBD AUX TRACK ATTACH FITTING, LOWER OTDB STRUT CORRODED AROUND NUTPLATE AT FWD END. R & R STRUT IAW DWG 114T2224 & SRM 51-40-02 STEP 7. CORRODED L2, PN 114T2224-15, PART NAME STRUT, STRINGER LOCATION WS 937 4 EDGE. ACFT WAS GNDED.SDR ABXA20150708118Support Fitting · corrodedLEFT WING NR 1 FLAP SUPPORT, RIB NR 4 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLE TO FINAL SIZE OF .7495 .7505 ON FLAP SUPPORT NR 1, HOLE NR 4 IAW REA B657-61641-MR. SDR INFO CORRODED L2, PN 113T1345-43, SN NONE, PART NAME NR 1 FLAP SUPPORT FISDR ABXA20150708117Support Fitting · corrodedLEFT WING NR 1 FLAP SUPPORT, RIB NR 3 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLE TO FINAL SIZE OF .7495 .7505 ON FLAP SUPPORT NR 1, HOLE NR 3 IAW REA B657-61641-MR. SDR INFO CORRODED L2, PN 113T1345-43, SN NONE, PART NAME NR 1 FLAP SUPPORT FISDR ABXA20150708116Support Fitting · corrodedREAMED HOLE TO FINAL SIZE OF 3.7495 .7505 ON FLAP SUPPORT NR 1, HOLE NR 2 IAW REA B657-61641-MR. CORRODED L2, PN 113T1345-43, SN NONE, PART NAME NR 1 FLAP SUPPORT FITTING, STRINGER & WS LOCATION ON ACFT WS 797. ACFT WAS GNDED.SDR ABXA20150708115Support Fitting · corrodedLEFT WING NR 1 FLAP SUPPORT, RIB NR 1 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLES TO FINAL SIZE OF .7495 & .7505 IAW REA NR B657-61641MR. SDR INFO CORRODED L2, PART NUMBER 113T1345-43, PART NAME NR 11 FLAP SUPPORT FITTING, STRINGER & WS LOCATSDR ABXA20150708114Support Fitting · corrodedRIGHT WING NR 7 FLAP SUPPORT, RIB NR 4 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLE TO FINAL SIZE OF .8745 & .88.55 IAW REA NR B657-61641-MR. CORRODED L2 PN 113T1345-48, PART NAME NR 7 FLAP SUPPORT FITTING, SN NSN, STRINGER LOCATION WB 61G.2. SDR ABXA20150708113Support Fitting · corrodedRIGHT WING NR 7 FLAP SUPPORT, RIB 11 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLE TO FINAL SIZE OF .8745 & .8755 IAW REA NR B657-61641-MR. SDR CORRODED L2, PN 113T1345-48, PART NAME NR 2FLAP SUPPORT FITTING, SN NSN, STRINGER LOCATION WB 61G.2.SDR ABXA20150708112Support · corrodedRIGHT WING NR 8 FLAP SUPPORT, RIB NR 3 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLE TO FINAL SIZE OF .7495 & .7505 IAW REA NR B767-61641-MR. SDR CORRODED L2, PN 113T1345-44, PART NAME 8 FLAP SUPPORT F1 WING, SN NSN, STRINGER LOCATION WS 807. ASDR ABXA20150708111Support Fitting · corrodedRIGHT WING NR 8 FLAP SUPPORT, RIB NR 2 HOLE SHOWS CRACK INDICATION WITH EDDY CURRENT. REAMED HOLE TO FINAL SIZE OF .7493 .7505 ON FWD SUPPORT NR 8, HOLE NR 2 IAW REA B767-61641-MR. SDR CORRODED L2, PN 113T1345-44, PART NAME 8 FLAP SUPPORT FITTING, SN NSN, STSDR ABXA20150707080Unknown · odorAFTER STARTING APU & TURNING ON PACK, STRONG ODOR OF JET FUEL NOTICED ON FLIGHT DECK. RESTARTED APU & CHECKED SYS WITH PACK ON IAW AMM 49-11-00. NO ODORS NOTICED. INSPECTED APU FOR OIL CONTAMINATION & INSPECTED WING ROOT AREAS FOR FUEL LEAKS. NO CAUSE OF OSDR ABXA20150706103Angle · corrodedLOWER ANGLE AT KEEL TO STATION 977 BULKHEAD LBL 5 CORRODED. R & R LOWER ANGLE KEEL STATION 977 IAW SRM 51-40-02 & DWG 145T8610. CORRODED L2, PN 145T8610-9, SN NSN, PART NAME ANGLE, FS LOCATION ON ACFT, 977 LT WW, KEEL STRINGER & WS LOCATION ON ACFT LBL 5. ASDR ABXA20150624090Rib · corrodedNUMBER 5 SLAT OTBD AUX TRACK, INBD LOWER STRUT CORRODED AROUND FWD NUTPLATE. REMOVED DAMAGED STRUT RIB & INSTALLED NEW STRUT RIB PN 114T2203 13AX IAW SRM 51-40-02. CORRODED LEVEL 2, PN 114T2203-15, PART NAME STRUT AIR LOAD RIB, FS & BS LOCATION LW, STRINGER SDR UIEA2015060400295A/C Pack · stiffLEFT THROTTLE EXTERIOR STIFF TO ADVANCE, RATCHETS WHEN THRUST LEVER ADVANCES. COMPLIED WITH FIM 76-11 FAULT TREE 805. THROTTLE LEVER FORCE IS 5 LBS, AUTO THROTTLE TEST 10 OK.SDR ABXA20150527067Smoke Detector · false activationSERVICE AREA SMOKE ALARM SOUNDED, NO SMOKE OBSERVED. CLEANED GRILL & DETECTOR UNIT. OPERATION CHECKED GOOD.SDR ABXA20150526066Smoke Detector · false activationLAVATORY SMOKE ALARM SOUNDED. NO SMOKE OBSERVED. LAVATORY SMOKE DETECTOR OPERATION CHECKED GOOD.SDR UIEA2015050900266Warning System · activatedAFTER TAKEOFF, RT PACK OFF, AFTER PACK OFF EICAS FWD EQUIP OVHT. RAN QRH CHECKLIST, MSG CONTINUED, ALSO NO COOLING LIGHT. EADI DISPLAYED FAILED AT 22.000 FT CABIN ALT EICAS MSG, AUTO CONTROLLER FAILED. PERFORMED FIM 21-51-811, NO FAULTS NOTED IAW WDM 21-51-SDR ABXA20150502068Mec · faultyADVANCED THRUST LEVER APPROX HALF WAY FOR TAKEOFF ON LT ENG & ENG WOULD NOT ACCELERATE. REPLACED LT ENG MAIN ENG CONTROL.SDR ABXA20150424037Panel Support · corrodedPANEL SUPPORT IN RT MLG WW CORRODED & SPLIT OUT APPROX 200 WS. R & R CHORD PART 113T1023-158 IN RT MLG WW AT APPROX STATION 200 IAW SRM 51-40-02. SDR INFO, CORRODED PN 113T1623-158, PART NAME CHORD, SN NSN, WS FROM 200 TO 200. ACFT WAS GNDED.SDR ABXA20150423038Splice Plate · corrodedLEFT WING UPPER SPLICE PLATE REQUIRES A REPLACEMENT SECTION INSTALLED FOR COI61410-001, REA B657-61466. REPLACED SPLICE PLATE IAW B657-61466. SDR INFO, CORRODED PN 114T0223-19, PART NAME SPLICE PLATE, SN NSN, STRINGER & WS LOCATION FROM 446 TO 519. ACFT WASSDR ABXA20150423036Structure · corrodedPANEL ATTACH LOWER CHORD FROM WING REAR SPAR TO TE AT WS 1054 CORRODED. LOWER CHORD AT TE WS 1054 CORRODED BEYOND LIMITS IAW SRM CH 57-51-02. INSTALL NEW CHORD PN 113T1676-21 IAW SRM CH 51-40-02. PART NUMBER 113T1676-21, PART NAME CHORD, SN NSN, WS LOC: 10SDR ABXA20150319032Unknown · odorHEAVY FUEL ODOR IN FLIGHT DECK WITH BOTH PACKS ON AFTER LANDING. PERFORMED FIM 21-00-801. GND CHECKED LT & RT PACK, INSPECTED PACKS. CHECKED FLIGHT DECK WITH PACK ON, NO FUEL ODOR NOTED. GND CHECKED GOOD. CAUSE OF REPORTED FUEL ODOR WAS NOT DETERMINED.SDR UIEA2015030500164Skin · corrodedCORROSION ON TOP OF WING AT FS 939 W STRINGER 2. REMOVED CORROSION, BLENDED AREA IAW REA 47136REA06.SDR UIEA2015030500165Rib · corrodedLEFT WING LES INTERNAL RIB IS CORRODED AT FWD UPPER CORNER & LOWER EDGE. R & R LES INTERNAL RIB WS 456 IAW REA 47136REA08, WORK ACCOMPLISHED SRM 51-40-02.SDR UIEA2015030500166Rib · corrodedLEFT WING LES INTERNAL RIB IS CORRODED ABOVE WIRE STANDOFF LOCATED AT APPROX LESS 479. FOUND CORROSION BEYOND LIMITS, REPAIRED AIR LOAD RIB IAW SRM 51-70-11.SDR UIEA2015030500167Skin · corrodedRIGHT OVERWING FUEL FILL PORT HAS CORROSION INSIDE OF TANK. REPAIRED AREA AROUND RT OVERWING FUEL FILL INSIDE TANK IAW AREA 47136, REA 04,47136, REA 09, & 47136 REA 10.SDR UIEA2015030500168Skin Panel · corrodedRIGHT WING OVERWING FUEL ACCESS HOLE HAS CORROSION ON UPPER SURFACE OF LIP. REMOVED FASTENERS FROM AREA & CLEANED CORROSION. FABRICATED & INSTALLED DOUBLER REPAIR TO AREA IAW REA 47136REA0, 47136REA09 & 47136REA10.SDR UIEA2015030500169Bushing · wornNUMBER 1 SUPPORT BEAM 1,2,3 HAS TWO EACH BUSHINGS WORN, LT WING. INSTALLED TWO EACH NEW BUSHINGS IN LT WING NR 1 SUPPORT BEAM 1,2,3 IAW REA 4713REA14.SDR UIEA2015030500171Rib · corrodedNUMBER 2 SLAT INBD AUX TRACK ATTACH FITTING LOWER OTBD STRUT CORRODED, AFT OF FITTING. R & R RT WING LOWER STRUT RIB AT STATION 884.732 IAW SRM 51-40-02.SDR UIEA2015030500170Beam · defectiveNUMBER 8 FLAP 1, 2, 3 BEAM HAS DEFECT ON THE .0620 INCH HOLE, DURING HFEC OPEN HOLE SCAN. REPAIRED HOLE TO REMOVE DEFECT & INSTALLED SERVICEABLE BUSHING IAW SRM 51-40-02, CMM 27-51-97 & REA 47136REA12.
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