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 ABXA201011090141Skin · chafedSKIN CHAFED THRU ON LEFT SIDE FUSELAGE WHOLE LOWER HORSE COLLAR OPERATES. REPAIRED AREA IAW 767 SRM 53-80-01.SDR ABXA201011170153Skin · crackedFUSELAGE SKIN CRACKED AT FS 1702, STRINGER 6L. CRACK IS .25 INCH LONG. REPAIRED DAMAGE AT FUSELAGE STA 1702, STRINGER 6L IAW B767 SRM 53-00-01. PRIMED AREA IAW B767 51-21-10-7.SDR ABXA201011170154Structure · damagedRIGHT CHORD STA 1809 HAS DEFECT INDICATIONS AT 2EA HOLES IN AREA 1 BELOW RUBSTRIP. REPAIRED RT OUTER CHORD STA 1809.5 IAW EA 53800002-003.SDR ABXA201011160152Fireseal · crackedNR 2 ENGINE OUTBOARD REVERSER INBOARD AFT FIRE SEAL MATING SURFACE IS CRACKED. REPAIRED AREA IAW B767 SRM 51-70-13.SDR ABXA201010010131Warning System · faultyTAKEOFF ROLL ABORTED DUE TO FAULTY FLAP WARNING. RECYCLED FLAP HANDLE. PERFORMED T/O CONFIG WARN ALERT CHECK IAW MM 31-51-00-5. OPS CHECK GOOD.SDR ABXA201011150151Mount · corrodedNR 1 ENG AFT MOUNT HAS SURFACE CORROSION. REMOVED AND REPLACED NR 1 ENGINE AFT MOUNT FROM STEP G1 TO G3 IAW AMM 71-2-04.SDR ABXA201010010125Panel · corrodedUPPER AND LOWER SURFACE OF REFUELING PANEL HAS AREAS OF CORROSION. REMOVED WIRE HARNESS TO FOM REMOVED CORROSION. TREATED PRIMED AND PAINTED. RE-INSTALLED WIRE HARNESS CONTINUITY CHECKED GOOD. OPS CHECK OF FUELING PANEL GOOD IAW B767 AMM 28-21-00-5 AND 28-SDR ABXA201010010130Skin Panel · damagedDURING TRIM OUT OF RIGHT SIDE FAIL-SAFE STRAP PER REA B653-58935-SB STEP 6 RT WING SKIN PANEL DAMAGED DURING CUTOUT PROCESS. POSSIBLE DAMAGE TO LONGERON SPLICE. RIGHT WING SKIN PANEL REPAIRED IAW REA B653-58942-MR & B653-58947-MR.SDR ABXA201010010128Strap · crackedRT FAIL-SAFE STRAP CRACKED AND CORRODED AT LWR FASTENER COMMON TO STRAP AND FITTING. REPAIRED RIGHT FAIL-SAFE STRAP IAW REA B653-58935-SB & REA B653-58851-MR.SDR ABXA201010010127Strap · corrodedLT FAIL-SAFE STRAP BLEEDING CORR OUTBOARD SIDE STA 955 BETWEEN SIDE LOAD FITTING AND AT UPPER BOLT AROUND BUSHING COMMON TO STRAP AND FITTING. LT FAIL-SAFE STRAP WAS REPAIRED ON REA B653-58932-MR AND B654-58937-SB. CORROSION FOUND. PERFORMED PREVENTATIVE RESDR ABXA201009200122Panel · missingAIRCRAFT EXPERIENCED A PART DEPARTING THE AIRCRAFT EVENT. CREW REPORTED HEARING A LOUD BANG AT 12,000 FT. COMPOSITE PANEL P/N 561QB TRAILING EDGE PANEL JUST FORWARD OF LT AILERON HAD 75 SCREWS MISSING OF 104. PANEL MEASURES 14 X 46 AND IS COMPLETELY MISSINGSDR ABXA201009220123Fitting · crackedPERFORMED OPEN HOLE HFEC ON STA 1809.5 RT SPLICE FITTING. TWO CRACKS FOUND IN AREA 2 REF EA 5380002-002 ESO1222. REMOVED AND REPLACED SPLICE FITTING IAW 767 SRM 51-40-02.SDR ABXA201010010129Fitting · corrodedRT FAIL-SAFE T-FITTING CENTER AND LOWER HOLES COMMON TO FAIL-SAFE CORRODED. REMOVED AND REPLACED T-FITTING IAW B767 SRM 51-40-02.SDR ABXA201010010126Mount · corrodedNR 2 ENGINE AFT MOUNT IS CORRODED. REMOVED AND REPLACED NR 2 ENG AFT MOUNT IAW B767 MM 71-21-02-4.SDR ABXA201009090121Structure · crackedNWW AFT LT VERTICAL CHORD CRACKED. REPAIRED CRACK ON NWW VERTICAL CHORD IAW BOEING 767 SRM 51-70-12.SDR ABXA201008200104Warning System · false activationLEFT FWD ENTRY DOOR LIGHT ILLUMINATED INFLIGHT DOOR HANDLE RAISED OUT OF POSITION. INSPECTED BOTH OUTER AND INNER DOOR HANDLES FOR OPERATION PER MM 52-11-2-5-5 BOTH WERE GOOD. COMPARED TO L1 AND R1 DOOR HANDLES AND OPERATION BOTH WERE THE SAME. CHECKED RIG SDR ABXA201008200115Skin · corrodedLEFT WING LOWER SURFACE SPLICE IS CORRODED ON THE UPPER AND LOWER SURFACE IN THE AREA OF THE REFUELING DOOR. REMOVED CORROSION AND REPAIRED AREA IAW REA B657-58923.SDR ABXA201008200110Frame · crackedINBOARD PYLON NR 1 BELOW 437 BR FRAME CRACKED. REMOVED STRIKER PLATES AND FRAME. RE-INSTALLED STRIKER PLATES AND NEW FRAME PER SRM 51-40-02.SDR ABXA201008200106Tee Fitting · corrodedFWD LOWER CARGO DOOR 2 BEAM FROM THE TOP HAS SEVERE CORROSION. REMOVED AND REPLACED CARGO DOOR BEAM TEE IAW SRM 51-3-0.SDR ABXA201008200109Support Fitting · crackedCRACK IN SUPPORT CLIP ABOVE AND AFT OF SLAT PDU BEHIND NR 6 SLAT. REMOVED AND REPLACED SUPPORT CLIP IAW SRM 51-40-01.SDR ABXA201008200114Shear Tie · corrodedSHEAR TIE CORRODED ON AFT SIDE OF FLOOR SUPPORT WEB BETWEEN STRINGER 36LT AT AFT SIDE OF STA 742. FABRICATED NEW SHEAR TIE. INSTALLED IAW SRM 51-40-02.SDR ABXA201008200112Support Bracket · damagedAFT LOWER CARGO DOOR INTERNAL LWR ANGLE SUPPORT BRACKET IS BENT AND GOUGED ON LWR SIDE OF DOOR. REMOVED AND REPLACED AFT LOWER CARGO DOOR INTERNAL LOWER ANGLE SUPPORT BRACKET WITH SERVICEABLE UNIT IAW SRM 51-40-02.SDR ABXA201008200111Stringer · crackedCRACK COMING FROM RIVET STA 1654 BETWEEN S4R AND S5R. REPAIRED FUSELAGE AND STRINGER DAMAGE IAW REA B653-58914-MR SRM 53-00-03 FIG 201 AND SRM 53-80-01 FIG 2.SDR ABXA201008200107Skin · crackedR1 DOOR LWR AFT CORNER HAS 1.5 INCH CRACK TWO CRACKS FROM DOOR CUTOUT .75 INCH LC RUNNING TO BOLT HOLE. ANOTHER .75 INCH LONG CRACK EMANATES FROM THE OPPOSITE SIDE OF THE SAME BOLT HOLE EXTERNAL SKIN. REPAIRED AFT LOWER DOOR CORNER AT R1 DOOR IAW SRM 53-10-0SDR ABXA201008200117Pressure Panel · chafedPRESSURE DOME CHAFED ON TS6 BETWEEN RS18 AND RS19. BLENDED AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-80-08. REMOVED AND REPLACED TEAR STRAP USING 2024T3 .040 IAW SRM 51-40-02. REMOVED LINER TO GAIN ACCESS TO RIVETS. RE-INSTALLED LINER IAW SRM 51-40-02.SDR ABXA201008090103Fire Warning · false activationWHEEL WELL FIRE ANNUNCIATOR LIGHT ON FORWARD PANEL COME ON DURING CRUISE. COMPLIED WITH ABNORMAL, FIRE TEST NORMAL. DEFERRED. WHEEL WELL LIGHT WILL NOT STAY ON WITH WHEEL WELL FIRE TEST OR LAMP TEST. TRIED NEW KORRY SWITCH & RELAY K693 - NO HELP.SDR ABXA201008200108Stringer · corrodedAFT INBOARD END OF STRINGER 39RT CORRODED AT STA 786. SPLICED NEW SECTION OF STRINGER 39 RT IAW SRM 53-3-00.SDR ABXA201008200113Beam · corrodedTHE INTERNAL SIDE OF THE AFT LOWER CARGO DOOR HAS SURFACE CORROSION ACROSS THE DOOR STRUCTURES BEAM BELOW VENT DOORS. INSTALLED NEW T CAP AND FASTENERS IAW SRM 51-40-02.SDR ABXA201008200105Rib · corrodedPOCKET OF CORROSION AT REFUELING PANELS DOOR INBOARD GROUND WIRE MOUNT ON AIRFRAME. REMOVED AND REPLACED 4E RIB IAW SRM 51-40-2.SDR ABXA201006140090Plate · corrodedFWD LOWER CARGO BAY HAS CORROSION BY THE EDGE OF A PANEL ON A FLOOR SEAM PLATE AT STA 610 AROUND LBL 18. REMOVED CORROSION & REPAIRED AREA IAW B767-200 SRM 53-00-07 FIG 201.SDR ABXA201006120089Handle · poppedEICAS MSG FWD ENTRY DOOR ILLUMINATED INFLIGHT 3 TIMES DOOR HANDLE POPPED SLIGHTLY OPEN EACH TIME, BUT WOULD NOT REMAIN IN FULL LOCKED POSITION. INSPECTED DOOR HANDLE & MECHANISM FOR WEAR. ALL WAS GOOD. INSPECTED DOOR PROX SW 194 & 195. BOTH WERE 52-11-25-5SDR ABXA201006110091Frame · crackedCUT OUT LOWER FRAME IS CRACKED AT FWD END UNDER PANEL 437 ELX. REPLACED FRAME UNDER PANEL 437 ELX IAW B767 SRM 51-40-02SDR ABXA201006070092Frame · crackedCUTOUT FRAME IS CRACKED AT FWD END UNDER PANEL 437 ERX. REPLACED FRAME UNDER PANEL 437 ERX IAW B767 SRM 51-40-2.SDR ABXA201006090088Angle · crackedANGLE CRACKED AT STA 1395 BETWEEN S39L AND S39R. REMOVED AND REPLACED ANGLE IAW B767 SRM 51-40-02.SDR ABXA201006090087Slat Track · corrodedNR 8 SLAT OUTBOARD MAIN TRACK CORRODED. REMOVED CORRODED SLAT TRACK AND INSTALLED NEW SERVICEABLE SLAT TRACK IAW B767 AMM 27-81-02-4.SDR ABXA201006010083Slat Track · corrodedNR 11 SLAT I/B AND O/B MAIN TRACKS HAVE SURFACE CORROSION ON UPPER AND LOWER SURFACES. REMOVED AND REPLACED NR 11 SLAT MAIN TRACKS IAW B767 AMM 27-81-54-4. REMOVED AND REPLACED NR 11 SLAT IAW B767 AMM 27-81-02-4, OPS CHECK GOOD.SDR ABXA201006010086Support · damagedNR 2 FLAP SUPPORT ACTUATOR FASTENER HOLES 3 EACH, 2 FWD UPPER SMALL DIA AND 1 LARGE AFT UPPER CENTER HOLE HAVE EDDY CURRENT INDICATION USING HOLD SCAN IAW 50-04 AND 51-00-16 PART 6 767 NDT. REWORKED HOLES AND INSTALLED FREEZE PLUGS IAW REA B657-58806-MR.SDR ABXA201006010085Channel · crackedBULK CARGO COMPARTMENT FLOOR PANEL ATTACH HAT CHANNEL HAS VERTICAL ATTACH ANGLE CRACKED AT STA 1417 RBL 8. REMOVED AND REPLACED ATTACH ANGLE IAW B767 SRM 51-40-02.SDR ABXA201006010084Support · corrodedLT WING L/E SUPPORT CORRODED ABOVE WING FUEL PANEL. REMOVED CORROSION. FOUND LT WING L/E SUPPORT TO BE OUT OF LIMITS. REPAIRED LT WING L/E SUPPORT IAW 767-200 SRM 57-41-09.SDR ABXA201005200082Structure · cracked#1 ENG I/B THRUST REVERSER #13 CASCADE HAS 3 CRACKS. REMOVED AND REPLACED #13 CASCADE IAW B767 AMM 78-31-16-4SDR ABXA201005200081Rib · corrodedLT WING L/E SUPPORT HAS CORROSION JUST INBD OF OUTBD AUX TRACK NR 3 SLAT. REMOVED AND REPLACED RIB IAW SRM 51-40-2SDR ABXA201005200079Support · corrodedLT WING LE NR 3 SLAT INBD AUX TRACK HAS CORROSION ON INBD & OUTBD SUPPORTS. REMOVED CORROSION ON I/B SUPPORT IAW SRM51-10-02. REMOVED AND REPLACED SUPPORT IAW SRM 51-47-02SDR ABXA201005200080Rib · damagedCLOSE OUT NOSE RIB AT LES 568 IS DAMAGED. REMOVED DAMAGED NOSE RIB FABRICATED NEW NOSERIB IAW B767 DWG 114T2512. INSTALLED NOSE RIB IAW B767-200 SRM 51-40-02SDR ABXA201005140076Structure · crackedCRACK EMANATING FROM RIVET AT BS 1702 BETWEEN S7L TO S8L. CRACK IS .1250 INCH IN LENGTH. REPAIRED AREA IAW B767 SRM 53-80-01-FIG 201.SDR ABXA201005140075Rib · crackedOUTBOARD NOSE RIB CRACKED AT NR 5 SLAT OUTBOARD DRIVE ROD CUTOUT. CRACK IS .75 INCH LONG. REMOVED AND REPLACED NOSE RIB IAW B767 SRM 51-40-02 AT NR 5 SLAT OUTBOARD DRIVE ROD CUTOUT.SDR ABXA201005140077Structure · crackedTHE NWW VERTICAL CHORD AT LBL 25 IS CRACKED APPROX .625 INCH IN LENGTH IN FLANGE LOCATED 11.5 INCHES BELOW CEILING PANEL. REPAIRED CRACKED CHORD AT LL25 IAW B767 SRM 51-70-12 FIG 1.SDR ABXA201005070072Warning System · malfunctionedON INITIAL CLIMBOUT MAIN CARGO DOOR LIGHT WITH AUDIO WARNING ACTIVATED. NOTE: LIGHT WENT OUT ON LANDING. DEFERRED MAIN CARGO DOOR LIGHT IAW B767 MEL 52-71-1-2. VERIFIED MAIN CARGO DOOR CLOSED AND LOCKED. PLACARD INSTALLED.SDR ABXA201005140078Rib · crackedLEADING EDGE RIB AT STA OSS574.05 IS CRACKED ON THE FORWARD ENG AT CLOSEOUT RIB ATTACH HOLE. REMOVED DAMAGE AND INSTALL BUSHING IAW 767 SRM 51-20-07.SDR ABXA201004120053Support Beam · corrodedCORROSION LT WING WBL 169 T/E STRUCTURE UPPER BONCED PANEL SUPPORT BEAM. REMOVED AND REPLACE SUPPORT BEAM IAW 767 SRM 51-40-02.SDR ABXA201004120052Support Beam · corrodedEXFOLIATION CORROSION LT WING TRAILING EDGE UPPER SUPPORT BEAM WBL 289.45 ANGLE I/B APPROX 12 INCH SPAN. REMOVED CORROSION IAW 767 SRM 51-10-00 IS WITHIN LIMITS IAW 767 SRM 57-51-02 FIG 101.
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