Boeing 767-300
Service difficulty reports · 2,148
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 = '767300' 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 = '767300' 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 IXXA2023042403Skin · crackedCRACK IN SKIN AND BEARSTRAPSDR IXXA2023042402Skin · damagedREPAIR AT STA 1329 STRR 35L NEEDS REPLACEDSDR IXXA2023042401Flap · delaminatedRW OB FLAP LOWER SURFACE DELAMSDR FDEA202304240751Unknown · cracked#1 PYLON APPROX NAC STA 377 AFT OF PANEL 437BL, INSIDE AFT FAIRING HAS LEFT SUPPORT BRACKET CRACKED REMOVED AND REPLACED CLIP IAW B767 SRM 51-40-02 AND BAC DWG 313T2303, SHEET 176, REVISION ASDR FDEA202304230746Flap · delaminatedLH WING OUTBD FLAP LEADING EDGE HAS AREA OF DELAMINATION ON INBD SIDE. REPAIRES LH WING O/B T/E FLAP LE NOTED AREA IAW B767 SRM 57-53-01-0I, 57-53-01-1A,57-53-01- 2R AND 51-70-17-OG.SDR FDEA202304220745Skin · dentedRIGHT WING #11 SLAT UPPER SURFACE HAS A LARGE SMOOTH DENT 3" FORWARD OF TRAILING EDGE AND 50" FROM OUTBOARD EDGE AS MARKED. 0000493008 : CRAIL, ROGER L - 23-APR-2023 03:10 REPAIRED SLAT REF B767 SRM 51-70-10-2R. E.A. H-5750-T0374154 P1 WINGS - FLIGHT SURFASDR IXXA2023042201Skin · crackedRW LEADING EDGE SKIN DAMAGED BEHIND #7 SLATSDR FDEA202304210735Flap · crackedL/H INBD ELEVATOR HAS DAMAGE ON THE UPPER SIDE. (MWT) SECOND LOCATION AT STA .125. REPAIRED LH IB ELEVATOR UPPER SKIN AT 63" AFT OF HINGE LINE AND 17" FROM IB EDGE OF PART. REF 767 SRM 55-20- 01-2R , 51-70-05-0G PAR 5C AND E.A. H-5520-T0374127 REV A P1. TSDR FDEA202304210734Flap · crackedL/H INBD ELEVATOR HAS DAMAGE ON THE UPPER SIDE. REPAIRED LH IB ELEVATOR UPPER SKIN AT 46" AFT OF HINGE LINE AND 17" FROM IB EDGE OF PART. REF 767 SRM 55-20- 01-2R , 51-70-05-0G PAR 5C AND E.A. H-5520-T0374127 REV A P1. THIS IS A MAJOR REPAIR.SDR FDEA202304210733Stringer · damagedCOMPLY WITH EO H-5310-EO365800 P2, FUSELAGE - MAINFRAME - INSTALLATION OF SPLICE FITTINGS ON STRINGERS S-20L AND S-20R AT STA 1506, STA1530, AND STA 1552 - BOEING SERVICE BULLETIN 767-53-0279 COMPLIED WITH EO H-5310-EO365800 P2, TITLE: FUSELAGE - MAINFRAMSDR FDEA202304210732Stringer · damagedCOMPLY WITH EO H-5310-EO365800 P1, FUSELAGE - MAINFRAME - INSTALLATION OF SPLICE FITTINGS ON STRINGERS S-20L AND S-20R AT STA 1506, STA1530, AND STA 1552 - BOEING SERVICE BULLETIN 767-53-0279 COMPLIED WITH EO H-5310-EO365800 P1, TITLE: FUSELAGE - MAINFRAMSDR FDEA202304190702Bracket · crackedR/H WING INBD L/E AREA HAS 1EA SLAT TORQUE TUBE GUIDE ATTACH BRACKET CRACKED IN MULTIPLE LOCATIONS AT APPROX IFSS 280 REMOVED AND REPLACE TORQUE TUBE GUIDE BRACKET IAW B767 SRM 51-40-02 AND BAC DWG 114T1240 SHEET 2 REVISION E.SDR IXXA2023041902Rib · crackedRW FIXED LEADING EDGE FRAME CRACKED.SDR IXXA2023041901Frame · crackedLEADING EDGE FRAME CRACKEDSDR FDEA202304150655Flap · unknownFOUND DENT ON RH INBOARD TRAILING EDGE FLAP TOPSIDE. REPAIRED RT WING- INBOARD FLAP UPPER SKIN TOP SURFACE TRAILING EDGE DENT AT LOCATION INBD FLAP TRAILING EDGE TOP SURFACE 39 INCHES FROM INB EDGE 9.5 INCHES WITH A 2 IN. CIRCLE REPAIR, IN REF. TO 767 SRMSDR FDEA202304140647Wheel · damagedON TAKEOFF ROLL LOTS OF VIBRATION ABOVE 130. ON LANDING ROLL ABOVE 130 SAME VIBRATION. ON POSTFLIGHT MECHANIC SAID WE HAD #6 TIRE HAD BLOWN. NO STATUS MESSAGES PERIOD TO SHUTDOWN. REMOVED & REPLACED #6 MLG TIRE PER AMM 32-45-01-4. PERFORMED BURST TIRE CSDR IXXA2023041401Rib · crackedLW AIR LOAD RIB CRACKED.SDR FDEA202304120629Flap · dentedRH WING, OUTBOARD FLAP, LOWER SURFACE, WITH DENT (NEAR TO INBOARD FLAP TRACK). RH WING, OUTBOARD FLAP, LOWER SURFACE, WAS REPAIRED IAW B767 SRM 57-53-01-2R PAG. 1-9 AND B767 SRM 51-70-10-2R REP. 4 PAG. 150-151 FIG. 201 REV. 85 DEC15/2022SDR IXXA2023041202Seat Track · crackedCAPTAIN'S FORWARD IB SEAT TRACK IS CRACKEDSDR FDEA202304120627Seal · crackedRH WING LE SKIN INTERNAL SPLICE STRAP IS CRACKED AT APPROX WS 508 REMOVED AND REPLACED RIGHT WING SEAL STRIP IAW B767 SRM 51-40-02 AND BAC DWG 114T2800, SHEET 6, REVISION C.SDR IXXA2023041201Seat Track · crackedFIRST OFFICERS FORWARD O/B SEAT TRACK CRACKEDSDR FDEA202304110623Seal · crackedL/H WING L/E SKIN INTERNAL SPLICE STRAP IS CRACKED AT APPROX WS 508 REMOVED AND REPLACED LEADING EDGE SEAL STRIP IAW B767 SRM 51-40-02 AND BAC DWG 114T2800, SHEET 6, REVISION C.SDR IXXA2023041102Rib · crackedCRACK AT FIXED LEADING LWS 549SDR IXXA2023041101Skin · delaminatedL/H VERTICAL BETWEEN AUX SPAR AND FRONT SPAR FSS270 EXTERIOR SKIN DELAMINATIONSDR FDEA202304100619Panel · dentedDENTS ON FLOOR PANEL 222BFF AT SECTION 41 OF MDC. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222 BFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR 4.B FIG 201 SHEET 2. REV 85 DEC 15/2022SDR FDEA202304100618Slat · wornRH WING, SLAT #8, TRAILING EDGE, LOWER SURFACE WITH WEAR (ABOVE OF INBOARD AUXILIARY SLAT TRACK). R.H. WING, SLAT # 8, TRAILING EDGE, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-43-02- 2R, FIG 201 SHEET 1-2 AND SRM 51-70-10-2R REP 4, FIG 202 SHEET 8, PAG 150SDR FDEA202304100617Panel · dentedDENTS ON FLOOR PANEL 222AFF AT SECTION 41 OF MDC. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222 AFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR 4.B FIG 201 SHEET 2 REV 85 DEC 15/2022SDR FDEA202304100616Panel · dentedDENTS ON FLOOR PANEL 221DFF AT SECTION 41 OF MDC MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221 DFF WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR 4.B FIG 201 SHEET 2 REV 85 DEC 15/2022SDR FDEA202304100615Panel · dentedDENTS ON FLOOR PANEL 221DFF AT SECTION 41 OF MDC. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221 DFF WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202304100614Panel · dentedDENTS ON FLOOR PANEL 221CFF AT SECTION 41 OF MDC. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221 CFF WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202304100613Panel · dentedDENTS ON FLOOR PANEL 222CFF AT SECTION 41 OF MDC. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222 CFF WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202304100607Angle · crackedMAIN CABIN LOWER RH FLOOR SUPPORT IS CRACKED AT APPROX STA 1580, RBL 78 OTBD ATTACH ANGLE REMOVED & REPLACED FLOOR SUPPORT ATTACH ANGLE IAW B767 SRM 51-40-02 & BAC DWG 146T5650, SHEET 5, REVISION CSDR FDEA202304100606Angle · crackedMAIN CABIN LOWER RH FLOOR SUPPORT IS CRACKED AT APPROX STA 1580, RBL 78 REMOVED & REPLACED FLOOR SUPPORT ATTACH ANGLE IAW B767 SRM 51-40-02 & BAC DWG 146T5650, SHEET 5, REVISION CSDR FDEA202304100605Angle · crackedMAIN CABIN LOWER LH FLOOR SUPPORT IS CRACKED AT APPROX STA 1580, LBL 78 REMOVED & REPLACED FLOOR SUPPORT ATTACH ANGLE IAW B767 SRM 51-40-02 & BAC DWG 146T5650, SHEET 5, REVISION CSDR FDEA202304100604Angle · crackedMAIN CABIN LOWER LH FLOOR SUPPORT IS CRACKED AT APPROX STA 1580, LBL 78, OTBD ATTACH ANGLE REMOVED & REPLACED FLOOR SUPPORT ATTACH ANGLE IAW B767 SRM 51-40-02 AND BAC DWG 146T5650, SHEET 5, REVISION C.SDR IXXA202304110001Skin · delaminatedL/H VERTICAL BETWEEN AUX SPAR AND FRONT SPAR FSS270 EXTERIOR SKIN DELAMINATIONSDR FDEA202304080602Panel · dentedMAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222AFF, WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222 AFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 85 DEC15/2022.SDR FDEA202304080601Panel · dentedMAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222 CFF, WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222 CFF WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 85 DEC 15/2022SDR FDEA202304080600Panel · dentedMAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221DFF, WITH DENTS MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221DFF WAS REPAIRED I.A.W. B767 SRM 53- 00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV 85 DEC. 15/2022SDR FDEA202304080599Panel · dentedMAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221CFF, WITH DENTS. MAIN CARTGO COMPARTMENT ACCESS FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR.4.B. FIG.201 SHEET 2 REV.85 DEC 15/2022.SDR FDEA202304080598Panel · dentedMAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222BFF, WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222 BFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 85 DEC 15/2022SDR IXXA2023040803Seat Track · wornCAPTAINS I/B AFT SEAT TRACK HOLE ELONGATED AND WEAR ON TOP FLANGE.SDR IXXA2023040802Seat Track · wornFO AFT I/B SEAT TRACK HOLES ELONGATED AND WEAR ON TOP FLANGESDR IXXA2023040801Roller Tray · corrodedROLLER TRAY CORRODEDSDR CALA2023041001070Skin · unknownEA5100-02345 REV E FOUND REINFORCINGT DOUBLER REPAIR ON AFT CARGO DOOR EXTERNAL SKIN AT 6OCLOCK FROM UPPER EDGE 13IN FROM AFT EDGE SIZE 13/12X9 REPAIR HAS A DEEP SCRATCH 3IN LONG REF AAR N/R 975221 REMOVED EXISTING DOUBLER AND REINSTALLED NEW DOUBLER ON AFT CASDR FDEA202304070587Flap · delaminatedRH WING I/B FLAP AFT FLAP LOWER SKIN HAS A DENT WITH SUBSTRATE BREAK THROUGH. REPAIRED RH I/B AFT FLAP ON THE LOWER SKIN IAW B767 SRM 57-53-01-2R AND 51-70-10-2RSDR FDEA202304070586Spoiler · delaminatedLH WING #6 SPOILER LOWER SURFACE IS PUNCTURED THROUGH BOTH THE UPPER AND LOWER SURFACES APPROX 12" O/B OF THE I/B EDGE. REPAIRED LH WING #6 SPOILER UPP AND LOWER SKINS IAW B767 SRM 57-70-01-2R FIG 201 SHEET 4 AND 51-70-05. MAJOR REPAIRSDR FDEA202304060577Web · crackedR/H WING L/E SUBSTRUCTRE BULLNOSE WEB IS CRACKED IN THE LOWER BEND RADIUS JUST FWD OF THE FUELING SVC PANEL. REPAIRED R/H WING L/E SUBSTRUCTURE BULLNOSE WEB IAW B767 SRM 57-41-13-2R.SDR FDEA202304060576Attach Angle · cracked#1 PYLON AFT FAIRING, 2EA FRAME ATTACH CLIPS ARE CRACKED ON INBD AND OUTBD SIDES AT NAC STA 376 REMOVED AND REPLACED CLIPS IAW B767 SRM 51-40-02 AND BAC DWG 313T2303, SHEET 146, REV -SDR FDEA202304060574Web · crackedL/H WING L/E BULLNOSE INTERNAL WEB IS CRACKED IN THE LOWER RADIUS JUST FWD OF THE FUELING SVC PANEL
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