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 FDEA202304030555Unknown · unknown#1 PYLON AFT FAIRING MID-FRAME IS CRACKED IN UPPER INBD CORNER AT APPROX NAC STA 330. REPAIRED #1 PYLON AFT FAIRING MID FRAME IAW B767-300 SRM 54-52-71-2R & BAC DWG 313T2303 REV - REMOVED AND REISTALLED LATCH BEAM IAW BAC DWG 313T2303 REV -SDR FDEA202304030554Unknown · cracked#2 PYLON, OB SIDE, FRAME JUST AFT OF HYDRO BAY DOOR HAS A CRACKED ANGLE REMOVED AND REPLACED CLIP IAW B767 SRM 51-40-02 & BAC DWG 313T2303, SHEET 146, REV-SDR FDEA202304030546Seat Track · damagedMEL 25-58-01-A MDC RESTRAINT ID503 INOP / SEAT TRACK DAMAGE. REPAIRED THE MAIN DECK CARGO DAMAGED SEAT TRACK PER B767 SRM53-00-52-2R REPAIR 9. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.SDR FDEA202304020543Former · crackedNOSE FORMER ANGLE AT OSS 648.59 ON THE RIGHT WING IS CRACKED. REMOVED AND REPLACED CRACKED FORMER REF SRM 51-40-02SDR FDEA202304020542Former · crackedNOSE FORMER ANGLE AT OSS 648.59 ON THE RIGHT WING IS CRACKED. REMOVED AND REPLACED CRACKED FORMER REF SRM 51-40-02SDR FDEA202304010541Former · crackedNOSE FORMER ANGLE AT OSS 499.6 IS CRACKED. REMOVED AND REPLACED CRACKED FORMER REF FEDEX DRAWING SR 67-57-002SDR FDEA202304010540Former · crackedNOSE FORMER ANGLE AT OSS 441 ON THE RIGHT WING IS CRACKED. REMOVED AND REPLACED CRACKED FORMER REF FEDEX DRAWING SR 67-57-002SDR IXXA2023040104Fitting · crackedCARGO HANDLING SUPPORT FITTING CRACKEDSDR IXXA202304010003Roller Tray · corrodedROLLER TRAY CORRODEDSDR IXXA202304010002Roller Tray · corrodedROLLER TRAY CORRODEDSDR IXXA202304010001Roller Tray · corrodedROLLER TRAY CORRODEDSDR IXXA2023032901Fitting · loose#1 PYLON OB SIDE LINK FITTING HAS LOOSE BUSHINGSDR FDEA202303260505Skin · unknownFUSELAGE SKIN WITH LIGHTNING STRIKE AND PREVIOUS BLEND OUT IN FASTENER HEAD BETWEEN STA 654 121 AND STG 35/36 RH. LIGHTNING STRIKE WAS REPAIRED ON RH FUSELAGE SKIN BTWN STA 654 121 AND STGR 35/36 I.A.W. SRM 53-00-01-2R REPAIR 12 REV. 85 DEC 15 2022SDR IXXA2023032501Skin · crackedLH FUSELAGE FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER HAS CRACK AT FASTENER HOLE.SDR FDEA202303220481Unknown · unknownRH WING - OUTBOARD FLAP LOWER SKIN SURFACE TRAING EDGE HAS A DENT AT LOCATION OUTBOARD OF THE OUTBOARD FLAP TRACK FAIRING. MWT. REPAIRED RH WING- OUTBOARD FLAP LOWER SKIN SURFACE TRAILING EDGE DENT AT LOCATION OUTBOARD OF THE FLAP TRACK FAIRING STA. WS 842SDR IXXA2023032201Skin · crackedFUSELAGE FWD SERVICE DOOR CUTOUT AFT LOWER CORNER LOWER FASTENER CRACK INDICATIONSDR FDEA202303170453Slat · wornRH WING, SLAT# 8, TRAILING EDGE, LOWER SURFACE WITH WEAR (TWO PLACES). RH WING, SLAT 8, TRAILING EDGE LOWER SURFACE WAS REPAIRED IAW SRM 57-43-02-2R PAG 1,FIG 201 AND SRM 51-70-10-2R PAG 150, 163 FIG 202 REV 85 DEC 15/2022.SDR IXXA20230315001Attach Fitting · gougedN/LDG L/H TRUNNION FITTING SCRATCH AND GAUGE DAMAGE.SDR FDEA202303060382Former · crackedRIGHT WING, @ WING STA. 441 CRACKED LEADING EDGE NOSE FORMER. REMOVED AND REPLACED FORMER WITH B67-57-002-02. REF FEDED DRAWING SR67-57-002.SDR FDEA202303060379Rib · crackedLH WING LEADING EDGE, MAINT TRACK RIB BETWEEN OSS 491-499, FRONT AND LOWER RADII WITH CRACK OF 0.480" LH WING LEADING EDGE MAIN TRACK RIB BETWEEN OSS 491-499 FRONT AND LOWER RADI WAS REPAIRED I.A.W. E.A. #H-5740-T0373203 RELASE DATE MAR 05, 2023SDR FDEA202303010358Fan · failedFWD EQ EXH FAN STATUS MESSAGE DURING CLIMB. CREW DETECTED A BURNING SCENT PRIOR TO THE MESSAGE BUT WENT AWAY IMMEDIATELY AFTER STATUS MESSAGE APPEARED. AMM: 21-58-06 PER FIM 21-58-00 TREE 992 & AMSDR IXXA2023030103Skin Panel · delaminatedRH VERTICAL SKIN PANEL IS DELAMINATED.SDR IXXA2023030102Bracket · corrodedFLC CORRODED BRACKET.SDR IXXA2023030101Fitting · crackedCRACKED RW LE FITTINGSDR IXXA2023022708Skin · damagedREPAIR FUSELAGE SKIN AND TEARSTRAP SECTION 41 STATION 256.25 AT STR 33RSDR IXXA2023022707Skin · damagedSTATIC DISCHARGE ON SKIN @ FS 434, STR37R-38RSDR IXXA2023022706Skin · damagedSTATIC DISCHARGE ON SKIN AT FS 370 STR 30RSDR IXXA2023022705Skin · damagedSTATIC DISCHARGE ON SKIN@ FS 65422 STR 33RAND 34RSDR IXXA2023022602Skin · crackedCRACK IN L1 DOOR CUTOUT SKINSDR IXXA2023022601Skin · crackedEXTERNAL SKIN FOUND CRACKED L! DOOR CUTOUTSDR IXXA2023022704Skin · damagedSTATIC DISCHARGE ON SKIN FS 325, STR 30RSDR IXXA2023022501Nose Cowl · corroded#1 INLET COWL CORRODED ON INNER BARREL.SDR IXXA2023030100001Skin · crackedSERVICE DOOR R1 CUTOUT LOWER CORNER FASTENER HOLE CRACK INDICATIONSDR IXXA2023022702Skin · damagedSTATIC DISCHARGE FOUND ON SKIN @ FS 138.5 FWD OF R AUX PITOTSDR IXXA2023022701None · noneSTATIC DISCHARGE FOUND ON SKIN FS 717 35R-36RSDR IXXA2023022703Skin · damagedSTATIC DISCHARGE FOUND ON SKIN 677 STR 36RSDR FDEA202302220336Slat · wornRH WING SLAT #8 LEADING EDGE LOWER SURFACE WITH WEAR (ABOVE OF INBOARD AUXILIARY TRACK). RH WING SLAT #8 WAS REPAIRED IAW SRM 57-43-02-2R REP. 1 FIG. 201 AND SRM 51-70-10-2R REP. 4 PAG. 150, 160, 163 FIG. 202 SHEET 8 REV. 85 DEC15/2022SDR FDEA202302220337Rudder · delaminatedRH VERTICAL STABILIZER RUD STA 230.972 WITH LIGHTNING STRIKE. RH VERTICAL STABILIZER RUD STA 230 WAS REPAIRED IAW B767 SRM 55-40-01-2R DETAIL I AND SRM 51-70-17-0G PAR. 4.B. REV. 85 DEC15/2022SDR IXXA2023022201None · crackedLH 1809 CHORD CRACKEDSDR IXXA2023032102Skin · crackedL1 DOOR LOWER AFT CORNER CUTOUT CRACK INDICATIONSDR IXXA2023022101Structure · crackedFORWARD R1 DOOR CUTOUT CRACK INDICATIONSDR FDEA202302210329Control Lever · failedWHEN LANDING GEAR LEVER PLACE TO OFF DURING AFTER TAKE OFF CHECK FROM MMMY THE RIGHT MAIN AND NOSE GEAR EXTENDED WITH GREEN LIGHTS ON. LEFT MAIN STAYED UP. DOORS AND GEAR ANNUNCIATORS AND GEAR DISAGREE EICAS WERE ON. ALL GEAR RETRACTED AND DOORS CLOSED WHSDR FDEA202302160339Skin · failedE.A.#:H-5330-T0372987 REPAIR FOR DAMAGE TO FORWARD WING-TO-BODY FAIRING AND SKIN, R/H SIDE, STA 698-720, STR 31-32R. COMPLY WITH E..A. H-5330-T0372987 REV NO: A PS P2 EA H-5330-T0372987 REV NO, P2 WAS SUPERSEDED BY EA H-5330-T0372987 REV A, P2. COMPLIED WSDR IXXA2023021602Rub Strip · corrodedENGINE COWL RUB STRIPSDR IXXA2023021502Panel · delaminatedUPPER HORIZONTAL SKIN PANEL DELAMINATED BEHIND LEADING EDGESDR FDEA202302110252Beam · worn#1 ENGINE PYLON O/B AFT FAIRING ACCESS PANEL, AFT HINGE MOUNTING POINT HAS DAMAGE AT BOTH FWD AND AFT BOLT HOLES. 0000231760 : ROWLAND, GLEN J - 12-FEB-2023 05:37 REPAIRED #1 ENGINE PYLON O/B AFT FAIRING ACCESS PANEL, AFT AND SECOND FROM AFT HINGE MOUNTING SDR FDEA202302110249Flap · dentedRH WING INBOARD FLAP AFT FLAP WITH DENT ON LOWER SURFACE. RH WING INBOARD AFT FLAP, ON LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-53-01-2R, TABLE I, FIG. 201 SHEET 4-5, PAGE 4-5 AND SRM 51-70-03-0G, PARA. 5.L, FIG. 16, PAGE 27, 30, 52 REV. 85 12-15-22SDR FDEA202302100251Beam · worn#2 ENGINE PYLON O/B AFT FAIRING ACCESS PANEL, AFT HINGE MOUNTING POINT HAS DAMAGE AT BOTH FWD AND AFT BOLT HOLES. REPAIRED #2 ENGINE PYLON O/B AFT FAIRING ACCESS PANEL, AFT HINGE MOUNTING POINT WORN LUGS PER SRM 54-52-70- 2R REPAIR 6.SDR FDEA202302100246Unknown · failedDURING CURRENT HMV2 CHECK AT MEXICANA FACILITIES (MEX), DAMAGE WAS INDUCED IN THE SLAT #4 COVER PANEL 523EB DURING SLAT EXTENSION/RETRACTION; AS A RESULT, THE REFERRED PANEL WILL HAVE TO BE REPLACED. LH WING ACCESS PANEL 523EB WAS MANUFACTURED IAW EA #: H-57SDR CALA2023020300311Module · not enteredSELECTED FLAPS ONE. GOT TRAILING EDGE DISAGREE. QRH RUN. UNEVENT FUL LANDING. REPLACED FLAP STAB MODULE.PARTS USED:76-2754-9-0001,QTY :1ROTABLE PARTS CHANGE WAS INDICATED - TT # 1147533 SN OFF 2812 FIM TASK 27-51 FAULT TREE 810 ACTIONED, FSEU BITE TEST SHOWED
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