Boeing 767-323
Service difficulty reports · 8,544
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 = '767323' 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 = '767323' 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 MK1Y20210221016Skin · damagedEXTERNAL FUSELAGE SKIN BETWEEN STA 380 AND STA 390, BELOW STR-2R, SECTION 41. SHOP FOUND 2 (2) EXISTING BLENDOUTS AREAS NAMED M0369 AND M0370 AT FUSELAGE SKIN IN THE NOTED LOCATION. THE BLENDOUTS FALL ON FASTENERS ZONE AND SPLICE JOINT ALONG S-2R.
ACCORDING SDR MK1Y20210221014Skin · debondedR/H HORIZONTAL STABILIZER PANEL, STAB STA 127.465 – AUX SPAR STA 157.277, 185T1001. THE INNER 7075-T6 ALUMINUM SKIN FOUND DISBONDED AND SEPARATED FROM THE ALUMINUM HONEYCOMB CORY PANEL 185T1001. IDENTIFICATION PER SRM 55-10-01 FIG. 1 (DETAIL I)SDR MK1Y20210221013Skin · damagedFUSELAGE SKIN PANEL, STA 919.5, STR 19L- STR 20L, P/N 145T3321-4, AN EXISTING AREA OF CORROSION WAS FOUND AND WAS BLENDED OUT AS PER SRM B767-300 SRM 53-00-01 ALLOWABLE DAMAGE 1. AFTER THE BLEND OUT, THE MEASURED MINIMUM FUSELAGE SKIN THICKNESS WAS 0.178", A 2SDR MK1Y20210221007Skin · damagedFUSELAGE SKIN STA 1270 BETWEEN STR 29R/34R P/N 146T3510-3 AND REPAIR SCUFF PLATES, BETWEEN STA 1270 AND STA 1285, P/N 146T8051-1 AND 146T8051-3.
IMPACT DAMAGE HAS BEEN FOUND ON FWD EDGE OF AFT CARGO DOOR AT STA 1270 STR 31R.
THE DAMAGE SKIN IS MADE FROM 0.SDR MK1Y20210221005Skin · scratchedSEVERAL SCRATCHES BLENDED OUT ON EXTERNAL FUSLAGE SKIN AT STA 1417 STR 29L-31L THE BLENDOUTS FALL ON RIVETED AREA AND DO NOT MEET SRM ALLOWABLE DAMAGE REQUIREMENTS.SDR MK1Y20210221003Skin · damagedSEVERAL SCRATCHES BLENDED OUT ON EXTERNAL FUSELAGE SKIN BELOW WING TO BODY FAIRING AT STA 698 STR 21R THE BLENDOUTS FALL ON RIVETED AREA AND DO NOT MEET SRM ALLOWABLE DAMAGE REQUIREMENTS.SDR MK1Y20210221002Skin · damagedSEVERAL SCRATCHES BLENDED OUT ON EXTERNAL FUSELAGE SKIN BETWEEN STA 1345- STA 1351 STR 21R-22R THE BLENDOUTS FALL ON RIVETED AREA AND DO NOT MEET SRM ALLOWABLE DAMAGE REQUIREMENTSSDR MK1Y20210221001Skin · damagedSEVERAL SCRATCHES BLENDED OUT ON EXTERNAL FUSELAGE SKIN BETWEEN STA 1344- STA 1356 STR 28R-30R THE BLENDOUTS FALL ON RIVETED AREA AND DO NOT MEET SRM ALLOWABLE DAMAGE REQUIREMENTSSDR 2021F00031Control Panel · shortedDURING SCHEDULE FLIGHT FROM MCO TO SJU, CREW CALLED WITH SMOKE IN THE COCKPIT. MASK WERE DEPLOYED AND EMERGENCY WAS DECLARED. NO DIVERSION FORM ORIGINAL DESTINATION. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. DURING MTX INSPECTION FOUND SHORT AT FIRE/OH PASDR 2021F00028Test Panel · smokeDURING SCHEDULE FLIGHT FROM MCO TO SJU, CREW CALLED WITH SMOKE IN THE COCKPIT. NO EMERGENCY DECLARED AND NO DIVERSION. AIRCRAFT LANDED WITHOUT INCIDENT. LOG PAGE 241630, ITEM 2.SDR NACA2021020500001Skin · corrodedDISCREPANCY, CORROSION DISCOVERED ON FUSELAGE SKIN LOCATED AT STA1582, BETWEEN STR18R AND STR19R. CORRECTIVE ACTION PERFORMED REPAIR OF SKIN PANEL PN 146T3441-1 SECTION 46 STA1582 & STR19R TO STR20R SKIN PANEL ASSEMBLY PN 146T3440-6 PER BAC B767-300 SRM 53-00SDR MK1Y01292021007Skin · damagedDURING MAINTENENCE INSPECTION FOUND EXISTING UNDOCUMENTED REPAIR ON FUSELAGE SKIN.SDR MK1Y01292021006Skin · damagedDURING MAINTENENCE INSPECTION FOUND DENT DAMAGE ON FUSELAGE SKIN COMMON TO DOCUMENTED EXISTING REPAIR.SDR MK1Y01292021005Skin · corrodedDURING MAINTENENCE INSPECTION FOUND CORROSION DAMAGE ON THE AFT UPPER SKIN OF CENTER WING THAT EXCEEDS UNDER THE TENSION FITTING.SDR MK1Y01292021004Support Beam · wornFAN COWL SUPPORT BEAM LINK FOUND WITH WORN BUSHING (8 EA) AT FWD AND AFT ATTACHMENT POINTS.SDR MK1Y01292021003Cowling · unknownUNDOCUMENTED REPAIR DOUBLERS FOUND AT LT ENGINE ON OUTBOARD CORE COWL OUTER SKIN.SDR MK1Y01292021002Skin · corrodedAFTER REMOVAL OF SATCOM ANTENNA FOUND CORROSION ON FUSELAGE SKIN UNDER ANTENNA ADAPTER.SDR MK1Y01292021001Flap · unknownDURING MAINTENENCE INSPECTION FOUND UNDOCUMENTED DOUBLER REPAIR ON RIGHT WING KRUGER FLAP AT ISS 351.5.SDR MK1Y01132021010Inlet · dentedDURING MAINTENENCE INSPECTION FOUND A DENT WITH CREASE AT ENGINE NR 2 INLET COWL INNER BARREL.SDR MK1Y01132021009Skin · dentedDURING MAINTENENCE INSPECTION FOUND A DENT ON RUDDER SKIN LEFT SIDE BETWEEN RUDDER STA 165 TO 181, 43" FROM RUDDER AFT EDGE.SDR MK1Y01132021008Skin · damagedDURING MAINTENENCE INSPECTION FOUND ON FUSELAGE SKIN, STA 1345 TO STA 1395, STR 24R TO STR 29R EXISTING BLENDOUTS, NICKS, GOUGES AND SCRATCHES.SDR MK1Y01132021007Skin · corrodedDURING MAINTENENCE INSPECTION FOUND CORROSION DAMAGE ON RT WING TRAILING EDGE INBOARD FLAP, REAR SPAR, UPPER CHORD, IFS 166.0.SDR MK1Y01132021006Skin · debondedTHE INNER ALUMINUM SKIN FOUND DISBONDED AND SEPARATED FROM THE ALUMINUM HONEYCOMB CORE PANEL AT STAB STA 107.927 AUX SPAR STA 127.465.SDR MK1Y01132021005Skin · damagedDURING MAINTENENCE INSPECTION FOUND EXISTING BLENDOUT, NICKS, GOUGES AND SCRATCHES ON FWD CARGO DOOR AFT CUTOUT.SDR MK1Y01132021003Skin · damagedDURING MAINTENENCE INSPECTION FOUND EXISTING BLENDOUT, NICKS, GOUGES AND SCRATCHES ON FUSELAGE SKIN, AFT CARGO DOOR CUTOUT, LOWER FWD CORNER.SDR MK1Y01132021002Skin · crackedDURING MAINTENENCE INSPECTION FOUND A CRACK ON THE EXTERNAL SKIN OF ENGINE NR 1 OUTBOARD CORE COWL, AFT EDGE SKIN, AT 10 O'CLOCK.SDR MK1Y01132021001Skin · corrodedDURING MAINTENENCE INSPECTION FOUND CORROSION ON THE UPPER SKIN OF CENTER WING, STA 955, RBL 85.0.SDR NP1Y202101180001Cable · bentNR 2 OUTBOARD THRUST REVERSER FOUND DEACTIVATED. B767-300, REG N348AN IS CURRENTLY UNDERGOING MAINTENANCE . WHILE CONDUCTING ENGINE PRE-CHECKS, IT WAS DISCOVERED THAT A LOCKOUT PLATE HAD BEEN INSTALLED IN THE DEACTIVATED POSITION ON THE CDU OF THE NR 2 ENGINSDR IXXA20210106001Battery · inoperativeIN THE COURSE OF SCHEDULED MAINTENANCE IT WAS NOTED, FLIGHT DECK ENTRY EMERGENCY FLASHLIGHT BATTERY DEAD. INITIATED DEFERRAL MAINTENANCE ITEM 19871. REMOVED AND REPLACED FLIGHT DECK ENTRY EMERGENCY FLASHLIGHT BATTERY, IAW B767 AMM 25-64-00 AND LOPA 767-300 DSDR MK1Y20201202018Skin · damagedUPPER FUSELAGE, STA 1197+66 TO STA 1197+132, STR 2L-STR 2R. DURING CONVERSION PROCESS, THE GLOBAL COMMUNICATION SUITE (G.C.S) ANTENNA WAS REQUESTED TO BE DEACTIVATED AND REMOVED FROM THE AIRCRAFT PER CUSTOMER REQUEST, PRODUCTION ORDER NR 11. THE SKIN UNDERNESDR MK1Y20201202017Skin · damagedFUSELAGE SKIN, STA 1347, 1.5" ABOVE STR-29R AND STR-30R, EXISTING BLEND OUTS (2 EA). SHOP FOUND EXISTING BLENDOUT IN FUSELAGE EXTERNAL SKIN THAT IS NOT PERMITTED IN ACCORDANCE WITH SRM 53-00-01, FIG 101, DETAIL II. PERFORMED NDT INSPECTION, ONE, ORIGINAL THSDR MK1Y20201202016Skin · scratchedFUSELAGE SKIN, STA 1417 STA 1461; STR 33L-STR 34L. DURING THE MAINTENANCE INSPECTION AT IAI, MULTIPLE SCRATCHES BLENDED OUT ON EXTERNAL FUSELAGE SKIN BETWEEN STA 1417 STA 1461, STR 33L STR 34L WAS FOUND. THE BLEND OUTS WERE MEASURED AND IT WAS FOUND THAT THESDR MK1Y20201202005Skin · damagedDURING MAINTENANCE INSPECTION AT IAI, AN EXISTING BLEND OUT WAS FOUND ON FUSELAGE EXTERNAL SKIN AT STA 372, STR 32R. A FASTENER IS LOCATED IN THE AFFECTED AREA WHILE IT IS RESTRICTED, PER SRM 53-00-01 ALLOWABLE DAMAGE 1. THE BLEND OUT WAS MEASURED AND FOUND SDR MK1Y20201202004Skin · damagedFUSELAGE SKIN STA 448-STA 455, STR 27R, DURING MAITENANCE FOUND EXISTING BLEND OUT AT FUSELAGE SKIN (SECTION 43) FROM STATION 448 TO STATION 455, STRINGER 27R. THE REWORK IS RESTRICTED, PER B767-300 SRM 53-00-01 ALLOWABLE DAMAGE 1 DETAIL II SEVERAL FASTENERS SDR MK1Y20201202002Skin · damagedFUSELAGE SKIN, STA 1043, STR 2L-STR 2R. DURING CONVERSION WORK, THE SATCOM ANTENNA HAS BEEN DEACTIVATED AND REMOVED FROM THE AIRCRAFT, PER CUSTOMER REQUEST. BURNT OUT FUSELAGE SKIN HAS BEEN FOUND AFTER THE REMOVAL.SDR MK1Y20201023007Skin · damagedDURING MAINTENENCE INSPECTION FOUND AN EXISTING BLENDOUT ON THE EDGE OF THE SKIN OF AFT CARGO DOOR SURROUND AT STA 1346, STR 30R TO STR 31R.SDR MK1Y20201023006Skin · deformedDURING MAINTENENCE INSPECTION FOUND DEFORMATION/CREASE ON THE NOSE SKIN OF SLAT NR 9 AT OSS 601.55.SDR MK1Y20201023005Skin · deformedDURING MAINTENENCE INSPECTION FOUND DEFORMATION/CREASE ON THE NOSE SKIN OF SLAT NR8 AT OSS 505.95.SDR MK1Y20201023004Skin · dentedDURING MAINTENENCE INSPECTION FOUND DEFORMATION/CREASE ON THE NOSE SKIN OF SLAT NR 4 AT OSS 583.55.SDR MK1Y20201023003Skin · dentedDURING MAINTENENCE A DENT WITH SCRATCH INSIDE FOUND ON FUSELAGE SKIN AT STA 1219, STR 24R.SDR MK1Y20201023002Skin · corrodedDURING MAINTENENCE INSPECTION CORROSION DAMAGE FOUND ON THE UPPER AFT SKIN OF CENTER WING AT STA 955, RBL 80.0.SDR MK1Y20201023001Skin · dentedDURING MAINTENANCE INSPECTION FOUND A DENT WITH CREASE ON FUSELAGE SKIN, STA 412 TO STA 434, STR 34L TO STR 35L, DENT RATIO IS 18.5.SDR NACA2020101500017Shutoff Valve · erraticDISCREPANCY: IN CRUISE AFTER 30 MINUTES GOT EICAS MESSAGE "RT ENGINE HPSOV". RETURNED TO KMIA. REPLACED RIGHT HPSOV, IAW AMM 36-11-07. OPERATIONS CHECKED GOOD DURING HIGH POWER ENGINE RUN. ETOPS SS.SDR 6PMR302203670003Spar · corrodedREPAIR: LEFT WING TRAILING EDGE, CORROSION ON SPAR UPPER CHORD WS 900. INSTALLED REPAIR STRAP 7075-T6, 0.063" THICK, PER EO NR 20425-2 REV IR 8110-3 ISSUED NR 20425-2.SDR 6PMR302201780002Door · corrodedREPAIR: POTABLE SERVICE DOOR HAS CORROSION UNDER AFT LATCH. CORRECTIVE ACTION: REMOVED AND REPLACE POTABLE WATER SERVICE DOOR, IAW B767-3 AMM 52-49-03.SDR 6PMR302201780001Skin · corrodedREPAIR: RT HORIZONTAL STABILIZER UPPER SKIN BETWEEN STAB STA 13.83 AND STAB STA 32.67 B767 8110-3 ISSUED NR 20415. FABRICATE EXTERNAL DOUBLER.SDR 120B2020091000105Display · inoperativeUPPER EICAS DISPLAY IS INOP.SDR 2020F00413Duct · gougedAIRBORNE/PEMCO NON-ROUTINE 2911N98 (3022.0098) DISCREPANCY: NR 2 ENGINE INBOARD T/R BIF-DUCT HAS 2 GOUGES ON AFT OUTER SLEEVE. CORRECTIVE ACTION: EVALUATED NR 2 ENGINE INBOARD TR BIF-DUCT AFT OUTER SLEEVE MATERIAL REMAINING AT LOWEST POINT .044", MAX ALLOWABLSDR 6PMR202008240002Skin · damagedDISCREPANCY: 4 EA FASTENER HOLES STA 1197+66 BETWEEN S1L AND S1R STEP UP HOLE SIZE UNTIL CLEAN AND ROUND, PERFORM ROTOPROBE INSPECTION. CORRECTIVE ACTION: CLEANED 2 EA HOLES TO 0.266, 1 EA HOLE TO 0.277 AND 1 EA HOLE TO 0.310, IAW B767-300 SRM 51-40-05. COMPSDR MK1Y20200731008Tee Fitting · crackedFOUND CRACK AT NOSE GEAR WHEEL WELL ON TEE CHORD AT STA 287, RBL 25, WL 174.
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