Boeing 767-241
Service difficulty reports · 165
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 = '767241' 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 = '767241' 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 TAMF2012FA0000001Warning Light · illuminatedDISCONTINUED TAKEOFF, DUE TO BULK CARGO DOOR LIGHT DISPLAYED ON EICAS. DURING GROUND INSPECTION FOUND 1 CARGO BOX LOCATED OVER THE BULK CARGO DOOR PROXIMITY SENSOR. INITIAL HYPOTHESIS IS THE BOX MOVED FROM THE AFT BULK CARGO AREA AND FELL OVER THE SENSOR DURISDR TAMF2011FA0000167Engine · leakingLT ENGINE OIL PRESSURE LIGHT ILLUMINATED EICAS MESSAGE LT ENG OIL PRESSURE. OIL PRESSURE WAS ZERO. OIL QTY ZERO. ENGINE SHUTDOWN, FLIGHT DIVERTED. ACFT LANDED SAFELY. AFTER ENGINE INSPECTION, A CONSIDERABLE QUANTITY OF OIL SPREAD IN ENGINE EXHAUST AREA. SDR TAMF2011FA0000166Electronic Unit · malfunctionedAFTER ACFT ROTATION EICAS DISPLAYED L/E SLAT DISAGREE WITH THE FLAP LEVER IN 5. OVERWEIGHT LANDING, 1000KG LW 1293 KG NO HARD LANDING. HARD LANDING INSPECTION WAS PERFORMED IAW AAM 05-51-35 PAGE 201 TO 203 PHASE I OPTION A. NO DAMAGE FOUND. DURING BITE TESTSDR TAMF2011FA0000165Unknown · odorPILOT REPORT: THE CABIN FILLED WITH SMOKE SMELLING LIKE BURNED HYD FLUID. AFTER 2 MIN SMOKE DISSIPATED. PERFORMED SMOKE OR FUMES IN THE CABIN INSPECTION IAW AMM 05-51-56, PG 201 AND FIM 21-00-21, PG 101-105. NO DISCREPANCIES NOTED.SDR TAMF2011FA0000164Warning Light · illuminatedDURING CLIMB, EICAS MESSAGE L/E SLAT ASSYM DISPLAYED L/E LIGHT ILLUMINATED WITH FLAP LEVER IN 1. BOTH FLAP POINTERS WERE CORRECT. AIR TURN BACK, AN OVERWEIGHT LANDING WAS NOT PERFORMED. ACFT IS DECLARED AOG. GROUND INSPECTION IS IN PROCESS. OPENSDR TAMF2011FA0000163Duct · brokenDURING TAKEOFF, LT BLEED DUCT MSG WAS SHOWN AND AFTERWARDS L/E SLAT ASSYM ALSO WAS ANNUNCIATED ON EICAS. AFTER 45 MIN OF FLIGHT, THE ACFT RETURNED TO DEPARTURE. GROUND INSP FINDINGS: LT WING FIXED L/E LWR PANEL 511KB MISSING, LT WING L/E AIR SUPPLY DUCT, SUPSDR TAMF2011FA0000162Rotary Actuator · corrodedDURING WALK AROUND ON ACFT, FOUND AT LT WING NR 5 SLAT HANGING DOWN FROM ONE SIDE. THE SLAT REMAINED SUPPORTED FROM ONE TRACK WHICH CAUSED HOLES OF SOME PANELS OF WING AND ANTI-ICE TUBES DEFLECTION. AFTER REMOVAL OF SLATS NR 4 AND NR 5 WAS FOUND GEARBOX ASSY SDR TAMF2011FA0000161Rotary Actuator · corrodedDURING CLIMBING STAGE L/E SLAT ASSY APPEARS. AIR TURNBACK. GROUND INSP FINDINGS: DURING VISUAL INSP WAS FOUND SLAT NR 12 HANGING DOWN FROM ONE SIDE. THE SLAT REMAINS SUPPORTED FROM 1 TRACK WHICH CAUSED HOLES OF SOME PANELS OF WING AND ANTI-ICE TUBES DEFLECTIOSDR 2011F00110Smoke Detector · defectiveDURING TAXING TO FINAL DESTINATION POSITION, AFT CARGO FIRE INDICATED, EICAS MSG AFT CARGO FIRE DISPLAYED, FIRE INDICATION REMAINS AFTER BOTTLES DISCHARGED. 3 EA FIRE EXTINGUISHING BOTTLES WERE R & R. 2 EA SMOKE DETECTORS WERE R & R. 2 EA SMOKE DETECTION FSDR TAMF20110430101Skin · corrodedDURING SC4 CHECK, FOUND CORROSION ON LOWER SKIN IFS 180.25-270 TO FRONT SPAR ON AFT FLAP LT. REPAIR WAS PERFORMED WITH EWO 767-57-089.SDR TAMF20110430100Skin · dentedDURING SC4 CHECK, FOUND DENT ON LT L/E SLAT NR4 WEDGE UPPER SKIN, REPAIR WAS PERFORMED WITH EWO 767-57-088.SDR TAMF20110430099Skin · corrodedDURING SC4 CHECK, FOUND CORROSION ON CENTER UPPER WING SKIN PANEL STA 955, RBL 11.06. REPAIR WAS PERFORMED WITH EWO 767-57-087.SDR TAMF20110430098Rib · corrodedDURING SC4 CHECK, FOUND CORROSION ON OTBD FLAP RIB STA 616.2-798.2. REPAIR WAS PERFORMED WITH EWO 767-57-085.SDR TAMF20100097SShaft · corrodedDURING SC4 CHECK, FOUND CORROSION ON OTBD FLAP DRIVE ARM SHAFT. REPAIR WAS PERFORMED WITH EWO 767-57-082.SDR TAMF20100095SLongeron Splice · damagedDURING SC4 CHECK, DURING ACCOMPLISHMENT TO OF EO 53-005 WAS DAMAGE A HOLE ON LONGERON SPLICE PLATE. REPAIR WAS PERFORMED WITH EWO 767-53-147.SDR TAMF201104300096Skin · crackedDURING SC4 CHECK, FOUND A CRACK ON INBD SKIN LT SIDE, FWD TO STA 237.500. REPAIR WAS PERFORMED WITH EWO 767-54-076.SDR TAMF201104300094Failsafe · corrodedDURING SC4 CHECK, FOUND CORROSION ON ONE HOLE SIDE FRAME FAILSAFE FITTING. REPAIR WAS PERFORMED WITH EWO 767-53-146.SDR TAMF201104300093Sill · corrodedDURING SC4 CHECK, FOUND CORROSION ON AFTER SERVICE DOOR LOWER MAIN SILL. REPAIR WAS PERFORMED WITH EWO 767-53-145.SDR TAMF20100092SSeat Track · corrodedDURING SC4 CHECK, FOUND SEAT TRACK LBL 33.00 STA 1329-1351 WITH CORROSION. REPAIR WAS PERFORMED WITH EWO 767-53-143.SDR TAMF201104300091Seat Track · corrodedDURING SC4 CHECK, FOUND TRACK, RBL 33.00, STA 1518-1605 WITH CORROSION. REPAIR WAS PERFORMED WITH EWO 767-53-142.SDR TAMF201104300090Frame · crackedDURING SC4 CK WAS FOUND 2 CRACKS ON FRAME WEB BS 1285, STR 33-35 LT. REPAIR WAS PERFORMED WITH EWO 767-53-137.SDR TAMF201104300089Skin · corrodedDURING SC4 CHECK, FOUND CORROSION ON EXTERIOR SIDE LOWER EDGE LAP SPLICE AREA OF SKIN 148T3221, STA 1582-1725, STR 36L AND SKIN 148T3251 STA 1725.5, STR 36 LT. REPAIR WAS PERFORMED WITH EWO 767-53-136SDR TAMF201104300088Skin · damagedDURING SC4 CHECK, FOUND DENT AND SCRATCH FUSELAGE SKIN STA 1175-1197, STR 23-24 LT. REPAIR WAS PERFORMED WITH EWO 767-53-131.SDR TAMF201104300087Skin · corrodedDURING SC4 CHECK, FOUND CORROSION ON FUSELAGE SKIN STA 478 STR 30-31 RT. REPAIR WAS PERFORMED WITH EWO 767-53-130.SDR TAMF201104300086Skin · corrodedDURING SC4 CK WAS FOUND CORROSION ON FUSELAGE SKIN, STA 1417-1439, STR 26-32, LT. REPAIR WAS PERFORMED WITH EWO 767-53-129.SDR TAMF201043000085Skin · dentedDURING SC4 CK WAS FOUND SKIN DENT STA 1559, STR 31-32 RT. REPAIR WAS PERFORMED WITH EWO 767-53-071.SDR TAMF20104300084Door · wornDURING SC4 CK WAS FOUND WEAR ON RAM AIR DOOR. REPAIR WAS PERFORMED WITH EWO 767-52-030.SDR TAMF201101300083Door Frame · scratchedDURING SC4 CK, FOUND SCRATCH ON FWD CARGO DOOR AFTER FRAME LOWER FITTING STA 614 AFT SIDE. REPAIR WAS PERFORMED WITH EWO 767-52-028.SDR 2011F00074Pin · installedEICAS MESSAGE GEAR DISAGREE DYSPLAYED WITH WITH GEAR HANDLE UP, NOSE GEAR GREEN DN LGT FAILED TO EXTIN DOORS AMBER LIGHT WAS EXT & GEAR LIGHT ILLUMINATED. PERFORMED NLG INSP CHECK AND IT WAS FOUND THE LANDING GEAR NOSE PIN INSTALLED . REMOVED IAW AMM 32-00-2SDR 2011F00073Pin · installedEICAS MESSAGE GEAR DISAGREE DYSPLAYED WITH WITH GEAR HANDLE UP, NOSE GEAR GREEN DOWN LIGHT FAILED TO EXTINGUISH DOORS AMBER LIGHT WAS EXT & GEAR LIGHT ILLUMINATED. PERFORMED NLG INSP CHECK AND IT WAS FOUND THE LANDING GEAR NOSE PIN INSTALLED . REMOVED IAW AMMSDR 2011F00072Pin · installedEICAS MESSAGE GEAR DISAGREE DISPLAYED WITH WITH GEAR HANDLE UP, NOSE GEAR GREEN DN LGT FAILED TO EXTEND DOORS AMBER LIGHT WAS EXT & GEAR LIGHT ILLUMINATED. PERFORMED NLG INSPECTION CHECK AND IT WAS FOUND THE LANDING GEAR NOSE PIN INSTALLED. REMOVED IAW AMM 3SDR TAMF201103110082Skin · corrodedDURING C4 CHECK LT WING UPPER SKIN CORROSION AT WS 349.70. REPAIR WAS PERFORMED WITH EWO 767-57-080.SDR TAMF201103110081Skin · dentedDURING C4 CHECK RT WING, SLAT NR 9, NOSE SKIN DENT AND SCRATCH REPAIR, REPAIR WAS PERFORMED WITH EWO 767-57-078.SDR TAMF201103110080Skin · corrodedDURING C4 CHECK CORROSION ON LT UPPER WING SKIN. BLEND OUT AT WS 416 AFTER OF REAR SPAR. REPAIR WAS PERFORMED WITH EWO 767-57-077.SDR TAMF20100079SArm · corrodedDURING C4 CHECK RT OTBD T/E FLAP DRIVE ARM CORROSION. REPAIR WAS PERFORMED WITH EWO 767-57-076.SDR TAMF201103110078Drive Shaft · corrodedDURING C4 CHECK RT OTBD T/E FLAP - DRIVE ARM SHAFT WITH CORROSION. REPAIR WAS PERFORMED WITH EWO 767-57-075.SDR TAMF201103110077Drive Shaft · corrodedDURING C4 CHECK LT OTBD OTBD T/E FLAP - DRIVE ARM SHAFT WITH CORROSION. REPAIR WAS PERFORMED WITH EWO 767-57-075.SDR TAMF201103110076Skin · corrodedDURING C4 CHECK RT WING - LOWER SKIN - 990.7 TO 1018.2 REAR SPAR - RT WITH CORROSION. REPAIR WAS PERFORMED WITH EWO 767-57-074.SDR TAMF201103110075Skin · corrodedDURING C4 CHECK RT WING - LOWER SKIN CORROSION REPAIR- CENTER SPAR STA WS 616.2 - 746.2 RT. REPAIR WAS PERFORMED WITH EWO 767-57-073.SDR TAMF201103110074Skin · damagedDURING C4 CHECK RUDDER SKIN PANEL ULTRASONIC INSP FINDING, STA 115.142- LT. REPAIR WAS PERFORMED WITH EWO 767-55-018.SDR TAMF201103110073Latch · corrodedDURING C4 CHECK FUSELAGE 43- LATCH FITTING BORE CORROSION LATCH LARGE CARGO DOOR STA 510-586. REPAIR WAS PERFORMED WITH EWO 767-53-127.SDR TAMF201103110072Cargo Track · corrodedDURING C4 CHECK MAIN CARGO COMPARTMENT SEAT TRACK - LBL 54.75 BETWEEN FSLG STA 1439 TO 1461 WITH CORROSION. REPAIR WAS PERFORMED WITH EWO 767-53-126.SDR TAMF201103110071Cargo Track · corrodedDURING C4 CHECK MAIN CARGO COMPARTMENT SEAT TRACK - LBL 33.00 BETWEEN FSLG STA 1580 TO 1605 WITH CORROSION. REPAIR WAS PERFORMED WITH EWO 767-53-125.SDR TAMF201103110070Cargo Track · corrodedDURING C4 CHECK MAIN CARGO COMPARTMENT SEAT TRACK - RBL 11.00 BETWEEN FSLG STA 1439 TO 1461 WITH CORROSION. REPAIR WAS PERFORMED WITH EWO 767-53-124.SDR TAMF201103110069Cargo Track · corrodedDURING C4 CHECK MAIN CARGO COMPARTMENT SEAT TRACK - RBL 33.00, BETWEEN FSLG STA 1518 TO 1605 WITH CORROSION. REPAIR WAS PERFORMED WITH EWO 767-53-123.SDR TAMF201103110068Keelbeam · corrodedDURING C4 CHECK FUSELAGE SECTION 45 - KEEL BEAM CORROSION DAMAGE, HORIZ WEB STA 805, RBL 9.5. REPAIR WAS PERFORMED WITH EWO 767-53-122.SDR TAMF201103110067Skin · corrodedDURING C4 CHECK FUSELAGE SECTION 41/43 CORROSION DAMAGE ON SKIN SPLICE PLATE STA 434, STR 38 RT. REPAIR WAS PERFORMED WITH EWO 767-53-121.SDR TAMF201103110066Frame · crackedDURING C4 CHECK FUSELAGE FRAME WEB STA 1395, RBL 14.5, STR 34L - 37L, THERE ARE 2 CRACKS IN THE FRAME WEB. REPAIR WAS PERFORMED WITH EWO 767-53-120.SDR TAMF201103110065Frame · corrodedDURING C4 CHECK FUSELAGE SECTION 45" CORROSION DAMAGE TO BULKHEAD WEB- UPPER FRAME STA 1065 S11R, S12R. REPAIR WAS PERFORMED WITH EWO 767-53-119.SDR TAMF201103110064Skin · dentedDURING C4 CHECK FUSELAGE SECTION 43 SKIN DENT DAMAGE STRINGER CRACK, STA 720 S22L - S24L. REPAIR WAS PERFORMED WITH EWO 767-53-118.
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