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.

SDR 21GA202605260000Skin · delaminatedDELAMINATION LOCATED ON LEFT SIDE OF VERTICAL STABILIZER PANEL BETWEEN SPAR AND FRONT SPAR FSS 220.521 - 270-784 (MAJOR REPAIR)May 26, 2026 · N999YV · Boeing 767241 · Vertical Stabilizer, Plate/SkinSDR 21GA2026052623801Seat Track · corrodedCORROSION FOUND ON SEAT TRACK AT STATION 1125 MAIN DECK AT LBL 11 AND RBL 11 (MAJOR REPAIR)May 26, 2026 · N999YV · Boeing 767241 · Fuselage, Seat/Cargo Attach FittingsSDR 21GA2026052623806Window Frame · crackedWINDOW FRAME AT STATION 944 LH SIDE IS CORRODED AT CENTER OF LOWER EDGE. (MAJOR REPAIR)May 26, 2026 · N999YV · Boeing 767241 · Fuselage Main, StructureSDR 21GA2026052623805Frame · crackedCRACK FOUND IN CENTER WING REAR SPAR AT STATION 953 BBL 1RMay 26, 2026 · N999YV · Boeing 767241 · Fuselage Main, FrameSDR 21GA2026052623803Skin · corrodedCORROSION FOUND ON UPPER SURFACE OF CENTER SECTION AT BS 955.1 AT BL 0 (MAJOR REPAIR)May 26, 2026 · N999YV · Boeing 767241 · Fuselage Main, Plate/SkinSDR 21GA2026052623802Skin · corrodedCORROSION ON LOWER RH WING AT WS 314.30 - 372.20 STR 16-18May 26, 2026 · N999YV · Boeing 767241 · Wing, Plate/SkinSDR 21GA20250724016Power Supply · faultedAT FL 390 BEGAN TO EXPERIENCE DUTCH ROLLS WITH AUTO PILOT AND AUTO THROTTLES ENGAGED.DISCONNECTD AP BUT HAD TO HOLD THE YOKE TO THE RIGHT TO MAINTAIN CONTROL. DELCARED EMERGENCY AND DIVERTED TO ST. LOUIS. MAINTENANCE PERSONNEL REPLACED RIGHT CSEU POWER SUPPLY.Jul 24, 2025 · N999YV · Boeing 767241 · Flight Control SystemSDR 21GA20250324003Valve · faultedDURING CRUSIE RECEIVED FWD EQUIPMENT COOLING OVHT MESSAGE. DIVERTED TO OMAHA. REPLACED RH ENG PRVC.Mar 22, 2025 · N999YV · Boeing 767241 · Air Distribution SystemSDR 21GA202503242002Warning Message · false activationDURING CRUISE AT FL 370, RECEIVED EICAS MESSAGE "EQUIPMENT OVERHEAT" MESSAGE. DECENDED TO FL 310. DURING THIS DECENT, RECEIVED "CABIN ALT" MESSAGE. DECLARED EMERGENCY AND DIVERTED. MAINTENANACE PERSONNEL PLACED THE EQUIPMENT COOLING SYSTEM ON MEL AND ACCOMPLISMar 22, 2025 · N999YV · Boeing 767241 · Central WarningSDR 21GA202412223021Engine · surgesRIGHT ENGINE SURGING. IT STOPPED WHEN THROTTLES REDUCED. THERE WERE NO EXCEEDENCES. ENGINE OPERATON BECAME NORMAL AGAIN. PERFORMED BORESCOPE INSPECTION. NO DEFECTS NOTED.Dec 22, 2024 · N881YV · Boeing 767241 · Engine (Turbine/Turboprop)SDR 21GA20241001019Skin · crackedDURING HEAVY CHECK, FOUND CRACKED SKIN CRACKED 1 INCH FWD AND 2.5 INCHES AFT OF IAI PG STRAP. REPAIRED IAW FLIGHT VEHICLES CONSULTING, INC EO #24151-3.Oct 1, 2024 · N999YV · Boeing 767241 · Fuselage Main, Plate/SkinSDR 21GA20241001018Skin · dentedDURING HEAVY CHECK, A DENT AND CREASE WERE FOUND AT FUSELAGE SKIN STA 1279.53 BETWEEN STR 33R AND 35R. WAS REPAIRED IAW FLIGHT VEHICLES CONSULTING, INC. EO # 24151-2.Oct 1, 2024 · N999YV · Boeing 767241 · Fuselage Main, Plate/SkinSDR 21GA20241001017Skin · dentedDURING HEAVY CHECK, DENTS AND CRACKS WERE FOUND BETWEEN FUSELAGE SKIN STA 347 AND 390 AT STR 19R TO 21R. WAS REPAIRED IAW FLIGT VEHICLES CONSULTING INC. EO# 24151-1.Oct 1, 2024 · N999YV · Boeing 767241 · Fuselage Main, Plate/SkinSDR 21GA20240917016Module · faultedON APPROACH TO CVG SELECTED FLAPS AND GOT TRAINING EDGE FLAP DISAGREEE MESSAGE. LANDED WITH FLAPS AT 20 DEGREES.Sep 17, 2024 · N881YV · Boeing 767241 · Trailing Edge Flap Control SystemSDR 21GA20240118001Flt Controls · abnormalAFTER TAKEOFF PASSING 5,000 FT, EXTREMELY LOUD BANGING NOISE ON RH SIDE OF AIRCRAFT. AIIRCRAFT WAS YAWING BACK AND FORTH. FLIGHT CONTROLS FELT LOOSE. DISCONNECTED AUTOPILOT AND RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE PERSONNEL INSPECTED THE AIRCRAFT WIJan 17, 2024 · N881Y · Boeing 767241 · Flight Control SystemSDR 21GA20230228005Skin · crackedDURING MAINTENANCE FOUND CRACK ON SKIN AT RH FUSELAGE FWD UPPER FASTENER AT STA. 1809 AT STR 12A.Feb 28, 2023 · N999YV · Boeing 767241 · Fuselage Structure (General)SDR 21GA20230218003Skin · corrodedCORROSION FOUND ON HORIZONTAL STABILIZER CENTER SECT. UPPER SKIN AT REAR SPAR BETWEEN BL 0.0 & RBL 10.0.Feb 18, 2023 · N999YV · Boeing 767241 · Horizontal Stabilizer StructureSDR 21GA20230202004Skin · corrodedCORROSION FOUND ON FUSELAGE SKIN SECTION 46 AT STA 1197 BETWEEN STR 39R AND STR 36L.Feb 2, 2023 · N999YV · Boeing 767241 · Fuselage Structure (General)SDR 21GA20230125002Keelbeam · corrodedCORROSION FOUND ON LH KEEL BEAM LOWER CHORD BETWEEN STA 959 & 969.5 BETWEEN STA 1000 & 1017.5 LBL 9.5.Jan 25, 2023 · N999YV · Boeing 767241 · Fuselage Structure (General)SDR 21GA202302150001Skin · corrodedCORROSION FOUND ON FUSELAGE SKIN SECTION 46 BETWEEN STA. 1072.75 & 1109 BETWEEN STR. 36L & 36R.Jan 25, 2023 · N999YV · Boeing 767241 · Fuselage Structure (General)SDR 21GA20221003004Keelbeam · corrodedCORROSION FOUND ON FUSELAGE SECTION 43 KEEL BEAM AROUND F.S. 740 AT LBL 9.5.Sep 29, 2022 · N999YV · Boeing 767241 · Fuselage Main, KeelSDR 21GA20220919003Skin · corrodedCORROSION FOUND ON RH INBOARD STABILIZER UPPER SKIN AT FRONT SPAR.Sep 13, 2022 · N881YV · Boeing 767241 · Horizontal Stabilizer, Plate/SkinSDR 21GA20220919002Skin · crackedCRACK FOUND ON RH SIDE OF LOWER FUSELAGE AT STA. 660.Aug 30, 2022 · N881YV · Boeing 767241 · Fuselage Main, Plate/SkinSDR 21GA20220416001None · noneDURING CRUISE, CABIN ALTITUDE AUTO 2 STATUS MESSAGE. ZERO DUCT PRESSURE FROM ENGINE OR APU BLEEDS. PERFORMED EMERGENCY DECENT DUE TO LOSS OF CABIN PRESSURE. MAINTENANCE PERSONNEL PERFORMED A CABIN PRESSURE CONTROL SYSTEM TEST PER AMM. NO FAULTS NOTED. PERFORMEApr 16, 2022 · N999YV · Boeing 767241 · Cabin Pressure Control SystemSDR 21GA20211119001Cooling Duct · rupturedLEFT ENGINE FIRE MASTER WARNING MESSAGE AT FLIGHT LEVEL 260. SHUTDOWN LEFT ENGINE AND RETURNED TO AIRPORT. FOUND LEFT ENGINE LOW PRESSURE TURBINE CASE COOLING DUCT RUPTURED. REPLACED DUCT.Nov 19, 2021 · N881YV · Boeing 767241 · Pneumatic Distribution SystemSDR 21GA20210401001Skin · corrodedCENTER WING-UPPER PLATING BETWEEN LBL 54 - LBL 43 AROUND REPAIR SPAR, CORROSION DAMAGE REPAIR.Apr 1, 2021 · N881YV · Boeing 767241 · Fuselage Main, Plate/SkinSDR 21GA20210401004Skin · corrodedLEFT WING, TRAILING EDGE STRUCTURE AT UPPER FORWARD SECTION BETWEEN WBL 296 TO 283, CORROSION DAMAGE REPAIR.Mar 31, 2021 · N881YV · Boeing 767241 · Wing, Plate/SkinSDR 21GA20210401003Skin · corrodedLEFT WING - UPPER PLATING BETWEEN WBL 190 TO 198 AROUND REAR SPAR, CORROSION DAMAGE REPAIR.Mar 31, 2021 · N881YV · Boeing 767241 · Wing, Plate/SkinSDR 21GA20210401002Skin · corrodedCENTER WING - UPPER PLATTING BETWEEN LBL 7-LBL 9.5 AROUND REAR SPAR, CORROSION DAMAGE REPAIR.Mar 25, 2021 · N881YV · Boeing 767241 · Fuselage Main, Plate/SkinSDR 21GA20191107008Skin · crackedLOWER FUSELAGE SKIN SECTION 43 SKIN CRACKED AT STRINGER 38R AT BS786.Nov 5, 2019 · N999YV · Boeing 767241 · Fuselage Main, Plate/SkinSDR 21GA20191107007Skin · corrodedMULTIPLE AREAS OF SCATTERED SURFACE CORROSION ON FASTENER HEADS ON THE UPPER SURFACE OF THE HORIZONTAL STABILIZER RH BETWEEN THE REAR SPAR AND TRAILING EDGE AT STATION 224.Nov 5, 2019 · N999YV · Boeing 767241 · Horizontal Stabilizer, Plate/SkinSDR 21GA20191107006Skin · corrodedLH WING LOWER SURFACE AT WING STATION 1075 HAS A BLOWOUT (CORROSION) WHERE MARKED AT REAR SPAR.Nov 5, 2019 · N999YV · Boeing 767241 · Wing, Plate/SkinSDR 21GA20191107005Skin · corrodedLH WING LOWER SURFACE AT WING STATION 715 HAS A BLOWOUT (CORROSION) WHERE MARKED AT REAR SPAR.Nov 5, 2019 · N999YV · Boeing 767241 · Wing, Plate/SkinSDR 21GA20191107004Structure · corrodedRH UPPER CENTER TANK SKIN HAS CORROSION AT RBL 71 OF REAR SPAR.Nov 5, 2019 · N999YV · Boeing 767241 · Fuel StorageSDR 21GA20191107003Skin · crackedRH R1 DOOR CUTOUT AFT LOWER CORNER SKIN CRACKED 4” LONG AT STATION 347 BETWEEN STRINGERS 19 & 20 R.Nov 5, 2019 · N999YV · Boeing 767241 · Fuselage Main, Plate/SkinSDR 21GA201702110001Engine · fluctuatesDURING CRUISE AT FLT LEVEL 390 LEFT ENGINE FLUCTUATED ERRATICALLY 400 DEGREES, OTHER PARAMETERS NORMALFeb 9, 2017 · N999YV · Boeing 767241 · Engine (Turbine/Turboprop)SDR 2D7A201612300001Battery Pack · dischargedDURING MAINTENANCE CHECK, THE EXIT SIGNS WOULD NOT ILLUMINATE. FOUND THE BATTERY PACK DISCHARGED.Dec 30, 2016 · N999YV · Boeing 767241 · Emergency LightingSDR 2DYA20151109018Door · wornDURING CRUISE, RECEIVED A E & E BAY DOOR EICAS MSG & DECIDED TO RETURN. NO EMER WAS DECLARED & RETURNED & LANDED SAFELY WITH NO FURTHER INCIDENT. PREVIOUS DMI 999-15-0090 WAS RE-OPENED MEL 52-71-01-01, E & E DOOR MUST BE VERIFIED CLOSED & LATCHED PRIOR TO EANov 7, 2015 · N999YV · Boeing 767241 · Electrical/Electronic Compartment DoorsSDR 2DYA20151101017Sensor · out of adjustAFTER TAKEOFF, CREW NOTICED DURING FLAP RETRACTION, LE SLAT DISAGREE & LE SLAT ASYMMETRICAL STATUS MESSAGE, LE SLAT SHUTDOWN AIR & GROUND DISAGREE, AFTER GEAR RETRACTION. AUTO BRAKES INOPERATIVE. CREW MADE DETERMINATION TO RETURN, DUE TO PREVIOUS DIVERT FOR Nov 1, 2015 · N881YV · Boeing 767241 · Leading Edge Slat Position Indicating SystemSDR 2DYA20151101016Sensor · dirtyAFTER TAKEOFF, CREW NOTICED DURING FLAP RETRACTION LE RETRACTION, LE SLAT ASYMMETRY AIR & GND DISAGREE, AFTER GEAR RETRACTION. AFTER FOLLOWING QRM PROCEDURES, CREW MADE DETERMINATION TO DIVERT. LANDED SAFELY WITH NO FURTHER INCIDENT. FOUND SENSORS VERY DIRTNov 1, 2015 · N881YV · Boeing 767241 · Leading Edge Slat Position Indicating SystemSDR 2DYA20151009013Light · inoperativeDURING C CHECK INSPECTION, INSPECTORS FOUND FLIGHT DECK EMER EXIT LIGHT INOPERATIVE. R & R EXIT LIGHT ASSEMBLY IAW MM 33-51-001. OPERATIONAL CHECKED NORMAL IAW MM 33-51-00 202.Oct 8, 2015 · N881YV · Boeing 767241 · Emergency LightingSDR 2DYA20150526008Light · inoperativeDURING A3 CHECK, INSPECTION FOUND COCKPIT DOOR EMER LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM 33-51-01. OPERATIONAL TESTED NORMAL.Jul 8, 2015 · N881YV · Boeing 767241 · Emergency LightingSDR 2DYA20150526006Terminal · brokenAIRCRAFT ARRIVED WITH NO INBD WRITE-UPS. WHILE MX WAS DOING THE ENG START CHECKLIST TO START TROUBLESHOOTING THE LT ENG PRSOV MEL, IT WAS FOUND THAT THE LT ENG FIRE DETECT SYS WOULD NOT TEST & ONLY NR 2 OVHT LOOP WOULD TEST. AFTER OPENING THE LT ENG COWLINGSMay 22, 2015 · N881YV · Boeing 767241 · Fire DetectionSDR 2DYA2015051300004Radio · failedDURING CRUISE JUST PRIOR TO DESCENT, THE CREW NOTICED THE CENTER VHF COMM WENT BLANK & WAS FOLLOWED BY A STRONG ELEC ODOR & SMOKE. COMPLETED NORMAL APPROACH & LANDED WITHOUT INCIDENT. SMOKE & FUMES IN COCKPIT INSPECTION WAS ACCOMPLISHED. AFTER TROUBLESHOOTIMay 10, 2015 · N999YV · Boeing 767241 · VHF Communications SystemSDR 2DYA20150602007Turbine Blades · damagedCLIMBING THROUGH 4000' CREW HAD HIGH ENG VIBRATION WITH EGT GOING INTO YELLOW ARC ON LT ENG. ENG PULLED BACK TO IDLE THRUST & STILL HAD VIBRATION. ENG SHUTDOWN & RETURNED. VISUAL DAMAGE TO TURBINE BLADES. UPON INSPECTION, BORESCOPE, IT WAS DETERMINED THAT May 6, 2015 · N881YV · Boeing 767241 · Turbine SectionSDR 2DYA20141030002Unknown · malfunctionedCABIN ALTITUDE CONTINUE TO CLIMB ABOVE 10,000 AT LEVEL FLIGHT 40,000. ACFT RETURNED FOR TROUBLESHOOTING. PERFORMED PRESSURIZATION TEST IAW AMM 21-31-00, TESTED GOOD. ACFT DEPARTED AT A LATER DATE WITHOUT EVENT.Oct 21, 2014 · N999YV · Boeing 767241 · Cabin Pressure Control SystemSDR 2DYA20140518002Proximity Switch · faultyAFTER FLAP RETRACTION, FLAP NEEDLES JUMPED BETWEEN 0 & 1. EICAS MSG LE SLAT ASYMMETRICAL & LE ANNUNCIATOR ILLUMINATED. DURING PSEU BITE IAW BFIM 32-09-03, FOUND PROXIMITY SWITCH 282 FAULTY. R & R PROXIMITY SWITCH IAW AMM 27-88-01. CHECKED CLEARANCE BETWEENMay 16, 2014 · N768QT · Boeing 767241 · Leading Edge Slat Position Indicating SystemSDR 2DYA20140518001Warning System · false activationFLAP & SLAT RETRACTION FROM F1 TO 0 SETTING EICAS MSG LE SLAT ASYMMETRICAL. TROUBLESHOOTING IAW BFIM 27-81 FAULT TREE 808 REVEALED NO FAULTS.May 16, 2014 · N768QT · Boeing 767241 · Leading Edge Slat Position Indicating SystemSDR TAMF2012FA0000003Tire · damagedDURING DAILY CHECK, FOUND MAIN TIRE NR 7 DAMAGED, TREAD LOOSE OF THE TIRE. R & R NR 7 TIRE AND WHEEL ASSY IAW AMM 32-45-01, PAGE 401-413. TIRE PRESSURE NORMAL.Dec 25, 2012 · N770QT · Boeing 767241 · TireSDR 2012F00107Engine · making metalEICAS MESSAGE FOR RT OIL FILTER. DISPLAY REMAINED WHEN THRUST REDUCED. RT ENGINE SHUTDOWN. ENGINE VIBRATION DURING CLIMB. DURING INSPECTION FOUND DEBRI IN ALL MAGNETIC CHIP DETECTORS. ENGINE REPLACED.Jun 12, 2012 · N769QT · Boeing 767241 · Engine (Turbine/Turboprop)
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