Boeing 767-332
Service difficulty reports · 11,959
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 = '767332' 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 = '767332' 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 DL76K050709Skin · gougedRT HORIZONTAL STABILIZER / UPPER SKIN AT RIB 12, S-5 / REPAIR OF GROUND DAMAGE. GOUGE DUE TO GROUND DAMAGE WAS CUT OUT OF THE RT HORIZONTAL STABILIZER UPPER SKIN AT RIB 12 AND S-5. AN ALUMINUM EXTERNAL DOUBLER IS INSTALLED WITH HI-LOKS TO REPAIR THE DAMAGE.SDR DL76L050703Brake Assy · leakingDURING LANDING ROLLOUT TOWER ALERTED CREW OF SMOKE/VAPOR IN WHEEL WELL AREA. BAA REQUESTED MTC CHECK PRIOR TO TOW ONTO STAND. AFTER INSPECTION, FOUND NR 4 BRAKE UNIT LEAKING AT BRAKE CYLINDER. ISOLATED SYSTEM AND TOWED ONTO STAND. BRAKE REPLACED PER MM ANDSDR DL76S050694Line · leakingIN FLIGHT EICAS MESSAGES C-HYD PRESS AND C-HYD QTY SHOWED .07RF, LATER WENT TO ZERO. CENTER ELEC 1 AND 2 PRESS AND CENTER AIR PRESS LIGHTS ILLUMINATED. C/W QRH PROCEDURE. INSPECTED AND FOUND HYD LINE COMING FROM RT BRAKE METERING VALVE TO T FITTING CRACKED.SDR DL76L050685Bulb · inoperativeSEAT 4FG EMERGENCY AISLE LIGHTS INOP. RELAMPED, OPS OK.SDR DL76L050684Oven · contaminatedSIGNIFICANT WATER LEAK AFT GALLEY BEHIND OVENS. RTB. REMOVED OVENS LT SIDE OF AFT GALLEY. INSPECTED AREA AROUND OVENS, FOUND SMALL AMOUNT OF WATER IN OVENS BUT NOT OUTSIDE OF OVENS. CLEANED UP AREA. NO LEAKS NOTED.SDR DL76L050676Charger · unknownMID CABIN SEAT EMERGENCY LIGHTS FROM SEAT ROW 6-20 FG. REPLACED POWER SUPPLY.SDR DL76G050675Fseu · failedON APPROACH T/E FLAP DISAGREE WHEN FLAPS 25 SELECTED RIGHT SIDE STAYED AT 20 LEFT WENT TO 25. LANDED WITH T/E FLAPS 20. REPLACED FSEU AND POSITION INDICATOR.SDR DL76L050673Fan · failedAFTER PUSHBACK AND ENGINE START SMOKE ODOR NOTICED IN CABIN. EICAS MESSAGE FORWARD EQ SUP FAN. REPLACED FAN.SDR DL76S050672Drag Brace · looseLANDING GEAR UNSAFE AURAL WARNING AND GEAR DOOR LIGHT ILLUMINATED ON LANDING TOUCHDOWN. REPLACED LEFT MLG UPPER DRAG BRACE SPINDLE. INSPECTED GEAR AS PER ERA 01-0451457-14.SDR DL76S050662Engine · making metalIN CRUISE, THE RT ENG HAD VIBRATION TO 5.0. DURING T/S IN FLT, THE ENG ANALYST AT HOME GOT A SMART SIGNAL THAT SHOWED A SHIFT IN F/F GET AND LOW N-2 ROTOR SPEED OCCURRED. CALLED THE MTC COORDINATOR WHILE ON THE RADIO PATCH AND ADVISED WHAT OBSERVED. ADVISEDSDR DL76L050660Tire · damagedA/C REJECTED T/O AT 100 KTS DUE SWERVED RIGHT AND POPPING NOISE HEARD ON LEFT. PERFORMED HIGH ENERGY STOP INSPECTION NR 1 AND NR 2 TIRES HAD MINOR CHUNKING DAMAGE. REPLACED SAME AND REPLACED NR 2 BRAKE AS PRECAUTION.SDR DL76G050656Scavenge Pump · failedFL 390 DURING CABIN WALK NOTICED SMELL IN MID CABIN AREA. MID CABIN SMOKE DETECTOR SOUNDED, NO SMOKE NOTICED. NO SMELL OR SMOKE IN COCKPIT. REPLACED LUBE SCAVENGE PUMP IN LEFT ENGINE.SDR DL76S050652Module · failedUNSHEDULED STAB TRIM EICAS MESSAGE. ABORTED T/O AT 100 KTS. REPLACED LEFT STAB TRIM CONTROL MODULE BRAKE PRESSURE SWITCH.SDR DL76G050651Engine · smokeCREW REPORTS SMOKE OIL SMELL HAZE IN CRUISE. DONNED MASK AND MADE AN EMERGENCY LANDING. SMOKE DETECTORS IN CABIN WENT OFF. ENGINE USED 5 PINTS OF OIL. ENGINE CHANGED.SDR DL76S050650Skin · corrodedFUSELAGE/SKIN/STA 1197+132 - STA 1219 BELOW S-36R CORRODED. CORROSION DAMAGE CUT OUT FROM SKIN AT LAP SLICE AND AN EXTERNAL ALUMINUM DOUBLER AND FILLER INSTALLED WITH HI-LOKS.SDR DL76L050648Connector · looseSEAT 38B EMERGENCY SEAT LIGHT INOP. RESEATED CONNECTOR AT SIDEWALL, OPS CHECK OK.SDR DL76L050646Computer · failedAT LEVEL OFF FL330 ALT DISAGREE EICAS LIGHT CAME ON. CAPT ALT READ 300 FEET DIFF FROM F/O ALT. AFTER DESCENT TO FL280 CAPT ALT READ 28010, F/O ALT READ 27760 STDBY READ 28350. PER FIM REPLACED F/O`S ADC AND CHECKS NORMAL. OPS OK PER M/M. ALSO REPLACED F/OSDR DL76S060033Skin · corrodedTHE FUSELAGE SKIN AT BS 1218, S-36R WAS FOUND CORRODED OVER AN APPROXIMATELY 4 INCH BY 8 INCH AREA. THE CORRODED SKIN WAS REMOVED AND A DOULBER INSTALLED.SDR DL76L050635Battery · inoperativeMAIN BATTERY CHARGER STATUS MESSAGE REMAINED ON IN FLIGHT. REPLACED MAIN BATTERY CHARGER AND MAIN BATTERY PER M/M, OPS NORMAL MSG CLEARED.SDR DL76G050626Controller · failedAFTER ENGINE START ACFT BEGAN TO PRESSURIZE THE CABIN TO 1000 FT MSL. AUTO INOP LIGHT CAME ON CABIN AUTO INOP EICAS MSG DISPLAYED AND CABIN AUTO 1 AND CABIN AUTO 2 STATUS MSG. BOTH CABIN PRESS CONTROLLERS FAULTED CONTROLLERS. REPLACED NR 1 CONTROLLER CKS OKSDR DL76G050623Indicator · failedABORTED TAKEOFF AT 100 KTS, DUE TO CAPTS AIRSPEED IND SHOWING 0 AND RED INOP FLAG A/SPD IND STARTED TO WORK AS SOON AS ABORT INITIATED. WORKED OK DURING DECEL ON RUNWAY. REMOVED AND REPLACED CAPT AIRSPEED IND, TESTS OPS NORMAL.SDR DL76S050661Frame · crackedTHE INNER CHORD OF THE LT STA 903.5 FRAME WAS FOUND WITH A 0.60 INCH LONG CRACK. REPAIR ANGLE INSTALLED PER ACTS PP B767-53-21657, REF ER/A 450982-14AD, AD 2003-18-10.SDR DL76L050603Girt Bar · sticking1R ENTRY DOOR SLIDE WILL NOT ARM. LUBRICATED GIRT BAR ARM HANDLE.SDR DL76L050599Module · malfunctionedON TAXI OUT, RUDDER RATIO LIGHT ILLUMINATED, RTB. FOUND LEFT RUDDER RATIO CHANGER MODULE IN TEST MODE. RESET SAME.SDR DL76G050617Engine · failedNR 1 ENGINE, S/N 704883 FAILED OPN 5155 BOROSCOPE INSP DUE TO 1 EA 1ST STAGE NGV HAVING BURN THRU AREA BEYOND M/M LIMITS. ENGINE REMOVAL REQUIRED. ENGINE S/N 704883, REMOVED AND REPLACED PER TRANS 1T160.SDR DL76G050596Controller · malfunctionedAFTER STARTING RT ENGINE PRIOR TO TAKEOFF THE CABIN ALT DESCENDED RAPIDLY APPROX 1000 FPM. AUTO INOP LIGHT ILLUM SHORTLY THEREAFTER. T/S PER FIM. BIT CHECKED CABIN AUTO CONTROLLERS. CABIN AUTO 1 FAULTED SELECTOR PANEL AND AUTO 2 FAULTED ITSELF. PER FIM RESDR DL76L050590Engine · leakingLEFT ENGINE LOSING OIL AT THE RATE OF 1 - 2 QTS/HOUR. CURRENTLY AT 4 QTS GOT DOWN TO 0 - 1 QTS AND ELECTED TO DIVERT TO LGW. REPLACED ENGINE.SDR DL76L050587Tire · cutNR 3 MAIN TIRE HAS DEEP CUTS /3 EA/ 2 THRU SECOND CHORD PLY AND 1 WITH TINY PIECE OF WHITE GLASS. FOUND ON ARRIVAL. REMOVED AND REPLACED NR 3 MAIN WHEEL ASSY. INSP RT MAIN GEAR, NO OTHER DAMAGE NOTED.SDR DL76L050584Lens · missingSEAT MOUNTED ESCAPE PATH LIGHTING AT 3F AND 6B MISSING 1 WHITE LENS AND BOTH BULBS. RELAMPED AND REPLACED WHITE LENS AT SEATS 3F AND 6B. OPS CKS OK.SDR DL76P050576Clamp · looseON TAKEOFF HAD RT DUCT BLEED CAUTION LIGHT AND EICAS MSG . RTO AT 70 KTS. MTC FOUND THE UPSTREAM CLAMP ON THE RT BLEED ISLN VALVE LOOSE. SECURED SAME.SDR DL76K050575Odor · detectedPASSENGERS AND FLIGHT ATTENDANTS SMELLED SMOKE IN CABIN NEAR ROW 46, RAN PACKS AND THOROUGHLY INSPECTED AIRCRAFT.SDR DL76L050571Tire · deflatedDURING PUSHBACK NR 6 MAINWHEEL DEFLATED AND 2 RIM BOLTS SHEARED OFF. REMOVED AND REPLACED MAINWHEEL NR 6 AS PER MM.SDR DL76L050564Altimeter · inoperativeRTB, DUE CAPT ALT INDICATOR FLAG IN VIEW. AFTER POWER RESET FLAG RETRACTED AND IND OK. AFTER TAKEOFF BRU, CAPT ALTIMETER FLAG IN VIEW FLT DIV TO FRA FOR REPAIRS. FRA MTC REPLACED THE CAPT ALTIMETER.SDR DL76G050561Indicator · malfunctionedSTANDBY ATTITUDE GYRO FLAG IN VIEW. REPLACED STANDBY ATTITUDE INDICATOR.SDR DL76S100221Bolt · unknownJOINT BARREL NUT/BOLT ASSY OF VERTICAL FIN REPLACEMENT IAW EO 01-074297-12 ME05.SDR DL76S100220Fitting · unknownWING T/E - INBD FLAP - MAIN FLAP - COLLAR FITTING REPLACEMENT IAW EO 01-073591-12 ME12 AND ME13. C/W EO 01-073591-12 ME12 AND ME13.SDR DL76L050556Bleed Valve · malfunctionedRIGHT ENG BLEED VALVE WILL NOT OPEN. HPSOV DEACT IN CLOSED POSITION. REACTIVATED VALVE BACK TO NORMAL. ENG GRD RUN OK. A/C OK FOR SERVICE.SDR DL76K050553Actuator · inoperativeRUDDER TRIM INOP. REPLACED RUDDER TRIM ACTUATOR.SDR DL76G050550Warning System · activatedSPOILER CONFIG WARNING ACTIVATED DURING TAKEOFF. SUBSEQUENT TAKEOFF CONFIG TEST CONFIRMED SAME PREFLT T/O TEST WAS NORMAL. ONLY SHOWED FLAPS, RESET M620 CARD T/O WARN SYS IN CARD FILE P51. OP CHKS NORMAL, ACTUAL DATE OF FLT 17 IS 091605.SDR DL76G050548Bolt · brokenLE SLAT ASYM EICAS MSG ON APPROACH. FOUND NR 5 SLAT IB S286 TARGET BOLT BROKEN. REPLACED SAME.SDR DL76S050543Engine · leakingODOR DETECTED AND SEVERAL SMOKE DETECTORS WENT OFF. ODOR DISSIPATED WITH UTILITY BUSSES OFF, BUT RETURNED WHEN POWER LEVERS ADVANCED. OIL LEAK NR 1 ENGINE. REPLACED NR 1 BEARING MANIFOLD PKNGS, PERF SAME INSPECTION ON NR 2 ENGINE CKS OK. RAN AT HIGH PWR WISDR DL76L050540Engine · malfunctionedAT T/O CREW REPORTED LEFT DUCT PSI FLUX ALONG WITH L-2 DOOR AREA HAVING VIBRATION AND VIBRATION WAS FELT IN CONTROL COLUMN ROLL MODE. RETURNED TO JFK FOR REPAIRS. INSPECTED LEFT ENGINE FOR BIRD STRIKE. BOROSCOPED AND VIBE SURVEYED. REPLACED PRSOV FOR HISTOSDR DL76G050537Oven · arcedOVEN NR 7 AFT GALLEY SPARKED WHEN TURNED ON AND POPPED C/B. REPLACED SAME.SDR DL76L050533Filter · bypassingRETURN TO GATE FOR PASSENGER CONCERN OF SURGING SOUND UNDER FLOOR AT MID CABIN AREA. REPLACED MODULATING AIR VALVE, NO HELP. REPLACED CONTROL PRESSURE SWITCH, NO HELP. FOUND FILTER BYPASS POPPED. REPLACED FILTER AND ADP, LEAK CHECK GOOD. OPS CHECK NORMAL.SDR DL76L050532Idg · failedRIGHT IDG DROP OFFLINE AND WOULD NOT RESET. BPCU BITE CHECK FAULTS GEN DIODE. REPLACED GCU, NO HELP. REINSTALL ORIGINAL GCU. REMOVED AND REPLACED RIGHT IDG. OPS AND LEAK CHECK OK.SDR DL76L050530Wire · chafedC/B 36 TRIPPED AND WOULD NOT RESET. FOUND WIRES AT THE P22 PNL CHAFED. REPAIRED WIRES.SDR DL76L050529Shutoff Valve · failedRIGHT ENGINE BLEED VALVE WOULD NOT OPEN WHEN SELECTED ON. TRIED NEW PRSOV FILTERS, NO HELP. RERACKED RIGHT ENGINE BLEED CARD, NO HELP. REPLACED RIGHT ENGINE PRSOV, OPS OK.SDR DL76G050514Iru · malfunctionedAFTER T/O IRUS DID NOT RADIO UPDATE. IRU POSITION SHOWED APPROX 200 MILES FROM FIRST WAYPOINT. PERFORMED FULL IRU ALIGNMENT. ALL 3 IRUS CHECKS OK PER AMM. PERFORMED FMS TEST, ALL INPUTS OK. FMS MONITOR TEST OK.SDR DL76G050508Engine · vibrationRIGHT ENGINE FAN VIBS 4.7 HIGH FREQ VIBES FELT. RETURNING TO JFK FOR MTC.SDR DL76L050498Valve · malfunctionedRTB - LEFT ENGINE BLEED LIGHT WITH PRV STATUS MSG . REPLACED VALVE.
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