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 DL76G060895Transmission · unknownRTB AFTER LGEN WAS INDICATED ON EICAS. L DRIVE LIGHT REMAIN ON. FWD TO MEL PLACARD PER 24-00-01. REMOVED AND REPLACED NR 1 ENG IDG ASSY IAW MM. PERFORMED ENG RUN PER DELTA PFH, OPS CHK OK LEAK CHK OK MSGS CLEARED MCO AND PLACARD REMOVED.SDR DL76G060890Valve · intermittentADVANCED THE POWER FOR T/O AND GOT T/O CONFIG WARNING HORN AND LIGHT ALONG WITH A FALSE RED PARKING BRAKE EICAS MSG. WE WERE ROLLING T/O AND WERE BELOW 60 KTS. THE PARKING BRAKE WAS NOT SET. RAN CONFIG TEST IAW AMM. PARK BRAKE SWITCH CKS, GOOD. REPLCD PARK BRASDR HALA0600832Cylinder · leakingETOPS SIGNIFICANT SYSTEM, APU VARIABLE VOLUME CHAMBER CYLINDER HAS AIR LEAKING FROM ATTACH POINT GASKET. REMOVED AND REPLACED GASKET VOLUME CHAMBER CYLINDER. RAN APU AIR LEAK CHK OK.SDR DL76G060886Pressure Switch · malfunctionedDURING TAXI OUT LT ENG FUEL FILTER STATUS MSG ILLUMINATED -RTB. REPLACED DIFF PRESS SWITCH AND FUEL FILTER. ETOPS CATEGORY (E): PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.SDR DL76G060878Line · brokenAT FL330 LEFT ENG OIL PRESSURE AND QUANTITY DROPPED TO ZERO. ENGINE SUBSEQUENTLY FLAMED OUT. ENGINE SHUTDOWN, CHECKLIST PERFORMED, 38K LBS OF FUEL DUMPED FROM CTR TANK. NORMAL SINGLE ENG LANDING. FOUND OIL LINE AND CLAMP GOING TO OIL PRESS TRANSMITTER BROKSDR DL76S060877Floorbeam · corrodedCORROSION WAS FOUND AROUND THE NUT PLATES ON THE LOWER TEE OF THE 1502 FLOORBEAM. THE CORROSION WAS REMOVED AND REPAIR PARTS INSTALLED PER BOEING INSTRUCTIONS AS CONTAINED IN 456631-14.SDR DL76S060876Skin · crackedTHE FUSELAGE SKIN WAS FOUND CRACKED AT THE NR 3 VHF ANTENNA, FS 1197+90, AT STR 39L 39R. REPAIR INVOLVED CUTTING OUT THE DAMAGE AND INSTALLATION OF BOEING APPROVED REPAIR PARTS PER ERA 455968-14.SDR DL76S060875Fitting · corrodedCORROSION WAS IDENTIFIED ON THE INBOARD FORWARD SURFACE OF THE REAR SPAR BULKHEAD TERMINAL FITTING. THE BOEING APPROVED REPAIR INVOLVED REMOVING BOLTS FOR ACCESS AND LIGHT BLENDING OF THE SURFACE TO REMOVE THE CORROSION PER ERA 456629-14.SDR DL76S060873Spar · crackedTHE NUMBER 1 PYLON UPPER SPAR FITTING, RHS AT ATTACH FITTING HOLE SHOWED A CRACK INDICATION. THE SUBJECT HOLE WAS OVERSIZED, AND THE BOEING APPROVED REPAIR INVOLVED INSTALLATION OF A STRAIGHT SHANK FREEZE PLUG PER ERA 456634-14.SDR DL76S060871Bulkhead · damagedDURING ACCOMPLISHMENT OF THE SIP MOD ON THE AIRCRAFT, AN EXISTING FREEZE PLUG REPAIR WAS FOUND ON THE NR 1 PYLON LHS UPPER ATTACH HOLE FOR GSE FITTING. THE PLUG WAS COMMON TO THE BULKHEAD FLANGE AND SIDE LOAD FITTING. THE SIDE LOAD FITTING WAS REPLACED AS PASDR DL76S060870Spar · damagedDURING ACCOMPLISHMENT OF EO 01-074906-03 THE NUMBER 2 PYLON SPLICE PLATE UPPER OUTBOARD HOLE WAS FOUND TO ALREADY BE OVERSIZED TO BEYOND MAX EO LIMIT. THE BOEING APPROVED REPAIR INVOLVED INSTALLATION OF AN OVERSIZED FASTENER PER ERA 456537-14.SDR DL76S060869Fitting · damagedTHE NUMBER 2 PYLON UPPER SPAR FITTING WAS FOUND TO HAVE A PREVIOUSLY OVERSIZED HOLE, AT THE AFT OUTER PERIMETER FASTENER. A BOEING APPROVED REPAIR WAS INSTALLED AT THE SUBJECT LOCATION, PER ERA 456536-14.SDR DL76S060868Skin · misrepairedA PREVIOUS REPAIR FOUND ON THE FUSELAGE SKIN AT 500 AND S36L DOES NOT CONFORM TO SRM AND NO RECORDS WERE FOUND. REPAIR WAS REMOVED AND A BOEING APPROVED REPAIR WAS INSTALLED PER ERA 456627-14.SDR DALA1102780137Bulkhead · unknownFUSELAGE NLG WHEEL WELL AFT BULKHEAD STA 287, LBL 25 CHORD, WL 173. REPAIRED IAW ERA 458240-14AD.SDR DL76S060867Charger · inoperativeON DOM A CHECK FOUND EMERGENCY LIGHTS BATTERY CHARGER M9010 AT ROW 45FG CAUSING EMERGENCY LIGHTS TO BE DIM FOR THE BACK PART OF THE CABIN ROW 35 AFT. REMOVED AND REPLACED BATTERY CHARGER ASSY PER M/M, CKS GOOD.SDR DL76L060864Oxygen Mask · unknownCREW O2 WENT TO 60 PSI DURING FLT CAPTS O2 MASK MADE A GASPING SOUND. DIVERTED TO YYT FOR REPAIR. AIR CANADA EQ AMTS SERVICED CREW O2 AND ISOLATED LEAK TO CAPTS MASK. SWAPPED WITH 2ND OBS MASK AND FWD 2 OBS O2 MASK TO MCO PER MEL 25-11-02B.SDR DL76G060865Transformer · unknownUPON THRUST APPLICATION TAKEOFF WARNING HORN SOUNDED AND FLAPS INDICATED ON EICAS. FLAPS/SLAT ELEC THEN ILLUMINATED ON STATUS PAGE. REPLACED T153 TRANSFORMER IN P36 PANEL. PERFORMED TEST PER FIM 27-58-00 PG 107 AND 108. SYS CHKS OK. ALSO RESET POPPED FLAP/SSDR DL76S060889Bulkhead · crackedTHE NLG BULKHEAD AFT WEB AND CHORD AT STA. 287, RBL 25 HAS DRILL DAMAGE TO THE WEB AND CHORD AND THE CHORD WAS STOP DRILLED INSTEAD OF CUT OUT AS REQUIRED PER THE SRM. THE EXISTING REPAIR ANGLE WAS REMOVED AND THE CRACKED CHORD WAS CUT OUT. THE DRILL DAMAGEDSDR DL76L060855Seat · arcedCAPT SEAT ARCED TWICE DURING ELECTRICAL MOVEMENT. DISCONNECTED SEAT CONNECTOR C/B H-15 ON P6-3 PANEL POPPED. FWD TO MCO C/B PULLED PLACARD INSTALLED. REPLACED CAPTS SEAT ASSY, CHECKS GOOD. MCO/PLAC REMOVED.SDR DL76L060854Mount · crackedDURING ENG EXT HARDWARE INSP, FOUND AFT MOUNT RAILS CRACKED. REPLACED NR 1 ENG.SDR DL76L060853Flange · crackedFOUND CRACKED R FLANGE ON NR 2 ENG OUT OF M/M LIMITS. REPLACED NR 2 ENG PER TRANS 1T149.SDR DL76G060852Actuator · unserviceableNR 1 ENG SPAR VALVE LIGHT REMAINS ILLUMINATED AFTER FUEL CONTROL SW IS PLACED TO RUN. THEREFORE NO FUEL FLOW AND NO ENG START. REPLACED NR 1 ENG SPAR VLV ACTUATOR MPN MA20A1001-1 PER M/M. CHECKS GOOD.SDR DL76L060849Battery Pack · dischargedLT SIDE EXTERIOR EMERGENCY LIGHTS INOP L396 AND L-645. REPLACED BATTERY PACK AT M-738.SDR DL76L060999Skin · dentedDURING HMV A DENT WAS FOUND IN THE EXTERIOR SKIN IN THE AREA OF THE AFT CARGO DOOR CUTOUT. THE DENT IS LOCATED AT FS 1373 BETWEEN S-28R AND S-29R. THE DENT WAS INSPECTED AND PUT ON A REPETITIVE RE-INSPECTION PROGRAM PER ERA 457839-14.SDR DL76S060844Skin · corrodedCORROSION WAS FOUND IN THE SKIN AROUND THE RHS DME ANTENNA CABLE. CORROSION WAS BLENDED AND A BOEING APPROVED REPAIR INSTALLED PER ERA 456420-14.SDR DL76S060843Floorbeam · crackedUPPER CHORD OF THE STA 999 AT LBL 33 FLOORBEAM WAS FOUND CRACKED IN THE VERTICAL FLANGE FROM THE AFT SLOTTED CUTOUT TO THE END OF THE CHORD. THE CRACK WAS REMOVED BY EXTENDING THE SLOT CUTOUT TO THE END OF THE CHORD AND WAS REPAIRED WITH A REPAIR ANGLE APPROSDR DL76S060839Spar · crackedCRACK WAS FOUND IN LOWER OB FASTENER HOLE IN REAR SPAR. THE CRACK WAS REMOVED BY OVERSIZING HOLE AND INSTALLATION OF A FLANGED BUSHING IAW MFG INSTRUCTIONS. REPAIR ERA 455471-14.SDR DL76S060838Web · damagedWEB AT STA 654+121, LBL 40 WAS FOUND DAMAGED, CARGO COMPARTMENT JUST BELOW INNER CHORD. REPAIR WILL INVOLVE CUTTING THE WEB, SPLICING IAW INSTRUCTIONS. REPAIRED IAW ERA 455777-14.SDR DL76S060846Skin · gougedGOUGES WERE FOUND IN THE FUSELAGE SKIN PANEL IN THE VICINITY OF AN EXISTING REPAIR. EXISTING REPAIR REMOVED AND ONE LARGE EXTERNAL REPAIR DOUBLER INSTALLED PER BOEING INSTRUCTIONS ERA 456554-14.SDR DL76G060857Skin · damagedTHE FUSELAGE SKIN WAS GOUGED AND DENTED BETWEEN STA 325 AND 347, S-34L-35L. THE DAMAGED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.SDR DL76S060834Skin · corrodedDURING ROUTINE MTC CORROSION AND MINOR CRACKS WERE FOUND IN FUSELAGE SKIN AT 789.5 AND S-38L. SKIN WAS TRIMMED, DOUBLER AND TRIPLER INSTALLED IAW 455466-14 IAW MFG INSTRUCTIONS.SDR DL76L060832Seal · failedCTR HYD SYSTEM QTY DECEASING .41RF CTR HYD QTY MSG. FOUND FILTER MODULE IN WHEEL WELL LEAKING. REPLACED DPI O-RING LEAK CK OK. OVERWEIGHT LANDNG INSP AND PDC DONE.SDR DL76L060828Projector · overheatedDURING TURN AROUND VIDEO PROJECTOR AT 24CDE CAUSING SMOKE. REPLACED PROJECT AT SEAT 24CDE, OPS CKS NORMAL MCO AND PLAC REMOVED.SDR HALA0600818Intercostal · crackedINTERCOSTAL AT BS 287-303 RBL 37 CRACKED AT LOWER FASTENER ROW ON WEB AND ANGLE. REMOVED INTERCOSTAL WEB AND ANGLE. FABRICATED NEW INTERCOSTAL AND WEB. REPAIR PARTS AND INSTALLED IAW SRM 51-40-02, SRM 51-40-05, AND 51-70-13/101 FIG 1.SDR DL76G060823Oxygen Mask · unwanted deployDURING TAXI, MASKS AT SEAT 19AB DROPPED. OXY MASKS AT SEAT 19AB RESTOWED OK. ETOPS CATEGORY (F): ANY OTHER EVENT DETRIMENTAL TO ETOPS.SDR HALA0600817Channel · damagedDURING REMOVAL OF RT HORIZONTAL STAB OB TE WEDGE, FOUND U-COMMON TO WEDGE AND STAB WITH LIGHTING STRIKE DAMAGE. REMOVED AND REPLACED RT HORIZONTAL STAB OB T/E WEDGE U-CHANNEL IAW SRM 51-40-02 AND DWG 183T1140.SDR DL76L060812Slide · unwanted deployREFERENCE: NR1492, DURING SLIDE ARMING, RT OVERWING SLIDE SYSTEM INADVERTENTLY ACTUATED. REPLACED RT OVERWING SLIDE AND COMPONENTS IAW OPN 7838AD.SDR DL76P060811Fan · odorEQUIPMENT COOLING OVHT LIGHT ON OVERHEAD PANEL ACCOMPANIED BY BURNING SMELL IN COCKPIT. FOUND EICAS MSG FWD EQUIP SUPPLY FAN 1 PULLED AND COLLARD C/B H-18 FWD TO MCO AND PLAC 21-58-03B FWD SUPPLY FAN MOTOR BURNED UP NEEDS NEW FAN ASSY. REMOVED AND REPLACED FWSDR DL76L060813Frame · crackedA CRACK WAS FOUND ON THE INNER CHORD OF THE STA 500 LOWER FRAME SEGMENT IN THE FORWARD CARGO BAY AT APPROX LBL 60. THE DAMAGED AREA OF CHORD WAS REMOVED AND A REPAIR ANGLE WAS INSTALLED.SDR DL76L060808Brake · smokeNR 3 WHEEL BRAKE ASSY EXCESSIVE SMOKE DURING TAXI FOR FCF. TOWER STOPPED AIRCRAFT AND NOTIFIED FIRE CREW. AIRCRAFT RETUNED TO HANGER SAFE. WHEEL BRAKE PUCK FOUND LEAKING AND CARBON FIBER DISK ASSY DISINTEGRATED. WHEEL ASSY BRAKE REPLACED ON LOG ENTRY AND NSDR DL76L060806Frame · crackedTHE FUSELAGE FRAME, LOWER END HAS A CRACK, STA 903 LT SIDE. THE DAMAGED END OF THE FRAME WAS REMOVED AND A REPAIR ANGLE WAS INSTALLED.SDR DL76L060800Bearing · bindingRUDDER PEDALS BINDING ON PRE FLT CHECK. FOUND BEARING IN RUDDER FEEL/CENTURING UNIT FROZEN. REPLACED SAME AND CHECKED OUT RUDDER FEEL AND CENTERING PER AMM 27-21-10-712-098 RUDDER AND PEDALS OPERATE NORMAL WITH FULL TRAVEL.SDR DL76L060798Computer · malfunctionedCAPTAINS ALTIMETER INOP. REMOVED AND REPLACED L ADC AND CAPT ALTIMETER PERFORMED TEST CHKS OK.SDR DL76S060797Floorbeam · corrodedCABIN FLOORBEAM UPPER CHORD STA 287 CORRODED AT RBL 51 TO RBL 62 AND ALSO EXISTING SPLICE PLATE CORRODED AT RBL 10 TO RBL 15. REPAIRED PER SRM 53-00-51D FIGURE 201, AMM 32-41-00.SDR DL76S060796Floorbeam · crackedCABIN FLOORBEAM AT STA 325 LBL 32 UPPER STRUCTURE BENT AND CRACKED IN RADIUS AS MARKED. REPAIRED PER SRM 53-00-51D FIGURE 201.SDR DL76L060794Fan · odorBURNING RUBBER SMELL AT ROW 30. TURNED OFF UTILITY BUSSES RECIRC FANS CARGO HEAT. SMELL DISSIPATED. INSPECTED AREA ALL AROUND ROW 30. TURNED ON ALL IFE OVENS/COFFEE MAKERS/RAN APU AND PACKS. RAN ENGS AND PACKS. INSPECTED GASPER FAN AREA AND RECIRC FANS. SDR DL76S060793Fitting · fatiguedDURING REWORK OF THE FORWARD UPPER SPAR FITTING PER SIP EO, CRACKING INDICATIONS WERE FOUND AT AFT OUTBOARD FASTENER LOCATIONS COMMON TO MIDSTRUT BULKHEAD FITTING ON EACH PYLON. HOLES WERE OVERSIZED AND BUSHED BACK TO DIAMETER.SDR DL76S060792Fitting · fatiguedCRACK INDICATIONS WERE FOUND AT THE FORWARD OUTBOARD BOLT HOLE LOCATION OF THE AFT PITCH LOAD FITTING, NR 1 PYLON. CRACK IS IN LOWER WING SKIN ALSO, AND REQUIRED SUBJECT HOLE TO BE OVERSIZED AND BUSHED BACK TO DIAMETER.SDR DL76S060791Frame · crackedFUSELAGE STATION 903.5 FRAME INNER CHORD FOUND CRACKED. ON BOTH LT AND RT AT TRANSITION BETWEEN CHORD FLANGES. AREA TRIMMED AND REPAIR INSTALLED.SDR DL76S060790Rib · corrodedRT WING RIB NR 8, LOWER OUTBOARD HOLE WAS FOUND WITH CORROSION PITTING. DAMAGE WAS REMOVED BY OVERSIZED HOLE, BUSHING INSTALLATION.
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