Boeing 767-281

Service difficulty reports · 1,831

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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 = '767281'
  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 UIEA2017022000220Attach Bracket · corrodedMAIN DECK CARGO BS 1257 TO 1277 LBL 48 TO 72. FOUR EACH BAT WING CARGO LOCKS ATTACH BRACKETS CORRODED. CLEANED & EVALUATED IAW SRM 51-10-02. FOUND TO BE IN LIMITS IAW CMM 25-50-94.Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Main, Attach FittingsSDR UIEA2017022000219Fitting · corrodedMAIN DECK CARGO BAY BS 1237 - 1217, LBL 48 TO 72. FITTING LOCATED UNDER REMOVED BATWINGS CORRODED. CLEANED & EVALUATED IAW SRM 51-10-02. FOUND IN LIMITS IAW CMM 25-50-94. TREATED & PRIMED IAW SRM 51-20-01-OG-0.Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Miscellaneous StructureSDR UIEA2017022000218Inlet · corrodedNR 2 ENGINE INLET LOWER TWO BOLT HOLES HAVE CORROSION. FREEZE PLUGS FABRICATED AND INSTALLED IAW SRM 51-20-07, PARA B, FIG 5 & FIG C, AND PARA 3B AND RDR PMO-TLS-17-007-14B.Mar 1, 2017 · N656GT · Boeing 767281 · Turbine Engine Air Inlet SectionSDR UIEA2017022000217Support Channel · corrodedRT WINE TE PANEL SUPPORT CHANNEL AT PANEL 661PB HAS CORROSION BETWEEN NUT PLATE HOLES. REMOVED AND REPLACED THE SUPPORT CHANNEL IAW SRM 51-40-05 & DWG 113T1912, SHEET 1, REV D.Mar 1, 2017 · N656GT · Boeing 767281 · Wing Main, Frame StructureSDR ABXA20170225012Escape Rope · defectiveWHILE THE AIRPLANE WAS REMOVED FROM SERVICE, TWO DESCENT DEVICES WERE FOUND PARTIALLY UNWOUND. THE DESCENT DEVICES WERE REPLACED. THE CAUSE FOR THE DESCENT DEVICES BECOMING UNWOUND IS UNKNOWN.Feb 25, 2017 · N795AX · Boeing 767281 · Emergency EquipmentSDR ABXA2017224017Beam · crackedNR 2 HYD BAY OTBD LOWER BEAM IS CRACKED AT FORWARD SIDE OF 1ST DOOR LATCH FITTING. REMOVED AND REPLACED THE NR 2 PYLON DOOR BEAM IAW SRM 51-40-02. AIRCRAFT WAS GROUNDED.Feb 24, 2017 · N769AX · Boeing 767281 · Nacelle/Pylon, Main FrameSDR ABXA2017215016Tee Fitting · corrodedKEEL BEAM INTERCOSTAL HAS CORROSION AT BS 960. REMOVED AND REPLACED INTERCOSTAL TEE IAW SRM 51-40-02. AIRCRAFT WAS GROUNDED.Feb 15, 2017 · N769AX · Boeing 767281 · Fuselage Main, Attach FittingsSDR ABXA20170215015Tee Fitting · corrodedKEEL BEAM INTERCOSTAL HAS CORROSION AT BS 866. REMOVED AND REPLACED INTERCOSTAL TEE IAW SRM 51-40-02. AIRCRAFT WAS GROUNDED.Feb 15, 2017 · N769AX · Boeing 767281 · Fuselage Main, Attach FittingsSDR ABXA2017215014Tee Fitting · corrodedKEEL BEAM INTERCOSTAL HAS MISSING NUT PLATE AND CORROSION. REMOVED AND REPLACED INTERCOSTAL TEE IAW SRM 51-40-02.Feb 15, 2017 · N769AX · Boeing 767281 · Fuselage Main, Attach FittingsSDR UIEA2017021300179Unknown · smokeON SHUTDOWN OF ENGINES SMOKE FILLED THE COCKPIT, APU SHUTOFF ON ITS OWN. PERFORMED CHAPTER 5 INSPECTION IAW AMM 21-00-21-862-051.Feb 13, 2017 · N657GT · Boeing 767281 · Air Distribution SystemSDR ABXA20170130005Failsafe · crackedRIGHT FAILSAFE STRAP BS 955 CRACKED AT LOWER ATTACH HOLE COMMON TO TEE FITTING. CRACKED AREA TRIMED OUT AND REPAIRED IAW SDR. AIRCRAFT WAS GROUNDED.Jan 30, 2017 · N768AX · Boeing 767281 · Fuselage Main, StructureSDR ABXA20170130004Failsafe · crackedLEFT FAILSAFE STRAP BS 955, CRACKED AT LOWER ATTACH HOLE COMMON TO TEE FITTING. REMOVED AND REPLACED THE FAILSAFE STRAP IAW JOB CARD EA 53500013-007 AND INSTALLED A NEW FAILSAFE AIRCRAFT WAS GROUNDED.Jan 30, 2017 · N768AX · Boeing 767281 · Fuselage Main, StructureSDR ABXA20170129003Rheostat · failedAFTER ENGINE START WHEN TURNING OFF THE LEFT OVERRIDE LIGHT SWITCH, THE "MAIN PNL FLOOD LT" CIRCUIT BREAKER TRIPPED OPEN. SMOKE AND AN ELECTRICAL ODOR WERE OBSERVED IN THE FORWARD-RIGHT SIDE OF THE FLIGHT DECK. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED)Jan 29, 2017 · N787AX · Boeing 767281 · Flight Compartment LightingSDR ABXA20170127010Frame · corrodedTWO HOLES IN LEFT HAND SIDE FRAME FITTING (PICKLE FORK) COMMON TO FUSELAGE SKIN SIZE .309" HAVE DEFECT INDICATION FROM HFEC HOLE SCAN. REAMED HOLES UP UNTIL NO FURTHER DEFECTS WERE NOTED REA WAS GIVEN TO REPAIR THE HOLES. HOLES REPAIRED IN ACCORDANCE WITH REA Jan 27, 2017 · N768AX · Boeing 767281 · Fuselage Main, FrameSDR ABXA20170127009Frame · corrodedCORROSION FOUND ON FORWARD LOWER FACE OF LEFT HAND SIDE FRAME FITTING (PICKLE FORK) AROUND SEVEN FASTENER HOLES COMMON TO MATING SURFACE OF REAR SPAR WEB PAD UP AREAS. REMOVED CORROSION SPOT FACED COMMOMON TO BOLT HOLES. NDT CHECKED NO DEFECTS REMAINING ROTO PJan 27, 2017 · N768AX · Boeing 767281 · Fuselage Main, FrameSDR ABXA20170127008Structure · corrodedAFT SPAR WEB HAS CORROSION ON THE PAD UP AREA COMMON TO MULTIPLE HOLES. REMOVED CORROSION, SPOT FACED CORROSION NEAR HOLES NDT CHECKED NO FURTHER DEFECTS NOTED ROTO PEENED BLENDED AND SPOT FACED AREAS REPAIRED BLENDED AND SPOT FACED AREAS IN ACCORDANCE WITH REJan 27, 2017 · N768AX · Boeing 767281 · Fuselage Main, StructureSDR ABXA20170119007Failsafe · crackedLEFT FAILSAFE STRAP AT BS 955 IS CORRODED AND CRACKED PAST TRIM OUT LIMITS. REPLACED THE FAILSAFE.Jan 19, 2017 · N768AX · Boeing 767281 · Fuselage Main, StructureSDR ABXA20170119006Skin · corrodedCORROSION FOUND ON RIGHT FUSELAGE INTERNAL SKIN BS 955 COMMON TO THE TWO LOWER FASTENER HOLES OF TEE FITTING AND FAILSAFE. REMOVED CORROSION, AND REPAIRED THE SKIN IAW REA B 653-62360-MR.Jan 19, 2017 · Boeing 767281 · Fuselage Main, Plate/SkinSDR ABXA20170114002Bolt · missingLEFT ENGINE FLAME OUT (SHUT DOWN) OCCURRED WHILE DESCENDING THROUGH APPROXIMATELY 10,000 FEET. THE QUICK REFERENCE HANDBOOK’S ENGINE FAILURE AND ENGINE IN FLIGHT START CHECK LIST WAS COMPLETED. THE ENGINE RESTART WAS SUCCESSFUL. THE AIRPLANE WAS REMOVED FROMJan 14, 2017 · N775AX · Boeing 767281 · Fuel HeaterSDR UIEA2016122701054Battery Pack · inoperativeEMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACKS IAW AMM 33-51-07. OPS GOOD.Dec 25, 2016 · N658GT · Boeing 767281 · Emergency LightingSDR UIEA2016092200767Module · faultyREJECTED T/O DUE TO T/O WARNING HORN. STATUS MESSAGE FLAP/SLAT ELECTRONIC LESS THAN 20KTS ACHIEVED. FOUND C FSPM FAULTING R & R C FSPM MODULE M839 IAW AMM 27-58-01. OPS CKS OK.Sep 22, 2016 · N657GT · Boeing 767281 · Trailing Edge Flap Control SystemSDR UIEA2016092000763Engine · power lossRTO ON TAKEOFF RT ENGINE DID NOT PRODUCE TAKEOFF THRUST, RTO BELOW 80 KNOTS. COMPLIED WITH GROUND TEST NR 4 VERIFIED BOTH ENGINE MAKE T/O POWER 108.6 NO THROTTLE SPLIT ELECTRONIC ENGINE CONTROL OFF REF AMM 71-00-00. TRANSFERED TO MDDR 70393 IAW MEL 73-21-01Sep 20, 2016 · N656GT · Boeing 767281 · Engine (Turbine/Turboprop)SDR ABXA20160916146Escape Reel · unwanted deployWHILE PERFORMING INSPECTION OF THE DESCENT DEVICES, TWO DESCENT DEVICES FELL TO THE FLOOR, BREAKING THE SEALS. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) UNTIL THE DESCENT DEVICES WERE REWOUND, RESEALED, AND RESTOWED. THE CAUSE FOR THE DESCENT DEVICES FASep 16, 2016 · N775AX · Boeing 767281 · Emergency EquipmentSDR ABXA20160913144Striker · inoperativeTHE FLIGHT DECK DOOR WILL NOT RELEASE ELECTRICALLY DURING THE CREW'S PREFLIGHT INSPECTION. THE DOOR CIRCUIT BREAKER OPENS. THE AIRPLANE WAS REMOVED FROM SERVICE, GROUNDED, UNTIL THE DOOR'S SECURITY SYSTEM WAS DEFERRED. 3 DAYS LATER, THE AIRPLANE WAS REMOVEDSep 13, 2016 · N798AX · Boeing 767281 · Passenger/Crew DoorsSDR ABXA20160830140Battery Pack · dischargedEMERGENCY LIGHT SPARE BATTERY PACK M737 IS INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK M737 WAS REPLACED. THE CAUSE OF THE INOPERATIVE BATTERY PACK WAS A DISCHARGED BATTERY.Aug 30, 2016 · N769AX · Boeing 767281 · Emergency LightingSDR ABXA20160830139Socket · inoperativeEXTERIOR EMERGENCY LIGHTING SYSTEM INOPERATIVE. THE LAMP WAS REPLACED IN THE EMERGENCY LIGHT LAMPHOLDER ASSEMBLY. THE CAUSE OF THE INOPERATIVE LIGHT WAS A FAILED LAMP.Aug 30, 2016 · N795AX · Boeing 767281 · Emergency LightingSDR ABXA20160830138Battery Pack · dischargedINTERIOR EMERGENCY LIGHTING SYSTEM INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK WAS REPLACED. THE CAUSE OF THE INOPERATIVE LIGHTS WAS A DISCHARGED BATTERY.Aug 30, 2016 · N795AX · Boeing 767281 · Emergency LightingSDR ABXA20160829137Battery Pack · dischargedCREW SERVICE AREA INTERIOR LIGHTS ARE INOPERATIVE WHEN IN EMERGENCY LIGHTS MODE. THE EMERGENCY LIGHT BATTERY PACK M736 WAS REPLACED. THE CAUSE OF THE INOPERATIVE LIGHTS WAS A DISCHARGED BATTERY.Aug 29, 2016 · N769AX · Boeing 767281 · Emergency LightingSDR ABXA20160812141Escape Rope · inoperativeONE DESCENT DEVICE WAS FOUND NOT PROPERLY STOWED AND INOPERATIVE DURING THE FLIGHT CREW’S PRE-FLIGHT INSPECTION. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) UNTIL THE DESCENT DEVICE WAS DEFERRED. THE NEXT DAY, THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDAug 12, 2016 · N775AX · Boeing 767281 · Emergency EquipmentSDR ABXA20160811132Wire · damagedTHE HORIZONTAL STABILIZER TRIM FAILED TO OPERATE USING CONTROL WHEEL SWITCHES. MANUAL CONTROL WAS NORMAL. AILERON LOCKOUT AND RUDDER RATIO EICAS MESSAGE DISPLAYED. AUTOPILOT DISENGAGED AND WOULD NOT RE-ENGAGE. ACCOMPLISHED WAS REPAIRING SHORTED WIRING IN TAug 11, 2016 · N783AX · Boeing 767281 · Flight Control System WiringSDR ABXA20160803114Lock · failedFLIGHT DECK DOOR LOCK CIRCUIT BREAKER TRIPPED. THERE WAS A BURNING ODOR IN THE VICINITY OF THE FLIGHT DECK DOOR. THE FLIGHT DECK DOOR LOCK WAS REPLACED. THE CAUSE OF THE ODOR WAS NOT FOUND.Aug 3, 2016 · N798AX · Boeing 767281 · Fixed Inner DoorsSDR ABXA20160730126Bulkhead · corrodedFOUND UNACCOUNTED OIL CAN REPAIR NEAR THE OUTER EDGE STIFFENER. REMOVED UNACCOUNTED REPAIR STIFFENER IAW SRM 51-40-02, FABRICATED NEW STIFFENER IAW SRM 53-80-08, REPAIR 8, STEP 3, LOCATED IAW SRM 53-80-08. TREATED IAW SRM 51-20-01 AND INSTALLED IAW SRM 51-40Jul 30, 2016 · N768AX · Boeing 767281 · Fuselage Main, BulkheadSDR ABXA20160730125Channel · crackedAFT FUSELAGE COMPARTMENT. REMOVED REPAIR CHANNEL IAW SRM 51-40-02. FABRICATED NEW REPAIR CHANNEL IAW SRM 53-80-08, REPAIR 3, PG 203, LOCATED CHANNEL IAW SRM 53-80-08. TREATED CHANNEL IAW SRM 51-20-01 AND INSTALLED IAW SRM 51-40-02 AND 53-80-08. REF REO G20Jul 30, 2016 · N768AX · Boeing 767281 · Fuselage Miscellaneous StructureSDR ABXA20160728119Keelbeam · corrodedCORROSION AT BS 990 - 1010 LEFT SIDE OF KEEL BEAM ALONG THE UPPER SIDE. FOUND TO BE OUT OF LIMITS IAW SRM 53-50-12. REPAIRED IAW SRM 53-50-12 REPAIR 1, REO-G20121 REV. A, AND REA B653-62037MR.Jul 28, 2016 · N768AX · Boeing 767281 · Fuselage Main, KeelSDR ABXA20160727123Bracket · crackedAFT CARGO STA 1087 UNDER STR 38L JUST AFT OF FORWARD BULKHEAD HAS EVALUATED BLEND ON STR 38L IN AFT CARGO STA 1087 AFT OF FORWARD BULKHEAD, ORIGINAL MATERIAL THICKNESS .125", REMOVED .048", REMAINING THICKNESS .077". FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15Jul 27, 2016 · N768AX · Boeing 767281 · Fuselage Miscellaneous StructureSDR ABXA20160720124Beam · corrodedFORWARD CARGO DOOR LOWER SILL BEAM UPPER SURFACE CORRODED AT AFT REPAIRED FORWARD CARGO DOOR LOWER SILL BEAM UPPER SURFACE, HIGH FREQUENCY, NO CRACKS NOTED. INSTALLED NEW FASTENERS IAW SRM 51-40-02. INNER CHORD, PART LOCATION: FLC STA 624-628 AT RBL44, PN: 1Jul 20, 2016 · N768AX · Boeing 767281 · Fuselage Main, StructureSDR ABXA20170720121Skin · crackedCRACK INDICATION FOUND L-1 DOOR CUTOUT LOWER FORWARD CORNER. REPAIRED FUSELAGE SKIN STA 287 TO STA 347, S18L TO S24L BELOW L-1 DOOR IAW REO-G20052, REV B AND NR-B653-62038MR. SDR INFO: PART NAME: FUSELAGE SKIN, PN: 141T3331-5, SN: NSN, STA 287-347, LT BELOWJul 20, 2016 · N768AX · Boeing 767281 · Fuselage Main, Plate/SkinSDR ABXA20160720121Seat Track · corrodedMAIN CABIN, SEAT TRACK, STA 440-STA 660, LBL11 HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION .090" MATERIAL LOSS, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101. REMOVED CORRODED SEAT TRACK, STA 440-660, LBL11 IAW SRM 51-40-02. FABRICATED SEAT TRACJul 20, 2016 · N768AX · Boeing 767281 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA20160720120Seat Track · corrodedMAIN CABIN SEAT TRACK, BS 530 - 660 LBL 54.75 HAS CORROSION. REMOVED CORROSION, AND FOUND TO BE OUT OF LIMIT IAW SRM 53-00-52 FIGURE 101. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 5140-02 DWG 368-53-13-909-08 REV A, AND DWG 368-53-13-90899.Jul 20, 2016 · N768AX · Boeing 767281 · Fuselage, Seat/Cargo Attach FittingsSDR IXXA20160725042Battery Pack · inoperativeDURING DAILY CHECK, FOUND ALL EMERGENCY LIGHTS INOPERATIVE. AIRCRAFT GROUNDED. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK M736. OPS SATISFACTORY IAW AMM 33-51-00. ACFT RELEASED TO SERVICE.Jul 20, 2016 · N791AX · Boeing 767281 · Emergency LightingSDR IXXA20160725041Battery Pack · inoperativeDURING DAILY CHECK FOUND ALL EMERGENCY LIGHTS INTERIOR AND EXTERIOR INOPERATIVE. AIRCRAFT GROUNDED. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK IN POSITION M735. OPERATIONAL CHECK IAW 757 AMM 33-51-00 SATISFACTORY. ACFT RELEASED TO SERVICE.Jul 20, 2016 · N791AX · Boeing 767281 · Emergency LightingSDR ABXA20160713118Keelbeam · corrodedLEFT MAIN WHEEL WELL KEEL BEAM BETWEEN BS 955 - 977. REMOVED CORROSION IAW SRM 51-10-02 AND FOUND TO BE WITHIN LIMITS IAW REO G20083 REVA.Jul 13, 2016 · N768AX · Boeing 767281 · Fuselage Main, KeelSDR ABXA20160706109Stringer · crackedSTRINGER 22L CRACKED 6 INCHES, REPAIRED THE STRINGER IAW SRM 53-00-03 REPAIR 2. AIRCRAFT WAS GROUNDED.Jul 6, 2016 · N787AX · Boeing 767281 · Fuselage Main, Longeron/StringerSDR ABXA20160705111Seat Track · crackedCRACK INDICATION DETECTED AT FASTENER HOLE NR 8 ON THE LEFT HAND STUB BEAM AT BS 883.5, LBL89. REMOVED FASTENERS FROM SEAT TRACK FOR ACCESS REAMED NR 8 HOLE UP UNTIL CLEAN AND ROUND. REPAIRED NR 8 HOLE IN CONJUNCTION WITH IAW REA B653-62098, B653-62101-MR AND Jul 5, 2016 · N787AX · Boeing 767281 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA20160701113Frame · crackedUPPER HALF BS 883.5 LBL89 LOWER SIDE FRAME INNER CHORD CRACKED IN RADIUS LOWER END. VERIFIED BY EDDY CURRENT. REMOVED FASTENERS FOR REPAIR AND FOR ACCESS COMPLIED WITH JOB CARD 53D00049-101 AND REA B653-62101-MR. TRACK TO BE INSTALLED ON NR 0338. SDR: CRACKED Jul 1, 2016 · N787AX · Boeing 767281 · Fuselage Main, FrameSDR UIEA2016070100557Tire · blownFOUND NR 2 TIRE BLOWN ON WALKAROUND. R & R NR 2 MLG TIRE IAW AMM 32-45-01, NR 1 TIRE REPLACED DUE TO NR 2 FAILURE IAW 32-45-01. PERFORMED BRAKE SEIZURE CONDITIONAL INSPECTION IAW AMM 05-51-15, FOUND NR 1 AND NR 2 BRAKE LINE CROSSED CORRECTED BRAKE LINES PERFJul 1, 2016 · N658GT · Boeing 767281 · TireSDR ABXA20160629110Stringer · crackedSTRINGER SPLICE 24L CRACKED BS 676. REMOVED AND REPAIRED THE STRINGER SPLICE BS 676 - 698 IAW SRM 53-00-03 REPAIR 2 DETAIL 3. AIRCRAFT WAS GROUNDED.Jun 29, 2016 · N787AX · Boeing 767281 · Fuselage Main, Longeron/StringerSDR ABXA20160628107Keelbeam · corrodedCORROSION ON KEEL PANEL EXTENSION STA 793 TO 808 LBL. REMOVED CORRODED AREA OF KEEL. NDT CHECKED SURFACE AND HOLES FOUND TO BE DEFECTIVE. COMPLIED WITH ENGINEERING REPAIR IAW SRM 51-40-02 AND REA NR B653-62113-MR. CORRODED: LEVEL 2, PN 145T8611-1, KEEL, FS/Jun 28, 2016 · N787AX · Boeing 767281 · Fuselage Main, KeelSDR ABXA20160628106Unknown · odorBOTH CREW MEMBERS SMELLED A STRONG ELECTRICAL ODOR. THE MAIN EQUIPMENT CENTER WAS INSPECTED. THERE WAS NO EVIDENCE OF BURNED WIRES OR EQUIPMENT. THE CAUSE OF THE ODOR WAS NOT FOUND.Jun 28, 2016 · N797AX · Boeing 767281 · Air Distribution SystemSDR UIEA2016062800534Door Frame · corrodedMAIN DECK OVERWING EXIT AFT FRAME OF CUTOUT DOOR, STA 885.5 JUST ABOVE LOWER DOORSILL FRAME FAILSAFE CHORD IS CORRODED. REMOVED CORROSION IAW SRM 51-10-02, FOUND AREA TO BE OUT OF LIMITS IAW SRM 53-00-15. FABRICATED REPAIR STRAP OUT OF 7075-TG .063 AND INSTAJun 25, 2016 · N658GT · Boeing 767281 · Fuselage Main, Structure
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