Boeing 767-306

Service difficulty reports · 2,510

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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 = '767306'
  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 UIEA2017041700601Adapter · wornNR 1 ENGINE, LT CORE COWL HOLD OPEN ROD STOW BRACKET AND ADAPTER FOUND WORN. THE BRACKET AND ADAPTER WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon Miscellaneous StructureSDR UIEA2017042000616Plate · wornNR 1 ENGINE, RT CORE COWL RELIEF DOOR FOUND TWO STRIKER PLATES WORN. THE STRIKER PLATES WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Main FrameSDR UIEA2017042000617Rivet · looseNR 1 ENGINE, LT CORE COWL EXTERIOR UPPER FWD AREA FOUND RIVET LOOSE. THE RIVETS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Main FrameSDR UIEA2017042000618Rub Strip · wornNR 1 ENGINE, LT CORE COWL INTERIOR AFT UPPER RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon Miscellaneous StructureSDR UIEA2017042000619Rub Strip · wornNR 2 ENGINE, LT CORE COWL UPPER AFT RUBSTRIP FOUND WORN. THE RUBSTRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon Miscellaneous StructureSDR UIEA2017042000620Plate · wornNR 2 ENGINE, RT CORE COWL PRESSURE RELIEF DOOR FOUND TWO STRIKER PLATES WORN. THE STRIKER PLATES WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Main FrameSDR UIEA2017042400628Seal · wornNR 1 ENGINE, LT CORE COWL FLIPPER DOOR SEAL FOUND WORN. THE DOOR SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Main FrameSDR UIEA2017042400629Angle · crackedNR 1 ENGINE, LT CORE COWL INTERIOR AFT UPPER AREA ANGLE FOUND CRACKED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Main FrameSDR UIEA2017042400630Bracket · wornNR 2 ENGINE, LT CORE COWL HOLD OPEN ROD STOW BRACKET AND ADPATER FOUND WORN. THE BRACKETS AND ADAPTER WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon Miscellaneous StructureSDR UIEA2017042400631Seal · wornNR 1 ENGINE, LT CORE COWL FWD UPPER SEAL FOUND WORN. SEAL REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Main FrameSDR UIEA2017042400632Rub Strip · looseNR 2 ENGINE RT CORE COWL UPPER AFT AREA FOUND RUB STRIP WITH LOOSE RIVET. THE RUB STRIP RIVETS REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Main FrameSDR UIEA2017042400633Duct · looseNR 2 ENGINE RT CORE COWL PRECOOLER EXIT DUCT FOUND RIVET LOOSE. DUCT RIVET REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Pneumatic Distribution SystemSDR UIEA2017042400634Support · looseNR 2 ENGINE RT CORE COWL UPPER SUPPORT PLATE FOUND RIVET LOOSE. SUPPORT PLATE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon StructureSDR UIEA2017050900733Skin · scratchedNR 1 ENGINE LT CORE COWL EXTERIOR SKIN FOUND SCRATCHED. SCRATCHES BLENDED OUT AND FOUND WITHIN LIMIT IAW SRM 54-42-01-1A-1, FIG 101, NOTE B, DETAIL III, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Plate/SkinSDR UIEA2017042800670Plate · wornNR 2 ENGINE LT CORE COWL INTERIOR AREA 5TH AND 6TH SUPPORT FRAME, SUPPORT PLATE FOUND WORN. THE SUPPORT PLATE WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Main FrameSDR UIEA2017042800671Intercostal · corrodedBS 933, STRINGER 18L FOUND INTERCOSTAL CORRODED. CORROSION BLENDED OUT AND FOUND OUT OF LIMITS IAW SRM 53-00-04-1A-1, FIG 101, ALLOWABLE DAMAGE 1, REV 104. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Fuselage Miscellaneous StructureSDR UIEA2017050200683Frame · corrodedBS 1329 FRAME FOUND CORRODED BETWEEN STRINGER 19 - 20R, RBL 90, WL 205. BLENDED OUT AND FOUND OUT OF LIMITS IAW SRM 53-00-07-1A-1, FIG 101, ALLOWABLE DAMAGE 1, REV 104. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Fuselage Main, FrameSDR UIEA2017050200690Frame · chafedNR 1 ENGINE RT CORE COWL LOWER AFT HAT FRAME FOUND CHAFED. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Main FrameSDR UIEA2017050800730Bracket · wornNR 1 ENGINE LT CORE COWL FWD UPPER BRACKET FOUND WORN. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Main FrameSDR UIEA2017051700807Torque Tube · wornLEFT WING INBD FLAP TORQUE TUBE AT BETWEEN IFS 92 - 124.5, FOUND TO HAVE LIGHT WEAR. REWORK CARRIED OUT IAW SB 767-57A0066, FIG 9, REV 4 IAW EO 6757A038, REV 3.Jun 7, 2017 · N1321A · Boeing 767306 · Trailing Edge Flap Control SystemSDR UIEA2017050900735Rod End · looseNR 2 ENGINE LT CORE COWL HOLD OPEN ROD , ROD END FOUND LOOSE. THE ROD END WAS REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Main FrameSDR UIEA2017050900736Bracket · wornNR 2 ENGINE RT CORE COWL HOLD OPEN ROD, BRACKET FOUND WORN. THE BRACKET WAS REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon Miscellaneous StructureSDR UIEA2017050900737Rod End · looseNR 1 ENGINE LT CORE COWL HOLD OPEN ROD, ROD END FOUND LOOSE. THE ROD END WAS REMOVED AND REPLACED IAW SRM 70-50-00, REV 120.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Main FrameSDR UIEA2017050900738Rod End · wornNR 1 ENGINE RT CORE COWL HOLD OPEN ROD, ROD END FOUND WORN. THE ROD END WAS REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Main FrameSDR UIEA2017051100769Rub Strip · crackedNR 2 ENGINE LT CORE COWL UPPER AFT RUB STRIP FOUND CRACKED. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Main FrameSDR UIEA2017051100770Rub Strip · wornNR 1 ENGINE L/H CORE COWL EXTERIOR FWD RUB STRIP FOUND WORN. THE RUB STRIPS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Main FrameSDR UIEA2017051100771Rub Strip · wornNR 2 ENGINE L/H CORE COWL EXTERIOR AREA RUB STRIP FOUND WORN. THE RUB STRIPS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Main FrameSDR UIEA2017051100772Rub Strip · wornNR 1 ENGINE RT CORE COWL EXTERIOR AREA RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Main FrameSDR UIEA2017051100774Frame · wornNR 1 ENGINE LT CORE COWL AFT HAT FRAME FOUND EXISTING REPAIRS WORN. THE HAT FRAME REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Frame/Spar/RibSDR UIEA2017051600795Frame · deformedAFT CARGO BAY, BS 1197+22, BL 0 - RBL 11 FRAME FOUND DEFORMED. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Fuselage Main, FrameSDR UIEA2017051700806Door Frame · wornBULK CARGO DOOR INTERNAL FRAME LOWER, MID SECTION FOUND WORN. A NEW LOWER FRAME WAS FABRICATED IAW DRAWING 146T6322, SHEET 1, REV A, THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Cargo/Baggage DoorsSDR UIEA2017060500923Warning Message · illuminatedAFTER ENGINE START, SWITCH SELECTED TO GROUND LT & RT UTILITY BUSS AND LT HYD SYSTEM PRESSURE EICAS MESSAGE. PERFORMED NR 2 ENGINE IDLE START PROCEDURES AND RUNS IAW AMM 72-00-00 OPS CHECKED GOOD, NO DEFECTS NOTED. REMOVED AND REPLACED C904 & BTB AS PRECAUTJun 4, 2017 · N1229A · Boeing 767306 · Hydraulic System, MainSDR P5CA2017060500154Relay · failedFWD CARGO BACKUP, EICAS MESSAGE DISPLAYED DURING DEPARTURE. QRH PROCEEDURE COMPLETED AND MESSAGE EXTINGUISHED. REMOVED AND REPLACED THE RELAY K1222 IN P37 MISC PANEL IAW FIM 21-61 FAULT TREE 812 & AMM 21-61-81, SYS OP CHECKED OK.Jun 1, 2017 · N647GT · Boeing 767306 · Cabin Temperature Control SystemSDR P5CA2017053000146Relay · misinstalledFWD EQUIPMENT VALVE EICAS MESSAGE AND VALVE LIGHT DISPLAYED AFTER START, WITH VALVE SWITCH IN THE STANDBY POSITION. PERFORMED TROUBLESHOOTING IAW FIM 21-58 FT 899. FOUND RELAY K1005 INSTALLED INCORRECTLY. SYSTEM TESTED OK.May 29, 2017 · N647GT · Boeing 767306 · Cabin Cooling SystemSDR UIEA2017070801133O-Ring · failedAPU LEAKING OIL FROM OIL FILL CAP. REMOVED AND REPLACE OIL FILLER CAP O-RING IAW AMM 79-11-03. NO OTHER LEAKS FOUND.May 28, 2017 · N1321A · Boeing 767306 · APU Oil SystemSDR P5CA2017053100149Button · inoperativeGCS BUTTON ON WX RADAR PANEL IS INOPERATIVE. RT SYSTEM TESTED OK IAW AMM 34-43-00.May 26, 2017 · N647GT · Boeing 767306 · Weather Radar SystemSDR P5CA2017053000148Fire Loop · out of positionLEFT ENGINE FIRE LOOP 2 STATUS MESSAGE. POSITIONED THE LEFT ENGINE FIRE LOOP 2 AND CLEANED ALL TERMINAL CONNECTORS. SYSTEM CHECKED OK IAW 26-11-00.May 25, 2017 · N647GT · Boeing 767306 · Smoke DetectionSDR P5CA2017050400103Cover · missingDURING INSPECTION FOUND COCKPIT WINDOWS NR 1 AND 2 HEATER TERMINAL LUG COVER MISSING. THE COVER WAS REPLACED IAW SWPM 20-61-11, REV 64.May 10, 2017 · N647GT · Boeing 767306 · Ice/Rain Protection System WiringSDR P5CA2017050400107Connector · crackedHMG SHUTOFF VALVE CONNECTOR FOUND CRACKED. THE CONNECTOR WAS REPLACED IAW SWPM 20-61-11, REV 64, WDM 24-25-11 AND 24-25-13, REV 11.May 10, 2017 · N647GT · Boeing 767306 · Landing Gear System WiringSDR P5CA2017050500109Pin · wornRT ENGINE OTBD FAN COWL FORWARD AND AFT HOLD OPEN ROD STOWAGE PIN FOUND WORN. THE PIN WAS REPLACED IAW AMM 70-50-00, REV 120A.May 10, 2017 · N647GT · Boeing 767306 · Nacelle/Pylon Miscellaneous StructureSDR P5CA2017050500108Skin · wornNR 1 NACELLE LT CORE COWL INTERIOR AFT UPPER SKIN FOUND WORN. REPAIRED IAW SRM 51-40-02, REV 104.May 10, 2017 · N647GT · Boeing 767306 · Nacelle/Pylon, Plate/SkinSDR P5CA2017050500110Pin · wornRIGHT ENGINE INBD CORE COWL HOLD OPEN ROD STOWAGE PIN FOUND WORN. REPLACED THE IAW AMM 70-50-00, REV 120A.May 10, 2017 · N647GT · Boeing 767306 · Nacelle/Pylon Miscellaneous StructureSDR P5CA2017050500111Heat Exchanger · leakingRIGHT ENGINE IDG AIR/OIL HEAT EXCHANGER FOUND LEAKING. AIR/OIL HEAT EXCHANGER REPLACED IAW AMM 24-11-04, REV 120A.May 10, 2017 · N647GT · Boeing 767306 · Turbine Engine Oil SystemSDR P5CA2017050600114Skin · erodedNR 1 ENG NOSE COWL EXTERIOR SKIN AFT OF NOSE COWL LIP FOUND EROSION CIRCUMFERENTIALLY. NR 1 NOSE COWL EXTERIOR SKIN AFT OF NOSE COWL LIP REPAIRED IAW SRM 54-12-01-2R-11 REPAIR 11, REV 104, AND PAINTED IAW AMM 51-21-10, REV 120.May 10, 2017 · N647GT · Boeing 767306 · Nacelle/Pylon, Plate/SkinSDR P5CA2017050700116Pin · missingNR 1 ENGINE LH FAN COWL FWD HINGE PIN MISSING. THE HINGE PIN WAS INSTALLED IAW AMM 71-11-04, REV 120A.May 10, 2017 · N647GT · Boeing 767306 · Nacelle/Pylon, Main FrameSDR P5CA2017050700117Spinner · damagedNR 1 ENGINE SPINNER PAINT FLAKED OFF. PAINTED IAW AMM 72-31-01, REV 120.May 10, 2017 · N647GT · Boeing 767306 · Turbine Engine Air Inlet SectionSDR P5CA2017050700118Skin · dentedRIGHT NACELLE O/B CORE COWL BELOW PRECOOLER EXHAUST, FOUND A DENT. FOUND WITHIN LIMITS IAW SRM 54-42-01-1A-1, FIG.101, REV 104.May 10, 2017 · N647GT · Boeing 767306 · Nacelle/Pylon, Plate/SkinSDR P5CA2017050800119Actuator · corrodedDURING A TE FLAP ROTARY ACTUATOR AND REACTION RING INSPECTION, FOUND CORROSION ON THE NR 2 TE FLAP ROTARY ACTUATOR. THE ACTUATOR WAS REMOVED AND REPLACED IAW EO 6727A007.May 10, 2017 · N647GT · Boeing 767306 · Trailing Edge Flap ActuatorSDR P5CA2017050800120Actuator · corrodedDURING A TE FLAP ROTARY ACTUATOR AND REACTION RING INSPECTION, FOUND CORROSION ON THE NR 3 TE FLAP ROTARY ACTUATOR. THE ACTUATOR WAS REMOVED AND REPLACED IAW EO 6727A007.May 10, 2017 · N647GT · Boeing 767306 · Trailing Edge Flap ActuatorSDR P5CA2017050800121Actuator · corrodedDURING A TE FLAP ROTARY ACTUATOR AND REACTION RING INSPECTION, FOUND CORROSION ON THE NR 4 TE FLAP ROTARY ACTUATOR. THE ACTUATOR WAS REMOVED AND REPLACED IAW EO 6727A007.May 10, 2017 · N647GT · Boeing 767306 · Trailing Edge Flap Actuator
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