Boeing 767-306

Service difficulty reports · 2,510

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 = '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 P5CA2017060900159Warning Message · false activationDURING PRE FLIGHT CHECK BY MAINT, FOUND THE LT ENGINE FIRE LOOP 2 MESSAGE. OPS CHECKED NORMAL IAW AMM 26-00-00.Jun 9, 2017 · N647GT · Boeing 767306 · Fire DetectionSDR P5CA2017060700156Circuit Card · not seatedEICAS MESSAGE DURING OFF, LOADING RT ENGINE SPEED CARD. SEATED THE RIGHT ENGINE SPEED AND PERFORMED N2 CARD TEST, PASSED IAW AMM 73-21-54 & MESSAGE CLEARED.Jun 7, 2017 · N647GT · Boeing 767306 · Engine Fuel Indicating SystemSDR UIEA2017060500939Sensor · erraticLEFT ENGINE N2 INDICATION FOUND ERRATIC ON EICAS DISPLAY DURING ENGINE RUN. THE LT ENGINE N2 SENSOR WAS REMOVED AND REPLACED IAW AMM 77-12-02, REV 121.Jun 7, 2017 · N1321A · Boeing 767306 · Engine BMEP/Torque IndicatingSDR UIEA2017060500942Bracket · crackedAPU DRAINMAST, FOUND HOLDING BRACKET CRACKED AND LINE MISSING. THE BRACKET REPLACED AND DRAIN LINE WERE REPLACED IAW AMM 49-16-00, REV 121. LEAK CHECKED IAW AMM 49-11-00, REV 121. FOUND NO LEAKD FOUND.Jun 7, 2017 · N1321A · Boeing 767306 · APU Engine Fuel and ControlSDR UIEA2017060500940Pressure Switch · malfunctionedLEFT ENGINE FUEL PRESSURE SHOWS 200 PSI ON EICAS DISPLAY DURING ENGINE RUN. THE PRESSURE SWITCH WAS REMOVED AND REPLACED IAW AMM 73-33-01, REV 121. POWER PLANT TEST 2 IDLE LEAK CHECK CARRIED OUT IAW AMM 71-00-00, REV 121.Jun 7, 2017 · N1321A · Boeing 767306 · Engine Fuel Indicating SystemSDR UIEA2017053100891Ring · corrodedCORRODED NR 2 TE FLAP REACTION RING ON THE LT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.Jun 7, 2017 · N1321A · Boeing 767306 · Trailing Edge Flap Control SystemSDR UIEA2017053100892Ring · corrodedCORRODED NR 4 TE FLAP REACTION RING ON THE LT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.Jun 7, 2017 · N1321A · Boeing 767306 · Trailing Edge Flap Control SystemSDR UIEA2017053100893Ring · corrodedCORRODED POSITION NR 5 TE FLAP REACTION RING ON THE RT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.Jun 7, 2017 · N1321A · Boeing 767306 · Trailing Edge Flap Control SystemSDR UIEA2017053100894Ring · corrodedCORRODED POSITION NR 6 TE FLAP REACTION RING ON THE RT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.Jun 7, 2017 · N1321A · Boeing 767306 · Trailing Edge Flap Control SystemSDR UIEA2017053100895Ring · corrodedCORRODED POSITION NR 7 TE FLAP REACTION RING ON RT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.Jun 7, 2017 · N1321A · Boeing 767306 · Trailing Edge Flap Control SystemSDR UIEA2017053100896Rotary Actuator · corrodedCORRODED NR 2 TE FLAP ROTARY ACTUATOR ON LT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.Jun 7, 2017 · N1321A · Boeing 767306 · Trailing Edge Flap ActuatorSDR UIEA2017053100897Actuator · corrodedCORRODED NR 3 TE FLAP ROTARY ACTUATOR ON LT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.Jun 7, 2017 · N1321A · Boeing 767306 · Trailing Edge Flap ActuatorSDR UIEA2017053100898Actuator · corrodedCORRODED POSITION NR 4 TE FLAP ROTARY ACTUATOR ON LEFT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.Jun 7, 2017 · N1321A · Boeing 767306 · Trailing Edge Flap ActuatorSDR UIEA2017053100899Actuator · corrodedCORRODED NR 5 TE FLAP ROTARY ACTUATOR ON RT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.Jun 7, 2017 · N1321A · Boeing 767306 · Trailing Edge Flap ActuatorSDR UIEA2017053100900Actuator · corrodedFLIGHT CONTROLS, TRAILING EDGE FLAP SYSTEM, TE FLAP NR 6 ROTARY ACTUATOR CORRODED. REMOVED AND REPLACED IAW 8017-TALLY 1113, ENGINEERING ORDER 6727A007_CS.Jun 7, 2017 · N1321A · Boeing 767306 · Trailing Edge Flap ActuatorSDR UIEA2017060100901Actuator · malfunctionedFLIGHT CONTROLS, TRAILING EDGE FLAP SYSTEM , TE FLAP ROTARY ACTUATOR AND REACTION RING INSPECTION, REWORKED AND REPLACEED IAW SB 767-27A0229 R1, AND AD 2014-22-09Jun 7, 2017 · N1321A · Boeing 767306 · Trailing Edge Flap ActuatorSDR UIEA2017060200905Structure · corrodedRIGHT OVERWING REFUELING PORT ACCESS CUTOUT FOUND CORRODED. REPAIRED IAW EN 1098-17 REV .Jun 7, 2017 · N1321A · Boeing 767306 · Wing Main, Frame StructureSDR UIEA2017060400907Clamp · leakingRIGHT AIR CONDITIONING BAY AFT ISOLATION BYPASS CHECK VALVE MOUNTING CLAMP FOUND LEAKING. THE CLAMP WAS REMOVED, REPLACED AND LEAK CHECKED IAW AMM 36-11-05, REV 121. FOUND SATISFACTORY.Jun 7, 2017 · N1321A · Boeing 767306 · Air Distribution SystemSDR UIEA2017060400908Clamp · leakingLEFT AIR CONDITIONING BAY LT TRIM AIR CHECK VALVE MOUNTING CLAMP FOUND LEAKING. THE CHECK VALVE MOUNTING CLAMP WAS REMOVED AND REPLACED IAW AMM 21-61-05, REV 121, AND LEAK CHECKED IAW AMM 21-61-05, REV 121. FOUND SATISFACTORY.Jun 7, 2017 · N1321A · Boeing 767306 · Air Distribution SystemSDR UIEA2017060400909Fuel Line · dentedNR 2 PYLON TOP FRONT SPAR FUEL LINE FOUND DENTED. THE FUEL LINE WAS REMOVED AND REPLACED IAW AMM 28-22-07, REV 120, BONDING RESISTANCE TEST CARRIED OUT IAW AMM28-22-07, REV 120. FOUND GOOD, LEAK CHECKED IAW AMM 28-22-07, REV 121. FOUND NO LEAKAGE.Jun 7, 2017 · N1321A · Boeing 767306 · Aircraft Fuel Distribution SystemSDR UIEA2017060400910Check Valve · damagedRIGHT AIR CONDITIONING TRIM AIR SUPPLY CHECK VALVE FOUND FLAPPER LOOSE AND INTERNAL HOUSING WITH CHAFED. THE CHECK VALVE WAS REMOVED, REPLACED AND LEAK CHECKED IAW AMM 21-61-05, REV 121. FOUND SATISFACTORY.Jun 7, 2017 · N1321A · Boeing 767306 · Cabin Temperature Control SystemSDR UIEA2017060400911Bracket · looseNR 1 ENGINE, RT CORE COWL HOLD OPEN ROD BRACKET FOUND LOOSE. THE BRACKET WAS REMOVED AND REPLACED IAW AMM 70-50-00, REV 121.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon Miscellaneous StructureSDR UIEA2017060400912Rod End · wornNR 2 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 Miscellaneous StructureSDR UIEA2017060400913Check Valve · damagedLEFT AIR CONDITIONING TRIM AIR SUPPLY, CHECK VALVE FOUND FLAPPER LOOSE AND INTERNAL HOUSING CHAFED. THE CHECK VALVE WAS REMOVED, REPLACED AND LEAK CHECKED IAW AMM 21-61-05, REV 121. FOUND SATISFACTORY.Jun 7, 2017 · N1321A · Boeing 767306 · Cabin Temperature Control SystemSDR UIEA2017060500916Check Valve · chafedLEFT PNEUMATIC CROSSOVER DUCT ISOLATION BYPASS CHECK VALVE FOUND FLAPPER LOOSE AND INTERNAL HOUSING WITH A CHAFE. THE CROSSOVER DUCT ISOLATION BYPASS CHECK VALVE WAS REMOVED, REPLACED, AND TESTED IAW AMM 36-11-05, REV 121. FOUND SATISFACTORY.Jun 7, 2017 · N1321A · Boeing 767306 · Pneumatic Distribution SystemSDR UIEA2017060500917Filter · trippedAPU LUBE FILTER ASSEMBLY, DIFFERENTIAL PRESSURE INDICATOR FOUND POPPED OUT. REPLACED IAW AMM 49-27-03, REV 121.Jun 7, 2017 · N1321A · Boeing 767306 · APU Oil SystemSDR UIEA2017060500919Sensor · malfunctionedLEFT PACK COMPRESSOR OUTLET TEMP INDICATION INVALID. LT PACK COMPRESSOR OUT TEMP SENSOR REMOVED & REPLACED IAW AMM 21-52-01, REV 121. FOUND SATISFACTORY.Jun 7, 2017 · N1321A · Boeing 767306 · Cabin Cooling SystemSDR UIEA2017060500920Sensor · malfunctionedRIGHT PACK COMPRESSOR OUTLET TEMP INDICATION INVALID. RT PACK COMPRESSOR OUTLET TEMP SENOR REMOVED & REPLACED IAW AMM 21-52-01, REV 121. FOUND SATISFACTORY.Jun 7, 2017 · N1321A · Boeing 767306 · Cabin Cooling SystemSDR UIEA2017060500921Sensor · abnormalLEFT PACK PRIMARY TEMP INDICATION INVALID. LEFT PACK TEMP SENSOR REMOVED & REPLACED IAW AMM 21-52-08, REV 121. FOUND SATISFACTORY.Jun 7, 2017 · N1321A · Boeing 767306 · Cabin Cooling SystemSDR UIEA2017060500922Shutoff Valve · inoperativeFWD CARGO HEAT INOPERATIVE. FWD CARGO HEAT SHUTOFF VALVE REMOVED AND REPLACED IAW AMM 21-43-01, REV 121. OPS TEST PERFORMED IAW AMM 21-43-01, REV 121, FOUND SATISFACTORY.Jun 7, 2017 · N1321A · Boeing 767306 · Heating SystemSDR UIEA2017060500924Strap · corrodedMID CABIN-LOWER STRAPS COMMON TO SATCOM, INTERCOSTAL FOUND CORRODED AT BS 977 TO 1043, STRINGER 1L TO 1R. REMOVED, FABRICATED, AND INSTALLED IAW EO 6753A451.Jun 7, 2017 · N1321A · Boeing 767306 · Fuselage Miscellaneous StructureSDR UIEA2017060500926Exciter · failedAPU FAILED TO START. APU EXCITER REMOVED AND REPLACED IAW AMM 49-41-03, REV 121. APU CONTROL UNIT BITE TEST AND APU STARTING AND OPERATION CARRIED OUT IAW AMM 49-61-05 AND & AMM 49-11-00, REV 121. FOUND SATISFACTORY.Jun 7, 2017 · N1321A · Boeing 767306 · APU Start/Ignition SystemSDR UIEA2017052300844Bracket · wornNR 2 ENGINE RT CORE COWL HOLD OPEN ROD STOW PIN BRACKET AND ADAPTER FOUND WORN AS MARKED. NR 2 ENG RT CORE COWL REMOVED AND REPLACED AS PER AMM 71-11-06, REV 121.Jun 7, 2017 · N1321A · Boeing 767306 · Engine Cowling SystemSDR UIEA2017052300845Support Bracket · wornNR 2 ENGINE RT CORE COWL HOLD OPEN ROD SUPPORT BRACKET AT BASE SIDE FOUND WORN AS MARKED. NR 2 ENG RT CORE COWL REMOVED AND REPLACED AS PER AMM 71-11-06, REV 121.Jun 7, 2017 · N1321A · Boeing 767306 · Engine Cowling SystemSDR UIEA2017052500859Bonding Jumper · frayedAPU AIR INTAKE ACTUATOR FOUND 02EA BONDING FRAYED. ITEM REPLACED IAW AMM 49-15-06 REV 121.Jun 7, 2017 · N1321A · Boeing 767306 · APU Cowling/ContainmentSDR UIEA2017052500860Skin · crackedNR 1 ENGINE RT CORE COWL EXTERIOR AREA PRECOOLER EXIT DUCT CUT-OUT AREA FOUND CRACK AS MARKED. NR 1 ENG RT CORE COWL SKIN PRECOOLER EXIT DUCT ASSY CUT-OUT BELOW NAC STA.281.12 LOWER SECTION CRACK AREA. EXTERNAL PATCH REPAIR CARRIED OUT AS PER SRM 54-42-01-2R-3Jun 7, 2017 · N1321A · Boeing 767306 · Engine Cowling SystemSDR UIEA2017053000876Skin · corrodedLT OVERWING REFUELING PORT ACCESS CUTOUT FOUND CORROSION. LT OVERWING CORROSION AROUND FUEL FILL PORT WAS LOCALLY BLENDED TO CREATE TWO FLAT SURFACE WITH CONSTANT THICKNESS OF 0.210" AND 0.250" TO ALLOW FLAT SEATING OF TWO CUSTOM FILLERS. THE MIN THK WAS 0.207Jun 7, 2017 · N1321A · Boeing 767306 · Wing, Plate/SkinSDR UIEA2017052300836Frame · damagedNR 1 ENGINE LT CORE COWL 2ND ZEE FRAME COUNT FROM FWD FOUND EXISTING REPAIR WORN AS MARKED. NR 1 ENG LT CORE COWL 2ND FROM FWD DAMAGED ZEE FRAME REMOVED AND REPLACED AS PER SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Engine Cowling SystemSDR UIEA2017052300837Cowling · wornNR 2 ENGINE RT CORE COWL PRECOOLER EXIT DUCT LIP FOUND WORN AS MARKED. NR 2 ENG RT CORE COWL REMOVED AND REPLACED AS PER AMM 71-11-06, REV 121.Jun 7, 2017 · N1321A · Boeing 767306 · Engine Cowling SystemSDR UIEA2017052300839Skin · crackedNR 2 ENGINE RT CORE COWL SKIN FOUND CRACK LOCATED AT AFT UPPER CUTOUT AREA AS MARKED. NR 2 ENG RT CORE COWL REMOVED AND REPLACED AS PER AMM 71-11-06, REV 121. REFER TO NRC 0688 FOR CORE COWL REPLACEMENT DETAILS.Jun 7, 2017 · N1321A · Boeing 767306 · Engine Cowling SystemSDR UIEA2017052300841Seal · crackedNR 2 ENGINE RT CORE COWL FLIPPER DOOR FOUND SEAL CRACK AS MARKED. NR 2 ENG RT CORE COWL REMOVED AND REPLACED AS PER AMM 71-11-06, REV 121.Jun 7, 2017 · N1321A · Boeing 767306 · Engine Cowling SystemSDR UIEA2017052300842Strip · wornNR 2 ENGINE RT CORE COWL FWD UPPER EXTERIOR AREA WEAR STRIP FOUND WORN AS MARKED. NR 2 ENG RT CORE COWL REMOVED AND REPLACED AS PER AMM 71-11-06, REV 121.Jun 7, 2017 · N1321A · Boeing 767306 · Engine Cowling SystemSDR UIEA2017051700808Torque Tube · wornRT I/B FLAP, TORQUE TUBE AT IFS 92 - IFS 124.5 FOUND LIGHT WEAR AS MARKED. LIGHT WEAR REWORK CARRIED OUT AS PER SB 767-57A0066, FIG 9, REV 4 IN ACCORDANCE WITH EO 6757A038, REV 3.Jun 7, 2017 · N1321A · Boeing 767306 · Trailing Edge Flap Control SystemSDR UIEA2017051700809Skin · gougedRT INBOARD AFT FLAP UPPER SURFACE TRAILING EDGE. FOUND GOUGE ON UPPER SURFACE AS INDICATED. RT INBOARD AFT FLAP UPPER SURFACE TRAILING EDGE REPAIRED AS PER SRM 51-70-10 REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Trailing Edge FlapsSDR UIEA2017051800814Bellows · deterioratedAPU COOLING DUCT BELLOWS AFT OF COOLING FAN FOUND DETERIORATED. APU COOLING DUCT BELLOWS AFT OF COOLING FAN REMOVED AND REPLACED AS PER AMM 49-51-01, REV 120.Jun 7, 2017 · N1321A · Boeing 767306 · APU Bleed Air SystemSDR UIEA2017051800815Adapter · wornNR 1 ENGINE RT CORE COWL HOLD OPEN ROD STOW ADAPTER FOUND WORN AS MARKED. NR 1 ENGINE RT CORE COWL HOLD OPEN ROD STOW ADAPTER REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.Jun 7, 2017 · N1321A · Boeing 767306 · Engine Cowling SystemSDR UIEA2017041000532Rivet · looseNR 1 ENGINE RT CORE COWL UPPER SUPPORT PLATE FOUND RIVET LOOSE AS MARKED. NR 1 ENG RT CORE COWL UPPER SUPPORT PLATE ATTACH LOOSE RIVET REMOVED AND REPLACED AS PER SRM 51-40-02, REV 103.Jun 7, 2017 · N1321A · Boeing 767306 · Engine Cowling SystemSDR UIEA2017041700598Skin · wornNR 2 ENGINE, LT CORE COWL FAIRING SKIN INTERIOR AREA FOUND WORN LOCATED AT UPPER AFT CUT-OUT. THE FAIRING SKIN WAS REPAIRED IAW SRM 54-45-01-2R-11, REPAIR 11, REV 103.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Plate/SkinSDR UIEA2017041700599Longeron · crackedNR 2 ENGINE, LT CORE COWL UPPER AFT LONGERON FOUND CRACKED. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Frame/Spar/RibSDR UIEA2017041700600Seal · crackedNR 2 ENGINE, LT CORE COWL UPPER AFT SPRING SEAL FOUND CRACKED. THE SPRING SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.Jun 7, 2017 · N1321A · Boeing 767306 · Nacelle/Pylon, Main Frame
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