N616US, cancelled Mar 17, 2014

Service difficulty reports · 45

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N616US' AND deregistration_id = 'N616US-2014-03-17'
  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 NWAA072326716Frame · crackedDURING "L" CHECK, FOUND CRACK IN FRAME AT BS 1800 S11R. REPAIRED PER EA 67-209723.Jun 25, 2007 · N616US · Boeing 747251F · Fuselage Main, FrameSDR NWAA072316716Skin · dentedDURING "L" CHECK, FOUND DENT IN FUSELAGE SKIN AT BS 560 S34R TO S35R. REPAIRED PER EA 67-209722.Jun 25, 2007 · N616US · Boeing 747251F · Fuselage Main, Plate/SkinSDR NWAA072336716Skin · crackedDURING "L" CHECK, FOUND CRACK IN FUSELAGE SKIN BETWEEN BS 320-340 S7L-S9L. REPAIRED PER EA 67-209718.Jun 24, 2007 · N616US · Boeing 747251F · Fuselage Main, Plate/SkinSDR NWAA072346716Skin · crackedDURING "L" CHECK, FOUND CRACK AT FORWARD UPPER CORNER OF UPPER DECK DOOR CUTOUT SKIN AT BS 390 S5R. REPAIRED PER EA 67-209244.Jun 23, 2007 · N616US · Boeing 747251F · Fuselage Main, Plate/SkinSDR NWAA072436716Frame · crackedDURING "L" CHECK, FOUND CRACK IN FUSELAGE FRAME AND DOUBLER AT BS 360 S24L. REPAIRED PER EA 67-209717.Jun 22, 2007 · N616US · Boeing 747251F · Fuselage Main, FrameSDR NWAA071816716Circuit Card · malfunctionedDURING CRUISE, PILOT HAD A MOMENTARY "CARGO FIRE " INDICATION, LIGHTS AND FIRE BELL. FLIGHT CONTINUED ON AND LANDING WAS UNEVENTFUL. MAINTENANCE TESTED BOTH LOWER AND MAIN DECK CARGO FIRE WARNING PER AMM 26-14-00, AND REPLACED A8 FIRE WARNING AND DETECTOR CAMay 11, 2007 · N616US · Boeing 747251F · Fire DetectionSDR NWAA071786716Fire Loop · no testDURING FLIGHT, PILOT HAD A MOMENTARY "FIRE DETECTION" LIGHT ON FORWARD PANEL WITH MOMENTARY AURAL WARNING. ACCOMPLISHED COM PROCEDURE AND FOUND "B" LOOP FAILED TEST. FLIGHT CONTINUED ON AND LANDING WAS UNEVENTFUL. MAINTENANCE INTERCHANGED FIRE DETECTOR CARDMay 10, 2007 · N616US · Boeing 747251F · Fire DetectionSDR 0601186716Frame · crackedDURING L-CHECK AND ACCOMPLISHMENT OF EM 5310-01357-01A FOUND CRACKS IN TENSION TIE FRAME FASTENER HOLES AT BS 860 LT. REPAIRED PER EA 67-206266.May 29, 2006 · N616US · Boeing 747251F · Fuselage Main, FrameSDR 0601156716Frame · crackedDURING L-CHECK AND ACCOMPLISHMENT OF EM 5310-01357-01A FOUND CRACK IN TENSION TIE FRAME FASTENER HOLE AT BS 920 RT. REPAIRED PER EA 67-206256.May 29, 2006 · N616US · Boeing 747251F · Fuselage Main, FrameSDR 0601136716Frame · crackedDURING L-CHECK FOUND CRACK IN FRAME CUTOUT AT BS 880 S9R. REPAIRED PER EA 67-206264.May 29, 2006 · N616US · Boeing 747251F · Fuselage Main, FrameSDR 0601126716Skin · corrodedDURING L-CHECK FOUND CORROSION ON RT WING LOWER SKIN AT WS 1530. REPAIRED PER EA 67-206259.May 27, 2006 · N616US · Boeing 747251F · Wing, Plate/SkinSDR 0601146716Frame · crackedDURING L-CHECK AND ACCOMPLISHMENT OF EM 5310-01357-01A FOUND CRACK IN TENSION TIE FRAME FASTENER HOLE AT BS 940 RT. REPAIRED PER EA 67-206260.May 26, 2006 · N616US · Boeing 747251F · Fuselage Main, FrameSDR 0601116716Frame · crackedDURING L-CHECK AND ACCOMPLISHMENT OF MOD PER EM 5310-01319-02K FOUND CRACK IN UPPER DECK FRAME WEB CHORD AT BS 420 S12R. REPAIRED PER EA 67-206251.May 24, 2006 · N616US · Boeing 747251F · Fuselage Main, FrameSDR 0600186716Actuator · failedAFTER TAKEOFF NR 3 HYDRAULIC SYSTEM QUANTITY WENT TO NEAR ZERO. AIRCRAFT DUMPED 150,000 LBS OF FUEL AND RETURNED TO ANC, AND LANDED WITHOUT INCIDENT. ANC MAINTENANCE REMOVED AND REPLACED RUDDER ACTUATOR, AND NR 3 ENG HYDRAULIC PUMP. OPERATIONAL CHECKED OK, Jan 20, 2006 · N616US · Boeing 747251F · Rudder Control SystemSDR 0201886716Skin · crackedDuring "L" check found crack in the fuselage skin and bonded doubler at aft cargo door cutout. Repaired per EA 67-189583.May 23, 2002 · N616US · Boeing 747251F · Fuselage Main, Plate/SkinSDR 0100856716Keelbeam · corrodedDURING M-CHECK, FOUND CORROSION ON UPPER SURFACE OF KEEL BEAM LOWER STRUCTURE, STATION 1310 TO 1329. REPAIRED PER EA 67-165004.Feb 9, 2001 · N616US · Boeing 747251F · Fuselage Main, KeelSDR 0100846716Skin · corrodedDURING M-CHECK, FOUND CORROSION UNDER FORWARD LOWER SKIN AT LT OUTFLOW VALVE, STATION 2184, STR 45L. REPAIRED PER EA 67-165012.Feb 9, 2001 · N616US · Boeing 747251F · Fuselage Main, Plate/SkinSDR 0100836716Frame · crackedDURING M-CHECK, FOUND CRACK AT LEFT SIDE INNER FRAME, AFT HOLE, STATION 2231, STR 25L. REPAIRED PER EA 67-165008.Feb 9, 2001 · N616US · Boeing 747251F · Fuselage Main, FrameSDR 0001196716Detector · false indicationDURING DESCENT, THE NR 5 CARGO SMOKE DETECTOR LIGHT ILLUMINATED AND FIRE BELL ACTIVATED. VISUALLY CONFIRMED NO CARGO SMOKE OR FIRE. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE NR 5B CARGO SMOKE DETECTOR, OPERATIONAL CHECK GOOApr 7, 2000 · N616US · Boeing 747251F · Smoke DetectionSDR 0000466716Detector · malfunctionedDURING CLIMB, THE NR 5 CARGO SMOKE DETECTOR LIGHT ILLUMINATED AND FIRE BELL ACTIVATED. AIRCRAFT RETURNED TO ANC AND LANDED WITHOUT INCIDENT. REPLACED NR 5 CARGO SMOKE DETECTOR, OPERATIONAL CHECK GOOD.Apr 7, 2000 · N616US · Boeing 747251F · Smoke DetectionSDR 9903446716Support · corrodedDURING P-CHECK, FOUND CORROSION UNDER NUT PLATE UPPER CHORD OF FLOOR SUPPORT. REPAIRED PER EA 67-166746 (P/N 65B01723-328).Jul 16, 1999 · N616US · Boeing 747251F · Fuselage Miscellaneous StructureSDR 9803326716Flaps · vibratingDURING CLIMB, THE AIRCRAFT EXPERIENCED VIBRATIONS AND THE NR 1 LEADING EDGE FLAP NEEDED TO BE RAISED ELECTRICALLY. AIRCRAFT RETURNED TO NRT AND LANDED WITHOUT INCIDENT. REPLACED THE NR 1 LEADING EDGE FLAP POWER DRIVE UNIT. OPERATIONAL CHECK GOOD. SPECIFIC Feb 23, 1998 · N616US · Boeing 747251F · Leading Edge Slat Control SystemSDR 9803146716Start Valve · failedDURING CLIMB, THE NR 3 START VALVE LIGHT ILLUMINATED. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO NRT. MAINTENANCE CHANGED THE START VALVE AND THE START PRESSURE SWITCH. ALL INDICATIONS WERE NORMAL AND THE AIRCRAFT RETURNED TO SERVICE. EXACT PARTFeb 18, 1998 · N616US · Boeing 747251F · Engine Start Valves/ControlsSDR 9719006716Breather Tube · leakingDURING CRUISE, THE OIL QUANTITY INDICATED FOR THE NR 4 ENGINE DROPPED TO ZERO. THE ENGINE WAS SHUT DOWN AND THE FLIGHT DIVERTED TO MNL. MAINTENANCE FOUND THE UPPER RIGHT MAIN ENGINE BREATHER TUBE LEAKING. THE TUBE WAS REPLACED AND NO LEAKS WERE NOTED DURINGOct 9, 1997 · N616US · Boeing 747251F · Turbine Engine Oil SystemSDR 9714056716Logic Card · looseDURING TAKEOFF, THE MASTER CAUTION FIRE LIGHT ILLUMINATED AND THE AURAL WARNING SOUNDED. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE. RESEATED FIRE DETECTOR LOGIC CARDS AND SECOND OFFICER'S MASTER CANCEL SWITCH. OPERATIONAL CHECKS GOOD.Jul 20, 1997 · N616US · Boeing 747251F · Fire DetectionSDR 9714396716Bracket · corrodedDURING ARMAR, FOUND CORROSION ON RIGHT BODY GEAR WHEEL WELL PRESSURE DECK LOWER SURFACE AT FS 1404, RBL 109 - 119. REPAIRED PER EA 67-150441.May 14, 1997 · N616US · Boeing 747251F · Fuselage Miscellaneous StructureSDR 9714466716Pressure Deck · corrodedDURING ARMAR, FOUND CORROSION ON RIGHT BODY GEAR WHEEL WELL PRESSURE DECK LOWER SURFACE AT FS 1360, RBL 63. REPAIRED PER EA 67-150399.May 13, 1997 · N616US · Boeing 747251F · Fuselage Miscellaneous StructureSDR 9714446716Pressure Deck · corrodedDURING ARMAR, FOUND CORROSION ON PRESSURE DECK UPPER SURFACE AT FS 1440, LBL 33. REPAIRED PER EA 67-150118.May 8, 1997 · N616US · Boeing 747251F · Fuselage Miscellaneous StructureSDR 9714406716Frame · crackedDURING ARMAR, FOUND A CRACK IN FRAME WEB FS 434 BELOW STR 26L. REPAIRED PER EA 67-150127.May 7, 1997 · N616US · Boeing 747251F · Fuselage Main, FrameSDR 9714456716Frame · crackedDURING ARMAR, FOUND CRACKED FRAME WEB FS 488, STR 25L. REPAIRED PER EA 67-150371.May 6, 1997 · N616US · Boeing 747251F · Fuselage Main, FrameSDR 9714436716Floorbeam · crackedDURING ARMAR, FOUND CRACK IN UPPER DECK LEFT FLOORBEAM WEB FS 380. REPAIRED PER EA 67-150379.May 6, 1997 · N616US · Boeing 747251F · Fuselage Main, Floor BeamSDR 9714426716Floorbeam · crackedDURING ARMAR, FOUND CRACK IN FLOORBEAM WEB FS 380, STR 13R. REPAIRED PER EA 67-150380.May 6, 1997 · N616US · Boeing 747251F · Fuselage Main, Floor BeamSDR 9714416716Floorbeam · crackedDURING ARMAR, FOUND CRACK IN FLOORBEAM CHORD FS 380, STR 13R. REPAIRED PER EA 67-150380.May 6, 1997 · N616US · Boeing 747251F · Fuselage Main, Floor BeamSDR 9705996716Spar Web · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON LEFT WING FORWARD SPAR WEB AT FSS 895. REPAIRED PER EA 67-106389.Feb 12, 1997 · N616US · Boeing 747251F · Wing SparSDR 9705986716Spar Web · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON LEFT WING FORWARD SPAR WEB AT FSS 930. REPAIRED PER EA 67-106389.Feb 12, 1997 · N616US · Boeing 747251F · Wing SparSDR 9705976716Spar Web · crackedDURING PERIODIC CHECK, FOUND CRACK IN LEFT WING MID SPAR WEB BETWEEN WS 382 AND 411. REPAIRED PER EA 67-106387.Feb 6, 1997 · N616US · Boeing 747251F · Wing SparSDR 9627216716Transducer · malfunctionedDURING CRUISE, THE FLIGHT CREW OXYGEN GAUGE INDICATED ZERO. AIRCRAFT RETURNED TO SFO AND LANDED WITHOUT INCIDENT. REPLACED THE OXYGEN PRESSURE TRANSDUCER, OPERATIONAL CHECK GOOD.Dec 28, 1996 · N616US · Boeing 747251F · Crew Oxygen SystemSDR 9624896716Egt Wire · failedDURING TAKEOFF ROLLOUT, THE NR 1 ENGINE EGT GAUGE INDICATED APPROXIMATELY 400 DEGREES WHILE OTHERS INDICATED 750 DEGREES. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A PREVIOUSLY REPAIRED WIRE FORNov 16, 1996 · N616US · Boeing 747251F · Engine EGT/TIT Indicating SystemSDR 9614246716Detector · malfunctionedDURING CRUISE, THE NR 2 MAIN DECK CARGO SMOKE DETECTOR ACTIVATED. AIRCRAFT DIVERTED TO YEG AND LANDED WITHOUT INCIDENT. REPLACED DETECTOR, OPERATIONAL CHECK GOOD.Jun 27, 1996 · N616US · Boeing 747251F · Smoke DetectionSDR 9604256615Fuel Control · malfunctionedDURING TAKEOFF, THE NR 2 ENGINE FAILED TO REACH TAKEOFF POWER. CREW ABORTED TAKEOFF AT 60 KNOTS AND RETURNED TO THE GATE. FOUND HYDRAULIC STAGE PRESSURE TO BE ZERO. REPLACED FUEL CONTROL AND FUEL PUMP. THE NR 2 ENGINE HIGH POWER RUNUP CHECK WAS NORMAL AND Feb 19, 1996 · N616US · Boeing 747251B · Fuel Control/Turbine EnginesSDR 9515006716Actuator · malfunctionedSFO-ANC - EN ROUTE, THE NR 1 LEADING EDGE DEVICE IN TRANSIT LIGHT ILLUMINATED. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND DIVERTED TO SEA. MAINTENANCE REPLACED THE LEADING EDGE FLAP DEVICE ACTUATOR AND PERFORMED FUNCTIONAL CHECK. CHECK WAS NORMAL AND AIRSep 30, 1995 · N616US · Boeing 747251F · Leading Edge Slat ActuatorSDR 9513506716Skin · delaminatedDURING PERIODIC CHECK, FOUND PREVIOUS FIBERGLASS REPAIR DELAMINATED ON THE RIGHT OUTBOARD ELEVATOR, 8 FORWARD OF THE TRAILING EDGE. REPAIRED PER SRM 51-40-12.Aug 30, 1995 · N616US · Boeing 747251F · Elevator, Plate/SkinSDR 9513296716Skin · delaminatedDURING PERIODIC CHECK, FOUND DELAMINATION ON RIGHT OUTBOARD AILERON UPPER SURFACE WS 1508. REPAIRED PER SRM 51-40-14, PART 4, FIG. 9.Aug 26, 1995 · N616US · Boeing 747251F · AileronsSDR 9512786716Support · crackedDURING PERIODIC CHECK, THE LEFT AND RIGHT NOSE CARGO DOOR PORTAL LATCH NR 4 SUPPORT FITTING AT LBL 70 AND RBL 70 WERE FOUND CRACKED. THE (P/N 65B13044-3), 4 SUPPORT FITTINGS WERE FOUND WITH A CRACK THROUGH THE VERTICAL AND HORIZONTAL FLANGES, MADE REPAIR PER Aug 22, 1995 · N616US · Boeing 747251F · Fuselage Miscellaneous StructureSDR 9511546716Connector · contaminatedDURING CRUISE, THE NR 4 ENGINE FIRE WARNING LIGHT ILLUMINATED AND BOTH TEMPERATURE LOOPS WERE READING FULL SCALE. THE ENGINE WAS SHUT DOWN. THE LEFT FIRE BOTTLE WAS DISCHARGED AND THE FLIGHT CONTINUED TO NRT WHERE AN UNEVENTFUL THREE ENGINE LANDING WAS ACCOMPJul 28, 1995 · N616US · Boeing 747251F · Fire Detection
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