Boeing 747-273C

Service difficulty reports · 647

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 = '747273C'
  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 EIAA980211Fire Detector · malfunctionedFJR - LOG PAGE: F80971 - ON CLIMB-OUT, FORWARD LOWER CARGO COMPARTMENT FIRE LIGHT ILLUMINATED. NO CARGO LOADED. NO SMOKE OR FIRE OBSERVED. RETURNED TO FJR. REPLACED FORWARD LOWER CARGO AFT SMOKE DETECTOR, AND OPS CHECKED SYSTEM PER MM 26-14-02. (X)Jun 19, 1998 · N471EV · Boeing 747273C · Fire DetectionSDR EIAA0211Smoke Detector · failedFJR - LOG PAGE: F80971 - ON CLIMB-OUT, FORWARD LOWER CARGO COMPARTMENT FIRE LIGHT ILLUMINATED. NO CARGO LOADED. NO SMOKE OR FIRE OBSERVED. RETURNED TO FJR. REPLACED FORWARD LOWER CARGO AFT SMOKE DETECTOR, AND OPS CHECKED SYSTEM PER MM 26-14-02. (X)Jun 19, 1998 · N471EV · Boeing 747273C · Smoke DetectionSDR EIAA9802206Line · chafedNGU - DURING CLIMB, LOST NR 3 HYDRAULIC SYSTEM, QUANTITY WENT OT ZERO AND PRESSURE WAS FLUCTUATING DOWN TO 2200 PSI. TURNED SYSTEM OFF. DIVERTED TO JFK. REPLACED HYDRAULIC LINE UNDER GAP COVER IN PYLON AND LEAK CHECKED GOOD MM 29-11-00. (M)Jun 16, 1998 · N471EV · Boeing 747273C · Hydraulic System, MainSDR EIAA980206Line · chafedNGU - LOG PAGE: F80966 - DURING CLIMB, LOST NR 3 HYDRAULIC SYSTEM, QUANTITY WENT TO ZERO, AND PRESSURE WAS FLUCTUATING DOWN TO 2,200 PSI. TURNED SYSTEM OFF. DIVERTED TO JFK. REPLACED HYDRAULIC LINE UNDER GAP COVER IN PYLON AND LEAK CHECKED GOOD. MM 29-11-Jun 16, 1998 · N471EV · Boeing 747273C · Hydraulic System, MainSDR EIAA980199Light · illuminatedABORTED TAKEOFF AFTER NOSE DOOR LIGHT ILLUMINATED ON TAKEOFF ROLL. OPENED AND CLOSED NOSE DOOR TWICE. VERIFIED AND CHECKED VISUALLY ALL LATCHES PINS PRIOR TO DEPARTURE. (M)May 11, 1998 · N471EV · Boeing 747273C · Landing Gear Position and WarningSDR 98ZZZX2244Wheel · deflatedWHILE PARKED AT GATE, NR 9 WHEEL LOST PRESSURE SUDDENLY. SUSPECT CAUSE - FUSIBLE PLUG FAILED AND BRAKE OVERHEATED.May 11, 1998 · N470EV · Boeing 747273C · Wheel/Ski/FloatSDR EIAA980151Oil System · lack of lubeJFK - SHUTDOWN NR 3 ENGINE AFTER 30 MINUTES INTO FLIGHT DUE TO LOSS OF OIL PRESSURE. OIL VISCOSITY WAS VERY THICK AND ENGINE REQUIRED 26 QUARTS TO FILL. (M)Mar 29, 1998 · N471EV · Boeing 747273C · Turbine Engine Oil SystemSDR EIAA980138Fitting · crackedHKG - DURING 'C5/D' CHECK INSPECTION, RT WS 669.5 BULKHEAD PYLON SUPPORT FORWARD INBOARD BACK-UP FITTING CRACKED AT STR 24. BACK-UP FITTING REPLACED IAW SB 54A2159. (X)Feb 19, 1998 · N471EV · Boeing 747273C · Nacelle/Pylon StructureSDR EIAA980137Shear Tie · crackedHKG - DURING 'C5/D' CHECK INSPECTION, RT WS 669.5 UPPER FORWARD MOST SHEAR TIE CAP CRACKED. REPAIRED IAW SB 57-2273 FIG 8 AND FIG 9. (X)Feb 19, 1998 · N471EV · Boeing 747273C · Wing Miscellaneous StructureSDR EIAA980136Fitting · corrodedHKG - DURING 'C5/D' CHECK INSPECTION, FORWARD CARGO COMPARTMENT NR 4 DOOR SILL LATCH CAM TRUSS FITTING CORRODED. REPLACED IAW SRM 51-10-01. (X)Feb 19, 1998 · N471EV · Boeing 747273C · Passenger/Crew DoorsSDR EIAA980135Track · crackedDURING 'C5/D' CHECK INSPECTION, FORWARD CARGO COMPARTMENT TIE-DOWN TRACK FOUND CRACKED AT BS 570 RBL 25. REPAIRED TRACK IAW SRM 53-10-05 FIG 5. (X)Feb 19, 1998 · N471EV · Boeing 747273C · Fuselage, Seat/Cargo Attach FittingsSDR EIAA980134Frame · crackedHKG - DURING 'C5/D' CHECK INSPECTION, BS 438 BETWEEN STR 25 - STR 26 FRAME WEB CRACKED. REPAIRED FRAME WEB IAW HAECO RS 53-11-33658. (X)Feb 19, 1998 · N471EV · Boeing 747273C · Fuselage Main, FrameSDR EIAA980131Panel · crackedHKG - DURING 'C5/D' CHECK INSPECTION, LT WING WHEEL WELL BS 1241 CANTED B/K CRACKED AT LT UPPER CORNER LBL 90 AT TRIM AIR DUCT CUT-OUT. PANEL REPLACED IAW SB 747-53-2329. (X)Feb 19, 1998 · N471EV · Boeing 747273C · Fuselage Miscellaneous StructureSDR EIAA980130Floor Beam · damagedHKG - DURING 'C5/D' CHECK INSPECTION, AFT CARGO COMPARTMENT BS 1880 FLOOR BEAM UPPER CHORD DAMAGED AT LBL 48. REPAIRED IAW SRM 51-40-03 FIG 2. (X)Feb 19, 1998 · N471EV · Boeing 747273C · Fuselage Main, Floor BeamSDR EIAA980129Skin · crackedHKG - DURING 'C5/D' CHECK INSPECTION, NR 4 PYLON INBOARD SKIN CRACKED AT NAC STA 180. REPAIRED IAW HAECO RS R54-51-33609. (X)Feb 17, 1998 · N471EV · Boeing 747273C · Nacelle/Pylon, Plate/SkinSDR EIAA980128Skin · crackedHKG - DURING 'C5/D' CHECK INSPECTION, NR 3 PYLON LT OUTER SKIN CRACKED AT NAC STATION 180. REPAIRED IAW HAECO RS R54-51-33636. (X)Feb 17, 1998 · N471EV · Boeing 747273C · Nacelle/Pylon, Plate/SkinSDR EIAA980127Frame · crackedHKG - DURING 'C5/D' CHECK INSPECTION, NR 1 PYLON FRAME CRACKED AT NAC 163. REPAIRED IAW SRM 51-10-01. (X)Feb 17, 1998 · N471EV · Boeing 747273C · Nacelle/Pylon, Frame/Spar/RibSDR EIAA980126Stringer · crackedHKG - DURING 'C5/D' CHECK INSPECTION, NR 1 PYLON, CRACKED STRINGER AT NAC 166 OUTBOARD SIDE OF PYLON. REPAIRED IAW SRM 52-40-04 FIG 2. (X)Feb 17, 1998 · N471EV · Boeing 747273C · Nacelle/Pylon, Longeron/StringerSDR EIAA980125Web · misinstalledHKG - DURING 'C5/D' CHECK INSPECTION, NR 1 PYLON MID-SPAR WEB CUT-OUT AREA ON REWORK HAS AS EXTRA ROW OF FASTENERS. REPAIRED IAW HAECO RS R54-53-33608. (X)Feb 17, 1998 · N471EV · Boeing 747273C · Nacelle/Pylon StructureSDR EIAA980122Floor Beam · damagedHKG - DURING 'C5/D' CHECK INSPECTION, AFT CARGO COMPARTMENT BS 1720 FLOOR BEAM UPPER CHORD DAMAGED BL ZERO - RBL 12. WEB REPAIRED IAW SRM 51-40-02, FIG 1, AND ANGLE REPLACED IAW SRM 51-10-01. (X)Feb 15, 1998 · N471EV · Boeing 747273C · Fuselage Main, Floor BeamSDR EIAA980121Floor Beam · damagedHKG - DURING 'C5/D' CHECK INSPECTION, AFT CARGO COMPARTMENT BS 1760 FLOOR BEAM UPPER CHORD DAMAGED LBL 15 - LBL 22. (X)Feb 15, 1998 · N471EV · Boeing 747273C · Fuselage Main, Floor BeamSDR EIAA980120Shear Tie · crackedHKG - DURING C5/D CHECK INSPECTION, LEFT BODY LANDING GEAR WHEEL WELL BS 1372 BULKHEAD UPPER CHORD, VERTICAL FRAME SHEAR TIE CRACKED. REPAIRED IAW SRM 53-10-04 FIG 4. (M)Feb 15, 1998 · N471EV · Boeing 747273C · Fuselage Miscellaneous StructureSDR EIAA980119Spar · crackedHKG - DURING C5/D CHECK INSPECTION, RT WING SPAR UPPER CHORD FSS 688 CRACK AT FASTENER HOLE. REPAIRED IAW HAECO RS 554-52-33482. (M)Feb 15, 1998 · N471EV · Boeing 747273C · Wing SparSDR EIAA980118Skin · dentedHKG - DURING C5/D CHECK INSPECTION, FUSELAGE BS 1840 AT STRINGER 46L - 47L, SKIN HAS A DENT. REPAIRED IAW SRM 53-30-03 FIG 1. (M)Feb 15, 1998 · N471EV · Boeing 747273C · Fuselage Main, Plate/SkinSDR EIAA980117Skin · damagedHKG - DURING C5/D CHECK INSPECTION, FWD CARGO DOOR AFT LOWER CORNER SKIN DAMAGED. REPAIRED IAW SRM 52-00-03 FIG 4. (M)Feb 15, 1998 · N471EV · Boeing 747273C · Cargo/Baggage DoorsSDR 98ZZZX1046Blades · damagedON ARRIVAL NADI, FOUND FOUR N1 BLADES ON NR 1 ENGINE SEVERELY DAMAGED. SUSPECT CAUSE: INGESTION OF FOREIGN OBJECTS ON RUNWAY 02 CAUSED BY GEMINI AIR CARGO DC10-30F BLOWN WHEELS THAT LANDED EARLIER.Feb 15, 1998 · N470EV · Boeing 747273C · Turbine Engine Compressor SectionSDR EIAA980115Web · damagedHKG - DURING C5/D CHECK INSPECTION, AFT CARGO COMPARTMENT, BS 1760 AT RBL 52 FLOORBEAM VERTICAL WEB DAMAGED. REPAIRED IAW SRM 51-40-02 FIG 1. (M)Feb 14, 1998 · N471EV · Boeing 747273C · Fuselage Miscellaneous StructureSDR EIAA98057Trunnion · corrodedHKG - DURING 'C5/D' CHECK INSPECTION, LEFT WING GEAR FWD TRUNNION H FITTING AND RETAINER NUT SEIZED. TRUNNION BEARING H FITTING REPLACED IAW MM 57-43-01. (M)Feb 12, 1998 · N471EV · Boeing 747273C · Main Landing Gear Attach SectionSDR EIAA980124Brace · wornHKG - DRUING 'C5/D' CHECK INSPECTION, NR 4 PYLON FORWARD DIAGONAL BRACE FITTING HAS THREE SLOTTED HOLES. REPAIRED IAW HAECO RS R54-54-33605. (X)Feb 10, 1998 · N471EV · Boeing 747273C · Nacelle/Pylon StructureSDR EIAA980123Brace · wornHKG - DURING 'C5/D' CHECK INSPECTION, NR 1 PYLON FORWARD DIAGONAL BRACE FITTING HAS THREE SLOTTED HOLES. REPAIRED IAW HAECO RS R54-54-33605. (X)Feb 10, 1998 · N471EV · Boeing 747273C · Nacelle/Pylon StructureSDR EIAA98054Shim · damagedHKG - DURING 'C5/D' CHECK INSPECTION, LEFT WING LANDING GEAR SUPPORT BEAM OUTBOARD END FITTING SHIM DAMAGED. SHIMS REPLACED IAW MM 57-15-01. (M)Feb 9, 1998 · N471EV · Boeing 747273C · Wing Miscellaneous StructureSDR EIAA98053Bushing · wornHKG - DURING 'C5/D' CHECK INSPECTION, NR 3 PYLON AFT UPPER MOUNT HAS WORN ATTACH BUSHING AND SIDE PLAY. ENGINE UPPER MOUNT BUSHING REPLACED IAW OHM 20-50-03. (M)Feb 8, 1998 · N471EV · Boeing 747273C · Engine Mount SectionSDR EIAA98052Bushing · wornHKG - DURING 'C5/D' CHECK INSPECTION, NR 4 PYLON AFT UPPER MOUNT HAS WORN ATTACH BUSHING AND SIDE PLAY. THRUST LINK END FITTING WORN. ENGINE UPPER MOUNT BUSHING REPLACED IAW OHM 20-50-03, THRUST LINK BEARING REPLACED IAW OHM 20-50-03. (M)Feb 8, 1998 · N471EV · Boeing 747273C · Engine Mount SectionSDR 98ZZZX904Bearing · wornHKG - DURING C5/D-CHECK INSPECTION, NR 4 PYLON AFT UPPER MOUNT HAS WORN ATTACH BUSHING AND SIDE PLAY. THRUST LINK END FITTING WORN. ENGINE UPPER MOUNT BUSHING REPLACED IAW OHM 20-50-03, THRUST LINK BEARING REPLACED IAW OHM 20-50-03. REFERENCE: OPERATOR CONFeb 8, 1998 · N471EV · Boeing 747273C · Engine Mount SectionSDR 98ZZZM333Bearing · wornHKG - DURING 'C5/D' CHECK INSPECTION, NR 4 PYLON AFT UPPER MOUNT HAS WORN ATTACH BUSHING AND SIDE PLAY. THRUST LINK END FITTING WORN. ENGINE UPPER MOUNT BUSHING REPLACED IAW OHM 20-50-03, THRUST LINK BEARING REPLACED IAW OHM 20-50-03. (M)Feb 8, 1998 · N471EV · Boeing 747273C · Engine Mount SectionSDR EIAA98051Floorbeam · damagedHKG - DURING 'C5/D' CHECK INSPECTION, AFT CARGO BS 1820 LBL 22, FLOORBEAM VERTICAL WEB DAMAGED. REPAIRED WEB IAW SRM 51-40-02 FIG 1. (M)Feb 7, 1998 · N471EV · Boeing 747273C · Fuselage Main, Floor BeamSDR EIAA98050Floorbeam · damagedHKG - DURING 'C5/D' CHECK INSPECTION, AFT CARGO BS 1800 AT RBL 6, FLOORBEAM VERTICAL WEB IS DAMAGED. REPAIRED WEB IAW SRM 51-40-02 FIG 1. (M)Feb 7, 1998 · N471EV · Boeing 747273C · Fuselage Main, Floor BeamSDR EIAA98049Skin · delaminationHKG - DURING 'C5/D' CHECK INSPECTION, RT OUTBOARD AILERON HAS SMALL AREA OF DELAMINATINO ON LOWER SURFACE OUTBOARD END. FIBERGLASS REPAIRED IAW SRM 51-40-15 FIG 7. (M)Feb 7, 1998 · N471EV · Boeing 747273C · AileronsSDR EIAA98048Bearing · rotatingHKG - DURING 'C5/D' CHECK INSPECTION, NR 4 PYLON THRUST LINK BEARING IS ROTATING IN THE HOUSING. BEARING REPLACED IAW OHM 20-50-03. (M)Feb 7, 1998 · N471EV · Boeing 747273C · Engine Mount SectionSDR EIAA98047Seat Track · corrosionHKG - DURING 'C5/D' CHECK INSPECTION, BS 560 -580 AT RBL 55 SEAT TRACK HAS CORROSION. REPAIRED IAW SRM 53-10-05. (M)Feb 7, 1998 · N471EV · Boeing 747273C · Fuselage, Seat/Cargo Attach FittingsSDR EIAA98046Stringer · corrosionHKG - DURING 'C5/D' CHECK INSPECTION, AFT CARGO BS 1680 STRINGER 40L HAS CORROSION. REPAIRED IAW SRM 53-10-03 FIG 1. (M)Feb 7, 1998 · N471EV · Boeing 747273C · Fuselage Main, Longeron/StringerSDR EIAA98045Floorbeam · corrosionHKG - DURING 'C5/D' CHECK INSPECTION, FLOORBEAM BS 760 LBL 34 LOWER CHORD HAS CORROSION. REPAIRED IAW SRM 53-10-07 FIG 12. (M)Feb 7, 1998 · N471EV · Boeing 747273C · Fuselage Main, Floor BeamSDR EIAA98044Pin · seizedHKG - DURING 'C5/D' CHECK INSPECTION, LEFT HORIZONTAL STAB HINGE BOLT ADJUSTMENT NUT SEIZED. HINGE PIN ASSEMBLE MODIFIED IAW SB 747-55-2020 REV 7. (M)Feb 6, 1998 · N471EV · Boeing 747273C · Horizontal Stabilizer StructureSDR EIAA98043Fitting · crackedDURING 'C5/D' CHECK INSPECTION, R1 DOOR DOOR BODY TORQUE TUBE SUPPORT FITTING CRACKED. FITTING REPLACED IAW SRM 51-10-01. (M)Feb 6, 1998 · N471EV · Boeing 747273C · Passenger/Crew DoorsSDR EIAA98042Fitting · crackedHKG - DURING 'C5/D' CHECK INSPECTION, BS 1480 RBL 33 LONGITUDINAL FLOORBEAM 01B LOWER SUPPORT FITTING CRACKED. FITTING REPLACED IAW SRM 51-10-1. (M)Feb 6, 1998 · N471EV · Boeing 747273C · Fuselage Miscellaneous StructureSDR EIAA98041Frame · crackedHKG - DURING 'C5/D' CHECK INSPECTION, NR 3 PYLON INTERIOR O/B VERTICAL FRAME AT STATION 180 IS CRACKED AT THE UPPER CORNER. REPAIRED IAW SRM 54-10-03 FIG 1. (M)Feb 6, 1998 · N471EV · Boeing 747273C · Nacelle/Pylon, Frame/Spar/RibSDR EIAA98040Floorbeam · crackedHKG - DURING 'C5/D' CHECK INSPECTION, BS 2140 LBL 98 FLOORBEAM UPPER CHORD HAS CORROSION AND CRACK. REPAIRED IAW SRM 53-10-07 FIG 12. (M)Feb 6, 1998 · N471EV · Boeing 747273C · Fuselage Main, Floor BeamSDR EIAA98056Support · corrodedHKG - DURNIG 'C5/D' CHECK INSPECTION, FUSELAGE KEEL BEAM LOWER PANEL SUPPORT CORRODED T BS 1266 LBL 16 RBL 16. PANEL SUPPORT REPLACED IAW SRM 51-10-1. (M)Feb 5, 1998 · N471EV · Boeing 747273C · Fuselage Miscellaneous StructureSDR EIAA980319Skin · corrodedHKG - DURING C5/D CHECK INSPECTION, CORROSION ON FUSELAGE SKIN AND TEAR STRAP AT BS 560 STRINGER 46R. CORRODED AREA TRIMMED AWAY FROM SKIN AND TEAR STRAP, REPAIRED BY INSTALLING TWO INTERNAL STRAPS AND THREE EXTERNAL REPAIR DOUBLERS, PER HAECO RS R53-21-33659Feb 5, 1998 · N471EV · Boeing 747273C · Fuselage Main, Plate/SkinSDR EIAA980113Spar · crackHKG - DURING C5/D CHECK INSPECTION, RIGHT WING FRONT SPAR CHORD HAS A FASTENER HOLE THAT IS CRACKED BEYOND LIMITS. OVERSIZED HOLE TO REMOVED CRACK AND INSTALLED NEW FASTENER IAW HAECO RS R54-52-33482. (M)Feb 5, 1998 · N471EV · Boeing 747273C · Wing Spar
Back to Boeing 747-273C