N471EV

Service difficulty reports · 366

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 = 'N471EV' AND registry_match = 'registration'
  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 EIA2007028Skin · crackedFWD CARGO DOOR LOWER CORNER VIEW PORT FOUND 3 CRACKS ON DOOR SKIN. REMOVED EXISTING REPAIR AND CUT OUT DAMAGED PART OF SKIN. FABRICATE NEW REPAIR DOUBLER AND FILLER, CARRIED OUT HFEC ON CUT EDGES AND ALL FASTENER HOLES. APPLY CHEM COATING AND PRIMER TO ALL Feb 22, 2007 · N471EV · Boeing 747273C · Cargo/Baggage DoorsSDR EIA2007027Spar · damagedDAMAGE FOUND COMMON TO FRONT SPAR, LOWER CHORD OF RT O/B ELEVATOR STA 227.65. TRIM OUT DAMAGED PORTION OF LOWER CHORD, CARRY OUT HFEC ON TRIM EDGES. FABRICATE FILLER AND REPAIR ANGLES. APPLY ALODINE COATING TO ALL REPAIR PARTS AND BASE METAL EDGES. INSTALLFeb 22, 2007 · N471EV · Boeing 747273C · Elevator, Spar/RibSDR EIA2007025Skin · corrodedPROPAGATING CORROSION WAS FOUND AROUND CEC DOOR CUT OUT AREA BETWEEN STA 780 TO 850. FUSELAGE SKIN AND CUTOUT DOUBLER REPLACED.Feb 22, 2007 · N471EV · Boeing 747273C · Fuselage Main, Plate/SkinSDR EIA2007023Seal · erodedMANY FLAP MOLDING SEALS WERE FOUND ERODED AT DIFFERENT LOCATIONS. ERODED MOLDING SEAL WAS REPLACED, REPAIRED PER N471EV-07-0001.Feb 22, 2007 · N471EV · Boeing 747273C · Trailing Edge FlapsSDR EIA2007022Skin · corrodedFORWARD CARGO CEC CUTOUT, BILGE, SKIN UNDER DOUBLER FOUND CORRODED AND FORWARD RIGHT DOUBLER FOUND CRACKED OFF. ACCOMPLISHED SKIN REPAIR PER BOEING RESPONSE 1-280156778.Feb 22, 2007 · N471EV · Boeing 747273C · Fuselage Main, Plate/SkinSDR EIA2007021Beam · corrodedFOUND FORWARD CARGO DOOR LOWER CLOSE OUT BEAM CORROSION AT SCREW HOLES FROM STA 567 TO 662. CORRODED BEAM WEB REPLACED AND INSTALLED FASTENERS WITH SHORT EDGE MARGINS WERE REPAIRED. FASTENERS WITH SHORT EDGE MARGINS WERE TRIMMED OUT AND REPAIR DOUBLERS WERE Feb 22, 2007 · N471EV · Boeing 747273C · Cargo/Baggage DoorsSDR EIA2007017Door Frame · crackedNR 3 MAIN ENTRY DOOR FRAME IS PRONE TO CRACKING FROM FATIGUE, INSPECTION REVEALED THE REQUIREMENT TO REPAIR/MODIFY BS 1265 FRAME WEB AND CHORD PER EO 53-747-1580-00 REV E. CARRIED OUT MODIFICATION OF INTERCOSTAL AND FRAME AND INSTALLED NEW INNER CHORD AS PER Feb 15, 2007 · N471EV · Boeing 747273C · Fuselage Main, StructureSDR EIA2007018Intercostal · crackedFOUND INTERCOSTAL MOUNTING SCREW HOLE FLANGE AREA CRACKED AT STA 2280 TO 2320 AT LBL 76. CRACKED INTERCOSTAL REPLACED IAW B747 SRM 51-10-01 PG 6-9 AND SRM 51-30-02 PG 5-9. NEW INTERCOSTAL MADE FROM BAC 1509-100506, 7075-76.Feb 15, 2007 · N471EV · Boeing 747273C · Fuselage Miscellaneous StructureSDR EIA2007016Beam · corrodedFOUND FORWARD CARGO DOOR INTERNAL LOWER, CLOSE OUT BEAM, CORROSION AT SCREW HOLES FROM STA 567 TO STA 662. CORRODED BEAM WEB REPLACED AND INSTALLED FASTENERS WITH EDGE MARGINS WERE REPAIRED AS PER BOEING MSG 1-273529392-12 AND FAA 8100-9 DATED 13 FEB 07.Feb 15, 2007 · N471EV · Boeing 747273C · Fuselage Main, StructureSDR EIA2007026Hinge Fitting · damagedINSTALLATION OF SPOILER HINGE FITTING AT WS1028.525 REQUIRES RIVETS AND TAPER LOOKS DUE TO DIFFICULTIES IN INSTALLING RIVETS, REPLACEMENT NEEDED. USE BACB30NX8K*Y HILOCKS WITH BACC30AC8 COLLARS PER BOEING MESSAGE 1-280951.970-8 DATED 5 FEB 07Jan 28, 2007 · N471EV · Boeing 747273C · SpoilersSDR EIA2007024Fitting · corrodedFOUND NR 6 FLAP TRACK AFT ALIGNMENT FITTING WITH CORROSION ON SURFACE BETWEEN FITTING AND WING SKIN. HOLES WERE OVERSIZED AND SPOT FACED. REPAIR BUSHINGS INSTALLED PER BOEING MESSAGE 1-277661910-9.Jan 24, 2007 · N471EV · Boeing 747273C · Trailing Edge FlapsSDR EIA2006372Power Supply · inoperativeUPPER DECK CREW EXIT DOOR EMERGENCY EXIT SIGN WILL NOT ILLUMINATE.Oct 26, 2006 · N471EV · Boeing 747273C · Emergency LightingSDR EIA2006371Light · inoperativeMAIN DECK CEILING LIGHT AT STA 350R FOUND INOP. INITIAL SUBMISSION, RESEARCHING COMPONENT TIMES.Oct 26, 2006 · N471EV · Boeing 747273C · Passenger Compartment LightingSDR EIA2006233Connector · defectiveAFTER TAKEOFF, HAD A RUDDER RATIO LIGHT CAME ON, RETURNED TO BLOCK. REPLACED SUSPECT ELECTRICAL CONNECTOR, SYSTEM OPS CHECK GOOD ON GROUND. PITOT STATIC CHECK C/W.Sep 29, 2006 · N471EV · Boeing 747273C · Rudder Control SystemSDR EIA2006160Smoke Detector · no testNR 5 LOWER LOBE SMOKE DETECTOR, NO TEST. REPLACED SAME.Aug 3, 2006 · N471EV · Boeing 747200B · Smoke DetectionSDR EIA2006084Light · inoperativeUPPER DECK EMERGENCY LIGHT INOP. REPLACED LIGHT PER MM 33-51-07, OPS CHECK GOOD.Jun 1, 2006 · N471EV · Boeing 747273C · Emergency LightingSDR EIA2006083Light · inoperativeMAIN DECK 5L AND 1L EMERGENCY LIGHTS INOP. REPLACED LIGHTS PER MM 33-51-07, ALSO RESET C/B D3306P.Jun 1, 2006 · N471EV · Boeing 747273C · Emergency LightingSDR EIA2006061Switch · failedFIRE WARNING LIGHTS ON CONSTANT, WILL NOT RESET OR TEST. FOUND BAD FIRE WARNING CUT-OUT SWITCH. REPLACED MASTER F/O SWITCH AND ASSY, OPS CHK GOOD.Apr 25, 2006 · N471EV · Boeing 747273C · Emergency LightingSDR EIAA200660Light · inoperativeFOUND UPPER DECK EMERGENCY EXIT SIGN INOP ON BATTERY ACCESS PANEL. REPLACED EMERGENCY LIGHT ASSEMBLY PER MM 33-51-07, OPS CHK GOOD PER MM 33-51-00.Apr 22, 2006 · N471EV · Boeing 747273C · Emergency LightingSDR EIA2006043Switch · damagedON LANDING, RT WING OVERHEAT LIGHT ON. FOUND SWITCH S874 NOT IN BRACKET AND PINCHED AGAINST STRINGERS. REINSTALLED SWITCH AS PER MM 26-18-02. OPS CHK GOOD AS PER MM 26-18-00.Apr 2, 2006 · N471EV · Boeing 747273C · Standard Practices/StructuresSDR EIA2006040Wire · brokenDURING CRUISE AT FL 310, NR 3 ENGINE SHUTDOWN DUE TO WING OVERHEAT INDICATION, UNABLE TO CLOSE PYLON VALVE NR 3. NACELLE SENSOR S1048 WITH BROKEN WIRES REPAIRED PER STD MAINT. PRACTICES. OPS CHK GOOD PER MM 26-18-00. PERFORMED ENGINE WINDMILL CHECK PER MM 7Mar 31, 2006 · N471EV · Boeing 747273C · Overheat DetectionSDR EIA2006042Doubler · crackedDURING B CHECK; FOUND L1 DOOR HINGE CUTOUT DOUBLER CRACK 1/8 AT LOWER CORNER. REPAIRED HINGE CUTOUT IAW SB747-52-2144- FIG 4.Mar 29, 2006 · N471EV · Boeing 747273C · Fuselage Main, Plate/SkinSDR EIAA2006041Pressure Panel · crackedDURING B CHECK; FOUND 2 CRACKS IN NOSE WHEEL WELL TOP PANEL WEB. CRACKS REPAIRED PER SRM 53-10-04, FIG 119.Mar 27, 2006 · N471EV · Boeing 747273C · Fuselage Main, BulkheadSDR EIA2006007Fan · odorWHEN RECIRCULATING FANS TURNED ON, FUMES WERE NOTED. FANS TURNED OFF, FUMES WENT AWAY. DEFERRED AND TROUBLESHOT TO DUCT WORK. DUCT PART ORDERED. REMAINS OPEN PENDING REPLACEMENT.Jan 6, 2006 · N471EV · Boeing 747273C · Air Distribution FanSDR EIA2005132Engine · failedFL 340 IN CRUISE, NO TURBULENCE LOUD BANG WITH YAW TO RIGHT ENG NR 4 N1, N2 EGT PARAMETERS INDICATION EXCEEDENCES (RED) ENGINE FLAMED OUT. SECURED ENG. NO FIRE WARNING. METAL IN TAILPIPE REMOVED AND REPLACED NR 4 ENGINE IAW F7201/9724001.Jun 30, 2005 · N471EV · Boeing 747273C · Engine (Turbine/Turboprop)SDR EIA2005125Connector · looseFOUND NR 5 EMERGENCY EXIT SIGN AT R5 DOOR INOPERATIVE, DMI 962 ISSUED. RECONNECTED CONNECTORS TO WIRING FROM SIGN. R5 DOOR EMERGENCY EXIT SIGN OPS CKS OK IAW MM 33-51-00 PG 501. DMI CLEARED. PLACARD REMOVED.May 16, 2005 · N471EV · Boeing 747273C · Emergency LightingSDR EIA2005124Light · inoperativeDURING INSPECTION, FOUND EMERGENCY LIGHT AT STATION 600 L/S INOPERATIVE. RELAMPED LIGHT ASSEMBLY 600 L/S, OP'S CHECK GOOD IAW MM 33-51-07.May 13, 2005 · N471EV · Boeing 747273C · Emergency LightingSDR EIA2005026Frame · crackedFUSELAGE STA 1000 CHORD IS CRACKED BETWEEN STR 37L-38L NEAR BATHTUB FITTING AT EXTERIOR SIDE UNDER RAM AIR DUCT. REMOVED DAMAGED CHORD FROM STA 1000 BETWEEN STR 37-38 LT AND REPLACED PER B747 SERVICE BULLETIN 747-53A2471 FIG 13 AND EO 53-747-1072-90 REV A PARFeb 22, 2005 · N471EV · Boeing 747273C · Fuselage Main, FrameSDR EIA2005025Stringer · crackedBETWEEN STA 260-280 STRINGER 41 LT CRACKED AT AFT END. REMOVED AND REPLACED STRINGER STA 260-280 NR 41 LT PER B747 SRM 51-30-02 PG 2-9. FABRICATED NEW STRINGER NR 41 LT STA 260-280 PER B747 SRM 51-20-01 PAGE 11-20.Feb 22, 2005 · N471EV · Boeing 747273C · Fuselage Main, Longeron/StringerSDR EIA2005024Skin · corrodedFUSELAGE BS 1000 LT BETWEEN STR 37 & 40 HAS CORROSION ON SKIN INSIDE OF FWD PIT. REMOVED CORROSION AT STA 1000 STR 39-41 LT PER B747 SRM 53-30-03 FIG 12. CUT OUT LIMIT SKIN AREA PER B747 SRM 53-10-01 FIG 1, NDT CHECKED NO CRACK NOTED FABRICATED INSTALLED REPFeb 22, 2005 · N471EV · Boeing 747273C · Fuselage Main, Plate/SkinSDR EIA2005023Floorbeam · crackedBS 420 LBL 43 UPPER DECK FLOORBEAM WEB HAS CRACK AT UPPER T-CHORD AREA. REMOVED DAMAGED SECTION OF WEB AND REPAIRED PER B747 SRM 53-10-07 PG 47-50 FIG II. BONDED WEB AND DOUBLER FOR STA 420 LBL 34-54 PER BAC 5514-5101 BOEING DRAWING 65B10931 SHEET 75 AND B74Feb 22, 2005 · N471EV · Boeing 747273C · Fuselage Main, Floor BeamSDR EIA2005022Skin · damagedSTA 240 AFT OF NOSE CARGO DOOR BOTTOM FUSELAGE SKIN WRINKLED. LOWER SKIN REPAIRED PER ECRA 471-53-246-2.Feb 22, 2005 · N471EV · Boeing 747273C · Fuselage Main, Plate/SkinSDR EIA2005021Spar · corrodedRT WING FWD T-CHORD CORRODED AT WSS 1336 FSSO 1349.0 LOWER T-CHORD. REPAIRED RIGHT WING FWD SPAR T-CHORD AT WS 1336 (FSSO 1349.0) LOWER CHORD PER ECRA 471-57-242-2.Feb 22, 2005 · N471EV · Boeing 747273C · Wing SparSDR EIA2005020Frame · crackedCRACK AT LOWER FRAME STR 25R, R5 DOOR STA 2231. INSTALLED NEW LOWER FRAME STA 2231 AT STR 25R PER B747 SRM 51-30-02 PG 8-9.Feb 22, 2005 · N471EV · Boeing 747273C · Fuselage Main, FrameSDR EIA2005019Spar · crackedLEFT WING, FWD SPAR, LWR CHORD HEAVY CORROSION AND CONFIRMED CRACK AT FSSO 1410. REPAIRED LEFT WING, FWD SPAR LOWER CHORD AND LOWER WING SKIN FROM FSSO 1370-1410 PER ECRA 471-57-247-2.Feb 22, 2005 · N471EV · Boeing 747273C · Wing SparSDR EIA2005018Frame · crackedCRACK INDICATION NOTED IN LWR FASTENER HOLES IN LTC-3 FRAME UPPER CLOSURE FITTING DURING OPEN HOLE HFEC INSPECTION. REAMED HOLE INSTALLED FREEZE PLUG IN LOWER HOLE AND INSTALLED FASTENER PER B747 SRM 51-10-08 PGS 1-11, 51-30-09 PGS 1-16, 20, 29, 30 AND BOEINGFeb 22, 2005 · N471EV · Boeing 747273C · Fuselage Main, FrameSDR EIA2005017Skin · delaminatedNR 2 SPOILER LOWER SURFACE SKIN DOUBLER DELAMINATED. COMPOSITE REPAIR MADE TO DELAMINATION ON PANEL EDGE NR 2 SPOILER PER B747 SRM 51-40-06 PG 13.Feb 22, 2005 · N471EV · Boeing 747273C · SpoilersSDR EIA2005016Stringer · crackedBETWEEN STA 300-320 STR 34 RT CRACK AT UPPER SURFACE. REMOVED DAMAGED SECTION BETWEEN STA 280-320 PER B747 SRM 53-10-03 PG 8-10. FABRICATED NEW STRINGER PER B747 SRM 53-10-03 PG 8, 51-30-02, 51-10-02 AND BSOPM 20-41-02 PG 7-9 NDT FOUND NO CRACKS. INSTALLED Feb 22, 2005 · N471EV · Boeing 747273C · Fuselage Main, Longeron/StringerSDR EIA2005015Frame · crackedCRACK INDICATION NOTED IN 4 EA FASTENER HOLES AT STA 800, STR 16L, FWD INNER FRAME CHORD. REMOVED EXISTING REPAIR PARTS, FABRICATED NEW STRAPS AND INSTALLED REQUIRED EXISTING AND FABRICATED STRAPS PER ECRA 471-53-230-2.Feb 22, 2005 · N471EV · Boeing 747273C · Fuselage Main, FrameSDR EIA2005014Frame · crackedMAIN CABIN INTERIOR, RT MAIN FRAME CRACK AT BS 360, BETWEEN STR 14 & 15. REMOVED AND REPLACED MAIN FRAME AT STA 360 RT MAIN CABIN PER ECRA 471-53-240-2 BETWEEN STR 13A TO 23 B747 SRM 51-30-02 PAGES 2, 3, 8 & 9.Feb 22, 2005 · N471EV · Boeing 747273C · Fuselage Main, FrameSDR EIA2005028Floorbeam · crackedBS 420 UPPER FLOORBEAM TOP CHORD AT RBL 57 AND OUTBOARD HAS NUMEROUS (5) FASTENER HOLES WITH CRACK INDICATIONS (RBL 57.75, 58.25, 63, 67.5, AND 89.5). REMOVED AND REPLACED STA 420 FLOORBEAM UPPER CHORD DUE TO NUMEROUS CRACK INDICATIONS PER SERVICE BULLETIN 74Feb 22, 2005 · N471EV · Boeing 747273C · Fuselage Main, Floor BeamSDR EIA2005013Skin · crackedRIGHT WING EXTERIOR, L/E NOSE IS CRACKED AT FASTENER HOLE 10 INCHES LONG AT WS 200.0. HOT BONDED METAL TO METAL REPAIR MADE TO RT WING L/E NOSE AT WS 200.0 PER ECRA 471-57-241-2 AND 747 SRM 51-40-06 PG 23.Feb 21, 2005 · N471EV · Boeing 747273C · Wing, Plate/SkinSDR EIA2005012Strap · crackedCRACK IN FRAME INNER STRAP AT STA 2231 LT FROM STR 25 TO STR 26 AT L-5 DOOR FWD FRAME. REMOVED STRUCTURE AS REQUIRED. FABRICATED REQUIRED PARTS AND INSTALLED FABRICATED STRAPS ALL PER ECRA 471-53-236-2P AND B747 SRM 53-10-04 PG 689-694.Feb 21, 2005 · N471EV · Boeing 747273C · Fuselage Main, FrameSDR EIA2005008Frame · crackedCRACK INDICATION IN LWR TWO FASTENER HOLES IN RT C-3 FRAME UPPER CLOSURE FITTING. REPAIRED RT C-3 FRAME UPPER CLOSURE FITTING PER ECRA 471-53-243-2.Feb 21, 2005 · N471EV · Boeing 747273C · Fuselage Main, FrameSDR EIA2005011Spar · corrodedRIGHT WING FWD SPAR AT WS 1485 LOWER T-CHORD CORRODED. REPAIRED THE RIGHT WING FWD SPAR WS 1485 PER ECRA 471-57-238-2P.Feb 21, 2005 · N471EV · Boeing 747273C · Wing SparSDR EIA2005010Doubler · damagedREMOVED EXTERNAL DOUBLER REPAIR NR 3 EXTERNAL FUSELAGE BS 2144-2164.5, STR 46R-48R. REMOVED EXTERNAL DOUBLER, FABRICATED REPAIR DOUBLERS AND FILLERS. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER PER B747 SRM 53-30-03 FIG 19.Feb 21, 2005 · N471EV · Boeing 747273C · Fuselage Main, Plate/SkinSDR EIA2005009Light · inoperativeUPPER DECK EMERGENCY LIGHT INOP. REPLACED INOP EMERGENCY LIGHT PER B747 MM 33-51-00.Feb 21, 2005 · N471EV · Boeing 747273C · Emergency LightingSDR EIA2005007Stringer · crackedSTR 22L CRACKED AT STA 303 UNDERNEATH STRINGER. REPAIRED CRACKED STRINGER AT 22L, STA 303 PER ECRA 471-53-248-2.Feb 21, 2005 · N471EV · Boeing 747273C · Fuselage Main, Longeron/StringerSDR 200500289Spar · corrodedDURING C-CHECK, FOUND CORROSION ON LEFT HAND WING LOWER FRONT SPAR CHORD. THE MAJOR REPAIR REQUIRED REPLACING 186 INCHES OF THE SPAR CHORD.Feb 13, 2005 · N471EV · Boeing 747273C · Wing SparSDR EIA2004034Radome · bird strikeJUST AFTER ROTATION AIRCRAFT FLEW THROUGH A FLOCK OF SEAGULLS, IMPACTING SOUNDS HEARD. ALL INSTRUMENT AND ENGINE PARAMETERS NORMAL. NO VISIBLE DAMAGE SEEN FROM CARGO COMPARTMENT. PERFORMED BIRD STRIKE INSPECTION IAW MM 05-51-14. FOUND RADOME DAMAGE BEYOND May 4, 2004 · N471EV · Boeing 747273C · Aerodynamic Fairings
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