Boeing 747-412
Service difficulty reports · 332
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 = '747412' 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.
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 = '747412' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR KCSA201712201090Skin · corrodedINTERNAL TO FUSELAGE, STATION 1475 BETWEEN STRINGER 16 L AND 17 L ON FUSELAGE SKIN, EVIDENCE OF CORROSION.SDR KCSA201712201089Skin · corrodedINTERNAL FUSELAGE SKIN, STATION 1475 BELOW STRINGER 15 RIGHT SIDE, EVIDENCE OF CORROSION.SDR WRNA201511280001Engine · shutdownDEPARTING NR 1 ENG LOST POWER, ALL OF ITS PARAMETERS DISPLAYED IDLE ON ECIAS. POWER RECOVERED IMMEDIATELY, MINUTES LATER SAME ENGINE LOST POWER AGAIN DURING CLIMB OUT. ALL ENGINE DISPLAYED IDLE ON ECIAS BUT THIS TIME POWER WAS NOT RECOVERED. ENGINE CHECKLISSDR Q2SA20140701207Bottle · dischargedWHILE CLOSING THE RIGHT UPPER DECK DOOR, THE DOOR ASSIST BOTTLE DISCHARGED AT A POINT WHEN THE DOOR WAS APPROX. 6-10 INCHES FROM BEING FULLY CLOSED. SLIDE DID NOT DEPLOY AND NO DAMAGE WAS NOTED. R & R RT UPPER DECK DOOR ASSIST BOTTLE IAW AMM 52-23-13. OPS CSDR Q2SA20140626206Structure · damagedDURING WALK AROUND INSPECTION, FOUND AFT CARGO DOOR LOWER AFT CORNER DAMAGED. REPAIRED IAW EO MTM-140628 REV -IR.SDR EPHR20140120004Skin · puncturedRT WING IB MID FLAP LEADING EDGE SKIN UPPER SURFACE PUNCTURED AT WBL 329. REPAIRED IAW SRM 51-70-06.SDR EPHR20140120003Skin · damagedRIGHT WING OTBD AFT FLAP HAS A SMALL AREA OF DAMAGE ON THE T/E OF THE T/E WEDGE AT APPROX WS 950. THE DAMAGE IS REPAIRED IAW SRM 51-70-06. PROJECT 743WA-305, NRI 3281.SDR EPHR20140120002Skin · gougedRIGHT WING OTBD AFT FLAP UPPER SURFACE HAS THREE SMALL AREAS OF DAMAGE, ON THE OTBD FWD EDGE BAND OF THE UPPER SKIN PANEL BETWEEN WBL 770 AND 808 WS 1141 TO 1178. THE DAMAGE AT ALL AREAS IS OUT OF SRM 57-53-01, FIG 101, DETAIL II DUE TO PROXIMITY TO FASTENER HSDR EIAA20130805013Sill · corrodedCORROSION AT MCD LOWER SILL AT NR 10 LATCH PIN FITTING. REMOVED CORROSION BLENDED OUT OF LIMITS. NDT AREA. CUT OUT AFFECTED WEB AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW RESPONSE KAC-EVR-13-0001-01C AND DWG 65B17670.SDR EIAA20130730012Skin · damagedSKIN DAMAGE AT BS 2742 BETWEEN LBL 11 AND RBL 6 ON BOTTOM OF TAIL CONE WHERE APU DOORS MEET. REMOVED DAMAGE. FABRICATED REPAIR PARTS AND INSTALLED IAW DWG 53801302-1.SDR EIAA20130730011Skin · chafedFUSELAGE SKIN CHAFED AT BS 2704-2705 BL 0 INSIDE APU COMPARTMENT. REMOVED DAMAGE. FABRICATED REPAIR PARTS AND INSTALLED IAW DWG 53301313-1 AND SRM 51-40-02.SDR EIAA20130730010Flange · wornNR 3 ENGINE NOSE COWL AFT FLANGE HAS WEAR MARK FROM FAN COWL AT 11:00 POSITION. FABRICATED REPAIR STRAP AND INSTALLED IAW DWG 54101306-1 AND SRM 51-70-10, PG 254-255, PAR 20-21.SDR EIAA20130729008Bullnose · dentedNR 9 L/E FLAP BULLNOSE HAS OUT OF LIMITS DENT APPR. 12" FROM OTBD EDGE. CUT OUT DAMAGE, FABBED REPAIR PARTS AND INSTALLED IAW SRM 57-43-02, FIG 201.SDR EIAA20130729007Fitting · brokenAPU VERTICAL SUPPORT TUBE FITTING IS BROKEN BETWEEN BS 2701.51 AND 2709.39, STR 0. REMOVED BROKEN FITTING, LOCATED DRILLED AND INSTALLED NEW FITTING AND 2EA INTERCOSTALS IAW SRM 51-40-05 AND AMM 49-13-04.SDR EIAA20130710005Skin · crackedBS 2373 S15L FUSALAGE SKIN CRACKED. CUT OUT DAMAGE FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW SRM 53-00-01, FIG 201.SDR Q2SA201306140006Cylinder · nickedINTERNAL SURFACE OF NLG OUTER CYLINDER NICKED.SDR Q2S2013F00005Skin · mismanufacturedFOUND EXISTING FASTENER HOLES HAVE A SHORT EDGE MARGIN. 8EA, STA 398, S44L-S46L.SDR Q2S2013F00004Structure · misrepairedFOUND THE DIMENSION OF DOUBLER PN 65B23284-9 AND PN 65B23284-11 IS SMALLER THAN REQUIRED.SDR Q2S2013F00003Structure · misrepairedFOUND THE DIMENSION OF DOUBLER, PN 65B23284-9 AND 65B23284-11 IS SMALLER THAN REQUIRED.SDR Q2S2013F00002Skin Panel · crackedNOSE WHEEL WELL LT AFT CORNER SKIN PANEL CRACKED, L=1-2", STA 400.SDR Q2S2013F00000Doubler · crackedTHE FUSELAGE LEFT TAIL SECTION UPPER LOBE DOUBLER CRACKED, STA 2521.5, L=08".SDR Q2SA20130224201Fairing · damagedON POSTFLIGHT WALKAROUND FOUND DAMAGE ON BODY FAIRING 191 B. REMOVED AND REPLACED PANEL 191 B WING TO BODY FAIRING IAW B-747 AMM 53-51-01. REPLACEMENT PANEL INSPECTED IAW B-747 SRM 51-10-06, NO DEFECTS NOTED.SDR Q2SA20121220200Unknown · odorODOR OF OIL FUMES IN COCKPIT WITH NR 1 PACK ON. COMPLIED WITH SMOKE OR FUMES ON CABIN CONDITIONAL INSPECTION AMM 05-51-56 NO OIL LEAKS NOTED. ACCOMPLISHED AIR CONDITIONING SYS OIL SMOKE/FUME CONTAMINATION REMOVAL IAW B747 AMM 21-00-01 PG 201, OPS CHECKED GOOSDR EIAA20120203011Sequence Valve · out of rigON DEPARTURE FROM JFK LANDING GEAR UP RT WING GEAR DID NOT RETRACT. AFTER CYCLED GEAR OP'S NORMAL. ITEM PLACED ON DMI AND FERRIED TO MZJ FOR MAINTENANCE. RIGGED DOOR SEQUENCE VALVE PER B747 AMM 32-12-00. NO OTHER RIGGING FAULTS FOUND. PERFORMED GEAR SWINGSDR EIAA20120203010Landing Gear · lack of lubeCREW REPORTED THAT AFTER TAKEOFF FROM BRU RT WLG DID NOT RETRACT, CREW PERFORMED ABNORMAL PROCEDURES, RT WLG RETRACTED. GREASED RT WING GEAR AS PER MM 12-21-00 REF WORK CARD 2127006 MOBIL GREASE 33.SDR EIAA2011245Floorbeam · corrodedCORROSION ON FLOORBEAM CAP AT NUT PLATE BS 2220 LBL 60. REMOVED CORROSION, REMOVED AND REPLACED SECTION OF FLOORBEAM AT BS 2220 LBL 60 PER 747-400 SRM 51-70-12 FIG 201 REPAIR 1.SDR EIAA2011244Floorbeam · corrodedCORROSION ON FLOORBEAM AT BS 2140 LBL 72. REMOVED CORROSION, FABBED AND INSTALLED REPAIR PER 747-400 SRM 51-70-12 FIG 201.SDR EIAA2011243Floorbeam · corrodedFLOORBEAM BS 2240 LBL 72 HAS CORROSION. REMOVED CORROSION AND INSTALLED REPAIR PER B747-400 SRM 51-70-12 PAGES 201-202.SDR EIAA2011242Floorbeam · damagedBS 840 BL 0 FWD CARGO PIT FLOORBEAM DAMAGED. REMOVED DAMAGED SECTION, FABBED REPAIR PARTS AND INSTALLED PER B747-400 SRM 51-70-12 PAGES 201-206.SDR EIAA2011103Smoke Warning · false activationMD CARGO 3 LP B STATUS MESSAGE ON LOWER EICAS. CARRIED OUT MAIN DECK C/C SMOKE DETECTION SYSTEM GROUND TEST THROUGH CMC IAW MM 26-14-00. OPS CHECK OK. CLEARED MESSAGE.SDR EIAA2011102Warning System · malfunctionedMD CARGO 5 LP A STATUS MESSAGE ON LOWER EICAS. CARRIED OUT MAIN DECK C/C SMOKE DETECTION SYSTEM GROUND TEST THROUGH CMC IAW CH 26-14-00 OPS CHECK OK CLEARED MESSAGE.SDR AU000197Valve · failed(AUS) INBOARD NR 3 FUEL TANK OVERRIDE/JETTISON PUMP INLET CHECK VALVEFLAPPER SEPARATED CAUSING DAMAGE TO THE PUMP. METAL IN NO3 ENGINE FUEL FILTER.
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