Boeing 747-273C
Service difficulty reports · 647
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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.
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
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 99ZZZM706Strap · 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 R53-21-33659SDR EIAA98039Skin · elongated holesHKG - DURING 'C5/D' CHECK INSPECTION, NR 3 PYLON LEFT SKIN HAS ELONGATED HOLES AT NAS STATION 180. REPAIRED IAW SB 54-2034 FIG 5. (M)SDR EIAA98038Bulkhead Angle · crackedHKG - DURING 'C5/D' CHECK INSPECTION, NR 3 PYLON AFT ENGINE MOUNT BULKHEAD RADIUS ANGLES CRACKING, ADJACENT TO FRONT SPAR NAC STATION 221. REPAIRED IAW SRM 54-10-03 FIG 19. (M)SDR EIAA98037Seat Track · crackedHKG - DURNG 'C5/D' CHECK INSPECTION, SEAT TRACK FOUND CRACKED BS 701, RBL 11. REPAIRED IAW SRM 53-10-05 FIG 14. (M)SDR EIAA98035Brace · corrosionHKG - DURING 'C5/D' CHECK INSPECTION, NR 1 PYLON DIAGONAL BRACE UNDER WING FITTING HAS CORROSION UNDER BUSHING. REPAIRED IAW SB 57-2246. LUG BORE AFTER INSURANCE CUT 2.457 INCH. (M)SDR EIAA980318Web · corrodedHKG - DURING C5/D CHECK INSPECTION, FOUND CORROSION AT LEFT WING FRONT SPAR WEB AT FSS 998.3. TRIMMED CORROSION FROM WEB, INSTALLED DOUBLER, ANGLE AND FILLER PER HAECO R57-21-33650 AND ECRA 471-99-176-1. (M)SDR EIAA980140Fitting · corrodedDURING 'C5/D' CHECK INSPECTION, ALL PYLON WING UPPER LINK FITTING OUTER LUG FACES FOUND CORRODED. PYLON NR 1 AND NR 4, CORROSION BLENDED OUT. BUSHINGS FABRICATED AND INSTALLED IAW SB 54-2164 AND HAECO RS R57-04-33646. PYLON NR 2 AND NR 3, CORROSION BLENDED SDR EIAA980139Fitting · misalignedDURING 'C5/D' CHECK INSPECTION, NR 1, 2, 3 AND 4 PYLON DSB AND BACKUP FITTING HOLES DO NOT ALIGN. ALTERNATE HOLE LOCATIONS IAW SB AND HAECO RS R57-04-33642, R57-04-33631, R57-04-33632, AND R57-04-33633. (M)SDR EIAA98058Spar Web · corrodedHKG - DURING 'C5/D' CHECK INSPECTION, RT WING FRONT SPAR WEB AT WS 1454 HAS CORROSION. CORRODED WEB WAS TRIMMED OFF. REPAIRED BY INSTALLING REPAIR DOUBLER, ANGLE AND FILLED AS PER HAECO RS R57-21-38620. (M)SDR EIAA980114Keel Beam · corrodedHKG - DURING C5/D CHECK INSPECTION, KEEL BEAM LOWER PANEL SUPPORT STRUCTURE CORRODED AT BS 1383 LBL 16 - RBL 16. REPLACED 'T' SECTION IAW SRM 51-10-01. (M)SDR EIAA980112Web · corrodedHKG - DURING C5/D CHECK INSPECTION, CORROSINO AT BS 1242 RBL 35 AND WL 180 RT MLG W/W CANTED BULKHEAD WEB CUTOUT. REPAIRED BY TRIMMING WEB, INSTALLING REPAIR DOUBLER AND FILLER IAW HAECO RS R53-48-33673. (M)SDR EIAA98005Fan Blades · bentJFK - APPROACH INTO JFK RUNWAY 22L, APPROXIMATELY 50-100 FEET, HAD BIRD STRIKE IN NR 1 ENGINE. LANDED WITHOUT INCIDENT, WITH AN OUTSIDE AIR TEMP OF 42 DEGREES F. REMOVED AND REPLACED FIVE PAIRS OF FAN BLADES PER MM 72-31-02. INSPECTED NR 1 ENGINE FOR BIRD ISDR EIAA98033Frame · crackedHKG - DURING 'C5/D' CHECK INSPECTION, APU COMPARTMENT, VERTICAL FRAME CRACKED AT BS 2669 W/L 310 RT SIDE. REPAIRED IAW SRM 51-40-03 FIG 3. (M)SDR EIAA98032Panel · delaminatedHKG - DURING 'C5/D' CHECK INSPECTION, LEFT OUTBOARD AFT FLAP PANEL 588 JT DELAMINATED. REPAIRED IAW SRM 51-40-06 PARA 3 RS 57-51-33622. (M)SDR EIAA98031Tie Cap · crackedHKG - DURING 'C5/D' CHECK INSPECTION, LEFT WING WS 669.5 UPPER MOST FWD SHEAR TIE CAP CRACKED. SHEAR TIE CAP REPAIRED IAW SB 57-2273 FIG 8 AND 9. (M)SDR EIAA98030Bulkhead Ftg · crackedHKG - DURING 'C5/D' CHECK INSPECTION, LEFT WING WS 669.5 PYLON BULKHEAD SUPPORT FWD BACK UP FITTING CRACKED AT UPPER AREA ALONG FASTENERS AT STRING 24. BACK UP FITTING REPLACED IAW SB 54A 2159 FIG 25. (M)SDR EIAA98029Floorbeam · corrosionHKG - DURING 'C5/D' CHECK INSPECTION, FLOOR SUPPORT CORROSION BS 2340 AT ABL 32. FLOORBEAM AND FLOOR SUPPORT REPAIRED IAW SRM 51-40-4 FIG 1. (M)SDR EIAA98028Seat Track · corrosionHKG - DURING 'C5/D' CHECK INSPECTION, SEAT TRACK FLANGE FOUND CORROSION AND CRACK. SEAT TRACK REPAIRED IAW SRM 53-10-05 FIG 1A. (M)SDR EIAA98027Frame · crackedHKG - DURING 'C5/D' CHECK INSPECTION, COCKPIT BS 320 LEFT STRINGER 1 TO STRINGER 2, FRAME FOUND CRACKED. FRAME WEB REPLACED IAW SRM 51-10-01. (M)SDR EIAA98026Frame · crackedHKG - DURING 'C5/D' CHECK INSPECTION, L5 DOOR CUTOUT AT BS 2300 FRAME 01B AREA IS CRACKED AT STRINGER 22L-23L. FRAME WEB REPAIRED IAW SRM 53-10-04 FIG 3. (M)SDR EIAA98025Seat Track · corrosionHKG - DURING C5/D CHECK INSPECTION, BS 2060-1080 ABL 89 SEAT TRACK FLANGE UPPER AND LOWER SURFACES HAS CORROSION. SEAT TRACK REPAIRED IAW SRM 53-10-05 FIG 1A. (M)SDR EIAA98024Floorbeam · crackedHKG - DURING 'C5/D' CHECK INSPECTION, BS 1720 LBL 80 FLOORBEAM FOUND CORROSION AND CRACK. REPAIRED FLOORBEAM IAW SRM 53-10-07 FIG 12. (M)SDR EIAA98023Support · crackedHKG - DURING 'C5/D' CHECK INSPECTION, COCKPIT BS 287 FRAME TO STRINGER 2L ATTACH CHORD SUPPORT FOUND CRACKED. SUPPORT REPLACED IAW SRM 51-10-01. (M)SDR EIAA98022Angle · damagedHKG - DURING C5/D CHECK INSPECTION, NOSE CARGO DOOR BS 180 AT STRINGER 28A-R THE STRINGER TO FRAME ATTACH IS DAMAGED. ANGLE REPLACED IAW SRM 51-10-01. (M)SDR EIAA98021Bushing · wornHKG - DURING 'C5/D' CHECK INSPECTION, NR 1 PYLON FORWARD UPPER ENGINE MOUNT HANGERS MOUNT BUSHING WORN. BUSHINGS REPLACED IAW OHW 20-50-03. (M)SDR EIAA98020Fitting · corrosionHKG - DURING 'C5/D' CHECK INSPECTION, NR 4 PYLON UPPER SPAR FITTING CORROSION FOUND IN LUG BORE. REMOVED CORROSION IAW SB 54.2164 FIG 2. (M)SDR EIAA98019Fitting · corrosionHKG - DURING C5/D CHECK INSPECTION, NR 3 PYLON UPPER SPAR FITTING CORROSION FOUND IN LUG BORE. REMOVED CORROSION IAW SB 54.2164 FIG 2. (M)SDR EIAA98018Fitting · corrosionHKG - DURING C5/D CHECK INSPECTION, NR 2 PYLON UPPER SPAR FITTING CORROSION FOUND IN LUG BORE. REMOVED CORROSION IAW SB 54.2164 FIG 2. (M)SDR EIAA98017Fitting · corrosionHKG - DURING C5/D CHECK INSPECTION, NR 1 PYLON UPPER SPAR FITTING CORROSION FOUND IN LUG BORE. REMOVED CORROSION IAW SB 54.2164 FIG 2. (M)SDR EIAA98016Tie Down Track · brokenHKG - DURING C5/D CHECK INSPECTION, BS 1700-1720 LBL 33 TIE DOWN TRACK 01B FLANGE BROKEN. TIE DOWN TRACK REPAIRED IW SRM 53-10-05 FIG 16. (M)SDR EIAA98015Angle · crackedHKG - DURING C5/D CHECK INSPECTION, BS 1335 FRAME TO WHEEL WELL PRESSURE DECK SUPPORT ANGLE CRACKED. SUPPORT ANGLE REPLACED IAW SRM 51-10-01. (M)SDR EIAA98014Shear Tie · crackedHKG - DURING C5/D CHECK INSPECTION, AFT CARGO COMPARTMENT BS 1840 AT STRINGER 46L - 47L SHEAR TIE IS CRACKED. SHEAR TIE REPAIRED BY SRM 53-10-04 FIG 3. (M)SDR EIAA98013Frame · crackedHKG - DURING C5/D CHECK INSPECTION, UPPER DECK BS 380 FRAME CRACKED AT STRINGER 7L. FRAME REPAIRED IAW SRM 51-10-04 FIG 85. (M)SDR EIAA98012Angle · crackedHKG - DURING C5/D CHECK INSPECTION, UPPER DECK BS 380 STRINGER ANGLE CRACKED AT STRINGER 2L. ANGLE REPAIRED IAW SRM 51-10-01. (M)SDR EIAA98034Skin · crackedHKG - DURING 'C5/D' CHECK INSPECTION, FUSELAGE BS 340-400 STRINGER GL LAP SPLICE TOP ROW FASTENER HOLES, FOUND 27 HOLES CRACKED. REPAIRED SKIN LAP IAW SRM 53-30-03 FIG 26. (M)SDR EIAA980132Skin · crackedHKG - DURING 'C5/D' CHECK INSPECTION, LT SIDE BS 370 STR NR 6 SKIN CRACKED AT TWO TOP ROW COUNTERSUNK FASTENER HOLES OF THE LAP SPLICE, BOTH RUNNING FORWARD AND AFT APROXIMATELY .0624 INCH IN LENGTH. CUT OUT SKIN SLAP, REPAIRED IAW SRM 53-30-03 FIG 26. (X)SDR EIAA98011Angle · crackedHKG - DURING C5/D CHECK INSPECTION, BULK CARGO BS 1960 LBL 38 LONGITUDINAL FLOOR SUPPORT CRACKED. REPLACED FLOOR SUPPORT 'Z' ANGLE IAW SRM 51-40-03 FIG 2. (M)SDR EIAA98036Skin · crackedHKG - DURING 'C5/D' CHECK INSPECTION, RT BS 340-380 S6 LAP SPLICE TOP ROW FASTENER, FOUND THREE HOLES CRACKED ON UPPER SKIN. REPAIRED IAW EV - EO 53-747-1032-90 REV B AND BOEING DWG 65B28215 SHEET 1. (M)SDR EIAA980133Skin · crackedHKG - DURING 'C5/D' CHECK INSPECTION, RT SIDE BS 370 STR NR 6 SKIN CRACKED AT ONE TOP ROW COUNTERSUNK FASTENER HOLE OF LAP SPLICE APPROX .0625 INCH IN LENGTH RUNNING AFT. CUT OUT SKIN LAP, REPAIRED IAW EV EO 53-747-1032-90 REV B AND BOEING DWG 65B28215 SHEET SDR EIAA98010Bulkhead Angle · crackedHKG - DURING C5/D CHECK INSPECTION, FUSELAGE BS 400 BULKHEAD AFT FACE AT RBL 19 FLOOR SUPPORT ATTACH ANGLE CRACKED. ANGLE REPLACED IAW SRM 51-10-01. (M)SDR EIAA98009Bulkhead Angle · crackedHKG - DURING C5/D CHECK INSPECTION, FUSELAGE BS 400 BULKHEAD AFT FACE AT RBL 6 FLOOR SUPPORT ATTACH ANGLE CRACKED. ANGLE REPLACED IAW SRM 51-10-01. (M)SDR EIAA98008Bulkhead Angle · crackedHKG - DURING C5/D CHECK INSPECTION, FUSELAGE BS 400 BULKHEAD AFT FACE AT RBL 1 FLOOR SUPPORT ATTACH ANGLE CRACKED. ANGLE REPLACED IAW SRM 51-10-01. (M)SDR EIAA98007Web · dentedHKG - DURING C5/D CHECK INSPECTION, RT HORIZONTAL STAB INTERNAL WEB DENTED AT STATION 281.8 20 INCHES FORWARD OF AFT SPAR. INTERNAL RIB WEB REPAIR IAW SRM 55-10-06 FIG 4. (M)SDR EIAA98002Bpcu · contaminatedJFK - AFTER TAKEOFF NR 1 GENERATOR TRIPPED OFF, UPPER YAW DAMPER LIGHT CAME ON ABOUT SAME TIME WITH SPLIT RUDDER INDICATION, SSB OPENED AND NR 3 AND NR 4 BTB'S OPENED. RETURNED TO JFK LANDING NORMAL. REMOVED WATER FROM LOWER CARGO AREA. REMOVED AND REPLACED SDR EIAA970210Control Cable · out of adjJFK - RIGHT AILERON REQUIRES EXTRA PRESSURE FOR RIGHT TURNS. RIGGED AILERON LOST MOTION PER MM 27-11-00, OPS CHECK OK. (M)SDR EIAA970204Air Distribution · smokeYSSY - ONE HOUR OUT OF SYDNEY, THAT CAP AND FE SAW SLIGHT SMOKE COMING FROM THE LAV AREA, NOTHING COULD BE FOUND WRONG. VISUAL INSPECTION OF FLIGHT DECK AND LAV AREAS FOUND NO BURNED WIRES OR ELECTRICAL EQUIPMENT. ALL SYSTEMS OPERATIONALLY PUT ON LINE AND FUSDR EIAA970193Fan · failedHKG - LOG PAGE: F17424 - NR 1 RECIRCULATING FAN MAKING NOISE. FILLED COCKPIT WITH SMOKE. REMOVED AND REPLACED NR 1 RECIRCULATING FAN IAW MM 21-25-01, OPS NORMAL. (X)SDR EIAA970192Gearbox · failedPANC - DURING CRUISE AT FL330, NR 2 ENG OIL QTY BEGAN DROPPING, THEN FWD ANNUNCIATOR LOW OIL PRESSURE LIGHT FLICKERED, ENGINE WAS SHUT DOWN, OIL PRESSURE WAS 15 PSI, WITH N2 25 PERCENT, N1 29.5 PERCENT, OIL QTY READING ONE GALLON AFTER SHUTDOWN. ENGINE PARAMESDR EIAA970190Ceiling Panel · out of positionJFK - DURING TAXI OUT, FLT CONTROL CHECK UNABLE TO MOVE AILERONS WITH CONTROL YOKE. RETURNED TO BLOCKS. FOUND CEILING PANEL AT STATION 240 PALLET POSITION NR 1 IMPACTED, INSPECTED AREA FOR INTEGRITY, FOUND OK. FOUND CEILING MATERIAL RUBBING AGAINST 1ST OFFISDR EIAA970188Fairing · crackedYSSY - WING TO BODY FAIRING DAMAGED BEHIND RIGHT BODY GEAR FROM NR 5 TIRE TREAD SEPARATION. REPAIRED AS PER SRM 53-50-02. PERMANENT REPAIR NEXT A CHECK 8/18/97. (M)
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