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 = 'DC6A' 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 = 'DC6A' 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 FXGA201302211306Skin · crackedRE-ENFORCING RING, SKIN & DOUBLER CRACKED AT CTR WING SECTION. CRACKS WERE FOUND IN THE WING SKIN, STATION 60 TO 60 DOUBLER & RE ENFORCING RING FOR PANEL PN 3479163, DOOR, CTR WING FUSELAGE FRAME CUT OUT, IN THE CTR WING SECTION OF THE AIRPLANE. THE CRACK ISDR FXGA201302201305Access Panel · crackedCRACK IDENTIFIED ON NR 1 ALT FUEL TANK ACCESS DOOR DOUBLER. REPLACE DOOR DOUBLER EO 1305.SDR FXGA201212071292Floor Support · corrodedCORRODED FLOOR SUPPORT BETWEEN BS 630 & 791L. R & R FLOOR SUPPORT.SDR FXGA201210051279Structure · crackedNR 4 ENGINE AIRFOIL ANTI-ICE HEATER EXHAUST OPENING CRACKING. REPAIR OF CRACKING AROUND AIRFOIL ANTI-ICE HEATER EXHAUST DUCT ON NR 4 ENG EO 1279.SDR FXGA201208301267Structure · corrodedHEATER COMPARTMENT CORRODED BS 500 - 541. REPAIRED IAW EO 1267.SDR FXGA20120313007Skin · crackedDURING HEAVY MX FOUND CRACKED WING SKIN AT WING STATION 70L BETWEEN STRINGERS 1 AND 2. AND ANOTHER CRACK AT WING STATION 70L AT STRINGER 5.SDR FXGA20120313006Frame · crackedDURING HEAVY MX, FOUND CRACKED FUSELAGE FRAME AT FUSELAGE STA 1053 BETWEEN STRINGERS 12L AND 14L.SDR FXGA20120313005Doubler · crackedDURING HEAVY MX, FOUND CRACKED LANDING DOUBLER FOR PANEL 145 BETWEEN STRINGERS 23R AND 25R AT WING STATION 259.5R.SDR FXGA20120313004Skin · crackedDURING HEAVY MX, FOUND CRACKED LOWER WING SKIN AT CENTER SPAR AFT FLANGE WING STA 211L.SDR FXGA20120313003Skin · corrodedDURING HEAVY MX, FOUND CORRODED FUSELAGE SKIN AND DOUBLER AT FUSELAGE BS 1030 BETWEEN STR 2L AND 2R.SDR FXGA20120313002Skin · corrodedDURING HEAVY MX FOUND CORRODED WING SKIN AND CENTER WING SPAR AT WING STATION 179L OF THE UPPER WING SURFACE.SDR FXGA20120313001Skin · corrodedDURING HEAVY MX FOUND CORRODED SKIN LAP AT FUSELAGE STA 724, STRINGER 13R.SDR FXGAN9056R2Skin · corrodedFOUND SKIN CORROSION FUS STA 157 AT STR 31L. REPAIRED IAW EAC EO 1133 AND 8110-3 DATED 1-19-05.SDR FXGAN9056R8Skin · corrodedSKIN CORROSION DISCOVERED AT FUS STA 780 CENTERED UNDER FUS STR 32L. REPAIRED IAW EAC EO 11321 AND 8110-3 DATED 9/29/2011.SDR FXGAN9056R7Structure · corrodedCORROSION DISCOVERED ON THE CABIN FLOOR FROM STA 625 TO FUS STA 661. REPAIRED IAW EAC EO 1129 AND 8110-3 DATED9/27/2011.SDR FXGAN9056R6Stringer · corrodedCORROSION FOUND ON FUS STR 32L AT FUS 780. REPAIRED IAW WITH EAC EO 1131 AND 8110-3 DATED 9/29/2011.SDR FXGA20111003005Skin · dentedRT WING HAD A LARGE DENT FROM STA 655 TP 675. REPAIRED IAW EO 1128 AND 8110-3 DATED 9-29-2011.SDR FXGA20111003002Floor Skin · corrodedFOUND CORRODED FLOOR SKIN AT FUS STA 120. REPAIRED IAW EAC EO 1135 AND 8110-3 DATED 9-20-11.SDR FXGA20111003001Skin · corrodedFOUND SKIN CORROSION AT FUS STA 157 BETWEEN STR 33L AND 33R. REPAIRED IAW EAC EO 1134 AND 8110-3 DATED 9-20-2011.SDR FXGAN9056R1Skin · corrodedFUSELAGE SKIN FOUND CORRODED FUS STA 89 TO STA 111 BETWEEN STR 10L AND 13L. REPAIRED IAW EAC EO 1130 AND AND 8110-3 DATED 9/15/2011.SDR FXGAN6174CMaster Rod · brokenNR 4 ENGINE SHUTDOWN DUE TO FIRE WARNING INDICATION. FIRE EXTINGUISHED AND AIRCRAFT LANDED WITHOUT INCIDENT. NR 9 CYL WALL RUPTURED DUE TO BROKEN MASTER ROD CAUSING AN OIL FIRE. ENGINE QEC ASSEMBLY REPLACED NO DAMAGE TO THE AIRFRAME.SDR FXGA20110217003Stringer · crackedDISCOVERED CRACKED STRINGER 23L AT WING STA 90L. REPAIRED IAW EAC EO 1105 AND 8110-3 DATED 2/12/11.SDR FXGA20110217002Stringer · crackedRIGHT WING STRINGER CRACKED AT WS 90R. REPAIRED IAW EAC EO 1104 AND 8110-3 DATED 2/12/11.SDR FXGA20110217001Spar · crackedTHE CENTER SPAR WEB WAS FOUND CRACKED AT W/S 90R. REPAIRED PER EAC EO 1103 AND 8110-3 DATED 2/12/11SDR FXGA74CHeater · crackedSHUTDOWN CABIN HEATER DUE TO POSSIBLE CO2 LEAK. REPLACED CABIN HEATER IAW AB LMM 27-55 PARA 2. OPS AND LEAK CHECK GOOD.SDR FXGA9056RStructure · corrodedDEEP CORROSION FOUND AT MULTIPLE NUT PLATE HOLES ALONG THE NR 2 NACELLE FILLET FAIRING BETWEEN THE FRONT AND CENTER SPAR. REPAIRED PER EAC EO 1044 AND 8110-3 DATED 8/20/10.SDR CA090813007Cylinder · crackedIN CRUISE, LEANING OF NR 2 ENG CAUSED BACKFIRING AND A BMEP DROP. ONCE INVESTIGATED NR 2 CYLINDER ON NR 2 ENG FOUND TO HAVE A CRACKED EXHAUST EAR.SDR 2008F00013Trim Tab · bindingAILERONS BINDING ON TAKEOFF AFTER GEAR RETRACTION (BEFORE TAKEOFF CONTROL CHECK) NORMAL. FOUND THAT THE AILERON SPRING TAB MECHANISM WAS BINDING PREVENTING MOVEMENT OF THE TAB SYSTEM WHICH IN TURN INCREASED THE FORCES REQUIRED TO MOVE THE AILERONS.SDR NACA20080002Oil System · low pressureNR 1 ENGINE SHUT DOWN DUE TO NO OIL PRESSURE. REMOVED AND REPLACED ENGINE DUE TO INTERNAL FAILURE, REF: NAC DC6MM SEC V PG 3.SDR NACA20080001Pump · power lossNR 3 ENGINE SHUT DOWN DUE TO LOSS OF BMEP. INSPECTION REVEALED FRONT OIL PUMP DRIVE FAILURE. REPLACED NR 3 ENGINE, REF: NAC DC6MM SECT V PG 3, 4 AND 5. CHECKED GOOD ON RUN-UP.SDR NACA20070020Cylinder · crackedNR 2 ENGINE SHUT DOWN DUE TO RUNNING ROUGH. REPLACED NR 18 CYLINDER DUE TO CRACKED HEAD. REF: NAC DC-6 MM SECT V PG 16 AND 16A.SDR NACA20070018Bolt · shearedLANDING GEAR UNSAFE CONDITION IN NEUTRAL. FOUND RIGHT UPLATCH SHEAR BOLT SHEARED. REPLACED BOLT AND PERFORMED GEAR SWING PER NAC PURDUE MB6-0-1. OPS CHECKED GOOD.SDR NACA20070013Cylinder Head · crackedNR 2 ENGINE FIRE ON TAXI. ENGINE SHUT DOWN LT BANK CO2 BOTTLES DISCHARGED. CREW ALSO DISCHARGED MAIN CABIN ABC, COCKPIT AND CABIN HALON BOTTLES TO EXTINGUISH FIRE. NR 2 ENGINE REPLACED AND SENT TO SHOP FOR INSPECTION: FIRE RESULTED FROM THE NR 9 CYLINDER CRSDR NACA20070007Bungee · brokenLEFT MAIN GEAR LIGHT DID NOT ILLUMINATE ON LANDING. RED TRANSIT LIGHT WAS ON. MADE VISUAL INSPECTION FROM CAPTAINS WINDOW AND A LOW PASS FOR MAINTENANCE TO INSPECT. FOUND INBD BUNGEE/SPRING BROKEN, REPLACED. LMLG DOOR SLIDER ROD BENT, REPLACED ROD AND RIGGSDR NACA20070002Cylinder · crackedNR 2 ENGINE SHUT DOWN DUE TO LOW COMPRESSION INDICATION ON NR 4 CYLINDER. REPLACED NR 4 CYLINDER DUE TO A CRACKED HEAD PER NAC DC-6MM SECT V PG 16 AND 16A. OP AND LEAK CHECKED GOOD.SDR NACA20060054Cylinder · crackedNR 4 ENGINE SHUT DOWN DUE TO BACKFIRING. REPLACED NR 16 CYLINDER DUE TO CRACKED HEAD, REF: NAC DC-6 MM TASK CARD V PG 16 AND 16A. GROUND RUN CHECK GOOD, NO LEAKS NOTED.SDR NACA20060051Cylinder · failedNR 1 ENGINE SHUTDOWN DUE TO DOUBLE SHORTED SECONDARY ON NR 1 CYLINDER.REPLACED NR 1 CYLINDER DUE TO RINGLAND FAILURE.SDR NACA20060048Engine · failedNR 4 ENGINE RAPID OIL LOSS ON DEPARTURE. REPLACED NR 4 ENGINE DUE TO INTERNAL FAILURE. REF: NAC DC-6MM SEC V PG 1-9.SDR NACA20060042Cylinder Head · separatedNR 4 ENGINE SHUTDOWN DUE TO BACK FIRING. REPLACED NR 2 CYLINDER DUE TO A BLOWN HEAD. REF: NAC DC-6MM SEC. V. PG.16-16A.SDR NACA20060045Stringer · crackedLT WING STRINGER CRACKED AT STA. 194. REPAIRED LT WING LOWER STRINGER 22 SPLICE, WING STA. 194. REF; NAC DRAWING: NAC2006-06 REV: 1R DATED 7 JULY 2006.SDR NACA20060044Skin · crackedLT HAND WING LOWER SKIN STA. 210, STR. 22 WING SKIN CRACKED AFT OF CENTER SPAR. REPAIRED LT WING LOWER SKIN STA. 213, STR. 22 REF: NAC DRAWING: NAC2006-05 REV: 1R DATED 12 JULY 2006.SDR NACA20060036Unknown · out of adjustNR 1, 2, 3, & 4 ENGINES FUEL FLOW 500 PPH, NO DERICHMENT OR ENRICHMENT. DETERMINED MIXTURE NOT ENGAGED TO FULL RICH POSITION FOR TAKEOFF. A 30" GROUND RUN CHECKED GOOD PER NAC DC-6MM SECT IV PG EC01.1 & EC01.2.SDR NACA20060035Cylinder · crackedNR 2 ENGINE FEATHERED DUE TO BACKFIRING. SUSPECT NR 4 CYLINDER. REPLACED NR 4 CYLINDER PER NAC DC-6MM SEC V PG 16-16A. OPERATIONAL CHECK AND LEAK CHECK GOOD.SDR NACA20060034Skin · puncturedTOP LEFT HAND WING STA 286 HAS PUNCTURE IN WING SKIN LEAKING FUEL. THE DAMAGED AREA WAS REMOVED, EXAMINED USING NDT, AND AN EXTERNAL DOUBLER INSTALLED PER FAA DER DRAWING NAC2006-02, DATED 29 MARCH 2006 AND FAA 8110-3, DATED 29 MARCH 2006.SDR NACA20060031Valve Seat · failedNR 3 ENGINE SHUT DOWN AT CRUISE FLIGHT DUE TO BACKFIRE. REPLACED NR 11 CYLINDER DUE TO EXHAUST VALVE SEAT FAILURE. PER REF: NAC DC-6MM SEC V PG 16 & 16A.SDR NACA20060013Ring · failedNR 2 ENGINE SHUT DOWN DUE TO BACKFIRING AT CRUISE, LOW COMPRESSION INDICATION ON NR 6 CYLINDER. REPLACED NR 6 CYLINDER DUE TO RING LAND FAILURE, PER NAC DC-6MM SEC V PG 16 & 16A. OPERATIONAL CHECK GOOD.SDR NACA20060010Floor Support · corrodedRIGHT CENTER FLOORBEAM BOTTOM CORRODED AT STATION 282-298. REMOVED DAMAGE AND INSTALLED REPAIR PER DER DRAWING NAC2006-01, IR & FAA 8110-3, DATED 2 FEBRUARY 2006. REPAIRED FLOOR SUPPORT BETWEEN STA 282-306. MANUFACTURED AND INSTALLED ANGLE PER ITEM 12 WITH SDR CA060126006Attach Fitting · cracked(CAN) DURING ANNUAL INSPECTION, AD 89-11-07 WAS BEING ACCOMPLISHED. THE LT IB MLG ATTACH FITTING WAS FOUND TO BE CRACKED BETWEEN THE 4TH AND 5TH FASTENER HOLES ON THE OB VERTICAL LEG. THERE WERE 2 CRACKS NOTED. THE LENGTH OF THE CRACK RUNNING BETWEEN THE 2 FASSDR NACA20060005Heater · leakingSUSPECT CABIN HEATER EXHAUST FUMES IN COCKPIT.REPLACED CABIN HEATER ASSEMBLY. LEAK AND OP CHECKED GOOD. REF: NAC MM. SEC. VII. PAGE 81 AND 82.SDR NACA20060004Carburetor · icedNR 4 ENGINE LOW BMEP AND LOW RPM. PERFORMED 30 INCH BAROMETRIC RUN PER NAC DC-6 OPS MANUAL SECT 9.200 DETERMINED CARB ICE TO BE PRESENT. RAN ENGINE TO GREEN RPM, ENGAGED CARB HEAT UNTIL IN GREEN RANGE. CLEANED ICE FROM CARBURETOR , RAN TO 30 INCH, OP CHECKE
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