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 FXGA2026FA0000411Skin · corrodedCORROSION WAS NOTED ON FUSELAGE PLATING @ L/H OVERWING EMERGENCY EXIT DOOR FRAME, LOWER AFT CORNER. REPAIRED PER EO 2608SDR FXGA2026FA0000410Flange · crackedCRACK INDICATION NR 3 TANK 182C FLANGE, REPAIRED PER EO 2609SDR FXGA2026FA0000409Doubler · corrodedR/H SPAR NEEDS REPAIR DOUBLER AT STA 167 REPLACED DUE TO CORROSION AT MAX LIMIT.SDR FXGA202212232233None · noneCRACKED TANG ON FRONT SPAR UPPER CAP. TO REPAIR A CRACKED TANG ON THE FORWARD EDGE OF THE FRONT SPAR UPPER CAP. USE THIS EO IN CONJUNCTION WITH STS EA 81-2022-151.SDR FXGA202110072132Skin · crackedCRACKED R/H HORIZONTAL STABILIZER LEADING EDGE AT STATION 109. TO REPAIR A CRACK LEADING EDGE SKIN ON THE R/H HORIZONTAL STABILIZER AT STATION 109. STOP DRILL CRACK AND REPAIR LEADING EDGE PER DC-6 A&B OVERHAUL MANUAL FIGURED 15-31 SHEET 2 OF 2.SDR FXGA20200813001Line · leakingDURING APPROACH, HYDRAULIC PRESSURE AND QUANTITY WENT TO ZERO. DIVERTED. MAINTENANCE FOUND THE NR 3 ENGINE DRIVEN HYD PUMP HYDRALIC PRESSURE LINE LEAKING FROM HOSE FAILURE UNDER PROTECTIVE HOSE COVERING. NO EXTERNAL DAMAGE EVIDENT ON LINE ASSEMBLY,SDR FXGA201909261976Angle · bentFORWARD PRESSURE BULKHEAD BEAM REPAIR. TO REPAIR A BENT ANGLE ON THE FORWARD PRESSURE BULKHEAD, ON THE WHEEL WELL SIDE. AT F/STA 0. REPAIR RT END OF LOWER HORIZONTAL BEAM OF FORWARD PRESSURE BULKHEAD PER A&B OVERHAUL MANUAL FIGURE 12-5.SDR FXGA201908281969Fitting · corrodedREPLACEMENT OF CORRODED FITTING AT STRINGER 17 W/STA 60L OUTBOARD. TO REPLACE CORRODED FITTINGS ON STRINGER 17L, OUTBOARD OF W/STA 60L. ON WING STRINGER 20L, REMOVE OUTBOARD STATION 60L STRINGER FITTINGS AND REPLACE WITH A NEW ONE.SDR FXGA201908281970Tee Fitting · corrodedREPLACEMENT OF TEE ANGLE AT L/H OUTER WING AT W/STA 421. AFTER REMOVAL OF THE L/H OUTER WING THE CENTER SPAR TEE ANGLE (W/STA 421) WAS FOUND CORRODED. ON L/H OUTER WING, REMOVE CENTER SPAR TEE ANGLE AT W/STA 421.SDR FXGA2019082820191Tee Fitting · corrodedREPLACEMENT OF TEE ANGLE AT L/H OUTER WING AT W/STA 421. AFTER REMOVAL OF THE L/H OUTER WING THE CENTER SPAR TEE ANGLE (W/STA 421) WAS FOUND CORRODED. ON L/H OUTER WING, REMOVE CENTER SPAR TEE ANGLE AT W/STA 421.SDR FXGA201908261967Skin · crackedMULTIPLE WING SKIN CRACKS AT W/STA 168R BETWEEN STRINGERS 6 AND 11. MULTIPLE SMALL CRACKS WERE FOUND ON THE UPPER WING SKIN IN THE HELL HOLE AREA AROUND W/STA 168R BETWEEN STRINGERS 6 AND 11. GAIN ACCESS TO THE REPAIR AREA BY REMOVING A SECTION OF NACELLE, RSDR FXGA201908161966Skin · corrodedFUSELAGE SKIN CORRODED AT LOWER EDGE OF MAIN CARGO DOOR. TO REPAIR CORRODED FUSELAGE SKIN AT LOWER EDGE OF MAIN CARGO DOOR BETWEEN F/STA 768 AND 790. CUT-OUT DAMAGE AND REPAIR SKIN PER EAC EO 0502.SDR FXGA2019081261963Stringer · crackedNR 4 NACELLE STRINGER AND SKIN SPLICE. TO SPLICE NR 4 NACELLE STRINGERS NR 1 AT STATION 436 AND STRINGER 32 AT STATION 432.5. THE NACELLE SKIN WILL BE SPLICED AT STRINGER 2 BETWEEN STATION 400 AND 473. NUMEROUS REPAIRS WERE PREVIOUSLY INSTALLED ON THE UPPERSDR FXGA201908061964Stringer Splice · corrodedFUSELAGE STRINGER SPLICES ON STRINGER 32L BETWEEN F/STA 625 AND 638, STRINGER REPAIRED IAW A&B OVERHAUL MANUAL FIGURE 12-2.SDR FXGA201908051958Spar Web · corrodedCORRODED REAR SPAR WEB AT W/STA 359L. TO REPAIR A CORRODED REAR SPAR WEB AT W/STA 359L. CUT OUT CORRODED AREA AND REPAIR PER DC-6 A&B OVERHAUL MANUAL FIGURE 13-5.SDR FXGA2019080521957Spar · crackedCRACKED OUTER WING CENTER SPAR WEB AT W/STA 435L. TO REPAIR A CRACKED OUTER WING CENTER SPAR WEB AT W/STA 435L. PERFORM OUTER WING CENTER SPAR WEB REPAIR PER DC-6 A&B OVERHAUL MANUAL FIGURE 13-7.SDR FXGA2019080541956Skin · corrodedFUSELAGE SKIN REPLACEMENT AND STRINGER REPAIRS BEHIND CABIN HEATER EXHAUST. TO REPLACE A CORRODED FUSELAGE SKIN FROM F/STA 596 TO 662; REPAIR CORRODED STRINGER #31L BETWEEN F/STA 629 AND 658, AND STRINGER 32L BETWEEN F/STA 629 AND 651. REMOVE AND REPLACE CORSDR FXGA2019080591954Skin · corrodedFUSELAGE SKIN CORRODED AT F/STA 801 STRINGER 8L. TO REPAIR CORRODED FUSELAGE SKIN LAP AFT OF THE MAIN CARGO DOOR AT F/STA 801 STRINGER 8L. CUT-OUT DAMAGE AND REPAIR SKIN PER EAC EO 0502.SDR FXGA2019080710001Landing Gear · malfunctionedDIVERTED AFTER MULTIPLE GEAR DOWN ATTEMPTS WITH NO DOWN AND LOCKED INDICATION ON RIGHT MAIN. AT FAI THERE WAS NO DOWN AND LOCKED INDICATION ON RITGHT MAIN UNTIL 500" AGL DURING ILS APPROACH. , FO SAW GEAR DOWN BUT NO CLEAR DOWN AND LOCKED SIGHTING.SDR FXGA201907091953Skin · corrodedFUSELAGE SKIN CORRODED ABOVE FORWARD BAG PIT DOOR. TO REPAIR CORRODED FUSELAGE SKIN ABOVE FORWARD BAG PIT DOOR, AT F/STA 162 BETWEEN STRINGER 23R & 24R. CUT-OUT DAMAGE AND REPAIR SKIN PER EAC EO 0502.SDR FXGA201906281950Rib · crackedLEADING EDGE RIB CAP REPAIR AT W/STA 184R. TO REPAIR A CRACKED LEADING EDGE RIB TEE CAP AT W/STA 184R. CUT CRACKED TEE CAP ANGLE IN A SUITABLE LOCATION FORWARD OF THE SWING PANEL HINGE. MANUFACTURE NEW TEE ANGLE AND SPLICE ANGLES PER DRAWING # 1950-01.SDR FXGA201909051942Skin · corrodedCORRODED FUSELAGE SKIN REPAIRS AROUND MULTIPLE CABIN WINDOWS. TO REPAIR CORRODED FUSELAGE SKIN AROUND CABIN WINDOWS AT THE FOLLOWING LOCATIONS: F/STA 285 LEFT SIDE, F/STA 770 LEFT SIDE, F/STA 790 RIGHT SIDE AND F/STA 930 RIGHT SIDE. THE FUSELAGE SKIN IS CORRSDR FXGA201905171943Doubler · crackedNR 2 ALT ACCESS DOOR DOUBLER REPLACEMENT. TO REPLACE A CRACKED ACCESS DOOR DOUBLER AT NR 2 ATLERNATE TANK. REMOVE AND REPLACE NR 2 ALTERNATE TANK ACCESS DOOR DOUBLER PER SERVICE BULLETIN #842.SDR FXGA201905141940Skin · corrodedCORRODED FUSELAGE SKIN AT F/STA 150 STRINGER 33L. CORROSION WAS FOUND 2 INCHES FORWARD OF AN EXISTING REPAIR MADE PER OVERHAUL MANUAL FIGURE 12-22. REMOVE EXISTING REPAIR AND CUT-OUT CORRODED AREA. EXTEND REPAIR PER OVERHAUL MANUAL FIGURE 12-22 TO COVER NEWSDR FXGA201908051955Fitting · corrodedREPLACEMENT OF CORRODED FITTING AT STRINGER 20 W/STA 60L OUTBOARD. TO REPLACE CORRODED FITTINGS ON STRINGER 20L, OUTBOARD OF W/STA 60L. ON WING STRINGER 20L, REMOVE OUTBOARD STATION 60L STRINGER FITTINGS AND REPLACE WITH A NEW ONE.SDR FXGA201905081937Fitting · corrodedREPLACEMENT OF CORRODED FITTING AT W/STA 60L STRINGER 21L. TO REPLACE CORRODED FITTINGS ON STRINGER 21L, INBOARD AND OUTBOARD OF W/STA 60L. ON WING STRINGER 21L, REMOVE INBOARD AND OUTBOARD STATION 60L STRINGER FITTINGS AND REPLACE WITH NEW ONES.SDR FXGA2019062681938Fitting · corrodedREPLACEMENT OF CORRODED FITTING AT W/STA 60R STRINGER 21. TO REPLACE CORRODED FITTING INBOARD AND OUTBOARD OF W/STA 60R. REMOVE INBOARD AND OUTBOARD RIGHT HAND STATION 60 FITTINGS AND REPLACE WITH NEW ONES.SDR FXGA201807311816Skin · chafedCHAFED SKIN ON RT FLAP UPPER SKIN AT W/STA 370R. THE RIGHT HAND FLAP UPPER SKIN WAS FOUND CHAFED ON THE LEADING EDGE SECTION AT W/STA 370R. REMOVE DAMAGE IN A RACE TRACK SHAPE AND REPAIR PER A&B OHM FIGURE 13-47A. USE NAS1097AD RIVETS INSTEAD OF AN426AD RIVSDR FXGA201712050001Warning System · activatedUNSAFE LEFT MAIN GEAR INDICATION AFTER CYCLING SEVERAL TIMES FINALLY GOT DOWN & LOCKED SAFE INDICATION.SDR FXGA201708031715Skin · crackedCRACKED SKIN AT STATION 239 AND STRINGER 33 1/2. REPAIR TO SKIN CRACK AT STATION 239. INSTALL REPAIR IN ACCORDANCE WITH DC6 OVERHAUL MANUAL FIGURE 12-21 AND 12-22.SDR 2017F00172Line · crackedCOMPLETE HYDRAULIC SYSTEM FAILURE, EMERGENCY LANDING PROCEDURES FOLLOWED. REPLACED HYDRAULIC PRESSURE LINE NR 2. FOUND CRACK AT B-NUT. REPLACED THE LINE. PREFORMED LEAK CHECK & OPS CHECK OKAY. RELEASED AIRCRAFT FOR CONT SERVICE.SDR FXGA2016080916162Stringer · corrodedCORRODED STRINGER 12L AT BS 1049. REPAIRED THE STRINGER IAW A&B OVERHAUL MANUAL FIGURE 12-2.SDR FXGA201607181618Skin · damagedFUSELAGE SKIN AND STRINGER REPAIR AT BS 341, STRINGER 27L. TO REPAIR THE CORRODED SKIN AND STRINGER 27L AT BS 341. CUT-OUT OF THE CORRODED SKIN AND REPAIR PER A&B OVERHAUL MANUAL FIGURE 12-22. CUT STRINGER 27L BETWEEN BS 332 AND 350. REPAIR PER A&B OVERHAUL MSDR FXGA201607191616Skin · damagedSKIN CORROSION AND HOLE IN SKIN AFT OF LOWER CORNER OF AFT BELLY DOOR BETWEEN STRINGERS 30 AND 31R. REPAIRED THE SKIN. REMOVE DAMAGE & PREFORM REPAIR IAW OVERHAUL MANUAL FIGURE 12-22.SDR FXGA201511111542Bulkhead · damagedHOLE IN BULKHEAD AT FS 341 ABOVE STRINGER 32R. REPAIRED DAMAGED BULKHEAD IAW DC-6A & B OVERHAUL MANUAL FIGURE 12 - 6.SDR FXGA201510281541Floor Skin · corrodedCORRODED FLOOR SKIN BETWEEN FS 520 & 540. REPAIRED CORRODED SKIN IAW DC-6 A & B OVERHAUL MANUAL FIGURE 12-15.SDR FXGA201510291540Floor Skin · corrodedCORRODED FLOOR SKIN, BETWEEN FS 866 & 902, AROUND RBL 10. REPAIR CORRODED SKIN IAW DC-6 A & B, OVERHAUL MANUAL FIG 12-16.SDR FXGA201503151512Skin · chafedCHAFED WING SKIN AT WS 297R, STRINGER 26R. TO REPAIR CHAFING, CAUSED BY A FAIRING, BEAVER TAIL, RUBBING AGAINST THE LOWER WING SKIN AT WS 297R, STRINGER 26R. CUT OUT DAMAGED AREA & INSTALLED AN EXTERNAL REPAIR DOUBLER IAW SRM AN 01-40NL-3 FIGURE 2-62.SDR FXGA20150323001Stringer · corrodedREPAIR OF CORRODED FUSELAGE STRINGER FS 541, STRINGER 33L. CUT DAMAGED STRINGER. REMOVE CORRODED SECTION & INSTALLED NEW STRINGER SECTION & SPLICES IAW DC6 A & B OVERHAUL MANUAL FIGURE 12 - 2 PAGE 3 & 4.SDR FXGA201411051445Aileron · damagedREPAIR TO AILERON PN 5488155-7, SN 629 BECAUSE OF DAMAGE TO TIP FROM APPROX STATION 679.0" OTBD. REPAIR IAW DC-6 A B OVERHAUL MANUAL. AILERON TO BE REBALANCED AFTER REPAIR.SDR FXGA20141104001Unknown · leakingHYDRAULIC FAILURE, LOSS OF PRESS & QTY EXPERIENCED WHILE TURNING ONTO RUNWAY 33.SDR FXGA201408141429Skin · crackedREPAIR CRACK IN THE UPPER WING SKIN AT WSTA 111 STRINGER 10R. STOP DRILL CRACK & INSTALL AN EXTERNAL DOUBLER MADE FROM 7075-T6 0.080 IAW DWG 1429-01 & DC-6 A & B OVERHAUL MANUAL FIGURE 13-30.SDR FXGA201408121428Frame · crackedFRAME CRACK AT FS 29.5L. THE LT FRAME RAIL LOCATED AT FS 29.5L CRACKED JUST ABOVE THE FWD HINGE POINT OF LT NLG DOOR. A NEW SECTION OF FRAME WILL BE SPLICED IN FROM STRINGER 22 TO 31.SDR FXGA20140808001Hydraulic Line · looseHYDRAULIC FAILURE ON DECENT, EMER DECLARED & 0 DEGREE FLAP LANDING PERFORMED.SDR FXGA201404071421Skin · damagedFLAP SKINS REPLACEMENT BETWEEN STATION 64 & 148. REPLACE PUNCTURED & DENTED LOWER FLAP SKINS LOCATED BEHIND THE RT MLG. REMOVE DAMAGED LOWER SKINS BETWEEN STATION 64 & 148, TE CLOSE OUT PIECE BETWEEN STATION 64 & 97. MANUFACTURE NEW SKINS & CLOSE OUT PIECESDR FXGA201404071420Doubler · crackedCABIN HEATER EXHAUST SKIN REPAIR CRACKS WERE FOUND ON THE CABIN HEATER EXHAUST STAINLESS STEEL DOUBLER SHIELD. STOP DRILL CRACKS WITH A 5/32 INCHES DRILL MINIMUM, MANUFACTURE DOUBLER FROM STAINLESS STEEL IAW DWG 1420-01 & DC 6 A & B OHM FIG 14 - 7 EO 1420.SDR FXGA2014010901Structure · corrodedCORROSION FOUND ON FRONT SPAR OF LT REAR HYD COMPARTMENT APPROXIMATELY STATION 412 FROM STRINGERS 26 -30. REPLACED STRINGER 25L FROM SPLICE AT STATION 341 TO ITS END AT STATION 41. INSTALLED DOUBLER OVER CUTOUT, REQUIRED BY STRINGER REMOVAL, AT STATION 341-3SDR FXGA20131206001Unknown · leakingA FUEL LEAK WAS DISCOVERED ON THE OTBD SIDE OF THE NR 3 NACELLE. THE FUEL LEAK WAS SUSPECTED TO BE FROM LOOSE RIVETS & BAD SEALANT. THE DOUBLER WAS REMOVED, THE AREA INSPECTED FOR DAMAGE & CORROSION & A NEW DOUBLER WAS MANUFACTURED & INSTALLED.SDR FXGA201305131344Skin · corrodedCORROSION ON WING SKIN BETWEEN LWS 167 & WS 216. REPAIRED IAW EO 1344.SDR FXGA201304221321Spar Cap · corrodedCORROSION ON LOWER CTR SPAR CAP AT RWS 177, REMOVED CORROSION. PERFORMED VISUAL & HFEC INSPECTIONS, NO CORROSION DETECTED. FOUND WITHIN LIMITS IAW TO 1C-118A-3-1 APPENDIX III FIGURE C-2. TREATED & PRIMED AREA FOR CORROSION PROTECTION. APPLIED SEALANT FOR AE
Back to Douglas DC-6A