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 = '7AC' 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 = '7AC' 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 2020FA0000117Spar · damagedAIRCRAFT GROUND LOOPED ON LANDING AND RT WING STRUCK GROUND AT WING TIP, SEE DRAWING BELOW. CAUSED LITTLE DAMAGE TO TIP BOW 7-440 AND NO DAMAGE TO RIB S-143. UPON INSPECTION FOUND 8 CRACKS IN GROWTH RINGS GOING ALL THE WAY TO PLYWOOD DOUBLER FOR REAR SPAR STSDR 2012FA0000229Spar · damagedTHIS REPORT IS BEING SUBMITTED IAW AD 200-25-02 R1. LT AND RT WING TIPS WERE DAMAGED DUE TO LOOSE TIE DOWN ROPES. OTBD MOST RIBS WERE REPLACED AND RT AFT SPAR WAS REPAIRED AT STA 195.SDR 2009FA0000822Screen · cloggedFUEL STRAINER SCREEN IN NOSE TANK, FOUND PLUGGED UP. CAUSE UNKNOWN. AGE OF PANT ESTM: 63 YRS.SDR 2009FA0000821Coil · failedMAGNETO FAILURE DUE TO COIL. UPON INSPECTION, FOUND OIL FROM COIL, INSIDE MAGNETO. AGE OF COIL ESTM: 36 YRS. (K)SDR CA090108003Door Frame · corroded(CAN) DOOR TUBE RUSTED THROUGH LOWER END, REPLACED.SDR 2005FA0001137Spar · crackedAFT RT SPAR HAS LONGITUDINAL CRACK ON LOWER END. CRACK OCATED AT STRUT ATTACH POINT. SPAR ALSO SHOWS SIGNS OF ROTTING IB OF CRACK AREA. (K)SDR 2005FA0000014Spar · crackedDURING PRE-PURCHASE, COMPLIED WITH INSPECTION. BOTH SPARS IN BOTH WINGS WERE FOUND TO HAVE LOOSE AND MISSING NAILS THAT HOLD RIBS OT THE SPARS. SEVERAL LONGITUDINAL CRACKS WERE FOUND. RECOMMENDATION TO OWNER WAS TO REPLACE ALL WOOD SPARS, WITH STC METAL SPASDR 2005FA0000694Rib · crackedTHE FIRST WING RIB LOCATED IB OF THE AILERONS WAS FOUND CRACKED ALONG THE RADIUS OF THE ATTACH TAB WHERE THE RIB IS SECURED TO THE AFT SPAR. THIS AIRCRAFT WAS SUBJECTED TO YEARS OF PREVAILING WINDS QUARTERING AGAINST THE T/E OF THE LT AILERON. NO GUST LOCKS SDR QH52004F00000Housing · crackedTHIS PART WAS TESTED IAW MFG 65-40-03. CRACKED LOCATED AT THE OIL GALLERY.SDR 2004FA0000142Spar · crackedAD 200-25-02-R1, INSPECTION OF WING SPARS WAS SIGNED OFF AS COMPLIANCE WITH, ON 19 AUG O1 AS A NON-REOCCURRING INSP. DURING ANNUAL INSPECTION IN JAN 04, BOTH MAIN SPARS WERE FOUND TO BE CRACKED AT THE ROOT END.SDR 2003FA0001157Spar · crackedANNUAL INSPECTION. PERFORMED AD2001-25-02R1. NOTED CRACK ON LEFT/AFT WING SPAR. CRACK IS ON WOOD SPAR OUTBOARD OF LIFT STRUT ATTACH POINT. AIRCRAFT TT 6517.08. SPAR ORIGIN UNKNOWN. NOTED PREVIOUS SPAR REPAIR IN DIFFERENT LOCATION DATED 1979. RECOMMEND ASDR BDJ2003F00001Spar · crackedOWNER REQUESTED AN INSPECTION IAW AD2000-25-02R1 WOOD SPAR INSPECTION. INSPECTION REVEALED THAT ALL INSPECTION HOLES HAD NOT BEEN ADDED IAW SL406 REV. A. UPPER FRONT SPAR HOLES WERE CUT AND CONVERED WITH DUCT TAPE, RT FRONT SPAR HAD OPEN CRACK AT BUTT EXTENDSDR BDJ2003F00000Spar · crackedOWNER REQUESTED AN INSPECTION IAW AD 2000-25-02R1, WOOD SPAR INSPECTION. INSPECTION REVEALED ADDITION INSPECTION. HOLES WERE NOT ADDED IAW LS406, REV A, RT REAR SPAR HAD AN OPEN CRACK AT THE BUTT INTO THE SPAR ATTACH PLATE BOLT HOLE, SPAR SEPARATING AT THE SDR CA020730005Spar · cracked(CAN) WING SPARS, RIGHT FRONT WING WITH SMALL CRACKS FROM NAIL HOLES VARIOUS LOCATIONS. RIGHT REAR SPAR WITH CRACK FROM TIP DAMAGE PREVIOUS.BOTH SPARS REPLACED.SDR 2002FA0000649Spar · crackedLEFT WING REAR SPAR COMPRESSION CRACK AT STRUT ATTACH POINT BETWEEN DOUBLER ON UPPER SURFACE.SDR 2002FA0000249Spar · crackedDURING INSPECTION OF AD INSPECTION. FOUND LEFT WING FORWARD SPAR CRACKED AT UNDER SIDE OF SPAR OUT BOUND OF LIFT STRUT ATTACH POINT. OWNER WAS CALLED TO INFORM HIM THIS WING WILL BE REPAIRED WITH NEW SPAR INSTALLED.SDR 2002FA0000055Cylinder · leakingENGINE WAS INSTALLED ON THE AIRCRAFT AND RUN UP. AN OIL LEAK WAS NOTICED IN THE LOWER SPARK PLUG BOSS AREA OF NR 1 CYLINDER. FURTHER EXAMINATION REVEALED THAT SOME CUTS BETWEEN FINS ADJACENT TO THE SPARK PLUG HOLE NEARLY PENETRATED THE THREAD AREA OF THE SPASDR 2002FA0000054Cylinder · cutENGINE WAS INSTALLED ON THE AIRCRAFT AND RUN UP. AN OIL LEAK WAS NOTICED IN THE LOWER SPARK PLUG BOSS AREA OF NR 1 CYLINDER. FURTHER EXAMINATION REVEALED THAT SOME CUTS BETWEEN FINS ADJACENT TO THE SPARK PLUG HOLE NEARLY PENETRATED THE THREAD AREA OF THE SPSDR 2002FA0000234Spar · crackedRIGHT REAR SPAR CRACKED ON TOP AT OUTBOARD END OF STRUT ATTACHMENT DUBBLER. TIP OF SPAR HAS DUBBLER PLATES. SPAR HAS BEEN DAMAGED BEFORE.SDR 2001FA0000390Carburetor · inoperativeENGINE FAILURE, BELIEVE DUE TO FUEL STARVATION. GOOD FUEL FLOW UP TO CARBURETOR. NO CONTAMINATION FOUND WITH GASCOLATOR. UPON CARBURETOR DISASSEMBLY FOUND VERY FINE DIRT IN CARBURETOR FUEL STRANER AND FLOAT CHAMBER. ALSO, FOUND MAIN AIR BLEED JET NEARLY TOSDR 2001F00205Spar · crackedSPAR CRACKEDSDR 2001FA0000080Spar · crackedDURING INSPECTION, FOUND LT WING FORWARD SPAR CRACKED AT UNDERSIDE OF SPAR OUT BOUND OF LIFT STRUT ATTACH POINT. THIS WING WILL BE REPAIRED WITH NEW SPAR INSTALLED.SDR 2001FA0000106Spar · crackedFOUND A SMALL LONGITUDINAL CRACK BETWEEN THE PLYWOOD DOUBLER PLATE AT THE FORWARD LIFT STRUT ATTACH FITTING AND THE NEXT OUTBOARD RIB ALONG THE REAR FACE OF THE SPAR. WITH A MIRROR IN THE NEXT OUTBOARD RIB BAY, THE CRACK PROTRUDED ABOUT THREE INCHES. WHEN THSDR 20010223CW001Spar · crackedDURING INSPECTION, CRACK FOUND ORIGINATING FROM RIB NAIL RUNNING HORIZONTAL. SPAR INSTALLED 5/17/59SDR 2002FA0000241Spar · cracked1) RIGHT WING/ CRACKS PROPAGATING FROM BOLT HOLES ADJACENT TO FUSELAGE ATTACHMENT FROM AND REAR. 2) CRACK OUTBOARD OF REAR LIFT STRUT REAR SPAR (RIGHT WING) 3) LEFT WING REAR SPAR (ORIGINAL FACTORY SPAR) EDGE GLUED JOINT DELAMINATED FROM ATTACH FITTING OUT TSDR 2002FA0000240Spar · cracked1) RIGHT WING FRONT SPAR BETWEEN 3RD AND 4TH RIB ON FORWARD FACE OF SPAR A CRACK CROSSING 3 ANNUAL RINGS APPROXIMATELY 4 INCHES IN LENGTH. 2) LEFT WING LOOSE OR MISSING NAILS IN FRONT SPAR AS 3RD AND 4TH RIBS LOOSE OR MISSING NAILS IN FRONT AND REAR SPARS ADJSDR 20000623SH003Wheel · crackedUPON DISASSEMBLY FOR C/W AD 48-08-02, A CRACK WAS DISCOVERED IN THE BEAD RADIUS OF THE INNER WHEEL HALF, EXTENDING APPROXIMATLEY 90 DEGREES AROUND THE WHEEL. THESE WHEELS MUST BE DISASSEMBLED AND INSPECTED WITH THE TIRE REMOVED IN ORDER TO SEE THIS AREA AND SDR 20000417SH018Rocker · brokenPILOT REPORTED A REDUCTION IN POWER. AFTER INVESTIGATING, THE ROCKER ARM HAD BROKEN AT THE CENTER. THIS IS THE OLD TYPE WHICH DOES NOT HAVE AS MUCH MATERIAL AS THE NEW TYPE. (X)SDR 99ZZZX2572Elt · inoperativeDURING ANNUAL INSPECTION AND C/W FAR 91.207(D) G-TEST FAILED WHILE IN THE ARM POSITION. UNIT WAS OPENED AND SEVERAL LOOSE PARTS WERE FOUND FLOATING AROUND. AIRCRAFT TOTAL TIME: 2,382:7 HOURS.SDR 99ZZZX2573Air Filter · alteredDURING ANNUAL INSPECTION, THE ORIGINAL AIR FILTER ASSEMBLY WAS FOUND TO HAVE HAD THE GUTS REMOVED AND ALTERED TO ACCEPT A BRACKET AIR FILTER ELEMENT BA-4106 WHICH WAS CUT TO SIZE. THIS IS NOT APPROVED AND NOT SAFE. AIRCRAFT TT: 2,385.0 HOURS.SDR CA970319008Spar · cracked(CAN) FOUND REAR WING SPAR CRACKED AT TOP OUTER STRUT ATTACH PLATE. THE CRACK WAS ONLY VISIBLE WHEN A LOAD WAS APPLIED TO SPAR TIP.SDR 96ZZZX5957Fabric · looseDURING FLIGHT, UNUSUAL NOISE WAS HEARD. IT WAS FOUND THAT FABRIC WAS LOOSE ON 1ST AND 2ND RIBS ON RT WING, AND NR 4 AND NR 8 SCREWS HAD PULLED OUT OF RIBS. SUBMITTER STATED IT IS BELIEVED THAT SCREW HOLES WERE SLIGHTLY OVERSIZE AND FABRIC WEAVE WAS FORCED INSDR EY2R9601181Propeller · corrodedCORROSION FOUND ON FIXED-PITCH PROPELLER.SDR 96ZZZX2470Rib · crackedDISMANTLED BOTH LT AND RT WINGS FOR THE PURPOSE OF RECOVERING. IN THE PROCESS OF REMOVING OLD COVER, DETERMINED THAT ALL THE SCREWS THAT SECURE THE FABRIC TO THE RIBS FOR THE NR 2 AND NR 3 INBOARD RIBS OF EACH WING, HAD ELONGATED THE HOLES IN THE RIBS AND WASSDR 96ZZZX2469Rib · crackedDISMANTLED BOTH LT AND RT WINGS FOR THE PURPOSE OF RECOVERING. IN THE PROCESS OF REMOVING OLD COVER, DETERMINED THAT ALL THE SCREWS THAT SECURE THE FABRIC TO THE RIBS FOR THE NR 2 AND NR 3 INBOARD RIBS OF EACH WING, HAD ELONGATED THE HOLES IN THE RIBS AND WASSDR 96ZZZX2467Fitting · crackedDISMANTLED LEFT WING FOR THE PURPOSE OF RECOVERING. AS A PRECAUTION, THE WING SPAR ATTACHMENT FITTINGS WERE MAGNAFLUXED. THE LEFT REAR SPAR ATTACHMENT FITTING WAS FOUND TO HAVE SEVERAL IMPERFECTIONS IN THE WELD AREAS OF BOTH THE TOP AND BOTTOM GUSSETS. THE SDR 96ZZZX2387Fitting · crackedDISMANTLED LEFT WING FOR THE PURPOSE OF RECOVERING. AS A PRECAUTION, THE WING SPAR ATTACHMENT FITTINGS WERE MAGNAFLUXED. THE LEFT FRONT WING SPAR ATTACHMENT FITTING WAS FOUND TO HAVE SEVERAL IMPERFECTIONS IN THE WELDED AREA OF BOTH THE TOP AND BOTTOM GUSSETSSDR 96ZZZX2386Spar · crackedDISMANTLED BOTH LEFT AND RIGHT WINGS FOR RECOVERING. ALL SPARS WERE REMOVED FOR CLEANING, INSPECTION, AND VARNISHING. WITH THE WING SPAR FITTINGS REMOVED, FOUND THE SPAR FITTING HOLES HAD CRACKS EMANATING FROM THE TWO INBOARD HOLES THROUGH THE BUTT OF THE SPASDR 96ZZZX2385Spar · damagedDISMANTLED LEFT AND RIGHT WING FOR THE PURPOSE OF RECOVERING. WITH THE OLD FABRIC REMOVED, FOUND BOTH REAR SPARS HAD BEEN CHEWED BY MICE MIDWAY BETWEEN THE WING ROOT AND THE STRUT ATTACH FITTING. IT APPEARS THIS DAMAGE WAS PRESENT WHEN THE WINGS WERE LAST RESDR 96ZZZX469Seat Valve · looseENGINE QUIT ON TAKEOFF. DISASSEMBLED CARBURETOR AND INSPECTION FOUND SEAT VALVE HAD NOT BEEN PROPERLY TORQUED. SEAT WORKED LOOSE AND LOWERED FLOAT LEVEL TO WHERE ENGINE COULD NOT DEVELOP FULL POWER. CARBURETOR OVERHAULED 10-95.SDR 95ZZZX5965Air Box Valve · failedTHE SPOT WELD WHICH ATTACHES THE BUTTERFLY VALVE TO THE SHAFT BROKE WHICH ALLOWED THE VALVE TO BE SUCKED UP INTO THE CARBURETOR AND BLOCK OFF THE AIR TO THE ENGINE. THIS CAUSED THE ENGINE RPM TO DROP TO 700 RPM. THE PILOT LANDED IN A PLOWED FIELD, NO FURTHERSDR 95ZZZX5107Valve · brokenEMERGENCY LANDING MADE AFTER EXHAUST VALVE HEAD SEPARATED. THIS ENGINE HAD 732 HRS SINCE 'TOP' OVERHAUL AND 2,246 HOURS SINCE NEW. THIS IS THE 446-HOUR PAST MANUFACTURER'S RECOMMENDED TIME.SDR 95ZZZX2418Gascolator · bowl failedTHIS AIRCRAFT WAS INVOLVED IN A FUEL STARVATION ACCIDENT BELIEVED CAUSED BY FAILURE OF GASCOLATOR GLASS BOWL. SAFETY WIRE AND SAFETYING DEVICE STILL ATTACHED TO ASSY. CHAMPION ACFT CORP. SERVICE HINT NR 15 RECOMMENDS GLASS BOWLS BE REPLACED WITH METAL UNITS SDR 95ZZZX578Elbow · bogus partOIL PRESSURE LINE LEAKING AT 45 DEGREES, ELBOW EXITING THE CRANKCASE. REPLACED AUTOMOBILE FITTING WITH MS20823-4D FITTING WITH A NR 60 RESTRICTOR. ALSO, REPLACED OIL PRESSURE LINE FROM CRANKCASE TO FIREWALL.
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