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 = '72721' 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 = '72721' 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 2002F00692Floor Panel · corrodedFOUND CORROSION ON UNDERSIDE OF COCKPIT FLOOR PANEL NR 2306. (M)SDR 2001F00411Floor Support · corrodedFOUND CORROSION ON COCKPIT FLOOR SUPPORT PANEL FROM BS 259.5 TO BS 282.5 AT LBL 8 INCHES. REMOVED FLOOR SUPPORT SECTION BETWEEN BS 259.5 TO 282.5. INSTALLED NEW SECTION IAW B727 SRM 51-30-2. (M)SDR 2001F00410Floor Support · corrodedCORRODED COCKPIT FLOOR SUPPORT ANGLE AT BS 295 RBL 10 INCHES. REMOVED CORRODED FLOOR SUPPORT AT BS 295 RBL 10 INCHES IAW B727 SRM 51-30-2. REMOVED CORROSION AND TREATED IAW B727 SRM 51-10-2 AND B727 SRM 51-10-6. INSTALLED NEW FLOOR SUPPORT IAW B727 SRM 51-3SDR 2002F00716Intercostal · corrodedFOUND CORROSION ON INTERCOSTAL BETWEEN BS 970 AND BS 990 AT LBL 16. (M)SDR 2002F00713Frame · crackedFOUND FUSELAGE LOWER FORWARD CARGO, BS 700 STATION 20L, AT FRAME TO SKIN WEB, HAS A CRACK AT RIVET. (M)SDR 2001F00430Frame · crackedFUSELAGE LOWER FORWARD CARGO, BS 700 STATION 20L, AT FRAME TO SKIN WEB, HAS A CRACK AT RIVET. CUT OUT DAMAGE AREA AND INSTALLED FRAME REPAIR AT BS 700 STATION 20L IAW B727 SRM 53-10-4. (M)SDR RYN2002F00004Stringer · corrodedSTRINGER EXFOLIATED BETWEEN BS 1148 TO BS 1166 BETWEEN STRINGER 3L AND 4L IN THE AFT CABIN CROWN AREA. ACCOMPLISHED FUSELAGE STRINGER REPAIR BS 1148 TO 1166 BETWEEN STRINGER 3L AND 4L. DUE TO CORROSION IAW SRM. (MATERIAL USED 301 CRESS .5000 HARD .050 INCH,SDR 2002F00848Fitting · crackedFOUND CRACK AROUND C2 DOOR FORWARD UPPER HINGE ATTACH POINT AT BS 1070 STRINGER 20R AND 19R. ACCOMPLISHED C2 DOOR FORWARD FRAME REPAIR AT BS 1070 STRINGER 20R AND 19R IAW B727 SRM 53-10-2, FIGURE 5. (M)SDR 2002F00710Doubler · crackedFOUND MAIN CARGO DOOR CUTOUT EXTERNAL DOUBLER CRACKED AND BULGED AT STATION 17L BS 560. (M)SDR 2002F00712Sill · crackedFOUND LOWER FORWARD CARGO COMPARTMENT BS 680 LOWER SILL BEAM AT SPLICE, BOTTOM ROUTED OUT, ELONGATED AND CRACKED. ALSO, MISSING RIVET INTERIOR TO FUSELAGE SKIN. (M)SDR 2002F00711Sill · crackedFOUND CABIN FUSELAGE STATION BS 480 STRINGER 17L LOWER SILL BEAM TIED FRAME TO FUSELAGE, FORWARD AND AFT, ARE CRACKED. (M)SDR 2001F00425Floorbeam · corrodedFOUND BS 620 FLOORBEAM CORRODED ON UPPER CAP AT RBL 50. INSTALLED FLOORBEAM REPAIR AT BS 620 UPPER CAP AT RBL 50 IAW SRM 53-10-8 FIG 3. (M)SDR 2002F00841Stringer · damagedHOLE FOUND IN LOWER RADIUS AT BS 370 STRINGER 6R. ACCOMPLISHED FUSELAGE STRINGER REPAIR AT BS 370, STRINGER 6R IAW B727 SRM 53-10-2, FIGURE 2. (M)SDR 2002F00847Structure · corrodedLEFT NOSE WHEEL WELL VERTICAL WEB EXFOLIATED AT INTERSECTION WITH UPPER NOSE CHORD AS VIEWED FROM DOG HOUSE AT BS 315 DUE TO CORROSION. ACCOMPLISHED NOSE WHEEL WELL LEFT VERTICAL WEB REPAIR DUE TO CORROSION IAW B727 SRM 53-10-2, FIGURE 1. (M)SDR 2002F00846Pressure Panel · corrodedNOSE WHEEL WELL SKIN CRACKED LEFT SIDE AT STATION 243.7. ACCOMPLISHED NOSE WHEEL WELL RIGHT SIDE SKIN REPAIR AT BS 243.7 IAW B727 SRM 51-40-2, FIGURE 1. (M)SDR 2002F00845Pressure Panel · crackedNOSE WHEEL WELL RIGHT SIDE SKIN HAS A VERTICAL CRACK AT STATION 270. ACCOMPLISHED NOSE WHEEL WELL RIGHT SIDE SKIN REPAIR AT BS 270 IAW B727 SRM 51-40-2, FIGURE 1 AND 53-10-2, FIGURE 2. (M)SDR 2002F00844Pressure Panel · corrodedDUE TO CORROSION, RIGHT NOSE WHEEL WELL VERTICAL WEB EXFOLIATED AT INTERSECTION WITH UPPER NOSE CHORD AS VIEWED FROM DOG HOUSE BS 315. ACCOMPLISHED RIGHT NOSE WHEEL WELL VERTICAL WEB REPAIR IAW B727 SRM 53-10-2 FIGURE 1. (M)SDR 2002F00843Frame · corrodedRIGHT NOSE WHEEL WELL, MID CHORD EXFOLIATED AT INTERSECTION OF RIGHT WEB AND FLOOR WEB AS VIEWED FROM DOG HOUSE. ACCOMPLISHED RIGHT NOSE WHEEL WELL MID CHORD REPLACEMENT IAW B727 SRM 51-30-2 AND 51-20-4. (M)SDR 2002F00842Skin · corrodedBULGING AND PILLOWING SKIN ON STRINGER 8L AT BS 1166 THROUGH BS 1183. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1166 TO BS 1183 STRINGER 8L DUE TO CORROSION IAW B727 SRM 53-30-3, FIGURE 3. (M)SDR 2002F00840Skin · corrodedBULGING SKIN ALONG STRINGER 10L AT BS 920 THROUGH 1005 DUE TO CORROSION. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 920 TO BS 1005 AT STRIGNER 10L IAW B727 SRM 53-30-3 FIG 14. (M)SDR RYN2002F00000Support · damagedAT MAIN CARGO DOOR FORWARD ACTUATOR, FORWARD AND AFT SUPPORT BLOCK ON DOOR STATION 540, 5 BOLTS HAVE OBLONGED/ELONGATED HOLES AND 1 LOOSE BOLT. ACCOMPLISHED MAIN CARGO DOOR FORWARD ACTUATOR SUPPORT BLOCK ATTACH INTERCOSTALS (2 EACH: FORWARD AND AFT) REPLACEMSDR 2001F00391Frame · corrodedRIGHT NOSE WHEEL WELL, MID CHORD EXFOLIATED AT INTERSECTION OF RIGHT WEB AND FLOOR WEB AS VIEWED FROM DOG HOUSE. ACCOMPLISHED RIGHT NOSE WHEEL WELL MID CHORD REPLACEMENT IAW B727 SRM 51-30-2 AND 51-20-4. (M)SDR RYN2002F00003Skin · corrodedBULGING SKIN/DISHED FASTENER AT BS 1176 THRU BS 1183, STRINGER 20L THRU 21L UNDER AFT LAV SERVICE VALVE. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1176 TO BS 1183 STRINGER 20L TO STRINGER 21L DUE TO CORROSION. (MATERIAL USED 2024-T3. 071, 28 INCHES X 30 INSDR RYN2002F00002Skin · damagedBULGING AND PILLOWING SKIN AT BS 1085 THRU BS 1110 ALONG FASTENER ROWS AT STRINGER 17R THRU 19R ON EXTERNAL FUSELAGE. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1085 TO BS 1110 BETWEEN STRINGER 17R AND 19R DUE TO CORROSION IAW MFG ENGINEERING RO. (MATERIAL USSDR RYN2002F00001Skin · damagedBULGING/PILLOWING SKIN ALONG STRINGER 4L AT LAP JOINT BS 1130 THRU BS 1183. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1130 TO BS 1183 STRINGER 4L DUE TO CORROSION IAW SRM. (MATERIAL USED 2024-T3 .050 INCH, 98 INCHES X 9.1250 INCHES)SDR 2002F00715Doubler · bulgedFOUND FUSELAGE EXTERIOR SKIN DOUBLER HAS BULGE AT STRINGER 10L BS 470, JUST FORWARD OF MAIN CARGO DOOR. (M)SDR 2002F00714Frame · crackedFOUND MAIN CABIN FUSELAGE FRAME CRACKED AND AFT SIDE ATTACH ANGLE CRACKED AT STATION 480 JUST BELOW STRINGER 17L. (M)SDR 2002F00699Screw · missingFOUND MAIN CABIN FLOOR SEAT TRACK, JUST AT MAIN CARGO DOOR FRAME, HAS LOOSE AND MISSING SCREWS, LBL 64 BETWEEN BS 540 TO BS 660. (M)SDR 2002F00698Seat Track · damagedFOUND MAIN CABIN FLOOR SEAT TRACK DAMAGED AT BS 640, RBL 24. (M)SDR 2001F00431Seat Track · damagedMAIN CABIN FLOOR SEAT TRACK DAMAGED AT BS 640, RBL 24. REMOVED AND REPLACED SECTION OF SEAT TRACK IN MAIN CABIN FROM BS 600 TO BS 740 RBL 24 IAW B727 SRM 53-10-8 AND 51-30-2. (M)SDR 2001F00424Spar · corrodedCENTER TANK UPPER SKIN AT REAR SPAR BS 870 HAS CORRODED AREAS FROM LBL 40 TO RBL 40. ACCOMPLISHED WING CENTER SECTION AFT SPAR UPPER CHORD AND SKIN REPAIR AT RBL 24 IAW AVHM-246RO-1 REV IR. (M)SDR 2002F00702Panel · corrodedFOUND CORROSION ON 2ND OBSERVER SEAT SUPPORT PANEL AFT AND FORWARD EDGE. (M)SDR 2002F00701Floor Panel · corrodedFOUND CORROSION ON COCKPIT FLOOR SUPPORT PANEL BETWEEN BS 289.5 AND BS 312 AT RBL 12. (M)SDR 2002F00700Floor Panel · corrodedFOUND CORROSION ON COCKPIT FLOOR SUPPORT PANELS FROM BS 257.5 TO BS 312, AT LBL 13. (M)SDR 2001F00412Floor Support · corrodedFOUND CORROSION ON COCKPIT FLOOR SUPPORT PANELS FROM BS 257.5 TO BS 312 AT LBL 13 INCHES. REMOVED CORROSION BETWEEN STATION 259.5-278 AND STATION 294-312 IAW B727 SRM 51-10-5. MATERIAL LOSS WITHIN LIMITS AS PER B727 SRM 55-10-1. TREATED AND PRIMED PER B727 SDR 2001F00259Wire · damagedNR 1 ENGINE START VALVE LIGHT ILLUMINATED IN FLIGHT. EMERGENCY DECLARED. COMPLIED WITH ENGINE SHUTDOWN CHECK LIST. DIVERTED TO MCI. AIRCRAFT LANDED WITHOUT INCIDENT. REPAIRED WIRE TO START VALVE AT CANNON PLUG. OPERATIONAL CHECK OF SYSTEM GOOD. (M)SDR 2002F00720Skin · bulgedFOUND EXTERNAL LEFT FUSELAGE LAP SEAM STATION 400 TO 420, STRINGER 26L HAS A BULGE. (M)SDR 2002F00719Skin · crackedFOUND LOWER AFT CARGO COMPARTMENT DOOR SKIN HAS A CRACK CLOSE TO REAR LOWER EDGE. (M)SDR 2002F00718Panel · crackedFOUND LOWER AFT CARGO COMPARTMENT DOOR INNER BOTTOM BAFFLE PANEL HAS A BEND AT CORNERS WITH TWO CRACKS, ONE OVER PREVIOUS REPAIR. (M)SDR 2002F00856Floorbeam · corrodedFUSELAGE INTERIOR AT BS 328 LBL 27 HAS CORROSION DAMAGE TO FLOORBEAM UPPER CAP FORWARD AREA. (M)SDR 2002F00724Angle · corrodedFOUND FUSELAGE INTERIOR AT BS 351.2 RBL 48, CORROSION DAMAGE TO UPPER END OF ANGLE BETWEEN SKIN AND FRAME, JUST ABOVE WALKWAY WEB PANEL, STRINGER 22 AREA. (M)SDR 2002F00723Stringer · corrodedFOUND FUSELAGE INTERIOR AT BS 294 THROUGH BS 314 STRINGER 21R HAS SURFACE CORROSION. (M)SDR 2002F00722Stop Fitting · crackedFOUND FORWARD ENTRY DOOR FORWARD CUTOUT STOP FITTING NR 4 FROM TOP IS CRACKED TO LOWER AFT. (M)SDR 2002F00721Plate · corrodedFOUND FUSELAGE INTERIOR AT BS 294 BL 0 CORROSION DAMAGE TO PLATE ABOVE NOSE WHEEL WELL STRUCTURE WHERE 2 CONTROL CABLES PASS THROUGH UP/DOWN DIRECTION. (M)SDR 2002F00704Skin · bulgedFOUND VERTICAL STAB BS 1342 RIGHT SIDE STRINGER 10R HAS BULGING SKIN. (M)SDR 2002F00703Door Frame · crackedAFT ENTRY DOOR LEFT SIDE FRAME BS 1183 NR 2 STOP FRAME CUTOUT IS CRACKED, RUNNING APPROX TO AFT WATERLINE 270. (M)SDR 2001F00466Frame · crackedNOSE GEAR WHEEL SIDE PANEL LEFT SIDE FORWARD LOWER CHORD CRACKED AT WEB STATION 244.0. (M)SDR 2001F00427Floorbeam · damagedFOUND CABIN FLOORBEAM BS 344 HAS EXCESS OF OVERSIZE HOLES ON UPPER CAP FROM LBL 62 INCHES TO RBL 62 INCHES. REPLACED SECTION OF CABIN FLOORBEAM UPPER T-CAP AT BS 344 IAW SRM 53-10-8. (M)SDR 2001F00404Spar · corrodedWING CENTER SECTION INTERNAL AFT SPAR WEB BULGED IN AREA OF UPPER SPAR CHORD BL 22L DUE TO CORROSION. INSTALLED WING CENTER SECTION AFT SPAR WEB REPAIR AT STATION 870 BETWEEN LBL 17.2 AND LBL 25.9 IAW AVITAS ENGINEERING REPAIR ORDER AVHM-237RO-1 REV 1R DATED SDR 2002F00858Skin · dentedFUSELAGE EXTERIOR SKIN APPROXIMATELY BS 510 LAP JOINT SILL LEFT HAS A DENT. (M)
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