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 = '737448' 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 = '737448' 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 XV6A2015031100002Repair · unknownREF TECH W/O 1502527. R & R EXISTING REPAIR AT BS 727G IAW DWG 53-15046. EXISTING CATEGORY "C" REPAIR TIME LIMITED REPLACED BY CATEGORY "B" REPAIR.SDR 7AHR201405307372Skin · corrodedRT WING UPPER SKIN AT FRONT SPAR BETWEEN WS475 & WS531 HAS CORROSION. REPAIRED IAW DWG 57-13172-1.SDR 7AHR201405307369Skin · corrodedRIGHT WING UPPER SKIN HAS CORRROSION BETWEEN WS479 & WS505 AT S-11. REPAIRED IAW DWG 57-13169-1.SDR 7AHR201405307374Skin · corrodedRIGHT WING UPPER SKIN AT REAR SPAR AREA HAS CORROSION BETWEEN WS315 & WS370. REPAIRED IAW DWG 57-13174-1.SDR 7AHR201405307373Skin · corrodedRIGHT WING UPPER SKIN HAS CORROSION AT FRONT SPAR BETWEEN WS315 & WS375. REPAIRED IAW DWG 57-13173-1.SDR 7AHR201405307392Skin · damagedRT WING UPPER SKIN BLENDOUTS BETWEEN WS270 & WS583.SDR 7AHR201405302121Skin · damagedAT STRINGER 21 RT BS 360 - 400 EXTERIOR FUSELAGE HAS LARGE CREASE SHOWING IMPRESSION OF FRAME & STRINGER. AREAS WERE FOUND TO BE OUT OF LIMITS IAW SRM 51-00-01. REMOVED DAMAGED AREAS, PERFORMED EDDY CURRENT INSPECTION OF AREA, FABRICATED REPAIR AND INSTALLED SDR 7AHR201405302150Structure · corrodedCORROSION ON VERTICAL STABILIZER ABOVE RUDDER BALANCE WEIGHT. REMOVED CORROSION AND INSTALLED REPAIR IAW SRM 51-70-12 & 51-40-02.SDR 7AHR201405202163Skin · corrodedCORROSION LT WING SKIN AREA BETWEEN WS 150 & WS558. REMOVED CORROSION AND SENT MEASURMENTS TO FLIGHT VEHICLE CONSULTING FOR EVALUATION. BLENDED AREAS WERE FOUND TO BE IN LIMITS IAW FVC DWG 57-13170-1 WITH 8110-3 APPROVAL.SDR 7AHR201405202311Spar · corrodedCORROSION FOUND ON VERTICAL STAB REAR SPAR STA 219RH SIDE REAR SPAR CHORD. REPAIR WAS ACCOMPLISHED IAW FLIGHT VEHICLE CONSULTING DWG 57-13176-1 WITH 8110-3 APPROVAL.SDR 7AHR201405302368Window Frame · corrodedEVIDENCE OF CORROSION RT SIDE PILOTS WINDOW FRAME. FLIGHT DECK CENTER WINDOW POST. R & R BY TEAM REF RELEASE VEG-RE-1302158.SDR XV6A2013042700004Engine · bird ingestionBIRD STRIKE NR 1 ENGINE, VIBRATION AT 3.8 FOR 1 MINUTE REDUCE TO BELOW 3.0 FOR THE REST OF FLIGHT. OTHER INDICATIONS NORMAL. ENGINE INSPECTED AND FOUND DAMAGE TO 8 EACH FAN BLADES. NO OTHER DEFECTS NOTED PER AMM 71-00-47 AND GMM 9-13. REMOVED AND REPLACED SDR XV6A2013022700005Skin · crackedDURING AN INSPECTION, FOUR CRACKS WERE FOUND IN FUSELAGE SKIN BS 727E & 727F AND BETWEEN STRINGERS 25-26L. INSTALLED REPAIR IAW SRM 53-00-00, REPAIR 31 DETAIL XXXIV.SDR 2013F00073Skin · crackedLT LOWER FUSELAGE SKIN BETWEEN FS 727C-727F WITH THREE NEW CRACKS ON SKIN.SDR XV6A2012081200007Sensor · failedNR 2 ENGINE OVERTEMPED AT 938FT ON TAKEOFF FOR APPROX 1 SECOND. PERFORMED VISUAL INSPECTION OF THE INLET AND EXHAUST AREA FOR FOD AND SIGNS OF DAMAGE. NO DAMAGE OR FOD FOUND. INSPECTION WAS PERFORMED IAW B737 AMM 72-00-00 PAR. 3, SEC A, REF TO MEL 73-8 CONTSDR XV6A2012070200006Unknown · odorODOR OF CHEMICALS OBSERVED IN CABIN AFTER T/O. INSPECTED BOTH LEFT AND RIGHT ACM AND THE BAY IAW B737 AMM 21-51-00. NO DEFECT FOUND. INSPECTED EQUIP COOLING SYSTEM IAW B737 AMM 21-58-51, NO DEFECT FOUND. C/W AFTER ENGINE WASH PROCEDURES IAW B737 AMM 72-00-SDR XV6A2012041200002Guide Vane · burnedAIR TURNBACK. NR 1 ENGINE EGT STARTED TO EXCEED 900'C ON TAKEOFF ROLL. PULLED THRUST LEVER BACK DURING CLIMB TO PREVENT EXCEEDING MAX CONTINUOUS EGT. ALSO, NR 1 ENGINE VIBE INDICATOR WAS SHOWING 4 AND 5 DURING CLIMB. PERFORMED BORESCOPE OF LPT STAGE 1 NOZZSDR ABXR2011111000051Skin · corrodedLOWER SKIN OF EXHAUST GATE CORRODED AT OUTBD EDGE. REMOVED FASTENERS AND REPLACED IAW B737 SRM 51-40-02 AND AMES PROCESS STANDARDS MANUAL CH 07 SECT 03 REV 09 DATED 10/6/2011.SDR TIPR20090024Floorbeam · corrodedFS 947.50 FLOORBEAM UPPER TEE RBL 70.53 TO LBL 70.53. REPAIRED IAW REO-G12924 REV B DATE 09/23/2009.SDR TIPR20090023Bear Strap · corrodedFS 344 STR 9L TO 11L AND STR 12L TO 15L- FWD ENTRY DOOR BEARSTRAP CORRODED. REPAIRED IAW REO-G12967 REV E DATE 10/3/2009. MAJOR REPAIR.SDR XV6A2009040800003Battery · dischargedOVERHEAD BIN EMERGENCY LIGHTS INOP AT 18-L, 12-L, AND 10-R SEAT LOCATIONS. CHARGED EMERGENCY LIGHT SYSTEM BATTERIES IAW AMM 33-51-02.SDR XV6A2009040800002Battery · dischargedFLOOR LEVEL RT OVERWING EXIT IDENTIFIER LIGHT INOP. CHARGED EMERGENCY LIGHT SYSTEM BATTERIES IAW AMM 33-51-02.SDR XV6A2009040600007Light · inoperativeEMERGENCY LIGHTS INOP AROUND ROW 19.SDR XV6A2009032000006Battery Pack · dischargedLEFT OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK IAW BOEING 737-400 AMM 33-51-51.SDR XV6A2009031200004Battery · dischargedR1 MAIN DOOR EMERGENCY LIGHT INOP.SDR 2008FA0000538Spar · corrodedDURING SCHEDULED INSP, FOUND CORROSION ON LT IB MID FLAP, MID SPAR UPPER CHORD. (K)SDR 2008FA0000514Spar · corrodedDURING SCHEDULED INSP, FOUND CORROSION ON LT IB MID FLAP, MID SPAR UPPER CHORD. (K)SDR 2008FA0000513Spar · corrodedDURING SCHEDULED INSPECTION, FOUND CORROSION ON LT IB MID FLAP, MID SPAR UPPER CHORD. (K)SDR 2008FA0000474Skin · dentedDURING SCHEDULED INSPECTION, FOUND NUMEROUS DENT ON AFT CARGO EXT DOOR SKIN. S/O 312001, OPS 24422. (K)SDR 2008FA0000475Floorbeam · corrodedDURING SCHEDULED INSPECTION, FOUND CORROSION ON UNDERSIDE OF "T" CAP REPLACEMENT 986.5 AROUND ATTACH HOLES BL 29R TO BL 29L, NUMEROUS HOLES. (K)SDR 2008FA0000393Frame · damaged(REF DU4R2008217) DURING SCHEDULED INSPECTION, FOUND DOUBLE-DRILLED HOLE ON MAIN FRAME UPPER CAP AT BS 986.5 AT FLOOR LEVEL RT. (K)SDR 2008FA0000392Floor Support · corroded(REF DU4R2008216) DURING SCHEDULED INSPECTION, FOUND CORROSION ON UPPER SURFACE OF FLOOR SUPPORT BEAM BS 328, RBL-16 TO RBL-60. S/O NR 312001,
OPS NR 24738. (K)SDR 2008FA0000390Cargo Track · corrodedDURING SCHEDULED INSPECTION, FOUND CORROSION IN THE AFT CARGO COMPARTMENT LT TIE DOWN TRACK LBL 17.20 FROM STA 727B - STA 727E. PARTICULARLY IN FASTENER HOLE UPPER AND LOWER SURFACE. (K)SDR 2008FA0000389Skin · dented(REF DU4R2008214) DURING SCHEDULED INSPECTION, FOUND DENT ON LWR RT LOWER AFT FUSELAGE BS 887 S-19R. (K)SDR 2008FA0000388Door Frame · cracked(REF DU4R2008213) DURING SCHEDULED INSPECTION, FOUND 1 INCH LONG CRACK ON FWD CARGO DOOR CUT-OUT AFT FRAME INNER CHORD RADIUS. (K)SDR 2008FA0000387Attach Angle · corroded(REF DU4R2008212) DURING SCHEDULED INSPECTION, FOUND CORROSION IN AFT LOWER CARGO COMPARTMENT AT STA 727A ATTACH ANGLE GBGETWEEN S-27R AND S-26R. (K)SDR DU4R2008211Frame · drilledDOUBLED DRILLED HOLE IN FUSELAGE FRAME AT BS 986L.5 AT WL 208.SDR DU4R2008210Skin · dentedDENT ON FUSELAGE SKIN AFT BS 910 AT S-21R.SDR DU4R2008209Skin · dentedDENT ON FUSELAGE SKIN AFT BS 947 AT S-23R.SDR DU4R2008208Support · gougedS/O NR312001 NR 24376, NR1 ENGINE PYLON FAN COWL SUPPORT UPPER CHORD FWD HORIZ END FLANGE NAC 166-175 APPROX IS GOUGED.SDR DU4R2008207Stringer Clip · crackedS/O 312001 OPS NR 24792 - CABIN BS 400 STR. 2L HAS CRACKED STRINGER CLIP.SDR DU4R2008203Floorbeam · corrodedS/O 312001 N/R 28019, CORROSION AT CABIN FLOORBEAM UPPER CHORD UPPER SURFACE BS 360 LBL 15 TO RBL 15 W/L 201.SDR DU4R2008198Frame · crackedS/O 312001 OPS NR 27955 - FLIGHT COMPARTMENT HAS CRACK AT SHEAR WEB FRAME BS 188 - 196 LT FLOOR LEVEL (CRACK EMANATING AT EDGE CUT OUT).SDR DU4R2008197Frame · crackedS/O 312001 OPS NR27954 - FLIGHT COMPARTMENT HAS CRACK AT MAIN FRAME BS 188 - 196 LT FLOOR LEVEL (CRACK AT RADIUS) OB CHORD W/L 208.SDR DU4R2008196Shear Web · crackedS/O 312001 OPS NR24728, FLIGHT COMPARTMENT CRACK AT SHEAR WEB BETWEEN SBS 188 - 196 RT FLOOR LEVEL (CRACK EMANATING AT EDGE CUT OUT).SDR DU4R2008195Frame · crackedS/O 312001 OPS NR 24727 - CRACK AT MAIN FRAME OB CHORD STA. 188 RT SIDE FLOOR LEVEL (CRACK IN RADIUS).SDR DU4R2008193Skin · dentedS/O 312001 OPS NR 24422 - AFT CARGO EXT DOOR SKIN HAS OUT OF LIMIT DENTS BETWEEN 2 EA EXISTING REPAIRS.SDR DU4R2008194Structure · corrodedS/O 312001 OPS NR 24701, CORROSION OUT OF LIMITS ON L-1 DOOR LOWER INNER CHORD AT BS 328,
LBL 58 TO LBL 60.SDR DU4R2008201Floorbeam · corrodedS/O 312001 N/R 24738 - CORROSION ON UPPER SURFACE OF FLOOR SUPPORT BEAM BS 328 RBL 16 - RBL 60.SDR DU4R2008200Floorbeam · corrodedS/O 312001 N/R 24703 - CORROSION ON TOP OF FLOORBOARD IN GOUGE BS 312 LBL 52 TO LBL 8, AND NUMEROUS PLACES AT RBL 0 TO RBL-54.
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