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 = '727' 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 = '727' 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 K11A2021092700077Gauge · failedR AND R #2 EGT GAUGE. PERFORMED OPS CHECK IAW B727 AMM 77-21-00 AND 77-21-51.SDR CA110810008Flap System · malfunctionedAFTER TAKEOFF WHEN MOVING FLAPS FROM 5 TO 2 ,THE INBD FLAPS REMAINED AT 5. SUPP PROCEDURE COMPLETED USING ALT FLAPS, AND RETURNED. SYS WAS INSPECTED & FUNCTION CHECKED FOR CORRECT OPERATION, ALL OK IAW AMM 27-51-00 PRIOR TO LUBING THE INBD & OTBD FLAP JACKSCRSDR FOTR2111712446Structure · crackedVERTICAL STAB, L/E HAS CRACKED DOUBLER TOP OF FWD SPAR CHORD CENTER, JUST AFT OF ELEVATOR CONTROL CABLE QUADRANT. REPAIRED ON FASI WO 21117, NR 12446.SDR CA100216017Frame · cracked(CAN) DVI OF NLG BAY APPROX BS 328 FOUND RT TRUNNION SUPPORT FITTING A FRAME CRACKED ABOUT 3 INCHES LONG IN THE UPPER PORTION OF THE A FRAME. REPAIR WAS COMPLIED IAW SRM. (TC 20100216017)SDR 2009FA0000003Brake Assy · damagedBRAKE, WHEEL, AND TIRE CAME INTO THE SHOP WITH SEVERE DAMAGE THAT OCCURRED WHILE INSTALLED ON THE ACFT. ACCORDING TO THE PRELIMINARY INSP PERFORMED IN THE SHOP, THE BRAKE'S, NR5 ROTOR LINK BROKE, CAUSING THE ROTOR TO SPREAD AND CAUSE DAMAGE NOT ONLY TO THE BRASDR DU4R2008189Frame · dentedS/O 304002 N/R 26446 DEEP DENT AT FLANGE AREA BS 720A S24 - 25L IN FWD PIT LT SIDE.
REPAIRED BY CUTTING OUT DENT, FABRICATED FRAME REPAIR 8.5 INCH X 3 INCH X 1 INCH FROM 7075-T6 .063 INCH IAW SRM 51-40-3 FIG. 1, 51-30-2 AND 51-10-2 PARA. 2.SDR DU4R2008190Skin · damagedS/O 304002 N/R 26068 DEEP TOOL MARKS (5 EA) IN EXT. FUSELAGE SKIN AT BS 1123 FWD OF OUTFLOW VALVE RT SIDE. REPAIRED 5 EA TOOL MARKS BY CUTTING OUT AREA, FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER 11 INCH X 10-3/4 INCH FROM 2024-T3.071 INCH AND 2024-T3SDR AMTA200600523Battery · dischargedFWD CABIN EMERGENCY FLASHLIGHT (TEST) RED LIGHTS NOT FLASHING. REMOVED AND REPLACED BOTH FWD FLASHLIGHT BATTERY AND SEAL IAW AMM, BOTH FWD FLASHLIGHTS TEST GOOD. (K)SDR 05FDEA04183Floorbeam · corrodedAFT PIT MAIN DECK FLOORBEAM HAS CORROSION STA BS 1130 LBL67.0 REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW B727 SRM 51-10-6 AND 53-10-1. FABRICATED REPAIR PARTS IAW B727 SRM 53-10-8 FIGURE 10. ALODINED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2.INSDR 05FDEA04176Floorbeam · corrodedMAIN CABIN FLOORBEAM HAS CORROSION AT FASTENER HOLES AT STA BS1130 BETWEEN RBL14 AND RBL40. REPAIRED OUT OF LIMTS SECTION OF STA BS 1130 FLOORBEAM IAW SRM 53-10-8 FIGURE 10. ALODINED AND PRIMED BARE METAL AREAS IAW SRM 51-10-2. INSTALLED REPAIR WITH WET SDR 05FDEA04175Floorbeam · corrodedFORWARD CARGO COMPARTMENT STA BS 620 BOTTOM SURFACE OF FLOORBEAM UPPER TEE CAP HAS CORROSION AROUND SCREW HOLES LBL50 TO RBL50. REMOVED DAMAGED SECTION OF TEE CAP AT STA BS 620 BETWEEN LBL45 AND RT CUSP. FABRICATED NEW TEE CAP, SPLICES, SHIMS: ALODINED ANDSDR 05FDEA04174Floorbeam · corrodedAFT PIT MAIN DECK FLOORBEAM HAS CORROSION AT FASTENER CLIP AT STA, BS 950F, LBL21.0. REMOVED CORROSION IAW SRM 51-10-6 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIGURE 4. REMOVED AND REPLACED FLOORBEAM UPPER TEE CAP SECTION FROM LBL8 TO LBL70 IAW STANDSDR 05FDEA04147Structure · damagedAFT CARGO DOOR, LOWER CHORD, UPPER TEE CAP AT STA BS 950D TO BS 950E, ABOVE STRINGER 27-R HAS SEVERAL HOLES WITH NO EDGE DISTANCE AND MINIMUM SPACING. REPAIRED DAMAGED CHORD IAW B727 SRM 51-40-4 FIGURE 1. REMOVED AND REINSTALLED 4 EACH CHORD FITTINGS, FISDR 05FDEA02575Skin · damagedFUSELAGE EXTERNAL SKIN DAMAGED AFT OF SECTION 41 AROUND STRINGER 19 LT, REMOVED DAMAGE FABRICATED REPAIR DOUBLER FILLER AND INSTALLED IAW SRM 53-30-3 FIG 24. PREP AND PAINTED AREA I.A.W. M/M 51-20-151-7. THIS IS A CLASS B REPAIR WITH AN INSPECTION THRESHOLSDR 2005FA0001040Piston · brokenPISTON BROKE AT THE KEY GROVE, FATIGUE. (196962/FXS) (K)SDR 2005FA0000911Cap · crackedCAP IS CRACKED IN BOTTOM OF PORT C. CAP IS TOO WEAK. MAKE CAP STRONGER. (K) (REF: 195902/FXS)SDR 2005FA0000804Seat · damagedRECEIVED APU FIRE EXTINGUISHER FOR OVERHAUL AFTER FIRING. DURING THE DISASSEMBLY, IT WAS DISCOVERED THAT THE PYROTECHNIC CARTRIDGE MELTED THE STAINLESS STEEL BOTTLE’S SEAT RENDERING THE PRESSURE VESSEL SCRAP. THIS TYPE OF DAMAGE IS CONSISTENT WITH PREVIOUSLYSDR 2005FA0000910Housing · brokenAIRCRAFT RETURNED FROM A FLIGHT WITH HYDRAULIC FLUID LEAKING FROM ACTUATOR. FLIGHT ENGINEER WALK AROUND, FOUND BODY END BROKE OFF AT RETAINER END. UNKNOWN, THIS IS A NEW AND IMPROVED POST SB BODY. (K) (REF: 194950/LEB)SDR 05FDEA00631Lamp · malfunctionedLOWER CARGO SMOKE LIGHT ILLUMINATED ON T/O AT 90 KTS, RTO- NO OTHER INDICATION ON CARGO PANEL OR BELL. BOTH FWD AFT COMPARTMENTS CHECK CLEAR. RELAMPED INDICATOR OPS TEST NORMAL IAW MM 26-17-012-2 OK FOR SERVICE.SDR 2005FA0000078Housing · crackedCRACKED THROUGH THREADS IN CYL 1 PORT. FATIGUE, STRONGER BODY. MECHANIC JW2, JOB NR 191405. (K)SDR 2005FA0000077Cylinder · crackedCRACKED THROUGH THREADS IN CYL 1 PORT. FATIGUE, STRONGER BODY. MECHANIC JW2, JOB NR 191407. (K)SDR 2005FA0000076Cylinder · crackedCRACKED THROUGH THREADS IN CYL 1 PORT. FATIGUE, STRONGER BODY. MECHANIC JW2, JOB NR 191413. (K)SDR C1HA200476004Floorbeam · corrodedCORROSION ON FLOORBEAM STA 1010 LBL 0 - 15 LBL. CLEAN, TREAT & INSTALLED REPAIR DOUBLER.SDR 2004F00095Wheel · crackedRETURNED, TO REPAIR SHOP, WHEEL/ TIRE ASSY REMOVED FOR LOSS OF TIRE PRESSURE ,CAUSED BY SEVERE CRACK TO OUTBOARD WHEEL HALF.(REURNING FRACTURED PART TO MFG. FOR ANALYSIS)SDR GAIA03025SPStringer · crackedDURING C-CHECK, FOUND MAIN CABIN FORWARD STATION 720C, STRINGER 15L IS CRACKED AFT OF WING LIGHT. CUT OUT CRACK FROM STRINGER 15L, IAW SRM 53-10-3 FIG 5, FABRICATED REPAIR PARTS ONE CHANNEL .040 7075-T6 DIM 5.2 INCH BY 3.2 INCH, TWO FILLERS .100 7075-T6 5.2 BSDR GAIA03029SPFrame · dentedDURING C-CHECK, FOUND MAIN CABIN FRAME BS 520 HAS A DENT INTO THE RADIUS AT STRINGER 16R FASN/R 35745. CUT OUT DAMAGED AREA, FABRICATED FILLER FROM MATERIAL 7075-T6 .050 PO NR 991420, DIM 2.5 INCH BY 3 INCH, DOUBLER FROM MATERIAL 7075-T6 .063, PO NR 9912495 DSDR GAIA03028SPFrame · dentedDURING C-CHECK, FOUND MAIN CABIN FRAME BS 540 HAS DENT INTO THE RADIUS AT STRINGER 16 RT, FASI N/N 35744. CUT OUT DAMAGED AREA, FABRICATED SECTION OF FRAME MATERIAL USED 7075-T6 .063 P/O NR 991245 DIM 12 INCHES BY 3.5 INCHES, DOUBLER 7075-T6 .071 P/O NR 99120SDR GAIA03038SPSplice · crackedDURING C-CHECK, FOUND MAIN CARGO DOOR DECK BS 640, FLOORBEAM SPLICE PLATE CRACKED FROM SLOT RADIUS FASI N/R 35932. REMOVED AND REPLACED FLOORBEAM SPLICE PLATE P/N AE727-1-42-11, PO NR 319397 IAW STC AE179850 DTD 4-7-93. (M)SDR GAIA03037SPSplice · crackedDURING C-CHECK, FOUND MAIN CARGO DECK BS 600, FLOORBEAM SPLICE PLATE CRACKED AT SLOT RADIUS FASI N/R 35931. REMOVED AND REPLACED FLOORBEAM SPLICE PLATE P/N AE727-1-42-11, PO NR 319397 IAW STC AE 179850 DTD 4-7-93. (M)SDR GAIA03036SPFloorbeam · crackedDURING C-CHECK, FOUND MAIN CARGO DECK BS 580, FLOORBEAM SPLICE PLATE CRACKED AT SLOT RADIUS, FASI N/R 35930. REMOVED AND REPLACED SPLICE PLATE P/N AE 727-1-42-11, PO NR 319397 IAW STC AE 179850-DTD 4-7-93. (M)SDR GAIA03034SPFrame · dentedDURING C-CHECK, FOUND MAIN CABIN FRAME BS 560 HAVE DENTS INTO THE RADIUS AT STRINGER 16R AND STRINGER 8R FASI N/R 35743. CUT OUT DAMAGED AREAS, FABRICATED DOUBLERS FROM MAT 7075-T6 .063 PO NR 9912495, DIM 7 INCH BY 4.5 INCH AND 10 INCH BY 3 INCH. INSTALLED DSDR GAIA03031SPFrame · crackedDURING C-CHECK, FOUND MAIN CABIN FRAME BS 360 HAS A DENT AND CRACK BETWEEN STRINGERS 7R AND 8R FASI N/R 35751. CUT OUT DAMAGED AREA, FABRICATED DOUBLER REPAIR FROM 7075-T6 .050, PO NR 9911488 DIM 11 INCH BY 5.5 INCH. INSTALLED REPAIR IAW B727 SRM 51-30-2 ANDSDR GAIA03030SPFrame · damagedDURING C-CHECK, FOUND MAIN CABIN FRAME BS 460 HAS A TOOLING HOLE INTO THE RADIUS AT STRINGER 17R FASI N/R 35747. CUT OUT DAMAGE AREA, FABRICATED DOUBLER FROM 7075-T6 .063 PO NR 9912495 DIM 3.5 INCH BY 7.75 INCH, INSTALLED REPAIR IAW B727 SRM 51-30-2. (M)SDR GAIA03042SPSeat Track · corrodedDURING C-CHECK, FOUND MAIN CABIN SEAT TRACK CORRODED LBL 45 BS 720D FASI N/R 36068. REPLACED DAMAGED PARTS 90 INCHES LONG P/N BAC1520-792 AND BAS 1593-100122 IAW B-727 SRM 53-10-5 FIG 1. (M)SDR GAIA03044SPSkin · chafedDURING C-CHECK, FOUND LOWER RUDDER LOWER L/E CLOSE OUT WEB CHAFED THROUGH FASI N/R 36010. REPLACED WEB P/N 65-16830-4 IAW B-727 SRM 51-30-2. (M)SDR DHL2003741501Skin · crackedDISCREPANCY DURING C CHECK, FUSELAGE UPPER LOBE INTERIOR BS 680 AND CARGO DOOR LWR. SILL BEAM FRAME CRACKED FWD. AND AFT. ALSO MISSING FASTENERS (8 EACH). REMOVED FASTENERS IAW B-727 SRM 51-30-2. CUT-OUT DAMAGED AREA AND FABRICATED ANGLE IAW B-727 SRM.SDR C1HA200396001Warning Light · illuminatedAFTER GEAR RETRACTION, THE FWD DOOR LIGHT AND F/E'S RT GEAR DOOR LIGHT REMAINED ILLUMINATED. PERFORMED COM PROCEDURE 2.32.29 AND BOTH LIGHTS EXTINGUISHED. INSTALLED 3 PINS LANDING GEAR AND CYCLED FOR 2 TIMES, DOORS LANDING GEAR LIGHTS WORKING GOOD IAW MM 32-SDR 2002FA0000614Nut · fracturedNUT FRACTURED INTO THREE PIECES UNDER NORMAL TORQUE OF (75-80 IN-LBS).SDR 2002FA0000609Cap · erodedACTUATOR CAP PORT (C) HAS EROSION INTERNALLY.SDR 2002FA0000608Cap · erodedACTUATOR CAP PORT HAS EROSION INTERNALLY.SDR 2001FA0000676Cap · corrodedCAP ASSEMBLY HAS SEVERE CORROSION IN THE PACKING GROOVE, THE INTERIOR AND EXTERIOR SURFACES. DISSIMILAR METAL CORROSION.SDR 2001FA0000675Cap · corrodedCAP ASSEMBLY HAS SEVERE CORROSION IN THE PACKING GROOVE, THE INTERIOR AND EXTERIOR SURFACES. DISSIMILAR METAL CORROSION.SDR 2001FA0000674Housing · corrodedELBOW HOUSING HAS SEVERE CORROSION IN THE BOLT HOLES, CHECK VALVE PORT, PACKING LANDS AND ON THE SEALING SURFACE. DISSIMILAR METAL CORROSION.SDR 2001FA0000678Coil · shortedBRAKE COILS ARE SHORTED AND BURNED. UNDER NORMAL OPERATION THE VIBRATION INCURRED HAS BEEN FOUND TO CAUSE ABRADING BETWEEN THE BRAKE COILS AND STUDS WHICH RESULTS IN A SHORT AND ARCING OF THE BRAKE COILS. REDUCE THE SIZE OF THE COIL WINDINGS OR DIAMETER OF TSDR 2001FA0000677Coil · shortedBRAKE COILS ARE SHORTED AND BURNED. UNDER NORMAL OPERATION THE VIBRATION INCURRED HAS BEEN FOUND TO CAUSE ABRADING BETWEEN THE BRAKE COILS AND STUDS WHICH RESULTS IN A SHORT AND ARCING OF THE BRAKE COILS. REDUCE THE SIZE OF THE COIL WINDINGS OR DIAMETER OF TSDR 2001FA0000673Housing · corrodedHOUSING ASSEMBLY HAS HEAVY PITTING AND CORROSION IN THE BOLT HOLES, PORTS, CAP ASSEMBLIES AND ON THE SEALING SURFACES. DISSIMILAR METAL CORROSION.SDR IU62001F00012Actuator · flakingCHROME PLATING IS FLAKING OFF INSIDE THE BORE.SDR 01FDEA00899Switch · failed01-344 #6 L/E FLAP INDICATING IN TRANSIT AFTER RETRACTION. AIR RETURN. ** S/D ** COMINGSDR DHL2001741017Controller · lack of lube1) DURING FLAP EXTENSION LEFT INBOARD FLAP WOULD NOT EXTEND TO FLAPS 30. APPROX. 1 NEEDLE WIDTH OUT OF BOX DURING APPROACH AND 2ND ATTEMPT WAS MADE AFTER LANDING. 2) LUBRICATED FLAP MECHANISM AND ADJUSTED LEFT INBOARD FLAP TRANSMITER CHECK OPS. IS GOOD PSDR 2001FA0000423Housing · crackedHOUSING IS CRACKED ALONG FIRST SHOULDER ON SAME SIDE AS PORTS.
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