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 jasc_code = '5700' 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 jasc_code = '5700' 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 ABXA010839Attach Angle · cracked#1 ENGINE PYLON FOOTSTOOL WAS CRACKED AT THE '6'O-CLOCK POSITION, CENTER BOLT AND NEXT BOLT OUTBOARD. REPAIRED AREA IAW D854-43106MR.SDR ABXA010853Support · crackedRIGHT WING SLAT CONTROL PULLEY BRACKET SUPPORT WAS CRACKED. INSTALLED NEW PULLEY BRACKET IAW DC-9 SRM.SDR ABXA010852Rib · crackedLEFT WING LEADING EDGE RIB AT THE #2 SLAT TRACK, INBOARD RIB WAS CRACKED. REPAIRED RIB IAW DC-9 SRM.SDR ABXA010851Fitting · crackedCRACK IN FITTING COMMON TO REAR SPAR, JUST BELOW THE INBOARD SPOILER/TORSION BAR. REPLACED STIFFENER AND REPAIRED AREA IAW DC-9 SRM.SDR ABXA010831Doubler · crackedLEFT WING 505F PANEL HAD 10 EACH CRACK INDICATIONS AT FASTENER HOLES. REPAIRED AREA IAW REA D857-43069MR.SDR DL73K020376Wedge · delaminatedFOUND ON V1 LETTER CK AFT WEDGE DALAMINATED O/B END NUMBER 5 SLAT.__C/A REPLACED WEDGE ASSEMBLYSDR ABXA010834Spar Cap · crackedRIGHT WING, FORWARD LOWER SPAR CAP HAD 9 EACH FASTENERS HOLES SHOWING CRACK INDICATIONS. REPAIRED DAMAGED HOLES IAW REA D857-43058.SDR ABXA010778Support · crackedVERTICAL SUPPORT FOR SLAT MECHANISM MOUNT HAD A CRACK AT LOWER INBOARD MOUNT BOLT. REPLACED VERTICAL SUPORT IAW DC-9 SRM 51-30-5.SDR IXXA0200031SWing · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED AROUND SCREW HEADS ON THE LEFT WING OUTBOARD LEADING EDGE XFS892 TO XFS930. REPAIR ACCOMPLISHED REMOVAL OF THE CORROSION, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH TSDR IXXA0200030SWing · corrodedDURING ROUTINE C-CHECK INSPECTION CORROSION WAS DETECTED AROUND THREE SCREW HOLES ON THE LEFT WING OUTBOARD LEADING EDGE AT STATION XFS 885. REPAIR ACCOMPLISHED, REMOVAL OF THE CORROSION, FACRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN ACCORDANCSDR CALA0200094Skin · crackedINSPECTION FOUND A 1/2" CRACK IN R/H WING #6 FLAP FAIRING LOWER SKIN WITH RIVETS PULLING THROUGH. A STIFFENER WAS INSTALLED IAW SRM 51-10-2.SDR ABXA010749Rib · crackedRIGHT WING LEADING EDGE RIB (JUST INBOARD OF #2 SLAT TRACK) CRACKED AT THE LOWER ATTACH FASTENER. REPAIRED RIB IAW DC-9 REA D957-43342.SDR UPS02237711Casting · corrodedINSPECTION TYPE:C #5 FLAP TRACK ATTACH POINT ON LWR SURFACE OF WING, CORROSION EXIDENT IN AFT PAD, O/B HOLE. CORROSION SEEMS TO BE CONFINED TO BARREL NUT CASTING. REMOVED CASTING ON O/B OF #5 FLAP TRACK IAW SRM 51-30-02, CASTING RE PLACED IAW BOEING DWGS SDR IXXA0200019SFitting · gougedDURING ROUTINE C-CHECK INSPECTION A GOUGE WAS DETECTED ON THE FLAP SUPPORT FITTING INBOARD INNER EDGE, STATION 405. BLENDED OUT DAMAGED AREA IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER 57-DC8-1839.SDR DHL2002805044AngleLT WING Z ANGLE CRACKED 5 IN AT STA XW 485.000SDR C2XA02TY008Bracket · gougedTYS During a scheduled inspection the right hand aileron PCA rod end attachment bracket was found to be gouged. Maintenance acomplished a blend-out repair including a dye penetrant inspection IAW Embraer GST-0046/02. The repair was found to be satisfactorySDR ABXA010666Spar · corrodedLEFT WING, FORWARD SPAR CAP AT XFS 520.76 HOLE HAD A CRACK INDICATION WITH HFEC DETERMINE CRACK LENGH AND LOCATION IAW ES00046. REPAIRED CRACKED HOLE IAW DAC DWG 4709980 AND DC-8 SRM 51-1-25. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8.SDR DL72S020023Angle · cracked1/8 IN CRACK COVE SKIN ATTACH ANGLE BELOW TAI DUCT NBR 2 SLAT REPAIR PER MM 57-54-000-8SDR GLBA2001244Fuel Cap · leakingLEFT O/B FUEL CAP LEAKING, REPLACED FUEL CAPSDR DL72W011876Angle · crackedNBR 7 SLAT ANGLE CRACKED AT INBD STOP PAD ATTACH FOUND AT F1 LETTER CK REPAIRED PER MM 57-54-000-8SDR DL72W011875Angle · crackedNBR 8 SLAT ANGLE CRACKED AT ANTIICE T DUCT CUTOUT FOUND ON F1 LETTER CHECK REPAIRED PER MM 57-54-000-8SDR DL72S011871Angle · cracked1.5 INCH CRACK UNDER STOP PAD NBR 6 SLAT OUTBOARD STOP PAD. COVE SKIN ANGLE REPAIRED PER M/M 57-54-000-8SDR S01257036Jackscrew · fracturedB-18755 GRD CHK FOUND # 2 FLAP TRACK JACKSCREW FITTING BROKEN.C/A:1.ISSUED REVISION OF EO 740-57-50-0004 TO PERFORM THE REPLACEMENT/OVERHAUL IN LIEU OF INSPECTION. 2.ISSUED THE EON 57-632472-002 TO DETECT THE CORROSION AND CRACK TO AIRPLANES THAT FITTINGS REPLSDR ABXA010579Spar Cap · crackedCRACK ON REAR SPAR LOWER T-CAP AT APPROXIMATELY XCW 3. REPAIRED AREA IAW DC-9 SRM 57-09.SDR DL72S011682Angle · crackedLWR COVE SKIN ANGLE IS CRACKED AT #7 SLAT I/B UPSTOP PAD. SLAT SER # BN324. REPAIRED PER M/M 57-54-000-8SDR DL72W011652Angle · crackedA/C IN TPA FOR E2 LETTER CK. NBR 7 SLAT ANTIICE T DUCT CUTOUT CRACKED. REPAIRED PER MM 57-54-000-8.SDR USAA011129Web · crackedCLT - FOUND ON WALKAROUND, WEB CRACKED .5 INCH AND .125 INCH, WHEEL WELL CEILING AT LBL 30 BS 685. INSTALLED DOUBLER PER TR 53-60-04. (M)SDR ABXA010442Fitting · crackedDURING REPLACEMENT OF THE LEFT WING LOWER AFT SPAR, INSPECTION FOUND WING BULKHEAD ATTACH FITTING CRACKED. LOCATED AT STATION XRS 111, STRINGER 11. REPLACED FITTING IAW DC-9 SRM 51-30-5.SDR ABXA010441Fitting · crackedDURING REPLACEMENT OF THE LEFT WING LOWER AFT SPAR, INSPECTION FOUND WING BULKHEAD ATTACH FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-5.SDR FE5F200200004Spar Cap · corrodedDuring the ¡§C3 Check¡¨ in AUG 2001, this A/C found corrosion on the L/H wing lower rear spar cap, XRS173~175. IAW manufacturer¡¦s instruction, operator performed temporary repair. Now manufacturer determined the accomplished temporary repair is acceptable forSDR WX0A01002Aileron · delaminatedLCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, LEFT AILERON INBOARD TAB DELAMINATION DETECTED ON LOWER OUTBOARD SIDE. DELAMINATION REPORTED TO BE AN AREA OF APPROXIMTELY 5 SQUARE INCHES. CUTOUT DELAMINATED AREA (APPROX 10 INCHES BY 3 INCHES). SDR DL72S011236Angle · crackedCOVE SKIN ATTACH ANGLE CRACKED BELOW TAI DUCT #3 SLAT __REPAIRED PER MM 57-54-000-8SDR DL72S011235Angle · crackedCOVE SKIN ATTACH ANGLE CRACKED BELOW TAI DUCT #2 SLAT __REPAIRED PER MM 57-54-000-8SDR DL72S011234Bracket · cracked3 INCH CRACK AT #1 SLAT ACT. ATTACH I/B AND O/B BRACKET __REPAIRED PER M/M 57-20-021-8SDR DL72S011231Angle · crackedFOUND ON F1 LETTER CK NUMBER 8 SLAT ACTUATOR INBD ATTACH ANGLE CRACKED . REPAIRED PER MM 57-20-021-8.SDR DL72S011223Angle · crackedFOUND ON MV4 1/4 CRACK IN #2 SLAT COVE SKIN ANGLE BELOW TAI DUCT. REPAIRED PER MM 57-54-000-8SDR GAIA01223STAngle · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED RIGHT WING LEADING EDGE CAVITY UPPER ATTACH ANGLE CRACKED AT SLAT STATION .260, WL 343. ACCOMPLISHED RIGHT WING LEADING EDGE CAVITY UPPER ATTACH ANGLE REPLACEMENT WS 343, SLAT STATION .260 IAW B727 SRM SDR RRXA11322Wedge · dentedDURING A MAINTENANCE VISIT FOUND DENTED DAMAGE TO L/H O/B FLAP T/E WEDGE AT STA.340-410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21.SDR RRXA11365Skin · corrodedDURING A MAINTENANCE VISIT FOUND R/H WING L/E SKIN DISBONDED & CORROSION AT XFS 300. *** CORRECTIVE ACTION *** REMOVED CORROSION, THICKNESS 0.82 - 0.88, MATERIAL LOSS WITHIN LIMITS. TREATED AND PRIMMED IAW SRM 51-1-8 AND 57-5-0 FIG 7 RESPECTIVELYSDR 2001FA0000219Nut · crackedDURING INSPECTION FOR ANNUAL, CRITERION AND FREQUENCY FOR WING BOLT INSPECTION. RECEIVED NEW HARDWARE. SENT OUT HARDWARE FOR MAGNETIC PARTICLE PROCESS PER MM. NDT PERSONAL INFORMED OF CONDITION OF NEW NUTS, STATING ROUGH INSIDE SURFACE AND LINEAR INDICATIONSDR ABXA010354Fitting · crackedSTRUCTURAL FITTING ON LEFT WING LEADING EDGE ON OUTBOARD SIDE OF #7 SLAT TRACK CRACKED BETWEEN TWO LOWER FASTENER HOLES. REPAIRED AREA IAW DC-9 REA D957-41317.SDR RRXA11255Doubler · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING CENTER L/E AT STA. XS461.372, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D SDR P2EA01092Tube · damagedMCI - FLT 906 - DURING WALK AROUND, FOUND THAT THE AIRCRAFT REFUELING DOOR HAD BEEN LEFT OPEN ON ITS FLIGHT FROM MSY. DAMAGE WAS CAUSED TO AN ANTI-ICE DUCT, TWO HOLD OPEN RODS AND ATTACH BRACKETS IAW BOEING MM 30-22-0, 57-30-00. (M)SDR USAA010720Angle · crackedPIT - FOUND ANGLE CRACKED 1 INCH, STATION 540 LEFT WING ROOT 2 INCHES ABOVE STRINGER. REMOVED DAMAGED AREA, INSTALLED FILLER, REPAIR ANGLE PER TR 53-50-03. (M)SDR USAA010721Angle · crackedPIT - FOUND ANGLE CRACKED 1 INCH, STATION 540 RIGHT WING ROOT 2 INCHES ABOVE STRINGER 22R. REMOVED DAMAGE, INSTALLED FILLER AND REPAIR ANGLE PER TR 53-50-03. (M)SDR SIMA200113111Bushing · corrodedSBP - DURING MBV MAINTENANCE, FOUND THE RIGHT MAIN LANDING GEAR INBOARD CONNECTING LINK AFT BUSHING IS CORRODED. REMOVED AND REPLACED BUSHING IAW SAAB AMM 57-40-05. (M)SDR SIMA200113112Bushing · corrodedSBP - DURING MBV MAINTENANCE, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD CONNECTING LINK AFT BUSHING IS CORRODED. REMOVED AND REPLACED BUSHING IAW SAAB AMM 57-40-05. (M)SDR C2XA01IA277Support · crackedSJK - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUR (4) SKIN SUPPORTS WERE FOUND TO BE CRACKED IN THE LEFT WING AT RIB 8. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA01IA276Support · crackedSJK - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, TWO (2) WING SKIN SUPPORTS WERE FOUND TO BE CRACKED AT RIB 20 OF THE LEFT HAND WING. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR RRXA10885Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H CENTER L/E AT STA XFS 291-500 AND 304.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2, 51-1-21 AND 51-1-20D.
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