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 EIA2003007Skin · corrodedFS 1350 RBL4 TO LBL4 TOP SURFACE OF WING BOX PILLOWING (CORROSION). REMOVED DAMAGE, NDT AREA, FAB'D & INSTALLED REPAIR PARTS PER ECRA 481-53-165-2.SDR 2003UALA00105Skin · dentedSCRAPE ON BOTTOM SURFACE OF RIGHT WING, 3 FEET INBD FROM TIP. FOUND DENT 3 BY 6 INCHES WITH DELAM. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED QUADRUPLER REPAIR.SDR DHL2003804668Door · crackedRT WING L/E OUTBD. SLOT DOORS SHOW .5000 CRACKS ON THREE SECTIONS BETWEEN STA. 435.789 - XS520.168 REMOVED DAMAGED L/E SLOT DOORS IAW MM 27-80-2 PG. 201-203 PERFORMED NEW HOLESAND COUNTERSUNK IAW SRM 51-1-22 FIG. 476 . INSTALLED NEW SLOT DOORS ON THE THREE SECSDR DL72S021413Angle · crackedNO. 12 SPOILER ACTUATOR ATTACH BRACKET CRACKED OUT BOARD ENDREPLACED ATTACH ANGLESDR CA021121002Fairing · damaged(CAN) PANELS 462EL AND 462FL FOUND MISSING OFF NR 2 ENGINE PYLON AND NR 1 TRAILING EDGE FLAP AND CANOE FAIRING FOUND DAMAGED ON WALK AROUND. AIRCRAFT WAS ON A DELIVERY FLIGHT AFTER HAVING UNDER GONE A HEAVY MAINTENANCE VISIT IN SINGAPORE. AIRCRAFT RELEASED FROSDR DL72S021344Stiffener · crackedNBR #3 SLATI/B ACT CASTING CRACKED AT FASTNER HOLE REMOVE AND REPLACE STIFFENERSDR DL72S021343Angle · cracked1/4IN CRACK AT NO.4 L/E SLAT LWR COVE SKIN ANGLE AT O/B STOP PAD REPAIRED PER MM 57-54-000-8SDR ABXA020315Support · crackedINBOARD SPOILER ACTUATOR OUTBOARD SUPPORT FITTING WAS CRACKED AT UPPER FLANGE. REPLACED SUPPORT IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA020314Former · crackedTHIRD LEADING EDGE RIB OUTBOARD OF #11 SLAT TRACK CRACKED AT AFT UPPER END. REPLACED RIB IAW DC-9 SRM 51-30-2, 51-30-5, AND 51-10-3B.SDR DL73K021205Skin · gougedUPPER SKIN WORN THROUGH AT NO 2 T/E FOREFLAP REPAIRED PER SRM 51-40-20 FIG 12SDR IXXA0200143SWing · crackedDURING ROUTINE C CHECK INSPECTION A CRACK WAS DETECTED ADJACENT TO THE INBOARD FIRE BOTTLE VIEWING DOOR ON LEFT WING LOWER LEADING EDGE. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS SSDR IXXA0200142SWing · crackedDURING ROUTINE C CHECK INSPECTION, CRACKS WERE DETECTED JUST OUTBOARD OF THE INBOARD STUB WING AREA ON THE LEFT WING UPPER LEADING EDGE. REPAIRED ACCOMPLISHED REMOVAL OF DAMAGED AREA FABRICATION AND INSTALLATION REPAIR OF DOULBER IN ACCORDANCE WITH THE DOUGLASSDR ABXA020285Strut · corrodedLEFT WING FIXED LEADING EDGE RIB, W.S. 456.98, HAD CORROSION IN ANTI-ICE TAIL DUCT TO LEADING EDGE SLAT AT WING FIXED LEADING EDGE RIB. REMOVED CORRODED RIB AND INSTALLED NEW STRUT IAW BOEING SRM 51-40-02, 57-41-09, AND BAC DWG 114T2202.SDR ABXA020259Support · crackedRIGHT WING OUTBOARD SPOILER TORSION BAR SUPPORT FITTING CRACKED AT UPPER END. REPLACED FITTING IAW DC-9 SRM 51-30-1.SDR ABXA020249Fitting · crackedSLAT TRACK X0S 429.1, INBOARD SUPPORT FITTING TO FRONT SPAR ATTACH ANGLE CRACKED. REPLACED AREA IAW REA D957-45321 AND DC-9 SRM.SDR IXXA0200138SWing · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE UPPER RIGHT WING, INBOARD OF FUEL PANEL 505F AT THE UPPER AFT PLANK. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR FILLERS AND DOUBLERS IN ACCORDANCE WITH THE DOUGLSDR DHL2002803506PanR/H WING L/E ZEE PAN UPPER PART CRACKED 2 IN AT STA XFS 245.000.REMOVED ZEE PAN PER SRM 51-1-21 PG 1.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW ZEE PAN PER SRM 51-1-21 PG 2,51-3-0 PG 1SDR ABXA020236Support · crackedINBOARD SPOILER TORSION BAR CENTER SUPPORT FITTING WAS CRACKED. REPLACED SUPPORT IAW DC-9 SRM 51-10-4 AND 51-30-5.SDR DL72S021034Web · crackedCRACK ON O/B WEB OF #1 SLAT ACT. MOUNT BRACKET REPAIR PER M/M 57-20-021-8SDR UPS02239396Bracket · corrodedINSPECTION TYPE:C R/H WING REAR SPAR LWR CHORD T BRACKET CORRODED WS 192 TO GAIN ACCESS #2 TANK FRONT SPAR PANELS REMOVED. NEW BRACKET INSTAL LED IOAW BOEING DWG 65-16201, WING PANELS CLOSED.SDR ABXA020288Hinge Fitting · corrodedCORROSION UNDER JUMPER BONDING BOLT, LEFT OUTBOARD AILERON, OUTBOARD HINGE FITTING, W.S. 1127.45. REPLACED FITTING IAW BOEING SRM 57-51-02, IPC 57-51-51-A01, AND DWG 113T1521.SDR IXXA0200118SWing · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE LEFT WING LOWER LEADING EDGE SCREW HOLE. REPAIR ACCOMPLISHED, REMOVAL OF PREVIOUS REPAIR, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF FILLER AND DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCSDR ABXA020126Skin · corrodedCORROSION AT RIGHT WING LOWER SKIN PANEL NO. 1 AT REAR SPAR, BETWEEN STRINGER 230 AND 277. REPAIRED AREA IAW REA B657-43583-MR.SDR DL72S020845Rib · crackedAT F-1 LETTER CK FOUND DOUBLER CRACKED #4 SLAT INBD ACTUATOR ATTACH NOSE RIB FOUND DOUBLER INCORRECTLY SHIMMED, RESHIMED AND REPLACED DOUBLER PER M/M 57-54-000-8 FIG 804SDR DL72S020844Angle · crackedFOUND ON F1 LETTER CK LOWER COVE SKIN ATTACH ANGLE IS CRACKED AT NUMBER 6 SLAT BELOW ACTUATOR. REPAIRED PER MM 57-54-000-8SDR DL72S020832Angle · crackedFOUND ON E1 LETTER CK. 1 INCH CRACK AT COVE SKIN ATTACH ANGLE NBR 6 SLAT BELOW ACTUATOR ROD REPAIRED PER M/M 57-54-000-8 FIG 805A,SDR DL72S020831Angle · crackedFOUND ON E1 L/C 1.25 INCH CRACK NBR 5 SLAT COVE SKIN ATTACH ANGLE AT INBD END REPAIRED PER M/M57-54-000-8 FIG 805ASDR 02FDEA00493Wing · corrodedINBD LT WING UNDER SURFACE TRAILING EDGE AT ZONE 575 FND CORRODED. TEMPORARY REPAIR PER E.A. 6-5710-64295.SDR ABXA020138RibLEFT WING LEADING EDGE SLAT #6 AUXILIARY RIB ASSEMBLY P/N 1143170, AUXILIARY RIB HAD MISDRILLED HOLE. REPAIRED AREA IAW REA B657-43455-MR.SDR ABXA020125Skin · crackedA 0.06" LONG CRACK WAS FOUND IN ONE FASTENER HOLE IN THE RIGHT UPPER WING WHILE ACCOMPLISHING SERVICE BULLETIN SB 767-54-0081. REPAIRED AREA IAW REA B657-43512-MR.SDR ABXA020124Skin · crackedA 0.06" LONG CRACK WAS FOUND IN ONE FASTENER HOLE IN THE UPPER LEFT WING SKIN PANEL AS SHOWN IN REF. (5) - SB 767-54-0081. REPAIRED AREA IAW REA B657-43511-MR.SDR ABXA020158Doubler · crackedANGLED DOUBLER COMMON TO #7 SLAT TRACK RIB INBOARD AND FRONT SPAR CRACKED. REPAIRED AREA IAW DC-9 SRM 57-09.SDR ABXA020103Fitting · cracked#4 ALT HAD A CRACKED STRINGER END FITTING AT XRS 408. SPLICE - STRINGER 59 AFT SIDE. INSTALLED NEW END FITTING AND BOOST PUMP BRACKET IAW DC-8 SRM 51-1-24, 51-1-8, AND 51-1-20D.SDR ABXA020047Slat · corrodedRIGHT WING #11 SLAT INBOARD LEADING EDGE ANGLE WAS CORRODED. REMOVED CORROSION OUT OF LIMITS IAW B767 SRM 57-43-02. REPAIRED AREA IAW B657-43913MR.SDR SIMA200216402Panel · corrodedDURING MBV-1 INSPECTION, RIGHT AILERON OUTBOARD UPPER PANEL CORRODED AROUND SCREW HOLES.SDR ABXA020040Frame · crackedCANTED FRAME 1137 HAD 2 EACH CRACKS COMMON TO STIFFENERS AT 11 AND 1 O'CLOCK POSITIONS. REPLACED LEFT AND RIGHT FRAMES IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA020039Former · cracked3RD LEADING EDGE NOSE RIB, OUTBOARD OF #11 SLAT TRACK, WAS CRACKED AT FASTENER, LOWER FORWARD END. REPLACED LEFT WING LEADING EDGE RIB FORMER IAW DC-9 SRM 51-30-2, 51-30-5 AND 51-10-3.SDR 2002F00832Skin · corrodedAT C-CHECK, FOUND CORROSION ON TOP OF RIGHT WING REAR SPAR, AT APPROXIMATELY WING STATION 251 TO 357. (M)SDR 2002F00829Skin · corrodedAT C-CHECK, FOUND CORROSION IN MIDDLE OF RIGHT WING TOP SKIN, AT APPROXIMATELY WING STATIN 320. (M)SDR 2002F00826Skin · corrodedAT C-CHECK, FOUND CORROSION ON RIGHT WING TOP SKIN TRAILING EDGE SPAR, AT APPROXIMATELY WING STATION 600. (M)SDR ABXA020049FittingLEFT WING OUTBOARD PITCH LOAD FITTING HAD EXISTING SHORT E.D. REPAIRED AREA IAW REA B657-43882MR.SDR DL72S020581Angle · crackedFOUND ON E1 LETTER CK LOWER COVE SKIN ATTACH ANGLE IS CRACKED BELOW #2 SLAT TAI DUCT. REPAIRED PER MM 57-54-000-8SDR DL72S020580Web · crackedFOUND ON E1 LETTER CK I/B MOUNT WEB CRACKED #1 SLAT ACTUATOR. REPAIRED PER MM 57-20-21-8.SDR DL72W020558Angle · crackedCRACK ON MLG W/W VERT ANGLE STA. 913 @ "H" BRACKET INSTALL TEMPORARY REPAIR PER M/M 53-11-000-8SDR UPS02238319Skin · crackedINSPECTION TYPE:C SUSPECT CRACK ON RH WING LE SKIN AT CUT OUT FOR NO 6 LE SLAT O/B SLA T HOOK REPAIR CARRIED OUT IAW 57-30-4 SRMSDR 2002FA0000577Skin · delaminatedPOSSIBLE WING SKIN DELAMINATION DISCOVERED. CRACKS IN PAINT IS REASON FOR DISCOVERY. POSSIBLE DELAMINATION AREA IS 72" OUTBOARD ON TOP SIDE OF RIGHT WING AND EXTENDS APPROXIMATELY 30" FURTHER OUTBOARD. DELAMINAITON AREA STARTS 2.25" AFT OF THE LEADING EDGE SDR ABXA020143Support Fitting · corrodedMIGRATED BUSHING, RIGHT MAIN LANDING GEAR SIDE STRUT SWIVEL SUPPORT FITTING, AFTER REMOVAL OF PART 113T1108-25, FOUND DEEP CORROSION ON FITTING. REPAIRED AREA IAW REA B657-43443-MR.SDR ABXA010884Clip · crackedLEADING EDGE SPLICE ANGLE CRACKED JUST OUTBOARD OF #6 SLAT TRACK CUT-OUT. REPLACED SPLICE IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA010844Doubler · crackedRIGHT WING 505F PANEL LAND NUT CHANNEL REMOVED, SEALANT REMOVED, AND HOLES POLISHED TO FACILITATE NDT INSPECTION. REPAIRED AREA IAW DC-8 SRM 51-1-20D AND REA D857-43117MR.SDR ABXA010843Doubler · crackedLEFT WING PANEL LAND 505F, UPPER SURFACE, 3 EACH FASTENER HOLES CRACKED. REPAIRED AREA IAW REA D857-43118MR.
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