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 = '5711' 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 = '5711' 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 CALA2011090100567Spar · corrodedRT WING FRONT SPAR CORROSION FOUND AT WS 564.5 AREA RT WING FRONT SPAR WEB AT OFSS 560 - OFSS 570 CORROSION REMOVED AND BLENDED AREA DEPTH 0.061" (ORGI 0.163") X WIDTH 0.86" X LENGTH 1.8" OUT OF SRM 57-20-10 ALLOWABLE DAMAGE FIG 103 LIMITS AND CORRODED FRONT SSDR IPXA11M69235Spar · corrodedINSPECTION TYPE:3C, BULGING SKIN ABOVE RT WING REAR SPAR UPPER SURFACE BETWEEN XORS786-830. REPAIRED CORROSION ON RT WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN XORS 786-830 IAW SRM 51-21-01, STA EA 011-5710-01-A3438 REV IR AND EO MD11-5710-44282-A.SDR FDEA201108293548Spar Cap · corrodedRT WING REAR SPAR CAP FOUND CORRODED. EXCEEDED LIMITS AT XORS 1040. CORROSION REMOVED IAW SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.148"; MATERIAL, REMOVED = 0.034"; MATERIAL REMAINED = 0.114" - FOUND EXCEEDED LIMIT IAW SRM 57-00-00, REV 47, FIGSDR DALA1501840967Spar · crackedWING REAR SPAR CRACKDED AT XRS 164. REPAIRED IAW AA 5710-01110.SDR FDEA201108253468Spar · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AND FOUND RT WING REAR SPAR LOWER CHORD NEAR RIB 1 HAS A CRACKED INDICATION. RT WING REAR SPAR REAMED TO DIAMETER 0.560" IAW EO 6-5710-7-3322 PART 1, WORK STEP 4.G. HIGH FREQUENCY EDDY CURRENT INSPECTION CARRSDR FDEA201108253467Spar · crackedHIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP CARRIED OUT AND FOUND HOLE ITEM 29 ON RT WING REAR SPAR, NEAR RIB 1 WITH CRACK INDICATION. RT WING REAR SPAR CRACKED FASTENER HOLE REAMED TO DIAMETER 0.560 INCH IAW EO 6-5710-7-3322, PART 1, WORK STEP 4G. HIGH FREQSDR AALA20110825TUL02Spar · corrodedLEFT WING AFT SPAR AT LEFT DEFUEL ADAPTER PLATE CORROSION WAS DISCOVERED WHEN CHECKING BONDING OF ADAPTOR PLATE TO WING. REMOVED CORROSION BY SPOT FACING AREA. PERFORMED NDT AND, VISUAL INSP TO ASSURE CORROSION REMOVAL. TREATED SPOT FACE AREA BY ETCHING, ANSDR DALA1515049229Spar · crackedWING REAR SPAR CRACKING REPAIRED IAW AA 5710-01119.SDR REXA201100520Spar · damagedA NR 30 HOLE DRILLED IN RT WING LEADING EDGE SPAR AT WS 353.00 LOWER LEADING EDGE ATTACHING FLANGE 3.90" INBOARD OF WS 353. REPAIRED IAW BOMBARDIER REO 601R-57-21-1486.SDR FDEA201108123248Spar · damagedWHILE ACCOMPLISHING EO 8-5710-7-5007, PT 2 MISDRILLED HOLE WHILE REMOVING FASTENERS. REPAIRED MISDRILLED HOLES BY REWORKING IAW EA 8-5710 -150976. MAJOR REPAIR.SDR IPXA1M68794Former · crackedINSPECTION TYPE:3C, LEFT WING L/E COMPTARTMENT AT STA XOS 1026 RIB SUPPORT CRACKED AT AFT END. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT RIB SUPPORT IAW DWG ARB2920, SRM 51-31-01, AND SRM 51-33-01.SDR FDEA201108053103Spar · corrodedRT WING REAR SPAR LOWER CHORD FOUND CORROSION LOCATED AT XORS 1042 -1070 AREA. CORROSION REMOVED AND PROTECTED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.060", MATERIAL REMOVED = 0.020" , REMAINED THICKNESS = 0.040", DIA. IS 27" X 1.25" FOUND EXCEEDED LSDR 2011FA0000496Spar · crackedFOUND SAFETY ISSUES WITH ALL FOUR WING SPARS ON THIS AIRCRAFT. THE WOODEN SPARS HAD SEVERAL CRACKS AND VARIOUS OTHER DEFECTS. I HAVE ALSO E-MAILED PICTURES OF SOME OF THE MORE NOTICEABLE AREAS. THIS AIRCRAFT WAS RECENTLY RESTORED AND NEW FABRIC WAS INSTALLED OSDR IPXA1M68541Spar Cap · corrodedINSP TYPE:3C, RT WING UPPER T/E PANEL BULGING ABOVE REAR SPAR CAP AT APPRX STA. XORS 675-690. GAINED ACCESS TO CORROSION ON AFT FLANGE OF RT REAR SPAR UPPER CAP AT XORS 675-690. CORROSION EXCEEDED ALLOWABLE LIMITS IAW SRM 57-00-10. REPAIRED CORROSION IAW STASDR K11A2011090772202Stiffener · corrodedWING FRONT SPAR STIFFENER CORROSION, 1X4 INCHES AND .5X1 INCHES.SDR K11A2011090772201Stiffener · corrodedWING FRONT SPAR STIFFENER CORROSION, 1X3 INCHES.SDR FDEA201107122651Spar · corrodedRIGHT WING L/E FRONT SPAR LOWER DOUBLER AT STA XORS 815 FOUND CORROSION. CORROSION. REMOVED IAW SRM 51-21-01, REV 47 FOUND EXCEEDED LIMIT, ORIGINAL THICKNESS =0.180", MATERIAL REMOVED = 0.140", REMAINED THICKNESS = 0.040", DIA IS 6' X 2.375" IAW SRM 57-40-SDR CA110711013Spar Cap · crackedRT WING LOWER SPAR CAP FOUND CRACKED AT STA Y3815.00 (RIB 9) THE CRACK IS FROM CAP EDGE THROUGH SCREW HOLE AND CONTINUE (.850").SDR FDEA201107072608Spar Cap · crackedRT WING REAR SPAR CAP HAS 2 HOLES WITH CRACK INDICATION. ACCOMPLISHED LIMITED REPAIR REF EA 8-5710-147784. PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 24 MONTHS.SDR CALA2011070700460Spar · corrodedLT WING L/E FRONT SPAR FOUND CORROSION AT OFFS 449 AREA L WING L/E FRONT SPAR WEB. CORROSION REMOVED AS PER SRM 51-10-02, REMOVED AREA DEPTH 0.121" (ORG. 0.185") WIDTH 1"X LENGTH 3" OUT OF SRM 57-20-10 ALLOWABLE DAMAGE 1 FIG 103 LIMIT AND FRONT SPAR WEB CORROSDR CHQA201100262Spar Cap · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE RIGHT WING FRONT SPAR LOWER CAP FROM THE CAP EDGE THROUGH THE SCREW HOLE. THE AIRCRAFT IS CURRENTLY IN C-CHECK INSPECTION.SDR IPXA1568074Spar · corrodedINSPECTION TYPE:C-CK, LT WING SPAR AT IRSS 211, STIFFENER IS CORRODED AROUND ATTACHMENT HOLE FOR DEFUEL VALVE BONDING JUMPER. REMOVED DAMAGE ON LT WING REAR SPAR STIFFENER AT IRSS 211 IAW EA 1108 09.SDR HYIA20110621001Spar · corrodedDURING HEAVY CHECK INSP, CORROSION WAS FOUND ON LT WING AFT SPAR UPPER HORIZ FLANGE AND UPPER SKIN AT RIP 29. THE CORROSION WAS REMOVED AND DAMAGE BLENDED IAW ATR S.R.I. DO/TS-3042/11-15468. THE REPAIR WAS PERFORMED BY TECH SERVICES UNDER WO 17010, TASK 323.SDR FDEA201106082184Spar · crackedLT WING LOWER T/E, FALSE SPAR INBD END IS CRACKED AT WBL118. REMOVED WEB AND DOUBLER IAW SRM 51-30-2 REV 103. CUT OUT CRACKED LOWER SPAR CHORD IAW DRAWING SR 27-57-038 REV C. FABRICATED NEW WEB, DOULER, SPAR CHORD SECTION, RADIUS FILLER, 2EA RADIUS BLOCKS ANDSDR DALA1140570627Spar · damagedWHILE PERFORMING WINGLET MOD FOUND 2 EA HOLES AT WSTA 810 WITH INCOMING TOOLING MARKS LT WINGLET FWD SPAR WEB. COMPLIED WITH AT SAA/SAT ON NON ROUTINE 195146.W/O 87883240001. AS PER ER/A 493028-14,SDR HYIA20110601001Spar Cap · corrodedDURING HEAVY CHECK INSPECTION CORRIOSON WAS FOUND ON THE RT WING AT THE AFT SPAR UPPER CAP VERTICAL FLANGE BETWEEN RIBS 27-30. CORROSION WAS FOUND TO BE OUT OF THE LIMITS OF THE SRM AND REQUEST FOR STRUCTURAL REPAIR INSTRUCTION WAS SUBMITTED. CORROSION WAS RSDR K11A2011082491502Spar · crackedUPPER AFT CENTER SPAR CHORD CRACKED, 1X8 INCHES.SDR K11A2011082391507Spar · corrodedWING REAR SPAR CORROSION, 1X2 INCHES.SDR DALA1139719861Doubler · crackedLEFT WING REAR SPAR WEB DOUBLER O/B SIDE OF AFT DOUBLER IS CRACKED, REF: EM 5710-00028, SECTION 03 UPON FURTHER INVESTIGATION, ALL WORK TO BE COMPLIED WITH ON WORK CARD 5710-00028-08A (LEFT WING SPAR AND/OR DOUBLER TRIM REPAIR) JOB 000-0009, WO 87938350001.SDR AALA20110520TUL12Spar · corrodedRIGHT WING REAR SPAR AT SPAR SHUTOFF ACTUATOR ADAPTER SHAFT/PLATE CORROSION UNDER PLATE. REMOVED CORROSION PER SRM 51-10-02. SPOT FACED, CLEANED HOLES AND FACE OF SPOT FACE. PERFORMED HFEC HOLE PROBE OF FASTENER HOLES. PERFORMED FPI INSPECTION IN REWORKED SDR 2011FA0000334Spar · corrodedDURING REPAIR OF LT WING THE AFT SPAR ATTACH FITTING WAS REMOVED. SEVERE CORROSION WAS FOUND UNDER THE FITTING. PROBABLE CAUSE IS TRAPPED MOISTURE, LACK OF PREVENTATIVE TREATMENT AND LACK OF PROPER INSPECTION OF AREA.SDR HALA2011051700238Spar Cap · corrodedRT WING - OTBD T/E FLAP HAS EVIDENCE OF CORROSION ON UPPER AFT SPAR CAP AT INBD END. CORROSION FOUND BEYOND LIMITS SRM 51-10-02-09-0 REV 85. REPAIR CARRIED OUT. CORROSION REMOVED IAW SRM 51-10-02-09-0, REV 85. FPI CHECK CARRIED OUT TO CONFIRM CORROSION REMOVSDR DALA1138930915Spar · crackedCRACKED NEW REAR SPAR BEAM LT WING. REMOVED DAMAGED AREA.SDR DALA1507610904Spar · crackedWING REAR SPAR CRACKED AT XRS 164. REPAIRED IAW AA 5710-01110.SDR AALA20110805TUL03Spar · corrodedRIGHT WING UNDER DEFUEL VALVE ADAPTER SHAFT PLATE HAS PITTING CORROSION. REPAIRED PER EA B757-57-017276 DATED 06-23-11.SDR ABXA2011051045Spar · damagedRT SPAR SIDE FRAME STA 955 (PICKLE FORK) LEVELING COMPOUND SHRUNK, CRACKED AND LIFTED IN SEVERAL AREAS. CORROSION IS ALSO EVIDENT IN AFT CENTER POCKET. REMOVED LEVELING COMPOUND FOUND SIDE FRAME (PICKLE FORK) CORRODED. REMOVED AND REPLACED SIDE FRAME IAW B7SDR GUUA94057050211DSpar · corrodedDURING SCHEDULED X-RAY INSPECTION DISCOVERED RIGHT WING LOWER MAIN SPAR AREA OF CORROSION BETWEEN WS 124.25 TO WS 135.86. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP.SDR ABXA2011051752Spar · corrodedLW FWD UPPER SPAR IS CORRODED EXTERIOR SURFACE AT LES698. REPAIRED UPPER SPAR IAW B657-59256. CORROSION 3.5" X 1.2" X .062.SDR FDEA201104291674Spar · crackedULTRASONIC INSP CARRIED OUT ON LT WING, FOUND ULTRASONIC INDICATION MORE THAN 30 PERCENT ON THE HOLE 'B' AT REAR SPAR UPPER CHORD OTBD OF RIB 9. REPAIRED AS PER E.A. 6-5730-150317 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.SDR DALA1138910915Spar · crackedTHREE CRACKS ON LEFT WING REAR SPAR. REMOVED AND REPLACED SECTION OF WEB FROM XRS 103-204.SDR FDEA201104281669Spar Cap · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON THE CENTER WING BOX CENTER SPAR, AT RIGHT CUT-OUT DOUBLER RUNOUT RIGHT SIDE UPPER HOLE SECOND LAYER AT 6 O' CLOCK POSITION LOOKING FORWARD. CRACKED AT CENTER WING BOX CENTER SPSDR FDEA201104281668Spar Cap · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON THE CENTER WING BOX CENTER SPAR, AT RIGHT HAND CUT-OUT DOUBLER RUNOUT LEFT SIDE LOWER HOLE FIRST LAYER AT 12 O' CLOCK POSITION LOOKING FORWARD. CRACKED AT CENTER WING BOX CENSDR FDEA201104281667Spar Cap · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON THE CTR WING BOX CTR SPAR, AT RT CUT-OUT DOUBLE RUN OUT LT LOWER HOLE SECOND LAYER AT 12 O' CLOCK POSITION LOOKING FORWARD. REPAIRED AS PER EA 6-5710-150318 PART 1. REPAIR CLASSSDR FDEA201104281666Spar Cap · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON THE CTR WING BOX CTR SPAR, AT RT CUT-OUT DOUBLE RUN OUT LT UPPER HOLE FIRST LAYER AT 12 O' CLOCK POSITION LOOKING FORWARD. REPAIRED AS PER EA 6-5710-150318. REPAIR CLASSIFIED ASDR FDEA201104281665Spar Cap · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON THE CTR WING BOX CTR SPAR, AT RT CUT-OUT DOUBLE RUN OUT LT UPPER HOLE SECOND LAYER AT 12 O' CLOCK POSITION LOOKING FORWARD. REPAIRED AS PER EA 6-5710-150318 PART 1. REPAIR CLASSSDR FDEA201104281664Spar Cap · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON THE CTR WING BOX CTR SPAR, AT LT CUT-OUT DOUBLE RUN OUT RT UPPER HOLE SECOND LAYER AT 12 O' CLOCK POSITION LOOKING FWD. REPAIRED AS PER EA 6-5710-150318 PART 1. REPAIR CLASSIFIED AS MSDR FDEA201104281663Spar Cap · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON THE CTR WING BOX CENTER SPAR, AT LT CUT-OUT DOUBLE RUN OUT UPPER HOLE SECOND LAYER AT 6 O' CLOCK POSITION LOOKING FWD. REPAIRED AS PER EA 6-5710-150318 PART 1. REPAIR CLASSIFIED AS SDR CA110504006Spar · misrepairedDURING INSPECTINO, PAINT WAS REMOVED FROM WING AND A LARGE AMOUNT OF FILLER WAS DISCOVERED NEAR THE WING TIP. UPON REMOVAL OF THE FILLER AN UNDOCUMENTED PATCH WAS DISCOVERED. UPON FURTHER INVESTIGATION IT WAS DISCOVERED THAT THE TIP RIB PN 33408-4 AND THE NESDR USAA2011051191834Spar · crackedMCN - C23 - CRACK ON RIGHT MAIN LANDING GEAR TRUNNION SPAR CHORD AT HOLE COMMON TO MAIN LANDING GEAR FITTING AT WBL 157. REPAIRED RIGHT MAIN LANDING GEAR TRUNNION SPAR CHORD AT HOLE COMMON TO MAIN LANDING GEAR FITTING AT WBL 157 IAW EA 130570.SDR CHQA201100144Spar · crackedDURING INSPECTION A CRACK WAS FOUND ON THE RIGHT WING FRONT SPAR LOWER FLANGE BETWEEN RIBS 15 AND 16. THE AREA OF THE SPAR FLANGE THAT WAS CRACKED WAS REMOVED AND WAS PATCHED IAW TI-145-11-100 WITH NO FURTHER DEFECTS NOTED.
Back to JASC 5711