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 00FDEA00749Spar Cap · corrodedRT WING UPPER ACCESS PNL FWD OF NR 4 SPOILER LIFTED. CORRODED AT XORS 683 REAR SPAR TOP SURFACE PER SRM 51-21-01 VOL II. *S/D* BLENDED AS PER FEDEX EA 1-5750-53258.SDR QXEA0002904Spar · scratchedYXX- SCRATCHES FOUND ON FRONT SPAR LEADING EDGE ATTACHMENT FLANGE, RIGHT HAND SIDE UPPER FLANGE BETWEEN YW210-315. REPAIRED IAW DHC-8 RD 8-57-1119 AND DHC-8 SRM 51-20-16, 51-20-36.SDR UPS00234503Spar · crackedINSPECTION TYPE:C, CRACK INDICATION AT LEFT WING UPPER CHORD OF THE REAR SPAR UPPER ROW FASTENER WS 568. INSTALLED REPAIR IN ACCORDANCE WITH SRM 57-10-6 FIG 2. MATERIAL USED (1) ANGLE, 7075--T6,0.080 INCH, 20.5 X 2 INCHES AND (1) ANGLE 7075-T6, 0.080 INCH, 1SDR MWEA001145Trunnion · corrodedLEFT MAIN LANDING GEAR TRUNNION ATTACH LUG FOR FIXED SIDE BRACE HAS LIGHT CORROSION ON FORWARD AND AFT FACES. BONDED WASHER TO LUG PER TELEX MWX-ORD-00-00552H.SDR RRXA003263Spar · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE AFT REAR SPAR ATTACH ''T'' FITTING AT STA XRS 446, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DSDR RRXA003275Spar · gougedDURING A MAINTENANCE VISIT FOUND 3 GOUGES ON BOTTOM SIDE OF ATTACH ANGLES AT REAR SPAR AT STA 690, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED DAMAGE AREA AND RETURNED TO SERVICE IAW EO 00-257SDR 20010326CW008Spar · damagedDURING HIDDEN DAMAGE INSPECTION SOME LIGHT DABAGE TO MID LEADING EDGE SKIN AND ONE NOSE RIB WAS FOUND. UNAPPROVED REPAIR FOUND TO AFT INBD SPAR ASSY. DAMAGE WAS FOUND ON ALMOST ALL NOSE RIBS IN WING. RECORDS CHECK BY OWNER FOUND WING WAS REPAIRED AND RETURNESDR QXEA0002804Spar · tool damageYXX- TOOLING DAMAGE FOUND ON FORWARD SPAR UPPER TANG. REPAIRED IAW DHC-8 RD8-57-1675.SDR RRXA003830Frame · damagedDURING A MAINTENANCE VISIT FOUND HOLE DAMAGE TO LOWER FRAME AT STA. XFS416, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-4.SDR 20001103SH005Spar · corrodedINSPECTION OF LEFT AND RIGHT WINGS DUE TO ACCIDENT. EXFOLIATION CORROSION IN LOWER SPAR CAP WAS FOUND IN THE SAME AREA ON LEFT AND RIGHT WING SPARS. CORROSION IS LOCATED JUST OUTBOARD OF SPAR SPLICE CONTINUING ON TO WING TIP OR SPAR END. DAMAGE IS EXTREMELYSDR AT0000446Spar · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON RIGHT WING FORWARD SPAR WEB AND SPAR CAP AT BS 414 AND BS 426. INSTALLED FILLER AND REPAIR ANGLE IAW REO L00277.SDR P2EA00253Angle · crackedSJO - DURING C-CHECK, FOUND LT WING FRONT SPAR VERTICAL ANGLE AT FSS 346 CRACKED (L = 1.5 INCHES). FABRICATED AND REPLACED ANGLE IAW SRM 51-10-00 PAGE 8. (X)SDR 0003229936Spar · corrodedBULGED CORROSION ON LEFT WING LEADING EDGE SPAR XRS 290. REMOVED FASTENERS, CUT OUT DAMAGE, FABRICATED FILLER FORM 7075-T6. FABRICATED DOUBLER FROM .063 17-7, HEAT TREATED TO 1050. REINSTALLED PER EA 99-177304.SDR UIEA00041Spar · corrodedDURING VISUAL INSPECTION OF CENTER WING REAR SPAR, FOUND WEB CORROSION TO THE UPPER CHORD AT BS 1241 LBL 4. REMOVED CORROSION FROM WEB SURFACE IAW SRM 57-10-01. REMOVED FASTENERS IN UPPER CHORD. PERFORMED HFEC INSPECTIONS OF WEB AND FASTENER HOLES, NO CRACKSDR 0003239936Spar Cap · corrodedAREAS OF CORROSION ON WING STA XRS 225 TO 234 AND 260 TO 290. AREAS INCLUDED LEADING EDGE SKIN, SPAR CAP, WING SURFACE. REPAIRS ACOMPLISHED ACCORDING TO EA 99-177304 AND EA 99-177299. L/P''S 1498556, 1497625, 1497623, 1498548, 1498466, AND 1498473.SDR EISA20000164Spar · corrodedRT WING AFT SPAR UPPER CHORD CORRODED 15 INCHES I/B OF O/B FLAP O/B TANS AT APPROX WS 626. REMOVED, FABRICATED 2 Z-STIFFENERS AND FILLERS AND ANGLES LOCATED, DRILLED, DEBURRED, AND INSTALLED IAW B727-200 SRM 51-10-2, 51-10-6, 51-30-2, 57-10-6, 57-10-1 AND MM SDR AU000815Angle · corroded(AUS) LEFT WING UPPER SPAR CAP ANGLE CONTAINED EXFOLIATION CORROSION. (X)SDR AU000814Angle · corroded(AUS) RIGHT WING LOWER SPAR CAP ANGLE CONTAINED INTERGRANNULAR CORROSION. (X)SDR ABXA000452Spar · crackedLEFT WING SPAR WEB DOUBLER CRACKED AT STATION XRS 146. REPAIRED LEFT WING SPAR DOUBLER IAW DC9 SRM.SDR CALA0001407Spar Cap · corrodedINSPECTION FOUND CORROSION ON CENTER WING FORWARD LOWER SPAR CAP AT XCW 0.0. THE SPAR CAP WAS REPAIRED IAW ECRA 5311-01104 AND FLS DRAWING 90-53-1071.SDR DL73E001722Beam · tool damageTHE AFT TRUNNION BORE OF THE LT WING MLG SUPPORT BEAM SUFFERED TOOLING DAMAGE IN THE HOLE BORE. THE BORE WAS OVERSIZED TO REMOVE THE TOOLING DAMAGE, ROTO PEENED, AND AN OVERSIZE BUSHGING INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 378444-14.SDR TWAA0014304Spar · crackedDURING OP 15 MAINT CHECK ON THE RT WING HAD A CRACK INDICATION ON REAR SPAR AT TOP HOLE FOR CENTER FLAP HINGE MOUNT AT STA XW251. REPAIRED HOLE PER DOUGLAS DRAWING JO6022.SDR EIA2000258Splice · crackedC1-CHECK, FOUND RHW REAR SPAR UPPER SPLICE FITTING AFT EDGE CRACKED CORNER ON FITTING UPPER SURFACE APPROX .1875 INCH IN LENGTH, AND SUSPECT CRACK SIGNAL AT ONE FASTENER HOLE. CARRIED OUT EO57-757-1011 SPLICE FITTING REPLACEMENT. (M)SDR AU000860Spar · corroded(AUS) REAR SPAR UPPER CHORD CORRODED AT UPPER SKIN INTERFACE INBOARD OF NR 4 SPOILER INBOARD HINGE. FOUND DURING CORROSION INSPECTION.SDR AU000861Spar Cap · corroded(AUS) REAR SPAR CAP CORRODED AT UPPER SKIN INTERFACE ADJACENT TOOUTBOARD FLAP OUTBOARD JACKSCREW GEARBOX. FOUND DURING CORROSIONINSPECTION.SDR TWAA0014307Spar · crackedDURING OP 15 MAINT CHECK, FOUND ON RT WING A CRACK APPROX .0625 INCH LONG ON REAR SPAR AT XW154, I/B FLAP HINGE LOWER O/B HOLE. CRACK CONTAINED PER NDT TWA 51-10-03 PART 6 HFEC. MADE REPAIR DOUBLER AND INSTALLED PER REPAIR DRAWING JO60271. REPAIR WORK IN COSDR AU000711Spar Cap · corroded(AUS) LEFT LOWER SPAR CAP CORRODED IN AREA BETWEEN THE FUSELAGE AND WHERE THE LOWER SKIN BEGINS. THE AREA IS COVERED BY AN ALUMINIUM ADHESIVE TAPE USED AS AN ANTI-CHAFING STRIP AND THE CORROSION WAS FOUND FOLLOWING REMOVAL OF THE TAPE. (X)SDR AU000690Spar · cracked(AUS) LT AND RT WINGS FORWARD AND REAR SPARS CRACKED IN AREA LOCATED OUTBOARD OF RIB NR 13.SDR AU000652Spar · corroded(AUS) LEFT WING MAIN SPAR CONTAINED PATCHES OF INTERGRANULAR CORROSION. (X)SDR RRXA002986Spar · damagedDURING A MAINTENANCE VISIT FOUND 7 DEFORMED BOLT HOLES TO THE RT CENTER AUX TANK AFT LT INNER ACCESS HOLE UPPER REAR SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.SDR RRXA002985Spar · damagedDURING A MAINTENANCE VISIT FOUND 4 DEFORMED BOLT HOLES TO THE LT CENTER AUX TANK AFT RT INNER ACCESS HOLE UPPER REAR SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.SDR AU000770Spar Cap · corroded(AUS) LEFT WING LOWER SPAR CAP CORRODED. SPAR CAP EXHIBITS SIGNS OF PREVIOUS UNAPPROVED REPAIRS. FOUND DURING INSPECTION IAWAD/C400/40 AMDT13. (X)SDR AU000769Spar · corroded(AUS) LEFT WING REAR SPAR ASSEMBLY UPPER AND LOWER SPAR CAPS CORRODED. FOUND DURING INSPECTION IAW AD/C400/40 AMDT13. (X)SDR UPS00233734Spar · corrodedINSPECTION TYPE:C, OPEN AREA AT LOWER CHORD, AFT SPAR ON CENTER TANK OUTBOARD END, LEFT SIDE INSPECTION FOR SUSCEPTIBLE CORROSION. ACCOMPLISHED REPAIR OF WING CENTER SECTION REAR SPAR LOWER CHORD AT BBL 41.82 IAW UPS EO B727-5710-13234-A AND BOEING TELEX PRO-SDR UPS00233737Spar · corrodedINSPECTION TYPE:C, CORROSION ON CENTER TANK, AFT SPAR, UPPER CHORD, OUTBOARD END, LEFT SIDE. ACCOMPLISHED WING CENTER SECTION REAR SPAR UPPER CHORD CORROSION REP AIR BETWEEN LBL 39.07 & LBL 70 IAW UPS EO B727-5710-13233-A, AVITAS EINGINEERING REPAIR ORDER AVHSDR USAA001335Spar · crackedPIT - FOUND REAR SPAR CRACKED .75 INCH, STATION 164 FLAP HINGE INBOARD LOWER STUD HOLE RIGHT REAR SPAR. INSTALLED TEMP REPAIR WITH REPEAT INSPECTIONS AT LOWER SPAR (REPUBLIC REPAIR) PER EA 2J06027-506, 55836. (M)SDR EIA2000240Spar · corrodedB-CHECK, CENTER TANK FRONT SPAR LOWER CHORD FOUND CORRODED AT DRAG SPLICE FITTING AT STATION 990 STRINGER 38R. CORROSION REMOVED PER SRM 51-10-01 AND REPROTECTED PER SRM 51-10-02. CORROSION BLEND OUT DEPTH .010 INCH, WIDTH 1 INCH, LENGTH 4 INCH WITH SRM 51-1SDR 0002936717Spar · crackedDURING M'' CHECK, STRESS CORROSION AND CRACKS WERE FOUND AT RIGHT WING FRONT SPAR LOWER CHORD AT FSSO 1460. REPAIRED PER EA 67-178254.SDR 0002926717Spar Cap · corrodedDURING M CHECK, FOUND STRESS CORROSION AND CRACKS AT RIGHT WING FRONT SPAR LOWER CHORD AT FSSO 1487. REPAIRED PER EA 67-178257.SDR RRXA003820Spar · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT CENTER AUX. TANK AFT LT INNER ACCESS HOLE UPPER REAR SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW EO 00-196 WITH APPROVSDR RRXA002796Spar · crackedDURING A MAINTENANCE VISIT FOUND A SMALL CRACK INSIDE OF HOLE EDGE ON THE RT CENTER AUX TANK AFT LT INNER ACCESS HOLE UPPER REAR SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED ISDR 2002FA0000178Strap · defectiveDEFECT IN SK SPAR STRAP SYSTEM.SDR 0003066717Spar · crackedDURING M CHECK, FOUND CRACK ON RIGHT WING MIDSPAR WEB AT WS 394 FASTENER LOCATION NR 37 COMMON TO THE UPPER CORD. REPAIRED PER EA 67-178260.SDR 0002706717Spar · crackedDURING C CHECK, FOUND CRACK IN THE MIDSPAR WEB AT FASTENER HOLE LOCATIONS NR 127 AND 129 NEAR MIDSPAR STATION 575. REPAIRED PER EA 67-178042.SDR RRXA002812Spar · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT SURFACE REAR SPAR LWR. CAP AT STA XRS 578, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4 AND EO 00-196SDR DHL200072104CSpar · crackedRIGHT WING L/E CAVITY WS 130.7 LATERAL WEB UPPER CHORD CRACKED AT DIFFERENT PLACES (5 EA). CRACKS RUNNING FROM ATTACHING BOLTS. REMOVED FASTENERS ON CRACKED ANGLE PER SRM 51-30-2. CUT OUT DAMAGED AREA, FABRICATED FILLER ANGLE PER SRM 51-40-4. INSTALLED REPSDR EIA2000220Spar · corrodedFOUND RHW FRONT SPAR LOWER CHORD CORRODED AT FS 1530 AND HOLES 1463-1479, TWO EACH REPAIRED ANGLES PREVIOUSLY INSTALLED AT AFT SIDE OF FRONT SPAR LOWER CHORD. REMOVED AND DISCHARGED EXISTING REPAIRS. CORROSION REMOVED, NDT INSPECTED FOR CRACK AND CORROSION FSDR DHL200072147CSpar · crackedRIGHT WING L/E CAVITY FRONT SPAR UPPER CHORD WS 735.5 SHOWS CRACK ABOUT 8 INCHES LONG JUST ABOVE NR 8 SLAT HYD ACTUATOR SUPPORT. REMOVED FASTENERS PER SRM 51-30-2. REMOVED STIFFENER TO GAIN ACCESS PER SRM 51-30-2. TRIMMED AREA OF CRACK PER SRM 57-10-6. HFESDR RRXA002808Spar Cap · chafedDURING A MAINTENANCE VISIT FOUND A CHAFFED AREA ON THE RT WING FRONT LWR. SPAR CAP AT STA XFS 7, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW EO#00-196 WITH APPROVED 8110-3 DATSDR SWAA001374Spar · crackedDURING SCHEDULED D-CHECK, FOUND RT WING AFT SPAR MOST I/B FASTENER HOLE CRACKED IN UPPER CHORD. REPAIRED PER ER 00-0797.
Back to JASC 5711