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 DALA1405160977Spar · crackedWING REAR SPAR CRACKED AT XRS 164. REPAIRED IAW AA 5710-01110.SDR R61A201211240686Spar · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND CRACK LIKE INDICATIONS A3 HOLE LEFT WING SPAR 2. MAINTENANCE REAMED A3 HOLE LEFT WING SPAR 2 IAW EMB SB 170-57-0053 REV 1. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR DALA12014060977Spar · damagedDURING ACCOMPLISHMENT OF RT WING LOWER SPAR CAP INSPECTION FOUND CRACK IN LOWER SPAR CAP EMANATING FROM INBD LOWER FLAP FITTING HOLE AT XRS=164.00. REF WC NR 5710-01110-0502. STOP DRILLED BOTH ENDS OF CRACK IAW DWG J060271. PERFORMED HFEC INSPECTION AT BOTH ESDR AALA20121121009Spar · corrodedCORROSION ON RIGHT WING FOWARD SPAR AROUND BOOST PUMP BONDING STRAPS. REMOVED CORROSION AND REPAIRED PER EA B737-57-027149.SDR HYIA20121120001Strap · corrodedDURING A REGULARLY SCHEDULED MAINTENANCE EVENT, THE LEFT LOWER NACELLE SKIN (PN 5654100-30) AND ASSOCIATED HEAT SHIELD WERE REMOVED FOR OTHER MAINTENANCE. AFTER REMOVAL, SEVERE CORROSION WAS FOUND AT LEFT SPAR STRAP INCLUDING SPAR CAP FASTENER FAILURE. VISUAL SDR AALA20121201005Stiffener · corrodedLEFT WING REAR SPAR STIFFENER 202 IS CORRODED AT BONDING JUMPER ATTACH POINT. ACCOMPLISHED CORROSION REMOVAL PER EA B757-57-027271.SDR 29GA2013021395557Spar Cap · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT WING MAIN SPAR UPPER CAP AT WS 124 CORRODED. BLENDED CORROSION AND PERFORMED NDT INSPECTION, NO CORROSION OR CRACKS NOTED.SDR 29GA2012110795557Spar · corrodedREPORT: DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT WING MAIN SPAR UPPER CAP HAS CORROSION.SDR FDEA201211063863Spar Cap · crackedRT WING T/E REAR SPAR LOWER CAP XORS 433 FOUND CRACKED. REMOVED AND REPLACED WITH NEW SILL AS PER SRM 51-34-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201211023818Spar Cap · crackedWHILE PERFORMING A HFEC INSPECTION OF RT WING REAR SPAR LWR CAP FOUND OTBD AFT HOLE CRACKED. REPAIR ACCOMPLISHED IAW EA 8-5710-163706. MAJOR REPAIR.SDR R61A201211010635Spar · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND RIGHT WING SPAR 2 AT RIB 10 CRACKED AT A3 AND A4 HOLES. MAJOR REPAIR, MAINTENANCE REPAIRED RIGHT WING SPAR 2, AT RIB 10, A3, AND A4 HOLES IAW EMB ETD 2012-170-015618-D REVISION D. THE AIRCRAFT IS OUT OF SERSDR AALA20121031003Stiffener · corrodedLEFT WING REAR SPAR STIFFENER WS 202.92 CORRODED AT BONDING JUMPER. ACCOMPLISHED NESTED ANGLE REPAIR PER EA B757-57-026844.SDR R61A201210290646Spar · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND CRACK LIKE INDICATIONS LEFT WING SPAR 2 A 3 HOLE. MAINTENANCE REAMED LEFT WING SPAR 2 A3 HOLE TO .590 IAW S/B 170-57-0053. THE AIRCRAFT IS SCHEDULED FOR CHECK FLIGHT 11-18-2012.SDR R61A201210290645Spar · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT WING SPAR 2 A2 HOLE HAS CRACK LIKE INDICATIONS. REAMED RIGHT WING SPAR 2 A2 HOLE TO .590 IAW S/B170-57-0053. THE AIRCRAFT IS SCHEDULED FOR CHECK FLIGHT 11-19-2012.SDR ABXA20121026290Spar · corrodedCENTER TANK UPPER SPAR CHORD CORRODED FROM OUTBOARD END APPROX LBL 28.6 STA 955. CORROSION OUT OF LIMITS. CUT AND REMOVED OUT OF LIMITS SECTION OF CHORD. REPAIRED IAW REA B657-60353-MR. REA B657-60353-MR, REA B657-60353-MR, ACFT WAS GROUNDED.SDR UALA2012102506121Spar · corrodedLEFT WING REAR SPAR WEB CORRODED AROUND FASTENERS IN THE AREA OF IRSS 347 WHERE FUEL BOOST PUMP IS INSTALLED. DAMAGE REPAIRED IAW ECRA 5720-02325.SDR FDEA201210243731Frame · crackedFOUND A CRACK 8MM IN LENGTH AT LT SIDE FRAME 40 LOWER OTBD RADIUS AREA. REPAIRED PER EA 6-5710-163147SDR SWAA2012111509379Plate · crackedRIGHT WING LWR REAR SPAR WAFFLE PLATE CRACKED AT RSS 423 I/B OF NR 8 FLAP TRACK. RE-INSTALLED RIGHT WING LWR REAR SPAR WAFFLE PLATE AT RSS 423 I/B OF NR 8 FLAP TRACK PER SRM 51-40-02.SDR ABXA20121019281Spar · corrodedAREA OF CORROSION ON THE REAR SPAR WEB 3 INCHES FROM THE TOP. LOCATED AT STA 955 LEFT LBL 79. REMOVED CORROSION IAW B767-200 SRM 57-10-10 FIGURE 101. BLENDOUTS EXCEEDED PUBLISHED LIMITS AREA REPAIRED IAW REA B657-60346MR, ACFT WAS GROUNDED.SDR DALA12010105651Spar · damagedDURING INSPECTION OF WC 5732-01010-0430, FOUND AT RIB 25 LT AFT SPAR UPPER CHORD 4 EA EXISTING .3125" HOLES, REGULAR HOLE SIZE ARE .2500" ACCOMPLISHED PERMANENT REPAIR IAW ERA 507367-14, REV ORIGINAL ON CARD 5732-01010-0430, JOB 124-0039. ASSOCIATED ER/A 14-50SDR R61A201210110589Spar · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT WING SPAR 2 A3 HOLE HAD CRACK LIKE INDICATIONS. MAINTENANCE REPAIRED THE LEFT WING SPAR 2 A3 HOLE IAW EMB SB 170-57-0053 REV1 PART 3. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR FDEA201210103587Spar · crackedFOUND A 2.5 INCH CRACK ON THE WING REAR SPAR TO WW LT BULKHEAD AT ATTACHMENT TEE ANGLE ON THE UPPER END. R & R APB7078-1 FITTING IAW DWG NPB6066 AND SP10570007.SDR ABXA20121009293Spar · corrodedSTA 955 REAR SPAR RIGHT O/B PAD UP AREA HAS SEVERAL AREAS OF CORROSION UPPER-LWR. REPAIRED AREA IAW REA B653-60342-MR, ACFT WAS GROUNDED.SDR UHLA2012100600345Spar · damagedMAJOR REPAIR - DURING PROCESS OF INSTALLING BUSHING INTO HOLE NR 1 IN SPAR II OUTBD OF RIB 9, A PIECE OF SPAR II FELL OFF AFT SIDE OF HOLE. REMOVED DAMAGED MATERIAL FROM AROUND HOLE NR 1 BY REAMING HOLE TO 0.373" DIAMETER AND COUNTERSINKING AREA AROUND HOLD TSDR FDEA201210053558Frame · damagedDURING SB A300-57-6086 ACCOMPLISHMENT, DAMAGE FOUND IN HOLE "P" AT FRAME 47 RT SIDE. DAMAGE WAS NOTED IN THE TEE AND SPAR. REMOVED NOMINAL FASTENER FROM HOLE "P" AT FRAME 47 RT SIDE, VERIFIED DAMAGE IN UPPER 2 LAYERS (TEE AND SPAR), OVERSIZED ALL FIVE LAYERS SDR UHLA2012100400344Spar Cap · damagedMAJOR REPAIR - 29 HOLES MISDRILLED IN SPAR II 3RD CAP SPLICE, BETWEEN RIBS 9 AND 11. HOLES MARKED FROM OUTBD TO INBD. REAMED HOLES 2, 5, 7-9, AND 11-29 TO 0.263". REAMED AND INSTALLED HAT BUSHINGS IN HOLES 3, 4, 6, AND 10, FINAL REAM IS 0.325". REAMED AND SDR ERAA20120073Spar · chafedRIGHT WING JACKPOINT FITTING P/N 85710423 HAS CHAFING.SDR FDEA201210033548Spar · damagedRT FR47 REAR SPAR HOLE, UNKNOWN IF BUSH EXISTS IN REAR FITTING . BORE OK AFT FACE OF HOLE, SURFACE FINISH REMOVED IAW SRM 51-75-20, NO BUSH PRESENT. NEW BOLT FITTED IAW SRM 51-40-21 SURFACE FINISH RESTORED IAW SRM 51-23-10 AND EO 6-5710- 7-3305 P2.SDR FDEA201210033547Spar · damagedRT FR47 REAR SPAR HOLE, UNKNOWN IF BUSH EXISTS IN REAR FITTING . BORE OK AFT FACE OF HOLE WITH SURFACE FINISH REMOVED IAW SRM 51-75-20, NO BUSH PRESENT. NEW BOLT FITTED IAW SRM 51-40-21 SURFACE FINISH RESTORED IAW SRM 51-23-10 AND EO 6-5710- 7-3305 P2.SDR FDEA201210033544Spar Cap · crackedRT WING REAR SPAR LWR CAP AFT OTBD HOLE IS CRACKED. XORS 345.750 REAMED HOLE TO A DIA OF .328". HFEC INSP NO CRACK NOTED IAW EA 8-5710-163354. COLD WORKED 1EA HOLE IAW SRM 51-12-01 VOL II. FINAL REAM OF HOLE TO A DIA OF.341. FASTENER INSTALLATION ACCOMPLISSDR FDEA201210023541Spar · crackedLEFT WING REAR SPAR LWR CAP FWD OTBD HOLE IS CRACKED. REAMED HOLE TO DIA OF .328". HEFC INSPECTION, NO CRACK NOTED IAW EA 8-5710-163353. COLD WORKED 1EA HOLE IAW SRM 51-12-01, VOL II. FINAL REAMED HOLE TO DIA OF .341". FASTENER INSTALLATION ACCOMPLISHEDSDR FDEA201210023540Spar · corrodedCORROSION FOUND AT RT AFT WING SPAR WEB SURFACE AT AFT FUEL BOOST PUMP OPENING LOWER BONDING JUMPER ATTACH POINT (MARKED) WINGS-MAIN FRAME -OUTER TANK-REAR SPAR CORRSION IRSS 183.0 RT SIDE (AFT BOOST PUMP) WORK ACCOMPLISHED ON EA F-5710-162542. MAJOR REPAIR.SDR R61A201209290547Spar · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND CRACK LIKE INDICATIONS IN A2 HOLE ON RIGHT WING. MAINTENANCE REAMED A2 HOLE TO .362" IAW EMB 175 SRM 51-40-02, AND SB 170-57-0053 TO REMOVE CRACK LIKE INDICATION. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHESDR SWIA201232072Spar · crackedRIGHT WING FORWARD LOWER AUXILIARY SPAR OUTBOARD OF NACELLE CRACKED IN 2 LOCATIONS. (C-CHECK) REPAIRED LOWER AUXILIARY SPAR.SDR UALA2012092905515Stiffener · gougedRIGHT WING LEADING EDGE, INBOARD FSS 231, SPAR STIFFENER IS GOUGED. MAJOR REPAIR ACCOMPLISHED: REMOVED AND REPLACED THE STIFFENER PER SRM 51-40-2 AND BAC DWG 112N2002.SDR FDEA201209283499Spar · damagedLEFT WING FRM 47 HOLE C, MECHANICAL DAMAGE FOUND IN INTERNAL BORE OF FASTENER HOLE. MECHANICAL DAMAGE REMOVED IAW SRM 51-40-30 FINAL HOLE C DIAMETER IS 0.561"/14.249MM. REWORKED IAW EA 6-5710-162973, PAGE 2.SDR FDEA201209283496Spar · damagedRT WING FR47 REAR SPAR HOLE V POSSIBLE BUSH WITH X4 IMPACT DAMAGE MARKS IN REAR FITTING. NO BUSH WAS FOUND AND HOLE V REMOVED. MECHANICAL DAMAGE IAW SRM 51-40-30 AND EA 6-5710-162973, PAGE 11. FINAL DIAMETER IS 0.584"/14.834 MM.SDR FDEA201209283495Spar · crackedRIGHT WING HOLE L CRACK INDICATED BY NDT INSP CRACK IS ASSESSED AS A CORNER CRACK IN THE FRM AT THE INTERFACE WITH REAR ANGLE FITTING AT 1 O'CLOCK POSITION HOLE L REWORKED UNTIL NO CRACK INDICATION IAW SRM 51-40-30. FINAL HOLE DIAMETER 0.624"/15.849 AS DESDR UHLA2012092600342Spar · crackedMAJOR REPAIR - RIGHT WING, HOLE A4, CRACK INDICATIONS, INBD AND OUTBD, SPAR 2 LWR FLANGE. CUT OUT DAMAGE ON SPAR 2 AROUND A3 AND A4 HOLES. CUT SECTION OF 3RD CAP TO ALLOW FOR DOUBLER INSTALLATION. INSTALLED BUSHING IN A3 HOLE. CUT OUT SECTION OF RIB 9. INSDR FDEA201209263467Spar · corrodedLT OTBD MAIN FLAP FRONT SPAR AFT FACE CORRODED AT APPROX WS 600. COMPLIED WITH EA F-5750-162538, MAJOR REPAIR.SDR WX0A071341Spar · corrodedLEFT WING O/B FLAP CENTER HINGE FITTING UPPER I/B ATTACH FITTING HOLE SURFACE CORRODED STA XRS267.00 OF WING REAR SPAR. REMOVED DAMAGE, FABRICATED FILLER, HFEL SPAR & BOND IN REPAIR PART IAW EA 14874IR 09/23/2012.SDR FDEA201209233414Spar · crackedLOWER LEFT WING, XOR 345 OTBD ROLL/MIDDLE BOLT HOLE SHOWING CRACK INDICATION. REAMED HOLE WITH CRACK INDICATION TO .325 REF SRM 51-21-01, VOL II PERFORMED HFEC OPEN HOLES INSPECTION IAW NDT SPM 93K0393, NO INDICATION FOUND. PERFORMED FINAL LEAK CHECK IAW MMSDR FDEA201209213386Spar · corrodedRT AFT WING SPAR WEB SURFACE BOTTOM SURFACE HAS CORROSION AT IRSS 183. COMPLIED WITH EA F-5710-162544-WINGS-MAIN FRAME-OUTER TANK-REAR SPAR CORROSION IRSS 183.0. RTS (AFT BOOST PUMP) REF FAA FORM 8100-9. MAJOR REPAIR.SDR K11A2013041629002Repair · separatedPREVIOUS REPAIR ON LEFT WING L/E LOWER SPAR CAP SEPARATING.SDR R61A201209130525Spar · crackedWHILE AIRCRAFT WAS OUT OF SERVICE FOR SPAR 2 LOWER FLANGE REINFORCEMENT EO R170EO-57-10-0003 MAINTENANCE FOUND CRACK LIKE INDICATIONS IN THE SPAR 2 A 3 HOLE RIGHT WING. MAINTENANCE REPAIRED RIGHT WING SPAR 2 AT RIB 10 IAW EMB ETD 2012-170-013118. THIS IS A SDR FDEA201209113296Spar Cap · damagedLEFT WING REAR SPAR, LOWER CAP AT XORS 345.75 FOUND TWO AFT FASTENER HOLES OVERSIZED WHILE ACCOMPLISHING EO 8-5710-7-5007. PT 1 COMPLIED WITH EA 8-5710-163343 BY REAMING HOLE A & D TO .371 AND INSTALLING BUSHINGS.SDR ABXA20120910274Spar · corrodedRIGHT WING LEADING EDGE LOWER SPAR FLANGE AT APPROX WING STATION 420 LOWER FLANGE EXFOLIATED. CUT OUT DAMAGED SPAR FLANGE. REPAIRED IAW REA B657-59996, ACFT WAS GROUNDED.SDR UHLA2012083100323Spar · crackedMAJOR REPAIR - WHILE PERFORMING HFEC FOUND CRACK LIKE INDICATION IN LEFT WING SPAR II RIB 10 A1 HOLE. REAMED A1 HOLE ON LEFT WING TO .361" IAW SRM 51-40-02. PERFORMED NDT, NO CRACKS NOTED IAW SB 170-57-0053 STEP 4D REVISION 1.SDR UHLA2012083100320Spar · crackedMAJOR REPAIR - FOUND CRACK LIKE INDICATION ON RIGHT WING SPAR II ROB 10 HOLE A3 WHILE PERFORMING HFEC. REAMED HOLE A3 RIGHT WING TO .361" IAW EMB 170 SRM 51-40-02. PERFORMED NDT, NO CRACKS FOUND.SDR IPXA12M75316Former · crackedINSPECTION TYPE:4C, LT WING FIXED L/E SUPPORT FORMER CRACKED BETWEEN FASTENERS AT APPX STA XOR 917. REMOVED, FABRICATED AND INSTALLED SUPPORT FORMER AT LT WING FIXED L/E AT STA XOR 917 REF SRM 51-31-01 PG 1 AND SRM 51-35-01.
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