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 LR7A0005Spar · crackedDURING SCHEDULED C2 INSPECTION PER JOB CARD HSP57170, FOUND RT REAR SPAR WEB CRACKED AT CWS 73 AND CWS 79. REPAIRED IAW LAC MEA 382-57-00-011. REINSTALLED WEB PER SRM 51-70-2 AND SRM 57-30-22.SDR QXEA0000615Spar · corrodedPDX - FRONT SPAR TOP FLANGE FOR LEADING EDGE 61A HAS CORROSION AT SCREW HOLE NR 13 NUT PLATE FROM INBOARD SIDE. REPAIRED IAW FOKKER SRM 51-31-01.SDR QXEA0000614Spar · corrodedPDX - LEFT WING FRONT SPAR STATION 4700 FRONT SIDE HAS CORROSION SURROUNDING SIX HI-LOCKS. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, NR 4.SDR AU000193Spar · corroded(AUS) RT WING CENTRE SECTION REAR SPAR WEB CORRODED IN THE AREA LOCATED BEHIND THE REAR SPAR BULKHEAD FITTING PNO 145T2521. AREA OF CORROSION APPROXIMATELY 215.9MM (8.5IN) BY 38.1MM (2.5IN) BY2.54MM (0.100IN) DEEP.SDR SWAA000178Spar · crackedDURING SCHEDULED D-CHECK, FOUND THRU HFEC INSP INDICATED CRACKED LT WING REAR SPAR UPPER CHORD IN HOLED. REPAIRED SPAR PER SRM AND ER.SDR QXEA0000271Spar · corrodedYYC - REAR SPAR HAS LIGHT SURFACE CORROSION FROM STATION YW45.0 - 139.0, ON RIGHT WING. REPAIRED IAW DHC 8 SRM 51-20-00, SRM 51-20-11, SRM 51-20-16, PAGE 4, SECTION C, SRM 51-20-36, PAGE 6, SECTION F-J.SDR DHL2000717105Spar · gougedAT D-CHECK, FOUND RIGHT HAND SPAR FITTING GOUGED (MLG BEAM O/B SIDE TO REAR SPAR SUPPORT FITTING). PERFORMED HFEC, BORED RT MLG SUPPORT FITTING PIN HOLE TO 1.795, WITHIN LIMITS PER BOEING TELEX 32-9430. FLAP PEENED AREA, INSTALLED BUSHINGS AND SUPPORT BEAM PSDR 20000404SH018Spar · crackedONE EACH CRACK EXISTED ON THE UPPER AFT T-SPAR MEASURING 5.0 INCHES LONG, LOCATED AT THE INBOARD END OF THE OUTBOARD MID FLAP. (X)SDR 20000404SH017Spar · crackedONE EACH CRACK EXISTS ON THE UPPER AFT T-SPAR MEASURING 1.5 INCHES LONG, LOCATED AT THE INBOARD END OF THE OUTBOARD MID-FLAP. (X)SDR RRXA000024Support · crackedDURING A MAINTENANCE VISIT FOUND CRACK, AUX SPAR SUPPORT CRACKED 1ST ONE I/B RT SIDE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4 & 51-1-21 & 51-1-24 & 51-1-20D.SDR ABXA000067Spar · corrodedRIGHT WING LOWER REAR SPAR CAP AFT TANG AT STATION XCW 69.5 CORRODED. REPARIED RIGHT WING AFT LOWER SPAR AFT TANG AT STATION XCW 69.5 IAW ABX REA D85733882 MR.SDR DHL2000803101Spar · brokenLEFT WING REAR SPAR UPPER CAP STEEL PLATE BROKEN 1 IN STA 350.00. REMOVED PLATE AND FASTENERS IAW SRM 51-1-21A PAGE 4. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8 PAGE 11. FABRICATED PLATE IAW SRM 57-2-1 PAGE 6. INSTALLED PLATE AND SECURED WITH SOLID RIVETSSDR ABXA000063Spar · corrodedDURING C-CHECK, FOUND THE FORWARD SIDE OF THE LOWER T-CAP OF THE FRONT SPAR CORRODED AT LBL 5 TO RBL 12 (CENTER WING). REPLACED FINGER DOUBLER IAW DC9 SRM 51-30-2.SDR CA000110098Spar · corroded(CAN) RIGHT WING FROM SPAR LOWER CHORD CORRODED BEYOND SRM LIMITS AT STA 122. REPAIRED PER BOEING INSTRUCTION - FAX.SDR AT9900893Spar · crackedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CRACK IN RIGHT WING REAR SPAR LOWER CAP. REMOVED AND REPLACED CRACKED SPAR SECTION IAW DC9 SRM 51-30-01, 51-30-05, 51-30-02, 57-40-01, AND DRAWING J060165..SDR QXEA0000122Spar · gougedPDX - GOUGE BELOW PANEL 92G AT AFT SPAR AND OUTER/CENTER WING ATTACHMENT. REPAIRED IAW HORIZON AIR EA 9-57-340 AND FOKKER SRM 51-10-4, PARAGRAPH 4 A, B, C.SDR QXEA0000121Spar · chafedPDX - LIGHT CHAFING BELOW PANEL 92G AT AFT SPAR AND OUTER/CENTER WING ATTACHMENT. REPAIRED IAW SRM 51-10-4, PAGE 9, PARAGRAPH 4 A, B, C.SDR TWAA0000603Spar · crackedDURING OP 16 MAINT CHECK, FOUND ON RT WING 2 EA SURFACE CRACKS AT TOP OF REAR SPAR, INBD HOLE 3/8 IN LONG, OTBD HOLE .5 IN LONG, AT CENTER FLAP HINGE AREA. STOP DRILLED CRACKS PER DOUGLAS REPAIR DOCUMENT JO60272. REPAIRED CRACKS AT TOP OF REAR SPAR RT WING ASDR 9905706626Spar · corrodedDURING M CHECK, FOUND CORROSION ON FRONT SPAR LOWER SURFACE OF THE LOWER CHORD. REPAIRED PER EA 66-171325.SDR RRXA000308Spar Cap · crackedDURING A MAINTENANCE VISIT FOUND RIGHT UPPER SPAR CAP CRACKED AT OUTBOARD AFT ATTACHMENT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW SPAR CAP IAW DC-8 SRM 51-3-0.SDR 99T64R477EWASpar · crackedFOUND DURING D-CHECK, RT AUX SPAR UPPER SPAR CAP CRACKED .625 INCH AT OUTBOARD AFT ATTACH BOLT. REMOVED AND REPLACED RIGHT AUX SPAR UPPER SPAR CAP IAW DC-8 SRM 51-1-24, 51-1-20D AND 51-3-0. (M)SDR 2000ZZZM192Spar · crackedPIT - DURING C-3 CHECK, FOUND 1.3125 INCH LONG CRACK IN LOWER SPAR CAP, LEFT SIDE STATION 164. DETECTED BY EDDY CURRENT. INSTALLED DOUBLER PER JO60271-503 DRAWING/EO 577D348. (M)SDR MWEA99860Spar · misrepairedSEVERAL PREVIOUS BLEND OUTS ON BOTTOM OF LEFT WING, BOTTOM OF AFT SPAR FROM STATION XRS 111.5 AND XRS 120 ARE NOT ACCEPTABLE. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER.SDR P2EA99346Rib · crackedSJO - SLAT TRACK RIB CRACKED AT RIGHT WING FRONT SPAR SS356. DEFECT SIZE, LENGTH 1.5 INCH, WIDTH .32 INCH. REPLACED RIB AT SS 356 OUTBOARD TRACK PER SRM 51-30-2. (M)SDR AT9900844Spar · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LEFT WING LOWER AFT SPAR FLANGE TO BE CORRODED AT BS 477.35. FABRICATED AND INSTALLED SPAR IAW EO 99-1384.SDR AT9900856Spar · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LEFT WING AFT SPAR FLANGE CORRODED BEYOND LIMITS AT BS 550. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW DC9 SRM 51-30-02, 51-30-03, AND 51-30-05.SDR GAIA99194Spar · crackedRIGHT WING BETWEEN WS 464 AND WS 491 BELOW NR 11 SPOILER LOWER AFT SPAR CHORD CRACK. INSTALLED REPAIR BETWEEN RIGHT WS 464 AND WS 491 BELOW NR 11 SPOILER AT THE LOWER AFT SPAR CHORD. REPAIR ACCOMPLISHED IAW BOEING TELEX KHC-MIA-99-0002H, 8110-3 DATED OCTOBERSDR 9905139976Spar · crackedDURING M CHECK, FOUND CRACK AT NBR 4 FLAP HING OUTBOARD BOLT HOLE AT BOTTOM APPROXIMATEY 3.8 INCH ON WING SPAR. REPAIRED PER EA 99-169349.SDR CA991208033Bracket · cracked(CAN) DURING AN INSPECTION REQUIRED BY SB 8-57-7, A CRACK WAS FOUND IN THE RIGHT AILERON TAB ACTUATOR ARM BRACKET. A REPLACEMENT TRIM TAB WAS INSTALLED.SDR TWAA9917614Spar · crackedDURING OP 16 MAINT CHECK, FOUND ON LT WING, 2 CRACKS AT TOP BOLT HOLES, OTBD APROX .375 IN LONG, INBD APPROX .25 IN LONG, ON REAR SPAR FACE AT CENTER FLAP HINGE SUPPORT, 1 O'CLOCK POSITION. STOP DRILLED CRACKS AROUND ATTACH BOLT HOLES PER SERVICE REWORK DRAWISDR 99ZZZX4491Spar · corrodedWHILE INVESTIGATING POSSIBLE SURFACE CORROSION ON THE LEFT WING TO FORWARD SPAR HINGE CAP DURING THE 12-MONTH SPAR CAP INSPECTION PER CHAPTER 5 OF THE MM, AN APPROXIMATE 2.6 INCH CRACK WAS FOUND AT APPROXIMATELY WS 153.735.SDR 9905149760Spar · corrodedDURING M CHECK, LEFT WING REAR SPAR CAP HAS CORROSION AFT SIDE STA. XRS 267, NR 3 FLAP HINGE FITTING UPPER STUD HOLES. REPAIRED PER EA 97-171707.SDR 9905646626Spar · corrodedDURING M CHECK, FOUND CORROSION ON LOWER SPAR CAP OF WING LEADING EDGE CAVITY AT FSSI 1445. REPAIRED PER EA 66-173191.SDR 2000ZZZX708Filler · missingDUE TO EXISTING REPAIR, DOUBLER ON LT FRONT SPAR (XRS 69.5) LOWER WING PLANK, TAPER FILLERS NEED TO BE FABRICATED TO COMPLETE SB 57-2OR5. FABRICATED FILLERS AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 11-22-99. REF: ZANTOP INTERNATIONAL AIRLINES,SDR 99T64R676EWASpar · misdrilledFOUND DURING D-CHECK, RIGHT WING OUTBOARD LEADING EDGE UPPER SPAR CAP HAS SEVERAL MISDRILLED HOLES AT NUT CHANNEL. DRILLED THE DISCREPANT HOLES ROUND TO ELIMINATE THE DOUBLE DRILLED CONDITION. TREATED AND PRIMED. LEFT OVERSIZED HOLES OPEN. INSTALLED REMAINSDR RRXA000300Spar Cap · crackedDURING A MAINTENANCE VISIT FOUND LEFT WING, FORWARD LOWERS PAR CAP CRACKED AT XFS 520. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER ENGINEERING SKETCH EO 99-186.SDR DLM88992457Spar Cap · oversized holesDURING INSTALLATION OF THE UPPER SURFACE HEATER BLANKETS FOR THE LEFT AND RIGHT WING THE HOLES COMMON TO THE UPPER CAP OF THE FRONT SPAR WERE NOT COLD WORKED. ERA 333738-14 ADDRESSED THE DISCREPANCY.SDR 2000ZZZX694Spar · crackedLOWER FRONT SPAR HORIZONTAL LEG 10 INCH CRACK BS 680 - 26.5 INCHES TO 36.50 INCHES RBL CENTER WING TANK. CUT OUT DAMAGE. FABRICATED FILLER, DOUBLERS, AND INSTALLED IAW DC-8 SB 57-30R5. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR 2000ZZZX671Spar · crackedLOWER FRONT SPAR 1.50 INCH CRACK FS 680 LBL 34 INCHES Z AXIS -47 AND .50 INCH CRACK BS 680 LBL XCW 39 INCHES AND XCW 43 INCHES Z AXIS -47 INCH. CUT OUT DAMAGE. FABRICATED FILLERS, DOUBLERS, AND INSTALLED IAW DC-8 SB 57-30-R5. REF: ZANTOP INTERNATIONAL AISDR 2000ZZZM213Spar · crackedLOWER FRONT SPAR HORIZ LEG 10 INCHES CRACK FS 680 - 26.5 TO 36.5 INCH RBL CENTER WING TANK. CUT OUT DAMAGE. FABRICATED FILLERS, DOUBLERS AND INSTALLED IAW DC-8 S/B 57-30R5. (M)SDR EIA990301Spar · corrodedMZJ - RIGHT WING TRAILING EDGE REAR SPAR AT APPROX STATION XW251.680 HAS CORROSION BY UPPER INBOARD BOLT HOLE. REPLACED SECTION OF RT WING REAR SPAR UPPER CAP BETWEEN XRS 180.1 AND XRS 319.5 PER ECRA 941-57-015-2. (M)SDR RRXA991671Frame · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, RT CENTER L/E OB UPPER T-CHORD AT STA XS 454. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 57-2-0 FIG 2.SDR RRXA991670Frame · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, NR 4 PYLON STUB WING FRAME AT STA XW 454. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER AND INST REPAIR IAW DC8 SRM 51-1-20 AND DCSDR CA991112014Rivets · sheared(CAN) AFTER REMOVAL OF FUEL TANK, TWO RIVETS WERE FOUND SHEARED ON THE FRONT SPAR. THE RIVETS WERE LOCATED AT THE SPAR ANGLE (PN 0523017-14) AND THE INBOARD RIB (PN 0523010-14).SDR TWAA9915403Spar · crackedDURING OP 16 MAINT CHECK, FOUND RT WING REAR SPAR OTBD FLAP MOUNT HOLES AT XRS 353 HAD THE LOWER OTBD HOLE CRACKED 1.125 INCH LONG. REAR SPAR REPAIRED AT XRS 353 PER ARA 16334.SDR TSAA0057021Spar · corrodedLEFT WING FRONT SPAR FORWARD SIDE CORRODED AT WBL 90 FSS 113. REPAIRED IAW 51-10-6. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0057020Spar · corrodedLEFT WING HAS CORROSION ON FRONT SPAR WEB AT FSS 286.9. REPAIRED WEB IAW ECO 3021 AND SRM 51-10-6. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0057018Spar · crackedFOUND CRACK IN PAINT BETWEEN RIVETS ON LEFT UPPER INBOARD WING SKIN 6 INCH FORWARD FROM REAR SPAR AT WBL 114. REPAIRED LEFT INBOARD WING SKIN IAW SB 737-57-1144. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0057016Spar · corrodedLEFT WING FRONT SPAR FORWARD SIDE WEB AND LOWER CHORD CORRODED AT WBL 367. REPAIRED LEFT WING FRONT SPAR IAW ECO3019 AND SRM 51-10-6. AIRCRAFT RETURNED TO SERVICE. (M)SDR 2000ZZZX695Spar · crackedFOUND DURING C-CHECK. A 4.75 INCH CORROSION CRACK APPROXIMATE STA XCW 31.0 LT IN FRONT SPAR LOWER T-CAP VERTICAL LEG. ROUTED OUT CRACK, BLENDED, NDT CONFIRMED CRACK, REMOVED. TREATED AND PRIMED. FILLED SEALER, CONTINUED THE INSTALLATION OF LOWER FRONT SPAR
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