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 = '5751' 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 = '5751' 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 A6WA201040348Skin · chafedRT AILERON UPPER SKIN L/E CHAFED. REPAIRED CHAFE DAMAGE IAW REO 601R-57-60-013, REV NC AND REO 601R-57-60-072 REV. ORIGINAL.SDR QXEA2010040600215Skin · chafedC-CHECK - RT LOWER L/E OF AILERON HAS CHAFING ON SKIN. BLENDED DAMAGE ON THE RT LOWER L/E SKIN AT AILS 330.68 AND AILS 370.66 TO A SMOOTH AND DAMAGE FREE CONDITION IAW SRM 51-12-00-001-001-A01. ALL BLENDS ARE WITHIN LIMITS IAW SRM 57-61-01-101-001-A01. ETCSDR QXEA2010040600214Skin · chafedC-CHECK - LT UPPER L/E OF AILERON HAS CHAFING ON SKIN. BLENDED CHAFE DAMAGE ON UPPER L/E AT AILS 365.00 IAW SRM 51-12-00-001-001-A01. BLEND IS A MAX 2.0 INCH LONG AND .75 INCH WIDE. REMAINDER MAX OF .005 OUT OF ORIGINAL .090. BLEND IS WITHIN LIMITS IAW SRSDR IPXA10M59056Wedge · delaminatedRT INBD AILERON T/E DELAMINATED IN 3 AREA, 2EA 6" AND 1EA 3". REMOVED DAMAGE AREA AND REPAIRED IAW EO MD11-5750-37242 AND SRM57-50-02 REPAIR 3.SDR ASAA1047631Rib · gougedLT AILERON 4TH FRAME FROM OUTBOARD IS GOUGED. REMOVED AND REPLACED NOSE RIB LT AILERON IAW B737 SRM 51 40 02.SDR ASAA1047623Skin · chafedLT AILERON BOTTOM SKIN IS CHAFED NEAR CONTROL ROD HINGE POINT. BLENDED AND SEALED SKIN.SDR ASAA1047622Aileron · delaminatedLT AILERON COVE PANEL LOCATED AT THE MID INBOARD HINGE IS DELAMINATED. TRIMMED AND SEALED AILERON.SDR ASAA1047621Aileron · damagedLT AILERON CARBON FIBER COVE PANEL MISSING MATERIAL. TRIMMED AND SEALED AILERON.SDR ASAA1047620Aileron · delaminatedMULTIPLE AREAS OF DELAMINATION ON LEFT AILERON OUTBOARD. TRIMMED AND SEALED DELAMINATION.SDR A6WA201040237Skin · chafedLT AILERON UPPER AND LOWER L/E`S ARE CHAFED. BLENDED LOWER SKIN IN LIMITS (REO 601R-57-60-020) UPPER SKIN OUT OF LIMITS - REPLACE SKIN.SDR C2XA10SH105Attach Bracket · damagedSHV - DURING C-CHECK RT AILERON PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED ATTACHMENT BRACKET IAW EC5750-01177. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH104Attach Bracket · damagedSHV - DURING C-CHECK, LT AILERON PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED ATTACHMENT BRACKET IAW EC5750-01177. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA201008102Fitting · damagedDURING MAINTENANCE BASE INSPECTION FOUND THE RIGHT AILERON DAMPER FITTING TO BE DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AILERON DAMPER FITTING AND THE AILERON ASSEMBLY IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SSDR SIMA201007801Attach Fitting · gougedDURING MAINTENANCE BASE INSPECTION FOUND DAMAGE AT THE LEFT AILERON ATTACHMENT FITTING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AILERON DAMPER ATTACH FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR NSVA201063Aileron · damagedAIRCRAFT REQUIRES MAJOR REPAIR FOR PERMANENT REPAIR IF RIGHT AILERON BURN DAMAGE IAW TD 400-57-10-01.SDR ASAA1047610Flange · delaminatedRT AILERON INBOARD LOWER AREA OF FORWARD FLANGE DELAMINATED. REMOVED DAMAGED AREA AND REPAIRED.SDR SWAA101499Aileron · delaminatedDURING SCHEDULED MV1 CHECK, FOUND RT WING AILERON T/E DELAMINATED. REMOVED AND REPLACED AILERON PER MM.SDR FDEA201003020594Skin · corrodedLT WING OTBD AILERON LOWER SURFACE HAS FASTENERS UNDER PAINT PULLING THROUGH SKIN AND CORROSION FORMING UNDER PAINT. R & R LT OTBD AILERON IAW AMM 27-10-02-4. OPS CHECKED AILERON IAW AMM 27-10-02-4. OPS CHECK GOOD.SDR FDEA201003020593Skin · corrodedRT WING OTBD AILERON SKIN LOWER SURFACE HAS CORROSION. R & R RT OTBD AILERON IAW AMM 27-10-02-4. OP CHECKED AILERON IAW AMM 27-10-02-4. OPS CHECK GOOD.SDR C2XA10SH068Attach Fitting · damagedSHV - DURING C-CHECK LEFT AILERON PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED ATTACHMENT FITTING IAW EC5750-01177. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 2010FA0000202Spar · crackedFOUND CRACK IN THE INBD AILRON BAY AREA.SDR IPXA10558534Skin · damagedINSP TYPE:C2 RT WING AILERON UPR SURFACE HAS 2 HOLES 29" FROM INBD EDGE 16" FROM FWD EDGE. REPAIRED HOLES 29" FROM INBD EDGE 16" FROM FWD EDGE ON RT WING AILERON UPPER SURFACE IAW SRM 51-70-04.SDR UALA2010021500575Skin · damagedRT WING TIP HAS DAMAGE. NEED TO REMOVE AILERON PRIOR TO UPPER AND LWR SKIN REMOVAL. AILERON REMOVED. SKIN PANELS READY FOR REMOVAL. RT SKIN PANELS ON AOG. LOWER SKIN PANEL INSTALLED, UPPER SKIN PANEL APPROX 80 PERCENT COMPLETE. DAMAGED PARTS REPLACED PERSDR FOTR20006NR2013Wedge · delaminatedRT AILERON OTBD T/E WEDGE HAS AREA OF DISBOND ON UPPER INBD END. REPAIRED ON FASI W/O NR 20006, N/R 02013. INSTALLED HOT BONDED REPAIR TO RIGHT WING OTBD AILERON TRAILING EDGE WEDGE UPPER OTBD END IAW B727 SRM 51-40-20 PARA. 8 AND PARA 20 REV 102. MATERIAL SDR FOTR20006NR2012Skin · delaminatedRT OTBD AILERON T/E WEDGE HAS AREA OF DISBOND ON UPPER SURFACE. REPAIRED ON FASI W/O NR 20006, NR 02012 - INSTALLED HOT BONDED REPAIR TO RT WING OTBD AILERON T/E WEDGE UPPER SURFACE IAW SRM 51-40-20 PARA 8 AND PARA 20 REV 102. MATERIAL USED: 2024 T3, 0.012". SDR DL757100394Skin · crackedRT AILERON UPPER SKIN FOUND CRACKED AT L/E AT WEIGHT SUPORT RIB. REPAIRED IAW SRM51-70-04, PARA 4E -4G, P10-18, P48 FIG14.SDR IPXA10M58567Skin · misrepairedINSPECTION TYPE:1C, REPAIR SURVEY SEQ NR 282-W4-08 RT WING IB AILERON LOWER SKIN APPROX BETWEEN STA XIA375-359 PREVIOUS REPAIR FASTENERS NOT IAW SRM 57-10-00, FIG 1, VOL 1. INSTALLED NAS1097AD4 IN LIEU OF NAS1097AD5. REMOVED INCOMING SKIN PANEL, FABRICATED ASDR FOTR20006NR1778Skin · delaminatedRT OTBD AILERON T/E WEDGE PUNCTURED ON LOWER SURFACE. REPAIRED ON FASI W/O NR 20006, NR 01778 - INSTALLED HOT BONDED REPAIR DOUBLER TO RT OTBD AILERON TAB IAW SRM 51-40-20 PARA 7, 20 AND 22, REV 102. MATERIAL USED: 2024-T3, 0.012” THICK, DIM.; 3 X 3. CALCULATSDR MALA100024Skin · puncturedUPPER SURFACE OF RT AILERON FOUND PUNCTURED. PERFORMED COLD BOND (WET LAY-UP) REPAIR TO RT AILERON AT WING STA 340.22, 2.75 FWD OF T/E. REPAIRED IAW EO S51031.SDR SWIA201023576Aileron · out of rigSELECTING FLAPS 45°, AIRCRAFT ROLLED TO THE RIGHT. (FLT 4493) REMOVED EXCESSIVE SEALANT AND PAINT RIDGE, RIGGED RIGHT AILERON.SDR FOTR20006NR5044Skin · delaminatedRT WING AILERON OTBD T/E WEDGE IS DELAMINATED AT OTBD END. REPAIRED ON FASI WO 20006. N/R 05044- REPAIRED RT WING OTBD T/E WEDGE BY HOT BONDING REPAIR IAW SRM 51-40-20, REV 102, CUT OUT, AND FILLER DIM: 1.0" X 1.0", 3.0" X 1.0", AND 4.0" X 1.0". MATERIAL USSDR TRBACPCP2010012Hinge Fitting · corrodedRT OTBD AILERON HINGE FITTING CORRODED IN 2 AREAS. EVAL DAMAGED CORROSION ON RT OTBD AILERON HINGE FITTING FOUND TO BE OUT OF LIMITS IAW SRM51-10-10. REMOVED HINGE FITTING AND INSTALLED NEW HINGE FITTING ON RT OTBD AILERON IAW SRM 51-25-01, 51-25-02.SDR CA100126003Skin · cracked(CAN) THERE WAS HAIRLINE CRACK ON THE UNDERSIDE OF THE SKIN OF THE LT AILERON. THE SKIN WAS ALSO SLIGHTLY WRINKLED, SO THERE WAS AN INSPECTION DONE ON THE AILERON SPAR AND A CRACK WAS FOUND IN THE ACTUAL SPAR.SDR FDEA201001210208Skin · crackedLT INBD AILERON LOWER SURFACE SKIN IS CRACKED AT FWD EDGE. SKIN CRACK FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA DIMS 4 1/2" X 5 1/8", FABRICATED DOUBLER, FILLER AND INSTALLED IAW SRM 57-50-1, 57-50-5, 51-10-1, AND 51-30-2.SDR FDEA201001200204Skin · delaminatedRT WING OTBD AILERON T/E LOWER SURFACE FOUND DELAMINATED. RT WING OTBD AILERON R & R IAW AMM 27-10-30-4 REVISION 64. OPS TEST OF THE AILERON NEUTRAL AND RANGE OF MOVEMENT CARRIED OUT IAW AMM 27-10-00-710-802 REVISION 64. REPAIR CLASSIFIED AS MINOR IAW GMM 6-SDR CA100127002Hinge Fitting · cracked(CAN) UPON INSP, IT WAS FOUND THAT THE LT AILERON HINGE FITTING NR4 WAS CRACKED. ACCORDING TO EXPERIENCED AMES ON THE FLOOR, THIS IS NOT A PROBLEM THAT THEY HAVE SEEN BEFORE AND THEREFORE SHOULD BE DOCUMENTED.SDR UALA2010011500179Skin · damagedLT OTBD AILERON UPPER OTBD EDGE HAS METAL BOND PATCH PEELED BACK AND TORN APPROX 8 INCHES BACK FROM FRONT EDGE. FOUND BY DEICE CREW. TRIMMED AND REPAIRED LIGHTNING STRIKE PICTURE FRAME ON LT OTBD UPPER AILERON SURFACE. REPAIR GOOD UNTIL NEXT CK OR 5000H.SDR IXXA10SMN004SSkin · crackedDURING ROUTINE C CHECK INSP FOUND LT INBD AILERON LOWER SKIN CRACKED AT STA XA 502.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PERFORMED LT INBD AILERON BALANCE.SDR IXXA10SMN003SSkin · deformedDURING ROUTINE C CHECK INSP FOUND RT OTBD AILERON LOWER SKIN L/E DEFORMED AT STA XA 724.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PERFORMED BALANCE. FOUND WITHSDR TRBACPCP2010001SUSkin · corrodedCORROSION FOUND BY DQC ON RT AILERON SKIN. NRWC NR 282327 FOR MORE INFORMATION. PERFORMED CORROSION CUT-OUT REPAIR IAW STRUCTURAL REPAIR INSTRUCTION DO/TS-164/10-12805.SDR TRBACPCP20100001Skin · corrodedCORROSION FOUND ON RT AILERON SKIN. AWAITING NRWC FOR DETAILS.SDR USAA2010011290082Skin · debondedCLT - S4 - MAJOR REPAIR - AREA DISBONDED ON RIGHT WING AILERON OUTBOARD LOWER SKIN AT TRAILING EDGE WEDGE. REPAIRED RIGHT WING AILERON OUTBOARD LOWER SKIN AT TRAILING EDGE WEDGE IAW A319 SRM 57-61-21.SDR UIEA201000088Skin · delaminatedLT WING UPPER SURFACE OTBD, ALL OTBD AREA FOUND DELAMINATED. RT WING OTBD AIL UPPER SURFACE DELAMINATED AT SEVERAL LOCATION AS MARKED. LT WING UPPER SURFACE OTBD AILERON REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU 507013-1. SDR UALA2010010700100Skin · gougedRT INBD AILERON IS GOUGED ON LOWER SURFACE. DAMAGE MEASURES .5" BY 10" IN LENGTH. PREPPING TO REMOVE AILERON. DURING THE RT INBD AIL OPS TEST, ACFT FAILS TEST. ALL OTHER TEST REQUIREMENTS CK NORMAL. ACCOMPLISHED REMOVAL AND INSTALLATION OF ROBBED AILERON IAW MSDR UIEA201000087Skin · delaminatedLT WING UPPER SURFACE OTBB AIL INBD AREA DELAMINATED AT SEVERAL LOCATIONS AS MARKED. RT WING - OTBD AILERON UPPER SURFACE REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NT: DJU 504200-1, EO 4457A224RA AND 4457A225RA.SDR UIEA201000089Aileron · delaminatedLEFT WING I/B AILERON O/B TRAILING EDGE CORNER FOUND DELAMINATION AS MARKED. LEFT WING - I/B AILERON REPAIRED AS PER SRM 51-70-06, FIG 9 AND REF HX PROCESS CARD, CONTROL SEQ MO: DJU 503673-1. EO 4457A224RA 4457A225RA.SDR C2XA09SH502Attach Fitting · damagedSHV - DURING C-CHECK LEFT AILERON OUTBOARD ACTUATOR ATTACHMENT FITTING HAS TOOLING MARKS. MAINTENANCE REMOVED AND REPLACED LT AILERON ACTUATOR ATTACHMENT FITTING IAW EC 5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH500Bracket · damagedSHV - DURING C-CHECK LT AILERON DAMPNER BRACKET HAS VARIOUS AREAS OF DAMAGE. MAINTENANCE REMOVED AND REPLACED LT AILERON DAMPNER BRACKET IAW EMB-145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH499Attach Fitting · damagedSHV - DURING C-CHECK LT AILERON OUTBOARD ACTUATOR ATTACH FITTING HAS TOOLING MARKS. MAINTENANCE REMOVED AND REPLACED LT AILERON ACTUATOR ATTACHMENT FITTING IAW EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR QXEA2009121101030Structure · chafedC5 CHECK - CHAFE DAMAGE ON RT ALIERON L/E. BLENDED DAMAGE IAW SRM 51-12-00-001-001-A01. BLENDED AREA IS WITH IN LIMITS IAW SRM 57-61-01-101-001-A01. TREATED AND PRIMED AREA WORKED IAW SRM 51-21-11-001-001-A01 AND 51-25-06-001-001-A01.
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