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 C2XA09SH185Hinge Fitting · damagedSHV - DURING C-CHECK LT AILERON O/B HINGE FITTING (ON AILERON) I/B HAT BUSHING HOUSING WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED LT AILERON O/B HINGE FITTING IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR HSYA2009061809Attach Fitting · crackedFOUND BOTH THE LT AND RT AILERON BALANCE WEIGHT CLIPS CRACKED IN HALF. REMOVED AND REPLACED BALANCE WEIGHT CLIPS IAW KIT NR 129-4036-001.SDR IPXA09M56705Skin · damagedINSPECTION TYPE: 1C REPAIR SURVEY SEQ NR 281-W4-03 RT INBD AILERON LWR SKIN EXTERNAL DOUBLER BETWEEN STA XIH329.911 TO XIH335.767, 2 EA FASTENER HEADS PULLED. REMOVED EXISTING REPAIR FROM RT WING INBD AILERON LWR SKIN BETWEEN STA XIH 329.911 TO XIH 335.767. SDR ERAA200900002Fitting · crackedWHILE INSPECTING IAW SB27-3928, FLIGHT CONTROLS- AILERON BALANCE WEIGHT CLIP INSPECTION; FOUND ONE CLIP CRACKED ON THE RT AILERON.SDR ERAA200900001Fitting · crackedWHILE INSPECTING IAW SB27-3928 FLIGHT CONTROLS- AILERON BALANCE WEIGHT CLIP INSPECTION; FOUND ONE CLIP CRACKED ON LT AILERON.SDR MALA090092Skin · debondedDURING 6Y/4Y INSPECTION IN CWA, LY AILERON HAS DISBONDED DENT LOCATED AT WS 340.82 AND 9.5 FROM TRAILING EDGE. REPAIRED IAW S51031.SDR Y9PAN610SM609Aileron · delaminatedDURING PRE-FLIGHT OF AIRCRAFT BEFORE DEPARTURE, FOUND RT AILERON WITH SEVERE DELAMINATION, APPROX 6 X 24 INCHES.SDR UIEA201000128Aileron · damagedTHE PURPOSE OF THIS EO IS TO RECORD A MAJOR REPAIR. DURING C CHECK INSPECTION BEING PERFORMED AT HKG; DAMAGE WAS FOUND TO THE RIGHT I/B AILERON, O/B AFT CORNER DELAMINATION / DAMAGE. PERMANENT REPAIR PERFORMED IN ACCORDANCE WITH THE 747-400 SRM 51-70-07 FIGUSDR C8GA20090167Skin · delaminatedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE RT OTBD AILERON T/E IS DELAMINATED ON INBD END. DAMAGED AREA WAS REMOVED DIM 3 INCH X 3 INCH, FABRICATED FILLER FROM 2024 T3 .012 INCH DIM 3 INCH X 3 INCH, DOUBLER FROM 2024 T3 .012 INCH DIM 5 INCH X 5 ISDR C8GA20090166Skin · delaminatedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE LT OTBD AILERON T/E IS DELAMINATED ON OTBD END. DAMAGED AREA WAS REMOVED DIM. 8 INCH X 3 INCH, FABRICATED FILLER FROM 2024 T3 .012 INCH DIM 8 INCH X 3INCH, DOUBLER FROM 2024 T3 .012 INCH DIM 8INCH X 5 ISDR C8GA20090146Skin · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE LEFT WING O/B AILERON T/E WEDGE IS DELAMINATED AT THE I/B END. DAMAGED AREA WAS REMOVED DIM 7" X 8". FABRICATED FILLER DIM. 7" X 8" FROM 2024 T3 .012", FABRICATED DOUBLER FROM 2024 T3 .012SDR C8GA20090139ASkin · dented"SUPPLEMENTAL INFORMATION" WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE RIGHT WING O/B AILERON IS DENTED ON THE UPPER T/E WEDGE. DAMAGED AREA WAS REMOVED, FABRICATED DOUBLER FROM 2024 T3 .012" DIM 4" DIA. INSTALLED HOT BOND REPAIR. NOSDR FDEA200906041912Hinge Bracket · wornFOUND WORN BORES IN HINGE BRACKET A576-61024-201 OF RT ASA. REPAIR PERFORMED BY OVERSIZING THE BORE AND BUSH INSTALLATION IAW RAS/FOK/132/2009 ISS B, APPROVED BY EA 6-5760-131211.SDR FDEA200906041911Hinge Bracket · wornFOUND WORN BORES IN HINGE BRACKET A576-61024-200 OF LT ASA. REPAIR PERFORMED BY OVERSIZING THE BORE AND BUSH INSTALLATION IAW RAS/FOK/134/2009 ISS B, APPROVED BY EA 6-5760-131210.SDR USAA2009060191360Aileron · delaminatedPHX - RON - MAJOR REPAIR - LOG 4521789 - DELAMINATION WITH PARTIAL SEPARATION ON RIGHT HAND AILERON LOWER LEADING EDGE JUST INBOARD OF OUTBOARD PCA. REPAIRED RIGHT HAND AILERON LOWER LEADING EDGE IAW B757 SRM 57-60-01, 51-70-04, & 51-70-17.SDR CA090515002Aileron · obstructed(CAN) INSP OF THE CONTROL SURFACES FOUND THAT AILERONS DO NOT MAKE TRAVEL LIMITS AND PUSH RODS ARE HITTING FWD SPARS OF THE LWR WINGS. ELEVATOR TAB IS UNABLE TO MAKE LIMITS AS STATED. BOTH TRAVEL LIMITS AS STATED IN MM 70206-001 DATED 5-20-1998 PAGE 6 STATE TRSDR IPXA09855858Skin · misrepairedINSPECTION TYPE:SVC SURVEY SEQ 852-W3-31 REPAIR DOUBLER AT LT INBD AILERON UPPER EDGE DOES NOT CORRELATE TO SRM REPAIR. REPAIR ACCOMPLISHED PER TIMCO REO-G12538 REV C AND UPS EO DC8-5720-33337-ASDR M2L2009F00000Hinge Bracket · brokenTHIS PART HAS 2 SMALL 90 DEGREE ANGLES AT EITHER SIDE BOTTOM. THEY HAVE LITTLE OR NO ACTUAL STRENGTH OTHER THAN TO PREVENT THE LOWER WING SKIN FROM NOT BEING SECURED. RT AILERON OTBD HINGE BRACKET. (K)SDR IPXA09M55886Aileron · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR 286-W3-05, EXISTING REPAIR DOUBLER ON LT WING INBD AILERON UPPER LE SKIN AT XIA 318-324 IS INCORRECT MATERIAL GAUGE. REMOVED EXISTING REPAIR DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER REF MD11 SRM 57-10-00 FIG 38.SDR C2XA09TY087Bracket · wornRT AILERON DAMPNER LUG MISSING HAT BUSHING. REMOVED AND REPLACED DAMPNER BRACKET IAW EMB 145 SRM 51-40-02.SDR C2XA09SH157Support Bracket · damagedSHV - DURING C-CHECK RT AILERON MOST O/B HINGE BRACKET I/B HOUSING DAMAGED. MAINTENANCE REMOVED AND REPLACED RT AILERON MOST O/B HINGE SUPPORT BRACKET ASSY IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR QXEA2009050500303Structure · chafedLEFT WING AILERON LEADING EDGE IS CHAFED ON CENTER AND OTBD EDGE. BLENDED DAMAGED AREA REF SRM 57-61-01-101-001-A01. HFEC INSPECTED BLENDED AREA FOR CRACKS IAW NDTM PART 6, 53-00-000-250-A01. NO CRACKS NOTED. UT THICKNESS CHECK IAW NDTM PART 1, 51-20-004 HSDR C2XA09SH137Attach Fitting · damagedSHV - DURING C-CHECK RT PCA ACTUATOR-TO-AILERON ATTACHMENT FITTING O/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND INSTALLED NEW RT PCA ACTUATOR-TO-AILERON ATTACHMENT FITTING IAW EMB-145 SRM 51-40-02 AND IAW EC 5750-01177 REV B. THE AIRCRAFT WAS APPROVED FSDR C2XA09SH136Attach Fitting · damagedSHV - DURING C-CHECK RT PCA ACTUATOR-TO-AILERON ATTACHMENT FITTING O/B ATTACHMENT POINT HAS TOOLING MARKS. MAINTENANCE REMOVED AND INSTALLED NEW RT PCA ACTUATOR-TO-AILERON ATTACHMENT FITTING IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS ASDR IPXA09M55865Wedge · misrepairedINSPECTION TYPE:C REPAIR SEQUENCE NBR 285-W4-015, RT WING, INBD AILERON INBD T/E, NEEDS VALIDATION FOR REPAIR. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-W4-015 DOES NOT CORRELATE TO SRM 57-20-00, FIG3, VOLI, REV40. EXISTING REPAIR WEDGE REMOVED PER SRM 5SDR CA090423006Balance Weight · corroded(CAN) AILERON INSP COMPLETED IAW ANNUAL INSP REQUIREMENTS. CORROSION DISCOVERED ON BALANCE WEIGHTS. BALANCE WEIGHTS REMOVED FOR FURTHER INVESTIGATION REVEALED CORROSION ON EACH ATTACH SCREW. CORROSION REMOVED FROM EACH BALANCE WEIGHT, NEW SCREWS INSTALLED AND SDR C2XA09TY063Bracket · damagedTYS - DURING C-CHECK INSPECTION THE LT AILERON PCA BRACKET OUTBOARD FITTING WAS FOUND DAMAGED/ELONGATED. THE PCA BRACKET WAS REMOVED AND REPLACED IAW EC 5750-0117 AND SRM 57-60-02. A/C STILL IN C-CHECK.SDR USAA2009042190943Skin · delaminatedBFM - C1 - MAJOR REPAIR - DELAMINATION ON RIGHT OUTBOARD AILERON LOWER SURFACE 12 INCHES INBOARD FROM OUTBOARD END. REPAIRED RIGHT OUTBOARD AILERON LOWER SURFACE IAW B767 SRM 51-60-01.SDR C2XA09SH126Attach Bracket · migratedSHC - DURING C-CHECK RT PCA TO AILERON O/B ROD O/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT PCA TO AILERON ATTACHMENT BRACKET IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH125Attach Bracket · wornSHV - DURING C-CHECK LT PCA TO AILERON ATTACHMENT HAS MIGRATED BUSHING. MAINTENANCE REMOVED AND REPLACED LT PCA TO AILERON ATTACHMENT BRACKET IAW EMB-145 EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH124Attach Bracket · gougedSHV - DURING C-CHECK LT AILERON PCA ATTACH POINT BRACKET O/B ROD ATTACHMENT I/B AND O/B HAT BUSHING HOUSINGS ARE GOUGED. MAINTENANCE REMOVED AND REPLACED LT PCA TO AILERON ATTACHMENT BRACKET IAW EMB-145 EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURSDR C2XA09SH123Attach Bracket · gougedSHV - DURING C-CHECK BRACKET ON THE RT AILERON THAT GOES TO THE PCA IS GOUGED. MAINTENANCE REMOVED AND REPLACED RT PCA TO AILERON ATTACHMENT BRACKET IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH122Attach Bracket · wornSHV - DURING C-CHECK RT AILERON TO PCA BRACKET MOST I/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT AILERON TO PCA ATTACHMENT BRACKET IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH121Attach Bracket · wornSHV - DURING C-CHECK RT PCA TO AILERON I/B ROD O/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT AILERON TO PCA ATTACHMENT BRACKET IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH120Attach Bracket · wornSHV - DURING C-CHECK RT PCA TO AILERON I/B ROD I/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT PCA TO AILERON ATTACHMENT BRACKET IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH119Bracket · wornSHV - DURING C-CHECK LT AILERON DAMPNER BRACKET I/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED LT AILERON DAMPNER BRACKET IAW SRM 51-40-02. MAINTENANCE PREPPED, PRIMED AND PAINTED LT AILERON DAMPNER BRACKET IAW EMB-145 CPM 51-21-06. THE AIRCRAFTSDR UIEA201000117Skin · damagedTHE PURPOSE OF THIS EO IS TO RECORD A MAJOR REPAIR. DURING C-CHECK INSP; DAMAGE WAS FOUND TO THE RT INBD AILERON UPPER SURFACE OTBD T/E CORNER MEASURING 0.5 IN. X 1.0 IN. (REF FIG 1). PERMANENT REPAIR PERFORMED IAW THE SRM 51-70-06 FIG 5.1. ACCOMPLISH REPAISDR 2009FA0000327Hinge Bracket · brokenLOWER SUPPORTING ANGLE CRACKED FROM MANY YEARS AND HOURS OF FATIGUE. THIS ACFT HAS BEEN OPERATED ON UNIMPROVED BACK COUNTRY DIRT LANDING STRIPS WHICH POUND AND SHAKE THESE ACFT EXTREMLY. THIS TYPE OF PART FAILURE IS TO BE EXPECTED UNDER THE CONDITIONS THIS ASDR FDEA200904111267Hinge · corrodedRT AILERON NR 1 HINGE BEARING BORE HAS PITTING CORROSION REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED BEARING BORE PER FED EX EA 6-5750-12450 AND RAS/BAE 1009828/2009.SDR FDEA200904111266Hinge · corrodedRT AILERON NR 4 HINGE BEARING BORE HAS PITTING CORROSION WITH EXFOLIATION REMOVED CORROSION FROM BORE FOUND TO OUT OF LIMITS. REPAIRED BEARING BORE PER FED EX EA 6-5750-12450 RAS/BAE/1009828/2009.SDR IPXA09M55671Skin · gougedINSPECTION TYPE:1C REPAIR SURVEY SEQ 291-W4-07, EXISTING REPAIR DOUBLER ON RT WING I/B AILERON UPPER SKIN BETWEEN XIZ 372.607-375.061 HAS A GOUGE. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW IPXA EO MD11-5750-33254-A. ALL WORK ACCOMPLISHED OSDR SWIA200922031Skin · chafedRIGHT AILERON LEADING EDGE SKIN CHAFED. (C CHECK) REPLACED PER SRM.SDR ASAA0945256Aileron · delaminatedLT AILERON LWR BOTTOM I/B EDGE DISBONDED. PREPPED DELAMINATED AREA, BONDED REPAIR IAW B737 400 SRM 51 70 03.SDR FDEA200904031167Hinge Fitting · corrodedFOUND CORROSION AND SCRATCHES ON LT AILERON HINGE FITTING. REPAIR PERFORMED BY REAM UP THE HOLE UNTIL DAMAGE REMOVAL AND INSTALLING A BUSHING IAW RAS/FOK/032/2009 ISS A , APPROVED BY EA 6-5750-120232.SDR CA090415001Screw · corroded(CAN) AILERONS REMOVED AT ANNUAL INSP. MASS BALANCE WEIGHT SCREWS MS35207-XXX REMOVED ON BOTH AILERONS AND FOUND CORRODED. AREA INSPECTED FOR CORROSION AND NEW SCREWS INSTALLED.SDR IPXA09655421Fairing · chafedINSPECTION TYPE:C LT WING - I/B AILERON FWD UPPER L/E FAIRING CHAFE DAMAGED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4G FIG 18.SDR C2XA09TY056Fitting · wornRT AILERON OUTBOARD PCA ROD BRACKET OUTBOARD BUSHING HOLE IS OUT OF LIMITS. REMOVED AND REPLACED PCA FITTING IAW EC 5750-01177. AIRCRAFT IS STILL IN C-CHECK.SDR AMCR200902Bushing · missingDURING ROUTINE INSP, FOUND TRAIL OF BLACK SOOT STREAMING FROM RT AILERON OTBD HINGE POINT. DISCOVERED BUSH MISSING IN AILERON SIDE OF HINGE WHEN CHECKING FOR PLAY. THE ARE (2) BUSHINGS REQUIRED, BUT ONLY ONE WAS INSTALLED ON AIRFRAME SIDE. OTHER FLIGHT CONTROLSDR IPXA09B55520Skin · misrepairedINSPECTION TYPE:C REPAIR SEQUENCE NUMBER 259-W4-006 NEEDS VALIDATION FOR REPAIR DUE TO NO CORRELATION WITH SRM. REPAIR DOUBLER & FILLER AT RT WING, INBOARD AILERON TOP FWD O/B SURFACE AT STA XIA 295, REMOVED PER SRM 51-35-01 & 51-31-01 VOL II REV 40 & EN115 2SDR CA090326010Structure · damaged(CAN) ACFT STRUCK BY LIGHTNING ON APPROACH. LT AILERON TIP REPLACED. P/N-35740407-007.REF:DEF: 836797,836938 AND WO-185137,NR-00001
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