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 DLM11991113Skin · delaminatedLEFT O/B AILERON / FRONT SPAR / LWR FLANGE / XDA 928: TOOLING DAMAGE TO LOWER SPAR FLANGE. SPAR IS M/F SOLID GRAPHITE LAMINATE, APPROX .208 THICK. LOWER FLANGE IS DELAMINATED THROUGH THICKNESS OVER APPROX 1 INCH DEPTH (CHORD-WISE) X 2 WIDTH (SPAN-WISE). RSDR AU990919Bracket · corroded(AUS) RIGHT AILERON CONTROL UNIT LOWER MOUNT BRACKET CORRODED.SDR UF6A990539Stringer · crackedSBN - RIGHT AILERON UPPER STRINGER NR 2 AT STATION 342.696 WAS FOUND TO BE CRACKED. MAINTENANCE FABRICATED NEW STRINGER FROM RIB 333.454 TO 359.216. AREA WAS ALODINED, PRIMED AND FINISHED PER FACTORY SPECIFICATIONS. ALL WORK WAS DONE IAW BAE ATP SRM 51-10-0SDR UPS99229647Casting · corrodedINSPECTION TYPE:C, RIGHT O/B AILERON TAB ROD HINGE CASTING CORRODED. HINGE CASTINGS REMOVED AND REPLACED IAW MM 27-10-41.SDR UPS99229628Hinge · corrodedINSPECTION TYPE:C, RIGHT I/B AILERON CENTER HINGE FITTING CORRODED. REPLACED HINGE FITTING IAW MM 27-10-01.SDR UF6A990518Skin · tearSBN - RIGHT AILERON HAS A SMALL TEAR IN THE OUTER SKIN AT THE RADIUS OF THE CENTER HINGE. MAINTENANCE BURNISHED TEAR AND WAS FOUND WITHIN IAW BAE ATP SRM 51-10-01. AREA WAS ALODINED AND PRIMED. (M)SDR TWAA9906302Rib · crackedDURING OP 16 MAINT CHECK, FOUND RT AILERON RIB WITH DENT AND .25 INCH IN LONG CRACK, APPROX 10 IN FROM OTBD END AND 5 IN FROM LE. ACCOMPLISHED HFEC TO LOCATE ENDS OF CRACK. REPAIRED PER SRM 53-01, PAGE 10 FIG 2 SHEET 4.SDR 99FDEA00152Hinge · corrodedNR 417 76C030-00 RT WING OUTBD AILERON-HINGE CASTING HAS DEEP PITTED CORROSION IN MAGNESIUM CASTING. REMOVED AND REPLACED CASTING WITH NEW SAND CASTED ALUM CASTING PER DRW BOEING NR 65-12959 AND FASTENERS IAW SRM 51-30-2 AND STANDARD PRACTICE.SDR 99FDEA00151Hinge · corrodedNR 415 76C030-00, RT WING-OUTBD AILERON 2ND AILERON HINGE OB HING CASTING HAS DEEP PITTED CORROSION TO MAGNESIUM CASTING. REMOVED AND REPLACED CASTING WITH NEW TYPE SANDCAST ALUM IAW BOEING INSTALL DRAW NR 65-19260 AND FASTENERS WITH SRM 51-30-2 AND STANDARD SDR ABXA9900363Skin · crackedDURING C-CHECK, FOUND RIGHT AILERON SKIN TRAILING EDGE CRACKED. REPLACED RIGHT AILERON SKIN TRAILING EDGE IAW DC9 SRM 51-30-08.SDR DHL9970153DFitting · crackedAT D-CHECK, LEFT WING O/B AILERON O/B HINGE FITTING CRACKED AT AFT UPPER END AT SKIN ATTACH FLANGE. REMOVED O/B HINGE FITTING AT LEFT WING PER SRM 51-30-2. REPLACED O/B HINGE FITTING PER SRM 57-30-2.SDR CALA9900407Skin · crackedINSPECTION FOUND A .5 AND .375 INCH CRACK IN LT O/B AILERON LOWER SKIN WITH A BEND AT I/B EDGE. THE AILERON WAS REMOVED AND REPLACED IAW MM 27-10-31.SDR UPS99229439Hinge · corrodedINSPECTION TYPE:C+SI, RT I/B AILERON CENTERING HINGE CORRODED. CENTERING HINGE REMOVED AND REPLACED IAW 27-10-01.SDR 99FDEA00187Hinge · corrodedNR 417 RT WING, OTBD AILERON HINGE CASTING HAS DEEP PITTED CORROSION IN MAGNESIUM CASTING. REMOVED AND REPLACED CASTING WITH NEW SAND CASTED ALUM CAST PER DRW BOEING NR 65-15959 AND FASTENERS IAW SRM 51-30-2 AND STANDARD PRACTICES.SDR 99FDEA00186Hinge · corrodedNR 415, RT, WING OTBD AILERON 2ND HINGE O/B HINGE CASTING HAS DEEP PITTIED CORROSION TO MAGNESIUM CASTING. REMOVED AND REPLACED CASTING WITH NEW TYPE SANDCASTING ALUMINUM IAW BOEING INSTALL DRW NR 65-19260 AND FASTENERS IAW SRM 51-30-2 AND STANDARD PRACTICES.SDR 99ZZZX2102Rib · crackedDURING THE NORMAL INSPECTION INTERVAL, CRACKS WERE FOUND IN THE WING RIBS WHERE THE INBOARD AILERON HINGE PLATES (PN 105-100011-51) AND THE OUTBOARD AILERON HINGE PLATES (P/N 105-100011-51) ATTACH. THE SAME PROBLEM HAS BEEN FOUND ON OTHER AIRCRAFT OF SAME MODSDR UPS99229224Fitting · corrodedINSPECTION TYPE:C, LEFT WING OUTBOARD AILERON CENTER OUTBOARD HINGE FITTING CORROED (AILERON SIDE). REPLACED PER SRM 51-30-2.SDR UPS99229210Fitting · corrodedINSPECTION TYPE:C LEFT WING OUTBOARD AILERON CENTER INBOARD HINGE FITTING CORRODED AILERON SIDE. REPLACED HINGE FITTING PER SRM 51-30-2.SDR DHL9970103DCasting · corrodedAT D-CHECK, LEFT WING I/B AILERON LOWER INPUT CASTING IS CORRODED. REMOVED AND REPLACED CASTING PER SRM 59-50-1. REBALANCE NOT REQD PER SRM 51-80-1. RERIGGED PER MM 27-10-0.SDR DHL9970154DCasting · corrodedAT D-CHECK, LEFT AILERON LOCKOUT SUPPORT CASTING IS PITTED AT ALL THRU BOLT ATTACH POINTS. REMOVED AND REPLACED SUPPORT CASTING PER SRM 51-30-2.SDR CALA9900333Skin · corrodedINSPECTION FOUND RT WING O/B AILERON LOWER SKIN CORRODED. THE AILERON WAS REMOVED AND REPLACED IAW MM 27-10-02.SDR UPS99229353Skin · damagedINSPECTION TYPE:C+SI, LT I/B AILERON HAS DAMAGE ON UPPER SKIN AT FWD O/B END. DAMAGED AREA TRIMMED IAW SRM 57-50-5.SDR DHL9980748CHinge · crackedAT C CHECK, LT WING AILERON HINGE NR 6 HAS CRACK ON AILERON MOUNT FLANGE. REMOVED HINGE AND INSTALLED NEW HINGE PER MM 27-10-1. N/R 896SDR DHL9980708CPanel · crackedAT C-CHECK, LT I/B AILERON I/B LOWER SURFACE ON ACCESS PANEL HAS CRACKED PLATE. FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 51-1-21, 5 X 4.SDR ABXA9900326Fitting · crackedRIGHT WING INBOARD AILERON, INBOARD ATTACH FITTING IS BROKEN OFF ON AILERON SIDE. REPLACED FITTING IAW DC8 SRM 27-10-00.SDR UPS99228977Skin · corrodedINSPECTION TYPE-C, RT OUTBOARD AILERON HAS CORROSION ON LOWER SKIN AFT OF NR 2 HINGE AREA. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPLACED RT OUTBOARD AILERON IAW MM 27-10-31.SDR UPS99228917Fitting · corrodedINSPECTION TYPE-C, CORROSION RT WING O/B AILERON CENTER O/B HINGE FITTING. REMOVED AND REPLACED PER SRM 51-30-2.SDR AU990501Bracket · cracked(AUS) AILERON MASS BALANCE ATTACHMENT BRACKET CRACKED.SDR 20000714SH016Bracket · crackedTHIS AIRCRAFT IS EQUIPPED WITH A ROBERTSON STOL KIT. BOTH OUTBOARD AILERON ATTACH BRACKETS WERE FOUND CRACKED AND BROKEN. THE ADDITIONAL STRESSES RELATED TO THE ROBERTSON CAUSED THIS CONDITON. ALL ROBERTSON STOL EQUIPPED AIRCRAFT SHOULD HAVE THIS BRACKET INSDR 20000714SH015Bracket · crackedTHIS AIRCRAFT IS EQUIPPED WITH A ROBERTSON STOL KIT. BOTH OUTBOARD AILERON ATTACH BRACKETS WERE FOUND CRACKED AND BROKEN. THE ADDITIONAL STRESSES RELATED TO THE ROTATION CAUSED THIS CONDITION. THESE PARTS SHOULD BE INSPECTED ON ALL ROBERTSON EQUPPED AIRCRAFSDR UPS99828926Skin · crackedINSPECTION TYPE-C3, RT I/B AILERON IS CRACKED, TOP O/B END UNDER THE WEIGHT COVER. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-0 FIG 2A.SDR P2EA99111Skin · delaminatedSJO - DURIGN Q-CHECK RIGHT AILERON WAS FOUND WITH DELAMINATION. AILERON WAS REPAIRED AS PER COOPESA NR COO-CMP-3-57-151-99. (M)SDR P2EA99106Skin · delaminatedSJO - DURING Q-CHECK, DELAMINATION WAS FOUND ON THE LEFT AILERON. THE AILERON WAS REPAIRED PER COOPESA EO COO-CMP-3-57-127-99. (M)SDR F3LA99022Fitting · brokenPHX - DURING C-CHECK INSPECTION, REPORTED LEFT WING CENTER AILERON HINGE FITTING AFT END BROKEN. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED ATTACH ANGLE AND REPAIRED PER SRM 51-30-2, 51-20-3, AND 51-20-1 AND 51-40-4. (M)SDR UPS99829087Skin · dentedINSPECTION TYPE-C, RT WING AILERON DENTED IN UPPER SKIN. CUT OUT DAMAGE, FABBED REPAIR DOUBLER IAW DC8 SRM 57-2-1- FIG 2, INSTALLED DOUBLER IAW DC8 SRM 51-1-21A (W & B DONE ON UPS NR 876762).SDR UPS99228967Casting · corrodedINSPECTION TYPE-D, LT I/B AILERON I/B HINGE CASTING CORRODED. CASTING REPLACED IAW DWG 65-21765 AND SRM 51-30-02.SDR UPS99228966Support · corrodedINSPECTION TYPE-D, LT I/B AILERON CENTRE HINGE SUPPORT CORRODED. CENTER HINGE SUPPORT REPLACED IAW MM 27-10-01.SDR UPS99228965Casting · corrodedINSPECTION TYPE-D, RT I/B AILERON ACTUATING ROD ATTACH CASTING HAS SEVERAL AREAS OF PITTING CORROSION. CASTING REPLACED IAW DRAWING 65-21765 AND SRM 51-30-02.SDR UPS99228754Hinge · corrodedINSPECTION TYPE-C, WHILE WORKING CUSTOMER CARD 866785 FOUND LT WING O/B AILERON CENTER O/B FWD HINGE HALF CORRODED. REMOVED CORRODED HINGE AND INSTALLED NEW HINGE IAW SRM 51-30-2.SDR UPS99228751Fitting · corrodedINSPECTION TYPE-C, RT WING O/B AILERON ACTUATOR ROD END FITTING IS CORRODED. REMOVED CORROSION FITTING AND INSTALLED NEW FITTING IAW SRM 51-30-2.SDR UPS99228750Hinge · corrodedINSPECTION TYPE-C, WHILE WORKING CUSTOMER CARD 866785 FOUND LT WING O/B AILERON CENTER I/B FWD HINGE HALF CORRODED. REMOVED CORRODED HINGE AND INSTALLED NEW HINGE IAW SRM 51-30-2.SDR UPS99228749Hinge · corrodedINSPECTION TYPE-C, WHILE WORKING CUSTOMER CARD 866785 FOUND O/B FWD HINGE HALF CORRODED, LT WING O/B AILERON. REMOVED CORRODED HINGE AND INSTALLED NEW HINGE IAW SRM 51-30-2.SDR DHL9974007CSkin · delaminatedAT C CHECK, L/W OUTBD AILERON UPPER SURFACE AT OUTSIDE UPPER SURFACE TRAILING EDGE DELAMINATED. INSTALLED BONDED REPAIR PER SRM 51-40-6, NO BALANCE REQUIRED PER SRM 51-80-4, 7 BY 2 N/R 1108.SDR UPS99228629Fitting · corrodedINSPECTION TYPE:SI R/W O/B AILERON, UPPER QUADRANT HINGE HAS PITTING AROUND HINGE BOLT. REMOVED PITTED FITTING, INSTALLED NEW FITTING IAW SRM 51-30-2 PG 14 PARA 7 AND PG 8 PARA A5.SDR 99ZZZX1030Skin · delaminatedAIRCRAFT WAS BEING ANNUALED AND AD 79-22-04 PARA (A)(2) WAS BEING PERFORMED. FOUND THE UPPER SKIN DELAMINATED FROM THE LEADING EDGE AFT FROM 1 INCH TO 4 INCHES AT THE BONDED RIBS.SDR RRXA991047Skin · damagedDURING A MAINTENANCE VISIT, FOUND DAMAGE, UPPER SKIN, RT O/B AILERON AT STA XW 698. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCSDR RRXA991045Skin · damagedDURING A MAINTENANCE VISIT, FOUND DAMAGE, SKIN, RT O/B UPPER SKIN RT O/B AILERON AT FWD AREA BETWEEN STA XA 630.250 AND 608.634. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER SDR P5CA9900035Panel · corrodedLEFT WING UPPER SURFACE OF OUTBOARD AILERON FIX PANEL SMALL AREA OF CORROSION. REPAIRED PER SRM 51-10-01 AND 51-10-02.SDR P5CA9900060Link · wornRIGHT INBOARD AILERON/REACTION LINK FOUND WORN. REPAIRED AND REPLACED BEARINGS PER OHM 20-50-03.SDR AU990033Balance Weight · corroded(AUS) RIGHT AILERON MASS BALANCE ARM SNAPPED OFF ADJACENT TO ITS CLAMP DURING MEDIUM WIND BUFFETING. INSPECTION OF THE ARM REVEALED CORROSION AROUND 70 PERCENT OF THE CIRCUMFERENCE. THE LEFT ARM ASSEMBLY WAS THEN INSPECTED AND FOUND TO BE CORRODED ON THE REA
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