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 = '5752' 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 = '5752' 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 DHL2008749014Tab · dentedDURING C CHECK, LT WING OUTBOARD AILERON CONTROL TAB HAS A DENT WBL 592 TOP SURFACE. DENTED AREA FOUND OUT OF LIMITS IAW SRM 57-50-1 FIG 4, CUT OUT DENTED AREA APPROXIMATE 2" DIAMETER. FABRICATED FILLER APPROXIMATE 2 INCHES DIAMETER AND DOUBLER APPROXIMATE 5SDR IXXA08SMN003STab · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CONTROL TAB AILERON DELAMINATED. REMOVED REPLACE AILERON CONTROL TAB IAW DC8 MM 27-11-4 PAGES 201-205, PERFORMED OPS CHECK TO ALL FLIGHT CONTROLS GOOD IAW DC8 MM 27-11-0 PAGES 10-14, DC8 MM 27-21-0 PAGES 5-9,SDR SWAA080235Skin · delaminatedDURING SCHEDULED 14Y CHECK, FOUND RT WING AILERON TAB DELAMINATED AT UPPER SURFACE T/E. REMOVED AND REPLACED TAB PER MM.SDR CA080108006Skin · cracked(CAN) AC UNDERGOING TURBO-PROP CONVERSION AT PRESENT. RT AILERON GEAR TAB INSPECTION REVEALED A CRACK IN THE LOWER SKIN UNDER THE LOWER IB MASS BALANCE WEIGHT MOUNT. THE CRACK IS APPROX 1.75 IN. LONG AND LOCATED LATERALLY, FWD OF THE BALANCE WEIGHT MOUNT ATTSDR SWAA080154Tab · debondedDURING SCHEDULED 20Y CHECK, FOUND LT WING AILERON BALANCE TAB T/E DISBONDED. REPAIRED TAB PER SRM.SDR USAA920080144Tab · delaminatedCLT - MAJOR REPAIR - C5 CHECK - LEFT WING AILERON TAB TRAILING EDGE DELAMINATED. REPLACED LEFT WING AILERON TAB IAW USAIRWAYS JOB CARD 03C30627009.SDR DHL2007746001Tab · debondedUPON WALK AROUND INSPECTION, FOUND RIGHT OUTBOARD AILERON TAB OUTBOARD DISBONDED ON UPPER SKIN APPROX 20 INCHES LONG. PART REPLACED.SDR DHL2007746002Tab · debondedUPON WALK AROUND INSPECTION, FOUND RIGHT OUTBOARD AILERON TAB OUTBOARD DISBONDED ON UPPER SKIN APPROX 20 INCHES LONG. PART REPLACED.SDR SWAA076168Tab · crackedDURING SCHEDULED 22Y CHECK, FOUND RT WING AILERON TAB CRACKED. REMOVED AND REPLACED TAB PER MM.SDR SWAA075867Bearing · wornDURING SCHEDULED C2 CHECK, FOUND LT WING AILERON TAB INBOARD HINGE HAS EXCESSIVE PLAY. REMOVED AND REPLACED NR 1 BEARING PER MM.SDR SWAA075701Tab · delaminatedDURING SCHEDULED BRDG CHECK, FOUND RT WING AILERON TAB DELAMINATED. REPAIRED TAB PER SRM.SDR SWAA075476Tab · delaminatedDURING SCHEDULED BRDG CHECK, FOUND LT WING AILERON TAB DELAMINATED. REPAIRED TAB PER SRM.SDR SWIA200718922Tab · corrodedLEFT AILERON TRIM TABS HAVE SURFACE CORROSION. REPLACED LEFT AILERON TRIM TAB OUTBOARD CONTROL ROD IAW EMB 120 MM 27-12-02.
SDR SWAA075024Tab · debondedDURING SCHEDULED BRDG CHECK, FOUND LEFT WING AILERON TAB DISBONDED AT AFT OUTBOARD CORNER. REPAIRED TAB PER SRM.SDR MWEA070213Trim Tab · corrodedRIGHT WING AILERON TRIM TAB HAS CORROSION UNDER SKIN, OUTBOARD TRAILING EDGE. REMOVED CORROSION AND FABRICATED AND INSTALLED AILERON TRIM TAB.SDR MWEA070212Tab · corrodedRIGHT WING AILERON CONTROL TAB HAS CORROSION UNDER SKIN, OUTBOARD TRAILING EDGE. REMOVED CORROSION AND FABRICATED AND INSTALLED CONTROL TAB.SDR CPCP20070108Channel · corrodedLT AILERON, TRIM TAB, CLOSING CHANNEL CORRODED. NEW TRIM TAB CLOSING CHANNEL REPLACED ON LT AILERON IAW SRM 51-25-03.SDR AWXA200700954Tab · delaminatedPHX - MAJOR REPAIR - NR 4109975, RIGHT WING AILERON TRIM TAB TRAILING EDGE IS DELAMINATED, WS 431.5. REPLACED RIGHT WING AILERON TRIM TAB TRAILING EDGE, WS 417 - WS 480 IAW AWA TASK CARD R3M27014.SDR SWAA073102Structure · crackedDURING SCHEDULED BRDG CHECK, FOUND LEFT WING AILERON TAB DELAMINATED ON OUTBOARD T/E. REMOVED AND REPLACED AILERON TAB PER MM.SDR SWAA073078Tab · wornDURING SCHEDULED C4 CHECK, FOUND RT WING AILERON TAB OUTBOARD HINGE FITTING WORN. REMOVED AND REPLACED AILERON TAB PER MM.SDR 07FDEA02076Tab · delaminatedRIGHT WING INBD AILERON TAB OTBD AFT AREA HAS 1" AREA OF DELAM REMOVED AND REINSTALLED R/W INBD AILERON TAB REF MM 27-10-011-4 ADJ/CHECK REF MM 27-10-000-5, OPS CHECK GOOD.SDR 07FDEA02024Tab · delaminatedRIGHT WING OTBD AILERON TAB HAS A 37" LONG AREA OF DELAM FROM OTBD EDGE. REMOVED AND REPLACED R/W OTBD AILERON TAB REF M/M 27-10-041-4. PERFORMED ADJ/TEST REF MM 27-10-000-5, OPS CHECK GOOD.SDR ASAA0741635Tab · delaminatedLEFT AILERON TAB IS DELAMINATED AT T/E. REMOVED AND REPLACED LEFT AILERION TAB IAW AMM 27-11-21 PG 401.SDR ABXA070122Tab · delaminatedRIGHT AILERON OUTBOARD TAB DELAMINATED 3 PLACES, 1 UPPER AND 2 LOWER APPROXIMATELY 3 BY 3, 3 BY1 1/2, OUTBOARD TIP REPAIR DISBOND. REMOVED AND REPLACED RIGHT AILERON TRIM TAB IAW DC9 MM 27-10-5.SDR QXEA200700543Hinge Fitting · wornC4 PDX - RIGHT AILERON TAB, INBOARD CENTER HINGE FITTING IS WORN. REPAIRED IAW SRM 51-40-11.SDR 07FDEA01182Tab · delaminatedLT WING IB AILERON TAB CONTROL ARM FAIRING IS DISBONDED AT AFT EDGE CLEANED AREA, REPAIRED FAIRING REFERENCE SOPM 20-50-12 PAGE 11 PARA 4.SDR SWAA071011Tab · wornDURING SCHEDULED C2 CHECK, FOUND RT WING AILERON TAB ATTACH POINTS WORN. REMOVED AND REPLACED AILERON TAB PER MM.SDR AWXA200700211Tab · delaminatedMCN - MAJOR REPAIR - LEFT WING AILERON TAB OUTBOARD TRAILING EDGE IS DELAMINATED, WBL 479.50 - 480.00. REPAIRED LEFT WING AILERON TAB OUTBOARD TRAILING EDGE, WBL 479.50 - 480.00 IAW B737-300 SRM 51-70-06 REPAIR 2.SDR AWXA200700198Tab · crackedMCN - FOUND LEFT WING AILERON TAB UPPER SKIN TRAILING EDGE CRACKED, WS 433.25, 16" FROM INBOARD EDGE. REPAIRED LEFT WING AILERON TAB UPPER SKIN TRAILING EDGE, WS 433.25, 16" FROM INBOARD EDGE IAW B737-300 SRM 51-70-07.SDR PIDR2006040Tab · separatedTRAILING EDGE OF THE RT AILERON TAB IS SEPARATED. REPAIRED MINOR DAMAGE PER SRM 51-70-16. BALANCED TAB, NO WEIGHT CHANGE.SDR ASAA0681151Tab · nickedRIGHT AILERON CONTROL TAB IS NICKED ON T E. REPAIRED WITH FILLER COMPOUND AND SANDED TO ORIGINAL CONTOUR PER SRM 51 70 1A.SDR AWXA200601629Tab · delaminatedC-17 CHECK - NR 5934335, LT AILERON TAB DELAMINATED ON T/E, 18IN FROM IB END. REPAIRED LT AILERON TAB T/E, 18IN FROM I/B END IAW SRM 51-70-06-0G REPAIR NR 7 FIG 14.SDR AWXA200601615Tab · delaminatedMAJOR REPAIR - C-17 CHECK, NR 5934335. LT AILERON TAB TRAILING EDGE IS DELAMINATED, 18 INCHES FROM IB END. REPAIRED LT AILERON TAB TRAILING EDGE, 18 INCHES FROM IB END IAW SRM 51-70-06, FIGURE 14, REPAIR NR 7.SDR DHL2006786002Tab · delaminatedLEFT OUTBOARD AILERON TAB HAS TWO AREAS OF DELAMINATION. ONE AREA IS BY THE CONTROL ROD AND THE OTHER IS AT THE INBOARD END AND IS SPLIT. FOUND DURING NORMAL VISUAL INSPECTION DURING A CHECK. TAB WAS REPLACED. NR ITEM NR 040740 PART NR OFF 65-27725-41 S/N SDR QXEA200602529Tab · wornC4 YYC - RIGHT AILERON TAB FITTING AT STATION YW 444 HAS WEAR FROM BUSHING. REPAIRED IAW SRM 51-40-11.SDR HALA0600687Crank Assy · chafedR/W OB FLAP ACTUATOR CRANK ARM 6-9 LINK LWR OB SIDE CHAFING ON LINK SUPPORT FITTING AT FWD OB SIDE. REPAIRED CHAFED AREA ON LINK SUPPOR AND 6-9 LINK IAW SRM 57-53-02 AND SRM 51-20-06.SDR SWAA063175Tab · delaminatedDURING SCHEDULED MV2 CHECK, FOUND RT WING AILERON TAB T/E DELMINATED. REMOVED AND REPLACED AILERON TAB PER MM.SDR USAA060969Tab · wornTRAILING EDGE OF TAB, RIGHT HAND AILERON TAB HAS WEAR. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 51-70-06 REPAIR 10, DEFECT SIZE: 10 X .50 INCH.SDR USAA060968Tab · wornRIGHT TAB TRAILING EDGE, RIGHT HAND AILERON HAS WEAR. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 51-70-06 REPAIR 10, DEFECT SIZE: 6 X .50 INCH.SDR IXXA06SMN105SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, RIGHT HAND WING- INBOARD AILERON TRIM TAB UPPER AND LOWER SKIN DELAMINATED. CLEANED AND BONDED RIGHT HAND INBOARD AILERON TRIM TAB UPPER AND LOWER SKIN EDGE WITH HYSOL IAW DC8 SRM 51-1-9.SDR DHL2006764517Tab · dentedDENT ON R/WING OB AILERON TAB UPPER SURFACE. CUT OUT DENTED AREA ON RT OB AILERON TAB APPROX 1 INCH DIA FABRICATED FILLER APPROX 1 INCH DIA AND DOUBLER APPROX 3.7500 INCHES X 4 INCHES FROM 2024-T3 .010 PO NR 9912184CLEANED, PREPPED PRIMED, BONDED CLEANED TREATSDR DU4R2006358Tab · delaminatedS/O 304001; NR 21453 - RT IB AILERON TAB DELAMINATED AT LOWER SURFACE OUTER L/E AREA. CUT OUT DISBONDED SKIN. FABRICATED AND BONDED DOUBLER 10.5 X 3.7500 INCH X 9 X 3.5 X 2.2500 INCH AND FILLER 8 INCH X 1.7500 INCH X 7.2500 INCH X 1 INCH X 1 INCH FROM 2024-TSDR AWXA200600658Tab · delaminatedMCN - DURING C19 CHECK DISCOVERED RIGHT AILERON TAB SEPARATED IN SPOTS ALONG TRAILING EDGE. MAINTENANCE REMOVED AND INSTALLED NEW RIGHT HAND AILERON TAB IAW AWA TASKCARD R3M27014.SDR UPS06246460Shim · looseRT WING O/B AILERON TAB DELAM DBLR LWR SURFACE. UPON INVESTIGATION FOUND DELAMINATION TO BE A SHIM THAT CAME LOOSE. STARTED REMOVAL OF AILERON BAL. TAB UP TO STEP D ON MM 27-10-19-4 REINSTALLED BOLTS IN TAB REDS AND INSTALLED COTTER PINS. RESECURED LOOSE SHSDR SWAA060668Tab · delaminatedDURING SCHEDULED 1/4D CHECK, FOUND RT WING AILERON TAB DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED TAB PER MM.SDR SWAA060669Bellcrank · brokenDURING SCHEDULED MV2 CHECK, FOUND LT WING OUTBOARD T/E FLAP INBOARD ACTUATOR BELLCRANK BROKEN. REMOVED AND REPLACED BELLCRANK PER MM.SDR ASAA0640104Tab · chippedTHE RIGHT AILERON TAB IS CHIPPED ON THE TE AT THE IB END. SMOOTHED DAMAGED AREA, PREPPED AND APPLIED ONE REPAIR AND TWO FILLER FIBERGLASS PLIES AND HOT BONDED IAW SRM 51-70-16 PG 4,10,20 AND 26.SDR SWAA060393Tab · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING AILERON TAB DELAMINATED. REMOVED AND REPLACED TAB PER MM.SDR AWXA200600266Tab · debondedMCN - DURING C19 CHECK DISCOVERED THE RT AILERON TAB DISBONDED ON CORNER FROM WS 476.5R TO WS 479.5R. MAINTENANCE REMOVED DAMAGED AREA ON THE RT AILERON TAB IAW BOEING 737-300 SRM 51-70-07-0G REPAIR 1 FIG 9. BONDED REPAIR PLIES TO THE RT AILERON TAB FROM WS SDR 2006FA0000060Bushing · wornAILERON TRIM MADE POPPING NOISE AS CONTROL WAS ROTATED. FOUND BUSHING FOR CONTROL SHAFT IN PEDESTAL SEVERELY WORN ALLOWING U-JOINT TO CONTACT STRUCTURE AS CONTROL WAS ROTATED. TRIM CABLE TENSION WAS WITHIN LIMITS, NO REASON FOR ACCELERATED WEAR NOTED. BUSHI
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