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 PNSA971001Screws · looseAILERON JAMMED IN LEFT TURN PILOT WAS ABLE TO FREE-UP CONTROLS AND LAND SAFELY. FURTHER INVESTIGATION REVEALED SCREWS THAT ATTACH AILERON BALANCE WEIGHT TO LEADING EDGE OF AILERON HAD BACKED OUT TO THE POINT OF CATCHING THE TRAILING EDGE OF THE WING GAP FAISDR UPS97224709Hinge · corrodedINSPECTION TYPE-SI, LEFT WING OUTBOARD AILERON INBOARD CENTER FIXED TRAILING EDGE HINGE FITTING CORROSION. REPLACED IAW 51-30-2 AND 27-10-00.SDR 97ZZZX4604Weight · wrong partFOKKER F27 SM, CHAPTER 51-50-00, 'CONTROL SURFACE BALANCING'. LT AILERON REMOVED FOR BALANCE CHECK AFTER REPLACEMENT OF THE LT BALANCE TAB. BALANCE TAB REPLACED DUE TO COLLISION WITH CESSNA 340 WHILE PARKED AT ALLEGHENY COUNTY AIRPORT, PITTSBURGH, PA. THE BSDR P5CA9701680Skin · splitSPLIT ON RIGHT OUTBOARD AILERON TRAILING EDGE. REPAIRED USING POTTING AND FIBERGLASS OVERLAYS PER BOEING SRM 51-40-09.SDR CA971010007Aileron · cracked(CAN) RIGHT AILERON LEADING EDGE SKIN CRACKED IN TWO PLACES UNDER INBD BALANCE WEIGHT. SCREW HEADS ABOUT 1 INCH LONG EACH. LEADING EDGE REPLACED. PART TC: 2,277 HOURS.SDR ABXA9701634Fitting · crackedINBOARD AILERON INBOARD HINGE FITTING, RT WING IS CRACKED. REPLACED INBD AILERON INBD HINGE FITTING RT WING PER SRM 51-1-21, 51-1-20D AND 51-3-0.SDR 97ZZZX4479Aileron · crackedWHEN REBONDING STATIC WICKS TO AILERON, MECHANIC NOTICED CRACKS BENEATH BOTH INBOARD AND OUTBOARD STATIC WICK BASES.SDR UPS97824604Hinge · crackedINSPECTION TYPE-C, RT O/B AILERON, O/B HINGE FITTING CRACKED. REMOVED AND REPLACED AILERON IAW MM 27-11-02.SDR AALA971808Rib · corrodedTUL - OUTBOARD AILERON INBOARD CLOSURE RIB CORRODED. REMOVED AND REPLACED INBOARD CLOSURE RIB PER ESO 2615. TST: 70,323.2 HOURS. CYCLES, 48,502. (X)SDR AALA971800Casting · corrodedTUL - RIGHT OUTBOARD AILERON MAG CASTING CORRODED BEYOND LIMITS AT NUMEROUS PLACES. REMOVED AND INSTALLED NEW RT OTBD AILERON CASTING. TST: 70,323.2 HOURS. CYCLES, 48,502. (X)SDR CALA9701474Aileron · disbondedRIGHT OUTBOARD AILERON OUTBOARD TRAILING EDGE SECTION INBOARD UPPER SURFACE DISBONDED. REMOVED DAMAGED AREA. FABRICATED NEW CORE AND SKIN. ACCOMPLISHED HOT BOND REPAIR PER SRM 51-40-6.SDR QXEA9700617Skin · dentedPDX - RIGHT AILERON 2X3X.065 DENT. REPAIRED IAW SRM 57-01-01 PAGE 86-C-(2).SDR P5CA9701445Skin · delaminatedRT INBOARD AILERON TRAILING EDGE SEPARATED AT OUTBOARD EDGE.SDR DL72K971627Skin · puncturedLT OB AILERON SKIN PUNCTURED. REPAIRED PER MM 57-51SDR 97ZZZX3888Aileron · out of balanceANNUAL INSPECTION FOUND ELEVATOR AND AILERONS OUT OF BALANCE DUE TO RECENT PAINT JOB. UNITS HAD NOT BEEN STRIPPED PRIOR TO PAINTING OR CHECKED FOR BALANCE. NO REFERENCE TO AD 87-02-02 OR AD 94-20-04 WAS FOUND IN RECORDS.SDR 97FDEA00534Fitting · corrodedNR 0271 005 - R/W I/B AILERON, I/B TAB FITTING CORRODED (AREA MARKED).SDR P5CA9701395Skin · puncturedLEFT OUTBD AILERON PUNCTURE INBD END. REPAIRED PER BOEING SRM 51-40-15.SDR 97ZZZX3992Spade · brokeRIGHT AILERON SPADE BENT AND BROKE JUST ABOVE TIG WELD.SDR 97ZZZX4280Bearing · failedINSTALLED NEW AILERON HINGE BEARING ASSY. DURING INSTALLATION OF AILERON HINGE BOLT, BEARING CAME APART. HAD BEARING ASSY BEEN ASSEMBLED AND INSPECTED PER S26-4558 SPEC, ITEM WOULD NOT HAVE BEEN SOLD TO OUTSIDE COMPANY AS SERVICEABLE PART.SDR 97ZZZX3630Rib · crackedWHILE REPLACING THE SKIN ON THE OUTBOARD SIDE OF THE LEFT AILERON, THE CENTER RIB WAS FOUND CRACKED IN THE FORWARD ATTACH FLANGE. THIS AREA IS RIGHT BEHIND THE ACTUATING PUSH ROD. BOLTS WERE TIGHT. TOTALLY INACCESSIBLE TO VIEW.SDR CALA9701185Hinge Fitting · crackedINSPECTION FOUND A .25 INCH CRACK IN HINGE FITTING FORWARD OF OUTBOARD AILERON, SECOND HINGE FROM OUTBOARD END. THE HINGE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2.SDR DL72S971362Skin · loose fastenersFASTENERS PULLING THROUGH UPPER SKIN. SPLICED SKIN PER SRM 57-50-5, RT AILERON.SDR DL72S971284Skin · damagedRIVETS PULLING THROUGH SKIN SEVERAL AREAS. SPLICED SKIN PER SRM 57-50-5, FIG 3.SDR CALA9701096Skin · debondedINSPECTION FOUND LT OUTBOARD AILERON OUTBOARD MOST TRAILING EDGE SPLIT/DEBONDED. THE AILERON TRAILING EDGE WEDGE WAS REMOVED. REPLACEMENT SKIN PANELS WERE FABRICATED AND INSTALLED IAW SRM 51-40-6 AND 51-30-2. THE AILERON WEDGE WAS REINSTALLED.SDR P5CA9701211Skin · delaminatedRT WING, INBD AILERON DELAMINATED. REPAIRED PER BOEING SRM 51-40-09.SDR UPS97824327Doubler · crackedINSPECTION TYPE-D, LT INBD AILERON INTERNAL DOUBLER AT ACCESS PANEL 541 IS CRACKED. REPAIRED IAW SRM 57-2-1.SDR UPS97824087Skin · crackedINSPECTION TYPE-D, THE LT INBD AILERON T/E, OTBD END IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT T/E IAW SRM 51-1-21, 53-1-0, 51-1-9A, AND 57-2-1.SDR CA970710009Longeron · cracked(CAN) DURING ENGINEERING ORDER EDDY CURRENT INSPECTION E.O. NO.07-238D AILERON LONGERON 6L AT FUSELAGE STN 688 FOUND CRACKED. CONFIRMED BY VISUAL INSPECTION. NEW SECTION OF LONGERON REPLACED AS PER STRUCTURAL REPAIR MANUAL 53-02 PAGE 2A.SDR 97FDEA00378Hinge · corrodedNR 0328 033 STA-PAE - R/W O/B AILERON CENTER O/B HINGE FITTING ON AIRCRAFT IS CORRODED (REQUIRES AILERON REMOVAL). REMOVED R/W O/B AILERON. REMOVED AND REPLACED R/W O/B AILERON, O/B HINGE FITTING. REINSTALLED R/W O/B AILERON ALL WORK DONE IAW FED-EX M/M 27SDR 97FDEA00363Hinge · corrodedSTA-PAE: RT WING O/B AILERON CENTER O/B HINGE FITTING ON AIRCRAFT IS CORRODED (REQUIRES AILERON REMOVAL). *S/D* REMOVED RT WING O/B AILERON. REMOVED AND REPLACED RT WING O/B AILERON, O/B HINGE FITTING. REINSTALLED RT WING O/B AILERON. ALL WORK DONE IAW FSDR UPS97223581Tab Hinges · corrodedINSPECTION TYPE:SI, L/W INBOARD AILERON TAB HINGES ARE CORRODED TAB SIDE. REMOVED AND REPLACED TAB HINGES IAW SRM 51-30-5 AND 51-30-2.SDR AALA971115Casting · corrodedTUL - WEB BULGING INBOARD OF INBOARD AILERON QUADRANT ATTACH CASTING. REMOVED AND INSTALLED SERVICEABLE AILERON QUAD CASTING. TST: 55,431 HOURS. CYCLES, 34,330. (X)SDR UPS97823650Skin · corrodedINSPECTION TYPE:D, RT AILERON UPPER L/E SKIN HAS HEAVY CORROSION AT BOTH CENTER BALANCE BAYS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SKIN PANEL IAW SRM 51-1-21, 51-3-0, 57-8-1 AND DWG 5705334.SDR MWEA97500Aileron · delaminatedDURING D-CK, RT AILERON CORRODED/DELAMINATED LT RUB STRIP. MAINT REPAIRED IAW SRM 51-70-2.SDR MWEA97499Aileron · delaminatedDURING D-CK, LT AILERON CORRODED AND DELAMINATED. MAINT REPAIRED IAW SRM 51-70-02.SDR 97ZZZX2946Aileron · water contamFOUND STAINS ON THE LT AND RT AILERON LEADING EDGES. INVESTIGATED AND FOUND WATER SEEPING FROM AILERON LEADING EDGE FASTENER HOLES. REMOVED NECESSARY FASTENERS TO DRAIN AND PURGED THE AILERON LEADING EDGE. RE-INSTALLED BLIND FASTENERS WITH SEALANT PER FAA FSDR 97ZZZX2945Aileron · water contamFOUND STAINS ON THE LT AND RT AILERON LEADING EDGES. INVESTIGATED AND FOUND WATER SEEPING FROM AILERON LEADING EDGE FASTENER HOLES. REMOVED NECESSARY FASTENERS TO DRAIN AND PURGED THE AILERON LEADING EDGE. RE-INSTALLED BLIND FASTENERS WITH SEALANT PER FAA FSDR W8PA971120Skin · damageLEFT AILERON UPPER SURFACE HAS PAINT DAMAGE. REMOVED LEFT AILERON AND LEFT AILERON TRIM TAB, PERFORMED BALANCE CHECK OF LEFT AILERON IAW SRM 51-60-01. (M)SDR 97ZZZX2944Skin · disbondedAILERON SKIN DISBOND, 3-4 YEARS AFTER BOND REPAIR PERFORMED. SUSPECT CAUSE: BREAKDOWN OF BOND DUE TO REPORTED ENTRANCE OF WATER FROM LEADING AND TRAILING EDGES. BOND FAILURE POSSIBLY DUE TO IMPROPER CLEANING PRIOR TO LAY-UP AND INSTALLATION OF FIBERGLASS RESDR UPS97223970Fitting · corrodedINSPECTION TYPE-C, LT WING O/B AILERON LOCKOUT FITTING IS CORRODED UNDER LOCKOUT GEARBOX MOUNT BOLTS. REMOVED CORROSION AND FOUND OUT OF LIMITS AND REPLACED FITTING IAW SRM 51-30-2, 51-10-6, 27-10-121, 27-10-131.SDR DL72S971043Spar · wornRT O/B AILERON REAR O/B SPAR WORN. INSTALLED REPAIR DOUBLER PER SRM 51-40-03.SDR DL72S971042Skin · loose rivetsRT O/B AILERON SKIN HAD LOOSE RIVETS ON UPPER SKIN. INSTALLED NEW SKIN SECTION REPAIR PER SRM 57-50-5.SDR CALA9700907Bracket · crackedINSPECTION FOUND A .25 INCH CRACK IN LT AILERON NR 4 HINGE BRACKET. THE HINGE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-01 AND MM 27-10-0.SDR AU970579Aileron · worn(AUS) AILERON CONTROL CABLES LOOSE - AILERON BEARINGS WORN - OUTBOARD TORQUE TUBES WORN - TRIM TABS LOOSE - FOUND DURING INSPECTION IAW SB 165ASDR ABXA9701042Aileron · crackedDURING C/P3 CHECK, .5 INCH LONG CRACK WAS FOUND IN LEFT WING AILERON BETWEEN STA'S XW617 AND XW630. *S/D* REPAIRED IAW DC-8 SRM 57-51-00.SDR P2EA97035Aileron · damagedPAE - FOUND C-CHECK MAINTENANCE VISIT, RIGHT AILERON HAS SEVERAL DENTS AND CREASES ON LOWER SURFACE. DURING OPEN UP FOR DAMAGE REMOVAL FOUND DELAMINATION AND WATER CONTAMINATION EXCEEDING REPAIR LIMITS. REPLACED RIGHT AILERON PER MM 27-11-11. (M)SDR P5CA9700788Skin · deterioratedDETERIORATED I/B AILERON LOWER SURFACE PREVIOUS FILLER REPAIR PATCH AREA NEAR I/B AFT CORNER. REPAIRED PER BOEING SRM 51-40-15.SDR P5CA9700787Channel · crackedCRACKED I/B AILERON POWER PACKAGE COMPT I/B VERT WEB ATT SUPPORT CHANNEL. REPLACED V-CHANNEL SUPPORT PER BOEING SRM 51-10-01.SDR P2EA97047Hinge Fitting · brokenPAE - FOUND C-CHECK MAINTENANCE VISIT, LEFT WING AILERON, OUTBOARD HINGE FITTING AT RSS 610 HAS BROKEN FLANGE ON CORNER OF THE FITTING. REMOVED DAMAGED AND REPAIRED IAW EWO 97-0473. (M)SDR 97ZZZM846Bolts · damagedLEFT AILERON RIB 20 'A FRAME' BOLTS SHOW EVIDENCE OF DISPLACED 'FAIL/SAFE' PIN. INSTALLED SERVICEABLE FAIL/SAFE BOLTS LEFT RIB 20 AILERON 'A FRAMES'.
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