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 = '5240' 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 = '5240' 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 MWEA99829Web · misdrilled holesGALLEY SERVICE DOOR HAS NUMEROUS MISDRILLED HOLES IN WEB. MTC FABRICATED AND INSTALLED NEW WEB.SDR CALA9901519Door · out of rigTHE R-2 EMERGENCY EXIT/GALLEY DOOR WOULD NOT OPEN PROPERLY PAST 90 DEGREES OF FUSELAGE. THE DOOR WAS RIGGED IAW MM 52-41-00 AND OPERATION CHECKED GOOD.SDR GAIA99172Clip · crackedDURING C-CHECK INSPECTION, FOUND A CRACKED CLIP AT THE FORWARD END OF THE NR 1 BEAM ON THE FORWARD GALLEY SERVICE DOOR. THE CLIP WAS REPLACED IAW THE DC-9 SRM THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR EISA99217Door · missingB-SYSTEM SERVICE DOOR MISSING. PER MAINTENANCE THERE IS SHEET METAL DAMAGE, TO AIRFRAME, HINGE IS MISSING AND RIVETS PULLED. REPLACED DOOR ASSEMBLEY, DALFORT COMPLETED STRUCTURAL REPAIR PER 727 SRM 51-30-2. (M)SDR USAA991206Angle · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 20 INCH AREA OF CORROSION AT RT AFT SERVICE DOOR Z-ANGLE (FLOOR), CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. REPLACED Z-ANGLE PER SRM 51-10-02. (M)SDR CALA9901472Skin · gougedINSPECTION FOUND R-1 DOOR SKIN GOUGED JUST ABOVE LOWER HINGE ARM. THE GOUGED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 52-00-01.SDR USAASB99266Seal · out of positionTPA - FLT 2733 - FLT DEPARTURED IAD, EN ROUTE TO FLL, OPERATING WITH MEL 26-12. AIRCRAFT BEGAN OT EXPERIENCED CABIN PRESSURE FLUCTUATIONS. AIRCRAFT HAD BEEN FLYING AT FL240 DUE TO MEL RESTRICTION WHEN THE CABIN ALTITUDE ROSE TO 8,500 FEET AND A PRESSURE DIFFSDR MWEA99761Web · chafedFORWARD GALLEY SERVICE DOOR CLOSE OUT WEB JUST BELOW BAYONET WAS CHAFED. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER.SDR CALA9901449Gate · corrodedINSPECTION FOUND R-1 DOOR LOWER GATE CORRODED AROUND STOPS. THE R-1 DOOR LOWER GATE ASSEMBLY WAS REMOVED AND REPLACED.SDR MWEA99747Pin · crackedSERVICE DOOR HOLD OPEN PIN WAS CRACKED. MTC DRILLED AND INSTALLED NEW PIN.SDR MWEA99746Doubler · crackedACCOMPLISH SERVICE DOOR HOLD OPEN PIN SKIN CUTOUT REWORK. MTC FABRICATED AND INSTALLED DOUBLER.SDR JBXA9900109Mechanism · not latchedON CLIMBOUT OF RDU ON FLIGHT NR 222 TO MEM, CREW RECEIVED A SERVICE DOOR AMBER FAULT. FLIGHT ATTENDANT (AFTER A/C HAD PULLED OFF RUNWAY) RESET SERVICE DOOR HANDLE AND FAULT CLEARED. CREW TURNED BACK ONTO RUNWAY AND TOOK OFF WITH NO FAULTS NOTED.SDR WXOA99029Beam · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND CRACK IN GALLEY SERVICE DOOR HORIZONTAL BEAM AFT EDGE. CRACK REPORTED APPROXIMATELY .240 INCH LONG, EXTENDING FROM FASTENER HOLE. FABRICATED DOUBLER PER DC-9 SRM 52-05 FIGURE 25, SHEET 7 ANDSDR COMA9960624Angle · corrodedTHE THRESHOLD ANGLE AT THE SERVICE DOOR IS SEVERELY CORRODED. PERFORMED A MAJOR REPAIR BY REMOVING THE DAMAGED ANGLE AND INSTALLING A NEW PART 601R38303-105 IAW WVAC EO 601R-53-0415A.SDR USAA991123Skin · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK AT FORWARD SERVICE DOOR LOWER HINGE CUT-OUT UPPER CORNER SKIN. INSTALLED EXTERNAL DOUBLER PER EA 65883. (X)SDR USAA991081Fitting · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK AT FORWARD SERVICE DOOR LOWER AFT DOOR STOP FITTING ASSEMBLY. REPLACED WITH IDENTICAL PART PER SRM 51-10-02. (X)SDR MWEA99682Beam · crackedGALLEY SERVICE DOOR NR 4 BEAM HAD A CRACK ON FORWARD END. ATC FABRICATED AND INSTALLED FITTING AND DOUBLER REPAIR.SDR USAA991105Service Door · corrodedPIT - DURING Q2 CHECK, FOUND CORROSION AT STATION 205 AT AFT SIDE OF SERVICE DOOR 2 INCH BY 3 INCH AT STATION 205 LONG 18 CUSP AREA. CORROSION LEVEL 1, CORROSION TASK NR C46-53301. INSTALLED NEW CUSP MEMBRANE AND SPLICED DOOR PAN PER SRM 53-05 SIG 55 AND EA SDR SWAA991679Skin · crackedDURING SCHEDULED BC2 CHECK, FOUND FWD SERVICE DOOR EXTERNAL SKIN CRACKED ABOVE LOWER HINGE CUT-OUT. REPAIRED SKIN PER SRM.SDR 99ZZZX4171Frame · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON A/C BAY STA 740 DOOR FRAME, LEFT.SDR SWAA991668Frame · crackedDURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR, AFT FRAME CRACKED AT TWO PLACES. REPAIRED FRAME PER SRM.SDR COMA9960629Angle · corrodedSERVICE DOOR FLOOR SUPPORT L ANGLE CORRODED BEYOND LIMITS P/N 601R38303-105. PERFORMED A MAJOR REPAIR, REMOVED AND INSTALLED A NEW THRESHOLD ANGLE (PART NUMBER 601R38303-239) IAW WVAC EO 601R-53-0391A.SDR MWEA99655Doubler · crackedGALLEY SERVICE DOOR NR 1 BEAM, AFT OUTER CORNER HAS A CRACK. MAINTENANCE FABRICATED AND INSTALLED DOUBLER ANGLE.SDR USAA991025Skin · crackedTPA - DURING A CX-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN UPPER AFT CORNER OF TOP HINGE CUT-OUT SERVICE DOOR SKIN. INSTALLED DOUBLER PER TR 52-40-03A FIG 2. (X)SDR USAA990992Skin · crackedTPA - DURING A CX-CHECK VISUAL INSPECTION, FOUND A .250 INCH LONG CRACK AT AFT SERVICE DOOR BOTTOM HINGE AFT CORNER DOOR SKIN. INSTALLED REPAIR DOUBLER PER TR 52-40-03A AND EA 65097. (M)SDR ASAA9980193Mechanism · out of adjustSEA - FLT 446 - AFTER ARRIVAL, CREW REPORTED THE L2 DOOR WOULD NOT OPEN FROM INSIDE. ADJUSTED THE TORQUE TUBE AND ADJUSTED THE L2 DOOR AND OPERATED NORMALLY. (M)SDR MALA976572Latch · out of adjustTHE FORWARD RIGHT EXIT DOESN'T STAY LATCHED OPEN. MAINTENANCE TIGHTENED THE HOLO OPEN LATCH TURNBUCKLE ON RIGHT FORWARD EXIT DOOR IAW AVRO DOOR CMM 52-10-13 PG 721. OPS AND SECURITY CHECKS GOOD.SDR AWXA9900311Skin · crackedC-CHECK, R1 DOOR AFT LOWER CORNER HAS 3 INCH LONG CRACK. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 53-10-01 FIG 202.SDR ABXA9900714Skin · crackedDURING C-CHECK, FOUND SERVICE DOOR EXTERIOR SKIN CRACKED. REPAIRED SERVICE DOOR IAW DC9 SRM 52-01.SDR UPS99830747Skin · damagedINSPECTION TYPE:C1, LT AFT SERVICE DOOR INNER LOWER STRUCTURE HAD A DOUBLE DRILLED HOLE. DOUBLE DRILLED HOLE WENT THROUGH EXISTING REPAIR. REMOVED EXISTING REPAIR DOUBLER AND EXTEND NEW DOUBLER PAST DOUBLE DRILLED HOLES. EXISTING INNER SKIN REPAIR DID NOT MSDR UPS99830668Beam · crackedINSPECTION TYPE:C1, RT AFT DOOR HAS CRACKED FRAME AT UPPER FWD CORNER. OPENED INNER WEB AND REMOVED CRACKED DOOR BEAM. FABRICATED NEW DOOR BEAM (P/N 5772639-21) IAW DC8 SRM 51-1-21, INSTALLED IAW DC8 SRM 51-1-2 0D, 51-1-21 AND REINSTALLED INNER WEB IAW DC8 SSDR USAA990877Skin · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AFT SERVICE DOOR FORWARD EDGE 30 INCH BELOW TOP SKIN. INSTALLED DOUBLER PER SRM 52-10-01. (M)SDR UPS99830583Skin · crackedINSPECTION TYPE:C3 5 CRACK IN FUSELAGE SKIN STA 190 AT FWD SERVICE DOOR CUTOUT LWR CORNER. ROUTED OUT DAMAGED SECTION OF SKIN AND FABRICATED AND INSTALLED DOUBLER IAW REO-06671.SDR SWAA991391Mechanism · not lockedAIR TURNBACK, AFT SERVICE DOOR LIGHT ILLUMINATED DURING CLIMB (DOOR HANDLE WOULD NOT LOCK DOWN). ADJUSTED AND TESTED AFT SERVICE DOOR PER MM.SDR SWAA991347Gusset · crackedDURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT LOWER STUB FRAME GUSSET CRACKED. REMOVED AND REPLACED STUB FRAME GUSSET PER SRM.SDR UPS99830408Web · crackedINSPECTION TYPE:C123, THE RT FWD SERVICE DOOR FRAME FWD WEB WAS CRACKED. REMOVED, FABRICATED AND REPLACED THE WEB IAW DWG 5615700 AND SRM 51-1-21.SDR USAA990827Skin · crackedTPA - DURING CX-2 CHECK EDDY CURRENT INSPECTION, FOUND A .125 INCH CRACK LOWER HINGE CUTOUT FORWARD SERVICE DOOR SKIN. REMOVED CRACK AND INSTALLED DOUBLER PER SB 737-52-1096 AND SRM 51-10-01. (M)SDR ASAA9980168Handle · roughPDX - FLT 419 - AFTER ARRIVAL, CREW REPORTED THE L2 DOOR WOULD NOT OPEN. FOUND EXTERIOR HANDLE CATCHING ON DOOR STRUCTURE. REMOVED BURR FROM HANDLE AND SMOOTHED AREA AND OPERATED NORMALLY. (X)SDR USAA990680Angle · corrodedCLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION AFT RT Z-ANGLE AT AFT SERV DOOR. CORROSION LEVEL 2. REPLACED PER SRM 51-10-02. (M)SDR UPS99830305Skin · gougedINSPECTION TYPE:C123, INNER SKIN GOUGED ON RT FWD SERVICE DOOR, AT AFT UPPER CORNER, ADJACENT TO LIGHTENING HOLE. FABRICATED AND INSTALLED DOUBLER, ATTACH ANGLE AND TWO FILLERS IAW DC8 SRM 52-2-3, 52-3-1 FIG 1, 51-9-0 AND 51-3-0.SDR UPS99830477Frame · crackedINSPECTION TYPE:C3 1 EA HOLE DRILLED THROUGH RT FWD SERVICE DOOR INNER SKIN IN CLOSE PROXIMITY TO ADJACENT RIVET LOCATED AT LOWER AFT CORNER OF DOOR. 51-9-0 INSTALLED FASTENERS IN PREVIOUS DOUBLER ON SKIN IAW DC8 SRM 5 1-1-2, SRM 51-1-20D. INSTALLED SEAL RETSDR UPS99830452Pan · damagedINSPECTION TYPE:C3, 1 HOLE IN AFT SIDE OF RT FWD SERVICE DOOR PAN AT APPROX LONG 14R DOT S815. FABRICATED AND INSTALLED DOUBLER, FILLER AND SEAL RETAINER IAW DC8 SRM 52-2-0, 51-1-9 & 51-3-0.SDR QXEA9901501Bushing · seizedPDX - SERVICE/EMERGENCY DOOR LATCH BUSHINGS FORWARD, LOWER AND BOTH AFT ARE NOT FREE WHEN DOOR CLOSED AND LATCHED. REPAIRED IAW FOKKER MM 52-40-1, PAGE 502, PARAGRAPH 3AC17.SDR USAASA99003Mechanism · not latchedSNA/PIT - FLT 148 - AFTER TAKEOFF, THE 2L CABIN DOOR WAS LEAKING AND DOOR ARMED INDICATOR WAS FLASHING. THE AIRCRAFT DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND 2L DOOR NOT PROPERLY CLOSED. THE DOOR WARNING SYSTEM AND THE OPERATION OF 2L SDR USAA990720Latch · crackedPIT - LGA MAINTENANCE FOUND .50 INCH CRACK AT SERVICE DOOR (RT SIDE) HOLD OPEN CUP. REPLACED WITH LIKE PART PER EA 52418A. (X)SDR JBXA9900088Service Panel · not closedOUT OF RDU, FLIGHT 930, HAD LOUD NOISE COMING FROM AIRCRAFT. RETURNED TO RDU. FOUND FRONT SERVICE PANEL LEFT OPEN. MAINTENANCE INSPECTED AND CLOSED SERVICE PANEL IAW AMM 52-20-00. AIRCRAFT RETURNED TO SERVICE.SDR SWAA991109Frame · crackedDURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED AT LOWER AFT STOP FITTING. REMOVED AND REPLACED DOOR FRAME PER SRM AND BOEING DRAWING.SDR USAA990626Skin · crackedTPA - DURING CX-3 VISUAL INSPECTION, FOUND TWO CRACKS, ONE CRACK .125 INCH AND ONE CRACK .25 INCH LOWER HINGE CUTOUT AT FORWARD SERVICE DOOR SKIN. INSTALLED FILLER, DOUBLER AND FASTENERS PER TR 52-10-01A. (M)SDR 99ZZZX2707Hinge · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON LOWER AFT LAVATORY SERVICE PANEL HINGE.SDR DHL9970220CFrame · crackedC CHECK, RIGHT SERVICE DOOR, THE DOOR FRAME HAS .5 INCH CRACK AREA OF FORWARD NR 2 STOP FROM THE BOTTOM. REMOVED RT SERVICE DOOR IAW B727 MM 52-40-0. INSTALLED RT SERVICE DOOR IAW B727 M/M 52-12-0. ADJUSTED RT SERV DOOR PER B727 M/M 52-12-0. LEAK OK IAW B7
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