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 = '5200' 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 = '5200' 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 ABXA020195Pan · crackedAFT LOWER CARGO DOOR HAD CRACKED INTERIOR DOOR STOP FITTING AT AFT UPPER CORNER. REPLACED AFT LOWER CARGO DOOR ON N.R. #0350 IAW DC-9 MM.SDR VNAA0208018Sensor · failedDURING TAKE OFF, THE CREW RECEIVED A DOOR SWITCH FAIL AND A PROXI SYSTEM FAIL CAS MESSAGE AND ABORTED TAKE OFF. MAINTENANCE INSPECTED AND CLEANED THE PROXI SENSOR AND RERACKED THE PSEU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKSDR 02081204PushrodLeft Center Door EICAS Message/Light appeared in flight. Handle popped up, out of locked position.Adjusted cocking pushrod in accordance with M/M 52-11-00 and 52-11-13. Handle torque test as per M/M 52-11-00 was good.SDR ABXA020186Pan · crackedCRACK IN FORWARD ENTRY DOOR ABOVE FORWARD LOWER STOP PAD. REPLACED DOOR IAW DC-9 MM.SDR VNAA0207026Pseu · failedENROUTE, THE CREW REPORTED AN INTERMITTENT PROXI SYSTEM FAIL CAS MESSAGE ALONG WITH A DOOR SWITCH FAIL CAS MESSAGE. MAINTENANCE INSPECTED AND RERACKED THE PSEU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE SDR VNAA0206019Sensor · failedTHE CREW REPORTED THE EMERGENCY EXIT DOOR SWITCH WAS FAILING INTERMITTENTLY. OUTSTATION MAINTENANCE INSPECTED AND FOUND THE EMERGENCY EXIT DOOR SENSOR TO BE TOUCHING ITS TARGET. OUTSTATION MAINTENANCE ADJUSTED THE SENSOR IN ACCORDANCE WITH DORNIER MAINTENSDR SIMA200216003Structure · gougedABI - PASSENGER DOOR FORWARD LOWER EDGE IS GOUGED. PERFORMED EDDY CURRENT INSPECTION, NO DEFECTS. GOUGE ACCEPTED AS IS IAW EMB GST-1895/02. (M)SDR SIMA200216004Door · dentedDENT IN PASSENGER DOOR ABOVE WINDOW, .006 X 1.0 X 1.1. (SUP) DENT ACCEPTED AS IS IAW MFG GST.SDR SIMA200215902Door · dentedCARGO DOOR NEAR MIDDLE HAS 3 DENTS 1).006 X 1.3 X 1.0 2).009 X 1.3 X 1.8 3) .003 X .3 X .5. (SUP) THREE DENTS FOUND TO BE WITHIN MFG SRM LIMITS.SDR IXXA0200067SDoor · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED UNDER A TEMPORARY REPAIR OF THE FORWARD ENTRANCE DOOR CUT OUT FORWARD UPPER CORNER. REPAIR ACCOMPLISHED, REMOVAL OF THE TEMPORARY REPAIR AND DAMAGED AREA, FABRICATION AND INSTALLATIN OF A REPAIR FILLER, SDR GLBA2002061Seal · tornCABIN DOOR SEAL LEAKING, REPLACED SEAL OPS CHECKED SATISFACTORYSDR VNAA0205002Sensor · failedAFTER DEPARTURE FROM DAY, THE CREW RECEIVED A LEFT HAND EMERGENCY DOOR OPEN INDICATION. FLIGHT 9412 THEN RETURNED TO DAY. MAINTENANCE INSPECTED AND ADJUSTED THE EMERGENCY DOOR PROXIMITY SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATISDR IXXA0200038SDoor · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DISCOVERED ON THE LEFT HAND PASSENGER DOOR CUT OUT LOWER CORNER. REPAIR ACCOMPLISHED DAMAGED AREA CUT OUT, FABRICATION AND INSTALLATION OF FILLER AND REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAISDR DHL2002807540Skin · crackedITEM REF. N/R 2098 M/C DOOR FRAME UPPER INNER SKIN CRACKED 4" @ STA. 200.000CORR. CUT OUT DAMAGED AREA IAW SRM52-2-3 FIG. 10A FABRICATED FILLER & DOUBLER IAW SRM 52-2-3 FIG 10A CLEANED , TREATED, PRIMED IAW SRM 51-1-8B INSTALLED DOUBLER IAW SRM 52-2-3 FIG 10ASDR DHL2002807539Skin · crackedITEM REF. N/R 2099 M/C DOOR FRAME UPPER INNER SKIN CRACKED 2.5" @ STA. 170.000CORR. CUT OUT DAMAGED AREA IAW SRM52-2-3 FIG. 10A FABRICATED FILLER & DOUBLER IAW SRM 52-2-3 FIG 10A CLEANED , TREATED, PRIMED IAW SRM 51-1-8B INSTALLED DOUBLER IAW SRM 52-2-3 FIG 10SDR COOSDR02073Skin · delaminatedMID CARGO COMPARTMENT BARRIER DOOR DELAMINATED.SDR IXXA0200037SDoor · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED UNDER A TEMPORARY REPAIR OF THE FORWARD ENTRANCE DOOR CUTOUT FORWARD UPPER CORNER. REPAIR ACCOMPLSISHED REMOVAL OF THE TEMPORART REPAIR AND DAMAGED AREA. FABRICATED AND INSTALLED REPAIR FILLER AND EXTERSDR HEEA078400Panel · crackedGREENHOUSE WINDOW TRIM PANEL CRACKED. REPLACED WITH SERVICEABLE PANEL.SDR IXXA0200016SDoor · gougedDURING ROUTINE C-CHECK INSPECTION, A GOUGE WAS DETECTED ON THE C-1 DOOR CUTOUT, AFT SECTION BY THE LIGHT SWITCH, STATION 340. BLENDED OUT DAMAGED AREA. FABRICATED AND INSTALLED NEW REPAIR ANGLE IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERINSDR ABXA010686Fitting · crackedAFT LOWER CARGO DOOR #1 BEAM AFT END FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.SDR DHL2002805022Fitting · crackedN/R 1994LT. AFT PAX DOOR UPPER INNER SECTION FITTING CRACKED 1" STA. 1600SDR VNAA0112020Door · failedWHILE IN CRUISE, THE CREW RECEIVED A RED WARNING PANEL DOOR LIGHT. THE SYSTEMS PAGE SHOWED IT WAS THEMAIN CABIN DOOR. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND DIVERTED TO TRI. OUTSTATION MAINTENANCE FOUND NO DEFECTS SO THE AIRCRAFT WAS FERRIED TSDR ABXA010661Fitting · crackedAFT LOWER CARGO DOOR #2 BEAM, AFT END FITTING WAS CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2, 51-30-1, 51-20-0.SDR ABXA010604Former · crackedFORWARD LOWER CARGO DOOR FRAME CRACKED INSIDE FORWARD LOWER LIGHTENING HOLE. REPLACED ANGLE IAW DC-9 SRM.SDR ABXA010544Fitting · crackedMAIN CARGO DOOR FITTING WAS CRACKED IN TWO PLACES, F.S. 313 LONGERON 15 - 16 LEFT. REPAIRED FRAME IAW REA D952-42464-MR.SDR USAA011128Skin · crackedCLT - FOUND SKIN CRACKED, SKIN ON AFT ENTRANCE DOOR L2 AROUND HOLE OPEN HOOK CUTOUT. INSTALLED DOUBLER PER E NR 72317. (M)SDR DHL2001365032FairingOn weekly check discrepance-FWD Lower cargo door cutout lower fairing has cracks and gauges at several places.1) Cut out damaged (cracked) areas and fabricated fillers I.A.W. A-300-SRM 51-40-11.2) O.K. to treat, prime and install repair installed fillers at FWSDR USAA011179Skin · crackedTPA - FOUND SKIN CRACKED 3 INCHES, AFT END OF DOOR HOLD OPEN HOOK OPENING DOOR SKIN. INSTALLED DOUBLER PER SRM 52-05 FIG 20A. (M)SDR GAIA01262STWeb · crackedDURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED E/E COMPARTMENT DOOR, RIGHT WEB HAS TWO CRACKS EMANATING FROM PUNCTURE. ACCOMPLISHED WEB REPAIR BS 420 IAW B727 SRM 51-40-2, FIG 1. (M)SDR GAIA01279STWeb · crackedDURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN AFT CARGO C-3 DOOR LOWER FORWARD WEB AND STRAP IS DENTED AND CRACKED AT STRINGER 26R. ACCOMPLISHED WEB AND STRAP REPAIR IAW B727 SRM 52-30-1, FIG 6 AND 51-40-2 FIG 1. (M)SDR C1HA200183005Seal · looseLoud high pitch sound coming from aft bulkhead above door.Return to DFW.overweight landing made smooth.ACTION TAKEN:Troubleshot in reported area found no structual damage. After visual inspection of sta.1183 bulkhead and crown area sta. 1140 to 1183 pressurizeSDR USAA010951Doubler · crackedPIT - FOUND DOUBLER/ANGLE CRACKED .75 INCH, AFT PSG CABIN DOOR JAMB, LEFT UPPER FRAME. REMOVED DOUBLER, INSTALLED DOUBLER ANGLE PER SRM 53-05 FIG 30A. (M)SDR CHQ00011Switch · out of adjA/C RETURNED TO FIELD. EICAS DOORS WARNING MSG. MAINTENANCE ADJUSTED MICROSWITCH.SDR DL72S011191Seal · tornON CLIMBOUT A LOUD SQUEAL DEVELOPED FROM FORWARD LEFT DOOR. NOISE WAS TOO LOUD TO CONTINUE FLIGHT. DECENDED TO 10,000 FTAND CHANGED CABIN TO 2.0 PSID. NOISE STOPPED. CA RPD L1 DOOR SEAL.SDR USAA010870Skin · crackedTPA - FOUND DOOR EXTERIOR SKIN CRACKED .25 INCH, FORWARD SERVICE DOOR, LOWER HINGE CUTOUT. INSTALLED REPAIR DOUBLER PER SRM 52-10-01 PAGE 201 AND SB 737-52-1096. (M)SDR USAASB01201Seal · failedCLT - FLT 1157 - SHORTLY AFTER TAKEOFF FROM CLT, EN ROUTE TO PBI, THE CABIN DEPRESSURIZED AT ABOUT 4,500 FEET. AIR WAS REPORTEDLY LEAKING FROM THE FORWARD MAIN ENTRY DOOR. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO OXYGEN MASKS SDR GAIA01217STSkin · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED C-3 DOOR SKIN CRACKED AT OUTER HANDLE COVER PLATE BS 1125 BETWEEN STRINGER 23-24 RIGHT, FILGHT STAR AIRCRAFT SERVICES, INC. ACCOMPLISHED NR 3 CARGO DOOR SKIN REPAIR AT BS 1125, STRINGER 23-24R IAW B727 SDR USAASB01193Seal · leakingMSY - FLT 429 - EN ROUTE FROM CLT-MSY, 140 NAUTICAL MILES AWAY FROM MSY AT FL350, THE CREW REPORTED A CABIN PRESSURIZATION LOSS WITH THE CABIN ALTITUDE WARNING HORN SOUNDING. CAPTAIN DESCENDED FLIGHT TO FL130 WHERE THE CABIN STABILIZED AT CABIN ALTITUDE OF 10SDR RRXA11329Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO C-PIT CROSS SLIDE FWD JAMB TRACK GUIDES AT STA. 1160 AND L33L-L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSSDR USAA010921Fitting · crackedPIT - FOUND FITTING CRACKED 4.5 INCHES, MAIN ENTRY DOOR UPPER HINGE FITTING BROKEN AT BASE. REPLACED WITH IDENTICAL PART NR. (M)SDR USAA010761Skin · crackedCLT - FOUND AFT CARGO DOOR SKIN CRACKED .5 INCH, HANDLE CUTOUT, AFT UPPER CORNER. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER SRM 52-30-03. (M)SDR AALA20011231Skin · dentedTUL - FOUND DENTS IN BOTH LOWER CORNERS OF OUTER SKIN. INSTALLED REPAIR DOUBLER PER AARD 52-10-00. (M)SDR AALA20011203DoorTUL - FOUND EXTERIOR SKIN EDGE ON FORWARD GALLEY DOOR BLENDED BEYOND LIMITS BETWEEN UPPER AND LOWER HINGE. INSTALLED DOUBLER PER SRM 52-00-03. (M)SDR RRXA11177Web · dentedDURING A MAINTENANCE VISIT FOUND DENT DAMAGE TO AFT LOWER CORNER WEB AT FORWARD ENTRY DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-SDR AALA20011146Door · crackedTUL - FOUND DOOR SKIN CRACKED, FORWARD EDGE ABOVE LOWER HINGE. ROUTED OUT CRACK, INSTALLED DOUBLER ESO 11697 DATED 5/24/2001. (M)SDR USAA010728Skin · crackedPIT - FOUND SKIN CRACKED .095 INCH, LOWER HINGE CUTOUT. ROUTED OUT CRACK AND INSTALLED DOUBLER PER SRM 52-10-01 S/B 737-52-1096. (M)SDR ASAA0110261HandleANC - DURING MAINTENANCE CHECK, FOUND L1 DOOR DIFFICULT TO OPERATE. CLEANED AND LUBED HANDLE AND HANDLE OPERATED NORMALLY. (M)SDR ASAA0110170Handle · stiffANC - DURING MAINTENANCE CHECK, FOUND L2 DOOR HANDLE STIFF TO OPERATE. CLEANED AND LUBED HANDLE AND HANDLE OPERATED NORMALLY. (M)SDR ASAA0110146Door · stiffANC - DURING MAINTENANCE CHECK, FOUND R2 DOOR DIFFICULT TO OPEN OR CLOSE. LUBED R2 DOOR AND DOOR OPENED NORMALLY. (M)SDR FJT01031261Door Seal · wornBNA - CREW REPORTED DURING CLIMB TO 27,000 FT GOING THROUGH APPROXIMATELY 26,000 FT JUST PRIOR TO CABIN ATTAINING MAXIMUM DIFFERENTIAL A LOUD HOWL WAS HEARD FROM THE CABIN DOOR WHICH TURNED INTO A LOUD WHINING SOUND WHEN AIRCRAFT LEVELED AT 27,000 FT. CREW NO
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