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 aircraft_model_key = '340B' 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 aircraft_model_key = '340B' 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 NSVA20120402496Fan · burned outFLIGHT DIVERTED TO ABE DUE TO THE RIGHT RECIRCULATION FAN LIGHT AND LEFT AIR VALVE LIGHT ILLUMINATED DURING FLIGHT FOLLOWED BY THE ODOR OF SMOKE. REMOVED AND REPLACED AVIONICS RECIRCULATION FAN. OPS CHECKED OK, CND THE AIR VALVE.SDR NSVA20120331495Socket · burnedPAX REPORTED ELECTRICAL ODOR FROM ROW 8. REMOVED AND REPLACED ROW 8 SIDEWALL LIGHTING SOCKET ASSY AND BULB. OPS CHECKED GOOD.SDR NSVA20120325488Duct · leakingA/C RETURNED TO AIRPORT DUE TO MX/ LT BLEED AIR LEAK INFLIGHT. THE CREW REPORTED THEY RAN THE QRH WHICH DIRECTED THEM TO ATTEMPT A REST (UP TO TWO RESETS ALLOWED) WHICH WERE BOTH UNSUCCESSFUL AND THE CAUTION LIGHT REMAINED ON. THE CHECKLIST THE ADVISES THE CSDR NSVA20120324492Warning System · false activationDURING INITIAL CLIMB RECEIVED A DEICE CAUTION LIGHT. FLIGHT WAS HEADING INTO ICING CONDITIONS, RETURNED TO IAD. OHMED OUT THE LOWER DUCT AND UPPER DUCT. ALL READINGS GOOD. MX HAS NOT BEEN ABLE TO GET THE INTAKE HEAT TO FAIL SINCE TAKING AIRCRAFT FROM LINE.SDR NSVA20120321486Electronic Unit · defectiveON TAKEOFF ROLL, THE CREW NOTICED THAT THERE WAS A LOSS OF COMMUNICATION / AVIONICS ISSUE BETWEEN THE CAPTAIN AND THE FIRST OFFICER. REPORTED TO THE DISPATCHER THAT THEY DID A LOW ENERGY ABORTED TAKEOFF AND WERE RETURNING TO THE GATE FOR MAINTENANCE PROCEDURESDR NSVA20120318484Wire Harness · defectivePILOT REPORTED WHILE PERFORMING THE CLIMB CHECKLIST NOTICED THAT THE FUEL FLOW INDICATOR WAS READING 0. CREW RAN THE CHECKLIST AND RETURNED BACK TO IAD FOR FURTHER MX. CHANGED THE HARNESS, OPS CK GOOD.SDR NSVA20120317481Web · chafedTOP WEB BETWEEN FRAMES 288 AND 294 CHAFED AT LEFT O/B SIDE FROM AIRSTAIR SLIDING TRACK COVER REF CONTROL #239-73 CA-M6 #138169 SEQ #138.SDR NSVA20120315483Cable · out of rigRETURNED TO FIELD DUE TO TEMPERATURE AND TORQUE FLUX. RIGGED RT ENGINE CABLES. ALL CHECKS GOOD. NO PARTS NEEDED.SDR NSVA20120314476Swivel · crackedAFTER LANDING, WHILE TAXIING TO GATE CREW REPORTED LOSS OF HYD PRESSURE IN OUTBOARD ACCUMULATOR / A/C STOPPED AND REQUESTED TOW TO GATE. REPLACED SWIVEL, SERVICED, BLED & LEAK & OPS CK'D GOOD. AIRCRAFT RELEASED.SDR NSVA20120313475Screw · improper partJUST AFTER DEPARTING IAH, THE CREW REPORTED TO DISPATCH THAT THERE WAS AN AVIONICS ISSUE WITH THE HEADING FLAG. WITH NO PAX ON BOARD, THEY DECIDED THAT A RETURN TO IAH WOULD BE BEST OPTION AND TO PROCEED WITH ANOTHER AIRCRAFT AND CONTINUE THE FLIGHT. FOUND TSDR NSVA20120310469Rib · corrodedREPAIRED CORROSION ON RIGHT WING RIB LOWER FLANGE AT WS 42.3 IAW TD 340-57-12-06.SDR NSVA20120306466Control Head · faultyCREW REPORTED DUAL TRANSPONDER FAILURE INFLIGHT. DISPATCH ACQUIRED ATC APPROVAL TO CONTINUE FLIGHT TO DESTINATION. MAINTENANCE REMOVED AND REPLACED TCAS CONTROL HEAD.SDR NSVA20120302465Sensor · looseA/C HAD A RIGHT ITT FLUX + OR - 40 DEG IN FLIGHT, AIR RETURNED TO IAH. RE-SECURED ITT SENSOR. ALL CHECKS GOOD.SDR NSVA20120303464Warning System · activatedDURING INITIAL CLIMBOUT A/C RECEIVED A RIGHT BLEED AIR LEAK LIGHT. RAN THE QRH, LIGHT WOULD NOT EXTINGUISH, THE QRH DIRECTED THEM TO ENGINE SHUTDOWN. CREW DECLARED AN EMERGENCY. ONCE LANDED TAXIED TO THE GATE UNDER THEIR OWN POWER.SDR NSVA20120306464Warning System · activatedDURING INITIAL CLIMBOUT A/C RECEIVED A RIGHT BLEED AIR LEAK LIGHT. RAN THE QRH, LIGHT WOULD NOT EXTINGUISH, THE QRH DIRECTED THEM TO ENGINE SHUTDOWN. CREW DECLARED AN EMERGENCY. ONCE LANDED TAXIED TO THE GATE UNDER THEIR OWN POWER.SDR NSVA20120229462Transorb · obstructedA/C RETURNED TO GATE DUE TO MX. ENGINE INTAKE LIGHT ILLUMINATED ON TAXI OUT. FOUND SPEED TAPE BYPASSING THE TRANSORBERS. MX REMOVED SPEED TAPE FROM TRANSORBERS CLEANED AND CHECKED POWER RELAYS 48HE AND 46HE. RESET C/B AND OP'S CHECKED INTAKE GOOD.SDR NSVA20120227461Pump · malfunctionedAFTER TAKEOFF CREW SELECTED GEAR TO THE UP POSITION. DURING RETRACTION THE HYD CAUTION LIGHT ILLUMINATED. HYDRAULIC PUMP WOULD NOT TURN ON IN AUTO OR MANUAL. CREW USED ALTERNATE GEAR EXTENSION, DECLARED EMERGENCY AND RETURNED TO AIRPORT. MX REMOVED AND REPSDR NSVA20120223460Seat Track · corrodedLT CENTER AISLE SEAT TRACK PREVIOUS SPLICE REPAIR NOT IN DAMAGE LOG. PREVIOUS REPAIR DETERMINED TO BE CORRODED BEYOND LIMITS REMOVED AND INSTALLED NEW REPAIR IAW TD 340-53-11-59 REF CA-M6 #138166 SEQ #135.SDR NSVA20120221459Hydraulic System · warning lightFLIGHT 4999, HYDRAULIC DOWN LIGHT AND LOSS OF HYDRAULIC PRESSURE. CREW RAN CHECKLIST AND DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY WITHOUT INCIDENT.SDR NSVA20120215451Unknown · vibrationABORTED TAKEOFF DUE TO MX (ON TAKEOFF A/C HAD EXCESSIVE NW SHIMMEY).SDR NSVA20120213450Warning System · activatedDURING TAXI CREW RECEIVED THE LEFT ENGINE INTAKE LIGHT. FLIGHT RETURNED TO GATE FOR MX.SDR NSVA20120208444Unknown · malfunctionedFLIGHT 5006 MLU-IAH ON AIRCRAFT 193CJ HAD LEFT ENGINE OIL TEMPERATURE HIGH WHEN ON DESCENT INTO IAH. FLIGHT LANDED WITHOUT INCIDENT. CREW DID DECLARE EMERGENCY AND SHUT DOWN ENGINE AFTER LANDING.SDR NSVA2011434002Structure · misrepairedPREVIOUS DOUBLER REPAIR TO LT AFT FUSELAGE AT STA 608 NOT INSTALLED IAW PRINCIPALS OF SRM. REPAIRED IAW TD340-53-12-05. CONTROL #343-12.SDR NSVA2011439Skin · dentedNR 2 ICE SHIELD ON THE LT FUSELAGE HAS DENTS UNDER THE ICE SHIELD. DENTS ARE ACCEPTED AS IS IAW SAAB STATEMENT 340-SDS-023546 PARA 4.SDR NSVA2011438Skin · debondedRT HORZ STAB UPPER SKIN DENT NR 41 IS DISBONDED. REPAIRED IAW TD340-55-11-02. CONTROL #343-42.SDR NSVA2011435Skin · dentedLT HORZ STAB UPPER SKIN DENT NR 73 IS DISBONDED. REPAIR IAW TD340-55-11-02. CONTROL #343-41.SDR NSVA2011426Flap · damagedRT FLAP L/E HAS TWO GOUGES NR 1 IS PUNCTURED ALL THE WAY THROUGH, NR 2 IS NOT ALL THE WAY THROUGH BUT IS SOFT AT THE LOWEST POINT OF GOUGE. NR 1 IS APPROX 15.5IN FROM THE INBOARD EDGE AND NR 2 IS APPROX. 20.25 FROM THE INBOARD EDGE. REPAIRED IAW TD 340-27-12SDR NSVA2011430Floor Support · corrodedBOTTOM FRAME WEB AT STA 225 HAS DEEP CORROSION ALONG THE TOP OF THE FLOOR SUPPORT ANGLE FROM LBL 3.5 TO RBL 6 WITH 100 PERCENT DEPTH 2.5 REF CONTROL # 343-24 CA-M6# 313 & CA-M6 #137708 SEQ #381. REPAIRED IAW TD 340-53-12-09 & SAAB STATEMENT SDS-023532 DATED SDR NSVA2011429Structure · damagedCONTROL #343-55 RT FORWARD COWLING FORWARD HORSEWCOLLAR FRONT ATTACH POINT HOLES ELONGATED AND CHAFED. COMPLETED DOUBLER REPAIR IAW TD 340-54-11-37.SDR NSVA2011428Structure · damagedCONTROL #343-48 LT FORWARD COWLING FORWARD HORSECOLLAR FRONT ATTACH POINT HOLES ELONGATED AND CHAFED. COMPLETED DOUBLER REPAIR IAW TD 340-54-11-37.SDR NSVA2011418Repair · crackedCONTROL #343-15: CRACK IN REPAIR PATCH ON RIGHT O/B NACELLE. COMPLETED PERMANENT REPAIR IAW TD 340-54-10-25.SDR NSVA2011420Skin · misrepairedPREVIOUS REPAIR TO LT FUSELAGE AT STA 630.112 TO 640 SL 1524-1526 NOT DONE IAW PRINCIPLES OF SRM OR SAAB STATEMENT 340SDS011466. UPSIZED PERIPHERY STRUCTURE ROWS AND INSTALLED FIELD RIVETS. COMPLETED TD 340-53-11-32 AND JC 51-00-00S.SDR NSVA2011421Structure · misrepairedCONTROL # 343-13: PREVIOUS REPAIR TO LT FUSELAGE AT STA 630.112 TO 640 SL 1524-1526 NOT DONE IAW PRINCIPLES OF SRM OR SAAB STATEMENT 340SDS011466. UPSIZED PERIPHERY STRUCTURE ROWS AND INSTALLED FIELD RIVETS. COMPLETED TD 340-53-11-32 AND JC 51-00-00S.SDR NSVA2011419Structure · corrodedCONTROL #343-30: LT COCKPIT HAS SMALL AREA OF DEEP CORROSION. COMPLETED REPAIR IAW TD 340-53--11-27.SDR NSVA2011414Repair · debondedLT FLAP UPPER SURFACE HAS PREVIOUS REPAIR, LOCATED IN T/E. COMPOSITE HONEY COMB UP TO AFT SPAR APROX STA 222.4 AREA IS 6" WIDE BY 5" IN LENGTH. CENTER OF REPAIR FAILS TAP AND DISBOND TESTS. REFERENCE CA-M6 #137723 SEQ 396 CONTROL #343-34.SDR NSVA2011404Skin · damagedFLIGHT 5011 A/C WAS DAMAGED BY A BAGGAGE CART. CREW REPORTED THAT THE CART HIT THE BACK OF THE AIRCRAFT CLOSE TO THE SKID PLATE. MAINTENANCE HAS BEEN ADVISED AND GOING TO THE AIRCRAFT TO INSPECT. THIS DAMAGE OCCURRED IN IAH AFTER FLIGHT 5011 ARRIVED.SDR NSVA2011402Unknown · noisyDURING EN ROUTE CRUISE A BEEPING NOISE WAS HEARD COMING FROM THE CARGO AREA. THE F/A WENT TO EACH PASSENGER AND ASKED THEM IF THEY HAD ANY DEVICE WITH AN ALARM ON IT IN THEIR CHECKED BAGS. NO ONE ON BOARD CLAIMED TO HAVE ANYTHING. MAINTENANCE CONFIRMED THERSDR NSVA2011400Skin · gougedPERFORMED DOUBLER REPAIR FOR LARGE GOUGE ON THE LT FWD FUSELAGE IAW SAAB STATEMENT (SDS 023412). TD 340-53-12-02 CREATED FOR MAJOR REPAIR DOCUMENTATION. REF CONTROL # 220-40.SDR NSVA20120213397Steering Sys · malfunctionedFLIGHT 5012 IS RETURNING TO GATE DUE TO LOSS OF NOSEWHEEL STEERINGSDR NSVA20110117393Steering Sys · malfunctionedFLIGHT 5012 IS RETURNING TO THE GATE DUE TO LOSS OF NOSE WHEEL STEERING.SDR NSVA20110111001Windshield · crackedAT FL200 85 MILES NORTHEAST OF LFK F/O'S FRONT WINDSHIELD CRACKED. CREW NOTIFIED ATC AND CONTINUED TO IAH. CREW DIDN'T DECLARE AN EMERGENCY AND A/C LANDED WITHOUT FURTHER INCIDENT.SDR NSVA2011391Unknown · malfunctionedAT 11000FT, VOR CREW RECEIVED (RECIRC FAN INOP MSG) AND A/C LOST CABIN PRESSURE TOO. CREW RAN THE CHECKLIST AND DESCEND TO FL080 AND CONTINUED. A/C LANDED WITHOUT FURTHER INCIDENT.SDR SIMA2012010008Mechanism · lack of lubeON FLIGHT 3242 THE CREW REPORTED THE MAIN CABIN DOOR HANDLE HARD TO OPEN AND CLOSE ALSO MADE A NOISE LIKE A SPRING RAPIDLY RELEASING. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBRICATED MAIN DOOR HANDLE LOCKING MECHANISM IAW EMB 145 AMM 52-18-00. SDR NSVA2011389Steering Sys · malfunctionedPILOT CALLED IN REPORTING THAT HE WAS HAVING STEERING ISSUES ON LANDING. STEERING FREED UP ON ITS OWN DURING ATTEMPTED STEERING TO GET ON RUNWAY DUE TO NO TUG FOR ASSISTANCE IN ACT. ONCE OFF THE RUNWAY AND AT GATE PILOTS LOOKED AND NOTED THAT ALL THE TIRES ASDR NSVA2011388Unknown · malfunctioned4986 IAH-DRT A/C LNJ/210 GATE RETURN DUE TO MX (NR 1 ENGINE HUNG START TWICE).SDR NSVA2011385Tail Cone · misrepairedDOUBLER REPAIR TO UPPER LT TAIL CONE SKIN AT STA 793 IS NOT IN DAMAGE LOG OR ON FILE. THE RIVET PATTERN AROUND THE CUTOUT IS IRREGULAR AND DOES NOT HAVE A DOUBLE ROW AT BOTTOM EDGE OF CUTOUT. THE FORWARD EDGE OF THIS REPAIR IS AT THE SKIN SPLICE OF FRAME STASDR NSVA2011383Tail Cone · misrepairedFOUND DOUBLER REPAIR TO RT UPPER TAIL CONE ABOVE AFT HORIZONTAL STAB FAIRING NOT IN DAMAGE LOG OR ON FILE. RIVET SPACING AND CUTOUT DOES NOT CONFORM TO THE PRINCIPLES OF SRM 53-90-10-202. REFER TO SAAB STATEMENT SDS023483 DATED 12-20-11, TD 340-53-11-101 & MSDR NSVA2011382Tail Cone · misrepairedDOUBLER/TRIPLER REPAIR TO RT UPPER TAIL CONE JUST BELOW VERTICAL STAB FAIRING NOT IN DAMAGE LOG OR ON FILE. THIS REPAIR IS MISSING MULTIPLE RIVETS IN THE FIELD. THERE IS A DENT IN THE AFT LOWER AREA OF THE PATCH AT STA 823. THE RIVET PATTERN AROUND THE CUTOSDR NSVA2011381Cargo Track · misrepairedPREVIOUS CARGO SEAT RAIL SPLICE LBL 18 FUSE STA 621 TO 687 NOT IN DAMAGE LOG, U-BEAM SPLICE DOES NOT HAVE SUFFICIENT NAS 1580 BOLT COUNT AND INCORRECT FASTENERS I/B & O/B SEAT RAIL FLANGES. U-BEAM SPLICE IS NOT MINIMUM LENGTH PER TD 340-53-11-59. ACCEPTED ASSDR NSVA2011380Skin · misrepairedFOUND BONDED DOUBLER REPAIR TO UPPER SKIN OF RT HORIZONTAL STAB NOT IN DAMAGE LOG OR ON FILE. THIS REPAIR IS RECTANGULAR IN SHAPE AND NOT RECOGNIZED AS AN APPROVED SRM REPAIR. CONTROL# 202-49 ACCEPTED AS IS PER SAAB STATEMENT 340-SDS-023486, TD# 340-55-11-15
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