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 n_number = 'N555NN' 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 n_number = 'N555NN' 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 VNAA2025112811102Selector Valve · faultedGEAR DISAGREE WARNING W/ LOSS OF STEERING ON LANDING. /REMOVED AND REPLACED MLG SELECTOR VALVE ASSEMBLY IAW AMM 32-10-000/400-801-A01. BLED HYD SYSTEM 3 IAW AM 29-10-00-870-802-A01.SDR VNAA2024090311101Light · burned outFLIGHT ATTENDANT REPORTED ELECTRICAL FUMES IN BACK OF AIRCRAFT. ON GND WAITING AT GATE APU BLEEDS ONLY / TROUBLESHOT PER FIM 21-22-00-810-806. FOUND AFT LAV VANITY LIGHT LED BURNT OUT. REMOVED AND REPLACED AFT LAV VANITY LIGHT LED IAW CRJ 900 AMM 33-25-03-000/SDR VNAA202310100009Skin · dentedDENTS BTW FS 1162.00 TO FS 1181.00 AND BTW STGR 25LH TO STGR 25RH. REPAIRED PER EA 23-C9-53-1365 REV.IR SECTION III - PERMANENT REPAIR.SDR VNAA202310100002Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 597AB) AT LH WING LOWER SKIN. REPAIRED PER EA 23-C9-57-1243 REV IR, EA 23-C9-57-1276 REV.A, EA 23-C9-57-1277 REV.IR, EA23-C9-57-1278 REV.IR SECTION III-PERMANENT REPAIR.SDR VNAA202310080003Bushing · corrodedCORROSION ON BUSHINGS SETTLEMENT AREA (8 LOCATIONS) HINGE 1,2, 3, 4 (INBD AND OUTBD) WAS FOUND. CORROSION ON BUSHINGS SETTLEMENT AREA (8 LOCATIONS) HINGE 1,2, 3, 4 (INBD AND OUTBD) WERE REPAIRED PER REO 690-57-51-299 REV. --SDR VNAA202310090005Intercostal · corrodedINTERCOSTAL DD3 WAS REPLACED AND ANGLE-TO-SKIN OF INTERCOSTAL BTW FORMER FS 320.163 AND FWD SUPPORT ANGLE OF PASSENGER DOOR INTERNAL STRUCTURE (INSIDE ACCESS PANEL 832DL) WAS CLEANED AND RE-INSPECT AND CORROSION WAS NOT FOUND PER CRJ-900 SRM 51-42-06-001-001-ASDR VNAA2023100910006Intercostal · wornWEAR ON INTERCOSTAL 3 RH BTW FS 364.00 TO FS 379.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE. INTERCOSTAL 3 RH BTW FS 364.00 TO FS 379.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE WAS REPLACED PER EA 23-C9-53-1282 REV. IRSDR VNAA202310080004Hinge · corrodedORROSION ON BUSHINGS (7 EA) OF AILERON HINGE 1 (OUTBD), HINGE 2,3, 4 (INBD AND OUTBD) AT LH WING REAR SPAR. AILERON HINGE 1 (OUTBD), HINGE 2,3, 4 (INBD AND OUTBD) AT LH WING REAR SPAR WERE REPAIRED PER REO 690-57-51-298 REV. - & EA 23-C9-57-1242 REV. ASDR VNAA202310080002Bushing · corrodedAFTER BUSHINGS REMOVAL OF AILERON HINGE LH IN REF NRC 00125, CORROSION ON BUSHINGS SETTLEMENT AREA (7 LOCATIONS) HINGE 1 (OUTBD), HINGE 2, 3, 4 (INBD AND OUTBD) WAS FOUND. SETTLEMENT AREA (8 LOCATIONS) HINGE 1,2, 3, 4 (INBD AND OUTBD) WERE REPAIRED PER REO 69SDR VNAA202310100005Support Plate · corrodedCORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/RH MAIN WHEEL WELL. REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED OUT LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/RSDR VNAA202310100007Strut · corrodedAFTER REMOVAL OF LEFT MLG PISTON AXLE, CORROSION ON SHOCK STRUT THREADS. SHOCK STRUT LH SIDE WAS REPAIRED PER REO 690-32-11-163 REV. - -SDR VNAA202310100006Landing · corrodedCORROSION AT SETTLEMENT AREA OF ACCESS PANEL 195AB. REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUATED OUT LIMITS PER CRJ-900 SRM 53-83-55-101-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01SDR VNAA202310090010Hinge Fitting · bentBENT AFT HINGE ON FWD BAGGAGE BAY DOOR STRUCTURE. DUE NOT ALLOWABLE DAMAGE AT AFT HINGE ON FWD BAGGAGE BAY DOOR STRUCTURE WAS REPLACED PER CRJ-900 SRM 53-31-23-101-001-A02 AND SRM 51-41-02-001-001-A01SDR VNAA202310100010Angle · crackedAFTER ACCESS PANEL REMOVAL WITH NRC 00030, CRACK AT FWD SUPPORT ANGLES (2EA) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARTMENT INTERNAL STRUCTURE (ACCESS PANEL 121AL). FWD SUPPORT ANGLES (2EA) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARTMENT INTERNAL STRUCSDR VNAA202310100008Bracket · crackedDURING DVI SERVICE DOOR STABILIZATION BRACKET ASSY STEP 4. BRACKET ASSEMBLY WAS FOUND CRACKED. BRACKET ASSY SERVICE DOOR P/N:CC670-38380-1 WAS REPLACED PER CRJ900 AMM 52-41-27SDR VNAA2023100910004Floorbeam · crackedCRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1596 REV.--SDR VNAA202310100003Fitting · wornPERM REPAIR - JACKING PAD HELICOIL INSERT, RHS CW PERM REPAIR PER REO INSTRUCTIONS. JACK FITTING PAD RH WING WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01SDR VNAA202310080010Seat Track · corrodedCORROSION ON SEAT RAILS OF RBL9 AND LBL9 BTW FS847.00 TO FS977.00. DUE NOT DAMAGE ALLOWED ON SEAT RAILS OF RBL9 AND LBL9 BTW FS847.00 TO FS977.00 (2E/A) WRE REPLACED PER CRJ-900 SRM 53-51-49-101-001-A02 AND CRJ/900 AMM 53-00-49 CONFIG. (A12)SDR VNAA202310080001Skin · dentedSEVERAL DENTS ON FUSELAGE SKIN, SETTLEMENT AREA OF LEFT AND RIGTH VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%. DENTS ON FUSELAGE SKIN, SETTLEMENT AREA OF LEFT AND RIGTH VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZESDR VNA2023F00006Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01SDR VNAA202310080009Seat Track · corrodedCORROSION ON SEAT RAIL RBL 9 BTW F.S.581.00 TO F.S.661.00. SEAT RAIL RBL 9 BTW F.S.581.00 TO F.S.661.00 WAS EVALUATED PER CRJ-900 SRM 53-31-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)SDR VNAA202310080008Seat Track · corrodedCORROSION ON SEAT RAIL RBL 9 BTW F.S.349.00 TO F.S. 485.00. SEAT RAIL RBL 9 BTW F.S.349.00 TO F.S. 485.00 WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02; CRJ900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)SDR VNAA202310080007Seat Track · corrodedCORROSION ON SEAT RAIL LBL 9 BTW FS 379. SEAT RAIL LBL 9 BTW FS379 WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ900 AMM 53-00-49SDR VNAA202310080006Bracket · corrodedCORROSION ON BRACKET MACHINED (6EA) AT INTERNAL STRUCTURE FWD BAGGAGE BAY CARGO BELOW FLOOR BETWEEN STGR 23RH/23LH AND FS501.00 TO FS661.00+32.00. BRACKET MACHINED (6EA) AT INTERNAL STRUCTURE FWD BAGGAGE BAY CARGO BELOW FLOOR BETWEEN STGR 23RH/23LH AND FS501SDR VNAA202310080005Hinge Fitting · excess playAFTER RUDDER REMOVAL, FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. RUDDER HINGE FITTINGS NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR, WERE REPLACED PER RIL #2103 REV. BSDR VNA2023F00007Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01SDR VNAA202310100004Striker · wornPAX DOOR SEAL STRIKER WITHIN 1,374.07 FH (BEFORE 20,312.15 FH) . REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND EA 23-C9-53-0145 REV.IRSDR VNAA202310100001Skin · wornWEAR ON FIXED LEADING EDGE (522AL, 522BL) AT LH WING. REPAIRED PER EA 23-C9-57-1196 REV.IR SECTION III PERMANENT REPAIR.SDR VNAA202310090014Skin · wornWEAR ON FIXED LEADING EDGE (631AR) AT RH WING. WEAR ON FIXED LEADING EDGE (631AR) AT RH WING WAS REPAIRED PER EA 23-C9-57-1191 REV.IR SECTION III PERMANENT REPAIRSDR VNAA202310090013Skin · nickedSEVERAL NICKS AND DENTS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5. SEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 WERE REMOVED PER CRJ900 SRM 51-12-00-001-001-A01; WERE EVALUATED WITHIN LIMITS BTW FLS 45 TO FLS 65 AND WERE ESDR VNAA202310090012Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB, 686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN. REPAIRED PER EA 23-C9-57-1258 REV IR, EA 23-C9-57-1259 REV IR, EA 23-C9-57-1260 REV IR, EA 23-C9-57-1261 REV IR, EA 23-C9-57-1262 REV IR.SDR VNAA202310090011Access Panel · corrodedCORROSION ON PASSENGER DOOR ACCES PANEL 832EL. CORROSION ON ACCESS PANEL 832EL WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01; WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 52-11-32-101-001-A01; AND WAS VERIFIED PER CRJ900 AIPC 52-11-32-20SDR VNAA202209081112None · noneGEAR DISAGREE RED WARNING AFTER GEAR SELECTED UP AFTER TAKE OFF. RAN QRF, RTF. DECLARED EMERGENCY. UPON INSPECTION OF PX22 FOUND UPPER DRAG BRACE BRACKET FOR PX22 AND PX21 LOOSE AND WIGGLING FROM SIDE TO SIDE AND UP AND DOWN. INSTALLED NEW WASHERS ON DRAG BRACSDR VNAA202110051111Seal · stickingDURING SCHEDULED INSPECTIONS, MX WAS UNABLE TO OPEN THE LH FWD EMERGENCY EXIT DOOR (FROM THE INSIDE SEAT 15A). LH FWD EMERGENCY DOOR REQUIRES DVI AND LEAK CHECK DUE TO SEALANT FOUND AROUND FLAPPER DOOR. / REMOVED AND REPLACED EMERGENCY DOOR FLAP SEAL IAW CRJ 9SDR VNAA202107051114Door · damagedOPERATOR HAS REPORTED DAMAGE TO RHS FWD NOSE LANDING GEAR DOOR & RHS ADG FUSELAGE SKIN PANEL (DWG. CC670-33109, REF) BETWEEN FS169 AND FS193. / WITNESSED CONSTANT AVIATION PERFORM REMOVAL AND REPLACEMENT OF THE RH FORWARD AIR DRIVEN GENERATOR SKIN PANEL (P/N: SDR VNAA202106041112Skin · damagedDURING OVERNIGHT MAINTENANCE AT CHARLOTTE NC, (CLT), MX REPORTS BURN MARK DAMAGE TO THE RH ELEVATOR P/N AV670-24100-040 SN MH570. THE DAMAGE DIMENSIONS ARE AS FOLLOWS .75"L X .5"W X .25"D AND IS LOCATED AT THE TRAILING EDGE BETWEEN RIBS 19 AND 20. THE ELEVATORSDR VNAA2020073011101Bleed Valve · failedL ENG DEGRADED, L ENG SURGE OPEN CAUTION, L ENG ITT EXCEEDED. CREW SENT ACARS TO DISPATCHER STATING THEY WERE RETURNING TO FIELD, DUE TO MX. CREW DID DECLARE AN EMERGENCY. CREW STATES THEY RECEIVED L ENGINE DEGRADED MESSAGE AND L ENGINE SURGE OPEN CAUTION SDR VNAA2020021751102Sign · crackedSERVICE DOOR EXIT SIGN CRACKED. R/R SERVICE DOOR EXIT SIGN LENSSDR VNAA2020021511101Housing · failedINTERIOR EMERGENCY LIGHT TO THE LEFT OF PAX DOOR (UPPER) ON THE FWD WARDROBE WONT ILLUMINATE. MX R+R EMERGENCY EXIT SIGN LIGHT ASSY DS156 IAW CRJ-900 AMM 33-51-05-000/400-801, CRJ-900 WM 33-23-04, AND CRJ-900 ESPM 20-26-11. OPS CHECK GOOD. NO DEFECTS NOTED.SDR VNAA201911299907Intercostal · corrodedPAX DOOR INTERCOSTALS BETWEEN FS 323 TO FS 335 3 INTER COSTALS CORRODED FROM THE TOP OF DOOR MARKED WITH TAPE. REMOVED INTERCOSTALS PAX DOOR FS 323 TO FS 335 3EA IAW CRJ 700 SRM 51-42-06-001-001-A01. INSTALLED 3EA NEW PAX DOOR MID INTERCOSTALS BETWEEN FS 323 FSDR VNAA2019062651103Actuator · failedDURING AN OCF FLIGHT FOR A FLAPS FAIL MESSAGE CREW RECEIVED THE SAME MESSAGE. THEY DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. R&R RH INBD FLAP ACTUATOR, OPS CHECK GOOD.SDR VNAA201906221103Flap System · malfunctionedFLAP FAIL IN FLIGHT. PERFORMED OPS CHECK FOR FLAP AND SLAT SYST IAW AMM. OPS CHECK GOODSDR VNAA201906221101Flap System · malfunctionedDURING THE APPROACH , THE CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE FLAPS WERE INDICATING 8 DEGREES. WHEN THE CREW TRIED TO PUT THE FLAPS DOWN TO 20 DEGREES THE FLAPS WOULD NOT GO DOWN. CREW RAN THE QRH AND DECLARED AN EMERGENCY. LANDED, CHECKED TIRES ASDR VNAA2016091700019Unknown · smokeCREW REPORTED SMOKE IN THE CABIN AT AROUND 11000 FEET. DECLARED AN EMERGENCY, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPS CHECK OF ALL SYSTEMS, OPS CHECKED GOOD. FOUND NO EVIDENCE OF BURNT WIRES OR COMPONENTS. THE AISDR VNAA2016020100002Controller · failedCREW REPORTED LT WIDOW HEAT CAUTION MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R LT WINDOW TEMPERATURE CONTROLLER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.SDR VNAA2015072800037Warning Light · illuminatedCREW REPORTED CENTER CARGO DOOR AMBER CAUTION MESSAGE DURING INITIAL CLIMB. RETURNED TO FIELD DUE TO NOT BEING ABLE TO PRESSURIZE CABIN AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPS CHECK OF CENTER CARGO DOOR INDICATING SYS AND OPS CHECK OF CABIN PR
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