N999YV
Service difficulty reports · 30
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 = 'N999YV' AND registry_match = 'registration' 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 = 'N999YV' AND registry_match = 'registration' 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 21GA202605260000Skin · delaminatedDELAMINATION LOCATED ON LEFT SIDE OF VERTICAL STABILIZER PANEL BETWEEN SPAR AND FRONT SPAR FSS 220.521 - 270-784 (MAJOR REPAIR)SDR 21GA2026052623801Seat Track · corrodedCORROSION FOUND ON SEAT TRACK AT STATION 1125 MAIN DECK AT LBL 11 AND RBL 11 (MAJOR REPAIR)SDR 21GA2026052623806Window Frame · crackedWINDOW FRAME AT STATION 944 LH SIDE IS CORRODED AT CENTER OF LOWER EDGE. (MAJOR REPAIR)SDR 21GA2026052623805Frame · crackedCRACK FOUND IN CENTER WING REAR SPAR AT STATION 953 BBL 1RSDR 21GA2026052623803Skin · corrodedCORROSION FOUND ON UPPER SURFACE OF CENTER SECTION AT BS 955.1 AT BL 0 (MAJOR REPAIR)SDR 21GA2026052623802Skin · corrodedCORROSION ON LOWER RH WING AT WS 314.30 - 372.20 STR 16-18SDR 21GA20250724016Power Supply · faultedAT FL 390 BEGAN TO EXPERIENCE DUTCH ROLLS WITH AUTO PILOT AND AUTO THROTTLES ENGAGED.DISCONNECTD AP BUT HAD TO HOLD THE YOKE TO THE RIGHT TO MAINTAIN CONTROL. DELCARED EMERGENCY AND DIVERTED TO ST. LOUIS. MAINTENANCE PERSONNEL REPLACED RIGHT CSEU POWER SUPPLY.SDR 21GA20250324003Valve · faultedDURING CRUSIE RECEIVED FWD EQUIPMENT COOLING OVHT MESSAGE. DIVERTED TO OMAHA. REPLACED RH ENG PRVC.SDR 21GA202503242002Warning Message · false activationDURING CRUISE AT FL 370, RECEIVED EICAS MESSAGE "EQUIPMENT OVERHEAT" MESSAGE. DECENDED TO FL 310. DURING THIS DECENT, RECEIVED "CABIN ALT" MESSAGE. DECLARED EMERGENCY AND DIVERTED. MAINTENANACE PERSONNEL PLACED THE EQUIPMENT COOLING SYSTEM ON MEL AND ACCOMPLISSDR 21GA20241001019Skin · crackedDURING HEAVY CHECK, FOUND CRACKED SKIN CRACKED 1 INCH FWD AND 2.5 INCHES AFT OF IAI PG STRAP. REPAIRED IAW FLIGHT VEHICLES CONSULTING, INC EO #24151-3.SDR 21GA20241001018Skin · dentedDURING HEAVY CHECK, A DENT AND CREASE WERE FOUND AT FUSELAGE SKIN STA 1279.53 BETWEEN STR 33R AND 35R. WAS REPAIRED IAW FLIGHT VEHICLES CONSULTING, INC. EO # 24151-2.SDR 21GA20241001017Skin · dentedDURING HEAVY CHECK, DENTS AND CRACKS WERE FOUND BETWEEN FUSELAGE SKIN STA 347 AND 390 AT STR 19R TO 21R. WAS REPAIRED IAW FLIGT VEHICLES CONSULTING INC. EO# 24151-1.SDR 21GA20230228005Skin · crackedDURING MAINTENANCE FOUND CRACK ON SKIN AT RH FUSELAGE FWD UPPER FASTENER AT STA. 1809 AT STR 12A.SDR 21GA20230218003Skin · corrodedCORROSION FOUND ON HORIZONTAL STABILIZER CENTER SECT. UPPER SKIN AT REAR SPAR BETWEEN BL 0.0 & RBL 10.0.SDR 21GA20230202004Skin · corrodedCORROSION FOUND ON FUSELAGE SKIN SECTION 46 AT STA 1197 BETWEEN STR 39R AND STR 36L.SDR 21GA20230125002Keelbeam · corrodedCORROSION FOUND ON LH KEEL BEAM LOWER CHORD BETWEEN STA 959 & 969.5 BETWEEN STA 1000 & 1017.5 LBL 9.5.SDR 21GA202302150001Skin · corrodedCORROSION FOUND ON FUSELAGE SKIN SECTION 46 BETWEEN STA. 1072.75 & 1109 BETWEEN STR. 36L & 36R.SDR 21GA20221003004Keelbeam · corrodedCORROSION FOUND ON FUSELAGE SECTION 43 KEEL BEAM AROUND F.S. 740 AT LBL 9.5.SDR 21GA20220416001None · noneDURING CRUISE, CABIN ALTITUDE AUTO 2 STATUS MESSAGE. ZERO DUCT PRESSURE FROM ENGINE OR APU BLEEDS. PERFORMED EMERGENCY DECENT DUE TO LOSS OF CABIN PRESSURE. MAINTENANCE PERSONNEL PERFORMED A CABIN PRESSURE CONTROL SYSTEM TEST PER AMM. NO FAULTS NOTED. PERFORMESDR 21GA20191107008Skin · crackedLOWER FUSELAGE SKIN SECTION 43 SKIN CRACKED AT STRINGER 38R AT BS786.SDR 21GA20191107007Skin · corrodedMULTIPLE AREAS OF SCATTERED SURFACE CORROSION ON FASTENER HEADS ON THE UPPER SURFACE OF THE HORIZONTAL STABILIZER RH BETWEEN THE REAR SPAR AND TRAILING EDGE AT STATION 224.SDR 21GA20191107006Skin · corrodedLH WING LOWER SURFACE AT WING STATION 1075 HAS A BLOWOUT (CORROSION) WHERE MARKED AT REAR SPAR.SDR 21GA20191107005Skin · corrodedLH WING LOWER SURFACE AT WING STATION 715 HAS A BLOWOUT (CORROSION) WHERE MARKED AT REAR SPAR.SDR 21GA20191107004Structure · corrodedRH UPPER CENTER TANK SKIN HAS CORROSION AT RBL 71 OF REAR SPAR.SDR 21GA20191107003Skin · crackedRH R1 DOOR CUTOUT AFT LOWER CORNER SKIN CRACKED 4” LONG AT STATION 347 BETWEEN STRINGERS 19 & 20 R.SDR 21GA201702110001Engine · fluctuatesDURING CRUISE AT FLT LEVEL 390 LEFT ENGINE FLUCTUATED ERRATICALLY 400 DEGREES, OTHER PARAMETERS NORMALSDR 2D7A201612300001Battery Pack · dischargedDURING MAINTENANCE CHECK, THE EXIT SIGNS WOULD NOT ILLUMINATE. FOUND THE BATTERY PACK DISCHARGED.SDR 2DYA20151109018Door · wornDURING CRUISE, RECEIVED A E & E BAY DOOR EICAS MSG & DECIDED TO RETURN. NO EMER WAS DECLARED & RETURNED & LANDED SAFELY WITH NO FURTHER INCIDENT. PREVIOUS DMI 999-15-0090 WAS RE-OPENED MEL 52-71-01-01, E & E DOOR MUST BE VERIFIED CLOSED & LATCHED PRIOR TO EASDR 2DYA2015051300004Radio · failedDURING CRUISE JUST PRIOR TO DESCENT, THE CREW NOTICED THE CENTER VHF COMM WENT BLANK & WAS FOLLOWED BY A STRONG ELEC ODOR & SMOKE. COMPLETED NORMAL APPROACH & LANDED WITHOUT INCIDENT. SMOKE & FUMES IN COCKPIT INSPECTION WAS ACCOMPLISHED. AFTER TROUBLESHOOTISDR 2DYA20141030002Unknown · malfunctionedCABIN ALTITUDE CONTINUE TO CLIMB ABOVE 10,000 AT LEVEL FLIGHT 40,000. ACFT RETURNED FOR TROUBLESHOOTING. PERFORMED PRESSURIZATION TEST IAW AMM 21-31-00, TESTED GOOD. ACFT DEPARTED AT A LATER DATE WITHOUT EVENT.
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