N227AZ
Service difficulty reports · 40
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 = 'N227AZ' 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 = 'N227AZ' 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 IXXA202604275038Controller · failedAT FL350, MASTER WARNING, AURAL ALARM, AND CABIN ALTITUDE. CABIN ALTITUDE 10, 000, CABIN ALTITUDE ON AUTO 2 WAS NOT RESPONDING IN MANAUL OR AUTO 1. CREW INITIATED DIVERSION. CREW DECLARED. LANDED WITHOUT INCIDENT. POST FLIGHT WALK AROUND WAS NORMAL. AIRCRAFT WSDR IXXA2026041801Web · damagedPUNCTURE DAMAGE ON THE WEB FRONT SPAR LOCATED ON THE RIGHT WING SLAT #12SDR IXXA20260416003Seal · damagedRIGHT HORIZONTAL BLADE SEAL PANEL 345AFB, REQUIRES COMPOSITE REPAIR.SDR IXXA20260416002Stop · gougedNR 1 PYLON OTBD SIDE JUST AFT OF THE UPPER AFT THRUST REVERSER STOP IS GOUGED.SDR IXXA20260416001Thrust Reverser · damagedNR 1 OTBD THRUST REVERSER UPPER AFT CORNER IS DAMAGED. OPENSDR IXXA20260415001Skin · crackedFUSELAGE SKIN AND BEAR STRAP IS CRACKED AT L1 DOOR CUTOUT AFT LOWER CORNER STA 335SDR IXXA20260410001Strap · crackedWHILE PREFORMING INSP AT STA. 1725.5 OF BULKHEAD OUTER CHORD STRAP FOUND CRACK AT STRINGER 6R INTERNAL FWD OF APU INTAKE DOORSDR IXXA2026040902Drain Line · dentedL/W SURGE TANK DRAIN LINE IS DENTED AND GOUGED.SDR IXXA2026040901Drain Line · dentedLEFT WING SURGE TANK DRAIN LINE IS DENTED AND GOUGED.SDR IXXA20260406001Angle · crackedFOUND ANGLE CRACKED AT STA 1746.125 NEAR STRINGER 10RSDR IXX2026F00002Bezel · crackedVIEWPORT WINDOW PRIZM ASSEMBLY L4 P/N 141T6665-11 CRACKEDSDR IXXA20260401002Channel · crackedNR 2 PYLON AFT FAIRING AFT MOST WEB OUTBOARD VERTICAL J CHANNEL IS CRACKED AT HI-LOC FASTENERSDR IXXA20260401001Channel · crackedNR 2 PYLON AFT FAIRING AFT MOST WEB INBOARD VERTICAL J CHANNEL IS CRACKED AT HI-LOC FASTENERSDR IXXA202604130001Cover · wornUPPER INBD FASTENER HAS WORN THROUGH THE AFT SIDE OF THE THROTTLE STRUT CONTROL BOX ON TOP OF #1 PYLON.SDR IXXA04132026CC02Cover · wornUPPER INBD FASTENER HAS WORN THROUGH THE AFT SIDE OF THE THROTTLE STRUT CONTROL BOX ON TOP OF #1 PYLON.SDR IXXA202604130002Cover · wornUPPER INBD FASTENER HAS WORN THROUGH THE AFT SIDE OF THE THROTTLE STRUT CONTROL BOX ON TOP OF #1 PYLON.SDR IXXA20260130001Skin · delaminatedPERFORM PERMANENT HOT-BOND REPAIRS UNDER VACUUM ON THE THREE DAMAGED AREAS OF THE RIGHT-WING OUTBOARD TRAILING EDGE FLAP LOWER SURFACESDR IXX2026F00003Bezel · crackedVIEWPORT WINDOW PRIZM ASSEMBLY R1 P/N 141T6665-1 CRACKEDSDR IXXA20240726001Skin · crackedR1 DOOR CUTOUT, AFT LOWER CORNER, ROTO SCAN SHOWS INDICATION AT SECOND HOLE FROM BOTTOMSDR IXXA2024070201Support · corrodedL1 DOOR SCUFF PLATE SUPPORT CORRODED.SDR IXXA20230123777A/C Pack · odorAFTER TAKEOFF, FIRST OFFICER AND CAPTAIN SUSPECTED SMELL OF OIL. SMELL WAS ONLY SLIGHTLY EVIDENT AS ALT INCREASED TO FL380. STRONGER SMELL BY 15,000 THROUGH 10,000. ODOR WAS MOST EVIDENT AT 4,000. FLIGHT CONTINUED UNAFFECTED WITH NO VISUAL OR AURAL INDICATIOSDR IXXA20230123333Door · false indicationMAIN CARGO DOOR LIGHT IN FLIGHT AT FL 19. ABNORMAL CABIN RATE CHANGE BETWEEN FL18.0 AND FL20.0, ALTERNATIVELY, NO LOSS OF CABIN PRESSURIZATION. FAULT NOT CREW DEFERRABLE. AIR TURN BACK TO DEPARTURE STATION WITH EMERGENCY DECLARATION. LANDING WAS UNEVENTFUL WITSDR IXXA20230121004Diffuser · damagedDURING START OF NR 2 ENGINE, N2 STOPPED AT 16% FOLLOWED BY A RIGHT ENGINE STARTER EICAS MESSAGE. SECONDS LATER APU SHUTDOWN. AIRCRAFT RETURNED TO BLOCKS. LINE MAINTENANCE INITIATED DEFERRAL MAINTENANCE ITEM-38063 MEL CAT C. AIRCRAFT RELEASED TO SERVICE. WHILESDR IXXA20220827001None · chafed#1 ENG RH CORE COWL LWR, FWD EDGE HAS DEEP CHAFE WEAR. -009 REF VT-SAA NR B000147SDR IXXA2022090403None · bentRAT COMPARTMENT IB INNER CHORD (PANEL LANDING) BENT AND DISTORTED REF ST-VAA NR B000501SDR IXXA2022090303None · gougedMAIN DECK CARGO DOOR SILL #2 LATCH PIN FITTING GOUGED (059-07) REF VT-SAA NR B000231SDR IXXA20220903002Floor Panel · crackedUPON REMOVAL OF FLOOR PANEL IN COCKPIT STA 246 AREA, FOUND FLOOR PANEL DAMAGED (141T5931-61)SDR IXXA20220802802Channel · elongatedAFTER REMOVAL OF DAMAGED STRIFFENER ON #2 AFT STRUT AT APPROX NAC 400,THE AFT WEB HORIZONTAL CHANNEL WAS FOUND WITH ELONGATED FASTENER HOLES. REF VT-SAA RN B000427 ATI-54-822-00-02SDR IXXA2022090304None · missingFWD CARGO COMPT ROLLER TRAY SPLICE STRAP MISSING AT RL 20.5 JUST FWD OF PDU 13R.018-101SDR IXXA20220802803Flap Track · gougedRIGHT WING INBOARD AFT FLAP OUTBOARD FLAP TRACK GOUGED. REF VT-SAA RN B000195 ATI-57-850-00-02SDR IXXA2022090405None · elongated#2 ENG/PYLON PANEL 446CL HAS 2 EA ELONGATED FASTENER HOLESSDR IXXA2022090402None · damagedTAIL COMPARTMENT RIGHT SIDE EWIS SUPPORT BRACKET UNDER CENTER STAB BOX AT STA 1798 DAMAGED REF ST-VAA RN B000205SDR IXXA2022090401None · gouged#1 ENG. I/B CORE COWL #2 RIB FROM AFT HAS GOUGE. 00-114 REF VT-SAA NR B000315SDR IXXA2022090404Stiffener · worn#2 ENG INBD PYLON ACCESS PANEL AFT LANDING 434AL WORNSDR IXXA20220903001None · chafed#2 ENG UPPER PYLON LANDIN FOR FAIRING 441AT HAS AREAS OF CHAFFING. 18-027SDR IXXA20220802801Channel · cracked#2 AFT STRUT OUTBD J CHANNEL CRACKED AT 2 PLACES AT APPROX NAC 400.18-003 REF VT-SAA RN B000365 ATI-54-822-00-02SDR IXXA2022090305None · crackedMEC ACCESS DOOR FWD EDGE IS DAMAGED IN 3 AREAS 49-012 REF VT-SAA NR B000056SDR IXXA20220804001Flap · crackedDENT ON LH IND FLAP 59.5 FROM INBD EDGE AND 44.5 FORM TRAILING EDGE. VT-SAA NR B000038SDR IXXA2022082602Stiffener · elongated#2 AFT STRUT INTERIOR AT APPROX NAC 400 OUTBD STIFFENER HAS BOLTS WORN THROUGH.SDR IXXA20210522036Relief Valve · malfunctionedCABIN AUTO INOPERATIVE EICAS MESSAGE. CABIN ALT AUTO 1 AND 2 STATUS MESSAGE. AT FL 400, CABIN ALTITUDE WARNING, LOST CABIN PRESSURE. CREW COMPLIED WITH QRH, DROPPED TO 10,000 FL AND ELECTED MANUAL CABIN ALT CONTROL. DIVERSION TO KILN, ATC EMERGENCY DECLARATION
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