# Service difficulty reports: N227AZ A list on [N227AZ](https://openairdocs.org/aircraft/N227AZ.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR IXXA202604275038](https://openairdocs.org/sdr/IXXA202604275038.md): Controller · failed · Apr 25, 2026 · N227AZ · Boeing 767323 · Cabin Pressure Controller > AT 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 W - [SDR IXXA2026041801](https://openairdocs.org/sdr/IXXA2026041801.md): Web · damaged · Apr 18, 2026 · N227AZ · Boeing 767323 · Wing Miscellaneous Structure > PUNCTURE DAMAGE ON THE WEB FRONT SPAR LOCATED ON THE RIGHT WING SLAT #12 - [SDR IXXA20260416003](https://openairdocs.org/sdr/IXXA20260416003.md): Seal · damaged · Apr 16, 2026 · N227AZ · Boeing 767323 · Horizontal Stabilizer Miscellaneous Structure > RIGHT HORIZONTAL BLADE SEAL PANEL 345AFB, REQUIRES COMPOSITE REPAIR. - [SDR IXXA20260416002](https://openairdocs.org/sdr/IXXA20260416002.md): Stop · gouged · Apr 16, 2026 · N227AZ · Boeing 767323 · Engine Thrust Reverser > NR 1 PYLON OTBD SIDE JUST AFT OF THE UPPER AFT THRUST REVERSER STOP IS GOUGED. - [SDR IXXA20260416001](https://openairdocs.org/sdr/IXXA20260416001.md): Thrust Reverser · damaged · Apr 16, 2026 · N227AZ · Boeing 767323 · Engine Thrust Reverser > NR 1 OTBD THRUST REVERSER UPPER AFT CORNER IS DAMAGED. OPEN - [SDR IXXA20260415001](https://openairdocs.org/sdr/IXXA20260415001.md): Skin · cracked · Apr 15, 2026 · N227AZ · Boeing 767323 · Fuselage Main, Plate/Skin > FUSELAGE SKIN AND BEAR STRAP IS CRACKED AT L1 DOOR CUTOUT AFT LOWER CORNER STA 335 - [SDR IXXA20260410001](https://openairdocs.org/sdr/IXXA20260410001.md): Strap · cracked · Apr 10, 2026 · N227AZ · Boeing 767323 · Fuselage Miscellaneous Structure > WHILE PREFORMING INSP AT STA. 1725.5 OF BULKHEAD OUTER CHORD STRAP FOUND CRACK AT STRINGER 6R INTERNAL FWD OF APU INTAKE DOOR - [SDR IXXA2026040902](https://openairdocs.org/sdr/IXXA2026040902.md): Drain Line · dented · Apr 9, 2026 · N227AZ · Boeing 767323 · Wing Miscellaneous Structure > L/W SURGE TANK DRAIN LINE IS DENTED AND GOUGED. - [SDR IXXA2026040901](https://openairdocs.org/sdr/IXXA2026040901.md): Drain Line · dented · Apr 9, 2026 · N227AZ · Boeing 767323 · Wing Structure > LEFT WING SURGE TANK DRAIN LINE IS DENTED AND GOUGED. - [SDR IXXA20260406001](https://openairdocs.org/sdr/IXXA20260406001.md): Angle · cracked · Apr 6, 2026 · N227AZ · Boeing 767323 · Horizontal Stabilizer Miscellaneous Structure > FOUND ANGLE CRACKED AT STA 1746.125 NEAR STRINGER 10R - [SDR IXX2026F00002](https://openairdocs.org/sdr/IXX2026F00002.md): Bezel · cracked · Apr 1, 2026 · N227AZ · Boeing 767323 · Door Windows > VIEWPORT WINDOW PRIZM ASSEMBLY L4 P/N 141T6665-11 CRACKED - [SDR IXXA20260401002](https://openairdocs.org/sdr/IXXA20260401002.md): Channel · cracked · Apr 1, 2026 · N227AZ · Boeing 767323 · Nacelle/Pylon Miscellaneous Structure > NR 2 PYLON AFT FAIRING AFT MOST WEB OUTBOARD VERTICAL J CHANNEL IS CRACKED AT HI-LOC FASTENER - [SDR IXXA20260401001](https://openairdocs.org/sdr/IXXA20260401001.md): Channel · cracked · Apr 1, 2026 · N227AZ · Boeing 767323 · Nacelle/Pylon Miscellaneous Structure > NR 2 PYLON AFT FAIRING AFT MOST WEB INBOARD VERTICAL J CHANNEL IS CRACKED AT HI-LOC FASTENER - [SDR IXXA202604130001](https://openairdocs.org/sdr/IXXA202604130001.md): Cover · worn · Mar 3, 2026 · N227AZ · Boeing 767323 · Nacelle/Pylon Miscellaneous Structure > UPPER INBD FASTENER HAS WORN THROUGH THE AFT SIDE OF THE THROTTLE STRUT CONTROL BOX ON TOP OF #1 PYLON. - [SDR IXXA04132026CC02](https://openairdocs.org/sdr/IXXA04132026CC02.md): Cover · worn · Mar 3, 2026 · N227AZ · Boeing 767323 · Nacelle/Pylon Miscellaneous Structure > UPPER INBD FASTENER HAS WORN THROUGH THE AFT SIDE OF THE THROTTLE STRUT CONTROL BOX ON TOP OF #1 PYLON. - [SDR IXXA202604130002](https://openairdocs.org/sdr/IXXA202604130002.md): Cover · worn · Mar 3, 2026 · N227AZ · Boeing 767323 · Nacelle/Pylon Miscellaneous Structure > UPPER INBD FASTENER HAS WORN THROUGH THE AFT SIDE OF THE THROTTLE STRUT CONTROL BOX ON TOP OF #1 PYLON. - [SDR IXXA20260130001](https://openairdocs.org/sdr/IXXA20260130001.md): Skin · delaminated · Jan 30, 2026 · N227AZ · Boeing 767323 · Trailing Edge Flaps > PERFORM PERMANENT HOT-BOND REPAIRS UNDER VACUUM ON THE THREE DAMAGED AREAS OF THE RIGHT-WING OUTBOARD TRAILING EDGE FLAP LOWER SURFACE - [SDR IXX2026F00003](https://openairdocs.org/sdr/IXX2026F00003.md): Bezel · cracked · Jan 4, 2026 · N227AZ · Boeing 767323 · Door Windows > VIEWPORT WINDOW PRIZM ASSEMBLY R1 P/N 141T6665-1 CRACKED - [SDR IXXA20240726001](https://openairdocs.org/sdr/IXXA20240726001.md): Skin · cracked · Jul 26, 2024 · N227AZ · Boeing 767323 · Fuselage Main, Plate/Skin > R1 DOOR CUTOUT, AFT LOWER CORNER, ROTO SCAN SHOWS INDICATION AT SECOND HOLE FROM BOTTOM - [SDR IXXA2024070201](https://openairdocs.org/sdr/IXXA2024070201.md): Support · corroded · Jul 2, 2024 · N227AZ · Boeing 767323 · Fuselage Miscellaneous Structure > L1 DOOR SCUFF PLATE SUPPORT CORRODED. - [SDR IXXA20230123777](https://openairdocs.org/sdr/IXXA20230123777.md): A/C Pack · odor · Jan 23, 2023 · N227AZ · Boeing 767323 · Air Distribution System > AFTER 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 INDICATIO - [SDR IXXA20230123333](https://openairdocs.org/sdr/IXXA20230123333.md): Door · false indication · Jan 19, 2023 · N227AZ · Boeing 767332 · Door Warning System > MAIN 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 WIT - [SDR IXXA20230121004](https://openairdocs.org/sdr/IXXA20230121004.md): Diffuser · damaged · Jan 17, 2023 · N227AZ · Boeing 767323 · APU Core Engine > DURING 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. WHILE - [SDR IXXA20220827001](https://openairdocs.org/sdr/IXXA20220827001.md): None · chafed · Aug 27, 2022 · N227AZ · Boeing 767323 · Engine Cowling System > #1 ENG RH CORE COWL LWR, FWD EDGE HAS DEEP CHAFE WEAR. -009 REF VT-SAA NR B000147 - [SDR IXXA2022090403](https://openairdocs.org/sdr/IXXA2022090403.md): None · bent · Aug 22, 2022 · N227AZ · Boeing 767323 · Fuselage Structure (General) > RAT COMPARTMENT IB INNER CHORD (PANEL LANDING) BENT AND DISTORTED REF ST-VAA NR B000501 - [SDR IXXA2022090303](https://openairdocs.org/sdr/IXXA2022090303.md): None · gouged · Aug 9, 2022 · N227AZ · Boeing 767323 · Cargo/Baggage Doors > MAIN DECK CARGO DOOR SILL #2 LATCH PIN FITTING GOUGED (059-07) REF VT-SAA NR B000231 - [SDR IXXA20220903002](https://openairdocs.org/sdr/IXXA20220903002.md): Floor Panel · cracked · Aug 3, 2022 · N227AZ · Boeing 767323 · Fuselage Floor Panel > UPON REMOVAL OF FLOOR PANEL IN COCKPIT STA 246 AREA, FOUND FLOOR PANEL DAMAGED (141T5931-61) - [SDR IXXA20220802802](https://openairdocs.org/sdr/IXXA20220802802.md): Channel · elongated · Jul 30, 2022 · N227AZ · Boeing 767323 · Nacelle/Pylon, Frame/Spar/Rib > AFTER 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-54-822-00-02 - [SDR IXXA2022090304](https://openairdocs.org/sdr/IXXA2022090304.md): None · missing · Jul 29, 2022 · N227AZ · Boeing 767323 · Fuselage, Seat/Cargo Attach Fittings > FWD CARGO COMPT ROLLER TRAY SPLICE STRAP MISSING AT RL 20.5 JUST FWD OF PDU 13R.018-101 - [SDR IXXA20220802803](https://openairdocs.org/sdr/IXXA20220802803.md): Flap Track · gouged · Jul 29, 2022 · N227AZ · Boeing 767323 · Trailing Edge Flap Control System > RIGHT WING INBOARD AFT FLAP OUTBOARD FLAP TRACK GOUGED. REF VT-SAA RN B000195 ATI-57-850-00-02 - [SDR IXXA2022090405](https://openairdocs.org/sdr/IXXA2022090405.md): None · elongated · Jul 28, 2022 · N227AZ · Boeing 767323 · Nacelle/Pylon Structure > #2 ENG/PYLON PANEL 446CL HAS 2 EA ELONGATED FASTENER HOLES - [SDR IXXA2022090402](https://openairdocs.org/sdr/IXXA2022090402.md): None · damaged · Jul 27, 2022 · N227AZ · Boeing 767323 · Fuselage Structure (General) > TAIL COMPARTMENT RIGHT SIDE EWIS SUPPORT BRACKET UNDER CENTER STAB BOX AT STA 1798 DAMAGED REF ST-VAA RN B000205 - [SDR IXXA2022090401](https://openairdocs.org/sdr/IXXA2022090401.md): None · gouged · Jul 27, 2022 · N227AZ · Boeing 767323 · Nacelle/Pylon Structure > #1 ENG. I/B CORE COWL #2 RIB FROM AFT HAS GOUGE. 00-114 REF VT-SAA NR B000315 - [SDR IXXA2022090404](https://openairdocs.org/sdr/IXXA2022090404.md): Stiffener · worn · Jul 26, 2022 · N227AZ · Boeing 767323 · Nacelle/Pylon Structure > #2 ENG INBD PYLON ACCESS PANEL AFT LANDING 434AL WORN - [SDR IXXA20220903001](https://openairdocs.org/sdr/IXXA20220903001.md): None · chafed · Jul 25, 2022 · N227AZ · Boeing 767323 · Nacelle/Pylon Structure > #2 ENG UPPER PYLON LANDIN FOR FAIRING 441AT HAS AREAS OF CHAFFING. 18-027 - [SDR IXXA20220802801](https://openairdocs.org/sdr/IXXA20220802801.md): Channel · cracked · Jul 25, 2022 · N227AZ · Boeing 767323 · Nacelle/Pylon Structure > #2 AFT STRUT OUTBD J CHANNEL CRACKED AT 2 PLACES AT APPROX NAC 400.18-003 REF VT-SAA RN B000365 ATI-54-822-00-02 - [SDR IXXA2022090305](https://openairdocs.org/sdr/IXXA2022090305.md): None · cracked · Jul 22, 2022 · N227AZ · Boeing 767323 · Doors > MEC ACCESS DOOR FWD EDGE IS DAMAGED IN 3 AREAS 49-012 REF VT-SAA NR B000056 - [SDR IXXA20220804001](https://openairdocs.org/sdr/IXXA20220804001.md): Flap · cracked · Jul 19, 2022 · N227AZ · Boeing 767323 · Trailing Edge Flaps > DENT ON LH IND FLAP 59.5 FROM INBD EDGE AND 44.5 FORM TRAILING EDGE. VT-SAA NR B000038 - [SDR IXXA2022082602](https://openairdocs.org/sdr/IXXA2022082602.md): Stiffener · elongated · Jul 7, 2022 · N227AZ · Boeing 767323 · Nacelle/Pylon Structure > #2 AFT STRUT INTERIOR AT APPROX NAC 400 OUTBD STIFFENER HAS BOLTS WORN THROUGH. - [SDR IXXA20210522036](https://openairdocs.org/sdr/IXXA20210522036.md): Relief Valve · malfunctioned · May 18, 2021 · N227AZ · Boeing 767323 · Cabin Pressure Control System > CABIN 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 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/aircraft/N227AZ/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.