N431AZ
Service difficulty reports · 65
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 = 'N431AZ' 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 = 'N431AZ' 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 IXXA2026100501Skin · corrodedSECTION 46, R2 DOOR AFT LOWER CORNER SKIN CUT-OUT WITH CORROSION BETWEEN STA 1540 AND STA 1526 AND BETWEEN STR-19R AND STR-20RSDR IXXA20260917082Transmitter · out of adjustFRM 27-51-03-00 EICAS MESSAGE TE FLAP ASYM DISPLAYED. TRAILING EDGE LIGHT ON. NO FLAP MOVEMENT. MESSAGE APPEARED WHEN FLAPS WENT TO 30. ON GO AROUND NO FLAP MOVEMENT. PERFORMED BITE OF FSEU IAW B767 AMM 27-51-45 FOUND LEGS 1-4 PINGING "FLAP POS XMTR 1". PERFORSDR IXXA20260206010Battery · inoperativeDURING SERVICE CHECK FOUND PEDESTAL EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-02. OPERATIONAL CHECK GOOD.SDR IXXA202601060002Guard · stickingEMERGENCY LIGHT GUARD/SPRING STICKS DISARMING LIGHTS. CYCLED SWITCH MULTIPLE TIMES, FOUND NO DEFECTS. SWITCH GUARD SEATS NORMALLY. OPERATIONAL CHECK IN ACCORDANCE WITH B767 AMM 33-51-00 NOTED NO FAULTS.SDR IXXA202512097082Fire Warning · false activationMAIN CARGO FIRE WARNING DURING CLIMBOUT FOR ONE SECOND. IAW FAULT ISOLATION MANUAL 26-10 FAULT TREE 803 AND AUTOMATIC FIRE OVERHEAT LOGIC TEST SYSTEM NO FAULTS NOTED. OPS CHECKED GOOD IAW AMM 26-10-00.SDR IXXA20251119001Support Channel · corrodedLEFT WING LOWER PANEL CHANNEL SUPPORT CORRODED AROUND MULTIPLE NUTPLATES AT WBL 97.5 STA 955 TO STA 999 (REFERENCE STREAMER TAG (22582) (SWISHER)SDR IXXA2025F00025Fire Warning · activatedRED FORWARD CARGO FIRE WARNING DURING CLIMB. CREW RETURNED TO DEPARTING STATION AND DECLARED EMERGENCY. AIRCRAFT ARRIVIED WITHOUT INCIDENT AND NO FURTHER PRCAUTIONARY ACTION WAS TAKEN. AIRCRAFT WAS GROUNDED FOR INSPECTION AND MAINTENANCE.SDR IXXA20251010063Battery · inoperativeFLIGHT DECK PEDESTAL FLASHLIGHT BATTERY INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IN ACCORDANCE WITH B767 AIRCRAFT MAINTENANCE MANUAL 25-64-02. OPERATIONAL CHECK GOOD.SDR IXXA20251004060Door · off trackWHILE PERSONNEL WAS ATTEMPTING TO CLOSE L1 DOOR, DOOR CAME OFF TRACKS AND WEDGED IN PLACE. PARTIALLY CLOSED. UPON FURTHER INSPECTION FOUND MOVABLE CEILING PANEL WEDGED INTO L1 DOOR. DISLODGED PANEL AND DOOR OPERATED NORMALLY. GENERAL VISUAL INSPECTION OF TRACSDR IXX2025F00008Skin · delaminatedL/H O/B T/E DELAMINATION OF FLAPSDR IXXA20250408001Skin · delaminatedL/H I/B T/E DELAMINATION OF FLAP.SDR IXXA20241031072Battery · no testFOLLOWING SERVICE CHECK, LINE MAINTENANCE REPORTED CENTER PEDESTAL EMERGENCY FLASHLIGHT INOPERATIVE. CENTER PEDESTAL EMERGENCY FLASHLIGHT BATTERY REMOVED AND REPLACED PER B767 AMM 25-64-02. OPERATIONAL CHECK GOOD.SDR IXXA20240529036Sliding Window · bindingFOLLOWING SCHEDULED MAINTENANCE AND INSPECTIONS LINE MAINTENANCE REPORTED, L2 WINDOW WOULD NOT CLOSE. AIRCRAFT GROUNDED FOR CORRECTIVE ACTIONS. AT KILN. L2 WINDOW MECHANISM REMOVED AND REPLACED PER BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 56-11-04. OPERATIOSDR IXXA2024022601Seat Track · crackedFIRST OFFICERS FWD O/B SEAT TRACK CRACKED AT FORWARD STOP HOLE.SDR IXXA2024022401Bracket · corrodedCORRODED BRACKETSDR IXXA2024022304Roller Tray · corrodedROLLER TRAY CORRODEDSDR IXXA2024022303Roller Tray · corrodedROLLER TRAY CORRODED.SDR IXXA2024022302Roller Tray · corrodedROLLER TRAY CORRODEDSDR IXXA2024022301Roller Tray · corrodedCORROSION ON ROLLER TRAY.SDR IXXA2024022202Skin · corrodedLEFT WING IB FLAP HAS CORROSION ON UPPER SURFACE.SDR IXXA2024022201Seat Track · crackedCAPTAINS FORWARD INBOARD SEAT TRACK CRACKED.SDR IXXA2024022104Bracket · corrodedALC CEILING PANEL SUPPORT BRACKET HAS CORROSION STA 1310 ABOVE ALC DOORSDR IXXA2024022103Support · corrodedCORROSION IN AFT LOWER CARGO FRAME SUPPORT STA 1417 RBL 43SDR IXXA2024022102Door · corrodedLMLG STRUT DOOR AFT CORNER ATTACH BRACKET CORRODEDSDR IXXA2024022101Precooler · cracked# 1 ENGINE CORE COWL PRE-COOLER EXHAUST DUCT MATING FLANGE CHAFED AND CRACKEDSDR IXX2024021600000Skin · cracked#1 PYLON UNDER TR HAS CRACKED SKIN.SDR IXX20240216000001Skin · cracked#1 PYLON UNDER TR HAS CRACKED SKIN.SDR IXXA2024021400001Door · corrodedRH APU DOOR CORRODED AT FWD CORNERSDR IXXA2024020803Skin · crackedIB CORE COWL CRACKED AT AFT LATCHSDR IXXA2024020802Skin · crackedIB CORE COWL SKIN CRACKEDSDR IXXA2024020801Skin · crackedAPU ACCESS DOOR SKIN CRACKEDSDR IXXA20231204087Unknown · unknownDURING PRE-FLIGHT INSPECTIONS AND MAINTENANCE LINE TECH REPORTED AFT FLIGHTDECK EMERGENCY FLASHLIGHT INOPERATIVE. LED NOT FLASHING AND NO ILLUMINATION WHEN REMOVED FROM BRACKET. AFT FLIGHTDECK EMERGENCY FLASHLIGHT BATTERY REMOVED AND REPLACED IAW B767 AIRCRAFSDR IXXA20231120081Unknown · unknownFORWARD EMERGENCY FLASHLIGHT INOPERATIVE. EMERGENCY FLASHLIGHT BATTERY REMOVED AND REPLACED PER B767 AMM 25-64-02. OPERATIONAL CHECK GOOD.SDR IXXA20230911057Unknown · unknownDURING CLIMB THRU 27,000 LEFT ENGINE SURGE. EGT HIT 937. CREW COMPLIED WITH QRH PROCEDURES LEVELED AT 28,000 AND SURGING ABATED. AUDIBLE POPS DURING CLIMB AND DESCENT. AROUND 17,000 FT AIRFRAME VIBRATIONS WERE NOTED. BOTH CLIMB AND DESCENT IN THE 60% N2 BAND.SDR IXXA20220529115Generator · inoperativeON CLIMB OUT, RIGHT GENERATOR DRIVE INOPERATIVE. APU CURRENTLY DEFERRED. FLIGHT CANNOT CONTINUE WITH SINGLE ELECTRICAL SOURCE. AIRTURN BACK TO DEPARTURE STATION KLAX WITH EMERGENCY DECLARATION. LANDING UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARSDR IXXA20220515111O-Ring · failedENROUTE FROM KSFO TO KAFW AT CRUISE OIL PRESSURE WAS IN AMBER RANGE AT 29 PSI. OIL PRESSURE THEN DROPPED REACHING RED RANGE AT 10 PSI AT 20000 FEET. CREW SHUT DOWN RIGHT ENGINE IN FLIGHT. AIR TURN BACK TO KSFO WITH EMERGENCY DECLARATION. LANDING WAS UNEVENTFULSDR IXXA202205120101Fitting · corrodedBS 954 RBL 99-113 WL 171-148, SIDE FITTING PN 145T2523-8 HAS NUMEROUS AREAS OF LIGHT CORROSION CIT THE LWR FORWARD MATTING SURFACE (FORK)_ NOTE: CLOSEST AREA OF CORROSION TO A FASTENER IS .20" FOR ITEM 1 ONLY. STA 954 RBL 99 WL 142 SIDE FITTING PN 145T2523-SDR IXXA2022051103Web · corrodedITEM 1
STA 955 RBL 90 WL 165
CORROSION EXISTS CIT THE AFT SIDE SURFACE OF 111T1003-5 REAR SPAR WEB
CORROSION IS 2.4'LX 1.2"W AND 0.055" D
QA NOTES PREVIOUS BLENDING EXISTS CIT R/S WEB MEASURING
2.8' L X 1.4' WAND 0.055" D NEAR THE CORROSION
ITEM2
STA 95SDR IXXA202205110101Skin · corrodedSTA955 RBL96 WL 149
THERE ARE QTY (2) AREAS OF CORROSION CIT THE IML OF THE 145T3421-4 SKIN.
MEASUREMENTS:
1 A) 2.5"L X 1.3"W
1 B) 1.8"L X .50'W REF BOEING REPAIR AGREEMENT TIN-RE-2201692 FRR-13SDR IXXA2022051104Splice Plate · crackedSTA 915-984, RBL 98, WL 182
Q1Y (6) COUNTERSUNK HOLES FOR YLR/16N HAVE NOTICEABLE DAMAGE ON THE INSIDE SURFACE OF THE
HOLES CIT 145T8840-18 LONGERON.
HOLES SHOULD BE CLEAN AND ROUND .496" - .500"
ITEM2
STA 958, RBL 98, WL 182
COUNTERSUNK HOLE FOR FASTENESDR IXXA2022051003Doubler · crackedSTA 975 RBL 96 WL 182
QTY (2) 0.186 ELONGATED HOLES EXISTS COMMON TO 145T8754-25 DOUBLER, FWD OTBD FASTENERS ONLY
ELONGATIONS, EDGE MARGINS AND MEASURMENTS ARE AS FOLLOWS:
1A) ELONGATION MEASURES 0.2395", E/M 0.35", DISTANCE TO NEAREST HOLE 0.55"
1B)) ELONSDR IXXA2022051002Intercostal · cracked145T2700--32 INTERCOSTAL FWD INBOARD HAS QTY(1) 0.186" HOLE CT 145T2703-8 AND 145T2700-30 IS ELONGATED AND CRACKED. ELONGATION MEASURES 0.236". VISIUAL CRACK IS C/T EDGE OF THE HOLE AND EXTENDS OUTWARDS FROM THE HOLE EDGE 0.0415". CRACK MEASURES 0.0415" X 0.15SDR IXXA20220506104Fairing · corrodedWING TO BODY RH AFT LWR OF WW DOOR CUT OUT IB SIDE HAS CORROSION. FAS WO N431AZ-01-01 NON ROUTINE 00124SDR IXXA2022050902Nut Plate · corrodedFWD CARGO DOOR LOWER CUTOUT APPROX STA 504 R/H SIDE BALLMAT SUPPORT ANGLE CORRODEDSDR IXXA2022041809Doubler · corrodedKEEL BEAM STA 1005 AROUND HYD GROUND SERVICE DOUBLER CORRODED. FAS WO N431AZ-01-01 NR 00133SDR IXXA2022050602Panel · corrodedRH WING FIXED LE AT WS 920 APROX LWR SUPPORT PANEL CORRODED. FAS WO N431AZ-01-01 NON ROUTINE 00353SDR IXXA2022050401Rib · crackedCRACK INDICATION ON RH REAR SPAR LOWER CHORD AT RIB POST 10. ONE CRACK INDICATION ON THE OUTBOARD SIDE OF RIB 10 AFT/OUTBOARD FASTENER TRAVELING APPROX 1/4" LONG. FAS WO N431AZ-01-01 NON ROUTINE 00327SDR IXXA2022051102Rib · crackedCRACK INDICATION NOTED ON RH REAR SPAR LOWER CHORD AT RIB POST 10. ONE CRACK INDICATION ON THE OUTBOARD SIDE OF RIB 10 AFT/OUTBOARD FASTENER TRAVELING FWD APPROX 1/4" LONG. REF FAS WO N431AZ-01-01 NON ROUTINE 00327SDR IXXA20220509201Angle · crackedRH WING LE STA 522 ANGLE CRACKED. FAS WO N431AZ-01-01 NON ROUTINE 00280SDR IXXA2022042404Skin · corrodedLH WING UPPER SURFACE HAS SEVERAL AREAS (AS MARKED) WITH EVIDENCE OF CORROSION. INBD T/E AT REAR SPAR W.S. 197 REF FAS WO N431AZ-01-01 NON ROUTINE 00293
Back to N431AZ