N331AZ
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 = 'N331AZ' 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 = 'N331AZ' 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 IXXA2022112710Fitting · corrodedRH HORIZONTAL STABILIZER AFT #7 FITTING CORRODED. REF FAS WO FS220060 NON ROUTINE 00456SDR IXXA2022112709Fitting · corrodedRH HORIZONTAL STABILIZER FWD #6 FITTING CORRODED. REF FAS WO FS220060 NON ROUTINE 00455SDR IXXA2022112708Fitting · corrodedRH HORIZONTAL STABILIZER FWD #4 FITTING CORRODED. REF FAS WO FS220060 NON ROUTINE 00454SDR IXXA2022112706Fitting · corrodedRH HORIZONTAL STABILIZER FWD #3 FITTING CORRODED. REF FAS WO FS220060 NON ROUTINE 00453SDR IXXA2022112705Fitting · corrodedRH HORIZONTAL STABILIZER FWD #2 FITTING CORRODED. REF FAS WO FS220060 NON ROUTINE 00452SDR IXXA2022112703Beam · corrodedCORROSION AREA ON BEAM PN 113T1911-40 BETWEEN WS841.20 & WS811.20 APPROX IN LENGTH 30".SDR IXXA2022112402Frame · crackedMAIN FRAME STA 903.5 RBL 89 INNER CHORD IS CRACKED. REF FAS WO FS220060 NON-ROUTINE 00115SDR IXXA2022112301Skin · corrodedRH HORIZ STAB UPPER SURFACE HAS AREA OF BARE METAL AND SURFACE CORROSION BETWEEN FRONT AND REAR SPARS JUST OB OF STAB TO BODY FAIRING. REF FAS WO FS220060 NON ROUTINE 00219SDR IXXA2022112001Frame Angle · crackedMAIN FRAME STA 903 LBL89 INNER CHORD IS CRACKED. FASWO FS220060 NON-ROUTINE 00116SDR IXXA20220712122Window · inoperativePRIOR TO DEPARTURE, FIRST OFFICER'S R2 WINDOW DIFFICULT TO OPEN. UNLOCK HANDLE DOES NOT SEAT IN THE OPEN POSITION. SECURED ROLL PIN IN LOCK HANDLE AND SAFETIED PIN. OPERATIONAL CHECK SATISFACTORY IAW B767 AMM 56-11-00. NO ADDITIONAL FAULTS NOTED.SDR IXXA20210303012Smoke Detector · false activationENROUTE MAIN CARGO DECK A-2 SMOKE DETECTION AMBER LIGHT ON CENTER CONSOLE WITH NO INDICATION OF SMOKE, MASTER CAUTION OR EICAS INDICATIONS. CREW DECLARED EMERGENCY AND DIVERTED TO KMSP. UPON LANDING NO THERMAL HOT SPOTS DETECTED BY FIRE CREW. MAIN DECK CARGO FSDR IXXA20210207301Skin · delaminatedVERTICAL STABILIZER LEFT SIDE SKIN PANEL WAS DELAMINATED BEYOND SRM LIMITS. REMOVED AND REPLACED CORE AND INNER SKIN AND REPAIRED PER AMES ENGINEERING DOCUMENT 47447REA02 REV IR AND APPROVED BY DERT-710167-SW ON 8110-3 DATED 1-19-21.SDR IXXA20210207300Failsafe · crackedPERFORMED A CRACK TRIM OUT OF THE RIGHT SIDE FAIL STRAP PER AMES ENGINEERING DOCUMENT 472070RD04.RIGHT SIDE STA 955 REFERENCING BOEING SERVICE BULLETIN 767-53A0100 AND BOEING SERVICE BULLETIN 767-53-0116.SDR IXXA20201001038Skin · crackedMAINTENANCE, DURING ROUTINE OPERATIONS AT CVG, DISCOVERED ON 331AZ A CRACK IN THE SECTION 46 FUSELAGE SKIN AT THE FORWARD JAMB OF THE RIGHT AFT LOWER CARGO DOOR, PN 146T3510, AT STA 1270, NEAR DOOR STOP NUMBER 10. THE SKIN IS MADE FROM 2024-T3 X 0.210 CLAD ALSDR IXXA20180109347Speaker · smokeVISUAL SMOKE EMITTING FROM CAPTAIN'S SPEAKER ON POWER TRANSFER TO GROUND POWER UNIT. DURING A DETAILED VISUAL INSPECTION OF CAPTAIN'S SIDE CONSOLE, DETERMINED THE SOURCE OF THE ODOR AND SMOKE COMING FROM CAPTAIN'S SPEAKER IAW AMM 20-60-01. REMOVED AND REPL
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