N26632, cancelled Nov 15, 2025
Service difficulty reports · 17
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 = 'N26632' AND deregistration_id = 'N26632-2025-11-15' 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 = 'N26632' AND deregistration_id = 'N26632-2025-11-15' 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 HYIA20201124002Axle · crackedTHE PILOT REPORTED THAT AFTER LANDING, THE AXLE BROKE WHILE EXITING THE RUNWAY. MAINTENANCE INSPECTED AND FOUND THE RIGHT AXLE TO BE CRACKED. REMOVED AND REPLACED THE RIGHT LOWER BARREL AND AXLE ASSEMBLY. NO FURTHER DEFECTS NOTED.SDR HYIA20190716001Fitting · crackedDURING MAINTENANCE A CRACK WAS IDENTIFIED ON THE OUTBOARD LEG OF THE LEFT HAND OUTBOARD NACELLE FITTING (P/N 5292029-09.) THIS CRACK MEASURES APPROXIMATELY .149 IN LENGTH, AND WAS DISCOVERED USING THE LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN MEL-5SDR HYIA20190307002Fitting · crackedDURING NDT INSPECTION AS NOTED IN SID 57-10-16 A CRACK WAS IDENTIFIED ON THE RIGHT HAND INBOARD NACELLE FITTING (P/N: 5292029-22). THIS CRACK LOCATED ON THE LOWER LEG OF THE OUTBOARD SIDE OF THE FITTING MEASURES APPROXIMATELY .083" LONG AND IS CONSISTENT TO OTSDR HYIA20170828016Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED IN THE RT OUTBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE OUTBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK MEASURED .123 IN LENGTH.SDR HYIA20151223001Unknown · odorPILOT REPORTED BURNING SMELL ON DESCENT, NO SMOKE, BUT WAS UNABLE TO IDENTIFY THE SOURCE. INSPECTED WIRING ON INSTRUMENT PANEL, SIDE CONSOLE & CO-PILOT CONSOLE. NO EVIDENCE OF BURNING FOUND AT THIS TIME.SDR HYIA20151203005Master Cylinder · malfunctionedPILOT REPORTED RT BRAKE FAILURE WHILE MAKING RIGHT 180 ON RUNWAY. LT MAIN GEAR EXITED RUNWAY. INSPECTED THE ACFT, NO DAMAGE NOTED. RE-SEALED RT MASTER CYLINDER, SERVICED & BLED. TAXI CHECKED GOOD.SDR HYIA2015072020150Master Cylinder · lowPILOT REPORTED ON LANDING, RT BRAKE PEDAL WENT TO THE FLOOR & APPLIED NO BRAKE PRESS. INSPECTED RT BRAKE SYS WITH NO DEFECTS OR LEAKS NOTED. SERVICED RT BRAKE MASTER CYLINDER WITH HYD FLUID IAW MM CH 32-40-00. OPERATIONALLY CHECKED GOOD.SDR HYIA03272015004Beam · crackedTHE LT NACELLE OTBD ENG BEAM WAS FOUND TO BE CRACKED JUST FWD OF AFT ENG MOUNT, TRANSVERSE TO LENGTH OF BEAM, ACROSS UPPER FACE OF BEAM, DURING NDT PRESCRIBED WITHIN MEL-54-01. REMOVE BEAM ASSEMBLY, PERFORM DETAILED VISUAL INSPECTION OF SURROUNDING STRUCTURE SDR HYIA20140414041Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A SDR HYIA20121008001Wire Harness · out of positionON LANDING, PILOT NOTED SPARKS ON THE RT ENGINE COWL. SHUTDOWN RT ENGINE ON LANDING. WHEN INSPECTED, DISCREPANCY WAS CLEARED BY REROUTING POWER WIRE HARNESS AND INSOLATED IT IAW STANDARD PRACTICE.SDR HYIA20140414023Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & ASDR HYIA20140415071Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5, WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAWSDR HYIA26632LSTRTRelay · overheatedAFTER TAXI IN, ON SHUTDOWN, LT ENG CONTINUED TO CRANK UNTIL MASTER SWITCH WAS SHUTOFF. MX REMOVED AND REPLACED STUCK START RELAY AND REPLACED ASSOCIATED WIRING AS A PRECAUTIONARY MEASURE. SYS CHECKED OK, ACFT RELEASED BACK TO SERVICE.SDR HYIA26632Brake Sys · failedLEFT BRAKE FAILED DURING TAXI. MAINTENANCE INSPECTED BLED AND SERVICED LEFT BRAKE SYSTEM.SDR 135632112407Engine · failedON TAKEOFF FROM MAZ, AT 2400 FEET AND CLIMBING TO 3500 FEET, PILOT HEARD LOUD BOOM WITH RIGHT ENGINE SHUT DOWN AND PROPELLER FEATHERING. THE PILOT PERFORMED ENGINE FAILURE FLOW CHECK LIST AND RETURNED TO MAZ. PRELIMINARY INSPECTION SHOWS CATASTROPHIC FAILURESDR 1350527N26632Circuit Breaker · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH.SDR HYI2003F00003Clutch · failedCREW REPORTED LEFT ENGINE FAILED TO START. MECHANIC REMOVED AND REPLACED STARTER CLUTCH. ON INSPECTION OF REMOVED STARTER CLUTCH, MECHANIC FOUND DRIVE GEAR TOOTH SHEARED. RECOVERED SINGLE TOOTH FROM OIL PUMP. RETURNED AIRCRAFT TO SERVICE AFTER FURTHER INS
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