# Service difficulty reports: N76 A list on [N76](https://openairdocs.org/aircraft/N76.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 2026F00032](https://openairdocs.org/sdr/2026F00032.md): Bleed Air Sys · faulted · Mar 17, 2026 · N76 · Beech B300 · Engine Bleed Air System > RIGHT BLEED AIR FAIL RED SEGMENT LIGHT ILLUMINATED AT FL 200 EMERGENCY CHECK LIST RUN LIGHT EXTINGUISHED DECENDING THROUGH 7000 MSL - [SDR RU3A2020120900036](https://openairdocs.org/sdr/RU3A2020120900036.md): Controller · failed · Dec 9, 2020 · N76 · Beech 300BEECH · Cabin Pressure Controller > CABIN ALT WARNING ILLUMINATED IN FLIGHT CABIN DIFF SHOWS "0". AIR PRESSURE CONTROLLER REPLACEMENT CORRECTED ISSUE. - [SDR RU3A20190212003](https://openairdocs.org/sdr/RU3A20190212003.md): Door · noisy · Feb 12, 2019 · N76 · Beech 300BEECH · Passenger/Crew Doors > PASSING 11,000 MSL, CABIN LOST PRESSURE. MS REPORTS HISSING SOUND FROM CABIN DOOR. - [SDR RU3A20180309010](https://openairdocs.org/sdr/RU3A20180309010.md): Pcb · loose · Mar 9, 2018 · N76 · Beech 300BEECH · Rudder Control System > RUDDER BOOST OFF LIGHT ILLUMINATED. RUNNING THE ABNORMAL CHECKLIST MADE NO DIFFERANCE. DISCOVERED LOOSE RELAY AND SOCKET. REPLACED LOGIC RELAY PCB. RUDDER BOOST LAMPS WORKING CORRECTLY. NO FURTHER ACTION REQUIRED. - [SDR RU3A20170721020](https://openairdocs.org/sdr/RU3A20170721020.md): Filter · restricted · Jul 21, 2017 · N76 · Beech 300BEECH · Cabin Pressure Control System > DUE TO A RESTRICTED SAFETY VALVE FILTER, PRESSURIZATION SYSTEM FAILED IN FLIGHT. SYSTEM PERFORMED WITHOUT FURTHER ISSUE AFTER FILTER WAS CLEANED. NO NOTED TREND - [SDR RU3A20131126015](https://openairdocs.org/sdr/RU3A20131126015.md): Warning Light · illuminated · Nov 26, 2013 · N76 · Beech 300BEECH · Landing Gear Position and Warning > THE IN TRANSIT LIGHT REMAINED ON WHEN THE GEAR WAS RETRACTED. WHEN MOVED TO THE DOWN POSITION, RECEIVED THREE GREEN, NO RED. GEAR DOWN AND LOCKED, LANDED WITHOUT INCIDENT. - [SDR RU3A20130503007](https://openairdocs.org/sdr/RU3A20130503007.md): Autofeather Sys · malfunctioned · May 3, 2013 · N76 · Beech 300BEECH · Propeller Feathering/Reversing > DURING RUN UP AUTO FEATHERS CHECKED SAT. DURING POWER UP ON TAKEOFF ROLL AUTO FEATHERS ARMED AT APPROX 80 KTS PLUS LEFT AUTO FEATHER LIGHT WENT OUT. TAKEOFF ABORTED. STOPPED ON RUNWAY, DID A RUN UP AND AUTO FEATHER ARMED. BEGAN A SECOND TAKEOFF ROLL AND AT - [SDR RU3A20121113001](https://openairdocs.org/sdr/RU3A20121113001.md): Wire · broken · Nov 13, 2012 · N76 · Beech 300BEECH · Fire Protection System Wiring > ON TAKEOFF ROLL AT APPROX 60 KIAS, PNF OBSERVED DISCHARGED LIGHT ILLUMINATION ON LEFT FIRE BOTTLE. PNF CALLED OUT AN ABORT AND PF ABORTED TAKEOFF. CREW TAXIED AIRCRAFT TO HANGAR WITH NO FURTHER INCIDENT. FOUND BROKEN WIRE TO NR 1 FIRE BOTTLE. REPAIRED BROK - [SDR RU3A1113](https://openairdocs.org/sdr/RU3A1113.md): Proximity Switch · defective · Apr 5, 2011 · N76 · Beech 300BEECH · Propeller Indication System > IN CRUISE FLIGHT AT 16000 MSL, RIGHT PROP PITCH ANNUNCIATOR ILLUMINATED. NO OTHER INDICATIONS ON INSTRUMENTS. NO AFFECTS ON AIRCRAFT HANDLING WERE DETECTED IN FLIGHT. CREW ELECTED TO RETURN TO HOME BASE. IN ANTICIPATION OF POSSIBLE ASYMMETRIC THRUST ON LAN - [SDR RU3A 1112](https://openairdocs.org/sdr/RU3A%201112.md): Lanyard · broken · Mar 3, 2011 · N76 · Beech 300BEECH · Fuel Storage > AFTER TAKEOFF FUEL WAS STREAMING FROM RIGHT MAIN FUEL CAP WITH FUEL CAP FLUSH WITH AIRCRAFT SURFACE. REQUESTED PRIORITY HANDLING FROM TOWER, LANDING WAS UNEVENTFUL. MAINTENANCE DISCOVERED LANYARD WAS BROKEN AND CAUGHT BETWEEN FUEL CAP AND SEALING SURFACE. - [SDR RU3A1105](https://openairdocs.org/sdr/RU3A1105.md): Shrader Valve · leaking · Feb 3, 2011 · N76 · Beech 300BEECH · Landing Gear Retraction/Extension System > ON APPROACH, LOWERED LANDING GEAR AND NO AUDIBLE SOUND HEARD NOR ANY LIGHTS INDICATED IN GEAR HANDLE OR ON POSITION LIGHTS. FLAPS LOWERED TO FULL POSITION IN ORDER TO CONFIRM ABNORMAL INDICATION. LANDING GEAR HORN SOUNDED INDICATING GEAR WAS NOT IN DOWN POSI - [SDR RU3A1020](https://openairdocs.org/sdr/RU3A1020.md): Connector · loose · Oct 7, 2010 · N76 · Beech 300BEECH · Landing Gear System > FLAPS AT APPROACH POSITION. SELECTED LANDING GEAR DOWN. POSITION INDICATORS SHOWED GREEN FOR NOSE AND LEFT MAIN GEAR. NO INDICATION ON RIGHT MAIN GEAR. CHECKED ANNUNCIATOR, GOOD. SELECTED FLAPS FULL DOWN AND RECEIVED CONFIGURATION WARNING HORN. DECLARED E - [SDR RU32005F00001](https://openairdocs.org/sdr/RU32005F00001.md): Warning Light · false indication · Mar 24, 2005 · N76 · Beech 300BEECH · Landing Gear Position and Warning > ON FINAL APPROACH, LOWERED GEAR AT FAF - NO LEFT MAIN GEAR LIGHT. CYCLED GEAR ONCE INSIDE FAF - STILL NO LIGHTS, EXECUTED FLY BY RWY 4R. 2 AIRLINE CREWS ADVISED ALL 3 GEARS APPEAR DOWN. FLEW LT TRAFFIC, CYCLED GEAR 3RD TIME, OBSERVED GEAR RETRACT AND EXTEND - [SDR 2005F00017](https://openairdocs.org/sdr/2005F00017.md): Odor · detected · Feb 17, 2005 · N76 · Beech 300BEECH · Communications System > ON DOWNWIND AFTER BPC RUN, SMELLED ELECTRICAL BURNING. NOTICED NUMBER 2 COMM NO LED READOUT. PULLED CB NR 2 COMM DUMPED CABIN. SMELL DID NOT DISPERSE TO OUR EXPECTATION. LANDED AIRCRAFT. (M) - [SDR 2005F00016](https://openairdocs.org/sdr/2005F00016.md): Power Supply · burned · Feb 17, 2005 · N76 · Beech 300BEECH · Communications System > ON DOWNWIND AFTER BPC RUN, SMELLED ELECTRICAL BURNING. NOTICED NUMBER 2 COMM NO LEAD READOUT. PULLED CB NUMBER 2 COMM DUMPED CABIN. SMELL DID NOT DISPERSE TO OUR EXPECTATION. LANDED AIRCRAFT. FOUND NR 2 COMM POWER SUPPLY BURNED, REPLACED NR 2 COMM. (M) - [SDR RU3A0421](https://openairdocs.org/sdr/RU3A0421.md): Cooling Fan · burned · Dec 8, 2004 · N76 · Beech 300BEECH · Inertial Guidance System > WHILE SETTING UP FOR FLIGHT INSPECTION MANEUVER, GOT A RED MASTER CAUTION LIGHT WITH AN AP TRIM DISC LIGHT. TEMPORARILY LOST TCAS, PILOTS FLIGHT DIRECTOR, AND THE PILOTS NCU. AT THE SAME TIME HEARD ELECTRICAL SHORTING SOUND. STRONG ELECTRICAL FUMES WERE DET - [SDR RU3A02006](https://openairdocs.org/sdr/RU3A02006.md): Indicator · false indication · Sep 10, 2002 · N76 · Beech 300BEECH · Engine BMEP/Torque Indicating > ON TAKEOFF ROLL AT 70KIAS, THE 1 TORQUE GAUGE JUMPED FROM 35 TO 120 WITH THROTTLES ALIGNED. RIGHT TORQUE DID NOT EXCEED 70 TAKEOFF ABORTED. REMOVED AND REPLACED NR 1 TORQUE INDICATOR. OPS CHECK SATISFACTORY. (M) ## 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 = 'N76' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N76/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.