N301AZ

EMBRAER EXECUTIVE AIRCRAFT INC EMB-505 · 2016 · Fixed-wing multi-engine · 2 engines · 8 seats · Valid Registration

Registered owner: PHENOM 300 LLC, FL (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
DOLPHIN ATLANTIC INC (F2PA)Certificate holder—Matched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

3 reports on file, 2019-05-04 – 2025-10-27.

FLT CONT AFFECTED · 2025-10-27 Matched by certificate designator
ATA 2750

Part: CONTROL LEVER — FAULTED (COCKPIT) · airframe 6,118 hrs · 4,275 cycles

ON APPROACH TO LAND AT KAPF THE FLAPS FAILED TO LOWER. AIRCRAFT MADE AN UN-EVENTFUL LANDING W/O FLAP USE. FLAP SYSTEM WAS TROUBLESHOT AND THE FLAP HANDLE CONTROL ASSEMBLY WAS DETERMINED TO BE FAULTY. THE FLAP HANDLE CONTROL ASSEMBLY WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO FURTHER INSTANCES OF ANY FLAP ISSUE HAS BEEN REPORTED SINCE THE INITIAL FAILURE AND REPLACEMENT

Source: SDR F2PA202511040256
WARNING INDICATION · 2021-09-10 Matched by certificate designator
ATA 2120

Part: VALVE — BROKEN (RAM AIR) · airframe 3,664 hrs · 2,509 cycles

RAM AIR VALVE FAILED (DOOR HINGE POINTS CRACKED/BROKEN). CREW RECEIVED A "DUCT1 OVR HT" FOLLOWED BY A "DUCT2 OVR HT" CAS MESSAGE. PER THE FLIGHT MANUAL, ENGINE POWER WAS REDUCED AND THE AIRCRAFT MADE AN UNSCHEDULED LANDING AT KBNA. AOG TEAM FOUND THE RAM AIR CONTROL VALVE BROKEN, AND REPLACED THE VALVE AND DOWNSTREAM HEAT EXCHANGER.

Source: SDR 2021F00220
ELECT. POWER LOSS-50 PC; WARNING INDICATION · 2019-05-04 Matched by certificate designator
ATA 2435

Part: STARTER GEN — FAILED (RT ENGINE) · airframe 1,832 hrs · 1,206 cycles

AT CRUISE, INDICATION OF LOSS OF ELECTRICAL POWER OF THE #2 DC STARTER/GENERATOR. CREW ELECTED TO MAKE AN UNSCHEDULED PRECAUTIONARY LANDING AT KATL. UPON INSPECTION, THE STARTER GENERATOR WAS DISCOVERED TO BE INTERNALLY FAILED, AND HAD SHEARED ITS DESIGNED DRIVE SHAFT SHEAR POINT. PRIOR TO IT SHEARING ITS SHAFT, THE STARTER GENERATOR SHEARED ITS QAD MOUNT DOWEL PINS AND ROTATED APPROXIMATELY 45 DEGREES ON ITS MOUNT PAD.

Source: SDR 2019F00212