N501PH - Aircraft Aircraft Registration
B407Aircraft Description
Airworthiness Date
Invalid Date
Classification
Standard Normal Category
Type Registration
Unknown
Status
N-Number assigned, has not been registered and is pending cancellation
Cert Issue Date
—
Registered Owner
The registered owner has requested to keep this data private under Title 49 of the United States Code, Section 44114.
Powerplant & Avionics
Engine Type
—
Number of Engines
—
Mode S Code (Oct)
51437364
Mode S Code (Hex)
A63EF4
NTSB Accident History (2)
| Date | NTSB # | Damage | Highest Injury | Probable Cause |
|---|---|---|---|---|
| Jun 8, 2015 | CEN15LA265 | Substantial | None | The fatigue fracture of the tail rotor gearbox attachment studs, which resulted in a loss of tail rotor control and a subsequent hard landing. |
| Mar 24, 2003 | FTW03FA117 | Substantial | None | The loss of tail rotor drive and anti-torque control resulting from the fracture and separation of the #5 tail rotor drive segment due to the overtemperature and subsequent failure of the #5 hangar bearing. |
Jun 8, 2015CEN15LA265
Substantial
None
The fatigue fracture of the tail rotor gearbox attachment studs, which resulted in a loss of tail rotor control and a subsequent hard landing.
Mar 24, 2003FTW03FA117
Substantial
None
The loss of tail rotor drive and anti-torque control resulting from the fracture and separation of the #5 tail rotor drive segment due to the overtemperature and subsequent failure of the #5 hangar bearing.
Additional Details
Registration
N501PH
Serial Number
53401
Number of Engines
—
Number of Seats
—
Expiration Date
—
Last Action Date
—
Last Update Date
—
Unique ID
—
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-05-01 01:32:20 UTC