# N49016: not currently registered

- Registered now: No (not in the FAA registry file). The mark may be reserved or free to assign
- Earlier aircraft: 2
- Last cancelled: December 18, 2012
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=49016
- Page: https://openairdocs.org/aircraft/N49016

## Aircraft that carried N49016

- [Cancelled 2012-12-18](https://openairdocs.org/deregistered/N49016-2012-12-18): Cessna 152, S/N 15281102, built 1977. Registration expired, pending cancellation. Owner: [Action Technical Associates Inc](https://openairdocs.org/faa-owner/ACTION%20TECHNICAL%20ASSOCIATES%20INC), [Glendale, AZ](https://openairdocs.org/faa-place/AZ/Glendale)
- [Cancelled 1955-10-11](https://openairdocs.org/deregistered/N49016-1955-10-11): Aeronca L-3, S/N 058B-10813. Owner: [John Kenneth Curry](https://openairdocs.org/faa-owner/JOHN%20KENNETH%20CURRY), [Gold Beach, OR](https://openairdocs.org/faa-place/OR/Gold%20Beach)

## NTSB investigations on N49016 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB LAX92FA331](https://openairdocs.org/ntsb/LAX92FA331), Aug 3, 1992: Cessna 152 (N49016), Maricopa, AZ, destroyed, 1 fatal. Probable cause: THE PILOT EXCEEDED THE DESIGN STRESS LIMITS OF THE AIRPLANE STRUCTURE BY ATTEMPTING AN ABRUPT MANEUVER AT A SPEED IN EXCESS OF THE MANEUVERING SPEED.

## FAA accident and incident reports on N49016 (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 19920803028749A](https://openairdocs.org/incident/19920803028749A), Aug 3, 1992: Cessna 152 (N49016), Maricopa, AZ, Destroyed, 1 fatal. Left wing lift strut failed at fuselage due to high "g" overload and over vne speed,such as abrupt pullup in drive.

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