# N623LB: not currently registered

- Registered now: No (not in the FAA registry file). The mark may be reserved or free to assign
- Earlier aircraft: 1
- Last cancelled: April 3, 2020
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=623LB
- Page: https://openairdocs.org/aircraft/N623LB

## Aircraft that carried N623LB

- [Cancelled 2020-04-03](https://openairdocs.org/deregistered/N623LB-2020-04-03): Mccleery Gregg A RANS S6ES, S/N 07011418ES, built 2006. Registration expired, pending cancellation. Owner: [Wilson Paul A](https://openairdocs.org/faa-owner/WILSON%20PAUL%20A), [Grass Valley, CA](https://openairdocs.org/faa-place/CA/Grass%20Valley)

## NTSB investigations on N623LB (2)

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 WPR12LA437](https://openairdocs.org/ntsb/WPR12LA437), Sep 25, 2012: Mccleery Rans S6ES (N623LB), Elverta, CA, substantial damage. Probable cause: A loss of engine power during initial climb due to a failed piston ring.
- [NTSB MIA98LA122](https://openairdocs.org/ntsb/MIA98LA122), Apr 7, 1998: Brock 162F (N623LB), Canton, GA, substantial damage. Probable cause: the pilot's improper use of throttle and collective pitch during initial takeoff climb, which resulted in a decay of rotor rpm and settling of the helicopter into a lake.

## FAA accident and incident reports on N623LB (2)

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 20120925020919A](https://openairdocs.org/incident/20120925020919A), Sep 25, 2012: Mccleery Gregg A RANS S6ES (N623LB), Elverta, CA, Substantial damage. The engine run-up was normal. Then seconds after the aircraft was maneuvering to establish a normal climb the engine shut down in flight. The loose of power…
- [Accident 19980407006149A](https://openairdocs.org/incident/19980407006149A), Apr 7, 1998: Amtr EXEC162F (N623LB), Canton, CA, Substantial damage. Departed helo pad rotor speed decayed due collective use. Unable pad. Autorotated into lake. Rotors struck cabin. (.4)the pilot stated he experienced a loss of…

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