# N1885H: 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: October 4, 1991
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=1885H
- Page: https://openairdocs.org/aircraft/N1885H

## Aircraft that carried N1885H

- [Cancelled 1991-10-04](https://openairdocs.org/deregistered/N1885H-1991-10-04): Piper PA-32R-300, S/N 32R7780197. Triennial form not returned. Owner: [Ameriflight Inc](https://openairdocs.org/faa-owner/AMERIFLIGHT%20INC), [Burbank, CA](https://openairdocs.org/faa-place/CA/Burbank)
- [Cancelled 1961-10-25](https://openairdocs.org/deregistered/N1885H-1961-10-25): Cessna 310C, S/N 35985. Exported to Argentina. Owner: [Cap Sales Corp](https://openairdocs.org/faa-owner/CAP%20SALES%20CORP), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)

## NTSB investigations on N1885H (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 LAX91LA085](https://openairdocs.org/ntsb/LAX91LA085), Jan 21, 1991: Piper PA 32-300 (N1885H), Anaheim, CA, substantial damage. Probable cause: MAINTENANCE PERSONNEL IN THAT THEY IMPROPERLY ADJUSTED THE LEFT MAGNETO WHICH RESULTED IN THE COMPLETE EROSION OF THE ELECTRODES FROM SIX OF THE TWELVE INSTALLED SPARK PLUGS. THE INSTALLATION OF…

## FAA accident and incident reports on N1885H (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 19910121003189A](https://openairdocs.org/incident/19910121003189A), Jan 21, 1991: Piper PA32R300 (N1885H), Anaheim, CA, Substantial damage. Lost power. Gear collapsed on forced landing. Igniter electrodes eroded from incorrect mag timing. Low compression.

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