N51774

Valid Registration

ENSTROM F-28C

N51774 is a ENSTROM F-28C registered to SALAIKA TIMOTHY A in DANBURY, TX. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 6 Airworthiness Directives may apply.

Registration Details

N-Number
N51774
Serial Number
440
Manufacturer
ENSTROM
Model
F-28C
Year
—
Registration Status
Valid
Airworthiness Date
1978-10-23
Owner
SALAIKA TIMOTHY A
Owner City
DANBURY
Owner State
TX

The ENSTROM F-28C is registered with the FAA under N-number N51774. Its manufacturer serial number is 440. The aircraft was issued its airworthiness certificate on 1978-10-23. The current registered owner is SALAIKA TIMOTHY A, based in DANBURY, TX. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

No injuries reported1997-01-29

LAKE JACKSON, TX, USA

Accident — Enstrom F-28C (NTSB FTW97LA094)

No injuries reported1989-04-08

PADRE ISLAND, TX, USA

Accident — ENSTROM F28C (NTSB FTW89LA079)

Severity reflects injuries to people involved, not damage to the aircraft. A “no injuries” accident can still involve significant aircraft damage.

N51774 has been involved in 2 NTSB accidents since 1982. Each record above includes the date, location, severity, and NTSB summary. Buyers should review the full accident narratives and verify repairs in the aircraft's logbooks before purchase.

Applicable Airworthiness Directives

6 found
AD E7-16770Effective: 2007-08-28

Airworthiness Directives; Enstrom Helicopter Corporation Model F-28A, F-28C, F-28F, TH-28, 280, 280C, 280F, 280FX, 480, and 480B Helicopters

This amendment adopts a new airworthiness directive (AD) for Enstrom Helicopter Corporation (Enstrom) Model F-28A, F-28C, F-28F, TH- 28, 280, 280C, 280F, 280FX, 480, and 480B helicopters that requires determining the installation dates for each main rotor push-pull control rod (push-pull rod), inspecting the push-pull rods for corrosion, replacing any push-pull rod which has corrosion that is severe enough to cause pitting, or has visible moisture inside the rod, and repairing each push-pull rod that has corrosion but no pitting. This amendment is prompted by one reported incident in which the helicopter pilot encountered severe in-flight vibration due to the failure of a push-pull rod, requiring an emergency landing. The actions specified by this AD are intended to detect corrosion and prevent failure of a push-pull rod, and subsequent loss of control of the helicopter.

Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N51774 may be affected by 6 directives. All applicable ADs must be complied with for the aircraft to remain legally airworthy. Buyers should verify AD compliance in the aircraft's logbooks before purchase.

+5 more Airworthiness Directives found for this aircraft

Full list, with effective dates and links to the official Federal Register documents, is included in the paid report.

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Other ENSTROM F-28C aircraft in our database

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Get the complete history for N51774

Full accident narratives, all Airworthiness Directives, ownership chain, and a downloadable PDF.

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