N3125D

Valid Registration

1955 CESSNA 180

N3125D is a 1955 CESSNA 180 registered to DAVIS RONALD L JR in SOLDOTNA, AK. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 11 Airworthiness Directives may apply.

Registration Details

N-Number
N3125D
Serial Number
31923
Manufacturer
CESSNA
Model
180
Year
1955
Registration Status
Valid
Airworthiness Date
1955-11-04
Owner
DAVIS RONALD L JR
Owner City
SOLDOTNA
Owner State
AK

The CESSNA 180 is registered with the FAA under N-number N3125D. This airframe was manufactured in 1955. Its manufacturer serial number is 31923. The aircraft was issued its airworthiness certificate on 1955-11-04. The current registered owner is DAVIS RONALD L JR, based in SOLDOTNA, AK. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

No injuries reported2018-06-22

Fairbanks, AK, USA

Accident — CESSNA 180 (NTSB ANC18LA048)

No injuries reported2014-03-27

North Pole, AK, USA

Accident — CESSNA 180 (NTSB ANC14CA021)

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

N3125D 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

11 found
AD 2011-10988Effective: 2011-05-13

Airworthiness Directives; Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190, 195, 206, 207, 210, T303, 336, and 337 Airplanes

We are superseding an existing airworthiness directive (AD) for Cessna Aircraft Company (Cessna) 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190, 195, 206, 207, 210, T303, 336, and 337 series airplanes. That AD currently requires repetitive inspections and replacement of parts, if necessary, of the seat rail and seat rail holes; seat pin engagement; seat rollers, washers, and axle bolts or bushings; wall thickness of roller housing and the tang; and lock pin springs. This new AD requires retaining all of the actions from the previous AD and adding steps to the inspection procedures in the previous AD. This AD was prompted by added steps to the inspection procedures, added revised figures, and clarification of some of the existing steps. We are issuing this AD to prevent seat slippage or the seat roller housing from departing the seat rail, which may consequently cause the pilot/copilot to be unable to reach all the controls. This failure could lead to the pilot/copilot losing control of the airplane.

Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N3125D may be affected by 11 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.

+10 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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Get the complete history for N3125D

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

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