N3844C

Valid Registration

CESSNA 310R

N3844C is a CESSNA 310R registered to MANSFIELD HELIFLIGHT INC in MILTON, VT. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 1 Airworthiness Directive may apply.

Registration Details

N-Number
N3844C
Serial Number
310R1238
Manufacturer
CESSNA
Model
310R
Year
—
Registration Status
Valid
Airworthiness Date
1977-11-21
Owner
MANSFIELD HELIFLIGHT INC
Owner City
MILTON
Owner State
VT

The CESSNA 310R is registered with the FAA under N-number N3844C. Its manufacturer serial number is 310R1238. The aircraft was issued its airworthiness certificate on 1977-11-21. The current registered owner is MANSFIELD HELIFLIGHT INC, based in MILTON, VT. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

No injuries reported2022-12-15

Lexington, KY, USA

Accident — CESSNA 310R (NTSB ERA23LA154)

No injuries reported1994-01-27

MEMPHIS, TN, USA

Accident — CESSNA 310R (NTSB ATL94LA045)

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

N3844C 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

1 found
AD 98-3640Effective: 1998-02-17

Airworthiness Directives; Cessna Aircraft Company Models T303, 310R, T310R, 335, 340A, 402B, 402C, 404, F406, 414, 414A, 421B, 421C, 425, and 441 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to Cessna Aircraft Company Models T303, 310R, T310R, 335, 340A, 402B, 402C, 404, F406, 414, 414A, 421B, 421C, 425, and 441 airplanes. This action requires revising the FAA-approved Airplane Flight Manual (AFM) to specify procedures that would prohibit flight in severe icing conditions (as determined by certain visual cues), limit or prohibit the use of various flight control devices while in severe icing conditions, and provide the flight crew with recognition cues for, and procedures for exiting from, severe icing conditions. The proposed AD is prompted by the results of a review of the requirements for certification of these airplanes in icing conditions, new information on the icing environment, and icing data provided currently to the flight crew. The actions specified by this AD are intended to minimize the potential hazards associated with operating these airplanes in severe icing conditions by providing more clearly defined procedures and limitations associated with such conditions.

Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N3844C may be affected by 1 directive. 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.

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Get the complete history for N3844C

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

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