N62V

Valid Registration

1967 BEECH 65-A90-1

N62V is a 1967 BEECH 65-A90-1 registered to DYNAMIC AVLEASE INC in BRIDGEWATER, VA. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 2 Airworthiness Directives may apply.

Registration Details

N-Number
N62V
Serial Number
LM-74
Manufacturer
BEECH
Model
65-A90-1
Year
1967
Registration Status
Valid
Airworthiness Date
2013-05-10
Owner
DYNAMIC AVLEASE INC
Owner City
BRIDGEWATER
Owner State
VA

The BEECH 65-A90-1 is registered with the FAA under N-number N62V. This airframe was manufactured in 1967. Its manufacturer serial number is LM-74. The aircraft was issued its airworthiness certificate on 2013-05-10. The current registered owner is DYNAMIC AVLEASE INC, based in BRIDGEWATER, VA. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

No injuries reported1994-10-18

WHEELING, IL, USA

Accident — QUESTAIR VENTURE (NTSB CHI95LA015)

Minor injuries1987-10-14

GREENSBORO, NC, USA

Accident — QUESTAIR 20 (NTSB ATL88DMG02)

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

N62V 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

2 found
AD 02-1206Effective: 2002-01-22

Airworthiness Directives; Raytheon Aircraft Company Beech Models 65-90, 65-A90, 65-A90-1, 65-A90-4, B90, C90, C90A, E90, and H-90 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to certain Raytheon Aircraft Company (Raytheon) Beech Models 65-90, 65-A90, 65-A90-1, 65-A90-4, B90, C90, C90A, E90, and H-90 airplanes. This AD requires you to repetitively inspect the main landing gear upper torque knees and lower torque knees for evidence of fatigue cracks; and replace any torque knee with evidence of fatigue cracks. This AD is the result of reports of many incidents of main landing gear torque knees cracking or breaking on the above-referenced airplanes. The actions specified by this AD are intended to detect and replace cracked main landing gear torque knees, which could result in failure of the main landing gear and consequent loss of control of the airplane during takeoff, landing, or other ground operations.

Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N62V may be affected by 2 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.

+1 more Airworthiness Directive 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 N62V

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

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