2000 CESSNA T206H
N206EA is a 2000 CESSNA T206H registered to ABRAMS EDWARD L in ROXBURY, CT. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 10 Airworthiness Directives may apply.
The CESSNA T206H is registered with the FAA under N-number N206EA. This airframe was manufactured in 2000. Its manufacturer serial number is T20608186. The aircraft was issued its airworthiness certificate on 2019-11-13. The current registered owner is ABRAMS EDWARD L, based in ROXBURY, CT. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.
WEST PALM BCH, FL, USA
Accident — Airbus Industrie A300B4-2C (NTSB MIA86FA208)
ATLANTIC OCEAN, AO
Accident — Airbus Industrie A-300B4-2C (NTSB MIA85FA178)
Severity reflects injuries to people involved, not damage to the aircraft. A “no injuries” accident can still involve significant aircraft damage.
N206EA 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.
Airworthiness Directives; Cessna Aircraft Company Models 172R, 172S, 182T, T182T, 206H, and T206H Airplanes
The FAA is adopting a new airworthiness directive (AD) to supersede AD 2006-17-04, which applies to certain Cessna Aircraft Company (Cessna) Models 172R, 172S, 182T, T182T, 206H, and T206H airplanes. AD 2006-17-04 currently requires you to inspect the two end fittings on each of the flexible fuel hoses located in the engine compartment for the correct torque values, and, if any incorrect torque values are found during the inspection, tighten the hose end fittings to the correct torque values. This AD results from four reports of loose fuel lines connected to the fuel servo or fuel flow transducer. Two reports were of in-flight engine failure on a Model T182T airplane. A third report was of in-flight engine failure on a Model 206H airplane. A fourth report was of a Model 172S airplane losing engine power on final approach. Consequently, this AD would require you to establish the correct torque values of the end fittings on fuel hoses for certain Cessna Models 172R, 172S, 182T, T182T, 206H, and T206H airplanes. This AD clarifies that the torque values need to be physically established and visual inspection only is not sufficient. We are issuing this AD to detect and correct potential loss of fuel flow, which may result in partial or complete loss of engine power and/or uncontrolled engine compartment fire due to fuel leakage forward of the firewall.
Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N206EA may be affected by 10 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.
+9 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.
Get the full report →Full accident narratives, all Airworthiness Directives, ownership chain, and a downloadable PDF.
View Full Report →