1978 CESSNA 182Q
N725AS is a 1978 CESSNA 182Q registered to GEORGIA CO OF ASPIRING FLYERS LLC in CLARKESVILLE, GA. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 2 Airworthiness Directives may apply.
The CESSNA 182Q is registered with the FAA under N-number N725AS. This airframe was manufactured in 1978. Its manufacturer serial number is 18266640. The aircraft was issued its airworthiness certificate on 1978-10-19. The current registered owner is GEORGIA CO OF ASPIRING FLYERS LLC, based in CLARKESVILLE, GA. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.
Reliance, TN, USA
Accident — CESSNA 182 (NTSB ERA23FA219)
Wauchula, FL, USA
Accident — CESSNA 182Q (NTSB ERA14CA023)
Severity reflects injuries to people involved, not damage to the aircraft. A “no injuries” accident can still involve significant aircraft damage.
N725AS 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 182Q and 182R Airplanes
We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 182Q and 182R airplanes that are equipped with Societ[eacute] de Motorisations A[eacute]ronautiques (SMA) Aircraft Diesel Engine (ADE) Model SR305-230-1 or Model SR305-230 converted to Model SR305-230-1 installed under Supplemental Type Certificate (STC) SA03302AT. This AD requires you to remove the intercooler and the intercooler inlet and outlet hoses, install a reworked intercooler and new intercooler inlet and outlet hoses, inspect hoses and clamp torques, repetitively inspect installation of the intercooler outlet and inlet hose assemblies for any displacement or damage of clamps or hoses, and, if necessary, replace any damaged clamps or hoses. This AD results from a report of two instances of induction hose disconnection occurring while in service, resulting in a loss of turbo boost and a significant loss of engine power. We are issuing this AD to detect and correct improper intercooler outlet and intercooler inlet hose assembly installations, which could result in loss of turbo boost and a significant loss of engine power. This failure could lead to an inability to maintain constant altitude in flight.
Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N725AS 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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