1998 CESSNA 182S
N5467C is a 1998 CESSNA 182S registered to STEAMBOAT SPRINGS FLYING CLUB INC in STEAMBOAT SPRINGS, CO. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 9 Airworthiness Directives may apply.
The CESSNA 182S is registered with the FAA under N-number N5467C. This airframe was manufactured in 1998. Its manufacturer serial number is 18280230. The aircraft was issued its airworthiness certificate on 1998-06-03. The current registered owner is STEAMBOAT SPRINGS FLYING CLUB INC, based in STEAMBOAT SPRINGS, CO. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.
Steamboat Springs, CO, USA
Accident — CESSNA 182S (NTSB CEN13CA435)
Waukesha, WI, USA
Accident — Cessna 182S (NTSB CHI05CA270)
Severity reflects injuries to people involved, not damage to the aircraft. A “no injuries” accident can still involve significant aircraft damage.
N5467C 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, 182S, 182T, T182T, 206H, and T206H Airplanes
The FAA adopts a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 172R, 172S, 182S, 182T, T182T, 206H, and T206H airplanes. This AD requires you to install Modification Kit MK172-25-10C or a steel lock rod/bar on both crew seat back cylinder lock assemblies. If a steel lock rod/bar has already been installed on the crew seat back cylinder lock assembly, no further action is required. If you have already installed Modification Kit MK172-25-10A or MK172-25-10B, this AD requires you to do an installation inspection and correct any discrepancies found. This AD results from reports of the crew seat back cylinder lock assembly failing at the aft end and other cylinder lock assemblies found cracked. We are issuing this AD to prevent the crew seat back cylinder lock assembly from bending, cracking, or failing. This failure could cause uncontrolled movement of the seat back, resulting in possible backward collapse during flight. Backward collapse of either crew seat back could result in an abrupt pitch-up if the affected crew member continues to hold on to the control yoke during this failure and could cause difficulty in exiting the airplane from an aft passenger seat after landing.
Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N5467C may be affected by 9 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.
+8 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 →