BEECH F90
N111AA is a BEECH F90 registered to BLUE WATER AVIATION LLC in VESTAVIA, AL. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 1 Airworthiness Directive may apply.
The BEECH F90 is registered with the FAA under N-number N111AA. Its manufacturer serial number is LA-6. The aircraft was issued its airworthiness certificate on 1999-11-05. The current registered owner is BLUE WATER AVIATION LLC, based in VESTAVIA, AL. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.
LOS ANGELES, CA, USA
Incident — MCDONNELL DOUGLAS DC-10-10 (NTSB LAX91IA308)
DETROIT, MI, USA
Incident — MCDONNELL DOUGLAS DC-10-10 (NTSB CHI85IA339)
Severity reflects injuries to people involved, not damage to the aircraft. A “no injuries” accident can still involve significant aircraft damage.
N111AA 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; Raytheon Aircraft Corporation Beech Models 65-90, 65-A90, 65-A90-1, 65-A90-2, 65-A90-3, 65-A90-4, B90, C90, C90A, E90, H90, and F90 Airplanes
This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 99-10-07, which was sent previously to all known U.S. owners and operators of Raytheon Aircraft Corporation (Raytheon) Beech Models 65-90, 65-A90, 65-A90-1, 65-A90-2, 65-A90-3, 65-A90-4, B90, C90, C90A, E90, H90, and F90 airplanes. This AD requires inspecting for interference or damage between the elevator control cable and equipment under the cockpit floor panels (wire harnesses, stainless steel clamps, etc.) and running a cloth wrap around the control cable to detect broken strands of the control cable. This AD also requires replacing or repairing any damaged items, securing any component that is interfering with the elevator control cable, and installing additional supports and clamps as necessary to prevent sagging or further interference. This AD resulted from reports of reduced or loss of elevator control on five of the affected airplanes. The actions specified by this AD are intended to detect and correct interference between the elevator control cable and equipment under the cockpit floor panels before the elevator control cable breaks, which could result in loss of elevator control with potential loss of control of the airplane.
Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N111AA 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.
Full accident narratives, all Airworthiness Directives, ownership chain, and a downloadable PDF.
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