N454SF

Valid Registration

1999 CESSNA 208B

N454SF is a 1999 CESSNA 208B registered to PA1 208B-0797 LLC in FORT LAUDERDALE, FL. Its FAA registration status is Valid. It has 4 NTSB accident records on file. 16 Airworthiness Directives may apply.

Registration Details

N-Number
N454SF
Serial Number
208B-0797
Manufacturer
CESSNA
Model
208B
Year
1999
Registration Status
Valid
Airworthiness Date
1999-12-17
Owner
PA1 208B-0797 LLC
Owner City
FORT LAUDERDALE
Owner State
FL

The CESSNA 208B is registered with the FAA under N-number N454SF. This airframe was manufactured in 1999. Its manufacturer serial number is 208B-0797. The aircraft was issued its airworthiness certificate on 1999-12-17. The current registered owner is PA1 208B-0797 LLC, based in FORT LAUDERDALE, FL. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

No injuries reported2020-02-04

Hooper Bay, AK, USA

Accident — Cessna 208 (NTSB ANC20LA020)

Minor injuries2008-01-15

Bethel, AK, USA

Accident — Cessna 208B (NTSB ANC08LA031)

No injuries reported2005-12-13

Newtok, AK, USA

Accident — Cessna 208B (NTSB ANC06CA011)

No injuries reported2002-02-24

Tununak, AK, USA

Accident — Cessna 208B (NTSB ANC02LA016)

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

N454SF has been involved in 4 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

16 found
AD E9-16465Effective: 2009-07-15

Airworthiness Directives; Cessna Aircraft Company Models 208 and 208B Airplanes

We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 208 and 208B airplanes. This AD requires you to measure the roll and the yaw bridle cable tension (adjusting as necessary) and to torque the clamp screws. This AD results from two reported incidences of slack bridle cables with the swaged balls unseating from their drum recesses. We are issuing this AD to detect and correct loose bridle cable clamps, which could result in the swaged ball unseating from the recess in the servo drum and contacting the cable guard pin. This failure could lead to very limited control of the rudder and/or aileron with consequent loss of control.

Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N454SF may be affected by 16 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.

+15 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.

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Get the complete history for N454SF

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

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