N732MD

Valid Registration

2004 CESSNA 208B

N732MD is a 2004 CESSNA 208B registered to UMB BANK NA TRUSTEE in SALT LAKE CITY, UT. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 16 Airworthiness Directives may apply.

Registration Details

N-Number
N732MD
Serial Number
208B1083
Manufacturer
CESSNA
Model
208B
Year
2004
Registration Status
Valid
Airworthiness Date
2004-09-24
Owner
UMB BANK NA TRUSTEE
Owner City
SALT LAKE CITY
Owner State
UT

The CESSNA 208B is registered with the FAA under N-number N732MD. This airframe was manufactured in 2004. Its manufacturer serial number is 208B1083. The aircraft was issued its airworthiness certificate on 2004-09-24. The current registered owner is UMB BANK NA TRUSTEE, based in SALT LAKE CITY, UT. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

No injuries reported2015-11-02

Chicago, IL, USA

Accident — CESSNA 208B (NTSB CEN16LA052)

No injuries reported2013-07-17

Chicago, IL, USA

Accident — CESSNA 208B (NTSB CEN13LA421)

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

N732MD 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.

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. N732MD 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 N732MD

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

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