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N208SD

Cancelled 2016

Deregistered aircraft · 1995 Cessna 208B · Pratt & Whitney PT6A series

Open in FAA registry

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Cancelled: November 9, 2016
Status when cancelled: Valid registration
Serial number: 208B0491
Year built: 1995
Type: Fixed wing single engine
Engine: Turbo-prop
Airworthiness: Standard, normal
Airworthiness date: December 5, 1995
Certificate issued: March 2, 2009
Last registry action: August 1, 2016
Mode S code: A1B14F
Owner when cancelled: Icecap LLC Trustee
Location: Anchorage, AK
Owner type: Corporation

Airframe modelCessna 208BTCDS A37CE · ADs, bulletins and aircraft registered now Engine modelPratt & Whitney PT6A seriesTurbo-prop

From the FAA registry file of October 29, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

NTSB investigations · 1

Matched to this aircraft by N208SD and the event date: up to this one’s cancellation.

NTSB ANC17MA001Accident · 3 fatalClass 1 · MajorFinal reportTogiak, AKThe flight crew's decision to continue the visual flight rules flight into deteriorating visibility and their failure to perform an immediate escape maneuver after entry into instrument meteorological conditions, which resulted in controlled flight into…Oct 2, 2016 · Destroyed

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N208SD and the event date: up to this one’s cancellation.

Accident 20161002019779ACruise/Level Flight · Togiak, AKA Cessna 208B N208SD departed quinhagak airport Alaska at 1133 local time on October 2, 2016 enroute for Togiak airport Alaska. A two pilot crew with on passenger and 40LBS of cargo. The weather was marginal VFR conditions with rain squalls in the area. The…Oct 2, 2016 · Destroyed · 3 fatal

Service difficulty reports · 5

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR EPUA20130124002Mount · damagedVERTICAL STABILIZER BOLT MOUNTING HOLES WORN. REPAIRED VERTICAL STABILIZER HOLES IAW FORM 8110-3 DATED 1-12-2013. REPLACED AN176 TAIL ATTACH HARDWARE WITH INCREASED DIAMETER AN177 HARDWARE.Jan 13, 2013 · N208SD · Cessna 208B · Vertical Stabilizer, Attach Fittings SDR EPUA20130124003Skin · looseRIGHT WING TOP SKIN NEAR L/E HAS LOOSE RIVETS. REPAIRED RT WING IAW SRM 57-23-01, PARA 4 A-C, REV 4.Jan 10, 2013 · N208SD · Cessna 208B · Wing, Plate/Skin SDR EPUA20130124001Skin · wornRT FUSELAGE SKIN AREA AT STA 187.00 AT WING STRUT ATTACH POINT HAS PREVIOUS REPAIR WORN BEYOND LIMITS. INSTALLED FUSELAGE SKIN REPAIR IAW FAA FORM 8110-3 DATED 1-13-13 AND DWG HAS-208-53-02.Jan 8, 2013 · N208SD · Cessna 208B · Fuselage Main, Plate/Skin SDR EPUA2012032901Unknown · odorA BURNING ODOR WAS REPORTED IN ACFT. MX COULD NOT DUPLICATE ANY BURNING ODOR ON THE GROUND. SUBSEQUENT FLIGHT CHECK SHOWED NORMAL CONDITIONS, NO BURNING ODOR WAS PRESENT.Mar 27, 2012 · N208SD · Cessna 208B · Air Distribution System SDR EPUA1553692Skin · chafedABRASION ON LT INBOARD WING SKIN CAUSED FROM LT INBOARD WING/FUSELAGE FAIRING. LOCATED LEFT WING STATION 35 TO 35.5 INCHES FROM TRAILING EDGE, EXTENDING FORWARD 11 INCHES.Feb 1, 2010 · N208SD · Cessna 208B · Wing, Plate/Skin