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N358PH

Cancelled 2019

Deregistered aircraft · 1998 Dehavilland DHC-8-202 · Pratt & Whitney Canada PW123

Open in FAA registry

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Cancelled: January 28, 2019
Exported to: Guernsey
Status when cancelled: Valid registration
Serial number: 506
Year built: 1998
Type: Fixed wing multi engine
Engine: Turbo-prop
Airworthiness: Standard, transport
Airworthiness date: January 29, 1998
Certificate issued: October 18, 2011
Last registry action: May 9, 2018
Mode S code: A403D2
Owner when cancelled: Wells Fargo Trust Co Na Trustee
Location: Salt Lake City, UT
Owner type: Corporation

Airframe modelDehavilland DHC-8-202TCDS A13NM · ADs, bulletins and aircraft registered now Engine modelPratt & Whitney Canada PW123TCDS E20NE · Turbo-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.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N358PH and the event date: up to this one’s cancellation.

Incident 20020212004289IDescent · Redmond, OR(-23) During descent to rdm, smoke entered cabin with lav smoke alarm sounding. Flight initiated smoke evacuation procedures and notifed CFR@rdm. Aircraft landed at rdm without further incident. Smoke was dissipated at landing. Maintenance performed borescope…Feb 12, 2002

Service difficulty reports · 429

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

SDR A8ZR20180817001Skin · dentedDENT FOUND AT BS331, STRINGER 31L. REFORMED THE DENT AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 42-2018-061, REV. A.Aug 11, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin SDR A8ZR20180823007Striker · out of limitsACCOMPLISHED RE-CONTOUR OF NR 2 ENGINE I/B COWL DOOR NACELLE STRIP-STRIKER FOR THE UPPER EDGE OF THE DOOR IAW EA 43-2018-083, REV A.Jun 27, 2018 · N358PH · Dhav DHC8202 · Nacelle/Pylon, Main Frame SDR A8ZR20180821002Skin · dentedDENT ON FUSELAGE AT STA 328.5 & S13P+6" THAT MEASURES .50"L X .9"W X .006"D SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR WITH NO OFFSETS TO MATERIAL THICKNESS. CONSIDRERED ACCEPTABLE REF STS EA 42-2018-055 REV B DATED 04/19/2018.May 7, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin

See all 429 reports