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N356PH

Cancelled 2014

Deregistered aircraft · 1997 Dehavilland DHC-8-202 · Pratt & Whitney Canada PW123D

Open in FAA registry

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Cancelled: June 16, 2014
Status when cancelled: Valid registration
Serial number: 502
Year built: 1997
Type: Fixed wing multi engine
Engine: Turbo-prop
Airworthiness: Experimental, crew training, market survey
Airworthiness date: May 20, 2013
Certificate issued: September 19, 2012
Last registry action: September 19, 2012
Mode S code: A3FC64
Owner when cancelled: Airborne Services Global II LLC
Location: Sparks, NV
Owner type: Corporation

Airframe modelDehavilland DHC-8-202TCDS A13NM · ADs, bulletins and aircraft registered now Engine modelPratt & Whitney Canada PW123DTCDS E20NE · Turbo-prop

From the FAA registry file of October 28, 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 N356PH and the event date: up to this one’s cancellation.

Incident 20001127031519IDescent · Medford, OR(-23) On November 27, 2000, horizon air flight 2249, inbound to Medford, OR. From seattle, WA. Received a terrian-terrian waring from the GPWS on descent into Medford. The a/c was approx. 20 nw of Medford descending 6200 feet MSL. The crew responded…Nov 27, 2000

Service difficulty reports · 206

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

SDR QXEA200800427Indicator · failedPDX- FLIGHT 2011, RETURNED TO THE FIELD FOR A NR 1 ENGINE TORQUE SURGE. ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE PRESSURE TRANSDUCER WITH NO HELP. THEN REPLACED THE PRESSURE INDICATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVIApr 25, 2008 · N356PH · Dhav DHC8202 · Engine BMEP/Torque Indicating SDR QXEA200800348Flap Track · wornPDX-C5 CHECK- LT NR 3 FLAP TRACK HAS SEVERAL AREAS OF WEAR ON THE LOWER HORIZONTAL TRACK UPPER SURFACE APPROX .500 INCHES BY .300 INCHES BY .010 DEEP. BLENDED AFFECTED AREAS ON NR 3 FLAP TRACK LOWER HORIZONTAL UPPER IAW RD8-57-987. HFEC INSPECTED BLENDED AREMar 30, 2008 · N356PH · Dhav DHC8202 · Trailing Edge Flaps SDR QXEA200800352Skin · corrodedUPPER COMM ANTENNA HAS CORROSION ON MOUNTING AREA ON ACFT SKIN. REMOVED LIGHT CORROSION IAW CPC MANUAL CHAPTER 4 AND SRM 51-20-11. NO MEASURABLE MATERIAL REMOVED. (S)Mar 30, 2008 · N356PH · Dhav DHC8202 · Fuselage Main, Plate/Skin

See all 206 reports