# N356PH: 1997 Dehavilland DHC-8-202, registration cancelled 2014-06-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 16, 2014
- Status when cancelled: Valid registration
- Airframe: [Dehavilland DHC-8-202](https://openairdocs.org/model/dehavilland-dhc-8-202) (registry code 2809007)
- Engine: [Pratt & Whitney Canada PW123D](https://openairdocs.org/engine/pratt-whitney-canada-pw123d) (registry code 52199)
- Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 502
- Year built: 1997
- Type of aircraft: Fixed wing multi engine
- Engine type: 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](https://openairdocs.org/faa-owner/AIRBORNE%20SERVICES%20GLOBAL%20II%20LLC)
- Location: [Sparks, NV](https://openairdocs.org/faa-place/NV/Sparks)
- Owner type: Corporation
- Owner's area on the map: 39.5406° N, 119.5440° W: Placed by OpenAirDocs at the center of ZIP code 89434, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N356PH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=356PH
- Page: https://openairdocs.org/deregistered/N356PH-2014-06-16

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.

ADs and bulletins for the Dehavilland DHC-8-202: https://openairdocs.org/model/dehavilland-dhc-8-202.md

## Service difficulty reports (206, newest 50)

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

- [SDR QXEA200800427](https://openairdocs.org/sdr/QXEA200800427), Apr 25, 2008: INDICATOR. FAILED. PDX- FLIGHT 2011, RETURNED TO THE FIELD FOR A NR 1 ENGINE TORQUE SURGE. ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE PRESSURE TRANSDUCER WITH NO 
- [SDR QXEA200800348](https://openairdocs.org/sdr/QXEA200800348), Mar 30, 2008: FLAP TRACK. WORN. PDX-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 A
- [SDR QXEA200800352](https://openairdocs.org/sdr/QXEA200800352), Mar 30, 2008: SKIN. CORRODED. UPPER 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 REMOVE
- [SDR QXEA200800351](https://openairdocs.org/sdr/QXEA200800351), Mar 30, 2008: SKIN. DAMAGED. BURNED RIVET AT STA X190.00 APPROX 1 INCH BELOW STR 4L. REMOVED RIVET AND FOUND DAMAGE LIMITED TO ONE RIVET ONLY. INSTALLED RIVET IAW D8-200 SRM 51-40-11. (S)
- [SDR QXEA200800347](https://openairdocs.org/sdr/QXEA200800347), Mar 30, 2008: STRUCTURE. CORRODED. PDX-C5 CHECK. CORROSION ON FLANGE AT GALLEY OUTBOARD AFT ATTACH POINT AT STA X227.70. BLENDED SURFACE CORROSION APPROX .001 MATERIAL REMOVED IAW DHC 8 200 SRM. 
- [SDR QXEA200800345](https://openairdocs.org/sdr/QXEA200800345), Mar 30, 2008: SKIN. CORRODED. PDX-C5 CHECK- AFT BAG PIT UPPER SKIN AT A LIGHTENING HOLE HAS LIGHT CORROSION FORMING IN RECESS HOLE Z100 X557 AND 27L. BLENDED OUT CORROSION AND MEASURED BLEND
- [SDR QXEA200800368](https://openairdocs.org/sdr/QXEA200800368), Mar 30, 2008: SKIN. DAMAGED. PDX-C4 CHECK - BURNT RIVET APPROX 6 INCHES AFT OF STA X160.500 & 3 INCHES OUTBOARD OF STR 4L. REPAIRED DAMAGE TO SKIN PER D8-200 RD8-53-137 PG 3 STEP 1. HFEC IA
- [SDR QXEA200800367](https://openairdocs.org/sdr/QXEA200800367), Mar 30, 2008: FLAP TRACK. WORN. PDX-C4 CHECK - LT WING NR 5 FLAP TRACK OUTBOARD LOWER TRACK UPPER SURFACE HAS WEAR MARKS. BLENDED IAW RD8-57-989. HFEC INSPECTED IAW D8-200 NDTM PART 651-00-01.
- [SDR QXEA200800357](https://openairdocs.org/sdr/QXEA200800357), Mar 30, 2008: SKIN. DENTED. PDX-C4 CHECK FOUND DENT ON THE BOTTOM OF THE RT ELEVATOR AT STN YH92.20, APPROX 13 INCHES FWD OF THE AFT SPAR. FOUND OUT OF LIMITS IAW RD8-55-1448. HFEC INSP FO
- [SDR QXEA200800358](https://openairdocs.org/sdr/QXEA200800358), Mar 30, 2008: SKIN. DAMAGED. PDX -C4 CHECK- FOUND A CREASE ON THE BOTTOM OF THE RT ELEVATOR AT STN YH94.20, APPROX 6 INCHES FWD OF THE AFT SPAR. CREASE IS APPROX 5.5 INCHES LONG. FOUND OUT 
- [SDR QXEA20080344](https://openairdocs.org/sdr/QXEA20080344), Mar 30, 2008: STRUCTURE. CORRODED. PDX C5 CHECK, AFT BAGGAGE PIT Z100 X600 AND 27R THERE IS LIGHT CORROSION FORMING TOPSIDE AND UNDERSIDE OF THE NUTPLATE. REMOVED THE NUTPLATE AND BLENDED LIGHT C
- [SDR QXEA20080343](https://openairdocs.org/sdr/QXEA20080343), Mar 30, 2008: STRUCTURE. CORRODED. PDX C5 CHECK, AFT BAGGAGE PIT HAS LIGHT CORROSION AT Z100 X 600 AND 21L UNDERSIDE AT NUTPLATE. REMOVED NUTPLATE AND BLENDED MINOR SURFACE CORROSION. BLENDED ARE
- [SDR QXEA20080342](https://openairdocs.org/sdr/QXEA20080342), Mar 30, 2008: BRACKET. LOOSE. PDX C5 CHECK - ELEVATOR BUMP STOP BRACKET IS LOOSE ON THE RIGHT SIDE WHERE IT ATTACHES TO THE HORIZ STAB. REMOVED THE JO-BOLTS AS REQUIRED. REPLACED FASTENERS P
- [SDR QXEA20080338](https://openairdocs.org/sdr/QXEA20080338), Mar 28, 2008: WARNING LIGHT. INTERMITTENT. SEA - ON TAXI, THE FIRE DETECTION LIGHT WAS FLASHING AND THE FAULT "B" LIGHT ILLUMINATED WITH A FLASHING INDICATION. RETURNED TO THE GATE AND PLACED THE SYSTEM 
- [SDR QXEA200800019](https://openairdocs.org/sdr/QXEA200800019), Jan 7, 2008: INVERTER. ODOR. PDX - FLIGHT 2172 - STRANGE ODOR FROM THE PRIMARY INVERTER. MAINTENANCE PLACED ON MEL 24-8. AIRCRAFT RETURNED TO SERVICE. REPLACED THE INVERTER. OPERATIONAL CHE
- [SDR QXEA200701588](https://openairdocs.org/sdr/QXEA200701588), Oct 20, 2007: WARNING LIGHT. FALSE ACTIVATION. RDM FLIGHT NR 2126, ON START UP NR 2 ENGINE MANUAL CAUTION LIGHT ILLUMINATED. COMPLIED WITH SUPPLEMENTAL PROCEDURE ON DASH 8 FSM PAGE 7.3.11. NO FURTHER DEFECTS
- [SDR QXEA200700799](https://openairdocs.org/sdr/QXEA200700799), May 16, 2007: PRESSURE SWITCH. MALFUNCTIONED. YVR FLIGHT NR 2035 - DURING NR 2 PROP TRANSITION FROM START/FEATHER TO 1200, RUD FULL PRESS CAUTION LIGHT INTERMITTENTLY ILLUMINATED SOMETIMES STAYING ON FOR A 
- [SDR QXEA200700715](https://openairdocs.org/sdr/QXEA200700715), May 3, 2007: COMPUTER. INOPERATIVE. PDX - ON FLIGHT 2211, ON CLIMB-OUT FO WAS HAND FLYING THE AIRCRAFT WHEN THE AUTOPILOT ENGAGED AND TURNED TO THE RIGHT. THE FO HIT THE DISENGAGE BUTTON ON THE YO
- [SDR QXEA200700521](https://openairdocs.org/sdr/QXEA200700521), Apr 7, 2007: SWITCH. FAILED. SEA - ON FLIGHT 2085, AUTO FEATHER SELECT LIGHT INDICATION FAILS TO ILLUMINATE UPON BEING DEPRESSED. MAINTENANCE REMOVED AND REPLACED THE AUTO FEATHER SWITCH. O
- [SDR QXEA200700508](https://openairdocs.org/sdr/QXEA200700508), Apr 2, 2007: LAMP. INOPERATIVE. PDX FLIGHT NR 2170, NR 2 TANK AUX PUMP LIGHT OUT. MAINTENANCE RELAMPED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200700392](https://openairdocs.org/sdr/QXEA200700392), Mar 18, 2007: UNKNOWN. UNKNOWN. PDX FLIGHT NR 2030 ON TAXI OUT, NR 1 ENGINE MANUAL CAUTION LIGHT ILLUMINATED DURING BETA BACKUP FIRST FLIGHT OF DAY CHECK. MAINTENANCE C/W REST PROCEDURE IAW AI
- [SDR QXEA200700247](https://openairdocs.org/sdr/QXEA200700247), Feb 26, 2007: STARTER GEN. MALFUNCTIONED. BOI FLIGHT NR 2192, DURING AFTER START FLOW WITH LEFT ENGINE FEATHERED WHEN TURNING MAIN BUSS TIE TO OFF AUX INVERTER CAUTION ILLUMINATED ALONG WITH SEVERAL ASS
- [SDR QXEA200602955](https://openairdocs.org/sdr/QXEA200602955), Nov 6, 2006: PUMP. MALFUNCTIONED. SEA FLIGHT NR 2162, NR 2 STANDBY HYDRAULIC PRESSURE GAUGE SHOW A READING BETWEEN 200-500 PSI. MAINTENANCE REPLACED NR 1 STANDBY HYDRAULIC PUMP UNIT IAW AMM 29-1
- [SDR QXEA200601849](https://openairdocs.org/sdr/QXEA200601849), Jul 17, 2006: CONNECTOR. DIRTY. SEA FLIGHT 2024 LEFT FUEL TEMPERATURE HIGH. MAINTENANCE CLEANED CONNECTOR. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200601730](https://openairdocs.org/sdr/QXEA200601730), Jun 30, 2006: GENERATOR. MALFUNCTIONED. SEA FLIGHT 2016, NR 2 AC GENERATOR CAUTION. MAINTENANCE REPLACED NR 2 AC GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200601215](https://openairdocs.org/sdr/QXEA200601215), May 9, 2006: PUMP. MALFUNCTIONED. PDX FLIGHT NR 2246 - NR 2 HYDRAULIC PUMP CAUTION. MAINTENANCE REPLACED THE HYDRAULIC PUMP. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200601200](https://openairdocs.org/sdr/QXEA200601200), Apr 25, 2006: STRINGER. CRACKED. PDX - C4 LEFT NACELLE FINGERNAIL DECK STRINGERS CRACKED BOTTOM SIDE AND FORWARD. REPAIRED IAW DHC-8-200 SRM 51-40-11.
- [SDR QXEA200601124](https://openairdocs.org/sdr/QXEA200601124), Apr 21, 2006: STOP. WORN. PDX - C4 MAIN CABIN DOOR AFT BOTTOM STOP ON APERTURE WORN. REPAIRED IAW RD 8-53-3933, PAGE 4, STEPS 4-7.
- [SDR QXEA200601123](https://openairdocs.org/sdr/QXEA200601123), Apr 21, 2006: STOP. WORN. PDX - C4 MAIN CABIN DOOR AFT TOP STOP GUIDE ON APERTURE WORN. REPAIRED IAW RD 8-53-3933, PAGE 4, STEPS 4-7.
- [SDR QXEA200601122](https://openairdocs.org/sdr/QXEA200601122), Apr 21, 2006: STOP. WORN. PDX - C4 MAIN CABIN DOOR FORWARD TOP STOP GUIDE ON APERATURE IS WORN. REPAIRED IAW RD 8-53-3933, STEPS 4 - 7.
- [SDR QXEA200601121](https://openairdocs.org/sdr/QXEA200601121), Apr 21, 2006: STOP. WORN. PDX - C4 MAIN CABIN DOOR FORWARD BOTTOM STOP ON APERTURE WORN. REPAIRED IAW RD 8-53-3933, PAGE 4, STEPS 4-7.
- [SDR QXEA200601184](https://openairdocs.org/sdr/QXEA200601184), Apr 20, 2006: ACCESS PANEL. CORRODED. PDX - C4 LAV ACCESS CUTOUT, THE LOWER EDGE HAS CORROSION AROUND ONE FASTENER. REPAIRED IAW DHC-8-200 SRM 51-20-11, RD 8-53-3299 AND HORIZON AIR EA 2-53-736.
- [SDR QXEA200601182](https://openairdocs.org/sdr/QXEA200601182), Apr 20, 2006: STRINGER. CORRODED. PDX - C4 THERE IS CORROSION ON STRINGER 31L ABOUT 4" FORWARD OF PILOT BULKHEAD X102.00. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-20-16, 51-20-36.
- [SDR QXEA200601189](https://openairdocs.org/sdr/QXEA200601189), Apr 19, 2006: SKIN. DENTED. PDX - C4 DENT ON LEFT FUSELAGE (UNDER LEFT ICE SHIELD) APPROXIMATELY STATION X303.0, Z156.5. REPAIRED IAW DHC-8-200 SRM 51-40-11, 51-20-16, 51-20-36, AND HORIZO
- [SDR QXEA200601199](https://openairdocs.org/sdr/QXEA200601199), Apr 19, 2006: SILL. CORRODED. PDX - C4 MAIN CABIN DOOR SILL HAS CORROSION ON UPPER AND LOWER SURFACE. REPAIRED IAW DHC-8-200 SRM 51-00-01, 51-20-16 AND 51-20-36.
- [SDR QXEA200601188](https://openairdocs.org/sdr/QXEA200601188), Apr 19, 2006: SKIN. DENTED. PDX - C4 DENT ON LEFT SIDE OF FUSELAGE (UNDER LEFT ICE SHIELD) APPROXIMATELY STATION X301.0 Z158.0. REPAIRED IAW RD 8-53-7988, DHC-8-200 SRM 51-20-16, 50-20-36,
- [SDR QXEA200601185](https://openairdocs.org/sdr/QXEA200601185), Apr 19, 2006: GALLEY TRACK. CORRODED. PDX - C4 CORROSION ON GALLEY OUTBOARD MOUNT TRACK JUST FORWARD OF RIGHT EMERGENCY DOOR, AROUND RIVET HOLES. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-20-16, 51-20
- [SDR QXEA200601193](https://openairdocs.org/sdr/QXEA200601193), Apr 18, 2006: DOOR FRAME. CORRODED. PDX - C4 CORROSION ON AFT LOWER PASSENGER DOOR FRAME. JUST FORWARD OF FRAME 253.4. REPAIRED IAW DHC-8-200 SRM 51-20-11, 2C (3), PAGE 7.
- [SDR QXEA200601119](https://openairdocs.org/sdr/QXEA200601119), Apr 18, 2006: PANEL. CHAFED. PDX - C4 REAR MATING SURFACE ON AIRCRAFT FOR PANEL 261NT HAS CHAFED AREA IN CENTER SECTION. REPAIRED IAW RD 8-57-1441 AND AMM 53-50-01.
- [SDR QXEA200601126](https://openairdocs.org/sdr/QXEA200601126), Apr 17, 2006: SKIN. CHIPPED. PDX - C4 THERE IS PAINT CHIPPING AND GOUGING WHERE THE CARGO NET HAS HIT THE FUSELAGE SKIN BETWEEN STRINGER 26L AND 27L, FUSELAGE STATION 539.00 AND 549.00. REP
- [SDR QXEA200601183](https://openairdocs.org/sdr/QXEA200601183), Apr 17, 2006: SKIN. GOUGED. PDX - C4 THERE IS GOUGING WHERE THE CARGO NRT HAS HIT THE FUSELAGE SKIN AT STRINGER 29L, FUSELAGE STATION 590.000 TO 597.000. REPAIRED IAW DHC-8-200 SRM 51-20-1
- [SDR QXEA200601125](https://openairdocs.org/sdr/QXEA200601125), Apr 16, 2006: PANEL. CHAFED. PDX - C4 RIGHT INBOARD WING LOWER INBOARD FLANGE FOR LEADING EDGE PANEL 611AR CHAFED. REPAIRED IAW RD 8-57-811, ISSUE 3, PAGE 4 STEPS 4-7.
- [SDR QXEA200601129](https://openairdocs.org/sdr/QXEA200601129), Apr 16, 2006: STRINGER. CORRODED. PDX - C4 CORROSION ON STRINGER 31 AT FRAME 202.75, FORWARD SIDE AROUND RIVETS. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-20-41.
- [SDR QXEA200601120](https://openairdocs.org/sdr/QXEA200601120), Apr 16, 2006: ATTACH ANGLE. CRACKED. PDX - C4 CENTER MOUNT ANGLE FOR WING DEICE TEE DUCT IS CRACKED AT RIGHT HAND END. REPAIRED IAW DHC-8-200 SRM 51-40-11 AND 51-40-00.
- [SDR QXEA200601118](https://openairdocs.org/sdr/QXEA200601118), Apr 16, 2006: RISER. CORRODED. PDX - C4 CARGO FLOOR RISER MACHINED DIAGONAL STIFFENER AT LOWER AFT CORNER OF DOOR OPENING, IS CORRODED ON BOTTOM SIDE AT 90 DEGREE RADIUS. REPAIRED IAW DHC-8-2
- [SDR QXEA200601194](https://openairdocs.org/sdr/QXEA200601194), Apr 15, 2006: WEB. CORRODED. PDX - C4 CORROSION AROUND SCREW HOLE ON TOP OF CARGO FLOOR WEB AT Y36L, X548. REPAIRED IAW DHC-8-200 SRM 51-20-16, 51-20-36 AND 51-20-56.
- [SDR QXEA200601195](https://openairdocs.org/sdr/QXEA200601195), Apr 15, 2006: WEB. CORRODED. PDX - C4 CORROSION AROUND SCREW HOLE ON TOP OF CARGO FLOOR WEB AT Y20L, X555. REPAIRED IAW DHC-8-200 SRM 51-20-16, 51-20-36 AND 51-20-56.
- [SDR QXEA200601191](https://openairdocs.org/sdr/QXEA200601191), Apr 15, 2006: RISER. CORRODED. PDX - C4 CARGO FLOOR RISER BOTTOM FLANGE CORRODED ON TOP FORM Y0 TO Y30, RIGHT SIDE. REPAIRED IAW DHC-8-200 SRM 51-20-16, 51-20-36 AND SRM 51-20-56.
- [SDR QXEA200601197](https://openairdocs.org/sdr/QXEA200601197), Apr 15, 2006: FITTING. CORRODED. PDX - C4 CORROSION ON UPPER CARGO FLOOR DECK AROUND SCREW HOLE JUST INBOARD OF AFT WALL BOTTOM LEFT HAND MOUNT FITTING AT Y21L, X649. REPAIRED IAW DHC-8-200 SRM
- [SDR QXEA200601190](https://openairdocs.org/sdr/QXEA200601190), Apr 15, 2006: FLOOR SUPPORT. CORRODED. PDX - C4 CORRODED NUT PLATE ON BOTTOM CARGO FLOOR SUPPORT, AFT LEFT CORNER OF 144BZ. REPAIRED IAW DHC-8-200 SRM 51-40-11, 51-20-16, 51-20-36 AND SRM 51-20-56.

All 206: https://openairdocs.org/deregistered/N356PH-2014-06-16/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20001127031519I](https://openairdocs.org/incident/20001127031519I), Nov 27, 2000: Dhav DHC8202 (N356PH), 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…

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