# N345PH: 1997 Dehavilland DHC-8-202, registration cancelled 2008-11-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 25, 2008
- Exported to: Canada
- Status when cancelled: Triennial form not returned
- Airframe: [Dehavilland DHC-8-202](https://openairdocs.org/model/dehavilland-dhc-8-202) (registry code 2809007)
- Engine: [Pratt & Whitney Canada PW123](https://openairdocs.org/engine/pratt-whitney-canada-pw123) (registry code 52129)
- Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 476
- Year built: 1997
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: December 8, 1998
- Certificate issued: June 13, 1997
- Last registry action: November 18, 2008
- Mode S code: A3D12E
- Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N345PH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=345PH
- Page: https://openairdocs.org/deregistered/N345PH-2008-11-25

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 (217, newest 50)

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

- [SDR QXEA2008112401195](https://openairdocs.org/sdr/QXEA2008112401195), Nov 20, 2008: BLEED VALVE. MALFUNCTIONED. PDX - NR 2 TORQUE INCREASED EXCESSIVELY. TAKEOFF ABORTED AT LOW SPEED (BELOW 60KTS) AIRCRAFT YAWED ACCORDING TO DIFFERENTIAL POWER. RETURNED TO THE GATE. REPLAC
- [SDR QXEA200800917](https://openairdocs.org/sdr/QXEA200800917), Aug 17, 2008: UNKNOWN. UNKNOWN. PDX - FLIGHT 2129. FLIGHT ATTENDANT REPORTS A "FOG" COMING FROM THE LAST 3 ROWS FROM ENG START THROUGH 10,000, THEN DISAPPEARED. MAINTENANCE PERFORMED A GROUND 
- [SDR QXEA200800698](https://openairdocs.org/sdr/QXEA200800698), Jun 29, 2008: SPRING. BROKEN. SEA - FLIGHT 2100. AFTER DEPARTURE, NOISE NOTED AFTER GEAR RETRACTION. TOWER REPORTED NOSE GEAR DOORS OPEN. RETURNED TO FIELD. UNEVENTFUL LANDING. FOUND RT FWD 
- [SDR QXEA200800651](https://openairdocs.org/sdr/QXEA200800651), Jun 16, 2008: LAMP. INOPERATIVE. PDX - AUX BATTERY AND EMERGENCY DISARM LIGHTS DIM. REPLACED LAMPS, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (A)
- [SDR QXEA200800454](https://openairdocs.org/sdr/QXEA200800454), May 7, 2008: POTENTIOMETER. OUT OF ADJUST. SEA - AUTOFEATHER SLOW TO ARM. ARMS ABOUT 90 PERCENT TORQUE. MAINTENANCE PLACED ON MEL 61-2. AIRCRAFT RETURNED TO SERVICE. MEL CLEARED BY RIGGING THE ARMING POT
- [SDR QXEA200800450](https://openairdocs.org/sdr/QXEA200800450), May 5, 2008: SWITCH. LOOSE. SEA - AUTOFEATHER SWITCH APPEARS LOOSE AND TAKES LONGER THEN NORMAL TO ARM. MAINTENANCE SECURED THE SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVIC
- [SDR QXEA200800453](https://openairdocs.org/sdr/QXEA200800453), May 5, 2008: CONTROL UNIT. MALFUNCTIONED. SEA - ON TAKEOFF, ABORTED AT 70 KNOTS, DUE TO AUTOFEATHER FAILED TO ARM. RETURNED TO THE GATE. MAINTENANCE REPLACED THE TSCU AND THE AUTOFEATHER SWITCH. OPERATI
- [SDR QXEA200800429](https://openairdocs.org/sdr/QXEA200800429), Apr 26, 2008: RELAY. MALFUNCTIONED. EUG - FLIGHT 2040 - ON TAKEOFF APPROACHING 70 KNOTS, THE AUTOFEATHER ARM LIGHT DID NOT ILLUMINATE. ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REP
- [SDR QXEA200800001](https://openairdocs.org/sdr/QXEA200800001), Jan 2, 2008: POPPET VALVE. LEAKING. PDX - FUEL DRIPPING FROM THE AREA AROUND THE REFUELING DOOR. MAINTENANCE FOUND THE FUEL DRIPPING FROM THE SPR POPPET. RESEATED THE POPPET VALVE. CHECKS GOOD, NO
- [SDR QXEA200701784](https://openairdocs.org/sdr/QXEA200701784), Dec 1, 2007: WARNING LIGHT. MULTIPLE IND. PDX - AFTER STARTING THE NR 1 ENGINE THE START LIGHT REMAINED ILLUMINATED. AFTER MOVING THE START SELECTOR SWITCH MANUALLY BACK TO CENTER THE LIGHT WENT OUT. TH
- [SDR QXEA200701647](https://openairdocs.org/sdr/QXEA200701647), Nov 3, 2007: SHUTOFF VALVE. MALFUNCTIONED. SEA FLIGHT NR 2152 DURING CLIMB THROUGH 17,000, NR 1 BLEED HOT CAUTION LIGHT ILLUMINATED. CYCLING ON AND OFF. CAUTION LIGHT EXTINGUISHED AFTER SELECTING FLOW SE
- [SDR QXEA200701646](https://openairdocs.org/sdr/QXEA200701646), Nov 2, 2007: WARNING SYSTEM. FALSE ACTIVATION. PDX FLIGHT NR 2058 - DURING CLIMB-OUT, NR 1 BLEED HOT CAUTION MESSAGE. PER CHECKLIST TURNED BLEED SELECTOR TO MIN LIGHT STOPPED CYCLING. PERFORMED BLEED AIR FUN
- [SDR QXEA200701475](https://openairdocs.org/sdr/QXEA200701475), Sep 26, 2007: SKIN. CRACKED. C5 PDX - ON NR 1 NACELLE SKIN AT THE FORWARD INBOARD CUTOUT RADIUS FOR THE FORWARD GEAR DOOR. THE NACELLE SKIN IS CRACKED 1/4" LONG. REPAIRED IAW RD8-54-873.
- [SDR QXEA200701482](https://openairdocs.org/sdr/QXEA200701482), Sep 23, 2007: DRAG STRUT. CHAFED. C5 PDX - RIGHT DRAG STRUT INBOARD ATTACH POINT IS CHAFED. REPAIRED IAW SRM 51-20-26.
- [SDR QXEA200701478](https://openairdocs.org/sdr/QXEA200701478), Sep 23, 2007: SEAT TRACK. DAMAGED. C5 PDX - LEFT INBOARD SEAT TRACK HAS WEAR DAMAGE, BOTTOM OF TRACK FRAME STATION X445 - X435/ Y9.2. REPAIRED IAW RD8-53-1339.
- [SDR QXEA200701477](https://openairdocs.org/sdr/QXEA200701477), Sep 23, 2007: SEAT TRACK. DAMAGED. C5 PDX - RIGHT INBOARD SEAT TRACK HAS WEAR DAMAGE, BOTTOM OF TRACK FRAME STATION X445 - X435/Y9.2. REPAIRED IAW RD8-53-1339.
- [SDR QXEA200701476](https://openairdocs.org/sdr/QXEA200701476), Sep 23, 2007: SEAT TRACK. DAMAGED. C5 PDX - RIGHT INBOARD SEAT TRACK HAS WEAR DAMAGE, BOTTOM OF TRACK FRAME STATION X507 - X516 Y9.2. REPAIRED IAW RD8-53-1339.
- [SDR QXEA200701458](https://openairdocs.org/sdr/QXEA200701458), Sep 23, 2007: SEAT TRACK. CORRODED. C5 PDX - CORROSION ON NR 9 SEAT TRACK AT STATION X597.5. REPAIRED IAW RD8-53-784.
- [SDR QXEA200701455](https://openairdocs.org/sdr/QXEA200701455), Sep 23, 2007: SEAT TRACK. DAMAGED. C5 PDX - LEFT INBOARD SEAT TRACK HAS WEAR DAMAGE, BOTTOM OF TRACK FRAME AT STATION X507 - X516/Y9.2. REPAIRED IAW RD8-53-1339.
- [SDR QXEA200701454](https://openairdocs.org/sdr/QXEA200701454), Sep 23, 2007: SEAT TRACK. DAMAGED. C5 PDX - RIGHT INBOARD SEAT TRACK HAS WEAR DAMAGE, BOTTOM OF TRACK FRAME STATION X473 - 484. REPAIRED IAW RD8-53-1339.
- [SDR QXEA200701474](https://openairdocs.org/sdr/QXEA200701474), Sep 22, 2007: WEB. CORRODED. C5 PDX - MTX REQUEST - CORROSION ON WEB MATING SURFACE TO STRINGER 24L FROM STATION X487 TO X501. REPAIRED IAW SRM 51-20-11, 51-40-11.
- [SDR QXEA200701472](https://openairdocs.org/sdr/QXEA200701472), Sep 21, 2007: SKIN. CORRODED. C5 PDX - X487 AND STRINGER 23L FORWARD OF FRAME AND UNDERSIDE THERE IS CORROSION IN 3 SPOTS. REPAIRED IAW SRM 51-20-11, 51-20-36.
- [SDR QXEA200701471](https://openairdocs.org/sdr/QXEA200701471), Sep 21, 2007: SKIN. CORRODED. C5 PDX - X487 STRINGER 23L THERE IS CORROSION FORWARD OF FRAME AT ATTACH CLIP. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-20-26.
- [SDR QXEA200701468](https://openairdocs.org/sdr/QXEA200701468), Sep 21, 2007: SKIN. CORRODED. C5 PDX - SKIN CORROSION AT NR 1 DME ANTENNA MOUNT LOCATED JUST AFT OF NOSE GEAR AT STATION 110 LT SIDE OF CENTER. REPAIRED IAW RD8-53-5384 AND RD8-53-9800, AND 
- [SDR QXEA200701457](https://openairdocs.org/sdr/QXEA200701457), Sep 21, 2007: SEAT TRACK. CORRODED. C5 PDX - CORROSION ON NR 1 SEAT TRACK AT STATION X342. REPAIRED IAW RD8-53-1342, SRM 51-40-00.
- [SDR QXEA200701469](https://openairdocs.org/sdr/QXEA200701469), Sep 20, 2007: SKIN. CORRODED. C5 PDX - AT STRINGER 23L X511 THERE IS CORROSION SHOWING AROUND A RIVET HEAD. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-20-26.
- [SDR QXEA200701466](https://openairdocs.org/sdr/QXEA200701466), Sep 20, 2007: STRINGER CLIP. CORRODED. C5 PDX - STRINGER 23L CLEAT IS CORRODED FORWARD SIDE OF FRAME 424.124 AT STATION X419-X422. REPAIRED IAW SRM 51-20-11, 51-40-11.
- [SDR QXEA200701473](https://openairdocs.org/sdr/QXEA200701473), Sep 20, 2007: FRAME. DAMAGED. C5 PDX - NR 2 NACELLE, FRAME FITTING FOR FORWARD MAIN LANDING GEAR DOOR, AFT HINGE ARM SUPPORT RIB HAS ONE FASTENER HOLE BLOWN OUT. REPAIRED IAW SRM 51-40-11.
- [SDR QXEA200701470](https://openairdocs.org/sdr/QXEA200701470), Sep 20, 2007: STRINGER. CORRODED. C5 PDX - AT STRINGER 23L X492 THERE IS CORROSION AT A RIVET HEAD. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-20-26.
- [SDR QXEA200701465](https://openairdocs.org/sdr/QXEA200701465), Sep 20, 2007: STRINGER. CORRODED. C5 PDX - STRINGER 24L CLEAT IS CORRODED AFT SIDE OF FRAME 424.124 AT STATION X426-X429. REPAIRED IAW SRM 51-20-11, 51-40-11.
- [SDR QXEA200701464](https://openairdocs.org/sdr/QXEA200701464), Sep 20, 2007: ARM. DAMAGED. C5 PDX - RIGHT NACELLE CUTOUT FOR FORWARD MAIN LANDING GEAR DOOR AFT HINGE ARM HAS DENT AND GOUGE IN SUPPORT RIB, AFT SIDE OF OPENING. REPAIRED IAW SRM 51-20-11
- [SDR QXEA200701467](https://openairdocs.org/sdr/QXEA200701467), Sep 19, 2007: STRINGER CLIP. CORRODED. C5 PDX - STRINGER 24L CLEAT IS CORRODED AFT SIDE OF FRAME 387.350 AT STATION X389-X392. REPAIRED IAW SRM 51-20-11, 51-40-11.
- [SDR QXEA200701459](https://openairdocs.org/sdr/QXEA200701459), Sep 19, 2007: FIREWALL. CRACKED. C5 PDX - THERE IS A CRACK IN THE RIGHT FIREWALL ABOUT 2" LONG JUST ABOVE AND INBOARD OF THE RIGHT ENGINE FIRE EXTINGUSHING LINE. REPAIRED IAW RD8-54-2396.
- [SDR QXEA200701462](https://openairdocs.org/sdr/QXEA200701462), Sep 19, 2007: SUPPORT BRACKET. CHAFED. C5 PDX - RIGHT NACELLE INBOARD FRAME SUPPORT BRACKET CHAFED. REPAIRED IAW SRM 51-20-51, RD8-54-2397.
- [SDR QXEA200701460](https://openairdocs.org/sdr/QXEA200701460), Sep 18, 2007: DOOR FRAME. CHAFED. C5 PDX - CHAF ON FRAME AT STATION 222 - 2100, LEFT SIDE, MAIN CABIN DOOR FORWARD SIDE. REPAIRED IAW RD8-53-9791.
- [SDR QXEA200701456](https://openairdocs.org/sdr/QXEA200701456), Sep 18, 2007: SEAT TRACK. CORRODED. C5 PDX - NUMBER 4 SEAT TRACK FLANGE CORRODED AT MAIN CABIN DOOR ENTRY. REPAIRED IAW RD8-53-4473 AND RD8-53-1102.
- [SDR QXEA200701453](https://openairdocs.org/sdr/QXEA200701453), Sep 18, 2007: SEAT TRACK. CORRODED. C5 PDX - NUMBER 7 SEAT TRACK, TOP SURFACE CORRODED FROM STATION 242 THRU 195, GALLEY AND LAV ATTACH AREA. REPAIRED IAW SRM 51-40-11, RD8-53-1102 AND RD8-53-4473
- [SDR QXEA200701463](https://openairdocs.org/sdr/QXEA200701463), Sep 17, 2007: MOUNT. DAMAGED. C5 PDX - HORIZONTAL STAB FORWARD RIGHT MOUNTING STRUCTURE HAS NICKS AND GOUGES ON OUTBOARD SIDE. REPAIRED IAW RD8-55-847, SRM 51-20-51, 51-20-16.
- [SDR QXEA200701461](https://openairdocs.org/sdr/QXEA200701461), Sep 17, 2007: MOUNT. DAMAGED. C5 PDX - HORIZONTAL STAB FORWARD MOUNT POSTS ARE SCRATCHED ON OUTBOARD SURFACE. REPAIRED IAW RD8-55-847 AND SRM 51-20-51, 51-20-16.
- [SDR QXEA200701479](https://openairdocs.org/sdr/QXEA200701479), Sep 16, 2007: SEAT TRACK. DAMAGED. C5 PDX - LEFT INBOARD SEAT TRACK HAS WEAR DAMAGE, BOTTOM OF TRACK FRAME STATION X473 - X484/ Y9.2. REPAIRED IAW RD8-53-1339.
- [SDR QXEA200701481](https://openairdocs.org/sdr/QXEA200701481), Sep 16, 2007: ANGLE. CRACKED. C5 PDX - SUSPECT CRACK IN FORWARD RIGHT CLOSING ANGLE RADIUS AT STATION X387, STRINGER 5 RIGHT UNDER PANEL 261JT. REPAIRED IAW RD8-53-5192.
- [SDR QXEA200701480](https://openairdocs.org/sdr/QXEA200701480), Sep 16, 2007: FLAP TRACK. CORRODED. C5 PDX - PITTING ON RIGHT INBOARD FLAP, LOWER SIDE OF UPPER NR 2 TRACK AT ZERO DEGREE ROLLER INDICATION. REPAIRED IAW RD8-57-986.
- [SDR QXEA200701483](https://openairdocs.org/sdr/QXEA200701483), Sep 15, 2007: ANGLE. CRACKED. C5 PDX - SUSPECT CRACK RIGHT AFT CLOSING ANGLE AT STINGER 6 RIGHT UNDER FLAP PCU. REPAIRED IAW RD8-53-5192.
- [SDR QXEA200701439](https://openairdocs.org/sdr/QXEA200701439), Sep 15, 2007: SKIN. CORRODED. C5 PDX - MAIN CABIN DOOR SHELL HAS CORROSION BY FORWARD NR 1 STOP/STEP ASSEMBLY ATTACH POINT. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-20-26.
- [SDR QXEA200701432](https://openairdocs.org/sdr/QXEA200701432), Sep 15, 2007: BRACKET. CORRODED. C5 PDX - SUSPECT CORROSION TO HORIZONTAL STRINGER/RISER BRACKET AT STRINGER 31R STATION 201. REPAIRED IAW SRM 51-40-11.
- [SDR QXEA200701436](https://openairdocs.org/sdr/QXEA200701436), Sep 14, 2007: FLOORBOARD. CORRODED. C5 PDX - FLOORBOARD FLANGE AT STATION 599.00 RIGHT END UPPER SURFACE HAS CORROSION. REPAIRED IAW SRM 51-20-11, 51-40-11, AND 51-20-16.
- [SDR QXEA200701429](https://openairdocs.org/sdr/QXEA200701429), Sep 14, 2007: STRINGER. CORRODED. C5 PDX - RIGHT STRINGER 21 HAS CORROSION ON INBOARD LEADING EDGE FLANGE AT STATION 357.70. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-20-36, AND 51-20-26.
- [SDR QXEA200701430](https://openairdocs.org/sdr/QXEA200701430), Sep 14, 2007: FRAME. CORRODED. C5 PDX - FORWARD CENTER UNDERFLOOR VERTICAL FRAME STRUCTURE AT STATION 201, STRINGER 31L. SUSPECT CORROSION UP FRONT SKIN ON AFT INBOARD CORNER OF FLOOR RISER F
- [SDR QXEA200701435](https://openairdocs.org/sdr/QXEA200701435), Sep 13, 2007: SEAT TRACK. CORRODED. C5 PDX - FLOORBOARD FLANGE TO SEAT TRACK GUSSET AT STATION 599.0 INBOARD OF LEFT INBOARD SEAT TRACK HAS CORROSION ON LOWER SURFACE AND ALONG EDGE ON FLANGE. REP
- [SDR QXEA200701434](https://openairdocs.org/sdr/QXEA200701434), Sep 13, 2007: SEAT TRACK. CORRODED. C5 PDX - FLOORBOARD NUT PLATE AND FLANGE ARE CORRODED AT STATION 599.0 INBOARD OF LEFT INBAORD SEAT TRACK. REPAIRED IAW SRM 51-40-11, 51-20-11, 51-20-36.

All 217: https://openairdocs.org/deregistered/N345PH-2008-11-25/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 19990708034389I](https://openairdocs.org/incident/19990708034389I), Jul 8, 1999: Dhav DHC8* (N345PH), Wenatchee, WA. (-23) No. 2 prop feathered without pilot command in climb. A/c returned to point of takeoff. Maint replaced prop, prop control unit and torque signal…

## Other aircraft with N345PH

- [Cancelled 2024-05-25](https://openairdocs.org/deregistered/N345PH-2024-05-25): Robinson Helicopter R66, S/N 0227, built 2012. Registration pending, canceled. Owner: [North Little Rock, AR](https://openairdocs.org/faa-place/AR/North%20Little%20Rock)

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