# N805WP: 1993 Dehavilland DHC-8-103, registration cancelled 2023-03-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 4, 2023
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Dehavilland DHC-8-103](https://openairdocs.org/model/dehavilland-dhc-8-103) (registry code 2809006)
- Engine: [Pratt & Whitney Canada PW120](https://openairdocs.org/engine/pratt-whitney-canada-pw120) (registry code 52114)
- Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 353
- Year built: 1993
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: March 3, 1993
- Certificate issued: November 5, 2013
- Last registry action: October 14, 2019
- Mode S code: AAF672
- Owner when cancelled: [Dynamic Avlease Inc](https://openairdocs.org/faa-owner/DYNAMIC%20AVLEASE%20INC)
- Location: [Bridgewater, VA](https://openairdocs.org/faa-place/VA/Bridgewater)
- Owner type: Corporation
- Owner's area on the map: 38.3781° N, 79.0272° W: Placed by OpenAirDocs at the center of ZIP code 22812, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N805WP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=805WP
- Page: https://openairdocs.org/deregistered/N805WP-2023-03-04

From the FAA registry file of November 5, 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-8-103: https://openairdocs.org/model/dehavilland-dhc-8-103.md

## Service difficulty reports (45)

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

- [SDR KPVA2013031201](https://openairdocs.org/sdr/KPVA2013031201), Mar 8, 2013: REPAIR. CRACKED. DURING A SCHEDULED MAINTENANCE INSPECTION IN THE NOSE WHEEL AREA, A CRACK WAS DISCOVERED ON AN EXISTING REPAIR ANGLE "B" AT STA X97.00. INFORMATION SENT TO BOMB
- [SDR KPVA201206](https://openairdocs.org/sdr/KPVA201206), Apr 30, 2012: STRAP. CRACKED. CRACK STRAPS (PN: 85711250 & PN: 85711248) ON STR 15 ON THE RT LOWER WING SKIN PANEL BTW YW189.9-YW207.0. REPAIRED PER BOMBARDIER RD 8-57-5485.
- [SDR KPVA 201110](https://openairdocs.org/sdr/KPVA%20201110), Sep 11, 2011: TURBINE BLADES. DRAGGING. LT PROP NOT SPINNING FREELY. MAINTENANCE BORESCOPED THE 1ST STAGE POWER TURBINE (PT) AND DISCOVERED THE PT BLADES RUBBING AT LOWER BLADE ROOTS CAUSING THEM TO W
- [SDR KPVA20110816001](https://openairdocs.org/sdr/KPVA20110816001), Aug 16, 2011: STRAP. CRACKED. LT WING STRINGER 14 AT STA YW 196 STRAP PN 85711248 CRACKED.
- [SDR KPVA 201108](https://openairdocs.org/sdr/KPVA%20201108), Aug 16, 2011: STRAP. CRACKED. LT WING STRINGER 14 AT STATION YW 196 STRAP PN 85711250 IS CRACKED.
- [SDR KPVA 2010 02](https://openairdocs.org/sdr/KPVA%202010%2002), Jul 4, 2010: PROPELLER. OVERSPEED. WHILE DEPARTING RUNWAY 05 FROM MKK EXPERIENCED OVERSPEED ON NR 2 PROPELLER ON CLIMBOUT. COMPLETED APPLICABLE CHECK LISTS, DECLARED AN EMERGENCY WITH MKK TOWER A
- [SDR KPVA 2009-03](https://openairdocs.org/sdr/KPVA%202009-03), Feb 14, 2009: WARNING SYSTEM. FALSE ACTIVATION. PIREP - ON TAKEOFF ROLL; ROLL SPOILER INBOARD GROUND, ROLL SPOILER OUTBOARD GROUND CAUTION LIGHTS ILLUMINATED. MX PERFORMED OPERATIONAL TEST ROLL SPOILER SYSTEM
- [SDR KPVA200718](https://openairdocs.org/sdr/KPVA200718), Oct 28, 2007: TIRE. FLAT. (PIREP) UPON DEPARTURE IN JHM, VIOLENT SHAKING FROM NOSE. TAXI CLEAR, REALIZED 2 NOSEWHEEL TIRES FLAT. (MX) REMOVED AND REPLACED NLG WHEEL ASSY NR 1 & 2 IAW DHC
- [SDR KPVA200621](https://openairdocs.org/sdr/KPVA200621), Oct 11, 2006: ENGINE. SMOKE. SMOKE IN COCKPIT AND CABIN IN FLIGHT. (MX) MAINT DETERMINED THE CAUSE WAS FROM ENGINE BLEEDS AND AUTHORIZED A FERRY FLIGHT WITH BLEEDS OFF, BACK FOR MAINTENANCE
- [SDR 20069](https://openairdocs.org/sdr/20069), Apr 27, 2006: WARNING LIGHT. LOW PRESSURE. (PIREP) NR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED DURING CLIMBOUT. GAUGE INDICATED LESS THAN 20 PSI WHILE IN FLIGHT. AFTER ABOUT 1 MINUTE, GAUGE STARTE
- [SDR KPVA20065](https://openairdocs.org/sdr/KPVA20065), Feb 20, 2006: SKIN. GROUND DAMAGE. COMMISSARY CART HIT AIRCRAFT, MADE A 4 INCH HOLE NEAR THE EXTERNAL POWER RECEPTACLE. REPAIRED FWD PUNCTURE AT STA X136.8 - X151.6 BETWEEN STRINGERS 24P AND 26P 
- [SDR 200514](https://openairdocs.org/sdr/200514), Sep 18, 2005: SMOKE DETECTOR. INTERMITTENT. (MX) SMOKE AND MASTER WARNING LIGHTS INTERMITTENT DURING TEST OF NR 2 BAGGAGE SMOKE DETECTOR. REMOVED AND REPLACED NR 2 BAGGAGE SMOKE DETECTOR. INSTALLED CONNEC
- [SDR KPV2005F00002](https://openairdocs.org/sdr/KPV2005F00002), Aug 8, 2005: PCU. FAILED. DURING TAXI OUT NR 1 BETA LIGHT CAME ON WITH THE POWER LEVERS ABOVE FLIGHT IDLE. RETURNED TO GATE. REPLACED NR1 PCU, OPERATIONALLY CHECKS GOOD. (K)
- [SDR 200510](https://openairdocs.org/sdr/200510), Jul 30, 2005: INDICATOR. STUCK. ON TAKEOFF, NR 2 TQ GAUGE STUCK AT 68 PERCENT TQ INDICATION ON BOTH ANALOG AND DIGITAL INDICATIONS. GAUGE STUCK EVEN AFTER ENGINE SHUT DOWN. PERFORMED POWER RUN
- [SDR 20058](https://openairdocs.org/sdr/20058), Jun 24, 2005: LINE. LEAKING. NR 2 HYD SYSTEM LEAK. NR 2 HYD AND NR 2 ENG HYD PUMP LIGHTS ILLUMINATED. FOUND A LEAK IN NLG WHEEL WELL BEHIND THE DEBRIS GUARD ON LINE (P/N 82910010-207) WHICH
- [SDR 20051](https://openairdocs.org/sdr/20051), Mar 17, 2005: PACKING. CUT. NR 1 HYD SYSTEM FAILURE (ISO VALVE). CAUTION PANEL DID NOT HAVE NR 1 ISO VALVE CAUTION LIGHT, ONLY A LINE. EMERGENCY LANDING OGG. ENGINE SHUT DOWN ON RUNWAY. IN
- [SDR 200412](https://openairdocs.org/sdr/200412), Jun 25, 2004: ENGINE. FOD. NR 1 ENGINE PCE 120692, LP IMPELLER FOD DAMAGED BEYOND LIMITS (ENGINE CHANGE). REMOVED AND REPLACED NR 1 ENGINE WITH PCE 120107 IAW FORM AIAM-105. PERFORMANCE E
- [SDR 200411](https://openairdocs.org/sdr/200411), Jun 24, 2004: ENGINE. MALFUNCTIONED. (PIREP) JUST AS THE GEAR FULLY RETRACTED, THE NR 1 ENGINE TORQUE DROPPED 10 PERCENT, ACCOMPANIED BY A LOW HUMMING NOISE. ALL OTHER INDICATIONS NORMAL, NOISE CEA
- [SDR KPVA200338](https://openairdocs.org/sdr/KPVA200338), Sep 20, 2003: POWER SUPPLY. INOPERATIVE. HNL - RIGHT AFT EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT 3351-PS4 IAW DHC-8 CMM CHAP 33-50-67. OPS CHECK GOOD IAW DHC-8 CHAP 33
- [SDR KPVA200329](https://openairdocs.org/sdr/KPVA200329), Jun 21, 2003: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS INOPERATIVE, PS2. REMOVED AND REPLACED POWER SUPPLY PS2 IAW DHC MM 33-51-00 PAGE 201-22 SECT 1A. OPS CHECK GOOD IAW DHC MM 33-51-00 PAGE 201-20
- [SDR KPVA200327](https://openairdocs.org/sdr/KPVA200327), Jun 9, 2003: BATTERY PACK. WEAK. PORTABLE EMERGENCY EXIT LIGHT BATTERY WEAK. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT. OPS CHECK GOOD IAW DHC 8 MM 33-51-00 PAGE 201-202. NO DEFECTS NOTED. 
- [SDR 2003F00355](https://openairdocs.org/sdr/2003F00355), May 9, 2003: SMOKE DETECTOR. MALFUNCTIONED. SMOKE WARNING LIGHT ON WHILE ON GROUND. TROUBLESHOT SYSTEM, FOUND TOP SMOKE DETECTOR TO BE FAULTY. DISCONNECTED CONNECTOR AND SECURED. DEFERRED PER MEL 26-8-1. 
- [SDR KPVA200315](https://openairdocs.org/sdr/KPVA200315), Mar 20, 2003: LIGHT. MALFUNCTIONED. FOUND COCKPIT PORT EMERGENCY LIGHT DIM. REMOVED AND REPLACED LIGHT. (M)
- [SDR 2003F00378](https://openairdocs.org/sdr/2003F00378), Mar 19, 2003: LIGHT. MALFUNCTIONED. PORTABLE EMERGENCY LIGHT DIM. REMOVED PORTABLE EMERGENCY LIGHT AND RE-INSTALLED SERVICEABLE PORTABLE EMERGENCY LIGHT BY RESECURING INTO LOCKING SOCKET. (M)
- [SDR 2003F00377](https://openairdocs.org/sdr/2003F00377), Mar 19, 2003: BOOT. SEPARATED. FOUND LEFT LEADING EDGE DE-ICE BOOT SEPARATED FROM LEADING EDGE. RE-SEALED LEFT LEADING EDGE 513BL DE-ICE BOOT IAW MM 30-10-46 PAGE 225-230. (M)
- [SDR 2003F00376](https://openairdocs.org/sdr/2003F00376), Mar 19, 2003: WHEEL. WORN. NR 4 MLG WHEEL ASSEMBLY WORN. REMOVED AND REPLACED NR 4 MAIN WHEEL ASSEMBLY IAW DHC8MM 32-41-11 PAGE 201-205. COMPLIED WITH MM INSPECTION AND NO DEFECTS NOTED. 
- [SDR 2003F00374](https://openairdocs.org/sdr/2003F00374), Mar 19, 2003: BOOT. CORRODED. DE-ICE BOOT LEADING EDGE 513BL SURFACE CORROSION ALONG TRAILING EDGE TOP AND BOTTOM, LEFT SIDE. REMOVED SURFACE CORROSION AND TREATED. APPLIED PAINT, COATING IA
- [SDR KPVA200313](https://openairdocs.org/sdr/KPVA200313), Mar 7, 2003: SIGNAL COND UNIT. MALFUNCTIONED. HNL - FLT 1550 - DURING AND AFTER TAKEOFF, AUTO FEATHER DE-SELECTED BUT ARM LIGHT STILL ILLUMINATED. WHEN POWER REDUCED BELOW 80 PERCENT ARM LIGHT OUT, ABOVE 80
- [SDR KPVA200311](https://openairdocs.org/sdr/KPVA200311), Feb 27, 2003: LIGHT. INOPERATIVE. COCKPIT PORTABLE EMERGENCY LIGHT DIM. REMOVED AND REPLACED PORT EMERGENCY EXIT LIGHT ASSEMBLY AND SECURED IN HOLDING ASSEMBLY AND LATCHED. OPS CHECKED GOOD IAW 
- [SDR KPVA200310](https://openairdocs.org/sdr/KPVA200310), Feb 25, 2003: BATTERY. INOPERATIVE. COCKPIT PORTABLE EMERGENCY LIGHT BATTERY WEAK. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT. OPERATIONAL CHECK OF SYSTEM GOOD. WORK IAW MM.
- [SDR KPVA20036](https://openairdocs.org/sdr/KPVA20036), Feb 13, 2003: BATTERY. WEAK. HNL - PORT EMERGENCY EXIT LIGHT BATTERY WEAK. REMOVED AND REPLACED PORT EMERGENCY EXIT LIGHT. OPS CHECK GOOD IAW DHC-8 MM 33-51-00 PAGE 201-202. NO DEFECTS NOTE
- [SDR KPVA20034](https://openairdocs.org/sdr/KPVA20034), Jan 27, 2003: BATTERY PACK. INOPERATIVE. RIGHT FORWARD EMERGENCY EGRESS LIGHT, RIGHT FORWARD EMERGENCY DOOR EXIT LIGHT AND FORWARD 2ND CEILING EMERGENCY LIGHT INOPERATIVE DURING OP CHECK OF EMERGENCY L
- [SDR KPVA200243](https://openairdocs.org/sdr/KPVA200243), Dec 25, 2002: LENS. DISLODGED. EXIT SIGN FELL OFF. RESECURED EXIT SIGN OVER GALLEY BY PUSHING INTO POSITION. SECURITY CHECK OF INSTALLATION GOOD.
- [SDR KPVA200242](https://openairdocs.org/sdr/KPVA200242), Dec 25, 2002: LIGHT. LOOSE. EMERGENCY EXIT LIGHT/SIGN BY SEAT 1E, LOOSE. C/A: REMOVED AND REPLACED EMERGENCY EXIT LIGHT/SIGN IAW MM. OPS CHECK GOOD IAW MM.
- [SDR 2003F00158](https://openairdocs.org/sdr/2003F00158), Nov 26, 2002: BLADE. CRACKED. FOUND CRACK ON NR 1 BLADE OF NR 2 ENGNE PROP ASSEMBLY. REMOVED NR 1 BLADE OF NR 2 ENGINE PROP ASSEMBLY IAW HAMILTON SUNDSTRAND MM 61-10-00, PATE 307-311 PARA 5A
- [SDR KPVA200236](https://openairdocs.org/sdr/KPVA200236), Nov 26, 2002: BLADE. CRACKED. MAINTENANCE FOUND CRACK ON NR 1 BLADE OF NR 2 ENGINE PROP ASSY. REMOVED NR 1 BLADE OF NR 2 ENGINE PROP ASSY IAW HAMILTON SUNDSTRAND MM 61-10-00, PAGE 307-311 PA
- [SDR KPVA200235](https://openairdocs.org/sdr/KPVA200235), Nov 21, 2002: CIRCUIT CARD. FAULTY. HNL - FLT 1139 - EMERGENCY LIGHTS COME ON WHEN SELECTED TO OFF POSITION AND STAY ON. ATTEMPTED TO RECYCLED SAME RESULTS. THE ONLY WAY TO TURN THEM OFF IS IN THE
- [SDR KPVA200225](https://openairdocs.org/sdr/KPVA200225), Sep 17, 2002: LIGHT. INOPERATIVE. PORTABLE EMERGENCY LIGHT ABOVE COCKPIT DOOR INOPERATIVE. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT ABOVE COCKPIT DOOR. OPS CHECK GOOD IAW DHC MM 33-51-00 PA
- [SDR KPV2002F00003](https://openairdocs.org/sdr/KPV2002F00003), May 16, 2002: CONTROL CABLE. FRAYED. NOSE WHEEL ALT EXTENSION CABLE FRAYED. REMOVED AND REPLACED NOSE WHEEL ALT EXTENSION HANDLE CABLE, RIGGED NLG ALT EXTENSION RELEASE CONTROL IAW DHC 8 MM. OPS CH
- [SDR KPVA200116](https://openairdocs.org/sdr/KPVA200116), Jul 26, 2001: CONTROL BOX. FAILED. HNL - FLT 1639 - EMERGENCY LIGHTS WILL NOT TURN OFF EXCEPT IN 'ARMED' POSITION WITH BATTERY POWER ON. TROUBLE SHOT SYSTEM AND DETERMINED THE SYSTEM CONTROL BOX 
- [SDR 20001122SH005](https://openairdocs.org/sdr/20001122SH005), Sep 22, 2000: BATTERY. INOPERATIVE. HNL - OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 4. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY 3351 PS4 AT AFFECTED POSITIONS. SYSTEMS OPS CHECKED 
- [SDR KPVA200026](https://openairdocs.org/sdr/KPVA200026), Jul 19, 2000: BATTERY. DISCHARGED. HNL - EMERGENCY LIGHT BATTERIES INOPERATIVE AT POSITIONS 2 AND 4, S/N 1351 AND 1998. REMOVED AND REPLACED BATTERY PACK AND AFFECTED POSITIONS. SYSTEMS OPS CHECK
- [SDR 99ZZZM369](https://openairdocs.org/sdr/99ZZZM369), May 27, 1999: SENSOR. OUT OF ADJUST. HNL - FLT 1552 - CLIMBING THROUGH 6500-7500 FT, THE AIRCRAFT WAS PRESSURIZED, THE MASTER WARNING LIGHT ILLUMINATED CONCURRENTLY WITH THE 'PASS DOOR' WARNING LIG
- [SDR 99ZZZM35](https://openairdocs.org/sdr/99ZZZM35), Dec 27, 1998: BATTERY. DISCHARGED. HNL - DISCREPANCY FOUND DURING MAINTENANCE DAILY INSPECTION, CABIN EMERGENCY LIGHTS DID NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERIES.
- [SDR 99ZZZX153](https://openairdocs.org/sdr/99ZZZX153), Sep 29, 1998: LIGHT. MALFUNCTIONED. HNL - DURING PRE-FLIGHT INSPECTION ACCOMPLISHED BY THE FLIGHT CREW, THE PORTABLE EMERGENCY LIGHTS WOULD NOT EXTINGUISH WITH THE EMERGENCY LIGHT SWITCH LOCATED I

## 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 20100727044149I](https://openairdocs.org/incident/20100727044149I), Jul 27, 2010: Dehavilland DHC-8-103 (N805WP), Kahululi, HI, Minor damage. Airport authority changed the arrival gate due to ramp maintenance. New gate did not have stop markings for DHC-8-100. The guide man was told to use a crack in…

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