# N803WP: 1989 Dehavilland DHC-8-103, registration cancelled 2008-02-20

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 20, 2008
- Status when cancelled: Sale reported
- Airframe: [Dehavilland DHC-8-103](https://openairdocs.org/model/dehavilland-dhc-8-103) (registry code 2809006)
- Engine: [Pratt & Whitney Canada PW121](https://openairdocs.org/engine/pratt-whitney-canada-pw121) (registry code 52124)
- Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 141
- Year built: 1989
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: July 2, 1996
- Last registry action: December 4, 2007
- Mode S code: AAEF04
- Location: Shannon Co Clare, Ireland
- Owner type: Individual
- The mark today: https://openairdocs.org/aircraft/N803WP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=803WP
- Page: https://openairdocs.org/deregistered/N803WP-2008-02-20

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-8-103: https://openairdocs.org/model/dehavilland-dhc-8-103.md

## Service difficulty reports (28)

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

- [SDR CBR2006F00016](https://openairdocs.org/sdr/CBR2006F00016), Aug 24, 2006: SELECTOR PANEL. MALFUNCTIONED. AIR TURNBACK, IN FLIGHT, GEAR HANDLE AND RED UNSAFE LIGHT FOR NOSE GEAR FLICKERED ON 4 SEPARATE OCCASIONS. REMOVED AND REPLACED SELECTOR PANEL IAW MM. OPS CHECK
- [SDR CBR2006F00014](https://openairdocs.org/sdr/CBR2006F00014), Jun 22, 2006: ENGINE. MALFUNCTIONED. ABORTED TAKEOFF- DURING TAKEOFF ROLL, PRIOR TO V1 THE NR 2 ENGINE ITT EXCEDDED LIMITATIONS. THE ITT WAS 790 DEGREES AT 94 PERCENT TORQUE. OIL PSI WAS 65. TAKEOF
- [SDR CBR2006F00005](https://openairdocs.org/sdr/CBR2006F00005), Apr 28, 2006: GAUGE. READS HIGH. NR 2 ENGINE DID NOT REACH TARGET TAKEOFF TORQUE, BEFORE REACHING NORMAL TAKEOFF MAX ITT OF 785 DEGREES. ENGINE GROUND RUN CARRIED OUT, ALL PARAMETERS FOUND WITH
- [SDR KPVA20018](https://openairdocs.org/sdr/KPVA20018), Mar 30, 2001: POWER SUPPLY. INOPERATIVE. HNL - FOUND ON DAILY INSPECTION, EMERGENCY LIGHTS AT REAR OVERHEAD CEILING LIGHT AND LEFT AFT EGRESS LIGHT, WILL NOT COM ON DURING TEST. REMOVED AND REPLACED EM
- [SDR KPVA200039](https://openairdocs.org/sdr/KPVA200039), Nov 17, 2000: LIGHT. MALFUNCTIONED. PORTABLE EMERGENCY LIGHT FLICKER WHILE ENGINES RUNNING. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT, SYSTEM OPS CHECKED GOOD. (M)
- [SDR KPVA200038](https://openairdocs.org/sdr/KPVA200038), Nov 15, 2000: BRACKET. INOPERATIVE. HNL - FLT 1641 - EMERGENCY DOME LIGHT ON IN CRUISE. REMOVED AND REPLACED PORTABLE EMERGENCY MOUNTING BRACKET, SYSTEM OPS CHECKED GOOD. (M)
- [SDR 20001212SH005](https://openairdocs.org/sdr/20001212SH005), Nov 9, 2000: LIGHT. MALFUNCTIONED. HNL - FLT 1631 - EMERGENCY LIGHTS CAME ON DURING FLIGHT. COULD NOT TURN OFF UNLESS SWITCH WAS IN OFF POSITION, IN ARM, POSITION LIGHTS STAYED ON CONTINUOUSLY. R
- [SDR KPVA200035](https://openairdocs.org/sdr/KPVA200035), Nov 7, 2000: CONTROL BOX. FAILED. FLT 1225 - MKK - EMERGENCY LIGHTS CAME ON DURING FLIGHT. RESET, CAME ON AGAIN (3-4 TIMES). CAME ON AGAIN DURING TAXI TO TERMINAL. REMOVED AND REPLACED EMERGENCY
- [SDR KPVA200034](https://openairdocs.org/sdr/KPVA200034), Nov 3, 2000: SENSOR. FAILED. MKK-HNL - FLT 1132 - GEAR SELECTED UP, RIGHT MAIN "AMBER" DOOR LIGHT ILLUMINATED. AFTER 5-10 MINUTES, LIGHT WENT OUT. MAINTENANCE T/S GEAR DOOR INDICATION SYSTE
- [SDR KPVA200031](https://openairdocs.org/sdr/KPVA200031), Oct 21, 2000: CONTROL BOX. FAILED. FLT 1641 - HNL - EMERGENCY LIGHTS CAME ON DURING DESCENT. INSPECTED AND CLEANED CONTROL UNIT BOX, OPERATIONAL CHECK OF SYSTEM TESTED GOOD IAW MM 33-51-00 PATES 
- [SDR KPVA200024](https://openairdocs.org/sdr/KPVA200024), Mar 11, 2000: CABLE. DAMAGED. AIRSTAIR DOORINERTIAL REEL CAGED CABLE. DOOR WILL NOT OPEN. REPLACED AIR STAIR DOOR CBLE ASSEMBLY, WORK IAW MM 52-10-00 PAGE 218-219 PARA 4 ITEMS B-E. SYSTEM OP
- [SDR KPVA200003](https://openairdocs.org/sdr/KPVA200003), Feb 17, 2000: SEAT TRACK. CORRODED. FUSELAGE CABIN RIGHT INBOARD SEAT RAIL INSPECTED AND FOUND EXCESSIVE CORROSION (TASK 40,000 CYCLE CARAD 53-10-1004). REPLACED SEAT RAIL AT STATION X531-X600 WIT
- [SDR KPVA200004](https://openairdocs.org/sdr/KPVA200004), Feb 17, 2000: ANGLE. CRACKED. NOSE WHEEL WELL RIGHT SIDE ANGLE AT STATION X101 AND Z112 CRACKED. REPAIRED ANGLE AT STATION X101, Z112 IAW DHC-8 RD 8-53-3630 AND RD8-53-1672. (M)
- [SDR KPVA200005](https://openairdocs.org/sdr/KPVA200005), Feb 17, 2000: BULKHEAD. DENTED. REAR PRESSURE BULKHEAD AT STATION X653, STRINGER 11 TO 12 DENTED. REPAIRED REAR PRESSURE BULKHEAD AT STATION X653, STRINGER 11 AND 12 IAW DHC-8-RD8-53-4788. THI
- [SDR KPVA200007](https://openairdocs.org/sdr/KPVA200007), Feb 17, 2000: SPAR. DENTED. FORE RUDDER FRONT SPAR AT RIB 13 DENTED. REPAIRED RIB 13, FORE RUDDER FRONT SPAR IAW DHC-8 RD8-55-0870. (M)
- [SDR KPVA200008](https://openairdocs.org/sdr/KPVA200008), Feb 17, 2000: ANGLE. CRACKED. RIGHT NACELLE TO WING INBOARD AND OUTBOARD DRAG ANGLES CRACKED AT STATION YW171 AND YW139 XN 169. REPAIRED DRAG ANGLES AT STATIN YW171 AND YW139 XN 169 IAW RD8-
- [SDR KPVA200009](https://openairdocs.org/sdr/KPVA200009), Feb 17, 2000: ANGLE. CRACKED. LEFT NACELLE TO WING INBOARD DRAG ANGLE AT STATION YW139XN127 TO DN169 CRACKED. REPLACED NACELLE TO WING INBOARD DRAG ANGLE AT STATION YW139 XN127 TO XN169 IAW 
- [SDR KPVA200013](https://openairdocs.org/sdr/KPVA200013), Feb 17, 2000: SKIN. DEBONDED. RIGHT WING LEADING EDGE STATION 613BR HAS SIGNS OF DISBONDMENT. REPAIRED AFFECTED AREA IAW DHC-8 RD8-57-0874 REPAIR SCHEME NR 2. (M)
- [SDR KPVA200014](https://openairdocs.org/sdr/KPVA200014), Feb 17, 2000: BRACKET. CORRODED. LEFT WING NR 4 FLAP TRACK SUPPORT BRACKET CORRODED. REPAIRED BRACKET IAW DHC-8 RD8-57-1606. BRACKET REPLACEMENT DUE WITHIN 500 HOURS. (M)
- [SDR KPVA200011](https://openairdocs.org/sdr/KPVA200011), Feb 17, 2000: SKIN. CORRODED. LEFT WING UPPER SKIN INTERNAL SURFACE CORRODED AT STATION YW 389 TO STATION YW400. UPPER SKIN INTERNAL SURFACE CORROSION REPAIRED AT STATION YW 389 - YW 400 IAW
- [SDR KPVA200015](https://openairdocs.org/sdr/KPVA200015), Feb 17, 2000: SKIN. CORRODED. RIGHT WING UPPER SKIN INTERNAL SURFACE HAS CORROSION AT STATION YW 389 TO YW 400. REPAIRED AFFECTED AREA IAW DHC-8 RD 8-57-1591. (M)
- [SDR KPVA200020](https://openairdocs.org/sdr/KPVA200020), Feb 17, 2000: FAIRING. DEBONDED. RIGHT NACELLE TAIL INBOARD FAIRING DISBONDED ON EXTERNAL SURFACE AT STATION XN250. REPAIRED DISBONDING IAW DHC-8 RD 8-54-0153. (M)
- [SDR KPVA200021](https://openairdocs.org/sdr/KPVA200021), Feb 17, 2000: FAIRING. DEBONDED. RIGHT NACELLE INBOARD FAIRING INTERNAL SURFACE DISBONDING AT STATION XN245. REPAIRED FAIRING AT STATION XN245 IAW DHC8- RD8-54-1195. (M)
- [SDR KPVA200001](https://openairdocs.org/sdr/KPVA200001), Jan 14, 2000: COMPUTER. MALFUNCTIONED. FLT 1224 - MKK - STICK SHAKER ACTUATED AND REMAINED ON. SYSTEM WAS DEFERRED UNDER MEL 27-3-1. AFTER AIRCRAFT RETURNED TO MAIN BASE THE LIFT COMPUTER WAS REPLACE
- [SDR 99ZZZM319](https://openairdocs.org/sdr/99ZZZM319), Apr 26, 1999: CONTROL BOX. INOPERATIVE. FLT 1521 - HNL - EMERGENCY LIGHTS FLICKERED ON AND OFF DURING TAXI. REMOVED AND REPLACED THE EMERGENCY LIGHT CONTROL BOX, AND PERFORMED AND OPERATIONAL CHECK OF
- [SDR 98ZZZM939](https://openairdocs.org/sdr/98ZZZM939), Nov 23, 1998: BATTERY PACK. DISCHARGED. ON PREFLIGHT, THE PILOTS FOUND THE RIGHT FORWARD EMRGENCY AND EGRESS LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY NR 2 BATTERY PACK OPS CHECK GOOD IAW 
- [SDR 98ZZZX2411](https://openairdocs.org/sdr/98ZZZX2411), Jun 24, 1998: STEERING. MALFUNCTIONED. NOSE WHEEL STEERING WILL NOT TURN RIGHT. MAINTENANCE RETURNED TO MKK AND MADE REPAIRS TO AIRCRAFT AND REPOSITIONED BACK TO HNL, SEVERAL PIECES, PARTS WERE REPLA
- [SDR 98ZZZX2073](https://openairdocs.org/sdr/98ZZZX2073), Feb 23, 1998: ANGLE. CRACKED. DURING SCHEDULED INSPECTION, (DISBONDING) CRACKS WERE DETECTED AT THE LEFT AFT CLOSING ANGLE VERTICAL FLANGE 2ND AND 3RD FASTENERS FROM OTBD EDGE. THE CRACKS TH

## FAA accident and incident reports (2)

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 19991223036489I](https://openairdocs.org/incident/19991223036489I), Dec 23, 1999: Dhav DHC8103 (N803WP), Kaunakakai, HI. (-23) MKU1429 @ 8,000', MKU1570 @ 7,000', N47D @ 6,500'. The TCAS on mku 1570 gave a resolution advisory to climb, loosing required separation by ATC. The TCAS…
- [Incident 19980429014729I](https://openairdocs.org/incident/19980429014729I), Apr 29, 1998: Dhav DHC8* (N803WP), Honolulu, HI. Narative missing.

## Other aircraft with N803WP

- [Registered now](https://openairdocs.org/aircraft/N803WP): Powrachute AIRWOLF 912ULS, S/N A272ULS, built 2017

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