# N806WP: 1993 Boeing / Dehavilland DHC-8-103, registration cancelled 2023-05-27

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 27, 2023
- Status when cancelled: Valid registration
- Airframe: [Boeing / Dehavilland DHC-8-103](https://openairdocs.org/model/boeing-dehavilland-dhc-8-103) (registry code 1386005)
- 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: 357
- Year built: 1993
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: May 19, 1993
- Certificate issued: March 6, 2014
- Last registry action: January 22, 2023
- Mode S code: AAFA29
- 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/N806WP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=806WP
- Page: https://openairdocs.org/deregistered/N806WP-2023-05-27

From the FAA registry file of October 31, 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 Boeing / Dehavilland DHC-8-103: https://openairdocs.org/model/boeing-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 KPVA2012092607](https://openairdocs.org/sdr/KPVA2012092607), Sep 26, 2012: PLATE. CRACKED. INSTALLED PERMANENT PER RD 8-57-5531 AND RD 8-57-876 REPAIR FOR CRACKED LADDER PLATE AT YW 139-2 AND STR 6.
- [SDR KPVA2012062907](https://openairdocs.org/sdr/KPVA2012062907), Jun 29, 2012: WARNING SYSTEM. ACTIVATED. NOSE GEAR AMBER LIGHT ILLUMINATED WHEN SELECTED UP AND GRINDING SOUND. INSPECTED NLG AREA. NO DEFECTS FOUND. PERFORMED NORMAL AND EMERGENCY EXTENSION. NO DEFECT
- [SDR KPVA201113](https://openairdocs.org/sdr/KPVA201113), Oct 28, 2011: ACTUATOR. CRACKED. DURING CRUISE AND AFTER SELECTING NR 2 STANDBY PUMP ON, THE NR 2 HYD ISO CAUTION LIGHT ILLUMINATED. NR 2 HYDRAULIC QUANTITY DROPPED TO ABOUT 1 QT. RAN THROUGH C
- [SDR KPVA201112](https://openairdocs.org/sdr/KPVA201112), Oct 22, 2011: ACTUATOR. CRACKED. NR 2 HYD ISO VALVE CAUTION LIGHT ILLUMINATED IN FLIGHT ACCOMPANIED BY LOSS OF ALL HYDRAULIC FLUID IN NR 2 QUANTITY SYSTEM. MAINTENANCE REPLACED THE LT OUTBOARD 
- [SDR KPVA201106](https://openairdocs.org/sdr/KPVA201106), Jun 6, 2011: ACTUATOR. CRACKED. NR 2 HYD ISO VLV (CAUTION) LIGHT ILLUMINATED WITH FLUID LOSS IN NR 2 HYDRAULIC SYSTEM. FLIGHT CREW DECLARED EMERGENCY, DIVERTED TO HNL AND USED ALTERNATE EXTENS
- [SDR KPVA201103](https://openairdocs.org/sdr/KPVA201103), Feb 20, 2011: BEARING RACE. CHIPPED. LT PROPELLER ASSY, NR 1 BLADE HAS OIL LEAK. UPON INVESTIGATION IT WAS DISCOVERED THAT THE OUTER BEARING FOR THE NR 1 BLADE WAS CHIPPED. THE HUB & ACTUATOR WAS R
- [SDR KPVA 201102](https://openairdocs.org/sdr/KPVA%20201102), Feb 17, 2011: ACM. MALFUNCTIONED. (PIREP) UPON SHUTDOWN IN HNL, SMOKE FILLED THE COCKPIT AND CABIN FOLLOWED BY A SUPER STRONG BURNING ODOR. SMOKE DISSIPATED AFTER 5-8 SECONDS HOWEVER A STRONG EL
- [SDR KPVA 201005](https://openairdocs.org/sdr/KPVA%20201005), Dec 9, 2010: WINDSHIELD. CRACKED. CRUISE FLIGHT 17,000 FEET, WINDSHIELD HEAT ON NORM, NOTICED A CRACK IN THE LT WINDSHIELD. OAT -5 DEG C. MAINTENANCE REPLACED PILOT FRONT WINDSHIELD.
- [SDR KPVA 200911](https://openairdocs.org/sdr/KPVA%20200911), Dec 2, 2009: DOUBLER. CRACKED. PREVIOUS REPAIR DOUBLER ON FLOORBEAM P/N 85310380 CRACKED. PREVIOUS REPAIR ACCOMPLISHED ON MARCH 14, 2001. TAT 16,295.9 TCY 26,203. DONE IAW RD 8-53-1416. NEW R
- [SDR KPVA2009-02](https://openairdocs.org/sdr/KPVA2009-02), Jan 25, 2009: WARNING SYSTEM. MALFUNCTIONED. ON FINAL APPROACH, RECEIVED MASTER WARNING LIGHT WITH SMOKE LIGHT. LIGHT STAYED ON FOR APPROX 20 SECONDS, THEN WENT OUT THEN FLICKERED ON THEN OFF. (MX) VISUAL 
- [SDR KPVA2009-01](https://openairdocs.org/sdr/KPVA2009-01), Jan 17, 2009: SWITCH. INOPERATIVE. SMOKE WARNING LIGHT ILLUMINATED DURING TAXI. (MX) REMOVED AND REPLACED SWITCH 2612-S1 AND AR1 CONTROL AMPLIFIER AT PLUG 2612-P1 IAW WD 26-12-00 PG. 1. OPS CHECK
- [SDR KPVA 2008-06](https://openairdocs.org/sdr/KPVA%202008-06), Dec 28, 2008: CONTROL UNIT. INTERMITTENT. ON TAXI, RECEIVED MASTER WARNING AND SMOKE WARNING LIGHT INTERMITTENT ON AND OFF 6 TIMES. MX REMOVE AND REPLACED CAUTION CONTROL BOX IAW MM CHAP 33-18-00 PAR 2A
- [SDR KPVA200710](https://openairdocs.org/sdr/KPVA200710), Aug 6, 2007: INDICATOR. FAULTY. (PIREP) PFCS INDICATOR GIVING REVERSE READING FOR INBOARD (L)SPOILER. (MX) REMOVE & REPLACED PFCS INDICATOR IAW DHC-8 MM CHAP 27-05-00 PG 201-206. OPS CHECK GOO
- [SDR KPVA200626](https://openairdocs.org/sdr/KPVA200626), Dec 17, 2006: GENERATOR. WARNING LIGHT. (PIREP) NR 2 AC GEN LIGHT WITH NR 2 AC GEN OFF, LAC BUS AND L TRU LIGHT CAME ON AND STAYED ON. (MX) REMOVED AND REPLACED NR 2 AC GEN IAW DHC PSM 1-8-2 PG 201-20
- [SDR KPVA200625](https://openairdocs.org/sdr/KPVA200625), Dec 11, 2006: SPRING. BROKEN. (PIREP) OUTBOARD REAR GEAR DOOR ON LEFT MAIN OPENED IN FLIGHT AFTER TAKEOFF FROM LANAI. NO LIGHTS FOR INDICATION IN COCKPIT. (MX) REMOVED AND REPLACED BROKEN SP
- [SDR KPVA200622](https://openairdocs.org/sdr/KPVA200622), Nov 22, 2006: HYDRAULIC LINE. LEAKING. (PIREP) NR 2 HYDRAULIC LEAK. (MX) INSTALLED TEMPLINE FOR SPU (NR 2) PRESSURE LINE IAW GMM 8.2 & DHC MM 20-06-03 PG 9. LEAK CHECK GOOD, NO DEFECTS.
- [SDR KPVA200616](https://openairdocs.org/sdr/KPVA200616), Aug 11, 2006: ADC. MALFUNCTIONED. (PIREP) DADC DATA INVALID. (MX) RE-INITIALIZED SYSTEMS IAW MM 34-12-01 PG. 204. NO FAULTS NOTED.
- [SDR KPVA200614](https://openairdocs.org/sdr/KPVA200614), Aug 6, 2006: GENERATOR. INOPERATIVE. NR 1 AC GEN LIGHT ILLUMINATED PRIOR TO TAKEOFF. DISCONTINUED AND TAXIED BACK TO TERMINAL. COMPLETED ABNORMAL CHECKLIST, NR 1 AC GEN LIGHT CONTINUED TO ILLUMINAT
- [SDR KPVA200613](https://openairdocs.org/sdr/KPVA200613), Jul 14, 2006: ENGINE. LACK OF LUBE. NR 1 ENG OIL PRESS LIGHT CAME ON DURING T/O ROLL. SERVICED NR 1 ENGINE OIL RESERVOIR. LEAK & OPS CHECK GOOD IAW DHC-8 MM 12-10-79 PG 1-3 & DHC-8 MM 71-00-00 PG 
- [SDR KPVA20061](https://openairdocs.org/sdr/KPVA20061), Jan 8, 2006: INDICATOR. FLUCTUATES. NR 1 TAKEOFF GAUGE READOUT ZERO ON TAKEOFF ROLL AND CONTINUOUS FLUCTUATION AT 20% AND 125% INTERMITTENT THEREAFTER. REMOVED AND REPLACED NR 1 TORQUE INDICATOR I
- [SDR 200519](https://openairdocs.org/sdr/200519), Dec 14, 2005: COMPUTER. MALFUNCTIONED. (PIREP) DADC DATA INVALID DISPLAYED ON ADVISORY DISPLAY ON TAKEOFF ROLL. (MX) PERFORMED AHRS SELF TEST IAW DHC-8 MM 34-20-14 PG 202-203 PAR 2B. NO FAULTS FOUND 
- [SDR 200513](https://openairdocs.org/sdr/200513), Aug 4, 2005: HYDROMECH UNIT. UNKNOWN. ON TAKEOFF ROLL, ABORTED DUE TO NR 1 ENGINE NOT PRODUCING TAKEODD POWER. NR 1 PROP AT 900 AND NR 2 PROP AT 1200 RPM. NR 1 TORQUE AT 40% AND NR 2 @ 60%. REMOVED 
- [SDR KPVA200511](https://openairdocs.org/sdr/KPVA200511), Jul 23, 2005: SKIN. DAMAGED. LT WING TIP IS TORN ALMOST ALL THE WAY OFF. REPAIRED LT WING TIP IAW RD8-57-3143. REMOVED AND REPLACED LT AILERON IAW DHC MM 27-12-11 PG 201-204. RIGGED AILERON
- [SDR 20052](https://openairdocs.org/sdr/20052), Mar 26, 2005: ENGINE. FOD. RIGHT ENGINE MADE POPPING NOISE DURING CRUISE AND INDICATED TORQUE FLUCTUATION AND SLIGHT VIBRATION. NO OTHER LIGHTS OR INDICATIONS WERE OBSERVED. REMOVED AND R
- [SDR 200421](https://openairdocs.org/sdr/200421), Dec 8, 2004: PRESSURE SWITCH. LEAKING. (PIREP) FUEL SMELL INTO CABIN AND COCKPIT WITH AIR CONDITIONING, ON GROUND ONLY. (MX) FOUND NR 1 ENGINE LOW FUEL PRESSURE SWITCH FAULTY. REPLACED NR 1 ENGINE FU
- [SDR 200415](https://openairdocs.org/sdr/200415), Jul 19, 2004: IMPELLER. FOD. RT ENGINE PCE 120968 1ST STAGE IMPELLER FOD DAMAGE. REMOVED AND REPLACED NR 2 ENGINE PCE 120968 IAW FORM IA M-105. O DEFECTS NOTED.
- [SDR KPVA20042](https://openairdocs.org/sdr/KPVA20042), Jan 21, 2004: CIRCUIT CARD. FAILED. NR 2 DC GEN CAUTION LIGHT ILLUMINATED BRIEFLY ON TAKEOFF ROLL, ON BRIEFLY DURING TAXI IN. INSPECTED NR 2 DC CAUTION LIGHT AND DEFERRED IAW MEL 24-16. COMPLIED W
- [SDR 2003F00354](https://openairdocs.org/sdr/2003F00354), Apr 25, 2003: SMOKE DETECTOR. WILL NOT TEST. HNL - NR 1 SMOKE DETECTOR INOPERATIVE DURING TEST MODE. REMOVED 4 SCREW AND 2 BOLTS, REMOVED SMOKE DETECTOR AND CANNON PLUG. INSTALLED NEW SMOKE DETECTOR WITH 4
- [SDR KPVA200312](https://openairdocs.org/sdr/KPVA200312), Feb 28, 2003: LIGHT. INOPERATIVE. COCKPIT PORTABLE EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED COCKPIT PORTABLE EMERGENCY LIGHT IAW MM. OPS CHECKED GOOD.
- [SDR KPVA20039](https://openairdocs.org/sdr/KPVA20039), Feb 26, 2003: LIGHT. INOPERATIVE. COCKPIT PORT EMERGENCY LIGHT, LOW BATTERY CHARGE. REMOVED AND REPLACED PORT EMERGENCY LIGHT. OPS CHECK GOOD.
- [SDR KPVA20031](https://openairdocs.org/sdr/KPVA20031), Jan 3, 2003: SMOKE DETECTOR. MALFUNCTIONED. FLT 1126 - HNL - BAGGAGE COMPARTMENT SMOKE WARNING ILLUMINATED DURING ENGINE START. NO SMOKE PRESENT AND ALL ELECTRICAL DEVICES VERIFIED OFF (CELL PHONES). REMO
- [SDR KPVA200237](https://openairdocs.org/sdr/KPVA200237), Dec 1, 2002: LIGHT. BROKEN. EXIT LIGHT ON ROW 1 RIGHT SIDE IS BROKEN. REMOVED AND REPLACED EXIT LIGHT ON ROW 1 RIGHT SIDE IAW DHC-8 MM 33-51-00 PAGE 201 SECTION 1A. OPS CHECK GOOD IAW DHC8
- [SDR KPVA200232](https://openairdocs.org/sdr/KPVA200232), Oct 24, 2002: CONNECTOR. DIRTY. HNL - FLT 1620 - SMOKE WARNING FLICKERED ON AND OFF MOMENTARILY IN FLIGHT. CLEARED MEL 26-8-1. CLEANED CANNON PLUGS AND INSPECTED BAGGAGE COMPARTMENT NR 2 SMOKE
- [SDR KPVA200227](https://openairdocs.org/sdr/KPVA200227), Sep 18, 2002: BOLT. LOOSE. HNL - A BOLT ON FORWARD SIDE OF AIRSTAIR SUPPORT FOR IS LOOSE AND INHIBITS DOOR FROM OPENING. INSTALLED THREADED BUSHING ON UPPER STAY STRUT IAW DHC 8MM 52-10-0
- [SDR KPVA200218](https://openairdocs.org/sdr/KPVA200218), Aug 10, 2002: CAM FOLLOWER. DAMAGED. A LOUD BINDING & GRINDING IN AIRSTAIR DOOR WHEN OPENING OR CLOSING. INSTALLED CAM FOLLOWER ON FORWARD HANDRAIL UPPER ASSEMBLY. OPS CHECK GOOD, NO DEFECTS NOTED.
- [SDR 2002F01108](https://openairdocs.org/sdr/2002F01108), Jun 29, 2002: CIRCUIT CARD. FAULTY. WEIGHT ON WHEELS CAUTION LIGHT CAME ON 3 TIMES ON TAKEOFF. REMOVED AND REPLACED CAUTION LIGHT PANEL CIRCUIT CARD NR 2. OPS CHECK IAW DASH 8 MM 33-12-01 PAGE 201
- [SDR KPVA20021](https://openairdocs.org/sdr/KPVA20021), Jan 3, 2002: STARTER GEN. INOPERATIVE. ON CLIMBOUT WE NOTICED THE AIR DATA COMPUTER FAILED ALONG WITH NR1 DC GEN CAUTION LIGHT ILLUMINATED. WE EXCUTED PROCEDURES IN ABNORMAL CHECKLIST, LIGHT EXTINGUI
- [SDR KPVA200125](https://openairdocs.org/sdr/KPVA200125), Nov 18, 2001: FLASHLIGHT. INOPERATIVE. HNL - FOUND PORTABLE EMERGENCY LIGHT WILL NOT COME ON WHEN SELECTED ON. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD IAW DHC 8MM 33-51
- [SDR KPVA200124](https://openairdocs.org/sdr/KPVA200124), Nov 14, 2001: BUTTON. BROKEN. OVERHEAD REMOVABLE EMERGENCY LIGHT 'TEST' PUSH BUTTON BROKEN. REMOVED PORTABLE EMERGENCY LIGHT (BROKEN) AND INSTALLED SERVICEABLE PORTABLE EMERGENCY LIGHT. NO D
- [SDR KPVA200121](https://openairdocs.org/sdr/KPVA200121), Oct 25, 2001: POWER SUPPLY. DISCHARGED. HNL - DS1, DS2 EMERGENCY PATH LIGHTS DON'T COME ON. REMOVED AND REPLACED EMERGENCY LIGHTS ESCAPE PATH POWER SUPPLY AT STATION 3352 PS2. OPS CHECK GOOD IAW DHC 8
- [SDR KPVA200119](https://openairdocs.org/sdr/KPVA200119), Sep 15, 2001: POWER SUPPLY. DISCHARGED. HNL - LEFT SIDE WALL EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY. SYSTEM OPS CHECKED GOOD. (M)
- [SDR 20001212SH003](https://openairdocs.org/sdr/20001212SH003), Oct 22, 2000: BOLT. SHEARED. HNL - FLT 1133 - LOST NR 2 HYDRAULIC SYSTEM FLUID AFTER GEAR EXTENSION WAS COMPLETED, LANDED WITHOUT INCIDENT. TAXIED IN WITH DIFFERENTIAL BREAKING AND THRUST. 
- [SDR KPVA200029](https://openairdocs.org/sdr/KPVA200029), Oct 22, 2000: BOLT. SHEARED. FLT 1133 - HNL - LOST NR 2 HYDRAULIC SYSTEM FLUID AFTER GEAR EXTENSION WAS COMPLETED AND LANDED WITHOUT INCIDENT (HNL). TAXI IN WITH DIFFERENTIAL BREAKING AND T
- [SDR KPVA200032](https://openairdocs.org/sdr/KPVA200032), Oct 21, 2000: BATTERY. DISCHARGED. HNL - RIGHT FORWARD AND LEFT AFT EMERGENCY EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLIES. SYSTEM OPS CHECKED GOOD. (M)
- [SDR 99ZZZX1958](https://openairdocs.org/sdr/99ZZZX1958), Mar 15, 1999: BULB. FAILED. EMERGENCY PATH LIGHT IS OUT AT FORWARD EMERGENCY EXIT. REMOVED AND REPLACED LAMP.

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