# N829PH: 1991 Boeing DHC-8-102, registration cancelled 2006-08-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 22, 2006
- Exported to: Canada
- Status when cancelled: Sale reported
- Airframe: [Boeing DHC-8-102](https://openairdocs.org/model/boeing-dhc-8-102) (registry code 1386002)
- 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: 304
- Year built: 1991
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: November 5, 1991
- Last registry action: July 7, 2009
- Mode S code: AB5397
- Location: Calgary, Canada
- Owner type: Individual
- The mark today: https://openairdocs.org/aircraft/N829PH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=829PH
- Page: https://openairdocs.org/deregistered/N829PH-2006-08-22

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 Boeing DHC-8-102: https://openairdocs.org/model/boeing-dhc-8-102.md

## Service difficulty reports (56, newest 50)

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

- [SDR QXEA0100783](https://openairdocs.org/sdr/QXEA0100783), May 23, 2001: UNKNOWN. ODOR. SEA- FUEL ODOR FROM BLEEDS AFTER ENGINE START. NO FUEL LEAKS NOTED. CYCLED BLEEDS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0002902](https://openairdocs.org/sdr/QXEA0002902), Oct 28, 2000: CONTROLLER. MALFUNCTIONED. SEA- NR 1 VHF RADIO SMOKING. REMOVED AND REPLACED NR 1 VHF CONTROL HEAD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0002894](https://openairdocs.org/sdr/QXEA0002894), Oct 24, 2000: CONNECTOR. DIRTY. ALW- EMERGENCY LIGHTS IN CABIN CYCLE ON AND OFF 1-2 TIMES A SECOND. GALLEY LIGHTS, ENGINE INTAKE AND PROPELLER SYNCRONIZATION LIGHTS ALSO FLICKER RAPIDLY. CLEAN
- [SDR QXEA0002893](https://openairdocs.org/sdr/QXEA0002893), Oct 24, 2000: GCU. MALFUNCTIONED. SEA- EMERGENCY LIGHTS IN CABIN FLICKER ON AND OFF 1-2 TIMES PER SECOND. ENGINE INTAKE BYPASS AND PROPELLER SYNCRONIZATION LIGHTS ALSO FLICKER RAPIDLY. REPLACED 
- [SDR QXEA0002873](https://openairdocs.org/sdr/QXEA0002873), Oct 13, 2000: CONTROL BOX. MALFUNCTIONED. SEA- ALL CABIN EMERGENCY LIGHTS FLICKER ON AND OFF IN TURBULENCE. REMOVED AND REPLACED FLIGHT ATTENDANTS EMERGENCY LIGHTS SWITCH AND EMERGENCY LIGHTS CONTROL BO
- [SDR QXEA0002722](https://openairdocs.org/sdr/QXEA0002722), Sep 30, 2000: BRAKE ASSY. LEAKING. BOI- NR 2 ISOLATION SHUTOFF VALVE LIGHT 50 MINUTES INTO FLIGHT, 30 SECONDS LATER NR 1 ISOLATION SHUTOFF VALVE CAUTION LIGHT WITH INBOARD SPOILER LIGHT, BOTH HYD
- [SDR QXEA0002489](https://openairdocs.org/sdr/QXEA0002489), Sep 5, 2000: SIGN. MALFUNCTIONED. SEA- FLIGHT COMPARTMENT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FLIGHT COMPARTMENT EMERGENCY LIGHT AS REQUIRED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETU
- [SDR QXEA00002278](https://openairdocs.org/sdr/QXEA00002278), Aug 14, 2000: LIGHT. INOPERATIVE. PDX- COCKPIT OVERHEAD LIGHT INOP. MAINTENANCE REPLACED THE LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0001431](https://openairdocs.org/sdr/QXEA0001431), Jun 4, 2000: SWITCH. DIRTY. PSC- NR 2 AUTOFEATHER SYSTEM, NR 2 ENGINE WILL NOT AUTOFEATHER. FEATHER PUMP LIGHT ILLUMINATED, POWER UPTRIM ILLUMINATED, AUTOFEATHER ARM LIGHT EXITING BUT PROP
- [SDR QXEA0001161](https://openairdocs.org/sdr/QXEA0001161), May 5, 2000: PUMP. MALFUNCTIONED. PDX- AFTER NORMAL TAKEOFF AT PDX ON CLIMBOUT, TORQUE ON NR 1 ENGINE STARTED DROPPING OFF. A 45 PERCENT TORQUE DIFFERENCE ON NR 1, 2.3 INCH SPLIT ON POWER LEVERS
- [SDR QXEA0001176](https://openairdocs.org/sdr/QXEA0001176), May 3, 2000: LIGHT. INOPERATIVE. YYC- TWO LIGHTS ON FWD EMERGENCY LIGHT TRACK ARE NOT ILLUMINATING. REPAIRED WIRING IAW DHC-8 W/D 33-51-01.
- [SDR QXEA0001172](https://openairdocs.org/sdr/QXEA0001172), May 3, 2000: FAIRING. DELAMINATED. YYC- AREAS OF DELAMINATION ON LEFT HAND WING TO BODY AERODYNAMIC FAIRING STATION X333.0. REPAIRED IAW HORIZON AIR EA 9-53-557.
- [SDR QXEA0001166](https://openairdocs.org/sdr/QXEA0001166), May 3, 2000: LIGHT. INOPERATIVE. YYC- EMERGENCY LIGHT, FLOOR TRACK STRIP ON PANEL 133DZ IS BROKEN. INSTALLED NEW TRACK IAW DHC-8 IPC 33-52-00 FIG 5.
- [SDR QXEA0001185](https://openairdocs.org/sdr/QXEA0001185), May 2, 2000: SKIN. CRACKED. YYC- LEFT HAND UPPER OUTBOARD FINGERNAIL INSIDE SKIN IS CRACKED. REPAIRED IAW HORIZON AIR EA 9-54-245.
- [SDR QXEA0001187](https://openairdocs.org/sdr/QXEA0001187), May 1, 2000: SKIN. CHAFED. YYC- SPAN WISE CHAFE DAMAGE ON UPPER SURFACE OF LEFT HAND INBOARD FLAP LEADING EDGE. REPAIRED IAW HORIZON AIR EA 9-57-501, DHC-8 SRM 51-2036 AND SRM 51-20-51.
- [SDR QXEA0001189](https://openairdocs.org/sdr/QXEA0001189), Apr 27, 2000: SPAR CAP. SCRATCHED. YYC- RIGHT HAND WING UPPER AND LOWER SPAR CAP ANGLES SCRATCHED. REPAIRED IAW RD 8-57-1119.
- [SDR QXEA0001186](https://openairdocs.org/sdr/QXEA0001186), Apr 27, 2000: STRUCTURE. CRACKED. YYC- RIGHT HAND FINGERNAIL INSIDE TUNNEL SKIN IS CRACKED IN TWO LOCATIONS ON THE FWD UPPER SIDE, AT STA XN216. REPAIRED IAW HORIZON AIR EA 9-54-246.
- [SDR QXEA0001178](https://openairdocs.org/sdr/QXEA0001178), Apr 27, 2000: SPAR CAP. SCRATCHED. YYC- VERTICAL STAB FWD SPAR CAP ANGLES SCRATCHED. REPAIRED IAW DHC-8 RD 8-55-584.
- [SDR QXEA0001184](https://openairdocs.org/sdr/QXEA0001184), Apr 27, 2000: STRUCTURE. DAMAGED. YYC- GOUGE MARKS ON RIGHT HAND NACELLE HORIZONTAL, BH AT INBOARD SIDE APPROX STATION XN240.0. REPAIRED IAW DHC-8 RD 8-54-1274 AND HORIZON AIR EA 9-54-244.
- [SDR QXEA0001179](https://openairdocs.org/sdr/QXEA0001179), Apr 25, 2000: FRAME. CRACKED. YYC- CRACKS IN RADIUS OF FRAME 4 AT STRINGER 4 LEFT HAND AND STRINGER 4 RIGHT HAND. REPAIRED IAW DHC-8 RD 8-55-199.
- [SDR QXEA0001175](https://openairdocs.org/sdr/QXEA0001175), Apr 25, 2000: ACCESS PANEL. DEBONDED. YYC- ACCESS PANEL 122AR MATING BENT AND CHAFED AND SEAL HAS DISBONDED. REPAIRED IAW DHC-8 SRM 51-20-11 PAGE 3 AND 51-20-16 PAGE 4.
- [SDR QXEA0001173](https://openairdocs.org/sdr/QXEA0001173), Apr 25, 2000: SKIN. CHAFED. YYC- VERTICAL SKIN CHAFED AT YW 48.00 RIGHT HAND 20 INCHES TO 41 INCHES AFT OF REAR SPAR. REPAIRED IAW DHC-8 MM 51-20-11 PAGE 7.
- [SDR QXEA0001171](https://openairdocs.org/sdr/QXEA0001171), Apr 25, 2000: SKIN. DENTED. YYC- DENT IN FUSELAGE FWD OF RIGHT HAND EMERGENCY EXIT STATION X234.5 BETWEEN STRINGER 19S AND 20S. REPAIRED IAW DHC-8 MM 53-30-21 FIGURES 5 AND 6.
- [SDR QXEA0001168](https://openairdocs.org/sdr/QXEA0001168), Apr 25, 2000: SHIELD. DENTED. YYC- DENT WITH CREASE BELOW LEFT HAND ICE SHIELD, STATION X302.4 BETWEEN STRINGER 19P AND 20P. REPAIRED IAW DHC-8 MM 8-53-4975.
- [SDR QXEA0001181](https://openairdocs.org/sdr/QXEA0001181), Apr 24, 2000: SKIN. SCRATCHED. YYC- SCRATCH ON VERTICAL STAB JUST BELOW FWD RIGHT HAND HORIZONTAL STAB ATTACH POINT. REPAIRED IAW DHC-8 RD 8-55-584.
- [SDR QXEA0001180](https://openairdocs.org/sdr/QXEA0001180), Apr 24, 2000: SPAR CAP. SCRATCHED. YYC- HORIZONTAL STAB SPAR CAP ANGLES HAVE LIGHT SCRATCHES. REPAIRED IAW DHC-8 RD 8-55-626.
- [SDR QXEA0001169](https://openairdocs.org/sdr/QXEA0001169), Apr 24, 2000: SHIELD. DENTED. YYC- SEVERAL DENTS ON LEFT HAND FUSELAGE, JUST AFT OF ICE SHIELD, APPROX STATION 333.3 BETWEEN STRINGERS 11P AND 17P. REPAIRED IAW DHC-8 MM 8-53-4974.
- [SDR QXEA0001188](https://openairdocs.org/sdr/QXEA0001188), Apr 20, 2000: SPAR. SCRATCHED. YYC- SCRATCHES FOUND IN RADIUS OF LEFT HAND FWD WING SPAR LEADING EDGE AND BETWEEN STATION YW351 - YW490. REPAIRED IAW RD 8-57-1119.
- [SDR QXEA0001183](https://openairdocs.org/sdr/QXEA0001183), Apr 20, 2000: SKIN. SCRATCHED. YYC- LEFT HAND WING INBOARD FUEL TANK PANEL OPENING HAS SMALL SCRATCHES ON LIP AROUND PERIMETER. REPAIRED IAW DHC-8 RD 8-57-611.
- [SDR QXEA0001170](https://openairdocs.org/sdr/QXEA0001170), Apr 20, 2000: SEAT TRACK. CORRODED. YYC- LEFT HAND FWD SEAT TRACK HAS CORROSION BEYOND LIMITS (OUTBOARD TRACK). REMOVED AND REPLACED SEAT TRACK IAW DHC-8 MM 51-40-00 PAGE 2.
- [SDR QXEA0001164](https://openairdocs.org/sdr/QXEA0001164), Apr 20, 2000: SEAT TRACK. CORRODED. YYC- AFT LEFT HAND INBOARD SEAT TRACK IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW DHC-8 MM 51-40-00 PAGE 2.
- [SDR QXEA0001162](https://openairdocs.org/sdr/QXEA0001162), Apr 20, 2000: SEAT TRACK. CORRODED. YYC- AFT RIGHT HAND INBOARD SEAT TRACK IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW DHC-8 MM 51-40-00 PAGE 2 TABLE 1 AND 2.
- [SDR QXEA0001190](https://openairdocs.org/sdr/QXEA0001190), Apr 20, 2000: FITTING. WORN. YYC- UPPER FUSELAGE FITTING HAVE WEAR MARKS ON LOWER FLANGE OF CARGO DOOR. REPAIRED IAW DHC-8 RD 8-53-489.
- [SDR QXEA0001174](https://openairdocs.org/sdr/QXEA0001174), Apr 20, 2000: PLATE. SCRATCHED. YYC- LADDER PLATES SCRATCHED BELOW PANEL 623 AT RIGHT HAND YW139 - YW171. REPAIRED IAW DHC-8 MM 8-57-499.
- [SDR QXEA0001165](https://openairdocs.org/sdr/QXEA0001165), Apr 19, 2000: SEAT TRACK. CORRODED. YYC- RIGHT HAND FWD INBOARD SEAT TRACK IS CORRODED BEYOND LIMITS AT STATION X202 THROUGH X222. REMOVED AND REPLACED SEAT TRACK IAW DHC-8 MM 51-40-00 PAGE 1.
- [SDR QXEA0001163](https://openairdocs.org/sdr/QXEA0001163), Apr 19, 2000: SEAT TRACK. CORRODED. YYC- FWD LEFT HAND INBOARD SEAT TRACK IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW DHC-8 MM 51-40-00 PAGE 1.
- [SDR QXEA0001182](https://openairdocs.org/sdr/QXEA0001182), Apr 18, 2000: FRAME. CORRODED. YYC- RIGHT HAND NACELLE MAIN LANDING GEAR FRAME SURFACE UNDER RETRACTION ACTUATOR FITTING HAS CORROSION. REPAIRED IAW HORIZON EA 9-54-159B.
- [SDR QXEA0000788](https://openairdocs.org/sdr/QXEA0000788), Mar 22, 2000: PSEU. MALFUNCTIONED. SEA- AFTER LOWERING LANDING GEAR, GEAR DOOR OPEN LIGHTS DID NOT EXTINGUISH, STAYED ON THROUGHOUT APPROCH, LANDING GEAR ROLL OUT ON INITIAL TAXI. DURING LATTER T
- [SDR QXEA9901930](https://openairdocs.org/sdr/QXEA9901930), Sep 18, 1999: WIRE. LOOSE. PDX - EMERGENCY LIGHTS DO NOT OPERATE FROM FLIGHT ATTENDENTS PANEL SWITCH. PILOTS SWITCH OPERATES NORMAL. RECONNECTED LOOSE WIRE AT SWITCH, OPERATIONAL CHECKS G
- [SDR QXEA9901663](https://openairdocs.org/sdr/QXEA9901663), Aug 19, 1999: LIGHT. INOP. PDX- COCKPIT EMERGENCY LANTERN LIGHT DIM THEN INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONAL TEST CHECK GOOD.
- [SDR QXEA990139](https://openairdocs.org/sdr/QXEA990139), Aug 10, 1999: MECHANISM. OUT OF ADJUST. MWH- GEAR DOOR LIGHT ILLUMINATED. GEAR DOOR REMAIN OPEN. ADJUSTED RIGGING OF LEFT HAND MAIN LANDING GEAR REAR/CENTER DOOR ACTUATOR, FUNCTIONAL CHECK OF GEAR GOO
- [SDR QXEA9900096](https://openairdocs.org/sdr/QXEA9900096), Jan 20, 1999: GAS SPRING. MALFUNCTION. MAIN CABIN DOOR HARD TO OPEN AND CLOSE. MAINTENANCE REPLACED THE MAIN CABIN DOOR GAS SPRINGS, OPERATIONAL CHECKS GOOD.
- [SDR QXEA9801723](https://openairdocs.org/sdr/QXEA9801723), Nov 17, 1998: LIGHT. BROKEN. SEA- LEFT UNDERWING CABIN EMERGENCY LIGHT BROKEN. MAINTENANCE REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA9801547](https://openairdocs.org/sdr/QXEA9801547), Nov 1, 1998: STRUT. CRACKED. PDX- DURING THE ACCOMPLISHMENT OF A SCHEDULED A CHECK, THE NOSE LANDING GEAR OUTER CYLINDER WAS FOUND CRACKED. THE CRACK WAS ON THE AFT SIDE OF THE OUTER CYLIND
- [SDR QXEA9800965](https://openairdocs.org/sdr/QXEA9800965), Jul 14, 1998: BATTERY. DISCHARGED. SEA - DURING THE TIME CHANGE OF THE EMERGENCY LIGHT BATTERY PACKS, THE BATTERY PACK FOR PS4 WAS FOUND TO BE BAD FROM STOCK. REPLACED BATTERY PACK. OPERATIONAL C
- [SDR QXEA9800941](https://openairdocs.org/sdr/QXEA9800941), Jul 9, 1998: SIGN. MISSING. SEA - ROW 4AB EMERGENCY EXIT SIGN MISSING. REPLACED EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA9800683](https://openairdocs.org/sdr/QXEA9800683), May 27, 1998: BULBS. FAILED. NUMEROUS BULBS OUT IN THE FLOOR PROX LIGHT STRIPS, AND THE AFT EMERGENCY EXIT SIGN IS INOP. RELAMPED FLOOR PROX STRIPS, AND RECONNECTED RIGHT AFT EMERGENCY EXIT
- [SDR QXEA9700692](https://openairdocs.org/sdr/QXEA9700692), Oct 28, 1997: AIR DISTRIBUTION. ODOR. NOTED FUEL SMELL WHEN NR 2 BLEED TURNED ON IMMEDIATELY AFTER ENGINE START. SMELL WENT AWAY WITHIN A COUPLE OF MINUTES. COMPLIED WITH SEVERAL ENGINE STARTS, COUL
- [SDR QXEA9700642](https://openairdocs.org/sdr/QXEA9700642), Oct 7, 1997: SIGN. BROKEN. BOI - MAIN CABIN DOOR LOWER EMERGENCY EXIT SIGN BROKEN. INSTALLED NEW EMERGENCY EXIT SIGN, OPERATIONAL CHECK GOOD.
- [SDR QXEA9700497](https://openairdocs.org/sdr/QXEA9700497), Aug 17, 1997: LAMP. FAILED. TWO FORWARD EMERGENCY PATH LIGHTS INOP. RELAMPED AND RESTORED WIRING, OPERATIONAL CHECK GOOD.

All 56: https://openairdocs.org/deregistered/N829PH-2006-08-22/reports.md

## Other aircraft with N829PH

- [Registered now](https://openairdocs.org/aircraft/N829PH): Paul B Howell DAKOTA HAWK, S/N 14

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.