# N826PH: 1990 Boeing DHC-8-102, registration cancelled 2013-06-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 10, 2013
- Status when cancelled: Sale reported, canceled
- 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: 214
- Year built: 1990
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: June 5, 1990
- Last registry action: June 1, 2005
- Mode S code: AB4872
- Location: Calgary Alberta, Canada
- Owner type: Individual
- The mark today: https://openairdocs.org/aircraft/N826PH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=826PH
- Page: https://openairdocs.org/deregistered/N826PH-2013-06-10

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

## Service difficulty reports (77, newest 50)

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

- [SDR QXEA0101355](https://openairdocs.org/sdr/QXEA0101355), Aug 11, 2001: SKIN. CRACKED. PDX - SEVERAL CRACKS IN AFT CONNECTION ANGLE FOR HORSE COLLAR TO UPPER SKIN AT TOP CENTER OF HORSE COLLAR STRUCTURE (MARKED). REPAIRED IAW EA 9-54-306.
- [SDR QXEA0100795](https://openairdocs.org/sdr/QXEA0100795), May 29, 2001: STOP. LACK OF LUBE. SEA - CREW REPORTED MAIN CABIN DOOR HARD TO OPERATE. CLEANED AND LUBED DOOR STOPS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0100790](https://openairdocs.org/sdr/QXEA0100790), May 28, 2001: SIGN. INOPERATIVE. SEA - EMERGENCY EXIT SIGN AT ROW 4 A/B REPORTED INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0100789](https://openairdocs.org/sdr/QXEA0100789), May 24, 2001: CONNECTOR. LOOSE. SEA- EMERGENCY EXIT ROW FLOOR PATH LIGHTING FOUND INOPERATIVE. FOUND LOOSE ELECTRICAL CONNECTION. RESEATED CANNON PLUG. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURN
- [SDR QXEA0002891](https://openairdocs.org/sdr/QXEA0002891), Oct 25, 2000: UNKNOWN. ODOR. SEA- STRANGE BURNING SMELL COMING FROM COCKPIT. INSPECTED ALL COCKPIT INSTRUMENTS AND LIGHTING. RAN BOTH BLEEDS. NO DEFECTS NOTED. NO PARTS REPLACED. OPERATIONA
- [SDR QXEA00002059](https://openairdocs.org/sdr/QXEA00002059), Jul 29, 2000: WIRE. BROKEN. SEA- BROKEN WIRE FOUND ON AFT EMERGENCY FLOOR TRACK LIGHT. MAINTENANCE REPLACED THE CONNECTOR AT THE EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED
- [SDR QXEA0000652](https://openairdocs.org/sdr/QXEA0000652), Mar 13, 2000: LIGHT. MALFUNCTIONED. PDX- COCKPIT EMERGENCY LIGHT ASSEMBLY INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT ASSEMBLY AND RECEPTICLE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETUR
- [SDR QXEA0000554](https://openairdocs.org/sdr/QXEA0000554), Feb 18, 2000: RADAR  UNIT. FAILED. BOI - ODOR IN COCKPIT APPEARS TO BE COMING FROM RADAR CRT. REMOVED AND REPLACED RADAR CRT UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0000281](https://openairdocs.org/sdr/QXEA0000281), Jan 31, 2000: SKIN. DAMAGED. YYC - APPROXIMATELY 2.2 SCRATCH IN PASSENGER DOOR SHELL NEAR BOTTOM FORWARD CORNER. REPAIRED IAW DHC 8 SRM 51-20-11, PAGE 3, SECTION B, SRM 52-00-16, PAGE 2 AND
- [SDR QXEA0000266](https://openairdocs.org/sdr/QXEA0000266), Jan 31, 2000: STRUCTURE. DENTED. YYC - DENT ON RIGHT SIDE OF FUSELAGE, 1 FORWARD OF STATION X405.737 AND APPROXIMATELY 5 BELOW STRINGER 16S. DENT WITHIN LIMITS DHC 8 SRM 53-00-16, PAGE 2, TABLE
- [SDR QXEA0000242](https://openairdocs.org/sdr/QXEA0000242), Jan 31, 2000: SKIN. DENTED. YYC - DENT IN FUSELAGE 12 AFT OF STATION X312.36 AT STRINGER 2P. REPAIRED IAW RD 8-53-4753.
- [SDR QXEA0000267](https://openairdocs.org/sdr/QXEA0000267), Jan 29, 2000: STUD. BROKEN. YYC - STUD FOR BONDING WIRE AT RIGHT OUTBOARD ELEVATOR TAB HINGE POINT BROKEN AWAY FROM TRAILING EDGE OF ELEVATOR. REPAIRED IAW DHC 8 SRM 51-40-00 AND RD 8-53-4
- [SDR QXEA0000278](https://openairdocs.org/sdr/QXEA0000278), Jan 28, 2000: PANEL. CORRODED. YYC- RIGHT WING PANELS, 632AT THROUGH TO 632DT, 626AT, 629BT AND 624CT HAVE CORROSION ON FASTENERS AND PANELS. REPAIRED IAW DHC 8 SRM 51-20-00, SRM 51-20-11, PA
- [SDR QXEA0000276](https://openairdocs.org/sdr/QXEA0000276), Jan 28, 2000: SKIN. CORRODED. YYC - NUMEROUS FASTENERS AND SURFACE AREAS HAVE LIGHT CORROSION ON RIGHT OUTBOARD WING, UPPER AND LOWER SURFACED, STATION 405.0 TO WING BOX END AT OUTBOARD. REP
- [SDR QXEA0000275](https://openairdocs.org/sdr/QXEA0000275), Jan 28, 2000: SKIN. CORRODED. YYC - LIGHT CORROSION ON FASTENERS AND SMALL SURFACE AREAS IN NUMEROUS PLACED OF RIGHT WING, STATION YW171.2-YW405.0. REPAIRED IAW DHC 8 SRM 51-20-11, SRM 51-20
- [SDR QXEA0000274](https://openairdocs.org/sdr/QXEA0000274), Jan 28, 2000: SKIN. CORRODED. YYC- NUMEROUS FASTENERS AND SMALL AREAS HAVE LIGHT CORROSION ON RIGHT WING, UPPER AND LOWER SURFACES, STATION YW139.0-YW171.12. REPAIRED IAW DHC 8 SRM 51-20-00 
- [SDR QXEA0000273](https://openairdocs.org/sdr/QXEA0000273), Jan 28, 2000: SKIN. CORRODED. YYC - RIGHT WING HAS NUMEROUS FASTENERS WITH CORROSION ON AND AROUND FASTENER HEADS. REPAIRED IAW DHC 8 SRM 57-20-00 AND SRM 57-20-11.
- [SDR QXEA0000271](https://openairdocs.org/sdr/QXEA0000271), Jan 28, 2000: SPAR. CORRODED. YYC - REAR SPAR HAS LIGHT SURFACE CORROSION FROM STATION YW45.0 - 139.0, ON RIGHT WING. REPAIRED IAW DHC 8 SRM 51-20-00, SRM 51-20-11, SRM 51-20-16, PAGE 4, SEC
- [SDR QXEA0000270](https://openairdocs.org/sdr/QXEA0000270), Jan 28, 2000: SKIN. CORRODED. YYC - AREAS OF LIGHT CORROSION ON UPPER AND LOWER SKIN OF RIGHT AILERON. REPAIRED IAW DHC 8 SRM 51-20-00 AND SRM 51-20-11.
- [SDR QXEA0000249](https://openairdocs.org/sdr/QXEA0000249), Jan 28, 2000: FRAME. CORRODED. YCC - GOUGE MARKS ON THREE FUSELAGE BULKHEAD FRAMES, FROM CONTACT WITH COLLAPSED WALL SUPPORT CHANNEL, STATION X653.34, X618.0 AND X636.0, BETWEEN STRINGERS 15S
- [SDR QXEA0000244](https://openairdocs.org/sdr/QXEA0000244), Jan 28, 2000: PANEL. DAMAGED. YYC - RIGHT ARMPIT PANEL 264BR, TWO ANCHOR NUTS REQUIRE REPLACEMENT. ANCHOR NUTS REPLACED IAW DHC SRM 51-40-11 AND RD 8-53-4758.
- [SDR QXEA0000239](https://openairdocs.org/sdr/QXEA0000239), Jan 28, 2000: SKIN. LIGHTNING STRIKE. YYC - LIGHTNING STRIKE PITS ALONG RIGHT SIDE OF FUSELAGE BETWEEN STATION X222.0 AND X424.12, BETWEEN STRINGER 26S AND 28S. REPAIRED IAW RD 8-53-4762.
- [SDR QXEA0000277](https://openairdocs.org/sdr/QXEA0000277), Jan 27, 2000: SKIN. CORRODED. YYC - RIGHT WING, OUTBOARD FLAP, SEVERAL FASTENERS HAVE CORROSION ON AND AROUND HEADS ON UPPER AND LOWER SKINS. REPAIRED IAW DHC 8 SRM 51-20-11, SRM 51-20-51.
- [SDR QXEA0000269](https://openairdocs.org/sdr/QXEA0000269), Jan 27, 2000: SKIN. CORRODED. YYC - CORROSION ON AND AROUND FASTENERS ON RIGHT AILERON. REPAIRED IAW DHC 8 SRM 51-20-00, SRM 51-20-11, SRM 51-40-00 AND SRM 57-60-16, PAGE 2, TABLE 1.
- [SDR QXEA0000265](https://openairdocs.org/sdr/QXEA0000265), Jan 27, 2000: STRUCTURE. GOUGED. YYC - GOUGES ON RIGHT FUSELAGE, 6 AFT OF STATION X333.3 BETWEEN STRINGER 16S AND 17S. REPAIRED IAW DHC 8 SRM 51-20-11, PAGE 3, SECTION B AND RD 8-53-2432.
- [SDR QXEA0000264](https://openairdocs.org/sdr/QXEA0000264), Jan 27, 2000: SKIN. DAMAGED. YYC - SCRATCH ON FUSELAGE ROOF BETWEEN STATION X618 AND X636, STRINGER 3P. REPAIRED IAW DHC 8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PAGE 4, SECTION C, 
- [SDR QXEA0000263](https://openairdocs.org/sdr/QXEA0000263), Jan 27, 2000: SKIN. DAMAGED. YYC - SCRATCH ON FUSELAGE ROOF ABOVE CARGO DOOR, APPROXIMATELY STATION X580.0, STRINGER 3P. REPAIRED IAW DHC 8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PA
- [SDR QXEA0000262](https://openairdocs.org/sdr/QXEA0000262), Jan 27, 2000: SKIN. DAMAGED. YYC - SCRATCH ON FUSELAGE ROOF, 6 FORWARD OF STATION 291.0, STRINGER 5S. REPAIRED IAW DHC 8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PAGE 4, SECTION C, SR
- [SDR QXEA0000261](https://openairdocs.org/sdr/QXEA0000261), Jan 27, 2000: STRUCTURE. DAMAGED. YYC - SCRATCHES ON FUSELAGE FOOR BEHIND COMM ANTENNA, APPROXIMATELY STATION X302.0 ON ROOF CENTER LINE. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, SECTION B, SRM 
- [SDR QXEA0000260](https://openairdocs.org/sdr/QXEA0000260), Jan 27, 2000: STRUCTURE. DAMAGED. YYC - SCRATCH ON RIGHT FUSELAGE, APPROXIMATELY STATION 467.0, STRINGER 15S. REPAIRED IAW DHC 8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PAGE 4, SECTION C,
- [SDR QXEA0000259](https://openairdocs.org/sdr/QXEA0000259), Jan 27, 2000: STRUCTURE. CORRODED. YYC - CORROSION SPOT ON RIGHT FUSELAGE, STATION 387.35, STRINGER 13S. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PAGE 4, SECTION C, SRM 5
- [SDR QXEA0000258](https://openairdocs.org/sdr/QXEA0000258), Jan 27, 2000: STRUCTURE. DAMAGED. YYC - SCRATCH ON RIGHT FUSELAGE AT APPROXIMATELY STATION 282.4, STRINGER 20S. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PAGE 4, SECTION 
- [SDR QXEA0000257](https://openairdocs.org/sdr/QXEA0000257), Jan 27, 2000: STRUCTURE. CORRODED. YYC - TWO NICKS/CORROSION SPOTS ON RIGHT SIDE FUSELAGE BETWEEN STATION X405.73 AND 424.12, STRINGER 16S AND 17S. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, SECTIO
- [SDR QXEA0000256](https://openairdocs.org/sdr/QXEA0000256), Jan 27, 2000: STRUCTURE. CORRODED. YYC - CORROSION SPOT ON RIGHT SIDE FUSELAGE, APPROXIMATELY STATION X545.01, STRINGER 12S. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PAGE
- [SDR QXEA0000255](https://openairdocs.org/sdr/QXEA0000255), Jan 27, 2000: STRUCTURE. GOUGED. YYC - SMALL GOUGE ON LEFT SIDE OF FUSELAGE, FORWARD OF STATION X167.0, STRINGER 18P. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PAGE 4, S
- [SDR QXEA0000254](https://openairdocs.org/sdr/QXEA0000254), Jan 27, 2000: STRUCTURE. DAMAGED. YYC - SCRATCHES ON LEFT SIDE OF FUSELAGE, APPROXIMATELY STATION X467.0, STRINGER 16P. REPAIRED IAW DHC-8 SRM 51-20-16, PAGE 3, SECTION B, SRM 51-20-16, PAGE 4, 
- [SDR QXEA0000253](https://openairdocs.org/sdr/QXEA0000253), Jan 27, 2000: STRUCTURE. DAMAGED. YYC - SMALL NICK IN LEFT FUSELAGE AT APPROXIMATELY STATION 480.0, STRINGER 13P. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PAGE 6, SECTIO
- [SDR QXEA0000252](https://openairdocs.org/sdr/QXEA0000252), Jan 27, 2000: STRUCTURE. CORRODED. YYC - TWO SMALL CORROSION SPOTS ON LEFT SIDE OF FUSELAGE JUST AFT OF CARGO DOOR, APPROXIMATELY STATION X606, STRINGER 17P. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE
- [SDR QXEA0000248](https://openairdocs.org/sdr/QXEA0000248), Jan 27, 2000: SEAT TRACK. CORRODED. YYC - LIGHT TO MODERATE CORROSION ON AFT SEAT TRACK, STATION X545.0 TO STATION X600.0, PARTICULARLY NEAR STATION 600.0, LEFT AND RIGHT TRACKS. REPAIRED IAW SRM 
- [SDR QXEA0000280](https://openairdocs.org/sdr/QXEA0000280), Jan 25, 2000: SKIN. DAMAGED. YYC - BAGGAGE DOOR EXTERNAL SKIN HAS A DEEP SCRATCH AT TOP OF DOOR. REPAIRED IAW DHC 8 SRM 51-20-11, PAGE 8, FIGURE 4, SRM 51-20-16, PAGE 4, SECTION C, SRM 51-2
- [SDR QXEA0000251](https://openairdocs.org/sdr/QXEA0000251), Jan 25, 2000: WEB. CORRODED. YYC - LIGHT CORROSION FOUND ON WEB FROM STATION X531.5 THROUGH TO STATION X600.0 AND AROUND THE AFT SEAT TRACK ON LEFT SIDE IN CARGO BAY AREA. REPAIRED IAW DHC-
- [SDR QXEA0000250](https://openairdocs.org/sdr/QXEA0000250), Jan 22, 2000: INTERCOSTAL. BENT. YYC - INTERCOSTAL FLANGE BENT, BAGGAGE COMPARTMENT, BETWEEN STATION X636.0 AND X653.34 AT STRINGER 18S. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 2, TABLE 1.
- [SDR QXEA0000247](https://openairdocs.org/sdr/QXEA0000247), Jan 22, 2000: ANGLE. CORRODED. YYC - LIGHT TO MODERATE CORROSION ON FLOOR SUPPORT ANGLE AT BASE OF COCKPIT FLOOR RISER BETWEEN THE INBOARD SEAT TRACKS, STATION 182.0. REPAIRED IAW SRM 51-20-1
- [SDR QXEA0000246](https://openairdocs.org/sdr/QXEA0000246), Jan 22, 2000: ANGLE. CORRODED. YYC - LIGHT CORROSION ON FLOOR TO RISER PANEL CLOSING ANGLE, STATION X600 FROM APPROXIMATELY AIRCRAFT CENTER LINE TO RIGHT END OF ANGLE. REPAIRED IAW SRM 51-20-
- [SDR QXEA0000272](https://openairdocs.org/sdr/QXEA0000272), Jan 21, 2000: SKIN. DEBONDING. YYC - RIGHT OUTBOARD LEADING EDGE HAS ALUMINUM STRIP DISBONDING ON UPPER EDGE. REPAIRED IAW DHC SRM 51-20-76, PAGES 1-5 AND RD 8-57-170.
- [SDR QXEA0000241](https://openairdocs.org/sdr/QXEA0000241), Jan 21, 2000: SKIN. DENTED. YYC - MULTIPLE DENTS IN FUSELAG SKIN, DIRECTLY AFT OF 229 AND LEFT ICE SHIELD, 6 FORWARD OF STN X333.30. APPROXIMATELY STRINGER 12P-13P. REPAIRED IAW DHC SRM 53
- [SDR QXEA0000245](https://openairdocs.org/sdr/QXEA0000245), Jan 17, 2000: SKIN. CORRODED. YYC - LIGHT CORROSION ON LAP JOINT, FUSELAGE ROOF STATION X370.80, STRINGER 3P. REPAIRED IAW SRM 51-20-11, SRM 51-20-16 AND SRM 51-20-26.
- [SDR QXEA0000240](https://openairdocs.org/sdr/QXEA0000240), Jan 17, 2000: SKIN. DENTED. YYC - DENT WITH DIMPLE CREASE IN THE CENTER, 4 FORWARD OF STATION 222.0, DIRECTLY ABOVE STRINGER 16S. REPAIRED IAW HORIZON AIR EA 9-53-537, DHC-8 SRM 53-00-16, 
- [SDR QXEA0000268](https://openairdocs.org/sdr/QXEA0000268), Jan 13, 2000: STRUCTURE. DAMAGED. YYC - SCRATCH ON FORWARD SPAR TOP SIDE OF BOTTOM LEADING EDGE ATTACH AREA BEHIND ANCHOR NUTS BETWEEN YW171.400 AND YW202..00. REPAIRED IAW DHC SRM 51-20-00 AND 
- [SDR QXEA0000243](https://openairdocs.org/sdr/QXEA0000243), Jan 13, 2000: SKIN. GOUGED. YYC - GOUGE IN FUSELAGE SKIN ON ROOF, 19 AFT OF STATION X312.36, APPROXIMATELY STRINGER 1S-2S. REPAIRED IAW DHC SRM 51-20-11, FIGURE 3 AND SRM 53-00-16, TABLE 1

All 77: https://openairdocs.org/deregistered/N826PH-2013-06-10/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB SEA97LA077](https://openairdocs.org/ntsb/SEA97LA077), Mar 26, 1997: de Havilland DHC-8 (N826PH), Wenatchee, WA, substantial damage. Probable cause: failure of the ground marshaller to marshal the airplane into a correct parking place on the ramp, her failure to verify clearance between the right wing of the airplane and the ground de-ice cart,…

## 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.

- [Accident 19970326003719A](https://openairdocs.org/incident/19970326003719A), Mar 26, 1997: Dhav DHC8102 (N826PH), Wenatchee, WA, Substantial damage. Aircraft struck a deice cart with its right wing while taxiing.

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