N356PH1997 Dehavilland DHC-8-202
This N-number isn't registered right now. Below is its last known registration, canceled Jun 16, 2014.
Safety record in brief:No NTSB accidents or incidents since 19823 ADs may apply206 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Airborne Services Global II LLC
- Owner type
- Corporation
- City, state
- Sparks, NV
- Certificate issued
- Sep 19, 2012
- Canceled
- Jun 16, 2014
- Airworthiness
- Experimental · Crew Training, Market Survey
- Airworthiness date
- May 20, 2013
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Dehavilland
- Model
- DHC-8-202
- Year
- 1997
- Serial number
- 502
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 40
- Engines
- 2
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- A3FC64
Engine
- Make and model
- P&W Canada Pw123d
- Type
- Turbo-prop
- Power
- 1950 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2012 – 2014Airborne Services Global II LLCSparks, NV
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (3)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2013-15-08 | Pratt & Whitney Canada Corp. Turboprop Engines | Sep 17, 2013 | Engine (PW123D)Serial numbers per Table 1 of the Appendix of P&WC Service Bulletin No. PW100-72-21823, Revision 3. Only with: First-stage power turbine blade P/N 3120973-01, 3120983-01, or 3054053-01 installed with a serial number listed in the referenced SB table. |
| 2012-26-08 | Pratt & Whitney Canada Corp. Turboprop Engines | Feb 15, 2013 | Engine (PW123D)Serial numbers per P&WC ASB No. PW100-72-A21813 Rev 3, PW100-72-A21802 Rev 4, and PW100-72-A21798 Rev 5. Only with: Engines with propeller shafts having serial numbers listed in the referenced P&WC ASBs. |
| 2004-20-01 | Pratt & Whitney Canada Models PW123, PW123B, PW123C, PW123D, PW123E, PW123AF, PW124B… | Nov 5, 2004 | Engine (PW123D)Only with: Mechanical fuel controls (MFCs) P/Ns 3244841-21, 3244853-17, 3244855-15, 3244857-14, 3244858-23, 3244871-5, 3244873-4, and 3244874-4 installed. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (206)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Engine indicating · indicator · failedApr 25, 2008
PDX- FLIGHT 2011, RETURNED TO THE FIELD FOR A NR 1 ENGINE TORQUE SURGE. ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE PRESSURE TRANSDUCER WITH NO HELP. THEN REPLACED THE PRESSURE INDICATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedMar 30, 2008
PDX-C5 CHECK- AFT BAG PIT UPPER SKIN AT A LIGHTENING HOLE HAS LIGHT CORROSION FORMING IN RECESS HOLE Z100 X557 AND 27L. BLENDED OUT CORROSION AND MEASURED BLENDED AREA IAW DASH 8 200 SRM 51-20-11. ALODINED, PRIMED, AND PAINTED BLENDED AREA IAW DHC 8 200 SRM 51-20-16, AND 51-20-36. (S)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · structure · corrodedMar 30, 2008
PDX-C5 CHECK. CORROSION ON FLANGE AT GALLEY OUTBOARD AFT ATTACH POINT AT STA X227.70. BLENDED SURFACE CORROSION APPROX .001 MATERIAL REMOVED IAW DHC 8 200 SRM. ETCHED, ALODINED AND PRIMED SURFACE IAW DHC 8 200 SRM 51-20-16. (S)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Wings · flap track · wornMar 30, 2008
PDX-C5 CHECK- LT NR 3 FLAP TRACK HAS SEVERAL AREAS OF WEAR ON THE LOWER HORIZONTAL TRACK UPPER SURFACE APPROX .500 INCHES BY .300 INCHES BY .010 DEEP. BLENDED AFFECTED AREAS ON NR 3 FLAP TRACK LOWER HORIZONTAL UPPER IAW RD8-57-987. HFEC INSPECTED BLENDED AREAS FOR CRACK IAW D8 200 NDTM PART 6…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · damagedMar 30, 2008
BURNED RIVET AT STA X190.00 APPROX 1 INCH BELOW STR 4L. REMOVED RIVET AND FOUND DAMAGE LIMITED TO ONE RIVET ONLY. INSTALLED RIVET IAW D8-200 SRM 51-40-11. (S)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedMar 30, 2008
UPPER COMM ANTENNA HAS CORROSION ON MOUNTING AREA ON ACFT SKIN. REMOVED LIGHT CORROSION IAW CPC MANUAL CHAPTER 4 AND SRM 51-20-11. NO MEASURABLE MATERIAL REMOVED. (S)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · skin · dentedMar 30, 2008
PDX-C4 CHECK FOUND DENT ON THE BOTTOM OF THE RT ELEVATOR AT STN YH92.20, APPROX 13 INCHES FWD OF THE AFT SPAR. FOUND OUT OF LIMITS IAW RD8-55-1448. HFEC INSP FOR CRACKS, NO CRACKS NOTED. REMOVED RIVETS, FABRICATED REPAIR DOUBLER IAW RD8-55-1930. INSTALLED DOUBLER IAW RD8-55-1930 STEPS 9-13. (S)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · skin · damagedMar 30, 2008
PDX -C4 CHECK- FOUND A CREASE ON THE BOTTOM OF THE RT ELEVATOR AT STN YH94.20, APPROX 6 INCHES FWD OF THE AFT SPAR. CREASE IS APPROX 5.5 INCHES LONG. FOUND OUT OF LIMITS IAW RD8-55-1448. HFEC INSP FOR CRACKS, NO CRACKS NOTED. REMOVED RIVETS, FABRICATED REPAIR DOUBLER IAW RD8-55-1930. INSTALLED…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · flap track · wornMar 30, 2008
PDX-C4 CHECK - LT WING NR 5 FLAP TRACK OUTBOARD LOWER TRACK UPPER SURFACE HAS WEAR MARKS. BLENDED IAW RD8-57-989. HFEC INSPECTED IAW D8-200 NDTM PART 651-00-01. NO CRACKS NOTED. (S)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · damagedMar 30, 2008
PDX-C4 CHECK - BURNT RIVET APPROX 6 INCHES AFT OF STA X160.500 & 3 INCHES OUTBOARD OF STR 4L. REPAIRED DAMAGE TO SKIN PER D8-200 RD8-53-137 PG 3 STEP 1. HFEC IAW PSM 1-82-7A PART 6 51-00-02 PER RD8-53-137. NO DEFECTS NOTED. (S)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 206 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026