N882EABoeing / Dehavilland DHC-8-103
This N-number isn't registered right now. Below is its last known registration, canceled Nov 20, 2013.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched68 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 19, 2026- Last registered owner
- Wells Fargo Bank Northwest NA Trustee
- Owner type
- Corporation
- City, state
- Salt Lake City, UT
- Canceled
- Nov 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
- Boeing / Dehavilland
- Model
- DHC-8-103
- Serial number
- 098
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 39
- Engines
- 2
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- AC25A8
Engine
- Make and model
- None None
- Type
- Turbo-prop
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- until 2013Wells Fargo Bank Northwest NA TrusteeSalt Lake City, UT
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
ADs published since 1998 that may apply (0)
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.
No ADs published since 1998 matched this airframe or engine model.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (68)
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.
- Electrical power · generator · defectiveSep 14, 2013
ACFT NR 2 GENERATOR FAILED. R & R NR 2 AC GENERATOR IAW MM 24-21-01. OPS AND LEAK CHECKED GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Electrical power · oil cooler · defectiveAug 23, 2013
NR 2 AC GENERATOR HOT ANNUNCIATOR ILLUMINATED ON TAKEOFF. ENGINE OIL TEMP 110 DEGREES INDICATED. TAKEOFF ABORTED-NO FLIGHT. R & R NR 2 ENGINE OIL COOLER TEMPERATURE REGULATOR VALVE. GROUND RUN OPS AND LEAK CHECKED GOOD. OK FOR SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · light · inoperativeFeb 21, 2013
EMERGENCY LIGHT INOP AFT ROW CEILING. RELAMPED AS REQUIRED, OPS CHECK GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuselage · frame · corrodedDec 8, 2012
FRAME FOUND CORRODED AT STATION X312 BETWEEN STRINGER 29P AND 30P AND 31P AND 32P. REPAIRED TO BOMBARDIER SRM 53-00-16.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · seat track · corrodedDec 8, 2012
CORROSION FOUND ON LEFT INBOARD SEAT TRACK. REPAIRED TO BOMBARDIER REPAIR DRAWING 8-53-3074.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin panel · gougedDec 8, 2012
SKIN DAMAGE TO RIGHT FUSELAGE SKIN AT STATION X342 BETWEEN STRINGER 12S AND 13S. REPAIRED TO BOMBARDIER REPAIR DRAWING 8-53-2181.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · crackedDec 8, 2012
CRACK FOUND ON RIGHT FUSELAGE FRAME AT STATION X354 BETWEEN STATION 20S AND 33S.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · nickedDec 8, 2012
NICK ON SKIN AT RIGHT FUSELAGE AT STATION X342 BETWEEN STRINGER 12S AND 13S. REPAIRED TO BOMBARDIER REPAIR DRAWING 853-2181.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · access panel · corrodedDec 7, 2012
LEFT STRESS PANEL HAS CORROSION UNDER COUNTERSINK SCREW HOLES. REPLACED LEFT STRESS PANEL P/N 85711802-005.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · access panel · corrodedDec 7, 2012
RIGHT STRESS PANEL HAS CORROSION UNDER COUNTERSINK SCREW HOLES. REPLACED RIGHT STRESS PANEL 85711802-005.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 68 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026