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Aircraft record

N120WA1982 Embraer EMB-110P1

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:1 NTSB accident (substantial damage, May 1985)1 AD may apply

Registration
Valid
expires Jan 31, 2033
Based in
North Salt Lake, UT
owner city / state
Engine
PT6A-60A · 1050 hp
P&W Canada
Owners
1
since 2026
NTSB events
1
substantial, 1985
ADs may apply
1
confirm with A&P
Service reports
0
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Registered owner
Tvpx Aircraft Solutions INC Trustee
Owner type
Corporation
City, state
North Salt Lake, UT
Certificate issued
Jan 1, 2026
Expires
Jan 31, 2033
Airworthiness
Standard · Normal
Airworthiness date
Jul 12, 1982

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 data

Airframe

Manufacturer
Embraer
Model
EMB-110P1
Year
1982
Serial number
110.404
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
20
Engines
2
Max takeoff weight
12,500 - 19,999 lb
Mode S code
A055A7

Engine

Make and model
P&W Canada Pt6a-60a
Type
Turbo-prop
Power
1050 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2026 – nowTvpx Aircraft Solutions INC TrusteeNorth Salt Lake, UT · current
  2. 2000 – 2009Individual ownerRockwood, ME · different airframe: 1946 Piper Pa-12 S/N 12-1519
  3. 1998 – 2000International Aviation Specialists LtdWilminton, DE · different airframe: Piper Pa-31 S/N 31-460

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Accident · substantial damage

May 20, 1985 · Atlanta, GA

THE ACFT WAS ON FINAL APCH WHEN THE CIRCUIT BREAKER CAUTION LIGHT ILLUMINATED. THE PIC FAILED TO VERIFY WHICH CB TRIPPED AND ASSUMED IT WAS THE GEAR CONTROL CB. PIC THEN ACTIVATED EMERG HYDRAULIC SYS AND MANUALLY LOWERED THE GEAR. AFTER LANDING THE HYDRAULIC SELECTOR WAS LEFT IN THE EMERG POSITION WHICH RESULTED IN THE TOE BRAKES HAVING ONLY NORMAL ACCUMULATOR PRESSURE. NORMAL ACCUMULATOR…

Damage
Substantial
Injuries
None
Report
ATL85FA168

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ATL85FA168)

Accident history for this model

ADs published since 1998 that may apply (1)

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.

ADSubjectEffectiveApplies to
2002-23-13Pratt & Whitney Canada PT6A Series Turboprop EnginesDec 31, 2002Engine (PT6A-60A)Only with: Engines with turbine exhaust ducts P/N 3012290, 3031988, 3032117, 3035784, 3035786, 3105890-01, 3112167-01, or 3111780-01 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 (0)

No Service Difficulty Reports found for this airframe since 1995.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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