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Aircraft record

N100VL1986 Verilite Aircraft Company INC V-100

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Mar 24, 2017.

Safety record in brief:1 NTSB accident (substantial damage, Apr 1987)No ADs since 1998 matched

Registration
Deregistered
Last based in
Santa Fe, NM
owner city / state
Engine
UNKNOWN ENG
Ama/Expr
Owners
1
since 1987
NTSB events
1
substantial, 1987
ADs may apply
0
confirm with A&P
Service reports
0
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Verilite Aircraft Co INC
Owner type
Corporation
City, state
Santa Fe, NM
Certificate issued
Apr 1, 1987
Canceled
Mar 24, 2017
Airworthiness
Experimental · Amateur Built
Airworthiness date
Feb 11, 1998

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
Verilite Aircraft Company INC
Model
V-100
Year
1986
Serial number
001
Aircraft type
Fixed wing single engine
Category
Land
Certification
Not Type Certificated
Seats
2
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
A0069A

Engine

Make and model
Ama/Expr Unknown Eng
Type
Reciprocating

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

Ownership history

Ownership history from FAA records
  1. 1987 – 2017Verilite Aircraft Co INCSanta Fe, NM

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Accident · substantial damage

Apr 18, 1987 · Albuquerque, NM

AN EXPERIMENTAL DESIGNED PROTOTYPE ACFT WAS BEING FLOWN ON ITS FIRST FLT. THE ACFT TOOK OFF AND FLEW IN GROUND EFFECT BEYOND THE ARPT BOUNDARY. AT FULL PWR, THE ACFT COULD NOT MAINTAIN ALTITUDE AND DESCENDED UNCONTROLLED TO AN IMPACT WITH THE TERRAIN. THE NOSE GEAR COLLAPSED AND THE ACFT NOSED OVER. ORIGINAL DESIGN OF THE ACFT WAS 950 LBS GW WITH A 60 HP ENG. AS THIS PROTOTYPE WAS EQUIPPED ITS…

Damage
Substantial
Injuries
None
Report
DEN87LA104

From NTSB records; matched by N-number.Read NTSB report (search CAROL for DEN87LA104)

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 (0)

No Service Difficulty Reports found for this airframe since 1995.

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

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