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Aircraft record

N1QB2006 Perry Richard Lee LANCAIR 1VP

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

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

Safety record in brief:No NTSB accidents or incidents since 19822 ADs may apply1 service difficulty report

Registration
Deregistered
Last based in
Malta, IL
owner city / state
Engine
TSIO-550-E · 350 hp
Cont Motor
Owners
1
on record
NTSB events
None
since 1982
ADs may apply
2
confirm with A&P
Service reports
1
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Individual owner
City, state
Malta, IL
Canceled
Aug 24, 2017
Airworthiness
Experimental · Amateur Built
Airworthiness date
Aug 29, 2006

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
Perry Richard Lee
Model
LANCAIR 1VP
Year
2006
Serial number
319
Aircraft type
Fixed wing single engine
Category
Land
Certification
Not Type Certificated
Seats
4
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
A00162

Engine

Make and model
Cont Motor Tsio-550-E
Type
Reciprocating
Power
350 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. until 2017Individual ownerMalta, IL

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 (0)

No NTSB accidents or incidents found for this airframe since 1982.

ADs published since 1998 that may apply (2)

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
2023-05-16Reciprocating Engine Power SectionMar 15, 2023Engine (TSIO-550-E)
2020-16-11Reciprocating Cylinder SectionSep 21, 2020Engine (TSIO-550-E)Only with: Engines originally manufactured, rebuilt, or modified with a cross-flow cylinder assembly replacement on or after November 1, 2014, with cross-flow cylinder assembly P/N 658538, 658540, 658542, 658591, 658595, 658613, 658624, 658539, 658541, 658590, 658594, 658603, 658623, or 658630 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 (1)

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.

  • Structures (general) · step · damagedSep 14, 2005

    RETRACTABLE STEP ASSEMBLY MECHANISM IS ATTACHED TO THE LANDING GEAR STRUT BY A STEEL BRAIDED CABLE WITH METAL CLAMP. CLAMP AROUND STRUT ROTATED ALLOWING EXCESSIVE SLACK IN THE CABLE. WHEN THE LT LANDING GEAR WAS EXTENDED IT CAME IN CONTACT WITH THE RETRACTABLE STEP ASSEMBLY AND WOULD NOT ALLOW THE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.

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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