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Aircraft record

N4035G1982 Fairchild Hiller FH-1100

DeregisteredUnclaimedSource: FAA, updated Oct 18, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Nov 29, 2019.

Safety record in brief:2 NTSB accidents (destroyed damage at worst, latest Oct 2016)3 ADs may apply

Registration
Deregistered
Last based in
Minneapolis, MN
owner city / state
Engine
250-C20B · 420 hp
Allison
Owners
1
since 2016
NTSB events
2
destroyed, 2016
ADs may apply
3
confirm with A&P
Service reports
0
since 1995

Registration

FAA Aircraft Registry · Oct 18, 2026
Last registered owner
Helicopter Connection LLC
Owner type
LLC
City, state
Minneapolis, MN
Certificate issued
Aug 18, 2016
Canceled
Nov 29, 2019
Airworthiness
Standard · Normal
Airworthiness date
Oct 20, 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
Fairchild Hiller
Model
FH-1100
Year
1982
Serial number
502
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
4
Engines
1
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
H2WE
Mode S code
A4BAD4

Engine

Make and model
Allison 250-C20b
Type
Turbo-shaft
Power
420 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. 2016 – 2019Helicopter Connection LLCMinneapolis, MN
  2. 1970 – 1972Individual ownerFort Worth, TX · different airframe: Bell 47g-5 S/N 7890

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 2026 · SDRs · Oct 16, 2026

NTSB events (2)

Accident · destroyed

Oct 6, 2016 · Lino Lakes, MN

The separation of the main rotor assembly due to mast bumping.

Damage
Destroyed
Injuries
Fatal
Report
CEN17FA012

From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN17FA012)

Accident · substantial damage

Jun 8, 2006 · Navarre, FL

The inadequate manufacturing of the plates of the tail rotor tension-torsion bar assembly resulting in fatigue failure.

Damage
Substantial
Injuries
None
Report
MIA06LA126

From NTSB records; matched by serial number.Read NTSB report (search CAROL for MIA06LA126)

Accident history for this model

ADs 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.

ADSubjectEffectiveApplies to
2006-16-04Rolls-Royce Corporation (Formerly Allison Engine Company, Allison Gas Turbine Division…Sep 7, 2006Engine (250-C20B)
2006-13-06Rolls-Royce Corporation (Formerly Allison Engine Company, Allison Gas Turbine Division…Jul 26, 2006Engine (250-C20B)Only with: Engines with gas producer rotor assembly tie bolt P/Ns A23008020, E23008020 (EXTEX), 23008020, 6843388, 6876991 (RRC), A23008020 (SAP), or 23008020P (Pacific Sky Supply) installed.
2005-10-13Rolls-Royce Corporation (Formerly Allison Engine Company) 250-B17B, -B17C, -B17D, -B17E…Jun 22, 2005Engine (250-C20B)Only with: Engines that do not have turbine energy absorbing ring RRC P/N 23035175, or an equivalent FAA-approved serviceable ring, 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 18, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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