Single-engine piston

N44MH

1979 Commander 112TCA

Registered 1 NTSB/FAA record
Built
1979
Serial
13308
Class
Single-engine piston
Engines
Lycoming T0-360 series
Status
Current as of October 2026
Registered owner
Individual · sign in to see
Based
Dayton, TX
1979 Commander 112TCA
Representative photo of a Commander 112TCA. Not a photo of N44MH.
Registration record

N44MH on the FAA register

Type
1979 Commander 112TCA
Serial
13308
Engines
Lycoming T0-360 series
Registered owner
Individual — the name of an individual registrant is shown to signed-in users. Sign in
Dayton, TX
Certificate issued
2018-10-23
Airworthiness date
1998-02-06
Registration expires
2028-10-31
Airworthiness class
Standard · normal, utility
Mode S (hex)
A5495F
Mode S (octal)
51244537
Seats (type)
4
Weight class
up to 12,499 lb
Range (type)
765 nm
Cruise (type)
163 kt
Status
Current as of October 2026
Registry history

Timeline

  • 2028-10-31
    Registration expires (renewal due).
  • 2018-10-23
    Certificate of registration issued as N44MH to the current registrant.
  • 2004-08-31
    Accident at San Rafael, CA; damage: substantial.
  • 1998-02-06
    Airworthiness date on the current FAA record (standard category (normal, utility)).
  • 1988-04-20
    N44MH previously assigned to a Beechcraft 58 Baron (s/n TH615); cancelled.
  • 1979
    Manufactured (1979).
Overview

About N44MH

N44MH is a 1979 Commander 112TCA, serial number 13308. It is registered to an individual in Dayton, Texas. The current certificate of registration was issued on October 23, 2018 and expires on October 31, 2028.

The FAA aircraft reference file describes the type as a single-engine piston, one Lycoming T0-360 series engine and 4 seats. Published figures for the type give a cruise speed of about 163 knots and a range of about 765 nm; actual performance depends on configuration, load and conditions. Its airworthiness certificate is standard category (normal, utility), dated February 6, 1998.

N44MH has 1 accident/incident record on file (most serious damage: substantial); details are below.

Cruise
163 kt
Range
765 nm
Landing over 50 ft
680 ft
Fuel burn
14 gph

Published figures for the Commander 112TCA type. They describe the model, not this airframe's equipment or condition.

Safety record

Accident & incident history

2004-08-31 Accident · San Rafael, CA Damage: Substantial Minor injury NTSB · LAX04LA308
Reported aircraft: Rockwell 112TCA
Probable cause: A total loss of engine power during initial climb due to fuel starvation, which was caused by the pilot's failure to turn on the electric boost pump and an undetermined failure of the engine driven pump to supply sufficient fuel to the carburetor.

Sources: NTSB aviation accident database and CAROL case system, FAA preliminary accident & incident notices. Search accident records

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Data: FAA Aircraft Registry (October 2026), including deregistered aircraft; NTSB and FAA accident data; fyiAero listing history. Individual owners' names are shown to signed-in users and street addresses are never shown. Type figures are published specifications, not this aircraft's.