Single-engine piston

N310MA

2023 Piper Archer TX

Registered No accidents on file
Built
2023
Serial
28020104
Class
Single-engine piston
Engines
Lycoming IO-360-B4A
Status
Current as of October 2026
Registered owner
Mbm Leasing LLC (LLC)
Based
Saint Louis, MO
Registration record

N310MA on the FAA register

Type
2023 Piper Archer TX (FAA: Piper PA-28-181)
Serial
28020104
Engines
Lycoming IO-360-B4A
Registered owner
Mbm Leasing LLC
Saint Louis, MO
Certificate issued
2024-07-22
Airworthiness date
2023-01-28
Registration expires
2031-07-31
Airworthiness class
Standard · normal
Mode S (hex)
A347E5
Mode S (octal)
50643745
Seats (type)
4
Weight class
up to 12,499 lb
Status
Current as of October 2026
Registry history

Timeline

  • 2031-07-31
    Registration expires (renewal due).
  • 2024-07-22
    Certificate of registration issued as N310MA to the current registrant.
  • 2023-01-28
    Airworthiness date on the current FAA record (standard category (normal)).
  • 2013-08-06
    N310MA previously assigned to a Mitsubishi MU-2B-20 (s/n 167); cancelled.
Overview

About N310MA

N310MA is a 2023 Piper Archer TX (FAA model PA-28-181), serial number 28020104. The FAA register lists Mbm Leasing LLC as the registrant in Saint Louis, Missouri. The current certificate of registration was issued on July 22, 2024 and expires on July 31, 2031.

The FAA aircraft reference file describes the type as a single-engine piston, one Lycoming IO-360-B4A engine and 4 seats. Its airworthiness certificate is standard category (normal), dated January 28, 2023.

No NTSB accident or incident reports and no FAA preliminary notices are on file for this airframe as N310MA. 1 earlier record involves a different aircraft that carried the same N-number.

Safety record

Accident & incident history

1996-04-07 Accident · Batesville, MS Damage: Substantial NTSB · ATL96LA078
Reported aircraft: Mitsubishi MU-2B — a different aircraft that carried the N310MA registration before this airframe.
Probable cause: an anomaly in the fuel system that allowed a pressure differential to occur between the center and outer portions of the main integral fuel tank, which in turn resulted in fuel starvation of both engines. A factor relating to the accident was: failure of company maintenance personnel to remove fuel system vent check valves as recommended by Mitsubishi MU-2 Service Bulletin 130A.

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.