Twin piston

N40978

1981 Piper Navajo Chieftain

Registered 2 NTSB/FAA records
Built
1981
Serial
31-8152199
Class
Twin piston
Engines
2 × Lycoming IO-540 series
Status
Current as of October 2026
Registered owner
Dodson International Parts Inc (Corporation)
Based
Rantoul, KS
Registration record

N40978 on the FAA register

Type
1981 Piper Navajo Chieftain (FAA: Piper PA-31-350)
Serial
31-8152199
Engines
2 × Lycoming IO-540 series
Registered owner
Dodson International Parts Inc
Rantoul, KS
Certificate issued
—
Airworthiness date
1981-11-13
Registration expires
—
Airworthiness class
Standard · normal
Mode S (hex)
A4D17E
Mode S (octal)
51150576
Seats (type)
8
Weight class
up to 12,499 lb
Status
Current as of October 2026
Registry history

Timeline

  • 2006-07-11
    Accident at Indianapolis, IN; damage: substantial.
  • 1989-03-02
    Accident at Toms River, NJ; damage: substantial.
  • 1981-11-13
    Airworthiness date on the current FAA record (standard category (normal)).
  • 1975-02-24
    N40978 previously assigned to a Piper Cherokee 180 / Archer / Challenger 180 (s/n 28-7405080); cancelled.
Overview

About N40978

N40978 is a 1981 Piper Navajo Chieftain (FAA model PA-31-350), serial number 31-8152199. The FAA register lists Dodson International Parts Inc as the registrant in Rantoul, Kansas.

The FAA aircraft reference file describes the type as a twin piston, two Lycoming IO-540 series engines and 8 seats. Its airworthiness certificate is standard category (normal), dated November 13, 1981.

N40978 has 2 accident/incident records on file (most serious damage: substantial); details are below.

Safety record

Accident & incident history

2006-07-11 Accident · Indianapolis, IN Damage: Substantial NTSB · CHI06CA181
Reported aircraft: Piper PA-31-350
Probable cause: The failure of the tug driver to maintain clearance from the airplane taxiing on an active taxiway. A factor was the night conditions.
1989-03-02 Accident · Toms River, NJ Damage: Substantial NTSB · NYC89FA093
Reported aircraft: Piper PA-31-350
Probable cause: FAILURE OF THE PILOT TO MAINTAIN AIRSPEED AND CONTROL OF THE AIRCRAFT, AND HIS EXCEEDING THE DESIGN STRESS LIMITS OF THE AIRCRAFT. FACTORS RELATED TO THE ACCIDENT WERE: AUTOPLT MALFUNCTION DUE TO IMPROPER INSTALLATION BY MAINTENANCE PERSONNEL AND THE PILOT'S FAILURE TO PREFLIGHT THE AUTOPILOT BEFORE USING IT IN FLIGHT.

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.