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Accidents · NTSB CEN18LA084 · Final report

Beech A36 accident near Abilene, Texas, January 22, 2018

On January 22, 2018 at about 2:45 pm local time, a 1978 Beech A36, registered N3600A, was substantially damaged in an accident during enroute (climb to cruise) near Abilene, Texas (Dyess Air Force Base airport). It was a personal flight under general aviation rules (Part 91). 1 person was seriously injured. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

Maintenance personnel’s improper maintenance of the engine, which resulted in a catastrophic engine failure due the shifting/slipping of the No. 2 bearing and the subsequent oil starvation and total loss of engine power during cruise flight.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
January 22, 2018 · about 2:45 pm local time
Place
Abilene, Texas · Dyess Air Force Base · map
Type
Accident
Injuries
1 person was seriously injured.
Weather
visual conditions (good weather)
Aircraft
Beech A36, built 1978 · all A36s on the register
Registration
N3600A · no longer on the register · serial E-1328
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The private pilot was conducting a cross-country, personal flight. He stated that, upon leveling off at cruise altitude, there was a "severe vibration" coming from the engine compartment, followed by a sound of the engine "coming apart." Oil covered the windshield, and the smoke entered the cockpit. The pilot was unable to return to the departure airport because it was beyond gliding distance, so he performed a forced landing on a field with the landing gear and flaps retracted. The pilot sustained serious injuries. Postaccident examination of the engine revealed a large hole in the left crankcase half over the No. 2 cylinder attachment point and a small hole in the right crankcase half over the No. 5 cylinder attachment point. The No. 2 main bearing had shifted in the bearing saddle, which cut off the oil supply to the No. 2 rod cap bearing. Shifting/slipping of the bearing can result from either improper torque application during cylinder replacement or improper grinding of the bearing journal during maintenance. The engine had been disassembled twice before the accident. An engine logbook entry showed that the No. 2 cylinder had been removed and replaced about 328 hours before the accident. It is likely that maintenance personnel did not conduct proper maintenance on the No. 2 cylinder during reassembly of the engine and that this ultimately led to the catastrophic engine failure due the shifting/slipping of the No. 2 bearing and the subsequent oil starvation and total loss of engine power.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

What happened, in order

  1. Aircraft maintenance event during prior to flight
  2. Powerplant sys/comp malf/fail during enroute (climb to cruise) defining event
  3. Loss of engine power (total) during enroute (climb to cruise)
  4. Off-field or emergency landing during landing
  5. Miscellaneous/other during landing

The NTSB's findings

  • cause Personnel issues › Task performance › Maintenance › Repair › Maintenance personnel
  • cause Aircraft › Aircraft power plant › Engine (reciprocating) › (general) › Failure
  • cause Aircraft › Fluids/misc hardware › Fluids › Oil › Not specified
  • cause Aircraft › Aircraft handling/service › Maintenance/inspections › Scheduled maint checks › Incorrect service/maintenance

Pilot

  • Certificate: private
  • Ratings: single-engine land
  • Flight time: 702 hours in all; 350 in this make and model; 7 in the last 90 days; 2 in the last 30 days; 702 as pilot in command; 0 on instruments
  • Last flight review: November 2, 2016
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: left
  • Injury: serious injuries

The aircraft

  • Airframe total time: 4,501 hours
  • Last inspection: annual inspection, February 9, 2017; 58 hours since
  • Maximum gross weight: 3,600 lb
  • Seats: 6
  • Landing gear: retractable
  • Engine: Continental IO-520-BA (piston); 1,997 hours total

The flight

  • Departed from: ABI Abilene TX at 2:35 pm
  • Destination: DYS Abilene TX
  • Flight plan: VFR

Weather at the time

  • Light: daylight
  • Wind: from 280° at 12 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 41°F (5°C), dew point 18°F (-8°C)
  • Altimeter: 30.12 inHg

Injuries

FatalSeriousMinorNone
Flight crew1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

5 documents, released by the NTSB on March 25, 2019. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.

The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.