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CEN17FA331 · Beech A36 UNDESIGNAT

28 Aug 2017 · Ellabell, GA, United States

Beech A36 UNDESIGNAT · Accident: loss of engine power (total) en route

From Savannah Hilton Head International Airport (SAV) to Cobb County International Airport-McCollum Field (RYY)

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Event

NTSB case
CEN17FA331
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
3 · all aircraft and ground
Ground fatalities
Unknown
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Beech A36 UNDESIGNAT

Aircraft type
Beechcraft 36
Category
Airplane
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N87RY
Operator
Unknown
Onboard fatalities
Unknown
Route
From Savannah Hilton Head International Airport (SAV), Savannah, GATo Cobb County International Airport-McCollum Field (RYY), Atlanta, GA
Aircraft age
About 23 years (built 1994)
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
En route · climb to cruise
Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Loss of engine power (total)
Also codedOther events the NTSB coded in the sequence, such as a wire strike after a loss of power. Flight Findings uses them for its kinds of event. Glossary
Tree(s)
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Destroyed

Cause areas

  • Aircraft › Aircraft power plant
  • Personnel issues › Task performance

Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.

NTSB narrative

The commercial pilot was conducting a business flight; while climbing out after departure, the pilot declared an emergency and reported a loss of engine power to air traffic control. The controller provided vectors to a private airport about 6.5 nautical miles (nm) behind the airplane and stayed in communication with the pilot until communications and radar were lost. The airplane then began a wide turn to head back to the private airport, traveling about 6.3 nm during the turn. The airplane impacted trees and terrain about 6 miles from the private airport. The airplane's maintenance records showed that all six engine cylinders were replaced about 15 months and 227 engine hours before the accident. Postaccident examination of the engine revealed that four of the eight nuts that retained the No. 1 cylinder and one nut that retained the No. 2 cylinder were loose during disassembly, and no breakout torque reading could be measured. Two of the loose nuts on the No. 1 cylinder were on the through-studs that provided clamping force on the No.1 main crankshaft bearing. Disassembly of the crankcase revealed that the No. 1 main bearing had shifted to the rear of the crankcase, which obstructed the oil flow to the No. 1 main bearing and the No. 1 connecting rod bearing. Given the available evidence, it is likely that, during replacement of the engine cylinders, improper torque of the cylinder hold-down bolts and through-studs resulted in an insufficient clamping torque, which allowed the No. 1 main bearing to shift. This shift precluded oil from reaching the No. 1 main bearing and the No. 1 connecting rod bearing, which led to the failure of the connecting rod during the accident flight. The display map data used by the controller handling the flight did not depict another private airport, which was closer (3.4 nm) and was in more of a direct path from the airplane's heading and position at the time of the emergency. The Federal Aviation Administration order governing display map data stated that they should contain airports and heliports among other items, but noted that facility managers could delete items not required. The only exception was that facility managers could not delete airports immediately outside their area of jurisdiction that were within airspace used to receive radar handoffs and that were depicted by the facility having jurisdiction over that airspace. In response to questions from the NTSB, the closer airport was not depicted on the controller’s video display because the air traffic facility was not aware the airport existed. Since the accident, the airport has been added to the display map data. On the basis of the distance that the airplane was able to glide after the pilot declared the emergency (6.3 nm), the airplane should have been able to reach the closer airport that was ahead of it. Thus, the omission of this airport on the controller's display map data resulted in the pilot attempting, at the direction of the controller, to reach an airport that was beyond the airplane's gliding distance.

Probable cause

The total loss of engine power due to oil starvation to the No. 1 connecting rod, which resulted from the improper torque of the No. 1 cylinder hold-down bolts and through-studs at the time of the cylinder's installation, which resulted in the failure of the connecting rod due to oil starvation. Contributing to the accident was the omission, from the air traffic control display map data, of a closer alternate airport for the emergency landing.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record CEN17FA331
Event ID
20170828X23633
Case number
CEN17FA331
Dataset
full-current
Source SHA-256
5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status, coordinates. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: 846866bd133f2528be84ee7abfb6ea2c837c33715a59f818c8ef89d293cf86f2; retrieved 2026-09-15T06:14:35.966Z.