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Accidents · NTSB ERA14FA074 · Final report

Raytheon G36 accident near Panama City, Florida, December 18, 2013

On December 18, 2013 at about 1:20 pm local time, a 2006 Raytheon G36, registered N89SN, was substantially damaged in an accident during enroute (cruise) near Panama City, Florida (Sandy Creek Airpark airport). It was a business flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot’s inadequate preflight and inflight fuel planning, which resulted in a total loss of engine power due to fuel exhaustion. Contributing to the pilot’s injuries was his failure to use the available shoulder harness.

Source: NTSB aviation accident database, copy made November 2, 2026. Docket and reports at the NTSB.

What the record shows

Date
December 18, 2013 · about 1:20 pm local time · cases in 2013
Place
Panama City, Florida · Sandy Creek Airpark · cases near this airport · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Raytheon G36, built 2006
Registration
N89SN · registry record · serial E-3738
Damage
Substantial damage
Flight
Business flight · general aviation rules (Part 91)

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

The flight was about 60 miles from the destination airport when the pilot reported a total loss of engine power to air traffic control. The controller provided information on nearby airports, and the pilot maneuvered the airplane toward the closest airport. The pilot reported the airport in sight; radio and radar contact were subsequently lost. A search for the airplane was initiated, and the wreckage was located in a heavily wooded swamp about 1 mile east of the airport. There were no known witnesses to the accident. The fuel tank selector handle was found in the "left main" (left wing tank) position. The left wing tank was not breached, and about 1 pint of fuel was recovered from the tank. The right tank was breached, and it contained residual fuel; however, there was no evidence of fuel leakage on the ground beneath the tank. The airplane was fitted with optional wing tip tanks, which were found empty. The total amount of fuel recovered, including the residual fuel in the tanks and fuel recovered from a small pool of water directly under the airplane, was about 2.5 gallons, which was less than the manufacturer-reported unusable fuel quantity of 6 gallons. The airplane was last serviced with fuel about 28 days before to the accident; however, the total fuel onboard at that time could not be determined. The propeller blades exhibited no rotational damage or signatures. After the accident, the engine was removed from the airframe and successfully test run at the manufacturer's facilities; no evidence of pre-accident malfunction or failure was observed. Although a shoulder harness was available, the pilot was found in the left seat with only his lap belt fastened. Damage to the airplane's multi-function display was consistent with impact by the pilot's head during the accident sequence. The pilot's cause of death was blunt force head trauma, and the impact forces that he experienced would likely have been reduced if he had been wearing his shoulder harness.

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. Fuel exhaustion during enroute (cruise) defining event
  2. Collision with terrain or object (not controlled flight into terrain) during emergency descent

The NTSB's findings

  • cause Aircraft › Fluids/misc hardware › Fluids › Fuel › Fluid level other cases naming the fuel system
  • cause Personnel issues › Task performance › Planning/preparation › Fuel planning › Pilot
  • factor Aircraft › Aircraft systems › Equipment/furnishings › Emergency equipment › Not used/operated other cases naming the cabin, seats and restraints
  • factor Personnel issues › Action/decision › Action › Lack of action › Pilot

Pilot

  • Certificate: airline transport pilot
  • Ratings: multi-engine land; single-engine land; instrument: airplane
  • Flight time: 5,000 hours in all; 53 in this make and model
  • Medical certificate: Class 1 (with waivers/limitations)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 734 hours
  • Last inspection: annual inspection, August 22, 2013; 51 hours since
  • Maximum gross weight: 3,650 lb
  • Seats: 6
  • Landing gear: retractable
  • Engine: Continental IO-550B (piston); 734 hours total
  • Operator: Grey Aviation Advisors & Solutions INC

The flight

  • Departed from: F45 West Palm Beach FL at 10:54 am
  • Destination: DTS Destin FL
  • Flight plan: IFR
  • Runway 27, 3,850 ft by 150 ft

Weather at the time

  • Light: daylight
  • Wind: from 020° at 9 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 48°F (9°C), dew point 39°F (4°C)
  • Altimeter: 30.31 inHg
  • Observation at 12:58 pm from PAM, 5 miles away

Injuries

FatalSeriousMinorNone
Flight crew1

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

27 documents, released by the NTSB on December 17, 2014. 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.

#DocumentWhat it is
1 Transcript of Communications - Tyndall Afb ATC PDF, 10 pages View Download
2 Airplane Flight Log Excerpt PDF, 1 page View Download
3 Maintenance Logbooks Excerpts PDF, 5 pages View Download
4 Fuel Records PDF, 4 pages View Download
5 Memorandum for Record - Recent Fueling at F45 PDF, 1 page View Download
6 Bay County Sheriff Incident Report PDF, 2 pages View Download
7 Engine Operational Test Log PDF, 1 page View Download
8 Flight Path and Accident Site Diagrams PDF, 2 pages View Download
9 Toxicological Report PDF, 1 page View Download
10 Certification of Party Representative PDF, 15 pages View Download
11 Release of Aircraft Wreckage, NTSB Form 6120.15 PDF, 1 page View Download
12 Evidence Control PDF, 1 page View Download
13 Photo 1 - Main Wreckage PDF, 1 page View Download
14 Photo 2 - Empennage PDF, 1 page View Download
15 Photo 3 - Fuselage and Empennage PDF, 1 page View Download
16 Photo 4 - Propeller Blade and Engine Compartment PDF, 1 page View Download
17 Photo 5 - Engine Cowling PDF, 1 page View Download
18 Photo 6 - Engine Compartment and Engine, Cowling Opened PDF, 1 page View Download
19 Photo 7 - Left Wing Inboard PDF, 1 page View Download
20 Photo 8 - Forward Fuselage and Left Wing PDF, 1 page View Download
21 Photo 9 - Left Wing PDF, 1 page View Download
22 Photo 10 - Main Wreckage, Right Side PDF, 1 page View Download
23 Photo 11 - Fuel Tank Selector Handle PDF, 1 page View Download
24 Photo 12 - Instrument Panel PDF, 1 page View Download
25 Photo 13 - Left Wing Fuel Tank Bladder, Removed from Wing PDF, 1 page View Download
26 Photo 14 - Engine Oil Dipstick PDF, 1 page View Download
27 Photo 15 - Engine Mounted in Test Cell PDF, 1 page View Download

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

Connections how this case links to the rest of the register

Aircraft
Place

The whole map of how records connect · these connections as data: /graph/accident/ERA14FA074.json.

The bigger picture in Aviation Analytics: accidents over time since 1982, by model, by phase of flight and conditions, by place and on the map.

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 does not name anyone involved, its policy at this time. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.