The U.S. aircraft register, updated daily
Accidents · NTSB ERA12LA234 · Final report

Cessna 172K accident near Pensacola, Florida, March 16, 2012

On March 16, 2012 at about 3:15 pm local time, a Cessna 172K, registered N79509, was substantially damaged in an accident during enroute (cruise) near Pensacola, Florida. It was an instructional flight under general aviation rules (Part 91). No one was hurt; 2 people were on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

A total loss of engine power due to the improper installation of the crankshaft gear bolt or lockplate by maintenance personnel. Contributing to the accident was the lack of suitable terrain for a forced landing.

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

What the record shows

Date
March 16, 2012 · about 3:15 pm local time
Place
Pensacola, Florida · map
Type
Accident
Injuries
No one was hurt; 2 people were on board or involved.
Weather
visual conditions (good weather)
Aircraft
Cessna 172K · all 172Ks on the register
Registration
N79509 · no longer on the register · serial 17258140
Damage
Substantial damage
Flight
Instructional flight · general aviation rules (Part 91)

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

During the training flight, the single-engine airplane was in cruise flight about 1,000 feet above ground level when the engine stopped operating. The flight instructor assumed control of the airplane and unsuccessfully attempted to restart the engine while descending for an emergency landing. He ditched the airplane into a nearby bay. The airplane sustained substantial damage to the windshield during the accident sequence and was submerged in salt water. Postaccident examination of the engine revealed that the bolt or lockplate, which attaches the crankshaft gear to the aft end of the crankshaft, was missing. Further, the alignment dowel was fractured across about one-third of the cross-sectional area. The bolt and lockplate were likely either not installed or were improperly installed, which would allow the bolt to loosen and become disengaged. Measurements of the dowel, pilot flange, and counterbore recess diameters were all within the manufacturer's specifications; the dowel also met the manufacturer's hardness requirement. Because the components were within manufacturer's specifications, it is likely that the components did not have any preexisting wear or manufacturing issues. Additionally, wear marks on the crankshaft, dowel, and gear were likely caused by the newly installed gear and were consistent with either no installation or improper installation of the bolt or lockplate. Therefore, it is likely that when the wear on the dowel had proceeded through about one-third of the cross-section, the stresses in the dowel became sufficiently high to initiate fatigue cracks at the base of the worn part of the dowel and eventually led to a fatigue fracture. The evidence is consistent with the failure of maintenance personnel to install, or properly install, the bolt and lockplate during the engine’s last overhaul, which resulted in the crankshaft gear becoming separated from the crankshaft and a total loss of engine power. If the engine had failed at a point that would have allowed the pilot to land the airplane on land, the airplane damage is less likely to have been substantial; therefore, contributing to the accident was the lack of suitable terrain.

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. Loss of engine power (total) during enroute (cruise) defining event
  3. Off-field or emergency landing during emergency descent
  4. Ditching during landing (flare/touchdown)

The NTSB's findings

  • cause Aircraft › Aircraft power plant › Engine (reciprocating) › Recip eng rear section › Incorrect service/maintenance
  • cause Aircraft › Aircraft power plant › Engine (reciprocating) › Recip eng rear section › Failure
  • factor Environmental issues › Physical environment › Terrain › Water › Contributed to outcome
  • cause Personnel issues › Task performance › Maintenance › Installation › Maintenance personnel

Flight instructor

  • Certificate: flight instructor, commercial pilot
  • Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
  • Flight time: 4,000 hours in all; 2,000 in this make and model; 100 in the last 90 days; 50 in the last 30 days; 4,000 as pilot in command; 2,000 on instruments
  • Medical certificate: Class 1 (with waivers/limitations)
  • Seat: rgt
  • Injury: no injuries

Dual student

  • Flight time: 3 hours in all; 3 in this make and model; 3 in the last 30 days
  • Medical certificate: Class 3 (without waivers/limitations)
  • Seat: left
  • Injury: no injuries

The aircraft

  • Airframe total time: 5,020 hours
  • Last inspection: annual inspection, October 1, 2011
  • Maximum gross weight: 2,450 lb
  • Seats: 4
  • Landing gear: fixed
  • Engine: Lycoming O-320 E2D (piston); 0 hours total
  • Operator: Skywarrior INC

The flight

  • Departed from: PNS Pensacola FL at 2:15 pm
  • Destination: PNS Pensacola FL
  • Flight plan: none
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 73°F (23°C), dew point 63°F (17°C)
  • Altimeter: 30.26 inHg
  • Observation at 2:53 pm from PNS, 3 miles away

Injuries

FatalSeriousMinorNone
Flight crew2

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

The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.

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.