DFW06LA007

NTSB accident investigation · Cessna 140 · Big Flat, AR · October 16, 2005

Accident · Serious injuriesLimited investigationFinal report
Date
October 16, 2005, 16:15 local (21:15 UTC)
Place
Big Flat, AR
Injuries
2 serious
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N72901Cessna 140
Weather
Visual (VMC) · Day
Status
Completed · report April 25, 2006
Report
Approved by Office Director
Parties
FAA FSDO, Cessna Aircraft Company
FAA report
20051016026409A
Case key
62673

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The NTSB’s determination of the probable cause, and any contributing factors.

The loss of engine power for undetermined reasons. A contributing factor was the lack of suitable terrain for a forced landing.

Analysis

The 345-hour private pilot completed a detailed preflight inspection and determined he had 26 gallons of fuel on-board for a cross-country flight. He then departed his home airfield, to pick up a passenger at another airfield approximately 17 nautical miles away The pilot then departed for another airfield located about 76 nautical miles away; no problems were noted during these flights. However, ten minutes after departing his last airfield, the engine experienced a loss of RPM. The pilot ran the emergency checklist and searched for a place to land as the airplane was unable to maintain altitude. The airplane had experienced several loss of engine power events before, but each time the pilot was able to make a safe landing. The first time was shortly after being sold to a new buyer; an inspection of the airplane's fuel tanks, revealed contamination in the form of "beads" in the fuel tank. Shortly after having the tanks flushed, the second loss of power event happened, (after each event, and after the airplane had landed the engine would produce power again). The carburetor was examined and the airplane returned to service. Approximately 15-30 hours later, another loss of power event happened. This time the carburetor was sent to a repair facility, which rebuilt the carburetor and told the owner that a "wrong jet" had been installed in the carburetor. The airplane then flew another 50-60 hours without a re-occurrence. The airplane's original fuel caps were replaced, sometime prior to the accident. The fuel caps installed on the airplane were an aftermarket design, with the label "2646V" inked on the top of the caps. The vent holes in these caps were less than half the size of the original fuel caps. Additionally, it was possible for the gasket (in the fuel cap) to cover one or both of the vent holes. A review of the airplane's records failed to reveal when the original fuel caps were replaced. The reason for the reported loss of engine power could not be determined.

Factual narrative

The factual narrative645 words

On October 16, 2005, approximately 1615 central daylight time, a single-engine Cessna 140 tail wheel-equipped airplane, N72901, was substantially damaged during a forced landing following a loss of engine power while maneuvering near Big Flat, Arkansas. The private pilot and passenger were seriously injured. The airplane was registered to and operated by a private individual, under the provisions of 14 Code of Federal Regulations Part 91, as a personal flight. Visual meteorological conditions prevailed and a flight plan was not filed for the local flight. The airplane departed the Gastons Airport (3M0) near Lakeview, Arkansas, at approximately 1600 en route to the Dennis F Cantrell Field Airport (CWS) near Conway, Arkansas.

The 345-hour private pilot reported in the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) that he completed his preflight inspection and determined that he 26 gallons of fuel on-board for the flight. He then departed for CWS, approximately 17 nautical miles away, to pick up a passenger. The pilot then departed CWS for 3M0, about 76 nautical miles away; no problems were experienced during these flights. However, ten minutes after departing 3M0, the pilot reported having "engine trouble and a loss of RPM". The pilot reported that "he ran the emergency checklist and searched for a place to land," but was unable to maintain altitude.

A Federal Aviation Administration (FAA) inspector examined the airplane at the accident site, and noted that the airplane impacted the ground on its right side after coming through trees in a heavily wooded area.

In a telephone conversation with the NTSB Investigator-in-charge, the owner stated that he owned the airplane for approximately two years. Additionally, he stated they only ran aviation fuel in the airplane (the airplane had decals near the fuel caps, allowing the use of automotive fuel). The owner added, that the airplane had experienced several loss-of-engine power events before, but each time the pilot was able to make a safe landing. The first time was shortly after buying the airplane; an inspection of the airplane's fuel tanks, revealed contamination in the form of "beads" in the tank. Shortly after having the tanks flushed, the second loss-of-power event happen (after each event, and after the airplane had landed the engine would produce power again). The carburetor "was looked at," and the airplane returned to service. Approximately 15-30 hours later, another loss-of-power event happened. This time the carburetor was sent-out for overhaul. The repair facility rebuilt the carburetor and told the owner that the "wrong jet" had been installed in the carburetor. The owner stated that since the rebuilt carburetor had been installed, the airplane had flown about 50-60 hours without any problem, and figured the problem had been finally resolved.

This Cessna 140 has two fuel tanks (one in each wing). The wing fuel tanks are vented by "vent holes" in the fuel caps. The accident airplane's original fuel caps were replaced sometime prior to the accident. The fuel caps installed on the airplane were an aftermarket design, with the label "2646V" inked on the top of the caps. The vent holes on these caps, were found to be less than half the size of the original fuel caps vent holes. Additionally, it was possible for the gasket (in the fuel cap) to cover one or both of the vent holes. The owner stated that he had not replaced the fuel caps, and they were on the airplane when he bought the aircraft. A review of the airplane's records failed to reveal when the original fuel caps were replaced. The reason for the power loss could not be determined.

At 1555, the automated weather observing system at Marion County Regional Airport (FLP), approximately 15 miles southwest of the accident site, reported calm wind, 10 statute miles visibility, a clear sky, temperature 77 Fahrenheit, dew point 48 degrees Fahrenheit, and an altimeter setting of 30.10 inches of Mercury.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine powerCruise
Reason for occurrence undeterminedCause
Forced landingDescent - emergency
In flight collision with objectEmergency descent/landing
Object - tree(s)Factor
Terrain condition - none suitableFactor

Aircraft

Registration
N72901
Reported as
Cessna 140
Category
Airplane
Serial number
10095
Engine
Continental C85, 85 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
Annual · October 1, 2004
Departed
3M0 · Lakeview, AR
Destination
CWS · Conway, AR

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
21
Injuries
Serious
Certificate
Private
Airplane ratings
Single-engine land, Single-engine sea
Medical
Class 3, Without waivers/limitations
Last flight review
April 1, 2005
Seat
Left
Flight hours
345 total · 224 in this make and model · 322 as pilot in command · 13 in the last 90 days · 6 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
0° at 0 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
77 °F, dew point 48 °F
Altimeter
30.10 inHg
Observed at
FLP, 15 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.

Other investigations on N72901 · 1

Matched to the same aircraft by N-number and date.