ERA10CA417

NTSB accident investigation · Piper PA-25-260 · St. Petersburg, FL · August 12, 2010

Accident · No injuriesData collectionFinal report
Date
August 12, 2010, 18:43 local (22:43 UTC)
Place
St. Petersburg, FL
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N254ABPiper PA-25-260
Defining event
Enroute-cruise: Loss of engine power (total)
Weather
Visual (VMC) · Day
Status
Completed · report May 11, 2011
Report
Approved by Office Director
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO
FAA report
20100812042939A
Case key
76947

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

On this page

Probable cause

The pilot’s improper fuel management, which resulted in a loss of engine power due to fuel exhaustion.

Findings · 2

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Fluids: fuelAircraft › Fluids/misc hardware · Fluid levelAll aircraft: 1,695 casesProbable cause
Planning/preparation: fuel planningPersonnel issues › Task performance · PilotAll aircraft: 719 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

According to the pilot, he departed with the airplane's fuel tank full (75 gallons) for the local banner towing flight. He flew for about 3 hours and 30 minutes and then initiated a return to the airport. During the return flight, at an altitude of approximately 1,000 feet, the airplane's engine lost power. Just prior to the power loss, while the airplane was in a climb, the pilot noted that the fuel gauge indicated 30 gallons of fuel remained. The pilot released the banner and performed a forced landing on a road. A postaccident examination of the airplane by a Federal Aviation Administration inspector revealed approximately 8-10 ounces of fuel remained in the single main fuel tank. The main fuel feed line at the bottom of the fuel tank fuel valve contained a few ounces of fuel. The fuel tank was filled with 30 gallons of fuel to test the accuracy of the fuel gauge, which read 33 gallons of fuel. The engine was test run on the airframe. It started and ran at full power with no anomalies noted. According to the airplane's Operating Handbook, the engine burns an average of 14-16 gallons of fuel per hour, at power settings likely used by the pilot. The fueler who fueled the airplane stated that he filled the airplane to a capacity of 68 gallons of fuel, which is what the pilot specifically requested. The examination revealed no evidence of a mechanical malfunction.

Factual narrative

According to the pilot, he departed with full fuel (75 gallons) in the airplane, for the local banner towing flight. He flew for about 3 hours and 30 minutes, and then initiated a return to the airport. During the return flight, at an altitude of approximately 1,000 feet, the airplane's engine lost power. Just prior to the power loss, while the airplane was in a climb, the pilot noted that the fuel gauge indicated 30 gallons of fuel remained. The pilot released the banner and performed a forced landing to a road. Examination of the airplane by a Federal Aviation (FAA) inspector revealed approximately 8-10 ounces of fuel in the single main fuel tank. The main fuel feed line at the bottom of the fuel tank fuel valve contained a "few ounces" of fuel. The fuel tank was filled with 30 gallons of fuel to test the accuracy of the fuel gauge, which read 33 gallons of fuel. The engine was test run on the airframe. It started and ran at full power with no anomalies noted. According to the Piper PA-25 Pilot Operating Handbook, the airplane's engine burned an average of 14-16 gallons of fuel per hour, at a power setting of 24 inches of manifold pressure and 2400 RPM. The fueler who fueled the airplane stated he filled the airplane to a capacity of 68 gallons of fuel, which is what the pilot specifically requested.

Aircraft

Registration
N254AB
Reported as
Piper PA-25-260
Category
Airplane
Serial number
25-7556048
Airframe hours
5,472
Engine
Lycoming O-540-G1A5, 260 horsepower, reciprocating
Damage
Substantial damage
Flight
Banner tow · Part 91
Operator
Aerial Banners Inc
Registered owner
Aerial Banners Inc
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · July 20, 2010
Departed
SPG · St. Petersburg, FL
Destination
SPG · St. Petersburg, FL

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
25
Injuries
None
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Without waivers/limitations
Last flight review
September 17, 2009
Seat
Single
Flight hours
488 total · 35 in this make and model · 322 as pilot in command · 35 in the last 90 days · 35 in the last 30 days · 0 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
250° at 10 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
88 °F, dew point 77 °F
Altimeter
29.88 inHg
Observed at
SPG, 5 nm away

Docket · 7

The files NTSB released with the investigation on February 16, 2011, on NTSB’s docket system: statements, records, photos and specialists’ reports. 7.4 MB in all.

FAA reports on this event · 1

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