MIA03LA006

NTSB accident investigation · Piper PA-28-140 · Las Palmas, PR · October 23, 2002

Accident · No injuriesLimited investigationFinal report
Date
October 23, 2002, 16:00 local (20:00 UTC)
Place
Las Palmas, PR
Injuries
3 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N2838TPiper PA-28-140
Weather
Visual (VMC) · Day
Status
Completed · report April 1, 2003
Report
Approved by Office Director
Parties
FAA FSDO
FAA report
20021023032229A
Case key
55931

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 failure to switch fuel tanks resulting in a partial loss of engine power due to fuel starvation during a go-around. Additionally, the pilot's failure to monitor airspeed and proper touchdown point during the emergency landing resulted in another go-around attempt with partial power and inadequate airspeed that caused a collision with a field off the end of the runway.

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 power(partial) - nonmechanicalGo-around (vfr)
Checklist - not complied withPilot in commandCause
Fuel tank selector position - improperPilot in commandCause
Fluid,fuel - starvation
Forced landingDescent - emergency
In flight collision with terrain/waterEmergency descent/landing
Airspeed - excessivePilot in commandCause
Proper touchdown point - not attainedPilot in commandCause
Go-around - attemptedPilot in command
Terrain condition - open field

Analysis

Following a 30 minute flight from Humacao, Puerto Rico, the pilot's first attempt to land on runway 10 at Patillas Airport, Las Palmas, resulted in a go-around because the approach path was too high. During the go-around, at between 400 and 500 feet agl, the engine lost partial power, and the pilot elected to execute a quick course reversal and land on runway 28. The emergency approach and landing were fast and long, necessitating another go-around with whatever power was available. The pilot managed to over-fly the airport perimeter fence, but collided with the terrain on the other side of the fence, sustaining substantial damage to the aircraft. Postcrash examination of the aircraft revealed the fuel selector was selected to the right fuel tank, which was found empty. The pilot stated he had not switched tanks since takeoff.

Factual narrative

On October 23, 2002, about 1600 Atlantic standard time, a Piper PA-28-140, N2838T, registered to East Wing Aviation, Inc., operating as a Title 14 CFR Part 91 personal flight, crashed in the vicinity of Las Palmas, Puerto Rico. Visual meteorological conditions prevailed and no flight plan was filed. The airplane was substantially damaged, and the private rated pilot and two passengers were not injured. The flight originated from Humacao, Puerto Rico, about 30 minutes before the accident.

According to the pilot, he realized that he was too high for a safe landing to Patillas Airport's runway 10, and elected to conduct a go-around. During the go-around, at 400 to 500 feet agl, the engine lost partial power, and his best option was to perform a 180- degree course reversal and attempt an emergency landing on runway 28. His touchdown occurred about runway mid-length with excessive approach speed. He attempted a partial power go-around, cleared the airport perimeter fence, and collided with the terrain on the other side of the fence due to insufficient airspeed. The surface of the terrain was rough dirt and grass, and the landing gear collapsed.

According to an FAA inspector, following examination of the wreckage and interviewing the pilot, during the pilot's go-around from runway 10, a partial engine power loss necessitated his attempting to make an emergency approach and landing to runway 28. That approach resulted in a long, fast touchdown due to a tailwind, and the pilot again attempted a go-around. During the second go-around, using partial engine power, the pilot had to effect an abrupt pull-up to miss a fence at the departure end of runway 28. The fence was cleared, but the aircraft crashed in a field on the other side of the fence, collapsing the three landing gear and striking the propeller. The right fuel tank was found empty, and the pilot admitted he did not switch tanks from right to left tank since his departure from Humacao. The left fuel tank contained about 18 gallons of 100 octane LL fuel, which was the quantity observed before departure. The underside of the wings and fuselage revealed no evidence of fuel leakage.

Aircraft

Registration
N2838T
Reported as
Piper PA-28-140
Category
Airplane
Serial number
28-7225247
Airframe hours
2,797
Engine
Lycoming O-320-D3G, 160 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
East Wing Aviation, Inc.
Airworthiness certificate
Standard, Utility; Standard, Normal
Last inspection
Annual · October 4, 2002 · 2.5 hours before
Departed
X63 · Humacao, PR
Destination
X64 · Las Palmas, PR
Airport
X64 · Patillas, runway 28, 2,000 × 50 ft, asphalt

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
50
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Last flight review
February 24, 2001
Seat
Left
Flight hours
341 total · 179 in this make and model · 260 as pilot in command · 1 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
100° at 7 knots
Visibility
7 statute miles
Lowest ceiling
25,000 ft broken
Temperature
84 °F, dew point 77 °F
Altimeter
29.94 inHg
Observed at
TJNR, 27 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 N2838T · 1

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