ERA23LA232

NTSB accident investigation · Piper PA28 · Selma, AL · May 12, 2023

Accident · No injuriesClass 3 · LimitedFinal report
Date
May 11, 2023, 19:15 local (May 12, 2023, 00:15 UTC)
Place
Selma, AL
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N1347TPiper PA28
Defining event
Enroute: Fuel starvation
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Investigation class
Class 3
NTSB office
Eastern Region Aviation
Parties
Piper Aircraft, FAA/FSDO, Lycoming Engines
FAA report
20230511004559A
Case key
174541

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 preflight inspection, during which the left wing fuel sump drain was moved to and left in the open and locked position, allowing for fuel to drain during the flight and resulting in a total loss of engine power due to fuel starvation. Contributing to the accident was the pilot’s failure to follow the emergency checklist by not switching fuel tanks following the loss of engine power.

Findings · 4

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.

Action: incorrect action performancePersonnel issues › Action/decision · PilotPiper PA-28-180: 10 casesAll aircraft: 1,386 casesProbable cause
Fluids: fuelAircraft › Fluids/misc hardware · Fluid managementPiper PA-28-180: 32 casesAll aircraft: 1,695 casesProbable cause
Use of equip/info: use of checklistPersonnel issues › Task performance · PilotPiper PA-28-180: 3 casesAll aircraft: 336 casesProbable cause
Inspection: preflight inspectionPersonnel issues › Task performance · PilotPiper PA-28-180: 2 casesAll aircraft: 551 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

The pilot reported that he performed a preflight inspection and observed 48 gallons of fuel in the fuel tanks before departing on the cross-country flight using fuel from the right wing fuel tank. About 30 minutes into the flight, he switched to the left wing fuel tank, and about 25 minutes later, the airplane engine lost power. He attempted to restore engine power; however, he did not move the fuel selector back to the right wing fuel tank and the engine did not regain power. The pilot attempted a forced landing to a field; however, the airplane impacted an area of pine trees before the field, resulting in substantial damage to the wings, fuselage, and empennage. Postaccident examination revealed that the fuel selector was positioned to the left tank, and the left wing fuel sump drain was in the open and locked position. The left wing fuel tank was mostly intact and void of fuel. Review of a photo of the airplane taken several minutes after the accident revealed fuel staining on the left flap aft of the fuel drain, consistent with fuel leakage during the flight. It is likely that when sampling the fuel from the left wing before the flight, the pilot inadvertently twisted the sump drain into the up and locked open position, allowing fuel to drain during the entire flight, resulting in fuel starvation. Had the pilot followed the emergency checklist procedures and switched to the right wing fuel tank he would have likely been able to restore power to the engine.

Factual narrative

On May 11, 2023, about 1915 central daylight time, a Piper PA-28-180, N1347T, was substantially damaged when it was involved in an accident near Selma, Alabama. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot reported that he performed a preflight inspection and observed 48 gallons of fuel in the fuel tanks before departing St. Clair County Airport (PLR), Pell City, Alabama. He departed PLR using the right wing fuel tank and about 30 minutes into the flight to Monroeville, Alabama, he switched to the left wing fuel tank. About 25 minutes later, the airplane engine “slow(ed) to what appeared to be an idle power setting.” He turned the fuel pump on, increased mixture to full rich, and turned on the carburetor heat; however, the engine did not regain power. The airplane continued to descend and the pilot attempted a forced landing to a field; however, the airplane impacted an area of pine trees before the field. The pilot stated that the engine may have “quit” at some point before the impact and he had not attempted to switch fuel tanks when attempting to restore engine power. Examination of the wreckage revealed that the main wreckage came to rest on its left side, resting on the outboard portion of the left wing, which had fractured at the wing root. The right wing was fractured at the wing root and resting on top of the left wing. The fuselage, empennage, and wings sustained substantial damage. A postaccident examination of the engine did not reveal evidence of any mechanical failures or malfunctions that would have precluded normal operation. Compression and suction were achieved on all cylinders. The throttle and mixture cables remained attached at the carburetor and moved in conjunction with movement of the controls in the cockpit. Borescope examination of the cylinders revealed no anomalies other than oil in the Nos. 2 and 4 cylinders. The spark plugs were visually examined and appeared normal. Both magnetos were tested and produced spark at all towers. A small amount of fuel was present in the carburetor float bowl. Examination of the airframe revealed that the fuel selector was positioned to the left tank. The left wing fuel sump drain was in the open and locked position and the left wing fuel tank was mostly intact and void of fuel. The right wing fuel tank, with its fuel sump drain in the closed position, was breached and void of fuel. Review of a fuel receipt revealed that 20.26 gallons of fuel were purchased on May 9, 2023, at PLR. Review of a photo provided by the owner of the airplane that was taken “minutes after” the accident revealed fuel staining on the left flap aft of the fuel drain. The first items in the emergency checklist for Engine Power Loss In-Flight in the manufacturer’s Owner’s Handbook are: 1. Fuel Selector – switch to another tank containing fuel 2. Electric Fuel Pump- ON 3. Mixture – Rich 4. Carburetor Heat – On

Aircraft

Registration
N1347T
Reported as
Piper PA28 (180)
Category
Airplane
Serial number
28-7205285
Built
1972
Airframe hours
3,000
Engine
Lycoming O-360-A4A, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
Annual · July 14, 2022 · 200 hours before
Departed
PLR · Pell City, AL
Destination
MVC · Monroeville, AL
Equipment
Electronic primary flight display, Electronic flight bag or handheld device, Stall warning system, ADS-B

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
66
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Without waivers/limitations
Last flight review
October 3, 2022
Seat
Left
Restraint
3-point
Flight hours
390 total · 360 in this make and model · 170 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Temperature
81 °F, dew point 72 °F
Altimeter
30.02 inHg
Observed at
SEM, 4 nm away
METAR
METAR KSEM 120015Z AUTO 00000KT 10SM SCT075 27/22 A3002 RMK AO2=

Docket · 9

The files NTSB released with the investigation on June 20, 2024, on NTSB’s docket system: statements, records, photos and specialists’ reports. 10.7 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.