MIA94LA084

NTSB accident investigation · Piper PA-28-161 · Sanford, FL · March 5, 1994

Accident · Minor injuriesLimited investigationFinal report
Date
March 5, 1994, 14:57 local (19:57 UTC)
Place
Sanford, FL
Injuries
2 minor
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N9134APiper PA-28-161
Weather
Visual (VMC) · Day
Status
Completed · report December 7, 1994
Report
Approved by Office Director
FAA report
19940305003819A
Case key
37503

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 failure of the pilot to maintain airspeed during the forced landing resulting in an inadvertent stall/mush. The total loss of engine power caused by fuel starvation due to inattentiveness by the pilot-in-command (CFI) to the fuel supply was also a cause.

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(total) - nonmechanicalTakeoff - initial climb
Fluid,fuel - starvationCause
Fuel tank selector position - improperPilot in command(cfi)Cause
Forced landingDescent - emergency
Loss of control - in flightManeuvering - turn to landing area (emergency)
Airspeed - not maintainedPilot in command(cfi)Cause
Stall/mush - inadvertentPilot in command(cfi)
Altitude - inadequate
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - ground

Analysis

During the upwind leg after the fourth or fifth touch-and-go landing, the engine experienced a total loss of engine power due to fuel starvation. The CFI took the controls and landed the airplane on the runway but there was insufficient runway remaining to stop. During the landing roll the engine power was restored and the CFI elected to take off to return for landing. During the upwind leg, the engine again experienced a total loss of engine power due to fuel starvation. During the left turn to return to the airport, the airplane stalled and impacted the ground nose and left wing low. The fuel selector was positioned to the left tank for the duration of the flight and the left fuel tank was empty. The right fuel tank contained 15.4 gallons of fuel.

Factual narrative

On March 5, 1994, about 1457 eastern standard time, a Piper PA-28-161, N9134A, registered to Air Orlando Sales, Inc. crashed shortly after takeoff while practicing touch-and-go landings at the Sanford Regional Airport, Sanford, Florida, while on a 14 CFR Part 91 instructional flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The airplane was substantially damaged and the certified flight instructor (CFI) and student pilot received minor injuries. The flight originated about 1 hour 24 minutes earlier from Orlando Executive Airport, Orlando, Florida.

The flight departed about 1333 and performed maneuvers then flew to the Sanford Regional Airport where the student was to perform touch-and-go landings. After the fourth or fifth touch- and-go landing during the upwind leg with the student flying the airplane, the engine experienced a loss of power. The CFI took control of the airplane and landed on the runway but stated that he was unable to stop on the runway. The engine power was restored after he cycled the auxiliary fuel pump. He elected to take off but the engine lost power again. During the turn to return for landing, the airplane stalled and impacted the ground nose and left wing low. The student pilot stated that the fuel selector was not moved at any time during the flight.

An FAA inspector arrived at the accident site about 3.5 hours after the accident and examined the airplane. The inspector stated that the left wing was damaged and the fuel line was broken near the wing root area but there was no fuel leakage. The fuel selector was in the "off" position but before being moved it was in the "left" position. He also examined the left wing fuel tank and there was no evidence of fuel inside the tank. The right wing fuel tank was drained and found to contain about 15.4 gallons of fuel. Power was applied directly to the auxiliary fuel pump terminals and the pump was found to operate. The engine-driven fuel pump was removed from the airplane for bench testing and found to operate normally.

According to the owner of the airplane, the airplane had been operated according to the Hobbs meter for 5.1 hours since the fuel tanks were filled.

Aircraft

Registration
N9134A
Reported as
Piper PA-28-161
Category
Airplane
Serial number
28-8616009
Airframe hours
4,060
Engine
Lycoming O-320-D3G, 160 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Registered owner
Air Orlando Sales, Inc.
Airworthiness certificate
Standard, Utility; Standard, Normal
Last inspection
100 hour · December 22, 1993 · 73 hours before
Airport
SFB · Central Florida Regional, runway 27R, 8,001 × 150 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
33
Certificates
Commercial, Flight instructor
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
436 total · 13 in this make and model · 378 as pilot in command · 172 in the last 90 days · 70 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
270° at 10 knots, gusting 15
Visibility
10 statute miles
Lowest ceiling
None
Temperature
77 °F, dew point 46 °F
Altimeter
29.00 inHg
Observed at
SFB, 1 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.