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Aviation safety reports, made easier to study

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NTSB Report

March 19, 1997 · Piper PA-28-161 · N2572Y

Broomfield, CO

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
March 19, 1997
Injury Outcomes
1 injury (1 minor injury)
Location
Broomfield, CO
Aircraft
Piper PA-28-161
Tail Number
N2572Y
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
FTW97LA132

The solo student pilot reported that after practicing 'air work', that he returned to the traffic pattern for landing practice when on an upwind departure, at 50 to 75 feet, the engine lost power. Documentation of flight times in the accident airplane revealed that it had been flown 3.3 hours since it's previous refueling. Examination by an FAA inspector at the accident site, revealed the left tank contained no fuel and the right tank contained five to six gallons of fuel. The fuel selector was found in the left tank position.

NTSB Probable Cause

the student pilot's improper use of the fuel tank selector which led to fuel starvation and loss of engine power. Factors were the pilot's inadequate fuel management and the lack of suitable terrain for the forced landing.

Full Narrative

On March 19, 1997, at 1658 mountain standard time, a Piper PA-28-161 airplane, N2572Y, was substantially damaged during a forced landing following a loss of engine power near Broomfield, Colorado. The student pilot, the sole occupant in the airplane, received minor injuries. The airplane was registered to and operated by Denver Air Center, Inc., under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the solo instructional local flight which originated approximately one hour prior to the accident. No flight plan had been filed. In a written statement, the student pilot reported that he flew a one hour dual instructional flight to renew his 90 day solo sign off. He then flew a solo flight. The pilot reported that he first left the traffic pattern to practice air-work for an hour, and then he returned to the traffic pattern for more touch-and-go landings. After completing his first "touch-an-go" on runway 29L, on takeoff upwind, at approximately 50 to 75 feet AGL, the engine lost power. The pilot performed a forced landing to a rough and uneven field. The engine separated from the mounts, both main gear penetrated their respective wings, the wings were bent, and the fuselage was twisted. Examination of the fuel truck log, for truck pump number "AV Truck #2", revealed that 24.3 gallons of fuel had been delivered to N2572Y on the morning of March 19, 1997. Examination of the aircraft log, for airplane N2572Y for March 19, 1997, disclosed that the airplane had been flown two times prior to the commencement of the accident flight, for a total time of 2.3 hours since last refueled. Examination of the airplane's fuel system by an FAA inspector, revealed that the left tank contained no fuel, the right tank contained five to six gallons of fuel and the structural integrity of the right and left fuel tanks were not compromised. The fuel selector was found in the left tank position.

Flight

Event TypeAccident
Event Time16:58 MST
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-28-161
Tail NumberN2572Y
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-320 · Reciprocating · 160
Seats4

People & Injuries

Injury Summary1 injury (1 minor injury)
Fatal0
Serious0
Minor1
Uninjured0
Total1
Crew 1Age 23 · First Class

Conditions

ConditionsVMC
LightDaylight
Wind350° @ 4 kt
Visibility60 sm
CeilingNone
Temperature / Dew Point21 C
Altimeter30.00 inHg
Observation Time23:47
Weather SourceWFAC

Appendix: Source Data