N6391R

Substantial
Minor

Piper PA-28-140 S/N: 28-21568

Accident Details

Date
Sunday, September 7, 1997
NTSB Number
CHI97LA289
Location
GRANT, MI
Event ID
20001208X08812
Coordinates
45.849819, -87.020393
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
3
Uninjured
0
Total Aboard
3

Probable Cause and Findings

the pilot's fixation on the end of the runway, his failure to place the airplane in an attitude to land (flare) which resulted in a hard landing, and the pilot's failure to recover from the subsequent bounced landing.

Aircraft Information

Registration
Make
PIPER
Serial Number
28-21568
Engine Type
Reciprocating
Year Built
1966
Model / ICAO
PA-28-140 P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-28-140

Registered Owner (Current)

Name
BARCELO JAVIER DAVID
Address
102 COLONY WAY
City
ROYSE CITY
State / Zip Code
TX 75189-7065
Country
United States

Analysis

On September 7, 1997, at 1800 eastern daylight time (edt), a Piper PA-28-140, N6391R, operated by a private pilot, sustained substantial damage when on landing the airplane impacted on a sod runway. Visual meteorological conditions prevailed at the time of the accident. The personal flight was being conducted under 14 CFR Part 91. There was no flight plan on file. The pilot and two passengers on board reported minor injuries. The local flight originated at Grant, Michigan, at 1730 edt.

In his written statement, the pilot said that he lined up on the runway for landing at Grant Airport, Michigan. "I was focusing on landing on the end of the runway and was going to touch down near the approach end. I failed to flare at a high enough altitude and struck the ground very hard and bounced back into the air. The plane bounced twice more before stalling and landing on the nose gear. The nose gear broke and the airplane came to rest about half way down the runway."

The Federal Aviation Administration (FAA) inspector who examined the wreckage found damage to the airplane's forward fuselage and cowling. The engine was pushed upward. The cowling was buckled upward and aft. The nose wheel was broken off of the airplane. The underside of the forward fuselage was crushed inward and aft.

The propeller showed torsional bending and chordwise scratches. Flight control continuity was confirmed. No anomalies were found with the engine, controls or other airplane systems.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI97LA289