N2947E

Substantial
None

PIPER PA-32-300 S/N: 32-7940222

Accident Details

Date
Friday, May 14, 1993
NTSB Number
CHI93LA172
Location
WEST CHICAGO, IL
Event ID
20001211X12354
Coordinates
41.879360, -88.220329
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

THE PILOT-IN-COMMAND'S INADEQUATE COMPENSATION FOR THE WIND CONDITIONS HE ENCOUNTERED DURING THE LANDING APPROACH AND TOUCHDOWN AND NOT MAINTAINING A PROPER DESCENT RATE

Aircraft Information

Registration
Make
PIPER
Serial Number
32-7940222
Engine Type
Reciprocating
Year Built
1979
Model / ICAO
PA-32-300 PA32
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
PA-32-300

Registered Owner (Current)

Name
SLIPSTREAM INC
Address
215 49TH ST S
City
SAINT PETERSBURG
State / Zip Code
FL 33707-1925
Country
United States

Analysis

On May 14, 1993, at 1439 central daylight time (CDT), a Piper PA-32-300, N2947E, registered to BCS Aero Sales of Polk City, Iowa, and piloted by a private pilot was substantially damaged during a hard landing on Runway 19L (3,300' X 75' dry concrete) at the DuPage County Airport, West Chicago, Illinois. Visual meteorological conditions prevailed at the time of the accident. The 14 CFR Part 91 flight was operating on a VFR flight plan. The pilot and passengers reported no injuries. The flight departed Cedar Rapids, Iowa, at 1329 CDT.

The pilot stated that the control tower told him to use Runway 19L when he was approximately 150 feet above the ground while aligned with Runway 19R. He said the control tower announced the wind had shifted to 280 degrees at 19 knots. As the pilot realigned the airplane for Runway 19L he stated the control tower announced the wind was at 260 degrees at 18 knots. The pilot stated the airplane's rate of descent was higher than it should have been due to his crosswind landing technique. He stated, "I should have had more power in, my descent was higher than normal. I was distracted by ATC, they kept announcing the winds." He stated the airplane landed hard and that he thought the main landing gear tires had struck the runway lip.

An on-scene investigation revealed the following damage: main landing gear mounting bolts had sheared and the spar bolt holes were elongated, top and bottom spar caps in the vicinity of the main landing gear mounts were twisted, bottom wing skins aft of the main landing gear mounts were punctured inward, the top wing skins above the lower puncture areas were punctured outward, both landing flaps were crushed in an area in line with the main landing gear mounts, both main landing gear wheels were deformed and the tires blown, brake disc on both wheels were bent outward, rivets separated from the stabilator main spar at its pivot point, the left side of the fuselage aft of the cabin's rear bulkhead had compression wrinkled skin, and the tail skid/tie down ring had pushed upward into the fuselage bulkhead and associated skin.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI93LA172