N3240R

Substantial
None

Beech 58 S/N: TH1740

Accident Details

Date
Friday, July 2, 1999
NTSB Number
CHI99LA206
Location
WHEELING, IL
Event ID
20001212X19174
Coordinates
42.130428, -87.920532
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

the landing gear extension not performed by the pilot. A contributing factor was the checklist not followed by the pilot.

Aircraft Information

Registration
N3240R
Make
BEECH
Serial Number
TH1740
Engine Type
Reciprocating
Model / ICAO
58 BE58
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Status
Deregistered
Country
United States

Analysis

On July 2, 1999, at 1103 central daylight time, a Beech 58, N3240R, piloted by a private pilot, sustained substantial damage during a wheels-up landing on runway 16 (5,001 feet by 100 feet, dry asphalt) at Palwaukee Municipal Airport (PWK), Wheeling, Illinois. Visual meteorological conditions prevailed at the time of the accident. The flight was operating under the provisions of 14 CFR Part 91 and was not on a flight plan. The pilot reported no injuries. The flight departed Three Lakes Municipal Airport, Three Lakes, Wisconsin, at approximately 0945, en route to PWK.

In a written statement, the pilot reported, "...Palwaukee gave me a straight in approach for runway 16 and to notify the tower 2 miles out. I flew to the left to line up with 16 and began a slow decent to traffic pattern altitude. About 3-1/2 miles out the tower cleared me to land. I began my pre landing checklist however I became distracted by what I thought was the collision avoidance equipment but in reality was my gear warning horn. There were a couple of aircraft showing up about a mile and a half away and I was looking for them and never completed the checklist and my normal prelanding GUMPS check. The aircraft landed gear up in the center of the runway and slid for a short distance. It stopped half off the left side of runway 16 however no lights were hit."

Federal Aviation Administration Advisory Circular 20-34D, Prevention of Retractable Landing Gear Failures, section 4. Operational factors and percentages involved in retractable gear aircraft accidents" as:

a. Neglected to extend landing gear - 35.8 percent. b. Inadvertent retraction of landing gear - 10.3 percent. c. Activated gear, but failed to check gear position - 11.3 percent. d. Misused emergency gear system - 0.9 percent. e. Retracted gear prematurely on takeoff - 2.8 percent. f. Extend gear too late - 1.8 percent.

Section 5(a)(1) states, "On the downwind leg, or at the final approach fix inbound, make it a habit to complete the recommended landing gear checklist for your aircraft...". Section 5(b)(3) states, Be familiar with the landing gear warning horn and warning light systems of your aircraft. Use the horn system to cross-check the warning light system when an unsafe condition is noted.".

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI99LA206