N94PB

Substantial
None

Beech 58PS/N: TJ-245

Accident Details

Date
Monday, June 24, 2002
NTSB Number
DEN02LA057
Location
Broomfield, CO
Event ID
20020701X01018
Coordinates
39.908611, -105.116943
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

the pilot's failure to follow procedures for a balked landing which resulted in a stall/mush.

Aircraft Information

Registration
Make
BEECH
Serial Number
TJ-245
Engine Type
Reciprocating
Year Built
1979
Model / ICAO
58PB58T
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2
Seats
6
FAA Model
58P

Registered Owner (Current)

Name
REGISTRATION PENDING
Address
1301 INDUSTRIAL PARK DR
City
TUSCALOOSA
State / Zip Code
AL 35401-0405
Country
United States

Analysis

On June 24, 2002, at 1657 mountain daylight time, a Beech 58P, N94PB, was destroyed during a go-around attempt at Jeffco Airport, Broomfield, Colorado. The instrument rated private pilot and his passenger were not injured. The pilot/owner was operating the airplane under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the cross-country flight that originated from the John Wayne - Orange County Airport, Santa Ana, California, approximately 3 hours 20 minutes before the accident. An IFR flight plan had been filed and activated.

The pilot said that he was attempting to land on runway 11L when a right crosswind gust struck the aircraft. He decided to go around. He applied full power and raised the landing gear; the flaps remained at 30 degrees (full down). The pilot said that the airplane settled to the ground and subsequently exited the left side of the runway. Both wings and the fuselage were wrinkled, and the right engine mount was broken.

The airplane's Pilot Owner's Handbook (POH) for a balked landing states:

1. Propellers -- High RPM

2. Throttles -- Full open

3. Airspeed -- Balked landing climb speed (92 knots)

4. Flaps -- Up (0 degrees)

5. Landing Gear -- Up

The POH also states that the maximum demonstrated crosswind for landing was 30 knots. The maximum calculated crosswind, at the time of the accident, was 20 knots.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN02LA057