Aviation Crash Map

Hawker Siddeley FB-60 N222CH

16 April 1996 · Lakeland, Florida, United States · Fatal

Summary

On 16 April 1996 at about 18:56 local time, a Hawker Siddeley FB-60 registered N222CH was involved in an accident near Lakeland, Florida, United States. One person was on board and one died. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 18:56
Classification
Accident
Location
Lakeland, Florida, United States
Nearest airport
Lakeland Linder Regional (LAL)
Coordinates
28.5696, -81.3205
Aircraft
Hawker Siddeley FB-60
Registration
N222CH
Category
Airplane
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Unknown
Phase of flight
Not recorded
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
MIA96FA118

People

1 person died.

On board Died Serious Minor Uninjured
1 1 0 0 0

Probable cause

The pilot's improper use of brakes and ailerons, during the landing rollout with a right crosswind, which resulted in a loss of directional control and subsequent nose over. Factors relating to the accident were: the crosswind and the pilot's lack of experience in the Hawker FB-60 airplane.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

Witnesses observed that the tailwheel equipped airplane landed on the runway with a right crosswind. It touched down on the main gear and decelerated to a three-point attitude. The airplane was observed to veer to the right, and the tail section became 'airborne' (raised off the surface). The airplane then went off the right side of the runway, nosed over and came to rest inverted. Examination of the runway revealed intermittent left main landing gear braking, starting abeam the 5,000' runway marker, and subsequent continuous left and right braking until the airplane went off the runway. Review of a video tape (shown on a television station) revealed the left aileron and both elevator surfaces were up during the landing rollout and during the accident sequence. During a functional test of the brake system, the hydraulic system pressurized normally. There was no visible brake caliper leakage and no abnormal wear on the brake disk or linings.

Quoted verbatim from the NTSB record.

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