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April 13, 2000 · Mccan Velox REV II Velox REV · N103MV

Mulberry, FL

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
April 13, 2000
Injury Outcomes
1 injury (1 minor injury)
Location
Mulberry, FL
Aircraft
Mccan Velox REV II Velox REV
Tail Number
N103MV
Injuries
Minor
Aircraft Damage
Destroyed
NTSB Number
MIA00LA131

The pilot was performing an aerobatic sequence in preparation for an airshow. After several maneuvers he experienced a loss of elevator control while inverted. He jettisoned the canopy and bailed out. Examination of the flight control system revealed a failure of the elevator pitch control rod. Further analysis of the pitch control rod revealed the rod had failed in bending overstress for undetermined reasons.

NTSB Probable Cause

The bending overstress separation of the elevator pitch control rod for undetermined reasons. This resulted in an in-flight loss of control, bail out, and subsequent in-flight collision with terrain.

Full Narrative

On April 13, 2000, at about 1230 eastern daylight time, a Velox Rev II, N103MV, registered to a private owner, operating as a 14 CFR Part 91 personal flight, experienced a flight control malfunction in flight while maneuvering in the vicinity of Mulberry, Florida. The pilot bailed out of the airplane. Visual meteorological conditions prevailed and no flight plan was filed. The commercial pilot reported minor injuries. The airplane was destroyed. The flight originated from Lakeland-Linder Regional Airport (LAL), Lakeland, Florida, about 10 minutes before the accident. The pilot stated he departed LAL and was practicing an aerobatic sequence in preparation for the airshow at Sun n' Fun. He completed several maneuvers and experienced a loss of elevator control while inverted and pointed slightly down. He jettisoned the canopy and bailed out of the airplane. He landed about 1,000 feet from the airplane which crashed adjacent to a public highway. Examination of the flight control system revealed the elevator pitch control rod was fractured. The elevator pitch control rod was forwarded to the NTSB Materials Laboratory for further analysis. Examination of the elevator pitch control rod revealed it was fractured through the end fitting and tube section. Optical examinations revealed the failures were consistent with bending overstress separations. No evidence of preexisting cracking, corrosion, or other damage was found. (For additional information see NTSB Materials Laboratory Factual Report No. 00-077, an attachment to this report.) The airplane was released to Mr. Daniel H. McCan, registered owner of N103MV on April 13, 2000. The fractured elevator pitch control rod was released to Mr. McCan on July 11, 2000.

Flight

Event TypeAccident
Event Time12:30 EDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftMccan Velox REV II Velox REV
Tail NumberN103MV
Aircraft CategoryAir
DamageDestroyed
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · IO540 · Reciprocating · 250
Seats2

People & Injuries

Injury Summary1 injury (1 minor injury)
Fatal0
Serious0
Minor1
Uninjured0
Total1
Crew 1Age 44 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind150° @ 6 kt
Visibility10 sm
CeilingBroken clouds 25000 ft
Temperature / Dew Point66 F
Altimeter30.00 inHg
Observation Time16:52
Weather SourceWFAC

Appendix: Source Data