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May 8, 1983 · Rotec Rally 2B · UNREG

Manvel, TX

Overview

Report Status
Preliminary report
Event Type
Accident
Date
May 8, 1983
Injury Outcomes
1 injury (1 fatality)
Location
Manvel, TX
Aircraft
Rotec Rally 2B
Tail Number
UNREG
Injuries
Fatal
Aircraft Damage
Destroyed
NTSB Number
FTW83FU001

The pilot had flown the ultralight vehicle to his employer's house and landed in the back yard. During the landing, the vehicle sustained damage which included a bent main landing gear axle, a sheared kingpin bolt, and a cracked tail boom to tailmount sleeve. A hardened bolt was purchased at an automotive parts store and partial repairs were made; however, the damage to the tail boom was not detected. The ultralight was preflighted and the pilot took off. After circling once and waving, he started on the return flight. Shortly after that, witnesses heard the engine slow or stop as the ultralight pitched nose down into a steep dive and crashed. An exam of the wreckage revealed that the right tail boom tube had separated in flight. During impact, it had penetrated the horizontal stabilizer sail without bending. The left tail boom was bent during impact. A picture of the ultralight (taken before takeoff) revealed that the horizontal stabilizer was slightly angled from the horizontal axis of the ultralight.

Full Narrative

THE PLT HAD FLOWN THE ULTRALIGHT VEHICLE TO HIS EMPLOYER'S HOUSE & LANDED IN THE BACK YARD. DURING THE LANDING, THE VEHICLE SUSTAINED DAMAGE WHICH INCLUDED A BENT MAIN LANDING GEAR AXLE, A SHEARED KINGPIN BOLT & A CRACKED TAIL BOOM TO TAILMOUNT SLEEVE. A HARDENED BOLT WAS PURCHASED AT AN AUTOMOTIVE PARTS STORE & PARTIAL REPAIRS WERE MADE; HOWEVER, THE DAMAGE TO THE TAIL BOOM WAS NOT DETECTED. THE ULTRALIGHT WAS PREFLIGHTED & THE PLT TOOK OFF. AFTER CIRCLING ONCE & WAVING, HE STARTED ON THE RETURN FLT. SHORTLY AFTER THAT, WITNESSES HEARD THE ENG SLOW OR STOP AS THE ULTRALIGHT PITCHED NOSE DOWN INTO A STEEP DIVE & CRASHED. AN EXAM OF THE WRECKAGE REVEALED THAT THE RIGHT TAIL BOOM TUBE HAD SEPARATED IN FLT. DURING IMPACT, IT HAD PENETRATED THE HORIZONTAL STABILIZER SAIL WITHOUT BENDING. THE LEFT TAIL BOOM WAS BENT DURING IMPACT. A PICTURE OF THE ULTRALIGHT (TAKEN BEFORE TAKEOFF) REVEALED THAT THE HORIZONTAL STABILIZER WAS SLIGHTLY ANGLED FROM THE HORIZONTAL AXIS OF THE ULTRALIGHT.

Flight

Event TypeAccident
Event Time12:45 CDT
Nearest Airport0nm N
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftRotec Rally 2B
Tail NumberUNREG
Aircraft CategoryUltr
DamageDestroyed
Operating RulePart 103
Engines1
Engine TypeReciprocating
Engine DetailsKohler · 440 · Reciprocating · 30
Seats1

People & Injuries

Injury Summary1 injury (1 fatality)
Fatal1
Serious0
Minor0
Uninjured0
Total1
Crew 1Age 30 · Unknown

Conditions

ConditionsVMC
LightDaylight
Wind350° @ 10 kt
Visibility15 sm
CeilingNone
Temperature / Dew Point55
Altimeter30.00 inHg
Observation Time17:47
Weather SourceWFAC

Appendix: Source Data