ASN Wikibase Occurrence # 39338
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information.
If you feel this information is incomplete or incorrect, you can
submit corrected information.
Date: | Sunday 8 May 1983 |
Time: | 12:45 |
Type: | Rotec Rally 2 b |
Owner/operator: | private |
Registration: | unreg. |
MSN: | |
Fatalities: | Fatalities: 1 / Occupants: 1 |
Aircraft damage: | Destroyed |
Category: | Accident |
Location: | Manvel, TX -
United States of America
|
Phase: | En route |
Nature: | Private |
Departure airport: | |
Destination airport: | Alvin, TX |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
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 flight. 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 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. CAUSE:
Sources:
NTSB:
https://www.ntsb.gov/ntsb/brief.asp?ev_id=20001214X42977 Revision history:
Date/time | Contributor | Updates |
24-Oct-2008 10:30 |
ASN archive |
Added |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation