ASN Wikibase Occurrence # 38068
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: | Tuesday 24 March 1998 |
Time: | 13:30 |
Type: | Bell 206A JetRanger |
Owner/operator: | Pinarsa |
Registration: | TG-JET |
MSN: | 86 |
Year of manufacture: | 1967 |
Total airframe hrs: | 2457 hours |
Engine model: | Allison 250-C18 |
Fatalities: | Fatalities: 2 / Occupants: 2 |
Aircraft damage: | Destroyed |
Category: | Accident |
Location: | Rio Hondo, TX -
United States of America
|
Phase: | Unknown |
Nature: | Ferry/positioning |
Departure airport: | New Braunfels, TX (3R5) |
Destination airport: | Brownsville, TX (BRO) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:A witness observed the Bell 206-A helicopter 'flying fast' in a southerly direction at about 500 to 600 feet agl. Flames were coming from the helicopter's right rear side in the vicinity of the engine compartment, and very little smoke was observed. Prior to descending from view, the helicopter appeared to be in controlled flight. Subsequently, the aircraft impacted the ground and was destroyed by the in-flight and postimpact fire. Examination of the engine compartment revealed that the step portion of the forward firewall where the throttle and fuel line pass through had localized bluing; however the fuel line connector which was still attached to the firewall fitting, did not exhibit any fire damage. The #3 tail rotor drive shaft segment was found 66 feet prior to the initial impact scar. It was fractured with fire damaged fiberglass cloth wrapped around the forward end of the fractured shaft. According to a NTSB metallurgist, 'the fracture was consistent with an overstress after exposure to elevated temperatures.' The helicopter was returning to Guatemala after completion of schedule maintenance performed in the United States. CAUSE: The engine compartment fire due to undetermined reasons, which resulted in the in-flight separation of the tailboom.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | FTW98FA156 |
Status: | Investigation completed |
Duration: | 2 years and 11 months |
Download report: | Final report |
|
Sources:
NTSB:
https://www.ntsb.gov/ntsb/brief.asp?ev_id=20001211X09660 Location
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