ASN Wikibase Occurrence # 294593
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Date: | Sunday 16 January 1994 |
Time: | 12:58 |
Type: | Piper PA-24-250 Comanche |
Owner/operator: | Private |
Registration: | N6522P |
MSN: | 24-1644 |
Total airframe hrs: | 2894 hours |
Engine model: | LYCOMING O-540-A1C5 |
Fatalities: | Fatalities: 2 / Occupants: 2 |
Aircraft damage: | Destroyed |
Category: | Accident |
Location: | near Ratcliff, TX -
United States of America
|
Phase: | Manoeuvring (airshow, firefighting, ag.ops.) |
Nature: | Private |
Departure airport: | Scholes International Airport, TX (KGLS) |
Destination airport: | Tyler Pounds Regional Airport, TX (KTYR) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:On January 16, 1994, at 1258 central standard time, a Piper PA- 24-250, N6522P, was destroyed upon impact with terrain following a loss of control while maneuvering near Ratcliff, Texas. The private pilot and his two passengers were fatally injured. Visual meteorological conditions prevailed for the personal flight.
BEFORE DEPARTING ON A FLIGHT FROM GALVESTON TO TYLER,TEXAS, THE NON- INSTRUMENT RATED PILOT WAS ADVISED THAT VFR FLIGHT WAS NOT RECOMMENDED. SUBSEQUENTLY, THE AIRPLANE CRASHED ALONG THE ROUTE NEAR RATCLIFF, TEXAS. WITNESSES INDICATED THAT BEFORE THE ACCIDENT OCCURRED, THE AIRCRAFT WAS MANEUVERING IN THE AREA. ACCORDING TO THEM, THERE WAS AN INTERUPTION IN THE SOUND OF THE ENGINE, THEN IT REVVED TO A HIGH POWER SETTING AS THE AIRCRAFT WENT INTO A DIVE & CRASHED. AN EXAM OF THE WRECKAGE REVEALED THAT AN IN-FLIGHT BREAKUP OF THE AIRCRAFT OCCURRED. BOTH HORIZONTAL STABILATORS & THE OUTBOARD SECTION OF THE RIGHT WING HAD FAILED. THEY WERE FOUND ABOUT 400 FEET SHORT OF WHERE THE MAIN WRECKAGE HAD IMPACTED. ABOUT 28 MILES EAST-SOUTHEAST AT LUFKIN, THE WEATHER WAS IN PART: 1200' BROKEN, 4 MILES VISIBILITY WITH HAZE, FOG & DRIZZLE. ONE WITNESS ESTIMATED THE AIRPLANE WAS FLYING AT ABOUT 1000' AGL WHEN HE FIRST SAW IT. THE INVESTIGATION DID NOT VERIFY WHETHER THE AIRPLANE WAS MANEUVERING ABOVE OR BELOW THE BASE OF THE CLOUDS BEFORE IT BROKE UP.
Probable Cause: THE PILOT FAILED TO MAINTAIN CONTROL OF THE AIRPLANE AND ALLOWED IT TO EXCEED ITS DESIGN STRESS LIMITS, WHICH RESULTED IN OVERLOAD FAILURE OF THE STABILATORS AND RIGHT OUTBOARD WING SECTION.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | FTW94FA065 |
Status: | Investigation completed |
Duration: | 1 year and 2 months |
Download report: | Final report |
|
Sources:
NTSB
Images:
Photos: NTSB
Revision history:
Date/time | Contributor | Updates |
12-Oct-2022 01:12 |
Captain Adam |
Added |
12-Oct-2022 01:12 |
Captain Adam |
Updated [Narrative, Photo] |
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