19970812021759A

Accident · Destroyed

FAA accident report · Beech 65-A90 · Alice, TX · August 12, 1997

Date
August 12, 1997 · 11:53 local
Place
Alice, TX
Airport
Alice International Airport
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N41VC
NTSB investigation
NTSBCHI97FA256
Reported as
Beech 65A90
Reported engine
Pratt & Whitney PT6A20
People aboard
4
Fatal injuries
4
Pilot’s flight hours
17,710 total

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Aircraft took off, started left turn back to airport, crashed. (.4)the flight was part of a pre-buy inspecion of the airplane. Witnesses reported the airplane did not climb more than 200 feet above groung level (AGL) after takeoff. The airplane entered a shallow left turn and completed about 210 degrees of heading change before it impacted a flat field near the approach end of runway 26. Witnesses reported that the landing gear were retracted and that the engines sounded like they running at hight power, but the airplane did not accelerate or climb normally. The airspeed was slow and 'mushy.' The engines gas generator sections exhibited strong rotational scoring. The engines power sections exhibited light rotational signatures. The left and right porpellers exhibited minimal leading edge damage. Both propellers exhibited high blade angles. The secondary low pitch stops (slps) had been instaled on the aircraft four days prior to the accident. A ground check, but no flight check, had been conducted. The slps sensors were found in the full aft position on the mounting bracket, not in the normal mid-range position. The slps control box installed on the aircraft was an up dated box and was incompatible with the existing wiring. The aircraft had liability insurance, but it did not have hull insurance. (-23) on August 12, 1997, at 11:53 central daylight time, a Beech BE-65-A90, N41VC, operated by south Texas aircraft, inc., was destroyed when it impacted terrain 1/4 mile from the Alice International Airport, Alice, Texas. Witnesses reported that the aircraft departed runway 13 but did not climb more than 200 feet above ground level (AGL). The airplane entered a shallow left turn and completed about 210 degrees of heading change before it impacted a field near the approach end of runway 26. The pilot, copilot, and two passengers were fatally injured. The 14 CFR part 91 flight departed Alice, Texas, on a local flight as part of an aircraft sales pre-buy flight. Visual meteorological conditions prevailed and no flight plan had been filed.

As the FAA filed it

AIRCRAFT TOOK OFF, STARTED LEFT TURN BACK TO AIRPORT, CRASHED. (.4)THE FLIGHT WAS PART OF A PRE-BUY INSPECION OF THE AIRPLANE. WITNESSES REPORTED THE AIRPLANE DID NOT CLIMB MORE THAN 200 FEET ABOVE GROUNG LEVEL (AGL) AFTER TAKEOFF. THE AIRPLANE ENTERED A SHALLOW LEFT TURN AND COMPLETED ABOUT 210 DEGREES OF HEADING CHANGE BEFORE IT IMPACTED A FLAT FIELD NEAR THE APPROACH END OF RUNWAY 26. WITNESSES REPORTED THAT THE LANDING GEAR WERE RETRACTED AND THAT THE ENGINES SOUNDED LIKE THEY RUNNING AT HIGHT POWER, BUT THE AIRPLANE DID NOT ACCELERATE OR CLIMB NORMALLY. THE AIRSPEED WAS SLOW AND 'MUSHY.' THE ENGINES GAS GENERATOR SECTIONS EXHIBITED STRONG ROTATIONAL SCORING. THE ENGINES POWER SECTIONS EXHIBITED LIGHT ROTATIONAL SIGNATURES. THE LEFT AND RIGHT PORPELLERS EXHIBITED MINIMAL LEADING EDGE DAMAGE. BOTH PROPELLERS EXHIBITED HIGH BLADE ANGLES. THE SECONDARY LOW PITCH STOPS (SLPS) HAD BEEN INSTALED ON THE AIRCRAFT FOUR DAYS PRIOR TO THE ACCIDENT. A GROUND CHECK, BUT NO FLIGHT CHECK, HAD BEEN CONDUCTED. THE SLPS SENSORS WERE FOUND IN THE FULL AFT POSITION ON THE MOUNTING BRACKET, NOT IN THE NORMAL MID-RANGE POSITION. THE SLPS CONTROL BOX INSTALLED ON THE AIRCRAFT WAS AN UP DATED BOX AND WAS INCOMPATIBLE WITH THE EXISTING WIRING. THE AIRCRAFT HAD LIABILITY INSURANCE, BUT IT DID NOT HAVE HULL INSURANCE. (-23) ON AUGUST 12, 1997, AT 11:53 CENTRAL DAYLIGHT TIME, A BEECH BE-65-A90, N41VC, OPERATED BY SOUTH TEXAS AIRCRAFT, INC., WAS DESTROYED WHEN IT IMPACTED TERRAIN 1/4 MILE FROM THE ALICE INTERNATIONAL AIRPORT, ALICE, TEXAS. WITNESSES REPORTED THAT THE AIRCRAFT DEPARTED RUNWAY 13 BUT DID NOT CLIMB MORE THAN 200 FEET ABOVE GROUND LEVEL (AGL). THE AIRPLANE ENTERED A SHALLOW LEFT TURN AND COMPLETED ABOUT 210 DEGREES OF HEADING CHANGE BEFORE IT IMPACTED A FIELD NEAR THE APPROACH END OF RUNWAY 26. THE PILOT, COPILOT, AND TWO PASSENGERS WERE FATALLY INJURED. THE 14 CFR PART 91 FLIGHT DEPARTED ALICE, TEXAS, ON A LOCAL FLIGHT AS PART OF AN AIRCRAFT SALES PRE-BUY FLIGHT. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND NO FLIGHT PLAN HAD BEEN FILED.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.