20000819009819A

Accident · Destroyed

FAA accident report · Amrgen AA-5B · Barrett, TX · August 19, 2000

Date
August 19, 2000 · 10:00 local
Place
Barrett, TX
Airport
Rogers
Phase of flight
Forced Landing
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N4516P
NTSB investigation
NTSBFTW00FA235
Reported as
Amrgen AA5B
Reported engine
Lycoming O360A4K
People aboard
4
Fatal injuries
4
Pilot’s flight hours
127 total56 in this make and model

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.

(-23) Witnesses stated aircraft appeared to be attemping emergency landing at private grass strip. Witnesses stated they heard engine sputtering during the approach and that pilot apparently tried to avoid people on the ground when he pulled up and banked. The airplane crashed in a heavily wooded area adjacent to the landing strip and was totally demolished by the post crash fire. All occupants were burned beyond recogition. (.4) witnesses located near the northwest end of a private airstrip reported that they observed the airplane approach from the west, and it appeared as if it was going to land. As the airplane flew by the witnesses, at about 30-60 feet AGL, the engine "sounded like it was cutting out." After the airplane passed the witnesses, it pulled up, and "suddenly the engine cut out." The airplane turned left and then nosed down into trees. The airplane was consumed by fire. No structural or mechanical anomalies were observed during the post accident examination of the airplane. The reason for the engine's loss of power could not be determined. The temperature was 86 degrees fahrenheit, and the dew point was 73 degrees fahrenheit. According to the car buretor icing probability chart, this places the airplane in the serious icing range at glide power.

As the FAA filed it

(-23) WITNESSES STATED AIRCRAFT APPEARED TO BE ATTEMPING EMERGENCY LANDING AT PRIVATE GRASS STRIP. WITNESSES STATED THEY HEARD ENGINE SPUTTERING DURING THE APPROACH AND THAT PILOT APPARENTLY TRIED TO AVOID PEOPLE ON THE GROUND WHEN HE PULLED UP AND BANKED. THE AIRPLANE CRASHED IN A HEAVILY WOODED AREA ADJACENT TO THE LANDING STRIP AND WAS TOTALLY DEMOLISHED BY THE POST CRASH FIRE. ALL OCCUPANTS WERE BURNED BEYOND RECOGITION. (.4) WITNESSES LOCATED NEAR THE NORTHWEST END OF A PRIVATE AIRSTRIP REPORTED THAT THEY OBSERVED THE AIRPLANE APPROACH FROM THE WEST, AND IT APPEARED AS IF IT WAS GOING TO LAND. AS THE AIRPLANE FLEW BY THE WITNESSES, AT ABOUT 30-60 FEET AGL, THE ENGINE "SOUNDED LIKE IT WAS CUTTING OUT." AFTER THE AIRPLANE PASSED THE WITNESSES, IT PULLED UP, AND "SUDDENLY THE ENGINE CUT OUT." THE AIRPLANE TURNED LEFT AND THEN NOSED DOWN INTO TREES. THE AIRPLANE WAS CONSUMED BY FIRE. NO STRUCTURAL OR MECHANICAL ANOMALIES WERE OBSERVED DURING THE POST ACCIDENT EXAMINATION OF THE AIRPLANE. THE REASON FOR THE ENGINE'S LOSS OF POWER COULD NOT BE DETERMINED. THE TEMPERATURE WAS 86 DEGREES FAHRENHEIT, AND THE DEW POINT WAS 73 DEGREES FAHRENHEIT. ACCORDING TO THE CAR BURETOR ICING PROBABILITY CHART, THIS PLACES THE AIRPLANE IN THE SERIOUS ICING RANGE AT GLIDE POWER.

NTSB investigation

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