20000422009619A

Accident · No damage

FAA accident report · Emigh TROJAN A-2 · Brentwood, CA · April 22, 2000

Date
April 22, 2000 · 14:00 local
Place
Brentwood, CA
Operating rules
General operating rules (Part 91)
Damage
No damage
Aircraft
N8324H
NTSB investigation
NTSBLAX00FA170
People aboard
2
Fatal injuries
2

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)A/c impacted ground in a northward direction. The a/c landed flat with litte or no forward motion. This is evident because the debris pattern and a metal spike that penetrated the wing leaving a small hole in the wing with little deformation or tearing that would have been presenting with forward a/c momentum. The engine was not turning when the a/c impacted the ground. This was evident because the propeller showed not tip damage and damage to the trailing edges and a straight rearward bending of the lower blade, little rearward bending of the upper blade. Engine examination is pending. Witness statements say the a/c was "sputtering" as it descended, banked right, banded right again appearing to attempt a landing in a open field. In the middle of a final 180 degree turn, at 60 to 70 feet AGL, the a/c turned to the left (final northward direction) and nosed over, falling to impact at about a 45 degree attitude, nose down. An explosion and fire immediately followed and burned out in about 10 minutes. 2 occupants fatal at scene.

As the FAA filed it

(-23)A/C IMPACTED GROUND IN A NORTHWARD DIRECTION. THE A/C LANDED FLAT WITH LITTE OR NO FORWARD MOTION. THIS IS EVIDENT BECAUSE THE DEBRIS PATTERN AND A METAL SPIKE THAT PENETRATED THE WING LEAVING A SMALL HOLE IN THE WING WITH LITTLE DEFORMATION OR TEARING THAT WOULD HAVE BEEN PRESENTING WITH FORWARD A/C MOMENTUM. THE ENGINE WAS NOT TURNING WHEN THE A/C IMPACTED THE GROUND. THIS WAS EVIDENT BECAUSE THE PROPELLER SHOWED NOT TIP DAMAGE AND DAMAGE TO THE TRAILING EDGES AND A STRAIGHT REARWARD BENDING OF THE LOWER BLADE, LITTLE REARWARD BENDING OF THE UPPER BLADE. ENGINE EXAMINATION IS PENDING. WITNESS STATEMENTS SAY THE A/C WAS "SPUTTERING" AS IT DESCENDED, BANKED RIGHT, BANDED RIGHT AGAIN APPEARING TO ATTEMPT A LANDING IN A OPEN FIELD. IN THE MIDDLE OF A FINAL 180 DEGREE TURN, AT 60 TO 70 FEET AGL, THE A/C TURNED TO THE LEFT (FINAL NORTHWARD DIRECTION) AND NOSED OVER, FALLING TO IMPACT AT ABOUT A 45 DEGREE ATTITUDE, NOSE DOWN. AN EXPLOSION AND FIRE IMMEDIATELY FOLLOWED AND BURNED OUT IN ABOUT 10 MINUTES. 2 OCCUPANTS FATAL AT SCENE.

NTSB investigation

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