19970526011779A

Accident · Substantial damage

FAA accident report · Amtrjf BARRACUDA · Arnold, MO · May 26, 1997

Date
May 26, 1997
Place
Arnold, MO
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N5926
NTSB investigation
NTSBCHI97FA146
Reported as
Amtrjf Barracuda
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.

(.4) A witness 'heard a plane flying very low and the engine was cutting in and out.' He looked across the valley and saw 'a small aircraft flying below the ridge very erratic.' The witness said he saw the airplane go into a roll and descend at a 45-degree angle. 'Just as I lost sight (of the airplane), the engine seemed to rev up slightly, then stop. I could hear the plane hitting the tree tops and then a loud thud.' Another witness said that he saw the airplane 'enter the clouds and then re-appear at tree top level in a descending left turn.' The witness said that as the airplane disappeared from sight, the engine sound increased, then decreased, followed by the sound of the airplane crashing into the trees. The pilot was not instrument rated. The weather was reported as broken to overcast ceiling of 400 feet mean sea level (MSL), 2 miles visibility, and winds from 110 degrees at 7 knots. There was no report that the pilot received a weather briefing before flight. The outboard 8 feet of the left wing was located 405 feet east-northeast of the main wreckage, and the left flap was found about 435 feet east-southeast of the main wreckage. An exam of the left wing revealed evidence of an in-flight breakup. The left main spar was bent upward and splintered. The wood laminates covering the forward and aft surfaces of the spar section showed wood fibers pulled apart in an upward vector. No anomalies were found that would have occurred before the in-flight breakup.

As the FAA filed it

(.4) A WITNESS 'HEARD A PLANE FLYING VERY LOW AND THE ENGINE WAS CUTTING IN AND OUT.' HE LOOKED ACROSS THE VALLEY AND SAW 'A SMALL AIRCRAFT FLYING BELOW THE RIDGE VERY ERRATIC.' THE WITNESS SAID HE SAW THE AIRPLANE GO INTO A ROLL AND DESCEND AT A 45-DEGREE ANGLE. 'JUST AS I LOST SIGHT (OF THE AIRPLANE), THE ENGINE SEEMED TO REV UP SLIGHTLY, THEN STOP. I COULD HEAR THE PLANE HITTING THE TREE TOPS AND THEN A LOUD THUD.' ANOTHER WITNESS SAID THAT HE SAW THE AIRPLANE 'ENTER THE CLOUDS AND THEN RE-APPEAR AT TREE TOP LEVEL IN A DESCENDING LEFT TURN.' THE WITNESS SAID THAT AS THE AIRPLANE DISAPPEARED FROM SIGHT, THE ENGINE SOUND INCREASED, THEN DECREASED, FOLLOWED BY THE SOUND OF THE AIRPLANE CRASHING INTO THE TREES. THE PILOT WAS NOT INSTRUMENT RATED. THE WEATHER WAS REPORTED AS BROKEN TO OVERCAST CEILING OF 400 FEET MEAN SEA LEVEL (MSL), 2 MILES VISIBILITY, AND WINDS FROM 110 DEGREES AT 7 KNOTS. THERE WAS NO REPORT THAT THE PILOT RECEIVED A WEATHER BRIEFING BEFORE FLIGHT. THE OUTBOARD 8 FEET OF THE LEFT WING WAS LOCATED 405 FEET EAST-NORTHEAST OF THE MAIN WRECKAGE, AND THE LEFT FLAP WAS FOUND ABOUT 435 FEET EAST-SOUTHEAST OF THE MAIN WRECKAGE. AN EXAM OF THE LEFT WING REVEALED EVIDENCE OF AN IN-FLIGHT BREAKUP. THE LEFT MAIN SPAR WAS BENT UPWARD AND SPLINTERED. THE WOOD LAMINATES COVERING THE FORWARD AND AFT SURFACES OF THE SPAR SECTION SHOWED WOOD FIBERS PULLED APART IN AN UPWARD VECTOR. NO ANOMALIES WERE FOUND THAT WOULD HAVE OCCURRED BEFORE THE IN-FLIGHT BREAKUP.

NTSB investigation

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