19970721045699A

Accident · Destroyed

FAA accident report · Amtr Renegadespit · Boonsboro, MD · July 21, 1997

Date
July 21, 1997 · 19:10 local
Place
Boonsboro, MD
Phase of flight
Descent
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N416RS
NTSB investigation
NTSBIAD97LA102
Reported as
Amtr Renegadespit
Reported engine
ROTAX ROTAX582
People aboard
1
Fatal injuries
1
Pilot’s flight hours
300 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.

Witnesses watched as the pilot/owner maneauvered his homebuilt airplane at a low altitude. Some witnesses reported the engine sounds stopped before impact. The airplane's nose dropped down and it descended until ground impact and was destroyed during a post crash fire. Witnesses reported observing the airplane on numerous other occasions performing low level meaneuvering. Examination of the airframe and engine did not reveal an anomalies. The propeller blades were not damaged. Toxicological tests revealed a blood-alcohol level of .049 percent and a vitreous fluid-alcohol level of .055 percent. Federal aviation regulation (FAR) 91.17 stated: (a) no person may act or attempt to act as a crew member of a civil aircraft...(4) while having .04 percent by weight or more alcohol in the blood.

As the FAA filed it

WITNESSES WATCHED AS THE PILOT/OWNER MANEAUVERED HIS HOMEBUILT AIRPLANE AT A LOW ALTITUDE. SOME WITNESSES REPORTED THE ENGINE SOUNDS STOPPED BEFORE IMPACT. THE AIRPLANE'S NOSE DROPPED DOWN AND IT DESCENDED UNTIL GROUND IMPACT AND WAS DESTROYED DURING A POST CRASH FIRE. WITNESSES REPORTED OBSERVING THE AIRPLANE ON NUMEROUS OTHER OCCASIONS PERFORMING LOW LEVEL MEANEUVERING. EXAMINATION OF THE AIRFRAME AND ENGINE DID NOT REVEAL AN ANOMALIES. THE PROPELLER BLADES WERE NOT DAMAGED. TOXICOLOGICAL TESTS REVEALED A BLOOD-ALCOHOL LEVEL OF .049 PERCENT AND A VITREOUS FLUID-ALCOHOL LEVEL OF .055 PERCENT. FEDERAL AVIATION REGULATION (FAR) 91.17 STATED: (A) NO PERSON MAY ACT OR ATTEMPT TO ACT AS A CREW MEMBER OF A CIVIL AIRCRAFT...(4) WHILE HAVING .04 PERCENT BY WEIGHT OR MORE ALCOHOL IN THE BLOOD.

NTSB investigation

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