Premium research interface

The modern interface for aviation safety intelligence.

Search investigations, review source evidence, monitor watched reports, and trace long-term patterns from one calm, data-first workspace.

63k+
Reports indexed
1940-2026
Coverage
Recent
Last data refresh
Featured Report

Loading…

Loading featured report…

Loading…
Open Report

Safety trends by operating rule

Track fatal and non-fatal accident patterns across Part 91, Part 135, and Part 121 operations.

Loading trend charts…

Browse the aviation graph

Move quickly by aircraft, airport, operator, and time with indexes built for research, not wandering.

Last Data Update

By Decade

By Month

Aircraft Manufacturer

More manufacturers

Airports

More airports

Operators

More operators

About

Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

The goal is practical safety education: make it faster to find relevant investigations, compare similar events, review factual records, and understand the evidence behind probable-cause and preliminary reports.

The investigative work and source records belong to the National Transportation Safety Board and the published investigation record. This site is not affiliated with or endorsed by the NTSB.

FAQs

NTSB Report

December 12, 2006 · Extra Flugzeugbau Gmbh EA 300/L · N91BH

Boulder City, NV

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
December 12, 2006
Injury Outcomes
1 injury (1 minor injury), 1 uninjured
Location
Boulder City, NV
Aircraft
Extra Flugzeugbau Gmbh EA 300/L
Tail Number
N91BH
Operator
Aerobatic Experience
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
SEA07CA033

The pilot lost directional control of the airplane during the takeoff run, and the airplane cartwheeled prior to coming to rest upright. The pilot was flying from the aft seat as pilot-in-command (PIC) and a pilot-rated passenger was in the front seat. During the takeoff run, the airplane veered from the runway and attempts were made to position the airplane back to runway heading. As it veered from the runway, the airplane entered soft soil, decreasing the available performance. The takeoff was continued due to a drainage ditch immediately in their direction of travel. After the airplane cleared the ditch, the right aileron spade impacted a fence post and the airplane cartwheeled. During the impact sequence, the engine was ripped from its mounts and the outboard portion of the left wing separated. The post-accident inspection revealed no evidence of mechanical malfunctions with the airplane prior to the accident.

NTSB Probable Cause

The pilot-in-command's failure to maintain directional control of the airplane during takeoff.

Full Narrative

On December 12, 2006, at 1430 Pacific standard time, an Extra Flugzeugbau GMBH EA 300/L, N91BH, veered off the runway during takeoff from runway 9R at Boulder City Municipal Airport, Boulder City, Nevada. The airplane was owned by a private company and was being operated by the Aerobatic Experience under the provisions of 14 CFR Part 91. The commercial pilot, who held an airline transport pilot certificate in multi-engine airplanes and a commercial certificate for single-engine airplanes, sustained minor injuries, and the commercial certificated passenger was not injured. The airplane sustained substantial damage. Visual meteorological conditions prevailed, and no flight plan was filed. The local formation flight was originating at the time of the accident. The pilot reported in a written statement that the purpose of the flight was a two-airplane formation flight, of which the accident airplane was in the number two position. The pilot was acting as pilot-in-command (PIC) of the flight and seated in the rear seat, and the passenger was performing the takeoff. As the tail rose during the takeoff roll, the airplane began to swerve across the runway. The right wing came up slightly and then the airplane veered to the right and departed the runway surface. Due to the soft terrain at the runway edge, the airplane would not accelerate. The PIC noted a large drainage ditch and decided that aborting the takeoff would not be possible with the obstruction. The airplane flew over the ditch and then touched down with the right main gear on the far side of the ditch. The airplane then cartwheeled and came to rest upright with the left wing separated at its mid-section and the right wing angled upward. The passenger stated that he had purchased the aircraft flight from Aerobatic Experience with the intent of obtaining formation instruction. During the flight, both the passenger and PIC were on the controls. The airplane accelerated and the PIC told the passenger that they had a left crosswind, so they applied crosswind correction. The right wing rose and the passenger said he eased control application of the left crosswind correction. As he eased off of the correction, the airplane canted to the right. At 50-60 knots, the airplane departed the runway surface to the right and just prior to impacting a ditch, became airborne. Following the ditch, the right aileron spade impacted a fence post and the airplane cartwheeled. The Federal Aviation Administration accident coordinator responded from the Las Vegas Flight Standards District Office. A flight control continuity check was performed and movement was obtained to the rudder, elevators, and right aileron. The left aileron had separated from the left wing. Examination of the braking system showed normal operation. No mechanical malfunctions were noted.

Flight

Event TypeAccident
Event Time14:30 PST
Nearest AirportBoulder City Muni Airport (0nm)
Runway9R
Runway Length4800 ft
Runway Width75 ft
Flight Plan FiledNone
Aircraft FireNo

Aircraft

AircraftExtra Flugzeugbau Gmbh EA 300/L
Tail NumberN91BH
Aircraft CategoryAir
DamageSubstantial
OperatorAerobatic Experience
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsTextron Lycoming · AEIO-540 · Reciprocating

People & Injuries

Injury Summary1 injury (1 minor injury), 1 uninjured
Fatal0
Serious0
Minor1
Uninjured1
Total2
Crew 1Age 55 · First Class
Crew 2Age 40 · First Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
CeilingNone
Temperature / Dew Point0 C / 0 C
Altimeter0

Appendix: Source Data