- Date
- July 14, 2013, 09:30 local (15:30 UTC)
- Place
- Bozeman, MT
- Injuries
- 2 uninjured
- Damage
- Substantial damage
- Phase of flight
- Initial climb
- Aircraft
- N5176NBoeing E75
- Defining event
- Initial climb: Loss of lift
- Weather
- Visual (VMC) · Day
- Status
- Completed · report September 12, 2013
- Report
- Approved by Office Director
- NTSB office
- Western Pacific Region
- Parties
- Federal Aviation Administration
- FAA report
- 20130714011209A
- Case key
- 87473
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
Probable cause
The pilot’s failure to maintain adequate airspeed during a turn, which resulted in a loss of lift and collision with terrain.
Findings · 3
NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.
Sequence of events
The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.
Analysis
The pilot reported that he and the pilot-rated passenger, departed from the turf runway in calm wind conditions. During the initial climb, the airplane’s climb rate was not as expected and he attributed this degraded climb performance to likely being the result of the addition of the passenger’s weight. Upon reaching 200 feet above ground level (agl), the pilot began a 180-degree turn to the north in an effort to gain altitude while avoiding maneuvering over obstacles and a more densely populated area. As the airplane entered the bank, the pilot felt a degradation in performance despite indications that both the engine power and airspeed were adequate. The airplane was not maintaining altitude and in an effort to avoid colliding into a subdivision, the pilot increased the bank angle. The airplane subsequently collided into terrain and came to rest in a ditch adjacent to the airport’s perimeter fence. During the accident sequence the airplane sustained damage to the wings and empennage. The pilot further stated that he believed the airplane’s descent during the turn was a result of either of the following: a downdraft, too high angle-of-attack attitude, or possible decrease in engine power output. He reported no mechanical malfunctions or failures with the airplane that would have precluded normal operation. The passenger opined that the accident was a result of the airspeed being too slow for the steep bank angle.
Factual narrative
The pilot reported that he and the pilot-rated passenger, departed from the turf runway in calm wind conditions. During the initial climb, the airplane’s climb rate was not as expected and he attributed this degraded climb performance to likely being the result of the addition of the passenger’s weight. Upon reaching 200 feet above ground level (agl), the pilot began a 180-degree turn to the north in an effort to gain altitude while avoiding maneuvering over obstacles and a more densely populated area. As the airplane entered the bank, the pilot felt a degradation in performance despite indications that both the engine power and airspeed were adequate. The airplane was not maintaining altitude and in an effort to avoid colliding into a subdivision, the pilot increased the bank angle. The airplane subsequently collided into terrain and came to rest in a ditch adjacent to the airport’s perimeter fence. During the accident sequence the airplane sustained damage to the wings and empennage. The pilot further stated that he believed the airplane’s descent during the turn was a result of either of the following: a downdraft, too high angle-of-attack attitude, or possible decrease in engine power output. He reported no mechanical malfunctions or failures with the airplane that would have precluded normal operation. The passenger opined that the accident was a result of the airspeed being too slow for the steep bank angle.
Aircraft
- Registration
- N5176N
- Reported as
- Boeing E75
- Category
- Airplane
- Serial number
- 75-5379
- Engine
- Lycoming R680, 215 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Airworthiness certificate
- Standard, Aerobatic
- Departed
- BZM · Bozeman, MT
- Destination
- BZM · Bozeman, MT
- Flight plan
- Unknown
- Airport
- BZM · Bozeman Yellowstone, runway 11, 3,197 × 80 ft, grass/turf
Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.
Flight crew
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 61
- Injuries
- None
- Certificate
- Private
- Airplane ratings
- Single-engine land
- Medical
- Class 3, With waivers/limitations
- Flight hours
- 1,780 total · 611 in this make and model
Weather
- Conditions
- Visual (VMC) · Day
- Visibility
- 15 statute miles
- Lowest ceiling
- None
- Temperature
- 64 °F, dew point 48 °F
- Altimeter
- 30.21 inHg
Docket · 1
The files NTSB released with the investigation on September 10, 2013, on NTSB’s docket system: statements, records, photos and specialists’ reports. 2.3 MB in all.
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.
Other investigations on N5176N · 1
Matched to the same aircraft by N-number and date.