Piper PA30 - NO SERIES accident near Bullhead City, Arizona, April 21, 2014
On April 21, 2014 at about 9:00 pm local time, a 1965 Piper PA30 - NO SERIES, registered N7880Y, was substantially damaged in an accident during approach (VFR pattern final) near Bullhead City, Arizona (Sun Valley airport). It was a personal flight under general aviation rules (Part 91). 1 person had minor injuries. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot's mismanagement of the throttle and propeller controls during the attempted go-around after encountering turbulence, which resulted in his failure to maintain adequate airspeed and climb rate and a subsequent forced landing and impact with terrain. Contributing to the accident was the pilot’s lack of knowledge about the airplane’s equipment.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- April 21, 2014 · about 9:00 pm local time
- Place
- Bullhead City, Arizona · Sun Valley · map
- Type
- Accident
- Injuries
- 1 person had minor injuries.
- Weather
- visual conditions (good weather)
- Aircraft
- Piper PA30 - NO SERIES, built 1965 · all PA30 - NO SERIESs on the register
- Registration
- N7880Y · no longer on the register · serial 30-965
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot reported that, upon arrival at the airport, he overflew the runway, checked the wind direction, and then entered the downwind leg for a landing to the north. While turning onto final approach, the airplane encountered severe turbulence, at which time the pilot initiated a go-around by adding full power to both engines. However, he noted that "it seemed like the airplane would not fly" and that it was "like it was being pushed down." He added that he was not sure if the engines completely failed or not but that "I just know I didn't have any power." The airplane subsequently impacted terrain about 1/4 mile from the departure end of the runway and then came to rest upright. The airplane sustained substantial damage to the wings and empennage. Postaccident examination of the airplane and engine revealed no mechanical malfunctions or failures that would have precluded normal operation. Fuel was drained from both the left and right fuel tanks, and no water or sediment was observed. The left propeller blades were found in the feathered position, and the right propeller blades were found in low pitch. The feathered propellers indicated that, despite the pilot's statement that the engine did not have power, the engine likely did have power but no thrust. Followup discussions with the pilot revealed that he had been improperly using the propeller controls as the throttles, with the throttle controls in the full-forward position, during the flight. Additionally, the pilot had pulled both propeller controls to the full-feather position upon touching down on the runway and then abruptly advanced them when he initiated a go-around rather than using the throttle as required. The pilot reported that he had an extensive amount of flight time in another airplane make and model that was configured with the propeller and throttle controls oriented in a position directly opposite their position in the accident airplane. The pilot's mismanagement of the throttle and propeller controls during the attempted go-around after encountering turbulence resulted in insufficient airspeed and degraded climb performance and a subsequent forced landing and impact with terrain.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Turbulence encounter during approach (VFR pattern final) defining event
- Loss of lift during approach (VFR go-around)
- Off-field or emergency landing during approach (VFR go-around)
- Collision with terrain or object (not controlled flight into terrain) during approach (VFR go-around)
The NTSB's findings
- cause Personnel issues › Action/decision › Action › Incorrect action sequence › Pilot
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Climb rate › Not attained/maintained
- cause Personnel issues › Task performance › Use of equip/info › Use of equip/system › Pilot
- cause Aircraft › Aircraft power plant › Engine controls › Power lever › Incorrect use/operation
- cause Aircraft › Aircraft propeller/rotor › Propeller system › Propeller controlling system › Incorrect use/operation
- factor Personnel issues › Experience/knowledge › Knowledge › Knowledge of equipment › Pilot
- Environmental issues › Conditions/weather/phenomena › Turbulence › Convective turbulence › Decision related to condition
Pilot
- Certificate: private
- Ratings: multi-engine land; single-engine land; instrument: airplane
- Flight time: 9,000 hours in all; 1,850 in this make and model; 3 in the last 90 days; 1 in the last 30 days; 9,000 as pilot in command
- Last flight review: May 22, 2012
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: left
- Injury: no injuries
The aircraft
- Airframe total time: 5,235.3 hours
- Last inspection: annual inspection, September 12, 2013; 4 hours since
- Maximum gross weight: 3,600 lb
- Seats: 6
- Landing gear: retractable
- Engine 1: Lycoming IO-320-B1A (piston); 5,239 hours total
- Engine 2: Lycoming IO-320-B1A (piston); 5,239 hours total
The flight
- Departed from: HII Lake Havasu AZ at 8:24 pm
- Destination: A20 Bullhead City AZ
- Flight plan: none
- Runway 36, 3,700 ft by 42 ft
Weather at the time
- Light: daylight
- Wind: from 210° at 8 knots, gusting 19
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 93°F (34°C), dew point 37°F (3°C)
- Altimeter: 29.90 inHg
- Observation at 8:35 pm from IFP, 10 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
10 documents, released by the NTSB on February 18, 2015. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.
| # | Document | What it is | |
|---|---|---|---|
| 1 | Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 | PDF, 9 pages | View Download |
| 2 | Weather Data | PDF, 1 page | View Download |
| 3 | FAA Inspector's Report | PDF, 1 page | View Download |
| 4 | Excerpts from Maintenance Records | PDF, 7 pages | View Download |
| 5 | Record of Conversation - FAA Inspector | PDF, 1 page | View Download |
| 6 | Statement from A&p Mechanic - Mark Naumer | PDF, 1 page | View Download |
| 7 | Release of Aircraft Wreckage, NTSB Form 6120.15 | PDF, 1 page | View Download |
| 8 | Photo 1 - Propellers (Photo Courtesy of FAA) | PDF, 1 page | View Download |
| 9 | Photo 2 - Power Control Quadrant (Photo Courtesy of FAA) | PDF, 1 page | View Download |
| 10 | Photo 3 - Earlier Beechcraft Baron Model Power Control Quadrant (Photo Courtesy of Textron Aviation) | PDF, 1 page | View Download |
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
