Aero Commander 500 S accident near Fort Huachuca, Arizona, May 17, 2014
On May 17, 2014 at about 5:20 pm local time, a 1976 Aero Commander 500 S, registered N40TC, was substantially damaged in an accident during initial climb near Fort Huachuca, Arizona (Sierra Vista Muni-Libby Aaf airport). It was an other work-use flight under general aviation rules (Part 91). 1 person was killed and 1 person was seriously injured. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot’s failure to maintain adequate airspeed and his exceedance of the airplane’s critical angle-of-attack after a total loss of engine power during the takeoff initial climb, which resulted in an aerodynamic stall and impact with terrain. The reason for the total loss of engine power could not be determined because an examination of the airframe and engines did not reveal any anomalies that would have precluded normal operation.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- May 17, 2014 · about 5:20 pm local time
- Place
- Fort Huachuca, Arizona · Sierra Vista Muni-Libby Aaf · map
- Type
- Accident
- Injuries
- 1 person was killed and 1 person was seriously injured.
- Weather
- visual conditions (good weather)
- Aircraft
- Aero Commander 500 S, built 1976 · all 500 Ss on the register
- Registration
- N40TC · no longer on the register · serial 3091
- Damage
- Substantial damage
- Flight
- Other work-use flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The commercial pilot reported that the purpose of the flight was to perform a check/orientation flight with the airline transport pilot (ATP), who was new to the area; the ATP was the pilot flying. The airplane was started, and an engine run-up completed. The commercial pilot reported that, during the takeoff roll, all of the gauges were in the "green." After reaching an airspeed of 80 knots, the airplane lifted off the ground. About 350 ft above ground level (agl), the pilots felt the airplane "jolt." The commercial pilot stated that it felt like a loss of power had occurred and that the airplane was not responding. He immediately shut off the boost pumps, and the ATP initiated a slow left turn in an attempt to return to the airport to land. The airplane descended rapidly in a nose-low, right-wing-low attitude and impacted the ground. A witness reported that he watched the airplane take off and that it sounded normal until it reached the departure end of the runway, at which point he heard a distinct "pop pop," followed by silence. The airplane then entered an approximate 45-degree left turn with no engine sound and descended at a high rate with the wings rolling level before the airplane went out of sight. Another witness made a similar statement. Based on the witnesses' statements and photographs of the twisted airplane at the accident site, it is likely that a total loss of engine power occurred and that, during the subsequent turn back to the airport, the ATP did not maintain sufficient airspeed and exceeded the airplane's critical angle-of-attack, which resulted in an aerodynamic stall and impact with terrain. Although a postaccident examination of the airframe and engines did reveal an inconsistency between the cockpit control positions and the positions of the fuel shutoff valves on the sump tank, this would not have precluded normal operation. No other anomalies were found that would have precluded normal operation.
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
- Loss of engine power (total) during initial climb defining event
- Off-field or emergency landing during initial climb
- Collision with terrain or object (not controlled flight into terrain) during initial climb
The NTSB's findings
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Not attained/maintained
- cause Not determined › Not determined › (general) › (general) › Unknown/Not determined
Pilot
- Certificate: airline transport pilot
- Ratings: multi-engine land; single-engine land; single-engine sea; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
- Flight time: 13,175 hours in all; 600 in this make and model; 8 in the last 90 days; 13,075 as pilot in command
- Last flight review: March 5, 2014
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: left
- Injury: fatal
Pilot
- Certificate: commercial pilot
- Ratings: multi-engine land; single-engine land; instrument: airplane
- Flight time: 16,560 hours in all; 4,100 in this make and model; 80 in the last 90 days; 20 in the last 30 days; 15,560 as pilot in command
- Last flight review: March 7, 2014
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: rgt
- Injury: serious injuries
The aircraft
- Airframe total time: 21,660 hours
- Last inspection: approved inspection programme, December 23, 2013; 26 hours since
- Maximum gross weight: 6,750 lb
- Seats: 5
- Landing gear: retractable
- Engine 1: Lycoming IO-540-E1B5 (piston); 0 hours total
- Engine 2: Lycoming IO-540-E1B5 (piston); 0 hours total
- Operator: Ponderosa Aviation INC
The flight
- Departed from: FHU Fort Huachuca AZ at 5:20 pm
- Destination: FHU Fort Huachuca AZ
- Flight plan: none
- Runway 26, 12,001 ft by 150 ft
- A second pilot was aboard
Weather at the time
- Light: daylight
- Wind: from 320° at 7 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 82°F (28°C), dew point 3°F (-16°C)
- Altimeter: 30.11 inHg
- Observation at 4:56 pm from FHU
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
10 documents, released by the NTSB on May 3, 2016. 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 | Pilot Statements Courtesy of the Federal Aviation Administration and Ponderosa Aviation | PDF, 3 pages | View Download |
| 3 | Witness Statements | PDF, 5 pages | View Download |
| 4 | Airframe and Engine Examination Summary | PDF, 6 pages | View Download |
| 5 | Magneto Examination Summary | PDF, 3 pages | View Download |
| 6 | Twin Commander Airframe Examination Summary | PDF, 8 pages | View Download |
| 7 | Statement of Party Representatives to NTSB Investigation | PDF, 2 pages | View Download |
| 8 | Release of Aircraft Wreckage, NTSB Form 6120.15 | PDF, 1 page | View Download |
| 9 | Evidence Control Form | PDF, 3 pages | View Download |
| 10 | On Scene Photos (Courtesy of Airport Operations) | PDF, 3 pages | 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.
