Yakovlev YAK11 accident near West Mifflin, Pennsylvania, July 25, 2016
On July 25, 2016 at about 1:45 pm local time, a 1952 Yakovlev YAK11, registered N5940, was substantially damaged in an accident during landing (landing roll) near West Mifflin, Pennsylvania (Allegheny County airport). It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
A malfunction of the electrical system, which resulted in an electrical fire in the right wing root of the airplane, which compromised the fuel system and resulted in ignition of fuel. Contributing to the accident was the routing of the electrical wiring near fuel system components. Contributing to the severity of the pilot's injuries was his failure to utilize the available fire-retardant suit.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- July 25, 2016 · about 1:45 pm local time
- Place
- West Mifflin, Pennsylvania · Allegheny County · map
- Type
- Accident
- Injuries
- 1 person was killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Yakovlev YAK11 NO SERIES, built 1952
- Registration
- N5940 · no longer on the register · serial 210
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
During the first leg of a multi-leg cross-country flight, the commercial pilot contacted the destination airport tower controller and advised that the airplane's transponder was inoperative. He was instructed to proceed straight in for the runway and was cleared to land. While taxiing after landing, the airplane turned and its right side became visible to control tower personnel, who observed a fire under the right wing and informed the pilot. The airplane continued off the paved surface of the runway, over a drainage ditch, and rolled through the airport infield until it came to rest near a taxiway. Increasing amounts of smoke and flames continued to emanate from the right side of the airplane. The pilot, who was clad in shorts, a T-shirt, socks, and tennis shoes, was able to egress the airplane after it came to rest, but sustained significant burn injuries and succumbed to his injuries about 6 days later. Had the pilot been wearing the fire-resistant clothing, shoes, and a helmet which were located in the airplane, it is likely that his burn injuries would have been much less severe. The airplane was a restored Soviet Union-designed military trainer, which had been modified with a larger radial engine and its associated systems as well as modern avionics. The previous owner of the airplane reported that, about 10 years earlier, he had experienced a fuel leak from one of the fuel pumps (though he could not remember which one). Examination of maintenance records indicated that, about 5 days before the accident, a mechanic had installed avionics and had fire-sleeved the oil and fuel hoses at the engine accessory case and those that were connected to the cockpit gauges. The metal and fabric fuselage skin in the areas of the cockpit, right wing, left wing root and forward portion of the empennage had been consumed by fire. The cockpit area was completely destroyed and displayed no evidence of fire blocking structure or materials. The remaining metallic skin on the outboard section of the right wing and empennage also exhibited extensive thermal damage, including melting, oxidation of aluminum surfaces, and brittleness. There was extensive fire damage on the aft inboard trailing edge of the right wing and adjacent areas. The right side of the fuel system engine feeder (sump) tank had multiple areas of melt-through on the upper surface. The wing structure outboard from the feeder tank was intact. The inboard edges showed signs of melting, sooting, and thermal discoloration of remaining paint. The tail section, engine cowling, and the left wing were intact. Based on this pattern of damage and witness reports, the fire originated in the right wing near the root of the wing, and not near the fuel pumps or the area where maintenance/alterations had been recently performed. Several sections of wiring were removed for examination from the area of the fire's origin, including the wiring associated with the recently-installed avionics. While the extensive fire damage precluded examination of the entirety of the airplane's wiring system, and it is possible that the ignition source was located in a different section of wiring; only the power wiring showed evidence of having power at the time of the fire. This wiring was routed in the area of the right wing root, and not near the recently-installed avionics. The power wiring showed signs of arcing, melting, and welding near a fractured end of the recovered section. Given its electrified state and location near the origin of the fire, it is likely that the power wiring was the initial source of ignition. Additionally, the power wiring's close proximity to the fuel feeder tank, fuel pump, fuel strainer, fuel shutoff valve unit, and all of their associated fuel lines allowed fuel to feed the fire and increased its intensity.
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
- Landing area overshoot during landing (flare/touchdown)
- Electrical system malf/failure during landing (landing roll) defining event
- Fire/smoke (non-impact) during landing (landing roll)
- Runway excursion during landing (landing roll)
- Part(s) separation from AC during landing (landing roll)
- Evacuation during after landing
The NTSB's findings
- cause Aircraft › Aircraft systems › Electrical power system › (general) › Malfunction
- cause Aircraft › Aircraft systems › Electrical power system › (general) › Failure
- cause Aircraft › Aircraft systems › Fuel system › (general) › Failure
- factor Aircraft › Aircraft systems › Electrical power system › Electrical pwr sys wiring › Design
- factor Aircraft › Aircraft systems › Fire protection system › (general) › Not installed/available
- factor Personnel issues › Action/decision › Action › Lack of action › Pilot
Pilot
- Certificate: commercial pilot
- Ratings: multi-engine land; single-engine land; instrument: airplane
- Flight time: 3,100 hours in all
- Last flight review: August 31, 2015
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: frt
- Injury: fatal
The aircraft
- Airframe total time: 318.5 hours
- Last inspection: condition inspection, August 28, 2015
- Maximum gross weight: 5,379 lb
- Seats: 2
- Landing gear: retractable
- Engine: P & W R-1830-75 (piston); 0 hours total
- Fire on the ground
The flight
- Departed from: MQS Coatesville PA at 12:30 pm
- Destination: AGC West Mifflin PA
- Flight plan: none
- Runway 28, 6,501 ft by 150 ft
Weather at the time
- Light: daylight
- Wind: at 5 knots
- Visibility: 6 statute miles
- Temperature: 82°F (28°C), dew point 73°F (23°C)
- Altimeter: 29.98 inHg
- Observation at 1:53 pm from AGC
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
11 documents, released by the NTSB on October 4, 2018. 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 | Witness Statements and Interview Summaries | PDF, 10 pages | View Download |
| 2 | Fuel Records | PDF, 4 pages | View Download |
| 3 | Excerpts from N5940 Maintenance Records | PDF, 7 pages | View Download |
| 4 | Weather Reports and Records - Kagc Metars and Tafs | PDF, 1 page | View Download |
| 5 | Air Traffic Control Recordings (Shelf Item) | PDF, 1 page | View Download |
| 6 | Photo Array | PDF, 18 pages | View Download |
| 7 | Airport Diagram - Kagc | PDF, 1 page | View Download |
| 8 | Satellite Images of Accident Area | PDF, 2 pages | View Download |
| 9 | Materials Laboratory Fire Factual Report | PDF, 17 pages | View Download |
| 10 | Security Camera Videos (Shelf Item) | PDF, 1 page | View Download |
| 11 | Wreckage Release and Evidence Control | PDF, 2 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.
