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Accidents · NTSB CEN17LA033 · Final report

North American TB 25N accident near Dallas, Texas, October 29, 2016

On October 29, 2016 at about 8:40 pm local time, a 1943 North American TB 25N, registered N25YR, was substantially damaged in an accident during maneuvering near Dallas, Texas (Dallas Executive airport). It was an air show or air race flight under general aviation rules (Part 91). No one was hurt; 9 people were on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The overstress failure of the landing gear connecting rod and the improper installation of the arresting cables, which allowed the landing gear door to depart in flight and impact the airplane.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
October 29, 2016 · about 8:40 pm local time
Place
Dallas, Texas · Dallas Executive · map
Type
Accident
Injuries
No one was hurt; 9 people were on board or involved.
Weather
visual conditions (good weather)
Aircraft
North American TB 25N, built 1943 · all TB 25Ns on the register
Registration
N25YR · registry record · serial 43-27868
Damage
Substantial damage
Flight
Air show or air race flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The airline transport pilot reported that the twin-engine, historic airplane was flying about 155 mph and 1,000 ft above ground level. Upon entering the left downwind leg of the airport traffic pattern, the pilot extended the landing gear. While the gear was in transit, the crew felt a jolt, as if a bird had impacted the front of the airplane. The pilot made a normal landing, parked the airplane, and noted damage to the left horizontal stabilizer and elevator. A crew from another airplane reported to the pilot that they observed an object depart the accident airplane during landing gear extension. A postaccident examination revealed that the left inboard landing gear door separated in flight and impacted the engine nacelle, left horizontal stabilizer, and elevator. The landing gear door was later found in a residential neighborhood about one mile north of the airport. The gear door was equipped with two arresting cables that were intended to prevent the door from hyperextending. The arresting cables were not installed in the correct position, and the investigation could not determine how long the arresting cables had been incorrectly installed. The landing gear door connecting rod was bent and fractured into two pieces at the safety wire drill hole. The fractured connecting rod was consistent with an overstress failure in bending. If the arresting cables had been installed correctly, it is likely that the landing gear door would not have separated from the airplane when the connecting rod failed.

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

  1. Part(s) separation from AC during maneuvering defining event

The NTSB's findings

  • cause Aircraft › Aircraft systems › Landing gear system › Landing gear door retract sec › Failure
  • cause Aircraft › Aircraft systems › Landing gear system › Landing gear door retract sec › Incorrect service/maintenance

Pilot

  • Certificate: airline transport pilot, flight instructor, flight engineer
  • Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane; rotorcraft: glider
  • Flight time: 22,000 hours in all; 150 in this make and model; 220 in the last 90 days; 75 in the last 30 days; 19,000 as pilot in command
  • Medical certificate: Class 1 (without waivers/limitations)
  • Seat: left
  • Injury: no injuries

Co-pilot

  • Certificate: airline transport pilot, flight instructor, flight engineer
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: rgt
  • Injury: no injuries

The aircraft

  • Airframe total time: 5,231.7 hours
  • Last inspection: condition inspection, February 12, 2016
  • Maximum gross weight: 24,000 lb
  • Seats: 10
  • Landing gear: retractable
  • Engine 1: Curtiss-Wright Cyclone (piston); 0 hours total
  • Engine 2: Curtiss-Wright Cyclone (piston); 0 hours total
  • Operator: Commemoative Air Force

The flight

  • Departed from: RBD Dallas TX at 8:00 pm
  • Destination: RBD Dallas TX
  • Flight plan: none
  • Runway 13, 6,451 ft by 100 ft
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Wind: from 170° at 7 knots, gusting 16
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 82°F (28°C), dew point 57°F (14°C)
  • Altimeter: 30.04 inHg
  • Observation at 8:53 pm from KRBD

Injuries

FatalSeriousMinorNone
Flight crew2
Passengers7

Documents from the investigation the NTSB's docket: the evidence folder behind the report

7 documents, released by the NTSB on July 17, 2017. 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.

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.