Beech C90A accident near Roanoke, Virginia, November 20, 2012
On November 20, 2012 at about 3:30 pm local time, a 1990 Beech C90A, registered N702DK, was substantially damaged in an accident during approach near Roanoke, Virginia (Roanoke Regional Airport). It was flown under charter and air-taxi rules (Part 135). No one was hurt; 4 people were on board or involved. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The failure of the right main landing gear bearing actuator support brackets. Contributing to the accident was the owner's and operator's failure to comply with the airplane manufacturer's mandatory service bulletin and the Federal Aviation Administration's failure to issue an airworthiness directive.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- November 20, 2012 · about 3:30 pm local time
- Place
- Roanoke, Virginia · Roanoke Regional Airport · map
- Type
- Accident
- Injuries
- No one was hurt; 4 people were on board or involved.
- Weather
- visual conditions (good weather)
- Aircraft
- Beech C90A, built 1990 · all C90As on the register
- Registration
- N702DK · no longer on the register · serial LJ-1259
- Damage
- Substantial damage
- Flight
- Flight · charter and air-taxi rules (Part 135)
The NTSB's narrative final · quoted from the NTSB record
During the downwind leg of the traffic pattern at the destination airport, the pilots lowered the landing gear. The pilot then noticed that the right main landing gear (MLG) was not down and locked in position for landing. The flight crew made multiple attempts to get a down-and-locked indication without success, so the pilot decided to abort the landing and divert to another airport with longer runways. After executing the manual gear extension checklist, the flight crew made a low pass at the diversion airport, and the air traffic controller in the control tower advised that the landing gear appeared to be in the down position. During the landing, the touchdown was normal, and the airplane slowed normally; however, as the airplane exited the runway, the right MLG collapsed. Examination of the wreckage revealed that the right wing, right nacelle, and right wheel well had received substantial damage and that the right MLG, after collapsing, had punctured the right nacelle fuel tank. The right MLG bearing actuator support bracket was made of aluminum. Examination of the right MLG revealed that the right MLG bearing actuator support bracket was broken and had separated from its mounting position. Multiple cracks in the bracket were visible, and, at the microscopic level, the cracks had shiny surfaces indicative of abrasion, and overload regions with a cloudy appearance. Essentially, with each cycle, whether it was with extension of the landing gear, retraction of the landing gear, or landing itself, the cracks were subjected to loading which caused them to continue to propagate until the entire assembly reached a point at which structural integrity was no longer present to hold the landing gear actuator. In December 2003, the airplane manufacturer issued a mandatory service bulletin to replace the right and left aluminum MLG bearing actuator support brackets with steel brackets and specified that the replacement of the brackets be accomplished "as soon as possible," but "no later than the next scheduled inspection, the next 200 flight hours or 24 months." The airplane manufacturer also requested that the Federal Aviation Administration (FAA) issue an Airworthiness Directive (AD) based on the service bulletin. However, the FAA did not find an "unsafe condition" and did not issue an AD, which would have made compliance with the service bulleting mandatory. Review of the airplane's maintenance records confirmed that the airplane owner and the operator had not had the new steel brackets installed. Further, the FAA has not issued an AD for the MLG bearing actuator support brackets.
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
- Aircraft maintenance event during prior to flight
- Aircraft structural failure during approach
- Sys/Comp malf/fail (non-power) during approach defining event
- Landing gear collapse during landing (landing roll)
The NTSB's findings
- factor Organizational issues › Development › Design › Policy/procedure development › FAA/Regulator
- factor Personnel issues › Action/decision › Action › Lack of action › Owner/builder
- factor Personnel issues › Task performance › Maintenance › Replacement › Maintenance personnel
- factor Aircraft › Aircraft systems › Landing gear system › Main landing gear attach sec › Not installed/available
- cause Aircraft › Aircraft systems › Landing gear system › Main landing gear attach sec › Failure
Pilot
- Certificate: airline transport pilot, flight instructor, commercial pilot
- Ratings: multi-engine land; single-engine land; instructor: airplane single-engine; instrument: airplane
- Flight time: 2,520 hours in all; 210 in this make and model; 75 in the last 90 days; 35 in the last 30 days; 1,700 as pilot in command; 1,090 on instruments
- Last flight review: July 27, 2012
- Medical certificate: Class 1 (without waivers/limitations)
- Seat: rgt
- Injury: no injuries
Co-pilot
- Certificate: airline transport pilot, flight instructor, commercial pilot
- Ratings: multi-engine land; single-engine land; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
- Flight time: 4,783 hours in all; 2,664 in this make and model; 49 in the last 90 days; 17 in the last 30 days; 4,655 as pilot in command; 1,301 on instruments
- Last flight review: October 1, 2012
- Medical certificate: Class 1 (with waivers/limitations)
- Seat: left
- Injury: no injuries
The aircraft
- Airframe total time: 5,086 hours
- Last inspection: approved inspection programme, March 29, 2012
- Maximum gross weight: 12,000 lb
- Seats: 6
- Landing gear: retractable
- Engine 1: P&W Canada PT6-21 (turboprop); 5,019 hours total
- Engine 2: P&W Canada PT6-21 (turboprop); 5,029 hours total
- Operator: Dominion Aviation Services INC
The flight
- Departed from: FCI Richmond VA at 2:23 pm
- Destination: BCB Blacksburg VA
- Flight plan: IFR
- Runway 34, 5,810 ft by 150 ft
- A second pilot was aboard
Weather at the time
- Light: daylight
- Wind: at 0 knots
- Visibility: 10 statute miles
- Sky: a few clouds at 11,000 ft
- Temperature: 46°F (8°C), dew point 37°F (3°C)
- Altimeter: 30.19 inHg
- Observation at 3:54 pm from ROA
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 2 | |||
| Passengers | 2 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.
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.
