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Accidents · NTSB LAX94LA030 · Final report

Beech 200 accident near Reno, Nevada, October 28, 1993

On October 28, 1993 at about 6:15 am local time, a Beech 200, registered N191FL, was substantially damaged in an accident near Reno, Nevada (Reno Cannon Intl airport). It was a personal flight under general aviation rules (Part 91). No one was hurt; 5 people were on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

THE IMPROPER OVERHAUL OF THE RIGHT MAIN LANDING GEAR ACTUATOR BY MAINTENANCE PERSONNEL, AND THE OPERATOR'S FAILURE TO ASSURE THAT THE AIRPLANE MANUFACTURER'S MANDATORY SERVICE BULLETIN REQUIRING MODIFICATION OF THE GEAR MOTOR CIRCUIT PROTECTION WAS ACCOMPLISHED.

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

What the record shows

Date
October 28, 1993 · about 6:15 am local time
Place
Reno, Nevada · Reno Cannon Intl · map
Type
Accident
Injuries
No one was hurt; 5 people were on board or involved.
Weather
visual conditions (good weather)
Aircraft
Beech 200 · all 200s on the register
Registration
N191FL · registry record · serial BB-107
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

AFTER MOVING THE LANDING GEAR HANDLE TO THE UP POSITION, THE COCKPIT BEGAN FILLING WITH SMOKE. THE PILOT NOTICED THAT THE GEAR APPEARED TO BE HUNG IN AN INTRANSIT POSITION. THE SMOKE, WHICH SMELLED OF BURNING ELECTRICAL INSULATION, BECAME HEAVIER, AND HEAT COULD BE FELT ON THE COCKPIT FLOOR.THE PILOT RETURNED TO THE AIRPORT, AND THE GEAR COLLAPSED DURING LANDING. EXAMINATION REVEALED THAT THE LANDING GEAR MOTOR AND ASSOCIATED WIRING WERE BURNED, AND THE COCKPIT FLOORING APPEARED TO BE PARTIALLY MELTED. THE RIGHT LANDING GEAR ACTUATOR WAS FOUND TO HAVE BEEN IMPROPERLY OVERHAULED, WHICH RESULTED IN THREE GEAR TEETH BREAKING AND JAMMING THE ACTUATOR. BEECH MANDATORY SERVICE BULLETIN NO. 2035, REV. II, REQUIRING REPLACEMENT OF THE 200-AMP GEAR MOTOR CIRCUIT BREAKER WITH A 60-AMP BREAKER TO PREVENT GEAR MOTOR DAMAGE, WAS NOT ACCOMPLISHED ON THIS AIRPLANE.

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

Pilot

  • Certificate: private
  • Ratings: multi-engine land; single-engine land
  • Flight time: 1,000 hours in all; 23 in this make and model; 60 in the last 90 days
  • Medical certificate: Class 3 (valid medical--no waivers/lim.)
  • Seat: left

The aircraft

  • Airframe total time: 6,420 hours
  • Last inspection: approved inspection programme, September 16, 1993; 12 hours since
  • Maximum gross weight: 12,500 lb
  • Seats: 8
  • Landing gear: retractable
  • Engine: P&W PT6A-42 (turboprop); 0 hours total

The flight

  • Departed from: RNO at 6:13 am
  • Destination: SQL San Carlos CA
  • Flight plan: none
  • Runway 25, 6,101 ft by 150 ft

Weather at the time

  • Light: night, dark
  • Wind: from 250° at 3 knots
  • Visibility: 20 statute miles
  • Sky: clear
  • Temperature: 43°F (6°C), dew point 0°F (-18°C)

Injuries

FatalSeriousMinorNone
Crew1
Passengers4

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.