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Accidents · NTSB ERA11LA117 · Final report

Convair 340-71 accident near Charlotte Amalie, January 17, 2011

On January 17, 2011 at about 11:56 am local time, a Convair 340-71, registered N8277Q, was substantially damaged in an accident during takeoff near Charlotte Amalie (Cyril E. King Airport). It was a positioning flight under general aviation rules (Part 91). No one was hurt; 2 people were on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The captain’s decision to continue the flight with the left engine backfiring, resulting in an engine fire shortly after takeoff. Contributing to the accident were the captain’s decision to continue the flight following a report of black smoke trailing the airplane and in-flight fire damage to the left wheel brake system, resulting in a loss of directional control during an emergency landing.

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

What the record shows

Date
January 17, 2011 · about 11:56 am local time
Place
Charlotte Amalie · Cyril E. King Airport · map
Type
Accident
Injuries
No one was hurt; 2 people were on board or involved.
Weather
visual conditions (good weather)
Aircraft
Convair 340-71 · all 340-71s on the register
Registration
N8277Q · no longer on the register · serial 282
Damage
Substantial damage
Flight
Positioning flight · general aviation rules (Part 91)

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

Before departing on the flight that preceded the accident flight, the flight crew performed an engine-run, including a magneto check, during which they noted backfiring from the left engine. The captain first attributed the issue to water contamination of the fuel but then attributed it to fouled spark plugs. An additional engine run resulted in no further backfiring, and the captain decided to depart on the cargo flight; no maintenance was requested or performed on the left engine before departure. When the airplane was near the destination airport, the left engine backfired once again. The flight continued to the destination airport where the airplane landed uneventfully and the cargo was off loaded; again, no maintenance was performed or requested for the left engine. For the accident flight, the first officer was the pilot flying and the captain was the pilot monitoring. During the takeoff, the local controller noted black smoke trailing the left engine and advised the flight crew; however, the captain attributed the smoke to normal operation for the airplane type and decided to continue the flight. Meanwhile, air traffic control communications for the flight were transferred to San Juan Combined En Route Approach Control (San Juan CERAP). The local controller who noted the black smoke continued to watch the airplane’s departure. When the airplane was about 1 mile west of the runway, the controller observed bright orange then red flames from behind the left engine and immediately informed the San Juan CERAP controller, who in turn immediately notified the flight crew. The captain assumed control of the airplane and directed the first officer to go to the cabin to visually inspect the left engine. The first officer returned to the cockpit and informed the captain that he observed fire, and they immediately executed the fire checklist and shut down the left engine. However, the fire continued because it was located in an area where fire suppression bottles could not reach. The pilots returned to the airport; fire rescue vehicles were pre-positioned along various portions of the runway. The airplane touched down on the runway centerline. Because the fire had damaged the left brake line, braking was asymmetrical, and the airplane departed the right side of the runway and came to rest adjacent to the airport perimeter fence. Postaccident examination of the left engine revealed a discrepancy of two cylinders in which the pistons did not move during rotation of the engine. This discrepancy could result in unburned fuel or oil entering the exhaust system and igniting in the exhaust or augmentor tubes. Examination of the airframe found that the augmentor tubes had been removed after the accident. Although they were not available for examination, the location of the fire suggests that there was a leak in the vicinity of the augmentor tubes and muffler junction, causing the fire to burn through the nacelle rather than exit out the aft end of the muffler. The left engine was installed on the accident airplane in September 2009. At the time of the accident, it had accumulated about 1,004 hours since the last known major overhaul in 1975. Copies of the maintenance records for the left engine were requested but not provided; therefore, how often or whether the engine was maintained during the 34 years between the known last overhaul and when it was installed on the accident airplane could not be determined. A service check of the engines, including compression check of the cylinders, was last performed 5 days before the accident. The captain twice decided to depart without reporting or requesting maintenance for the backfiring of the left engine. If maintenance had been accomplished, it is likely that the lack of movement of the two cylinder pistons would have been detected and repaired, thereby preventing the engine fire. Because of the airplane’s distance from the airport at the time the flight crew received the local controller’s report about black smoke, it is unknown whether fire damage to the brake line would have been mitigated if the captain had decided to return to the airport immediately. However, the captain demonstrated poor judgment in deciding to continue the flight rather than immediately follow up on the report.

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. Aircraft maintenance event during prior to flight
  2. Powerplant sys/comp malf/fail during takeoff defining event
  3. Fire/smoke (non-impact) during takeoff
  4. Flight control sys malf/fail during maneuvering
  5. Sys/Comp malf/fail (non-power) during maneuvering
  6. Loss of control on ground during landing (landing roll)

The NTSB's findings

  • cause Personnel issues › Action/decision › Info processing/decision › Identification/recognition › Pilot
  • Aircraft › Aircraft power plant › Engine (reciprocating) › Recip eng cyl section › Failure
  • factor Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
  • factor Aircraft › Aircraft systems › Landing gear system › Brake › Damaged/degraded
  • factor Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Directional control › Attain/maintain not possible

Pilot

  • Certificate: airline transport pilot, flight instructor, commercial pilot
  • Ratings: multi-engine land; single-engine land; instructor: airplane single-engine; instrument: airplane
  • Flight time: 15,130 hours in all; 6,810 in this make and model; 120 in the last 90 days; 42 in the last 30 days; 10,090 as pilot in command
  • Last flight review: September 23, 2010
  • Medical certificate: Class 1 (without waivers/limitations)
  • Seat: left
  • Injury: no injuries

Co-pilot

  • Certificate: commercial pilot
  • Ratings: multi-engine land; single-engine land; instrument: airplane
  • Flight time: 9,828 hours in all; 237 in this make and model; 3,086 as pilot in command
  • Last flight review: June 28, 2010
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: rgt
  • Injury: no injuries

The aircraft

  • Airframe total time: 17,279 hours
  • Last inspection: approved inspection programme, January 12, 2011; 2 hours since
  • Maximum gross weight: 47,000 lb
  • Seats: 4
  • Landing gear: retractable
  • Engine: Pratt & Whitney R-2800 (piston); 0 hours total
  • Fire in flight and on the ground

The flight

  • Departed from: STT Charlotte Amalie at 11:47 am
  • Destination: SJU San Juan PR
  • Runway 10, 7,000 ft by 150 ft
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Wind: from 100° at 8 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 75°F (24°C), dew point 70°F (21°C)
  • Altimeter: 30.01 inHg
  • Observation at 11:53 am from STT

Injuries

FatalSeriousMinorNone
Flight crew2

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.