N8277Q

HISTORY OF FLIGHT

On January 17, 2011, about 0756 Atlantic standard time, a Convair 340-71, N8277Q, registered to Kestrel, Inc., operated by Tiger Contract Cargo, experienced an in-flight fire aft of the left engine shortly after takeoff from Cyril E. King Airport (STT), St. Thomas, U.S.V.I. Visual meteorological conditions prevailed at the time and a VFR flight plan was filed for the 14 Code of Federal Regulations (CFR) Part 91 positioning flight from STT to Luis Munoz Marin International Airport (SJU), San Juan, PR. The airplane sustained substantial damage and the airline transport pilot and commercial co-pilot were not injured. The flight originated from STT about 0747.

The transcription of communication indicates that the flightcrew established contact with ground control requesting runway 28 and advised the ground controller they were VFR to SJU. The controller cleared the flightcrew to taxi to runway 28, and at 0746:54, the controller cleared the flight for takeoff, which was acknowledged at 0747:05, by a comment from the flightcrew that the flight was, “…rolling runway two eight….” The co-pilot (pilot flying) later stated that after becoming airborne and positive rate of climb was established the call was made to retract the landing gear. The transcription of communications indicates at 0748:44, the local controller advised the flightcrew, “convair seven seven quebec observe a lot of smoke coming from your left engine are you in need of any assistance sir”, to which the captain (pilot not flying) stated, “ah no we are fine….” The co-pilot later stated that the captain attributed the smoke trailing from the left engine due to the age of the airplane. The flight continued and the captain later reported that after being notified of smoke coming from the left engine, he decided to send the co-pilot to visually inspect the left engine.

The flight continued and at 0749:04, air traffic control (ATC) communications were transferred to San Juan Combined En Route Approach Control (San Juan CERAP), which was acknowledged by the flightcrew. The controller who had cleared the flight for takeoff and switched ATC communications to San Juan CERAP reported that after doing so when the flight was 1 mile west of the departure end of runway 28, observed flames coming from the rear of the left engine. The controller later stated that the smoke first observed was black in color and the flames observed were bright orange and then red in color.

At 0749:20, the flightcrew attempted to establish contact with San Juan CERAP, but that communication was not acknowledged by the controller. The transcription of communications indicates that at 0749:30, the local controller from STT established contact with San Juan CERAP and asked if the flightcrew of the accident airplane had established contact yet, to which the controller said no. At 0750:04, the flightcrew established contact with San Juan CERAP, and 4 seconds later the local controller informed the San Juan CERAP controller of seeing flames from behind the left engine which was immediately broadcast to the flightcrew, and acknowledged by, “okay eleven.”

After being notified of the fire, the co-pilot reported they checked the engine instruments and did not have any indication of a fire. About that time the owner of the company who was airborne in another airplane told them they needed to return. The captain ordered the co-pilot to go into the cabin to visually look at the left engine and after returning to the cockpit informed the captain there was a fire. The captain advised that he executed the procedures for fire checklist and secured the left engine but the fire continued. The flight returned for landing at STT, and at 0750:50, the pilot of a company airplane reported, “…you definitely have a fire going.”

The flight continued towards STT and ATC communications were transferred to STT ATCT. At 0753:21, the flight was cleared to land and 15 seconds later the STT local controller advised the San Juan CERAP controller that the fire rescue vehicles were already positioned and standing by. The captain later reported that while returning to STT, he noticed an issue with the left aileron which the co-pilot assisted with. The airplane was landed on runway centerline at 90 knots, but the flightcrew were unable to stop the airplane. The captain also reported that there was no steering, the brakes were not working properly. During the landing roll the airport fire rescue vehicles followed the airplane while attempting to extinguish the fire and avoiding debris that was separating from the airplane. The airplane departed the right side of the runway, crossed a taxiway and a perimeter road, then went thru the airport perimeter fence and came to rest upright with the nose section over a public road outside of the airport property.

After the airplane came to rest, the flightcrew exited the airplane from the overwing exits, and the fire rescue vehicles converged on the airplane and extinguished the fire reporting it was extinguished “within seconds.” The ARFF personnel removed the flightcrew to safety, and immediately secured area until law enforcement support arrived.

PERSONNEL INFORMATION

The captain, age 42, holds airline transport, commercial, certified flight instructor, and mechanic certificates. At the airline transport pilot certificate level, he has airplane multi-engine land rating with type ratings in Convair 240, 340, 440, A340, and A440 airplanes. At the commercial level, he has airplane single-engine land category and class rating, and on the flight instructor certificate he has airplane single engine rating. He has airframe and powerplant ratings on his mechanic certificate, and also holds inspection authorization first issued January 24, 2005. He was issued a first class medical certificate with no restrictions or limitations on April 20, 2010.

On the National Transportation Safety Board (NTSB) Pilot/Operator Aircraft submitted by the operator, the captain was reported having 15,130 hours total time, and 6,810 hours total time in the accident make and model airplane, of which 4,150 were as pilot-in-command. In the previous 90 days, he reported 120 hours total time, of which 35 were in the accident make and model airplane, and in the previous 30 days, he reported 42 hours total time of which 11 were in the accident make and model airplane. In the previous 24 hours, he reported 3 hours total time. His last flight review or equivalent including federal air regulation (FAR) 121 or 135 checks was performed on September 23, 2010. The flight review was performed in a Convair C131F airplane.

The co-pilot, age, 66, holds a commercial pilot certificate with airplane single and multi-engine land, instrument airplane ratings. On the commercial pilot certificate he had type ratings in Convair 240, 340, 440, and Douglas DC-3 airplanes; the type ratings were for second-in-command (SIC) only. He was issued a second class medical certificate with a restriction to wear corrective lenses on October 26, 2010.

On the National Transportation Safety Board (NTSB) Pilot/Operator Aircraft submitted by the operator, the co-pilot was reported having 9,828 hours total time, and 237 hours total time in the accident make and model airplane none of which were logged as pilot-in-command. In the previous 90 days, he reported 90 hours total time in the accident make and model airplane, and in the previous 30 days, he reported 30 hours total time in the accident make and model airplane. In the previous 24 hours, he did not report any flight time. His last flight review or equivalent including federal air regulation (FAR) 121 or 135 checks was performed on June 28, 2010. The flight review was performed in a Convair “340/440” airplane.

AIRCRAFT INFORMATION

The airplane was manufactured in 1955, and was removed from military service where it was designated as a C-131F/R4Y-1, which is a military cargo version of the Model 340. Military records were not available for inspection.

In September 1995, the airplane was presented to the FAA Manufacturing Inspection Satellite Office prior to the issuance of a Standard Transport Category Certificate of Airworthiness. During the conformity inspection to the airplane Type Certificate Data Sheet, non-conformance items were noted. In December 1999, a Transport Category Airworthiness Certificate was issued to the Convair 340-71 airplane, manufacturer serial number 282.

The Convair 340-71 airplane is an all-metal, low-wing, pressurized, twin-engine, propeller-driven airplane powered by two 18 cylinder Pratt & Whitney R-2800 engines.

The engines and nacelles are installed on the wings centered at about wing inch station (WIS) 150 and wing bulkhead station (WBS) 7. The nacelles are permanently attached to the wing and consist of three main portions; the power section, the nacelle body section, and the nacelle afterbody section.

The engine exhaust from the 18 cylinders is routed to two manifold assemblies. Each manifold assembly consists of 8 Siamese stacks, 2 single stacks, and 9 port extensions. The Siamese stacks receive the exhaust gases from two cylinders and the single stacks receive the exhaust gas from one cylinder. Each manifold, thus, carries the exhaust gases from 9 cylinders to the augmentor bellmouth located in the upper firewall. The thrust augmentor assemblies extend from the engine firewall aft to the exhaust transition assembly and muffler. They are situated within the nacelle body section above the upper wing skin and are mounted through shock mounts to the upper nacelle body section frames. The cross-sectional area of the augmentor ducts is considerably larger than the total cross-sectional area of the exhaust stacks in the manifold assembly at the bellmouth. This difference in area and the high speed of the exhaust gases entering the augmentors causes a pressure decrease which draws more air through the cowling to provide cooling. The augmentor...