Primary finding
Probable cause
The pilot-in-command's failure to obtain the proper touchdown point or landing reference speed and failure to initiate a go-around when it became evident that the airplane was landing long and fast. Contributing to the incident was a lack of effective flight crew coordination and communication.
Investigator assessment
Analysis narrative
The airplane was approaching the destination airport in night visual meteorological conditions. The pilot-in-command (PIC) was the pilot flying and was not familiar with the destination airport. The second-in-command (SIC) was the pilot monitoring and was familiar with the destination airport. While the airplane was at 2,000 feet mean sea level, about 10 miles from the airport, the PIC did not see the airport; however, the SIC observed the airport beacon, but not runway 33R. The controller then offered either a clearance for a visual approach to runway 33R or a vector for the runway 33R instrument landing system (ILS) approach. The PIC indicated to the SIC that he wanted the ILS; however, the SIC stated that he saw runway 33R and asked the PIC if he saw it, to which he replied no. The SIC then told the controller that they had the runway in sight. The PIC subsequently stated to the SIC that he saw runway 33R, but he confused it with runway 28. About 2 minutes later, with the SIC assisting, the PIC visually acquired the correct runway. At that time, the airplane was about 6 miles from the runway, at 1,400 feet msl. The airplane made a left turn, followed by a right turn, which positioned it from a final approach to runway 28, to a final approach to runway 33R. The airplane was lined-up for runway 33R about 4 miles from the runway threshold, at 1,000 feet and 145 knots groundspeed. While on short final approach, about 300 feet agl, the airspeed went below the landing reference speed (Vref) by about 3 to 5 knots. The SIC responded by emphasizing "below Vref" two times, followed by "power" four times. The PIC added power and the airplane's speed went above Vref by about 10 knots. The airplane touched down about halfway down the 5,000 foot-long runway, about 140 knots groundspeed with an approximate 5-knot tailwind. Although the flight crew did not believe the thrust reversers activated, non-volatile memory (NVM) of the engine controls revealed that they deployed for 13 seconds; however, the airplane still traveled off the end of the runway and came to rest in mud about 200 feet from the departure end. Examination of the airplane and its other NVM did not reveal any preimpact mechanical malfunctions. The flight crew did not report any additional anomalies, including the breaking system, and 226 feet of pulsing skid marks were identified near the departure end of the runway.
Source record
Factual narrative
HISTORY OF FLIGHT On January 30, 2012, at 1843 eastern standard time, a Gulfstream G150, N272CB, operated by Chattem Inc., sustained minor damage during a landing overrun at Baltimore Washington International Airport (BWI), Baltimore, Maryland. The two certificated airline transport pilots were not injured. The corporate repositioning flight was conducted under the provisions of 14 Code of Federal Regulations Part 91. Night visual meteorological conditions prevailed and an instrument flight rules flight plan was filed for the flight that departed from Pocono Mountains Municipal Airport (MPO), Mount Pocono, Pennsylvania, at 1808. According to their written statements, the pilot-in-command (PIC) was the pilot flying and the second-in-command (SIC) was the pilot monitoring. The PIC stated that they obtained the current BWI automated terminal information system (ATIS) report, which stated that visual approaches were being conducted to runways 33L and 33R. The flight crew reported the airport in sight to Baltimore Approach and were cleared for a visual approach to runway 33R. While established on the approach, the PIC viewed the precision approach path indicator and listened to the enhanced ground proximity warning system (EGPWS) report altitudes. He adjusted engine power to remain on glideslope and recalled that the airspeed was about 5 or 6 knots above the landing reference speed (Vref) of 129 knots. The PIC continued with engine power and attitude adjustments. He then proceeded with a routine landing on the main landing gear. As the PIC lowered the nosegear he raised the thrust reverser handles; however, there was no feeling of deceleration or sound of engine power change. While maintaining directional control and braking with rudder pedals, the PIC reached again with both hands to initiate thrust reverser controls, but the thrust reversers did not respond. He stated to the SIC that the thrust reversers did not deploy and continued with heavy braking as the airplane traveled off the end of the 5,000-foot runway. The SIC added that during the approach, he saw the airport beacon and then the runway 33R lights. At that time, the flight was cleared by air traffic control (ATC) for a visual approach. The PIC initially mistook runway 28 for runway 33R, but the SIC used a chart on the multifunction display to assist the PIC in orienting to the correct runway. The SIC then noticed that the airplane was "a little slow" on final approach, and advised the PIC to watch the speed. The PIC then proceeded to correct the airspeed and it went "somewhat above" Vref. The SIC added that when the airplane touched down, he was concerned (about the runway length remaining) and the PIC appeared to be struggling to activate the thrust reversers. Toward the end of the runway, the SIC assisted the PIC with braking; however, the airplane overran the runway and came to rest in mud. PERSONNEL INFORMATION The PIC, age 61, held an airline transport pilot certificate, with ratings for airplane single-engine land and airplane multiengine land. He held a commercial pilot certificate, with a rating for airplane single-engine sea. He also held a mechanic certificate, flight instructor certificate, and type ratings in the Gulfstream 150 and Cessna 650. His most recent Federal Aviation Administration (FAA) first-class medical certificate was issued on February 16, 2011. The PIC reported a total flight experience of 12,604 hours; of which 109 hours were in the same make and model as the incident airplane. He flew 58 hours and 31 hours in the Gulfstream 150 during the 90-day and 30-day periods preceding the incident, respectively. The SIC, age 49, held an airline transport pilot certificate, with a rating for airplane multiengine land. He held a commercial pilot certificate, with a rating for airplane single-engine land. He also held type ratings in the Boeing 737, Cessna 650, and Gulfstream 150. The SIC's most recent FAA first-class medical certificate was issued on July 11, 2011. The SIC reported a total flight experience of 13,633 hours; of which, 120 hours were in the same make and model as the incident airplane. He flew 60 hours and 31 hours in the Gulfstream 150 during the 90-day and 30-day periods preceding the incident, respectively. AIRCRAFT INFORMATION The 9-seat airplane, serial number 0262, was manufactured in 2008. It was powered by two Honeywell TFE 731-40AR-200G engines, each capable of generating 4,250 pounds of thrust. The airplane was maintained under a manufacturer's approved inspection program. The airplane's most recent inspection was completed July 18, 2011. At the time of the incident, the airframe and engines had accrued 494 total hours of operation. METEOROLOGICAL INFORMATION The airport elevation at BWI was 146 feet. The recorded weather at BWI, at 1850, was: wind from 140 degrees at 4 knots; visibility 10 miles; few clouds at 10,000 feet; broken ceiling at 25,000 feet; temperature 4 degrees C; dew point minus 11 degrees C; altimeter 30.30 inches Hg. According to the U.S. Naval Observatory, Sun and Moon Data, sunset occurred at 1724 and the end of civil twilight at 1753. FLIGHT RECORDERS A cockpit voice recorder (CVR), EGPWS, anti-skid computer, maintenance diagnostic computer (MDC), and two digital electronic engine control systems (DEECs) were retained by the NTSB and forwarded to the NTSB Vehicle Recorders Laboratory, Washington, D.C., for data download. CVR A CVR Group was convened at the NTSB Vehicle Recorders Laboratory, Washington, D.C. Data was successfully downloaded and a transcript was prepared of approximately the last 22 minutes of the recording. At 1828, the airplane was at 12,000 feet mean sea level (msl) and the flight crew was in radio contact with Baltimore Approach. The SIC advised the controller that he had ATIS information victor. The controller instructed the flight to expect a visual approach to runway 33L, which the SIC acknowledged. At 1830, the SIC requested runway 33R, which the controller acknowledged and advised the flight to descend to 4,000 feet. At 1832, the SIC noted that they were 27 miles from the airport. At 1833, Potomac Approach instructed the flight to proceed direct BWI and maintain 3,000 feet, which the SIC acknowledged. At 1836, while receiving descent vectors, the controller instructed the flight to descend to 2,000 feet, which the SIC acknowledged. The SIC also selected the ORIOL intersection on the flight management system. At 1838, when the airplane was at 2,000 feet, the controller advised that the airport was at 2 o'clock and 10 miles. The PIC remarked to the SIC that he did not see it and was unfamiliar with the airport. The SIC reported to the controller that they saw the airport beacon, but had not yet seen the runway. The controller then offered either a clearance for a visual approach to runway 33R, a vector for the runway 33R instrument landing system approach, or a different approach. The PIC stated yes to the SIC; however, the SIC stated that he saw the runway and asked the PIC if he saw it, which he replied no. The SIC then told the controller that they had the runway in sight and the PIC subsequently told the SIC he now saw it. The controller cleared the flight for a visual approach to runway 33R, with an instruction to switch to the tower radio frequency, which the SIC acknowledged. At 1839, the tower controller cleared the flight to land on runway 33R and provided wind information, which was from 160 degrees at 5 knots. The PIC asked the SIC if what he saw was the runway. The PIC added that he was not looking at the correct runway. The SIC then acknowledged the landing clearance to air traffic control and continued to assist the PIC in visually acquiring runway 33R. At 1840, the PIC stated to the SIC that he saw the correct runway. He asked him for 20-degrees of flap extension, to extend the landing gear, and to remove the