The Wm Wrigley Jr. Company of Chicago has a rare bird, one of only two Gulfstream G550s equipped with a second crew-rest area, divided from the remaining aft end of the cabin by a sound-damping lead curtain. The second crew-rest area was built and installed at Gulfstream’s Long Beach, Calif. completion center. The other aircraft with a second crew-rest area is operated by NetJets.
In response to a congressional inquiry, the Government Accountability Office (GAO) has determined that the NTSB Training Center near Washington Dulles International Airport should either be made more cost-effective or vacated.
Bell 206B-3 JetRanger, Shelbyville, Texas, March 10, 2005–The NTSB could not determine the reason for the loss of control and subsequent crash of the JetRanger and blamed the accident on the pilot’s failure to maintain altitude and clearance for undetermined reasons.
Cessna 208B Caravan, Portland, Ore., Dec. 24, 2005–The reason for the Caravan’s loss of power on takeoff has not been determined, said the NTSB. The pilot reported, “After becoming airborne, the airplane quit accelerating and a positive climb rate was not established.”
Aerospatiale SA 319B, Escalante, Utah, Dec. 14, 2005–The NTSB said the probable cause of the SA 319 accident was the pilot’s inadequate remedial action when the helicopter entered ground resonance. The rough/uneven terrain and inadequate company maintenance were contributing factors.
Bell 206L-3 LongRanger, Gulf of Mexico, Aug. 13, 2003–The NTSB said that the cause of the accident was the pilot’s inadequate compensation for crosswind conditions and failure to obtain and maintain directional control. The crosswind was a contributing factor, as was the pilot’s attempt to position the helicopter near the refueling station in a crosswind to perform a hot refueling.
Bell 407, Broadus, Texas, March 27, 2003–The NTSB said the probable cause of the 407 crash was “the partial loss of engine power due to erratic fuel flow metering to the engine resulting from the single-point failure of the PLA potentiometer in the hydro-mechanical fuel control unit.” A contributing factor was the lack of suitable terrain for a forced landing.
Raytheon Beech King Air 100, Pawtucket, R.I., Aug. 13, 2006–The NTSB said that the cause of the gear-collapse accident was the pilot’s misjudging distance and speed during final approach, which resulted in an undershoot and subsequent gear collapse. The 3,374-hour commercial pilot said that while landing on Runway 33 with a seven-knot wind at 300 degrees, the right main gear touched down about two feet before the runway.
Raytheon Beech King Air 200, Hondo, Texas, Sept. 5, 2006–The King Air had just been painted when the 18,500-hour ATP-rated pilot arrived to fly it back to home base. The airport at which it had been painted did not have jet-A, so he planned to fly to an airport 30 miles away to refuel. While taxiing out, he ran into a pothole, which was not visible because of standing rainwater. There was no notam warning about the damaged taxiway.
Aerospatiale AS 350B/Eurocopter EC 130B4, Homestead, Fla., Nov. 20, 2005–The Biscayne Helicopters AS 350B and the HelicopterShuttle.com EC 130 collided on approach to the Motorsports Complex VIP Heliport (Speedway Heliport) in Homestead. Weather was VMC and neither helicopter was on a flight plan. The commercial pilot of the EC 130 was killed; the commercial pilot of the AS 350 was not injured. Both helicopters were substantially damaged.