Ferry

After a flight from Dallas-Addison, the crew made two stops at Palm Coast, Florida, and Goldsboro, North Carolina, before returning to his base at Washington-Warren Field. After landing on runway 23, the airplane suffered a runway excursion and came to a halt, bursting into flames. Both crew members evacuated safely while the airplane was partially destroyed by fire.

A Piper PA-31 Navajo operated by Airborne Energy Solutions Inc. was conducting a round robin instrument flight rules flight from Calgary International Airport (CYYC), AB, to Hinton/Entrance Aerodrome (CEE4), AB, and back to CYYC with only the pilot on board. The plan was to conduct the flight without refueling in CEE4. Prior to departure from CEE4, the pilot determined there was sufficient fuel for the return flight to CYYC. While in cruise, with the left engine being supplied by the left outboard tank, the pilot observed the left engine fuel pressure start to fluctuate, and the engine operation became erratic. The pilot then selected the left engine to run on the left inboard fuel tank. Concerned about the fuel quantity in the left-wing fuel tanks, the pilot elected to cross feed the left engine from the right-side fuel system. During the final approach into CYYC the right engine stopped running. The pilot secured the right engine, feathered the propeller, declared a Mayday with ATS and elected to continue the approach. Two to three minutes later, the left engine stopped operating, and the pilot proceeded to perform a forced approach onto a golf course located directly south of the approach end for Runway 35R. The aircraft came to a rest approximately 1/2 nm south of the threshold for Runway 35R. The pilot received minor injuries; however, the aircraft was substantially damaged. There was no post-accident fire. On site post-accident examination of the aircraft found the left-hand fuel selector in the outboard position, the right-hand fuel selector in the off position and the cross-feed valve in the off (normal) position. The aircraft was subsequently removed from the golf course and transported to a secure location for further investigation. The investigation found that there was no fuel remaining in the left inboard, left outboard and left nacelle fuel tanks. The right nacelle tank was empty, however approximately 24 USG were recovered from the right inboard, and approximately 29 USG were recovered from the right outboard fuel tanks.

The airplane departed Dunkirk-Chautauqua County Airport, State of New York, on a ferry flight to Fort-Lauderdale-Executive Airport, carrying a crew of two. After he reached the altitude of 10,000 feet, the crew reported technical problems with the onboard electric system and elected to divert to Jamestown-Chautauqua County Airport. On final approach to runway 25, at an airspeed of 157 knots and with a rate of descent of 1,000 feet per minute, the airplane impacted the ground at runway threshold and went out of control. It caught fire, veered off runway to the left and came to rest in a grassy area, bursting into flames. Both crew members were rescued with various injuries. The airplane was totally destroyed by fire.

The airplane departed Kathmandu-Tribhuvan Airport at 1111LT, carrying technical engineers and staff of the airline. The airplane was ferried to Pokhara to proceed with a C-check maintenance program. Less than two minutes after takeoff from runway 02, the crew encountered an unexpected situation when the airplane rolled to the right, went to an almost vertical attitude before it crashed 200 meters to the right of the runway centerline, bursting into flames. The captain was seriously injured while 18 other occupants were killed.

The airplane departed Lukhovitsy-Tretyakovo Airport at 1452LT on a ferry flight to Moscow-Vnukovo Airport, carrying a crew of three. About eight minutes after takeoff, it entered an uncontrolled descent and crashed in an almost vertical attitude in a dense wooded area located near the village of Bokovo-Akulovo, some 37 km northwest of Tretyakovo Airport. The airplane disintegrated on impact and all three crew members were killed. The airplane was ferried back to Moscow following a maintenance program at Tretyakovo Airport.

The pilot departed runway 19 at Albany International Airport on a ferry flight to Montreal. After takeoff, while climbing, the pilot informed ATC about engine trouble and was able to climb to an altitude of about 800 feet when the airplane entered a left descending turn. It later gained a little altitude then entered an uncontrolled descent and crashed in a residential area, bursting into flames. The airplane was destroyed and the pilot, sole on board, was killed. The airplane was en route to Montreal-Pierre Elliott Trudeau International Airport.

The twin engine airplane departed Sunshine Coast-Caloundra Airport at 0733LT on a flight to Pago Pago, US Samoa, with two people on board. About 45 minutes into the flight, while cruising at an approximate altitude of 12,000 feet, the pilot inform ATC about an engine failure and elected to return to Sunshine Coast. He made a 180 turn and reduced his altitude. About 45 minutes later, unable to reach his departure airport, the pilot ditched the airplane some 30 nautical miles east of Sunshine Coast. Both occupants found refuge in a dinghy and were quickly rescued. The airplane sank and was lost.

On August 21, 2023, about 1315 central daylight time, an Israel Aircraft Industries 1125 Westwind Astra airplane, N39TT, sustained substantial damage when it was involved in an accident near Wheeling, Illinois. The pilot and co-pilot were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 positioning flight. According to the flight crew, they were cleared to land on runway 16 at Chicago Executive Airport, Wheeling, Illinois, and the airplane touched down within the touchdown zone. The pilot applied the brakes and deployed the thrust reversers. The pilot applied additional brake pressure and “found they were not grabbing.” The pilot released the brakes and reapplied brake pressure with no effect and advised the co-pilot he had no brakes. The co-pilot applied his brakes with no effect. The pilot selected the emergency brake handle and applied emergency braking. The pilot reported the emergency braking produced some slowing, and with the airplane’s nose wheel tiller, he attempted a right turn to exit the runway onto the 45° taxiway D, which he thought provided additional stopping distance. Due to the airplane’s energy and momentum, the airplane slid off the taxiway and into the adjacent grass. The airplane’s right main landing gear collapsed, and the airplane came to rest upright.

The airplane departed Santa Rosa-Sonoma County Airport on a ferry flight to Honolulu, carrying two pilots. It crashed in unknown circumstances into the Pacific Ocean some 54 km west of Half Moon Bay. No trace of the aircraft or the crew was found.

The pilot was taking the airplane on a flight to another airport for maintenance. During the preflight inspection, the pilot turned on the electrical power and noticed that the fuel gauge was indicating 80 gallons of fuel. The pilot reported the airplane holds a maximum of 156 gallons of fuel and he calculated that he needed 113 gallons of fuel to legally complete the flight. He informed the fixed base operator (FBO) that he wanted the fuel tanks topped off, but was informed by the ramp technician that the fuel tanks were full and he did not need fuel. The pilot went back to the airplane and removed the fuel cap. He noticed fuel in the filler neck and assumed the fuel tanks were full. He did not push open the anti-siphon fuel valve to see if the tanks were full or if residual fuel was pooled on top of the anti-siphon fuel valve. When the pilot started the engines, he noticed the fuel gauge was flickering and thought it was malfunctioning. He proceeded to depart for the maintenance base. After about 2 hours of flight time both engines lost power. Unable to reach the closest airport, the pilot executed an off field landing in a cotton field. After landing, the airplane rolled into the trees and the left wing separated from the fuselage. The airplane sustained substantial damage to the left and right wings. According to the fueler at the FBO, she drove out to the airplane to fuel it on the morning of the accident and, after removing the single fuel cap, saw fuel on top of the anti-siphon valve. She used her finger to push down the valve and felt fuel, so she believed the airplane was full of fuel and it did not need additional fuel. Both wing fuel bladders were breached during the accident and a minor amount of fuel was leaked onto the ground. Personnel from the company who recovered the wreckage stated that there was no fuel in the fuel tanks when the airplane was recovered. The fuel quantity transmitter was sent to the manufacturer for examination. Testing of the transmitter revealed no anomalies with the unit. Based on this information, it is likely that the pilot erred in his assessment of the airplane’s fuel quantity prior to departing on the accident flight and that the available quantity of fuel was exhausted, which resulted in the total loss of engine power and the subsequent forced landing.