Crash of a Beechcraft C90 King Air in Fort Lauderdale: 1 killed

Date & Time: Jun 13, 2001 at 2122 LT
Type of aircraft:
Operator:
Registration:
YV-2466P
Flight Type:
Survivors:
Yes
Schedule:
Charallave – Fort Lauderdale
MSN:
LJ-591
YOM:
1973
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
3205
Captain / Total hours on type:
1800.00
Aircraft flight hours:
8279
Circumstances:
The Venezuelan registered Beech King Air C90 departed Caracas, Venezuela's Óscar Machado Zuloaga International Airport at 1516 eastern daylight time with a pilot and two passengers aboard, and flew to Fort Lauderdale-Hollywood International Airport, Florida. The route of flight filed with air traffic control was: after departure, direct to Maiquetia, thence Amber Route-315 to Bimini, thence Bahama Route 57V to Fort Lauderdale. The {planned} flight level was 220, and the pilot stated that 7 hours 15 minutes of fuel was aboard. Immigration/customs general declaration papers found aboard the wreckage stated the flight's intended destination was Nassau, and the pilot's daughter stated he always stopped at Nassau for fuel on many previous trips. After 6 hours 6 minutes, the aircraft crashed into a highway abutment about 1,700 feet short of his intended landing runway at Fort Lauderdale with total accountable onboard fuel of 3 to 4 gallons. One passenger received fatal injuries, one passenger received serious injuries, and the pilot received serious injuries. Engine factory service center disassembly examination revealed that the engines and their components exhibited no evidence of any condition that would have precluded normal operation, precrash. No precrash abnormalities with the propellers, their respective components, or any other aircraft system component were noted. Type certification data sheets for the C90 state that the unusable fuel aboard is 24 lbs., (3.6 gallons of Jet-A fuel).
Probable cause:
The pilot's failure to properly plan fuel consumption and to perform an en route refueling, resulting in a total loss of engine power due to fuel exhaustion while on downwind leg for landing at eventual destination, causing an emergency descent and collision with a highway embankment.
Final Report:

Crash of a Beechcraft C90 King Air in Islip

Date & Time: May 18, 2001 at 1725 LT
Type of aircraft:
Operator:
Registration:
N270TC
Flight Type:
Survivors:
Yes
Schedule:
East Hampton - Ronkonkoma
MSN:
LJ-858
YOM:
1979
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2439
Captain / Total hours on type:
98.00
Copilot / Total flying hours:
1613
Copilot / Total hours on type:
114
Aircraft flight hours:
6581
Circumstances:
After about a 20 minute flight, while on final approach for landing, the airplane experienced a loss of engine power on both engines, and the pilot-in-command (PIC) performed a forced landing into trees about 1/2 mile from the airport. The left and right boost pumps and the left and right transfer pumps, were observed in the "OFF" position. According to the PIC, after he exited the airplane, he returned to the cockpit and "shut off the fuel panel. The fuel quantity indicator toggle switch was observed in the "TOTAL" position. Examination of the fuel system revealed both engine nacelle tanks, both wing center section tanks, and the right wing fuel tanks were not compromised. About 1 quart of fuel was drained from the left and right engine nacelle tanks, respectively. Less than a quart of fuel was drained from the right wing tanks. The left wing tanks were compromised during the accident; however there was and no evidence of a fuel spill. Examination of the left and right wing center tanks revealed approximately 27 gallons (approximately 181 lbs) of fuel present in each tank. Battery power was connected to the airplane, and when the fuel transfer pump switches were turned to the "ON" position, fuel was observed being pumped from the left and right wing center tanks to their respective nacelle tanks. The accident flight was the third flight of the day for the flight crew and airplane. According to a flight log located in the cockpit, the flight crew indicated 750 lbs of fuel remained at the time of the takeoff. According to the airplane flight manual (AFM),"Fuel for each engine is supplied from a nacelle tank and four interconnected wing tanks...The outboard wing tanks supply the center section wing tank by gravity flow. The nacelle tank draws its fuel supply from the center section tank. Since the center section tank is lower than the other wing tanks and the nacelle tank, the fuel is transferred to the nacelle tank by the fuel transfer pump in the low spot of the center section tank...." Additionally, with the transfer pumps inoperative, all wing fuel except 28 gallons from each wing will transfer to the nacelle tank through gravity feed.
Probable cause:
The pilot’s failure to activate the fuel transfer pumps in accordance with the checklist, which resulted in fuel exhaustion.
Final Report:

Crash of a Beechcraft B90 King Air near San Jon: killed

Date & Time: May 14, 2001 at 2322 LT
Type of aircraft:
Registration:
N221CH
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Tucson – Springdale
MSN:
LJ-436
YOM:
1969
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
16800
Captain / Total hours on type:
3000.00
Aircraft flight hours:
7557
Circumstances:
The pilot was flying a pressurized airplane at 25,000 feet (cabin altitude of 10,000 feet). For approximately 43 minutes before the accident, ARTCC called the pilot approximately six times and asked him to correct his altitude. Two transmissions from the pilot, between 2305 and 2311, were made with "slurred, and unclear speech." A 2 minute period followed with over 30 hot mike transmissions in which heavy breathing could be heard in some. At 2318:20, the pilot's last transmission was "ah Charlie Hotel, we, we've a little bit of a problem here. We're in a descent, we'll straighten it out in a minute." Witnesses observed the airplane spin into ground. The pilot's autopsy revealed moderate emphysema in his lungs with the presence of air filled bullae measuring up to 3 cm. On the two flights before the accident flight, the owner of the aircraft said that the pilot slept 2 hours out of the 4.5 hours of flight. Several friends of the pilot reported that he was also observed to "easily doze" off while on the ground, but he did so more regularly and for longer time periods while flying.
Probable cause:
The pilot's failure to maintain aircraft control due to his incapacitation for an undetermined reason. A contributing factor was the subsequent inadvertent stall/spin to the ground.
Final Report: