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Crash of a Rockwell Gulfstream 695A Jetprop 1000 in San Bernardino: 1 killed

Date & Time: Apr 13, 2024 at 2019 LT
Operator:
Registration:
N965BC
Flight Type:
Survivors:
No
Site:
Schedule:
Stockton - Chino
MSN:
96071
YOM:
1984
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The pilot departed Stockton Airport on a solo flight to Chino. On a standard approach in rainy conditions, the airplane suffered two altitude deviations which the pilot attributed to a problem with the autopilot. Towards the end of the flight, the airplane descended past the Minimum Vectoring Altitude (MVA) of 7,400 feet and was issued an altitude alert by the controller, but there was no response from the pilot. The airplane entered an uncontrolled descent with a rate of about 10'000 feet per minute until it crashed in mountainous terrain. The airplane was destroyed by impact forces and the pilot was killed.

Crash of a Beechcraft B100 King Air in Abbotsford

Date & Time: Feb 23, 2018 at 1204 LT
Type of aircraft:
Operator:
Registration:
C-GIAE
Flight Phase:
Survivors:
Yes
Schedule:
Abbotsford - San Bernardino
MSN:
BE-8
YOM:
1976
Flight number:
IAX640
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
10000
Captain / Total hours on type:
800.00
Aircraft flight hours:
10580
Circumstances:
Weather conditions at Abbotsford at the time of departure consisted of a temperature of -2°C in moderate to heavy snowfall with winds of approximately 10 knots. Prior to the departure, the fuel tanks were filled to capacity and the pilot and passengers boarded the aircraft inside the operator's heated hangar. The aircraft was towed outside of the hangar without being treated with anti-ice fluid, and taxied for the departure on runway 07. Due to an inbound arrival at Abbotsford, C-GIAE was delayed for departure. Once cleared for takeoff, the aircraft had been exposed to snow and freezing conditions for approximately 14 minutes. After becoming airborne, the aircraft experienced power and control issues shortly after the landing gear was retracted. The aircraft collided with terrain within the airport perimeter. Four passengers and the pilot sustained serious injuries as a result of the accident which destroyed the aircraft.
Probable cause:
The accident was the consequence of the combination of the following findings:
- The occurrence aircraft exited a warm hangar and was exposed to 14 minutes of heavy snow in below-freezing conditions. This resulted in a condition highly conducive to severe ground icing,
- As the aircraft climbed out of ground effect on takeoff, it experienced an aerodynamic stall as a result of wing contamination,
- The pilot’s decision making was affected by continuation bias, which resulted in the pilot attempting a takeoff with an aircraft contaminated with ice and snow adhering to its critical surfaces,
- The pilot and the passenger seated in the right-hand crew seat were not wearing the available shoulder harnesses. As a result, they sustained serious head injuries during the impact sequence,
- During the impact sequence, the cargo restraint system used to secure the baggage in the rear baggage compartment failed, causing some of the baggage to injure passengers seated in the rear of the aircraft cabin,
- The aircraft was not airworthy at the time of the occurrence as a result of an incomplete airworthiness directive.
Final Report:

Crash of a PZL-Mielec AN-2R in San Bernardino

Date & Time: May 6, 2016 at 1200 LT
Type of aircraft:
Operator:
Registration:
N2AN
Flight Type:
Survivors:
Yes
Schedule:
Upland - San Bernardino
MSN:
1G210-55
YOM:
1985
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3350
Captain / Total hours on type:
58.00
Aircraft flight hours:
2924
Circumstances:
The commercial pilot was entering the airport traffic pattern for landing during a familiarization flight. He reported that he turned on the carburetor heat, switched the fuel tank selector to the right fuel tank, and shortly thereafter, the engine experienced a total loss of power. The pilot attempted numerous times to restart the engine but was unsuccessful. After realizing that he would not be able to reach the runway, he decided to make a forced landing to a small field. During the landing approach, the airplane contacted a power line, nosed over, and came to rest inverted, resulting in substantial damage to the wings and fuselage. During the postaccident examination of the airplane, about 16 ounces of water were removed from the fuel system. Water was present in the lower gascolator, the fine fuel filter (upper gascolator), and subsequent fuel line to the carburetor inlet. A brass screen at the carburetor inlet and 2 carburetor fuel bowl thumb screens also contained corrosion, water, and rust. The approved aircraft inspection checklist called for washing the carburetor and main fuel filter every 50 hours and cleaning and/or replacing the fine fuel filter every 100 hours. The fine fuel filter is not easily accessible and not able to be drained during a preflight inspection. The mechanic who completed the most recent inspection stated that he did not drain or check the fine fuel filter. The last logbook entry that specifically stated the fuel filters were cleaned was about 4 years before the accident.
Probable cause:
The mechanic's failure to inspect the fine fuel filter gascolator as required during the most recent inspection, which resulted in a total loss of engine power due to fuel contamination.
Final Report:

Crash of a Lockheed P2V-7 Neptune near San Bernardino: 2 killed

Date & Time: Oct 3, 2003 at 1116 LT
Type of aircraft:
Operator:
Registration:
N299MA
Flight Type:
Survivors:
No
Site:
Schedule:
Prescott – San Bernardino
MSN:
726-7211
YOM:
1958
Flight number:
Tanker 99
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
7803
Captain / Total hours on type:
1853.00
Copilot / Total flying hours:
7363
Copilot / Total hours on type:
853
Circumstances:
The fire tanker airplane was on a cross-country positioning flight and collided with mountainous terrain while maneuvering in a canyon near the destination airport. Witnesses who held pilot certificates were on a mountain top at 7,900 feet and saw a cloud layer as far to the south as they could see. They used visual cues to estimate that the cloud tops were around 5,000 feet mean sea level (msl). They noted that the clouds did not extend all the way up into the mountain canyons; the clouds broke up near the head of some canyons. When they first saw the airplane, they assumed that it came from above the clouds. It was proceeding north up a canyon near the edge of clouds, which were breaking up. They were definitely looking down at the airplane the whole time. They saw the airplane make a 180-degree turn that was steeper than a standard rate turn. The wings leveled and the airplane went through one cloud, reappeared briefly, and then entered the cloud layer. It appeared to be descending when they last saw it. About 2 minutes later, they saw the top of the cloud layer bulge and turn a darker color. The bulge began to subside and they observed several smaller bulges appear. They notified local authorities that they thought a plane was down. Searchers discovered the wreckage at that location and reported that the wreckage and surrounding vegetation were on fire. The initial responders reported that the area was cloudy and the visibility was low. Examination of the ground scars and wreckage debris path disclosed that the airplane collided with the canyon walls in controlled flight on a westerly heading of 260 degrees at an elevation of 3,400 feet msl. The operator had an Automated Flight Following (AFF) system installed on the airplane. It recorded the airplane's location every 2 minutes using a GPS. The data indicated that the airplane departed Prescott and flew direct to the Twentynine Palms VORTAC (very high frequency omnidirectional radio range, tactical air navigation). The flight changed course slightly to 260 degrees, which took it to the northeast corner of the wilderness area where the accident occurred. At 1102:57, the data indicated that the airplane was at 11,135 feet msl at 204 knots. The airplane then made three left descending 360-degree turns. The third turn began at 6,010 feet msl. At 1116:57, the last recorded data point indicated that the airplane was at an altitude of 3,809 feet heading 256 degrees at a speed of 128 knots.
Probable cause:
The pilot's inadequate in-flight planning/decision and continued flight into instrument meteorological conditions that resulted in controlled flight into mountainous terrain.
Final Report:

Crash of a Curtiss C-46A-1-CU Commando near Upland: 4 killed

Date & Time: Oct 5, 1945
Type of aircraft:
Operator:
Registration:
41-5190
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Norton - Reno
MSN:
26392
YOM:
943
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
Few minutes after takeoff from Norton AFB, in San Bernardino, while cruising in poor weather conditions, the aircraft hit the west slope of Mt Baldy at a height of 10,064 feet. The wreckage was found a day later and all four occupants have been killed. At the time of the accident, visibility was poor due to low clouds and precipitations.

Crash of a Potez 25 in Altos: 3 killed

Date & Time: Sep 7, 1940
Type of aircraft:
Operator:
Registration:
7
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Asunción – San Bernardino
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The single engine aircraft was on its way from Asunción to San Bernardino with two passengers and a pilot on board. While approaching the destination, the pilot encountered poor visibility due to fog and failed to realize his altitude was too low when the airplane impacted the ground and crashed in an open field located in Altos, about 10 km north of San Bernardino. The wreckage was spotted few hours later by the crew of a Brazilian Air Force's Waco. All three occupants were killed, among them General José Félix Estigarribia, President of the Republic of Paraguay and his wife who were travelling to their private house located on the shore of Lake Ypacaraí.
Crew:
Maj Carmelo Peralta, pilot.
Passengers:
General José Félix Estigarribia,
Mrs. Julia Miranda Cueto.
Probable cause:
Controlled flight into terrain.

Crash of a Lockheed 1 Vega in San Bernardino: 3 killed

Date & Time: Jul 9, 1934
Type of aircraft:
Registration:
NC32E
Flight Phase:
Survivors:
Yes
MSN:
33
YOM:
1929
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
Crashed in unknown circumstances. The aircraft was completely demolished and a passenger was seriously injured while all three other occupants were killed.