Crash of a Piper PA-31-350 Navajo Chieftain off Amagansett: 4 killed

Date & Time: Jun 2, 2018 at 1433 LT
Registration:
N41173
Flight Type:
Survivors:
No
Schedule:
Newport – East Hampton
MSN:
31-8452017
YOM:
1984
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
3000
Aircraft flight hours:
5776
Circumstances:
The commercial pilot of the multiengine airplane was the first of a flight of two airplanes to depart on the cross-country flight, most of which was over the Atlantic Ocean. The pilot of the second airplane stated that he and the accident pilot reviewed the weather for the route and the destination before departing; however, there was no record of the accident pilot receiving an official weather briefing and the information the pilots accessed before the flight could not be determined. The second pilot departed and contacted air traffic control, which advised him of thunderstorms near the destination; he subsequently altered his route of flight and landed uneventfully at the destination. The second pilot stated that he did not hear the accident pilot on the en route air traffic control frequency. Two inflight weather advisories were issued for the route and the area of the destination about 42 and 15 minutes before the accident flight departed, respectively, and warned of heavy to extreme precipitation associated with thunderstorms. It could not be determined whether the accident pilot received these advisories. Review of air traffic control communications and radar data revealed that, about 5 miles from the destination airport, the pilot of the accident airplane reported to the tower controller that he was flying at 700 ft and "coming in below" the thunderstorm. There were no further communications from the pilot. The airplane's last radar target indicated 532 ft about 2 miles south of the shoreline. The airplane was found in about 50 ft of water and was fragmented in several pieces. Postaccident examination revealed no preimpact anomalies with the airplane or engines that would have precluded normal operation. A local resident about 1/2 mile from the accident site took several photos of the approaching thunderstorm, which documented a shelf cloud and cumulus mammatus clouds along the leading edge of the storm, indicative of potential severe turbulence. Review of weather imagery and the airplane's flight path showed that the airplane entered the leading edge of "extreme" intensity echoes with tops near 48,000 ft. Imagery also depicted heavy to extreme intensity radar echoes over the accident site extending to the destination airport. It is likely that the pilot encountered gusting winds, turbulence, restricted visibility in heavy rain, and low cloud ceilings in the vicinity of the accident site and experienced an in-flight loss of control at low altitude. Such conditions are conducive to the development of spatial disorientation; however, the reason for the pilot's loss of control could not be determined based on the available information.
Probable cause:
The pilot's decision to fly under a thunderstorm and a subsequent encounter with turbulence and restricted visibility in heavy rain, which resulted in a loss of control.
Final Report:

Crash of a Rockwell Shrike Commander 500S in Exeter: 1 killed

Date & Time: Feb 17, 2002 at 1752 LT
Registration:
N999N
Survivors:
No
Schedule:
Wilmington - Newport
MSN:
500-3277
YOM:
1976
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
900
Captain / Total hours on type:
200.00
Aircraft flight hours:
2145
Circumstances:
The airplane was in instrument meteorological conditions and the pilot was cleared for an approach. As the airplane neared the final approach fix, the controller observed the airplane diverge from the approach course and change altitude rapidly. Shortly thereafter, the pilot said he had "all sorts of problems." The pilot requested and received vectors to an alternate airport. At 1748:29, the pilot was cleared for an ILS approach and was told to report when "established" on the approach. When asked if he was established on the ILS course, the pilot replied "I sure hope so." The controller observed the airplane descend below the published glide slope intercept altitude and advised the pilot to climb back to 2,000 feet. The pilot reported "I have problems." When asked the nature of the problem, the pilot reported "...I'm all over the place...I think I'm iced up..." Radar data indicated the airplane's radar track began following a left descending turn from 1,900 feet, about 1 minute before radar contact was lost. At 1751:33, the controller advised the pilot that his altitude was 1,000 feet, and requested that he climb to 3,000 feet. The pilot responded, "hey, I'm trying like hell." Radar contact with the airplane was lost about 1752, at 800 feet. A witness near the accident site stated he observed the airplane come out of the clouds, "wobbling" from side to side, make a "hard" left turn and strike the ground. He stated the engine was "loud" and seemed to be at "full throttle." Examination of the airplane did not reveal any pre impact mechanical malfunctions. The pilot purchased the accident airplane about 2 months prior to the accident. His total flight time in make and model was estimated to be about 200 hours. Airman's Meteorological Information (AIRMET) Zulu, Update 4, for Ice and Freezing Level was valid for the accident site area at the time of the accident. The AIRMET advised of occasional moderate rime/mixed icing in cloud in precipitation below 12,000 feet. The AIRMET reported the freezing level was from the surface to 4,000 feet. According to United States Naval Observatory astronomical data obtained for the accident site area, Sunset occurred at 1723, and the end of civil twilight was at 1751. The airplane was equipped with both wing leading edge and empennage de-icing boots. The switches for the de-icing boots were observed in the "Auto" position. The propeller de-ice and windshield anti-ice switches were observed in the "off" position.
Probable cause:
The pilot's failure to maintain control after encountering icing conditions while on approach for landing. Factors in this accident were the night light conditions and pilot's failure to select the airplane's propeller de-icing switches to the "on" position.
Final Report:

Crash of a Cessna 402 in New Bedford

Date & Time: Jan 31, 1986 at 1544 LT
Type of aircraft:
Registration:
N4033Q
Flight Type:
Survivors:
Yes
Schedule:
Newport - New Bedford
MSN:
402-0133
YOM:
1967
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1249
Captain / Total hours on type:
242.00
Aircraft flight hours:
4052
Circumstances:
The pilot experienced inadequate left engine manifold pressure during a takeoff attempt at Newport. The takeoff was aborted and afterwards the pilot decided to ferry the aircraft to New Bedford for inspection. The engine were restarted and operation was good. The flight to New Bedford was without incident until the aircraft was on a two miles final to runway 05 at this time the left engine stopped while the pilot attempted to feather the engine, both the engine and part of the left wing caught on fire. The pilot continued to the airport with the flaps and gear down and a speed at 125 mph. The pilot stated he was in a good position to land when he heard a loud bang which he described sounded like a cable. The aircraft entered a 25° left bank. He leveled the wings by reducing right engine power. Collision with trees to the left of the runway occurred afterwards. Examination of the aircraft disclosed that the left engine exhaust manifold header assembly, which is connected to the turbocharger, was cracked along a weld seam. Also revealed was that the aileron cables that are routed behind the left engine were burned to separation. Both occupants were injured.
Probable cause:
Occurrence #1: loss of engine power
Phase of operation: approach - vfr pattern - final approach
Findings
1. (c) exhaust system, manifold/pipe - cracked
2. (c) exhaust system, turbocharger - disabled
----------
Occurrence #2: fire
Phase of operation: approach - vfr pattern - final approach
Findings
3. (c) exhaust system - fire
----------
Occurrence #3: loss of control - in flight
Phase of operation: approach - vfr pattern - final approach
Findings
4. (c) flt control syst, aileron control - burned
5. (c) flight control, aileron - disabled
6. (f) aileron - not possible - pilot in command
----------
Occurrence #4: in flight collision with object
Phase of operation: approach - vfr pattern - final approach
Findings
7. Object - tree(s)
Final Report:

Crash of a Loening 23 Air Yacht off Newport

Date & Time: Dec 31, 1923
Type of aircraft:
Survivors:
Yes
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The airplane crashed in the sea off Newport. There were no casualties. The exact date of the mishap remains unknown.