Crash of a Cessna 402C II in Martha's Vineyard

Date & Time: Jan 30, 2001 at 1835 LT
Type of aircraft:
Operator:
Registration:
N6837Y
Flight Type:
Survivors:
Yes
Schedule:
Providence – Martha’s Vineyard
MSN:
402C-0467
YOM:
1981
Flight number:
9K415
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1668
Captain / Total hours on type:
348.00
Aircraft flight hours:
19131
Circumstances:
The pilot departed on a scheduled flight conducted under night instrument meteorological conditions. Arriving in the area of the destination airport, the weather was reported as, winds from 220 degrees at 18 knots, gusts to 25 knots; 1/2 statute miles of visibility and haze; vertical visibility of 100 feet. The pilot was vectored and cleared for the ILS 24 approach. As the airplane crossed the glideslope, the pilot observed that the "ride" became increasingly bumpy and turbulent, with a strong wind component from the right. The approach lights came into view as the airplane neared the runway, but soon disappeared due to the low visibility. The pilot executed a missed approach, and as full power was applied, the airplane began to move laterally to the left. During the missed approach, a "thunk" was heard on the left side of the fuselage, and the airplane descended into the trees. The airplane came to rest in a wooded area about 1/4 mile from the Runway 24 threshold, about 1,000 feet to the left of the extended centerline. Review of the approach plate for the ILS 24 approach revealed that the glide slope altitude at the final approach fix for the non-precision approach, which was located about 4 miles from the approach end of the runway, was 1,407 feet. The glide slope altitude at the middle marker, which was located about 0.6 miles from the approach end of the runway, was 299 feet. Review of radar data revealed that the airplane intercepted the glideslope about 4 miles from the threshold of runway 24. In the following 2 minutes, 30 seconds, the airplane deviated below and returned to the glideslope centerline approximately 4 times, with a maximum deviation of 2-dots below the glideslope centerline. About 1-mile from the runway, the airplane began a trend downward from the glideslope centerline, descending below the 2- dot low deviation line of the glideslope to an altitude of about 300 feet, when the last radar hit was recorded. During the approach, the airplane's ground speed varied between 50 and 125 knots. According to the Aeronautical Information Manual chapter on Navigation Aids, Instrument Landing System (ILS), it stated that "Make every effort to remain on the indicated glide path." It also cautioned the pilot to, "Avoid flying below the glide path to assure obstacle/terrain clearance is maintained."
Probable cause:
The pilot's failure to maintain a stabilized approach with an adequate vertical and lateral track. Also causal was his failure to maintain obstacle clearance.
Final Report:

Crash of a Piper PA-31T Cheyenne II in Lawrence

Date & Time: Mar 20, 1987 at 2300 LT
Type of aircraft:
Operator:
Registration:
N200FD
Flight Type:
Survivors:
Yes
Schedule:
Providence - Lawrence
MSN:
31-7520040
YOM:
1975
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9530
Captain / Total hours on type:
789.00
Aircraft flight hours:
3707
Circumstances:
The crew of the PA-31T Cheyenne had made one missed approach and the copilot was calling out the altitudes to the pilot. The pilot's reply to the copilot that he was just going to descend to 400 feet. The approach minimums were published for an MDA of 660 feet plus 80 feet when the control zone is not in effect. The aircraft flew into rising terrain. The copilot suffered minor injuries, the aircraft was destroyed due to impact and fire.
Probable cause:
Occurrence #1: in flight collision with terrain/water
Phase of operation: approach - faf/outer marker to threshold (ifr)
Findings
1. (f) weather condition - obscuration
2. (f) weather condition - snow
3. (f) light condition - dark night
4. (c) ifr procedure - not followed - pilot in command
5. (c) minimum descent altitude - not maintained - pilot in command
6. Overconfidence in personal ability - pilot in command
Final Report:

Crash of a De Havilland DHC-6 Twin Otter 300 near Providence: 1 killed

Date & Time: Feb 21, 1982 at 1533 LT
Operator:
Registration:
N127PM
Flight Phase:
Survivors:
Yes
Schedule:
Groton - Boston
MSN:
105
YOM:
1968
Flight number:
PM458
Crew on board:
2
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
6500
Captain / Total hours on type:
2700.00
Copilot / Total flying hours:
2100
Copilot / Total hours on type:
400
Aircraft flight hours:
27015
Circumstances:
At 4,000 feet light icing on the windshield was noted, and the deicing system was activated. After two cycles of deicing, alcohol was smelled in the cockpit, and smoke was coming up from the control yoke. An emergency landing was attempted at Providence, RI, but smoke and flames forced the crew to land on 10-12 inch thick ice on a reservoir. By then, heavy black smoke poured in the cockpit and fire was seen. Upon landing, the left main gear collapsed and the right wing was sheared off. Eleven occupants escaped and were injured while a passenger was killed.
Probable cause:
The deficient design of the isopropyl alcohol windshield washer/deicer system and the inadequate maintenance of the system which resulted in an in-flight fire. The ignition source of the fire was not determined.
Final Report:

Crash of a Beechcraft E18S in Newark: 2 killed

Date & Time: Sep 23, 1972 at 0018 LT
Type of aircraft:
Operator:
Registration:
N107T
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Newark - Providence
MSN:
BA-122
YOM:
1956
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
4850
Captain / Total hours on type:
62.00
Circumstances:
Shortly after takeoff, while climbing by night, one of the engine lost power. The twin engine airplane lost height and crashed in flames on a railroad track located near the airport. The aircraft was destroyed by impact forces and a post crash fire and both occupants were killed.
Probable cause:
Loss of control after takeoff due to a loss of power on one engine. The following factors were reported:
- Failure of the exhaust system: external supercharger,
- Material failure,
- The pilot-in-command failed to maintain flying speed,
- The crew failed to follow the approved procedures,
- Improper emergency procedures,
- Partial loss of power on one engine,
- Broken pieces of ball bearings from impeller shaft found in inertia coupling.
Final Report:

Crash of a Rockwell 1121A Jet Commander in New York: 5 killed

Date & Time: Jan 27, 1971 at 1955 LT
Operator:
Registration:
N400CP
Flight Phase:
Survivors:
No
Schedule:
Burlington - Providence
MSN:
1121-30
YOM:
1965
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
9908
Captain / Total hours on type:
692.00
Circumstances:
While cruising by night over the State of New York on a flight from Burlington, Vermont, and Providence, Rhode Island, the twin engine airplane disappeared from radar screens without the pilots having been able to transmit all or part of an emergency message. SAR operations were conducted but eventually suspended few days later as no trace of the aircraft nor the crew was ever found. It is believed that the aircraft may crash into Lake Champlain but again, no trace was ever found.
Probable cause:
Due to lack of evidences, the exact cause of the accident could not be determined.
Final Report:

Crash of a Martin B-10B in Providence: 4 killed

Date & Time: Sep 22, 1936
Operator:
Registration:
35-242
Flight Phase:
Flight Type:
Survivors:
No
MSN:
657
YOM:
1935
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
While departing Hillsgrove Airport in Providence, the airplane stalled and crashed, killing the entire crew.

Crash of a Waco YOC in Providence: 2 killed

Date & Time: Aug 28, 1935 at 0815 LT
Type of aircraft:
Registration:
NC14621
Survivors:
No
Schedule:
Boston – Providence – Cleveland
MSN:
4245
YOM:
1935
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
On final approach to Providence Airport, at a height of 500 feet, the aircraft banked left, dove into the ground and crashed, bursting into flames. Both occupants were killed. The pilot was en route from Boston to Cleveland, making an intermediate stop in Providence to pick up an additional passenger.
Probable cause:
It is the opinion of the Accident Board that the probable cause of this accident was a failure of the pilot to maintain sufficient flying speed to properly control the aircraft in the existing gusty wind conditions. At the time of the accident, gusty winds were up to 32 km/h from southwest.