Crash of a BAe Jetstream 31 in Wilkes-Barre: 19 killed

Date & Time: May 21, 2000 at 1148 LT
Type of aircraft:
Operator:
Registration:
N16EJ
Survivors:
No
Schedule:
Atlantic City – Wilkes-Barre
MSN:
834
YOM:
1988
Crew on board:
2
Crew fatalities:
Pax on board:
17
Pax fatalities:
Other fatalities:
Total fatalities:
19
Captain / Total flying hours:
8500
Captain / Total hours on type:
1874.00
Copilot / Total flying hours:
1282
Copilot / Total hours on type:
742
Aircraft flight hours:
13972
Aircraft flight cycles:
18503
Circumstances:
On May 21, 2000, about 1128 eastern daylight time (EDT), a British Aerospace Jetstream 3101, N16EJ, operated by East Coast Aviation Services (doing business as Executive Airlines) crashed
about 11 miles south of Wilkes-Barre/Scranton International Airport (AVP), Wilkes-Barre, Pennsylvania. The airplane was destroyed by impact and a post crash fire, and 17 passengers and two flight crewmembers were killed. The flight was being conducted under 14 Code of Federal Regulations (CFR) Part 135 as an on-demand charter flight for Caesar’s Palace Casino in Atlantic City, New Jersey. An instrument flight rules (IFR) flight plan had been filed for the flight from Atlantic City International Airport (ACY) to AVP. The captain checked in for duty about 0800 at Republic Airport (FRG) in Farmingdale, New York, on the day of the accident. The airplane was originally scheduled to depart FRG at 0900 for ACY and to remain in ACY until 1900, when it was scheduled to return to FRG. While the pilots were conducting preflight inspections, they received a telephone call from Executive Airlines’ owner and chief executive officer (CEO) advising them that they had been assigned an additional flight from ACY to AVP with a return flight to ACY later in the day, instead of the scheduled break in ACY. Fuel records at FRG indicated that 90 gallons of fuel were added to the accident airplane’s tanks before departure to ACY. According to Federal Aviation Administration (FAA) air traffic control (ATC) records, the flight departed at 0921 (with 12 passengers on board) and arrived in ACY at 0949. According to passenger statements, the captain was the pilot flying from FRG to ACY. After arrival in ACY, the flight crew checked the weather for AVP and filed an IFR flight plan. Fuel facility records at ACY indicated that no additional fuel was added. The accident flight to AVP, which departed ACY about 1030, had been chartered by Caesar’s Palace. According to ATC records, the flight to AVP was never cleared to fly above 5,000 feet mean sea level (msl). According to ATC transcripts, the pilots first contacted AVP approach controllers at 1057 and were vectored for an instrument landing system (ILS) approach to runway 4. The flight was cleared for approach at 1102:07, and the approach controller advised the pilots that they were 5 nautical miles (nm) from Crystal Lake, which is the initial approach fix (IAF) for the ILS approach to runway 4. The pilots were told to maintain 4,000 feet until established on the localizer. At 1104:16, the approach controller advised that a “previous landing…aircraft picked up the airport at minimums [decision altitude].” The pilots were instructed to contact the AVP local (tower) controller at 1105:09, which they did 3 seconds later. The airplane then descended to about 2,200 feet, flew level at 2,200 feet for about 20 seconds, and began to climb again about 2.2 nm from the runway threshold when a missed approach was executed (see the Airplane Performance section for more information). At 1107:26 the captain reported executing the missed approach but provided no explanation to air traffic controllers. The tower controller informed the North Radar approach controllers of the missed approach and then instructed the accident flight crew to fly runway heading, climb to 4,000 feet, and contact approach control on frequency 124.5 (the procedure published on the approach chart). The pilots reestablished contact with the approach controllers at 1108:04 as they climbed through 3,500 feet to 4,000 feet and requested another ILS approach to runway 4. The flight was vectored for another ILS approach, and at 1110:07 the approach controller advised the pilots of traffic 2 nm miles away at 5,000 feet. The captain responded that they were in the clouds. At 1014:38, the controller directed the pilots to reduce speed to follow a Cessna 172 on approach to the airport, and the captain responded, “ok we’re slowing.” The flight was cleared for a second approach at 1120:45 and advised to maintain 4,000 feet until the airplane was established on the localizer. At 1123:49 the captain transmitted, “for uh one six echo juliet we’d like to declare an emergency.” At 1123:53, the approach controller asked the nature of the problem, and the captain responded, “engine failure.” The approach controller acknowledged the information, informed the pilots that the airplane appeared to be south of the localizer (off course to the right), and asked if they wanted a vector back to the localizer course. The flight crew accepted, and at 1124:10 the controller directed a left turn to heading 010, which the captain acknowledged. At 1124:33, the controller asked for verification that the airplane was turning left. The captain responded, “we’re trying six echo juliet.” At 1124:38, the controller asked if a right turn would be better. The captain asked the controller to “stand by.” At 1125:07, the controller advised the pilots that the minimum vectoring altitude (MVA) in the area was 3,300 feet. At 1125:12, the captain transmitted, “standby for six echo juliet tell them we lost both engines for six echo juliet.” At that time, ATC radar data indicated that the airplane was descending through 3,000 feet. The controller immediately issued the weather conditions in the vicinity of the airport and informed the flight crew about the location of nearby highways. At 1126:17, the captain asked, “how’s the altitude look for where we’re at.” The controller responded that he was not showing an altitude readout from the airplane and issued the visibility (2.5 miles) and altimeter setting. At 1126:43, the captain transmitted, “just give us a vector back to the airport please.” The controller cleared the accident flight to fly heading 340, advised the flight crew that radar contact was lost, and asked the pilots to verify their altitude. The captain responded that they were “level at 2,000.” At 1126:54, the controller again advised the flight crew of the 3,300-foot MVA and suggested a 330° heading to bring the airplane back to the localizer. At 1127:14 the controller asked, “do you have any engines,” and the captain responded that they appeared to have gotten back “the left engine now.” At 1127:23, the controller informed the pilots that he saw them on radar at 2,000 feet and that there was a ridgeline between them and the airport. The captain responded, “that’s us” and “we’re at 2,000 feet over the trees.” The controller instructed the pilots to fly a 360° heading and advised them of high antennas about 2 nm west of their position. At 1127:46, the captain transmitted, “we’re losing both engines.” Two seconds later the controller advised that the Pennsylvania Turnpike was right below the airplane and instructed the flight crew to “let me know if you can get your engines back.” There was no further radio contact with the accident airplane. The ATC supervisor initiated emergency notification procedures. A Pennsylvania State Police helicopter located the wreckage about 1236, and emergency rescue units arrived at the accident site about 1306. The accident occurred in daylight instrument meteorological conditions (IMC). The location of the accident was 41° 9 minutes, 23 seconds north latitude, 75° 45 minutes, 53 seconds west longitude, about 11 miles south of the airport at an elevation of 1,755 feet msl.
Probable cause:
The flight crew’s failure to ensure an adequate fuel supply for the flight, which led to the stoppage of the right engine due to fuel exhaustion and the intermittent stoppage of the left engine due to fuel starvation. Contributing to the accident were the flight crew's failure to monitor the airplane’s fuel state and the flight crew's failure to maintain directional control after the initial engine stoppage.
Final Report:

Crash of a Mitsubishi MU-2B-60 Marquise in Allentown

Date & Time: Jan 19, 1996 at 1930 LT
Type of aircraft:
Registration:
N888TP
Survivors:
Yes
Schedule:
Wilkes Barre - Allentown
MSN:
1541
YOM:
1982
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2265
Captain / Total hours on type:
350.00
Aircraft flight hours:
2788
Circumstances:
The flight was on the ILS approach to runway 6, broke out of the clouds at 500 feet, and then re-entered the clouds. The airplane had not yet touched down when it drifted to right of the runway centerline and struck a snow bank located in the grass to the right of the runway, between the runway and the taxiway. The pilot stated he was just starting the missed approach when the accident occurred, and '...that there was no indication of a malfunction of the aircraft.' The reported ceiling was, 100 sky obscured, and the visibility was 1/4 mile, wind 040 degrees, 6 knots.
Probable cause:
The pilot's failure to comply with IFR procedures in that he attempted an instrument approach with visibility below the required minimums, and his delayed execution of a missed approach. A factor was the reduced visibility due to clouds.
Final Report:

Crash of a Piper PA-46-350P Malibu Mirage in Wilkes-Barre

Date & Time: Dec 15, 1993 at 1745 LT
Operator:
Registration:
N92GP
Flight Type:
Survivors:
Yes
Schedule:
Leesburg - Bedford
MSN:
46-22120
YOM:
1991
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
675
Captain / Total hours on type:
175.00
Aircraft flight hours:
206
Circumstances:
While cruising at FL240, the pilot observed the engine oil pressure gradually decrease from the normal to the caution range and a drop in manifold pressure. He requested and received vectors for a precautionary landing at an airport short of his destination. During the descent, the oil pressure continued to drop to zero and engine power was lost. He was able to locate the airport underneath the overcast, but loss of engine power prevented him from reaching the runway. The airplane impacted trees 1,200 feet from the airport. The 6 engine cylinder assemblies were changed 7 hours prior to the accident. Examination of the engine and turbochargers did not reveal the source of the oil loss.
Probable cause:
The loss of engine oil for undetermined reasons and the subsequent engine failure, resulting in a forced landing and collision with trees.
Final Report:

Crash of a Rockwell CT-39A-1-NO Sabreliner in Wilkes Barre: 5 killed

Date & Time: Apr 20, 1985 at 1800 LT
Type of aircraft:
Operator:
Registration:
62-4496
Flight Type:
Survivors:
No
MSN:
276-49
YOM:
1962
Crew on board:
3
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
After landing at Wilkes-Barre Airport, the twin engine airplane was unable to stop within the remaining distance. It overran and went down a 125 feet embankment before coming to rest in flames. All five occupants were killed.

Crash of a Beechcraft H18 in Allentown: 2 killed

Date & Time: Nov 25, 1983 at 0808 LT
Type of aircraft:
Registration:
N105PE
Flight Type:
Survivors:
No
Schedule:
Philadelphia - Wilkes Barre
MSN:
BA-672
YOM:
1964
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3800
Captain / Total hours on type:
145.00
Aircraft flight hours:
7046
Circumstances:
While en route, the pilot encountered icing conditions, then reported he was unable to maintain altitude and was having engine problems. He diverted toward Allentown, PA, then advised he had lost power in the left engine. Approach control began issuing vectors for a VOR approach; however, the pilot advised he was unable to open his approach plates and requested a surveillance radar approach. Radar vectors and advisories were provided until the pilot reported he had the airport in sight. Several witnesses observed that the left prop was feathered as the aircraft approached the airport. The pilot maneuvered the aircraft to a left downwind for runway 24 at about 400 feet agl with the landing gear extended. Witnesses reported the aircraft's nose pitch up, then down, then the aircraft rolled to the left and crashed. In a trailer court it hit a mobile home and a propane tank and burned. A person in the mobile home was fatally injured. An exam of the wreckage revealed the left prop blades were at the low pitch stops. No preimpact failures were found.
Probable cause:
Occurrence #1: in flight encounter with weather
Phase of operation: cruise - normal
Findings
1. (f) weather condition - carburetor icing conditions
2. (f) planning/decision - improper - pilot in command
----------
Occurrence #2: loss of engine power (total) - nonmechanical
Phase of operation: cruise
Findings
3. (f) delayed - pilot in command
4. (f) fuel system, ram air/induction air - ice
5. (f) fuel system, ram air/induction air - blocked (total)
----------
Occurrence #3: loss of control - in flight
Phase of operation: approach - VFR pattern - downwind
Findings
6. Precautionary landing - initiated - pilot in command
7. (c) airspeed (vmc) - not maintained - pilot in command
----------
Occurrence #4: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Findings
8. Emergency procedure - attempted - pilot in command
Final Report:

Crash of a Grumman E-2B Hawkeye in Wilkes-Barre: 1 killed

Date & Time: Nov 13, 1979
Type of aircraft:
Operator:
Registration:
150537
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
A017
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
En route, the crew encountered an unexpected situation. One pilot was able to bail out while the second was killed. The aircraft dove into the ground and was destroyed.

Crash of a Beechcraft B99 Airliner in Allentown: 4 killed

Date & Time: Oct 24, 1971 at 2307 LT
Type of aircraft:
Operator:
Registration:
N986MA
Survivors:
Yes
Site:
Schedule:
Wilkes Barre - Allentown
MSN:
U-044
YOM:
1968
Flight number:
VM098
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
4600
Captain / Total hours on type:
800.00
Circumstances:
Monmouth Airlines Flight 98 departed Wilkes-Barre at 2253LT for a short IFR flight to Allentown. Allentown Approach Control cleared the flight for a VOR approach and instructed the pilot to report when it was 12 miles North of the Allentown VOR. At 2307LT, upon receiving the flight's position estimate, Allentown Approach Control cleared Monmouth 98 for a VOR approach to a landing on runway 06. Monmouth 98 was requested to report when inbound over the Allentown VOR. The airplane then collided with the ridge of Blue Mountain at an elevation of 1540 ft (470 m). The wreckage was found 11,3 miles north of Allentown-Bethlehem Easton Airport. Both pilots and two passengers were killed while four other passengers were injured. The aircraft was destroyed.
Probable cause:
The pilot's nonadherence to approved approach procedures for executing a non precision instrument approach in instrument flight conditions. The Board further finds that there is a high degree of probability that the extensive on-duty time and actual instrument flight time prior to this accident resulted in the fatigue of both pilots and affected their judgment and decisions during the approach.
Final Report: