White Plains-Westchester County

Witnesses reported aircraft was high during approach and landed nosewheel 1st about 1,600 feet beyond threshold, then became airborne and bounced 2 times. Pilot stated that before touchdown, he started to 'spool up' engines, but noted lack of response, then retarded throttles and landed. He said he applied brakes and selected 'full reverse' and noted no response. Reportedly, nosewheel 'skipped into air' while aircraft still had flying speed. With insufficient runway remaining to stop, he elected to stow reversers and began go-around. He noted no response from engines, tho aircraft had became airborne. Aircraft then settled beyond departure end of runway and crashed on rough terrain. Examination revealed engines had ingested twigs, grass and dirt. Reverse load limiters (l/l) on both engines were found in tripped position. Flight man stated that to avoid actuation of l/l, do not advance primary throttle after returning reverse thrust lever to stow until unlock light is out; maint required to reset actuated l/l. L/l was incorporated on thrust reverser to reduce engine power to idle, if inadvertently deployed in flight. During post-accident check, both engines were operated to 85% after l/l reset.

The cross country business flight was uneventful from Concord, New Hampshire to white Plains, New York under clear sky. During final approach, the pilot extended the gear but did not notice that the circuit breaker had opened and the gear was not lowered. The aircraft landed gear up and the gear doors partially open. The gear warning horn did not operate. The pilot stated that he failed to check for 3 green lights.

During preflight preparation for departure from a short field the pilot failed to remove the Pitot tube covers. On takeoff roll, the stall warning light began to flicker. Pilot noted airspeed was not registering but did not consider this unusual in the early part of a takeoff roll. Pilot turned left stall warning switch off, then back on, warning light remained on. Pilot then initiated abort procedures, using full reverse thrust and brakes. The aircraft overran runway by about 100 feet and down a rough embankment which separated the landing gear.

During arrival, there were indefinite delays at White Plains, NY, so the pilot diverted to Newburgh, NY. He was vectored for an ILS runway 09 approach. While en route, the pilot requested and was given the ILS frequency, minimums for the approach, the airport elevation (491 feet msl), the Newburgh weather and the frequency for the outer compass locator (even tho, current approach charts were on board). He was cleared for the approach, but the aircraft hit trees and crashed, 2.58 miles west of runway 09. Elevation of the crash site was about 580 feet. The minimum descent altitude (MDA) for the approach was 682 feet. An exam of the wreckage revealed no preimpact part malfunction or failure. The pilot was required to wear lenses to correct his vision. The area forecast called for icing, turbulence, low level wind shear, low ceilings, rain, drizzle, fog and a chance of light freezing rain/drizzle. Reportedly the pilot received a full weather briefing, but was not briefed on sigmets Juliett 7 and Lima 4 which called for moderate to severe turbulence and low level wind shear and occasional moderate to severe mixed/clear icing in clouds and precipitations below 8,000 feet.

About 1840 e.s.t., on February 11, 1981, a Lockheed JetStar L-1329-731, N520S, crashed during an instrument landing system approach to runway 16 at the Westchester County Airport, White Plains, New York. The area weather was dominated by low obscured ceilings, rain, fog, and reduced visibility. Winds were strong and gusty with moderate to severe turbulence in the lower levels. Following a recent modification of the generator control. circuitry, the aircraft's electrical system had experienced several multiple generator failures.

While in cruising altitude in good weather conditions, en route from Concord to White Plains, the twin engine airplane collided with a Piper PA-60 Aerostar (Ted Smith Aerostar 600) owned by Northeast Cellulose Inc and registered N8011J. En route from Boston to Syracuse, it was carrying one passenger and one pilot. Following the collision, both aircraft entered a dive and crashed near Templeton. Both aircraft were destroyed and all five occupants were killed.

En route from Boston to White Plains in normal cruise, both engines failed. The pilot reduced his altitude and attempted an emergency landing when the airplane struck trees and crashed in Framingham. Both occupants were seriously injured and the aircraft was destroyed.

En route from Philadelphia to White Plains with three people on board, the twin engine airplane collided with a Cessna 172 operated by Teterboro Flight Service, registered N75604 and carrying two people. Following the collision, both aircraft went out of control and crashed into the Hudson River near the Tappan Zee Bridge. Both aircraft were destroyed and all five occupants have been killed.

The crew departed Norfolk-Chambers Field on a flight to the Northrop Grumman facilities in White Plains, NY. About two minutes after takeoff from runway 10, while in initial climb, the airplane encountered difficulties, stalled and crashed on a beach located in Ocean View Beach, about 4 miles east of the airport. The aircraft was destroyed and all five crew members were killed.
Crew:
Lt Walter J. MacLeod Jr.,
Lt Randall M. Moore,
Lt Edward W. Cassel,
Lt Arthur T. Dunn,
Ens Howard E. Wagoner.

While cruising on a night cargo flight from Arkansas City to White Plains, NY, the airplane went out of control and crashed in flames in an open field located near Winfield. The aircraft was totally destroyed and both occupants have been killed.