New York - Brussels

Before flight, the flight engineer (f/e) had calculated 'v' speeds and horizontal stabilizer trim setting for takeoff, but neither the captain nor the 1st officer (f/o) had verified them. During rotation for takeoff, the captain noted that the forced needed to pull the yoke aft was greater than normal and that the aircraft would not fly (at that speed). Subsequently, he aborted the attempted takeoff. Realizing the aircraft would not stop on the remaining runway, he elected to steer it to the right to avoid hitting traffic on a highway near the departure end. The aircraft struck ILS equipment; the landing gear collapsed and all 4 engines tore away. Subsequently, the aircraft was destroyed by fire. Investigations revealed the f/e had improperly computed the takeoff data. He had calculated the 'v' speeds and horizontal stabilizer trim setting for 242,000 lbs; however, the actual takeoff wt was 342,000 lbs. Rotation speed (Vr) for this weight was 28 knots above the speed that was used. Investigations revealed shortcomings in the operator's flightcrew training program and questionable scheduling of qualified (but marginally experienced) crew members for the accident flight.

Flight / Schedule

New York - Brussels

Aircraft

Douglas DC-8

Registration

N730PL

MSN

46161

Year of Manufacture

1971

Date

March 12, 1991 at 09:06 AM

Type

CRASH

Flight Type

Cargo

Flight Phase

Takeoff (climb)

Crash Site

Airport (less than 10 km from airport)

Crash Location

New York-JFK New York

Region

North America • United States of America

Coordinates

40.6429°, -73.7794°

Crash Cause

Human factor

Narrative Report

On March 12, 1991 at 09:06 AM, New York - Brussels experienced a crash involving Douglas DC-8, operated by Air Transport International, with the event recorded near New York-JFK New York.

The flight was categorized as cargo and the reported phase was takeoff (climb) at a airport (less than 10 km from airport) crash site.

5 people were known to be on board, 0 fatalities were recorded, 5 survivors were identified or estimated. This corresponds to an estimated fatality rate of 0.0%.

Crew on board: 3, crew fatalities: 0, passengers on board: 2, passenger fatalities: 0, other fatalities: 0.

The listed crash cause is human factor. Before flight, the flight engineer (f/e) had calculated 'v' speeds and horizontal stabilizer trim setting for takeoff, but neither the captain nor the 1st officer (f/o) had verified them. During rotation for takeoff, the captain noted that the forced needed to pull the yoke aft was greater than normal and that the aircraft would not fly (at that speed). Subsequently, he aborted the attempted takeoff. Realizing the aircraft would not stop on the remaining runway, he elected to steer it to the right to avoid hitting traffic on a highway near the departure end. The aircraft struck ILS equipment; the landing gear collapsed and all 4 engines tore away. Subsequently, the aircraft was destroyed by fire. Investigations revealed the f/e had improperly computed the takeoff data. He had calculated the 'v' speeds and horizontal stabilizer trim setting for 242,000 lbs; however, the actual takeoff wt was 342,000 lbs. Rotation speed (Vr) for this weight was 28 knots above the speed that was used. Investigations revealed shortcomings in the operator's flightcrew training program and questionable scheduling of qualified (but marginally experienced) crew members for the accident flight.

Aircraft reference details include registration N730PL, MSN 46161, year of manufacture 1971.

Geospatial coordinates for this crash are approximately 40.6429°, -73.7794°.

Fatalities

Total

0

Crew

0

Passengers

0

Other

0

Crash Summary

Before flight, the flight engineer (f/e) had calculated 'v' speeds and horizontal stabilizer trim setting for takeoff, but neither the captain nor the 1st officer (f/o) had verified them. During rotation for takeoff, the captain noted that the forced needed to pull the yoke aft was greater than normal and that the aircraft would not fly (at that speed). Subsequently, he aborted the attempted takeoff. Realizing the aircraft would not stop on the remaining runway, he elected to steer it to the right to avoid hitting traffic on a highway near the departure end. The aircraft struck ILS equipment; the landing gear collapsed and all 4 engines tore away. Subsequently, the aircraft was destroyed by fire. Investigations revealed the f/e had improperly computed the takeoff data. He had calculated the 'v' speeds and horizontal stabilizer trim setting for 242,000 lbs; however, the actual takeoff wt was 342,000 lbs. Rotation speed (Vr) for this weight was 28 knots above the speed that was used. Investigations revealed shortcomings in the operator's flightcrew training program and questionable scheduling of qualified (but marginally experienced) crew members for the accident flight.

Cause: Human factor

Occupants & Outcome

Crew On Board

3

Passengers On Board

2

Estimated Survivors

5

Fatality Rate

0.0%

Known people on board: 5

Operational Details

Schedule / Flight

New York - Brussels

Flight Type

Cargo

Flight Phase

Takeoff (climb)

Crash Site

Airport (less than 10 km from airport)

Region / Country

North America • United States of America

Aircraft Details

Aircraft

Douglas DC-8

Registration

N730PL

MSN

46161

Year of Manufacture

1971