Narrative:JAL Flight 46E departed Anchorage about 12:24 local time. The flight release/weather package provided to the pilots by Evergreen operations contained a forecast for severe turbulence and indicated that severe turbulence was reported by other large airplanes. As flight 46E taxied onto the runway to await its takeoff clearance, the local controller informed "the flightcrew that the pilot of another
Evergreen B-747 reported severe turbulence at 2,500 feet while climbing out from runway 06R.
After takeoff, at an altitude of about 2,000 feet, the airplane experienced an uncommanded left bank of approximately 50 degrees. While the desired air speed was 183 knots, the air speed fluctuated about 75 knots from a high of 245 knots to a low of 170 knots. Shortly thereafter, the flightcrew reported a "huge" yaw, the No. 2 throttle slammed to its aft stop, the No. 2 reverser indication showed thrust reverser deployment, and the No. 2 engine electrical bus failed. Several witnesses on the ground reported that the airplane experienced several severe pitch and roll oscillations before the engine separated. Shortly after the engine separated from the airplane, the flightcrew declared an emergency, and the captain initiated a large radius turn to the left to return and land on runway 06R. The No. 1 engine was maintained at
emergency/maximum power. While on the downwind portion of the landing pattern, bank angles momentarily exceeded 48 degrees, alternating with wings level. About 12:45, flight 46E advised the tower that they were on the runway.
Probable Cause:
PROBABLE CAUSE: "The lateral separation of the No. 2 engine pylon due to an encounter with severe or possibly extreme turbulence that resulted in dynamic multi-axis lateral loadings that exceeded the ultimate Iateral load-carrying capability of the pylon, which was already reduced by the presence of the fatigue crack near the forward end of the pylon's forward firewall web."
Accident investigation:
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Investigating agency: | NTSB  |
Status: | Investigation completed |
Duration: | 196 days (7 months) | Accident number: | NTSB/AAR-93/06 | Download report: | Final report
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Classification:
Turbulence
Engine separation
Forced landing on runway
Sources:
» Air Safety Week 7:14 5 April 1993 (5)
» NTSB Safety Recommendations A-94-9 and -10
» NTSB/AAR-93/06
Follow-up / safety actions
NTSB issued 10 Safety Recommendations
Issued: 20-JUL-1992 | To: FAA | A-92-58 |
DEVELOP A BROADER METEOROLOGICAL AIRCRAFT HAZARD PROGRAM TO INCLUDE OTHER AIRPORTS IN OR NEAR MOUNTAINOUS TERRAIN, BASED ON THE RESULTS OBTAINED IN THE COLORADO SPRINGS, COLORADO, AREA. (Closed - Acceptable Action) |
Issued: 15-NOV-1993 | To: FAA | A-93-136 |
DEVELOP AND IMPLEMENT A METEOROLOGICAL PROGRAM TO OBSERVE, DOCUMENT, AND ANALYZE POTENTIAL METEOROLOGICAL AIRCRAFT HAZARDS IN THE AREA OF ANCHORAGE INTERNATIONAL AIRPORT, ANCHORAGE, ALASKA, WITH AN EMPHASIS ON THE APPROACH AND DEPARTURE PATHS OF THE AIRPORT. (Closed - Unacceptable Action) |
Issued: 15-NOV-1993 | To: FAA | A-93-137 |
AMEND THE DESIGN LOAD REQUIREMENTS OF 14 CFR PART 25 TO CONSIDER MULTIPLE AXIS LOADS ENCOUNTERED DURING SEVERE TURBULENCE. (Closed - Unacceptable Action) |
Issued: 15-NOV-1993 | To: FAA | A-93-138 |
REQUIRE THE BOEING-PROPOSED B-747 ENGINE PYLON STRUCTURAL MODIFICATION PROGRAM TO INCLUDE INCREASING THE LATERAL LOAD CAPABILITY OF THE PYLON STRUCTURE. (Closed - Acceptable Action) |
Issued: 15-NOV-1993 | To: FAA | A-93-139 |
REQUIRE ANY FUTURE STRUCTRUAL MODIFICATIONS OF EXISTING ENGINE PYLONS TO CONSIDER MULTIPLE AXIS LOADING. (Closed - Unacceptable Action) |
Issued: 15-NOV-1993 | To: FAA | A-93-140 |
ISSUE AN AIRWORTHINESS DIRECTIVE TO REQUIRE COMPLIANCE WITH BOEING SERVICE BULLETIN 747-54-2160. (Closed - Exceeds Recommended Action) |
Issued: 15-NOV-1993 | To: FAA | A-93-141 |
CONSIDER THE NECESSITY AND FEASIBILITY OF REQUIRING THE MODIFICATION OF THE AIRCRAFT DEPARTURE ROUTES AT ANCHORAGE INTERNATIONAL AIRPORT DURING PERIODS OF MODERATE OR SEVERE TURBULENCE TO MINIMIZE THE POTENTIAL OF AIRCRAFT ENCOUNTERING MOUNTAIN-INDUCED LOW LEVEL TURBULENCE. (Closed - Acceptable Action) |
Issued: 15-NOV-1993 | To: National Weather Service | A-93-142 |
USE THE WSR-88D DOPPLER WEATHER RADAR SYSTEM AT ANCHORAGE, ALASKA, TO DOCUMENT MOUNTAIN-GENERATED WIND FIELDS IN THE ANCHORAGE AREA AND TO DEVELOP IN GREATER DETAIL LOW ALTITUDE TURBULENCE FORECASTS. (Closed - Acceptable Action) |
Issued: 31-JAN-1994 | To: FAA | A-94-10 |
REVIEW THE SERVICE EXPERIENCE OF OTHER TYPES OF AIRPLANES TO DETERMINE IF SIMILAR INSPECTIONS OF THE ENGINE MOUNT STRUCTURES SHOULD BE CONDUCTED FOLLOWING ENCOUNTERS WITH SEVERE TURBULENCE IN WHICH THE AIRPLANE EXPERIENCES LARGE VARIATIONS IN ROLL AND YAW ATTITUDE. (Closed - Acceptable Action) |
Issued: 31-JAN-1994 | To: FAA | A-94-9 |
ISSUE AN AIRWORTHINESS DIRECTIVE TO REQUIRE THAT THE MIDSPAR FUSE PINS ON BOEING 747 AIRPLANES BE REMOVED AND INSPECTED FOR DEFORMATION FOLLOWING AN ENCOUNTER WITH SEVERE TURBULENCE IN WHICH THE AIRPLANE EXPERIENCES LARGE VARIATIONS IN ROLL AND YAW ATTITUDE, AS PROVIDED IN THE BOEING COMMERICAL AIRPLANE COMPANY\'S PROPOSED MODIFICATIONS TO THE BOEING 747 MAINTENANCE MANUAL, SECTIONS 5-51-03 AND 5-51-06. (Closed - Acceptable Action) |
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Photos

accident date:
31-03-1993type: Boeing 747-121
registration: N473EV

accident date:
31-03-1993type: Boeing 747-121
registration: N473EV
Map
This map shows the airport of departure and the intended destination of the flight. The line between the airports does
not display the exact flight path.
Distance from Anchorage International Airport, AK to Chicago-O'Hare International Airport, IL as the crow flies is 4534 km (2834 miles).
This information is not presented as the Flight Safety Foundation or the Aviation Safety Network’s opinion as to the cause of the accident. It is preliminary and is based on the facts as they are known at this time.