Louisville-Winston County

On August 14, 2013, about 0447 central daylight time (CDT), UPS flight 1354, an Airbus A300-600, N155UP, crashed short of runway 18 during a localizer non precision approach to runway 18 at Birmingham-Shuttlesworth International Airport (BHM), Birmingham, Alabama. The captain and first officer were fatally injured, and the airplane was destroyed by impact forces and postcrash fire. The scheduled cargo flight was operating under the provisions of 14 Code of Federal Regulations Part 121 on an instrument flight rules flight plan, and dark night visual flight rules conditions prevailed at the airport; variable instrument meteorological conditions with a variable ceiling were present north of the airport on the approach course at the time of the accident. The flight originated from Louisville International Airport-Standiford Field, Louisville, Kentucky, about 0503 eastern daylight time. A notice to airmen in effect at the time of the accident indicated that runway 06/24, the longest runway available at the airport and the one with a precision approach, would be closed from 0400 to 0500 CDT. Because the flight's scheduled arrival time was 0451, only the shorter runway 18 with a non precision approach was available to the crew. Forecasted weather at BHM indicated that the low ceilings upon arrival required an alternate airport, but the dispatcher did not discuss the low ceilings, the single-approach option to the airport, or the reopening of runway 06/24 about 0500 with the flight crew. Further, during the flight, information about variable ceilings at the airport was not provided to the flight crew.

The pilot received a weather briefing before departure and when near the destination airport, cleared for the NDB approach. The pilot reported the procedure turn inbound; published MDA is 1,300 feet msl. Witnesses on the airport reported heavy low fog and heard the pilot announce over the UNICOM frequency, 'Oh there is fog rolling into Starkville too?' One of the witnesses advised the pilot they could go to another airport due to the fog; the pilot responded he would execute the approach. The witnesses heard the engines operating at full power then heard the impact and saw a fireball. The airplane impacted the runway inverted, slid across the runway, and came to rest in grass off the runway. A post crash fire destroyed the airplane. Tree contact approximately 972 feet northwest of the runway impact location separated approximately 51 inches of the left wing. Examination of the engines, propellers, and flight controls revealed no evidence of preimpact failure or malfunction. The pilot had twice failed his airline transport pilot checkride. The designated examiner of the second failed flight test indicated the pilot was marginal in all flight operations. The NDB was checked after the accident; no discrepancies were noted.

The pilot and two mechanics were on a maintenance test flight. As the aircraft was on a straight-in approach to runway 11 from the west, the pilot was advised of traffic ahead and told to slow his speed as much as possible. The pilot acknowledged. About 15 seconds later, the controller told the pilot (of N63XL) to make a 360° turn to the left for spacing. Shortly hereafter, witnesses observed the aircraft enter a steep bank (turn), then go into a steep spiraling, nose down, descent and crash. No preimpact mechanical malfunction or failure of the aircraft or engines was found. All three occupants were killed.