# National Airlines Flight 27

National Airlines Flight 27 was a scheduled passenger flight between Miami, Florida, and San Francisco, California, in the United States, with intermediate stops at New Orleans, Houston and Las Vegas.
On November 3, 1973, the aircraft involved, a McDonnell Douglas DC-10-10 with the tail number N60NA (as Barbara), experienced an uncontained engine failure, causing significant damage to the plane. The aircraft later managed to make a safe emergency landing at the Albuquerque International Sunport. One passenger died after being ejected from the aircraft at cruising altitude, in addition to minor injuries sustained by twenty-four passengers. It was the first fatal accident involving a DC-10.

## Flight crew

The captain of Flight 27 was William R. Broocke, aged 54, who had been employed by National Airlines since 1946 and had qualified to fly the McDonnell Douglas DC-10 in 1972, accumulating 21,853 flight hours during his career with 801 hours on the DC-10. First Officer Edward H. Saunders, aged 33, had been employed by National Airlines since 1965, with 7,086 flight hours of which 445 hours were on the DC-10. Flight Engineer Golden W. Hanks, aged 55, employed by National Airlines since 1950, with 17,814 flight hours of which 1,252 flight hours were on the DC-10.

## Incident

On November 3, 1973, Flight 27 took off from Houston, Texas, bound for Las Vegas International Airport. The aircraft leveled off at 39,000 feet (12,000 m) with an indicated airspeed of about 300 knots (350 mph; 560 km/h).
At about 16:40 MST, while the aircraft was at cruising altitude, 65 miles (56 nmi; 105 km) southwest of Albuquerque, New Mexico, the No. 3 (starboard) engine fan assembly disintegrated in an uncontained catastrophic failure. Smoke was reported to fill the cabin before the fragments of the fan assembly penetrated the fuselage, the numbers 1 and 2 engine nacelles and the right wing at high speeds, causing a cabin window to dislodge and eject the adjacent passenger from the aircraft. The resultant damage caused decompression of the cabin and the loss of certain electrical and hydraulic systems.
The flight crew initiated an emergency descent, and the aircraft landed safely at Albuquerque International Sunport nineteen minutes after the engine failed. 115 passengers and 12 crew members exited the aircraft by using the evacuation slides. The plane was returned to service with National Airlines after repairs (being renamed Suzanne) and was later flown by Pan Am (as Clipper Meteor).

## Casualties

Of the 116 passengers on board, 24 people were treated by medical personnel from nearby Kirtland Air Force Base for smoke inhalation, ear problems and minor abrasions.
One passenger was partially blown into the opening made by the failed cabin window, after it too was struck by engine fragments. He was temporarily retained in that position by his seatbelt. "According to a witness...efforts to pull the passenger back into the airplane by another passenger were unsuccessful, and the occupant of seat 17H was subsequently forced entirely through the cabin window."
The New Mexico State Police and local organizations searched extensively for the missing passenger, George F. Gardner of Beaumont, Texas, who was blown out of the window. Computer analysis was made of the possible falling trajectories, which narrowed the search pattern. However, the search effort was unsuccessful. A ranch hand later found a pair of sunglasses and a tobacco pipe while working on a ranch near Alamo, New Mexico. He turned over the items to state police, where the family of the missing passenger identified them as belonging to him.

## Investigation

The National Transportation Safety Board (NTSB) determined the probable cause of this accident was the disintegration of the No. 3 engine fan assembly as a result of an interaction between the fan blade tips and the fan case. According to the NTSB, "the precise reason or reasons for the acceleration and the onset of the destructive vibration could not be determined conclusively", but enough was learned to prevent the occurrence of similar events. The speed of the engine at the time of the accident caused a resonance wave to occur in the fan assembly when the tips of the fan blades began to make contact with the surrounding shroud. The engine was designed to have a rearward blade retaining force of 18,000 pounds (8,200 kg) to prevent the blades from moving forward in their mountings slots and subsequently departing from the fan disk. The rearward force was not enough. As a result of this accident, General Electric re-designed the engine so that the blade retaining capability was increased to 60,000 pounds (27,000 kg), and that change was incorporated into all engines already in service.
In addition to this, it was found that between August 8 and September 12, 1973, there had been fifteen problems reported about the third engine. The engine had been taken off the aircraft for repairs, and between the time it was replaced and the accident, a further twenty-six faults had been reported by the flight crew. It was found that the bolts that had held the front covering in place, which had failed in the accident, were outside the tolerances laid down. An engineering dispatch was sent out to inspect these engines, and six more discrepancies were found in the National Airlines fleet alone. Therefore, this dispatch was made compulsory for all early DC-10s in order to prevent the issue from occurring again.
The NTSB expressed concern about the flight crew conducting an unauthorized experiment on the auto-throttle system. They had been wondering where the system took its engine power readings from and, to see if it was the N1 tachometer readout, "the flight engineer pulled the three N1 tachometers [circuit breakers]" and then adjusted the autothrottle setting. The cockpit voice recorder showed that the engines altered their power setting when requested, proving to the crew that the system was powered from another source. The crew then manually reset the throttles to the normal cruising power before the flight engineer had closed the tachometer circuit breakers. It was considered whether the crew had accidentally over-sped the engine when setting power without the tachometers, but there was insufficient evidence to deliver a certain verdict. Nonetheless, "regardless of the cause of the high fan speed at the time of the fan failure, the Safety Board is concerned that the flight crew was, in effect, performing an untested failure analysis on this system. This type of experimentation, without the benefit of training or specific guidelines, should never be performed during passenger flight operations."