Tag Archives: Aircraft Accident

10 May 1911

Second Lieutenant George E.M. Kelly, United States Army. (SDASM)

10 May 1911: Second Lieutenant George Edward Maurice Kelly, 30th Infantry Regiment, United States Army, was killed during his primary pilot qualification flight at Fort Sam Houston, Texas.

Kelly had been sent to San Diego, California, in January 1911 as one of three U.S. Army officers to attend Glenn H. Curtiss’ Curtiss School of Aviation, newly established on North Island. After three months of training he was sent to Texas where the Army had set up its own training field.

Lieutenant Kelly was flying the Army’s second airplane, S.C. No. 2, a Curtiss Model D Type IV. The airplane had been accepted just two weeks earlier.

Curtiss Type IV Model D, S.C. No. 2, 1911. (U.S. Air Force)
Curtiss Model D Type IV, S.C. No. 2, 1911. (U.S. Air Force)

The New York Times reported in its 11 May 1911 issue:

LIEUT. KELLY KILLED; HIS AIRSHIP WRECKED;

Army Airman Suffers Fractured Skull in Fall at San Antonio and Dies and Hour Later.

CARTER AND STAFF PRESENT

Only Up Five Minutes When Mishap in Control Equipment prevented His Shutting Off Power.

Special to The New York Times

SAN ANTONIO, Texas, May 10.—Second Lieut. George E.M. Kelly of the United States Signal Corps, one of four army aviators on duty with the division of regulars mobilized here, was killed this morning when a Curtiss aeroplane he was flying got beyond control, after which it ran through the air for over a hundred yards, and crashed to the ground, burying Lieut. Kelly in its wreckage.

The machine was reduced to splinters, the only parts of it left intact being the engine and the rear plane work. Lieut. Kelly suffered a fractured skull and died in the Fort Sam Houston Hospital an hour later. He never regained consciousness. The accident happened about 7:30 this morning, in full view of Gen. Carter and his staff and hundreds of soldiers.

The exact cause of the accident will probably never be known, although a board of officers from the Signal Corps who investigated the accident are of the opinion that it was due to a break in some part of the controlling mechanism, making it impossible for Kelly to shut off the power when he realized his peril.

The accident happened about one hundred yards from Gen. Carter’s headquarters. The young officer had been in the air about five minutes, and Major Squier, Chief Signal Corps officer, had commented on the fine flight he was making, when the aviator pointed his machine downward for the purpose of making a landing. The machine was going at a speed estimated at between forty and fifty miles an hour. It shot down, apparently under perfect control, and landed a few feet away from one of the main driveways that intersect the mobilization camp. Kelly could be seen working frantically at the steering wheel as the machine descended, and when it struck the ground everybody breathed a sigh of relief, believing the officer was safe.

But the unexpected happened. The machine ran along the ground for ten or fifteen yards and then the fork into which is fitted the front wheel struck some obstruction and a moment later the propeller began to revolve at a wild speed. It could be seen that the left part of the machine was absolutely beyond the control of the aviator. It suddenly shot forward several yards, and then ascended to an altitude of between fifteen and twenty feet. It darted through the air in the direction of the Eleventh Infantry camp, tumbling and rolling like a wounded bird. The officer could be seen working the broken controller, but those who witnessed the sight say that at no time did he have a chance to escape with his life.

The machine gave a last tumble in the air and fell with a crash to the ground. Kelly was pitched out just as it started downward. The aviator and the machine struck the ground at the same instant.

Photograph o fteh accident scene at Fort San Antonio, published in the San Antonio Express, 11 May 1911.
Photograph of the accident scene at Fort San Antonio, published by the San Antonio Express, 11 May 1911.

Major Squier, Lieut. Foulois, Frank Coffyn, the Wright aviator, and a trooper were the first to reach the side of the dying aviator, whose skull was crushed. He lay under the wreckage of one of the planes, his face to the ground. The ambulance came up a moment later. Lieut. Foucar of the Medical Corps, in charge of the ambulance, examined Lieut. Kelly and informed Major Squier that he was mortally hurt.

By this time the Third Cavalry galloped up and formed a cordon around the place where Kelly lay dying. Lieut. Foucar, aided by troopers, picked him up and hurried him to the hospital, where Major Hutton, the Chief Surgeon, after examining him said there was no chance to save his life. An hour and ten minutes later he died.

Others new when Kelly was killed, besides Gen Carter, were Col. Stephen Mills, Chief of Staff; Lieut. Col. Ladd, the Adjutant General, and Col. Birmingham, Col. Straub, Capt. Leonard and Capt. Craig, all of the division staff. The whole camp knew of the accident within a few minutes after it had happened, and on all sides the deepest feelings of regret were expressed for the unfortunate aviator, who was one of the most popular members of the army corps.

Major General George Owen Squier, Signal Corps, United States Army.
Major General George Owen Squier, Signal Corps, United States Army.

As soon as order was restored Major Squier appointed a board of three signal officers to investigate the accident. Lieut. Paul W. Beck, chief of the corps, was President of the board, the other members being Lieut. Fulois and Lieut. Walker. After a hearing that lasted several hours they reported that atmospheric conditions were good at the time of the accident, that Kelly’s first landing was a good one, and that the cause of the accident was due to a break in some part of the control equipment which made impossible the management of the engine and planes. The report has been forwarded to Gen. Allen, Chief of the Signal Corps, in Washington.

The accident to Lieut. Kelly is the third within the last ten days. All of them befell the same Curtiss aeroplane in which Kelly was flying. Lieut. Walker figured in the first accident. On that occasion, in making a turn, the machine got out of his control and fell 150 feet before it righted itself. Lieut. Beck was the victim of the next accident.  He fell over 200 feet and landed in a mesquite tree. The machine was badly wrecked. When Lieut. Kelly went up this morning it was the first time the machine had been in the air since its mishap with Lieut. Beck.

Second Lieutenant George E.M. Kelly, U.S. Army, at Curtiss School of Aviation, North Island, San Diego, California, ca. April 1911. (George Hammond Curtiss Historical Society)
Second Lieutenant George E.M. Kelly, U.S. Army, at Curtiss School of Aviation, North Island, San Diego, California, ca. April 1911. (San Diego Air and Space Museum Archives)

Lieut. Kelly came to San Antonio about six weeks ago with Lieuts. Beck and Walker. All had been receiving instruction from Glenn H. Curtiss at San Diego, Cal., and had certificates from Mr. Curtiss testifying that they were capable aviators. When the Curtiss machine arrived several weeks ago Eugene Ely, one of the Curtiss aviators, was sent here to look after the instruction of Lieuts. Beck, Kelly, and Walker, who had been assigned to fly the machine. Ely left ten days ago to fulfill some exhibition engagements, and is not due back until May 14.

Speaking of the accident this afternoon, Major Squier said that, in his opinion, it was unavoidable.

“Lieut. Kelly,” he added, “was one of the best men in the Signal Corps. He was a quiet, unassuming fellow, devoted to his work, and gave every promise of becoming one of the army’s most valuable aviators. However, we must all remember that an aviator’s life is one in which the danger phase must be considered. Orders have been issued forbidding further flying for the next few days.”

Lieut. Kelly was a native of England and joined the army in 1904 as a private in the Coast Artillery. He held every non-commissioned rank from Corporal to Sergeant, and was commissioned a Second Lieutenant in the Thirtieth Infantry in 1907. He was unmarried and is said to have a sister living in New York City. His parents are believed to be in England.

Lieut. Kelly was the second army officer to be killed in an aeroplane. The other was Lieut. Thomas B. Selfridge, who fell with Orville Wright at Fort Myer, Va., in September, 1908.

The New York Times, 11 May 1911, Page 2. (The photographs are from other sources and were not part of the original New York Times article.)

Second Lieutenant George Edward Maurice Kelly was the second U.S. Army aviator killed in an airplane accident, however he was the first pilot killed while flying the airplane. His remains were interred at the San Antonio National Cemetery, San Antonio, Texas.

In 1916, the Army replaced the air field at Fort San Antonio with a new field on the opposite side of the city. The new airfield was initially named Camp Kelly, then Kelly Field. In 1948, it was renamed Kelly Air Force Base.

Main Gate, Kelly Field, circa 1916. (U.S. Air Force)
Main Gate, Kelly Field, circa 1916. (U.S. Air Force)

© 2019, Bryan R. Swopes

6 May 1937

Airship D-LZ129 Hindenburg moored at New Jersey at the end of a previous voyage.
Airship D-LZ129 Hindenburg moored at New Jersey at the end of a previous voyage.

6 May 1937: After a three-day Trans-Atlantic crossing from Frankfurt, Germany, the rigid airship Hindenburg (D-LZ129) arrived at Lakehurst, New Jersey, with 36 passengers and 61 crewmembers.

Airship LZ-129 Hindenburg burning, 1925 hours, 6 May 1937, at Lakehurst, New Jersey.
Airship LZ-129 Hindenburg burning, 1925 hours, 6 May 1937, at Lakehurst, New Jersey.

At 7:25 p.m., while the airship was being moored, it suddenly caught fire. The fabric covering burned first, but then the hydrogen gas contained in the buoyancy tanks exploded and burned. Hindenburg settled to the ground and was completely destroyed within 30 seconds.

Water ballast rains down as Hindenburg burns at the mooring mast 1925 hours, 6 May 1937, at Lakehurst, New Jersey. SFA003016395
Hindenburg NY Daily News
Hindenburg settles to the ground. (Arthur Cofod, Jr./USAF 12293 A.C.)

Of those on board, 13 passengers and 22 crewmembers died. One member of the ground crew was also killed.

Surprisingly, though there were many survivors and witnesses—as well as newsreel footage of the accident—the cause has never been determined.

This dramatic accident ended the airship passenger industry.

Airship LZ-129 Hindenburg burning, 1925 hours, 6 May 1937, at Lakehurst, New Jersey.
Airship LZ-129 Hindenburg burning, 1925 hours, 6 May 1937, at Lakehurst, New Jersey.
Hindenburg burning
Wreckage of Hindenburg, photographed the following day.

© 2015, Bryan R. Swopes

4 May 1949

Fiat G.212CP I-ELCE. (Wikimedia Commons)

4 May 1949: At 5:04 p.m., Central European Time (16:04 UTC), a chartered Avio Linee Italiane Fiat G.212CP airliner, I-ELCE, was descending in very poor weather conditions for landing at the Aeroporto di Torino-Aeritalia (ICAO: LIMA). The flight crew was using a Non-Directional Beacon (NDB) to align itself with the airport’s Runway 28. This beacon provided no vertical course (“glide slope”) guidance.

The airliner crashed into a wall of the Basilica di Superga, located on a 672 meter (2,205 feet) hill east of Turin, and 12 kilometers (7.5 miles) from the runway. All 31 persons on board, the 4-man crew, and 27 passengers, were killed.

Most of the passengers were members of the Grande Torino football club (soccer, as it is known in the United States).

Wreckage of Fiat G.212CP I-ELCE at the Basilica di Superga, Turin, Italy. (Wikipedia)

I-ELCE was a Fiat G.212CP, serial number 5. The G.212 is an all-metal, three-engine, low-wing monoplane with retractable landing gear. The crew consists of a pilot and co-pilot, a flight engineer and a radio operator. It could carry up to 34 passengers. Originally a military transport, the G.212A, the G.212CP variant was produced as a commercial airliner. There was also a cargo version, the G.212TP.

The G.212CP is 75 feet, 8 inches (23.063 meters) long with a wing span of 96 feet, 3 inches (29.337 meters) and overall height of 26 feet, 8 inches (8.128 meters). It has an empty weight of 24,742 pounds (11,223 kilograms) and maximum gross weight of 38,440 pounds (17,436 kilograms).

The G.212CP is powered by three 1,829.4-cubic-inch-displacement (29.978 liter) air-cooled, supercharged, Pratt & Whitney Twin Wasp S1C3-G two-row, 14-cylinder radial engines. These were rated at 1,200 horsepower at 2,700 r.p.m. at Sea Level for takeoff. The maximum continuous rating for normal operation was 1,050 horsepower at 2,550 r.pm., up to 7,500 feet (2,286 meters). Each engine drives a three-bladed constant-speed propeller through a 16:9 gear reduction. The S1C3-G is 48.19 inches (1.224 meters) long, 61.67 inches (1.566 meters) in diameter, and weighs 1,465 pounds (665 kilograms).

The G.212CP has a cruise speed of 160 knots (184 miles per hour/296 kilometers per hour), and maximum speed of 210 knots (242 miles per hour/389 kilometers per hour) at 12,100 feet (3,688 meters). Its service ceiling is 24,600 feet (7,498 meters), and its maximum range is 1,620 nautical miles (1,864 statute miles/3,000 kilometers).

The G.212 was produced from 1947 to 1950. The total number built is variously reported as 19 to 26.

The Basilica di Superga

Thanks to regular This Day in Aviation reader Paolo Nocilli for suggesting this topic.

© 2024, Bryan R. Swopes

3 May 1948

One of the three Douglas D-558-I Skystreaks. (Smithsonian Institution National Air and Space Museum, NASM A4958D)

3 May 1948: At Muroc Air Force Base in the high desert of southern California (after 1949, known as Edwards AFB), NACA 141, the second of three Douglas D-558-I Skystreak research aircraft, took off on a test flight to study stability at transonic speeds. In the cockpit was National Advisory Committee for Aeronautics Engineering Test Pilot Howard Clifton (“Tick”) Lilly. It was his twentieth flight in the Skystreak.

As Lilly climbed through 200 feet (61 meters), the Skystreak’s J35 turbojet engine suffered a catastrophic compressor failure. Fragments of the compressor cut through the airplane’s flight controls. With Lilly unable to control the airplane, it yawed to the left, then rolled over, and at 3:04 p.m., Pacific Daylight Saving Time (22:04 UTC), crashed onto Rogers Dry Lake. Lilly was decapitated in the crash.

Howard C. Lilly was the first NACA test pilot to be killed during a test flight since the commission had been established in 1915.

NACA Engineering Test Pilot Howard Clifton Lilly. (National Aeronautics and Space Administration )
Howard C. Lilly

Howard Clifton Lilly was born 27 August 1916 at Crow, West Virginia. He was the fourth of five children of Ova Ashton Lilly, a locomotive engineer, and Amanda Elmira Bragg Lilly.

Lilly was given the nickname, “Tickie,” by a friend who, as a child, had been unable to pronounce his middle name, Clifton.

Lilly attended Beaver Elementary School. He graduated from Shady Spring High School, and then attended Beckley College (now, the West Virginia University Institute of Technology), both in Beckley, West Virginia. He also studied at the Concord State Teachers College at Athens, WV (now, Concord University).

Lilly began flying at Mount Hope Airport in Beckley as a member of the Civilian Pilot Training Program. His flight instructor was Karl Williams.

Howard C. Lilly registered for Selective Service (conscription) on 16 October 1940. He was described as having a ruddy complexion with brown hair and blue eyes. Lilly was 5 feet, 10½ inches (179.1 centimeters) tall and weighed 150 pounds (68 kilograms). He was employed as a pressman for the Beckley Newspaper Corporation, and later in the stereotyping department of the Charleston Gazette.

Aviation Cadet Howard C. Lilly, USNR. (Tooley-Myron Studios)

Howard C. Lilly enlisted in the United States Navy as a seaman second class, 11 September 1941, at Washington, D.C. As part of the Navy’s V-5 Program, Seaman Lilly was assigned to U.S. Naval Reserve Aviation Base at Anacostia, D.C., for Elimination Flight Training. He was then transferred to the Naval Reserve Air Base, New Orleans, Louisiana. Although Lilly had hoped to fly fighters, he was assigned to fly seaplanes.

Aviation Cadet Lilly requested to be discharged from the Navy. His request was approved and he was discharged 18 September 1942.

Lilly joined the National Advisory Committee for Aeronautics (NACA) as a test pilot at the Langley Memorial Aeronautical Laboratory, Hampton, Virginia, in October 1942. He was then assigned to the Lewis Flight Propulsion Laboratory, Cleveland, Ohio, in May 1943.

Mrs. H. Clifton Lilly (Raleigh Register)

Howard C. Lilly married Miss Arline Eveyn Grentzer, 20 July 1945, at the St. James Rectory in Cleveland. The ceremony was officiated by Rev. George R. Betting. Following their wedding, the couple resided at the Westlake Hotel in Cleveland. They divorced in 1947.

On 1 September 1946, Lilly flew a Bell P-63A Kingcobra, 42-69063, in the Thompson Trophy Race at Cleveland. His airplane, with civil registration NX69901 and carrying race number 64, had qualified for the race in eighth place with an average speed of 346.155 miles per hour (557.083 kilometers per hour). He finished in ninth place at an average speed of 328.154 miles per hour (528.113 kilometers per hour). Bell Aircraft test pilot Tex Johnston won the race in his Bell P-39Q Airacobra with an average speed of 373.908 mph (601.746 kilometers per hour).

Howard Clifton Lilly, NACA engineering test pilot, with his 1946 Thompson Trophy racer, Bell P-63A NX69901. (NASA E-49-0091)

In August 1947, Lilly was assigned to NACA’s Muroc Flight Test Unit at Muroc Air Force Base as the commission’s first permanently assigned engineering test pilot there. He first flew the Bell XS-1 rocketplane on 9 January 1948. On 31 March 1948, Lilly flew the XS-1 to Mach 1.10, becoming just the third pilot to break sound barrier. Lilly made six test flight in the XS-1, all in the number two aircraft, 46-063.

Bell X-1 46-063. (NASA E49-001)

On 29 April 1948, Lilly flew the D-558-I to 0.88 Mach at 36,000 feet (10,973 meters). This was the highest speed that a Skystreak had reached up to that time.

Howard Clifton Lilly’s remains were interred at the Arlington National Cemetery. Lilly Avenue at Edwards AFB was named in his honor.

In May 1950, Lilly was posthumously awarded the Air Medal.

One the the three Douglas D-558-I Skystreaks in flight near Muroc Air Force Base. (Naval Aviation Museum)

NACA 141 (U.S. Navy Bureau of Aeronautics serial number 37971) was the second of three Douglas D-558-I Skystreak transonic research aircraft.

The D-558 Program was intended as a three-phase test program for the U.S. Navy and the National Advisory Committee on Aeronautics (NACA) to investigate transonic and supersonic flight using straight and swept wing aircraft powered by turbojet and/or rocket engines.

The Douglas Aircraft Company designed and built three D-558-I Skystreaks and three D-558-II Skyrockets. The Phase I aircraft were flown by Douglas test pilot Gene May and the Navy’s project officer, Commander Turner Caldwell.

Cutaway illustration of the Douglas D-558-I Skystreak. (U.S. Navy)

The D-558-I Skystreak was a single-engine, turbojet-powered airplane. It was built of magnesium and aluminum for light weight, but was designed to withstand very high acceleration loads. It was 35 feet, 8 inches (10.871 meters) long with a wingspan of 25 feet (7.62 meters) and overall height of 12 feet, 1¾ inches (3.702 meters). The airplane had retractable tricycle landing gear. Its empty weight was approximately 7,500 pounds (3,400 kilograms), landing weight at the conclusion of a flight test was 7,711 pounds (3,498 kilograms). The maximum takeoff weight was 10,105 pounds (4,583.6 kilograms). The aircraft fuel load was 230 gallons (870.7 liters) of kerosene.

The D-558-I was powered by a single Allison J35-A-11 turbojet engine. The J35 was a single-spool, axial-flow turbojet with an 11-stage compressor section, 8 combustion chambers and single-stage turbine. The J35-A-11 was rated at 5,000 pounds of thrust (22.24 kilonewtons). The engine was 12 feet, 1.0 inches (3.683 meters) long, 3 feet, 4.0 inches (1.016 meters) in diameter and weighed 2,455 pounds (1,114 kilograms). The J35-A-11 was a production version of the General Electric TG-180, initially produced by Chevrolet as the J35-C-3. It was the first widely-used American jet engine.

Cutaway illustration of J35 turbojet engine. (General Electric)

The D-558-I had a designed service ceiling of 45,700 feet (13,930 meters). Intended for experimental flights of short duration, it had a very short range and took off and landed from Rogers Dry Lake at Muroc. The experimental airplane was not as fast as the more widely known Bell X-1 rocketplane, but rendered valuable research time in the high transonic range.

The three D-558-I Skystreaks made a total of 229 flights.

Douglas test pilot Gene May (left) and Howard C. Lilly with the number two Douglas D-558-I Skystreak, Bu. No. 37971, at Muroc, circa 1948. (NASA E95-43116-8)

© 2023, Bryan R. Swopes

19 April 2006

Albert Scott Crossfield, Jr., with the Victor Black Edition Continental engine overhauled by Victor Aviation of Palo Alto, California.
Albert Scott Crossfield, Jr., with the Victor Black Edition Continental IO-470-E engine installed in his Cessna 210A, N6579X. The engine was overhauled by Victor Aviation of Palo Alto, California. (Victor Aviation)

19 April 2006: Former experimental test pilot Albert Scott Crossfield, Jr., was enroute from Prattville, Alabama, to Manassas, Virginia. Crossfield was flying his personal Cessna 210A, N6579X. The Cessna was cruising at 11,000 feet (3,353 meters) under Instrument Flight Rules (IFR), and under the control of the Atlanta Air Route Traffic Control Center (ARTCC).

During the flight, he encountered a Level 6 thunderstorm.

Crossfield requested to deviate from his planned course to avoid the severe turbulence. Atlanta Center authorized his request and he began to turn. Approximately 30 seconds later, at 11:10 a.m., radar contact was lost near Ludville, Georgia. The last indication was that the Cessna was descending through 5,500 feet (1,676 meters).

The wreckage of N6579X was located the following day by a Civil Air Patrol search team, 3.3 nautical miles (6.1 kilometers) northwest of Ludville at an elevation of 1,269 feet (386.8 meters) above Sea Level. [N. 34° 30.767′, W. 84° 39.492′] The airplane had descended through the forest canopy nearly vertically and created a crater approximately 4½ feet (1.4 meters) deep and 6 feet (1.8 meters) across. Albert Scott Crossfield’s body was inside.

Scott Crossfield’s 1962 Cessna 210A Centurion, photographed at Santa Monica Airport, California, 26 September 1999. (AirNikon Collection, Pima Air & Space Museum, Tucson, Arizona, via airliners.net. Image used with permission.)

N6579X was a Cessna Model 210A, serial number 21057579, built in 1960 by the Cessna Aircraft Company, Inc., of Wichita Kansas. It was a six-place, single-engine, high-wing monoplane with external struts to brace the wings, and retractable, tricycle landing gear. The airplane was certified for instrument flight by a single pilot. At the time of the crash, N6579X had been flown 4,987.4 hours, total time since new (TTSN).

The Cessna 210A was 28 feet, 2 inches (8.585 meters) long with a wingspan of 36 feet, 6 inches (11.125 meters) and overall height of 9 feet, 7 inches (2.921 meters). The airplane had an empty weight of 1,839 pounds (834.2 kilograms) and maximum gross weight of 2,900 pounds (1,315.4 kilograms). It had a fuel capacity of 65 gallons (246 liters), with 10 gallons (37.9 liters) unusable, and 12 quarts of engine oil (11.4 liters).

N6579X was powered by an air-cooled, fuel-injected, 471.239-cubic-inch-displacement (7.722 liters) Teledyne Continental IO-470-E horizontally-opposed six-cylinder direct-drive engine with a compression ratio of 8.6:1. The engine was rated at 260 horsepower at 2,625 r.p.m. for takeoff, using 100LL aviation gasoline. It weighed 429 pounds (195 kilograms). This engine, serial number 77583-0-E, was original to the airplane and accumulated 4,987.4 hours, total time since new (TTSN). It had been overhauled by Victor Aviation, Palo Alto, California, 1,259.8 hours prior to the accident (TSO). A three-bladed McCauley constant-speed propeller with a diameter of 6 feet, 10 inches (2.083 meters) was installed in 2005.

The Cessna Model 210A has a maximum structural cruise speed (VNO) of 175 miles per hour (282 kilometers), and maximum speed (VNE) of 200 miles per hour (322 kilometers per hour). Maneuvering speed, which should be used in turbulent conditions, is 130 miles per hour (209 kilometers per hour). The 210A has a maximum rate of climb of 1,300 feet per minutes (6.6  meters per second) and service ceiling of 20,700 feet (6,309 meters). Its maximum range is 1,284 miles (2,066 kilometers).

Albert Scott Crossfield, Jr., aeronautical engineer and test pilot, 1921-2006. (Jet Pilot Overseas)

Albert Scott Crossfield, Jr., was born 2 October 1921 at Berkeley, California. He was the second of three children of Albert Scott Crossfield, a chemist who was employed as the superintendant of the Union Oil Company refinery in Wilmington, California, and Lucia M. Dwyer Crossfield.

When he was five years old, young “Scotty” contracted pneumonia. He was comatose for a while and was not expected to survive, but after several weeks he began to recover. A year later, he again became seriously ill, this time with rheumatic fever. He was confined to total bed rest for four months, and continued to require extensive bed rest until he was about ten years old. It was during this time that he became interested in aviation.

Scott Crossfield attended Boistfort Consolidated School, southwest of Chehalis, Washington, graduating in 1939, and then studied engineering at the University of Washington until taking a job at Boeing in late 1941. During this time, Scotty learned to fly in the Civilian Aviation Training Program.

The week following the attack on Pearl Harbor and the United States’ entry into World War II, Scott Crossfield enlisted as an aviation cadet in the United States Army Air Corps. After numerous delays, he joined the United States Navy on 21 February 1942, and resigned from the Air Corps. He began aviation cadet training at NAS Sand Point, near Seattle, and then was sent to NAS Corpus Christi, Texas. In December 1942, he graduated, received his gold Naval Aviator wings and was commissioned as an Ensign, United States Naval Reserve.

Ensign Crossfield was assigned to NAS Kingsville, near Kingsville, Texas, as an advanced bombing and gunnery instructor.

In April 1943 at Corpus Christi, Texas, Ensign A. Scott Crossfield married Miss Alice Virginia Knoph of Seattle. They would have nine children.

Ensign Crossfield served as a gunnery instructor for two years. He was promoted to Lieutenant (junior grade), 1 March 1944. In 1945 he was transferred to Air Group 51 in the Hawaiian Islands, which was preparing for the invasion of Japan. Crossfield was promoted to Lieutenant, 1 August 1945, while serving aboard the Independence-class light aircraft carrier USS Langley (CVL-27). With the end of World War II, though, the Navy was cutting back. Lieutenant Crossfield was released from active duty 31 December 1945.

Following the War, Scotty returned to the University of Washington to complete his degree. He took a part time job operating the University’s wind tunnel. At the same time, he remained in the Naval Reserve, assigned to VF-74, a fighter squadron which flew both the Grumman F6F Hellcat and Chance Vought F4U Corsair out of NAS Sand Point, back where his naval career began.

Chance Vought F4U-4 Corsair, Bu. No. 82034, assigned to Fighter Squadron 74 (VF-74). (United States Navy)

Crossfield graduated from the University of Washington with a bachelor’s degree in aeronautical engineering in June 1949, and a master’s degree in 1950.

In 1950 Crossfield joined the National Advisory Committee for Aeronautics (NACA) as a research test pilot at the High-Speed Flight Station, Edwards Air Force Base, California. He flew the Republic YF-84, F-84F Thunderstreak, and North American Aviation F-86 Sabre. Crossfield made 25 flights in the delta-winged Convair XF-92A, which he described as “the worst flying airplane built in modern times.” He also flew the Northrop X-4 and Bell X-5. He made 17 flights conducting stability tests in the Douglas D-558-1 Skystreak. Scotty made 65 flights in the North American Aviation F-100A Super Sabre, including a test series which discovered a fatal flaw which led to the death of North American’s chief test pilot, George S. Welch.

NACA Research Test Pilot Albert Scott Crossfield in the cockpit of the Douglas D-558-II Skyrocket after exceeding Mach 2, 20 November 1953. (NASA)

Crossfield is known as a rocketplane pilot. He made 10 flights in the Bell X-1, 89 in the Douglas D-558-II Skyrocket, and 14 in the North American Aviation X-15. He became the first pilot to exceed Mach 2 when he flew the Skyrocket to Mach 2.005, 20 November 1953.

Scott Crossfield discusses the X-15 with North American Aviation engineers Edmond R. Cokeley and Charles H. Feltz. (North American Aviation, Inc.)

Crossfield flew for NACA for approximately five years. During that time, approximately 500 flights were made at Edwards by NACA test pilots. Scott Crossfield flew 181 of them.

Scott Crossfield left NACA in 1956 to join North American Aviation, Inc., as chief engineering test pilot for the X-15 project. Between 8 June 1959 and 6 December 1960, he made fourteen flights in the X-15. He reached a maximum speed of Mach 2.97 and altitude of 88,116 feet (26,858 meters). Once the contractor’s flight tests were completed and the rocketplane turned over to the U.S. Air Force and NACA, the customers’ test pilots, Joe Walker and Major Robert M. White, took over.

Albert Scott Crossfield made 113 flights in rocket-powered aircraft, more than any other pilot.

After completing his work on the X-15, Crossfield followed Harrison (“Stormy”) Storms, who had been the Chief Engineer of North American’s Los Angeles Division (where the X-15 was built) to the Space and Information Systems Division in Downey, California, where he worked in quality assurance, reliability engineering and systems testing for the Apollo Command and Service Modules and the Saturn S-II second stage.

Crossfield left North American at the end of 1966, becoming Vice President for Technological Development for Eastern Air Lines. In this position, he flew acceptance tests for new Boeing 720 and 727 airliners at Boeing in Seattle.

In The X-15 Rocket Plane, author Michelle Evans quoted Crossfield as to why he had not entered NASA’s space program as an astronaut:

    One question that pressed was, with his love of flight and the early responsibility of going into space with the X-15, why would Scott not apply to the NASA astronaut office? He explained, “[Dr.] Randy Lovelace and General [Donald] Flickinger were on the selection board. They took me to supper one night and asked me not to put in for astronaut. I asked them, ‘Why  not?’ and they said, ‘Well, we’re friends of yours. We don’t want to have to turn you down.’ I asked, ‘Why would you have to turn me down?’ and they said, ‘You’re too independent.’ “

The X-15 Rocket Plane: Flying the First Wings into Space, by Michelle, Evans, University of Nebraska Press, 2013, Chapter 1 at Page 33.

The remains of Albert Scott Crossfield are interred at the Arlington National Cemetery.

Scott Crossfield is in the cockpit of X-15 56-6670, under the right wing of NB-52A 52-003. (NASA)

© 2017, Bryan R. Swopes