21 May 1949: Captain Hubert Dale Gaddis, Field Artillery, United States Army, flew a prototype Sikorsky S-52-1 helicopter, serial number 52003, registration NX92824, to a Fédération Aéronautique Internationale (FAI) World Record for Altitude Without Payload of 6,468 meters (21,220 feet) over Bridgeport, Connecticut. ¹ The flight was observed by National Aeronautic Association representatives Walter Goddard and Charles Logsdon.
The Sikorsky S-52-1 was a completely new design based on the company’s experience with the earlier R-4 and R-5/S-51 models. It was a two-place light helicopter of all metal monocoque construction, using primarily aluminum and magnesium. With Sikorsky test pilot Harold Eugene (“Tommy”) Thompson at the controls, the prototype made its first flight 4 May 1948.
The three-bladed fully-articulated articulated main and two-bladed tail rotor were also of all metal construction. The main rotor had a diameter of 33 feet (10.058 meters) and rotated counter-clockwise as seen from above. (The advancing blade is on the right side of the helicopter.) It had an extruded aluminum spar, covered with sheet duralumin, riveted and glued in place. The blade used a NACA 0012 airfoil with -6° twist. The two-bladed semi-rigid tail rotor was mounted on the left side of the tail boom in a pusher configuration. It had a diameter of 6 feet, 4 inches (1.930 meters) and rotated counter clockwise, as seen from the helicopter’s left. (The advancing blade is at the top of the tail rotor arc.)
The S-52-1 was powered by an air-cooled, normally-aspirated, 425.29-cubic-inch-displacement (6.97 liter) Franklin Engine Company 6V6-245-B16F (O-425-1) vertically-opposed 6-cylinder overhead valve engine. The engine was rated at 245 horsepower at 3,275 r.p.m.
On 27 April 1949 Tommy Thompson flew the same helicopter to an FAI speed record of 208.49 kilometers per hour (129.55 miles per hour) over a 3 kilometer straight course at Cleveland, Ohio, ² and on 6 May, to 197.54 kilometers per hour (122.75 miles per hour) over a 100-kilometer course between Milford and Westbrook, Connecticut. ³
Hubert Dale Gaddis was born in Jasper County, Missouri, 9 September 1920, the first of two children of Hubert E. Gaddis, a utility company purchasing agent, and Beatrice Mae Cook Gaddis.
The family trelocated to Tulsa, Oklahoma, where Hubert attended Central High School. While there, he developed an interest in radio. Gaddis graduated in 1938.
Gaddis married Martha Tucker in 1950. They would have three children,Cheryl, Sandra and Dale.
Gaddis enlisted in the United States Army in Oklahoma, 24 September 1942. He had brown hair and hazel eyes, was 5 feet, 6 inches (1.68 meters) tall and weighed 133 pounds (60.3 kilograms).
Gaddis was commissioned a second lieutenant, Army of the United States (AUS), 18 February 1944. He remained in the Army following World War II as an officer in the Field Artillery (Regular Army). In 1956, he graduated of the Army Command and General Staff College.
On September 8 1966, Gaddis was promoted to the rank of colonel (temporary). The rank became permanent 1 July 1971. He was released from military service 28 February 1974. During his career, Colonel Gaddis had been awarded the Distinguished Flying Cross, the Bronze Star Medal, and the Air Medal with 14 oak leaf clusters (15 awards).
Colonel Hubert Dale Gaddis, United States Army (Retired) died 24 February 1976 at the age of 55 years. He was buried at Woodlawn Memorial Gardens, Ozark, Alabama.
In the years following World War II, Jacqueline Cochran, WASP organizer and instructor, test pilot, racer, record-setter, adviser to generals and presidents, owned three North American Aviation, Inc., P-51 Mustang fighters which had been modified for racing.
I. P-51B-15-NA 104-25789, 43-24760, NX28388, 1946–1948
[Note: NX28388 should not be confused with NC28388, which was a Douglas DC-3 twin-engine airliner, registered to the Douglas Aircraft Company, Inc., 1 October 1940.]
Jackie’s first Mustang was a P-51B-15-NA, U.S. Army Air Corps serial number 43-24760, with a civil experimental registration, NX28388. It was raced in the Bendix Trophy Race three times. Jackie also used it to set four world speed records over distances from 3 to 2,000 kilometers. NX28388 was painted “Lucky Strike Green” and carried the white race number 13 on each side of its fuselage.
43-24760 was manufactured at North American Aviation’s Inglewood, California, plant, completed on 14 March 1944. It was a Model NA-104 P-51B Mustang with manufacturer’s serial number 104-25789, one of 1,588 Mustangs contracted by the U.S. Army Air Corps on 20 October 1942. Its service history is not known, but the fighters built just before and after, 43-24759 and 43-24761, were flown by the 361st Fighter Group from bases in England. Both were lost in combat during the summer of 1944.
After the end of World War II, 43-24760, identified as a TP-51B, was sold back to North American Aviation, Inc., by the War Assets Administration. North American paid “$3,500.00, cash in hand” at Denver, Colorado, 24 May 1946.
Jackie Cochran bought 43-24760, now registered NX28388, from North American Aviation on 6 August 1946, for “ten dollars plus other consideration.” The Bill of Sale identifies the Mustang as a P-51B-15-NA, manufacturer’s serial number 25789. Its engine was a Packard V-1650-7, serial number V332415, a license-built version of the Rolls-Royce Merlin V-12.
NX28388 was inspected for an initial Airworthiness Certificate, 7 August 1946. It was required to be marked “EXPERIMENTAL” and limited to “INSTRUMENT DAY FLIGHT – For Racing and exhibition flight only.” This initial airworthiness certificate was valid for six months.
On 26 August 1946, the Civil Aviation Administration issued a certificate of ownership to Jacqueline Cochran, “dba Jacqueline Cochran Cosmetics” at her company’s Newark, New Jersey address. [Note: “dba” is an abbreviation for “doing business as”]
On 31 August 1946, Cochran flew NX28388 in the Bendix Air Race from Metropolitan Airport, Van Nuys, California, to Cleveland Municipal Airport, Cleveland, Ohio. Other long distance air racers had their wings modified to hold more fuel, but there hadn’t been time to modify NX28388. For this race, it carried two drop tanks manufactured for the Lockheed P-38 Lightning. Cochran placed 2nd to race winner Paul Mantz and his red P-51C NX1202, Blaze of Noon, who had finished with a time of 4:34:14 at an average speed of 435.501 miles per hour (700.871 kilometers per hour). Jackie’s elapsed time was 4:52:00, averaging 420.92 miles per hour (677.41 kilometers per hour). Mantz won the $10,000 prize for first place, and Jackie won a $5,500 prize.
The airplane received its next airworthiness inspection 19 August 1947. The report was signed by Louis S. Wait, Agent. Wait was the Administrative Test Pilot for North American Aviation, Inc. (Wait had made the first flight of AG345, the very first production Mustang Mk.I, on 23 April 1941.)
Cochran had entered the 1947 Bendix Trophy Race scheduled for 31 August, but her husband, Floyd Bostwick Odlum, became seriously ill. Jackie asked pilot Bruce Gimbel to fly her airplane. During the race, a problem with the propeller governor limited his speed. Gimbel finished in 4th place with an average speed of 404.080 miles per hour (650.304 kilometers per hour) and elapsed time of 5:04:10. (Paul Mantz won the race, again, winning the $10,000 prize.)
On 10 December 1947, Jackie flew NX28388 to set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a Closed Circuit of 100 Kilometers at Coachella, California, with an average speed of 755.668 kilometers per hour (469.549 miles per hour).
A week later, 17 December 1947, she flew her green Mustang to an FAI World Record for Speed Over a 3 Kilometer Straight Course, with an average speed of 663.054 kilometers per hour (412.002 miles per hour). The flight at Thermal, California, was flown at Sea Level.
On 22 May 1948, again flying NX28388, Cochran set a Fédération Aéronautique Internationale and a U.S. National Aeronautic Association Record for Speed Over a Closed Circuit of 2,000 Kilometers Without Payload with an average speed of 447.470 miles per hour (720.134 kilometers per hour) over a 1,242.7 mile course from Palm Springs, California to a point near Santa Fe, New Mexico, and return. Famed female aviator Katherine Stinson was the chief judge at the pylon turn west of Santa Fe. Jackie broke the previous record, 708.592 kilometers per hour (440.299 miles per hour), which had been set by Lieutenant John J. Hancock, U.S. Air Force, with a Lockheed P-80 Shooting Star jet fighter, two years earlier. (FAI Record File # 8941)
In an interview, Jackie said, “Last Saturday’s flight was for blood. I bought this P-51 two years ago and ever since have been fixing it up for the one objective of beating the Army’s jet 2,000 kilometer speed record. The Bendix Race and other flights were just incidental. I knew that I couldn’t beat the 1,000 kilometer jet record today, and I also new that I could establish a new record for planes powered with reciprocating engines, so I made things slightly easier on the engine and myself in today’s flight. But even so, considering the double climb that I had to make at the check point to be seen and timed by the judges, it would have been impossible over this shorter distance to equal the 448 miles per hour flown last Saturday.”
— WASP NEWSLETTER, July 1948, Volume V, Number Two, at Page 2.
Two days later, 24 May 1948, Jackie set another world and national record of 431.094 miles per hour (693.780 kilometers per hour) over a 1,000 kilometer (621.371 miles) closed circuit from Palm Springs to Flagstaff, Arizona, and return. This record broke her own record which she had set 6 April 1940, flying a Republic AP-7.
On 19 August 1948, NX28388 received another airworthiness inspection. The report was signed by J.E. Smith, Agent.
Jackie once again flew NX28388 in the 1948 Bendix Air Race from Long Beach, California, to Cleveland, Ohio. She placed third with an average speed of 445.847 miles per hour and an elapsed time of 4:35:07.3. Paul Mantz and Blaze of Noon won the race for a third consecutive time. Linton Carney, also flying a P-51C, took second place. Cochran’s P-51B finished just 1 minute, 19 seconds behind Mantz.
Following the 1948 race, Cochran asked a friend and Lockheed test pilot, Sampson Held of North Hollywood, California, to fly her P-51 racer back to California, but,
“. . . my plane crashed, carrying my associate, Sam Held, with it to his death.”
— The Stars At Noon, by Jacqueline Cochran, Little, Brown and Company, Boston, 1954, Chapter IV at Page 79.
NX28388 crashed six miles south of Sayre, Oklahoma, 8 September 1948, killing the pilot, Sampson Held. Two witnesses saw a wing come off of the Mustang, followed by an explosion.
II. P-51C-5-NT 103-26311, 42-103757, Beguine, NX4845N, 1949
North American Aviation P-51C-5-NT 42-103757 was one of a group of 1,350 Mustangs contracted by the U.S. Army Air Corps in August 1942. It was built at North American’s Dallas, Texas, plant, 25 April 1944. Its North American contract number was 103-26311. The fighter’s military service history is not known.
Immediately after the close of World War II, 6 October 1945, 42-103757 was transferred to the Reconstruction Finance Corporation (a Depression-era agency of the United States government) at Searcy Field (SWO), Stillwater, Oklahoma. On 19 February 1946, it was included in a group of 475 war surplus airplanes, including heavy and medium bombers and fighters, purchased by aviator Paul Mantz of Burbank, California. On the same day, Mantz resold 464 of these airplanes to a partnership of himself, J.W. Heath and L.P Hapgood, for $70,000. 42-103757 was one of 6 North American P-51Cs in this second group.
Mantz, Heath & Hapgood sold 42-103757 to Frank J. Abel, 3101 Sherwood Lane, Wichita Falls, Texas, for $1,500.00 on 21 July 1947. Abel registered the airplane with the Civil Aeronautics Administration and it was assigned registration number NX4845N.
On 10 July 1948, Frank Abel sold the P-51 to J.D. Reed Co., Inc., an aircraft sales dealership at Hangar 8, Municipal Airport, Houston, Texas, now known as William P. Hobby Airport (HOU). The Bill of Sale reported the purchase price as “one dollar and other consideration.” J.D. Reed Co., Inc., applied to the C.A.A. for registration of 42-103757 on the same date. However, a new C.A.A. Certificate of Registration was issued to Abel on 12 July 1948.
An annual airworthiness inspection of 42-103757 was completed by Paul E. Penrose, Pilot-Engineer, 20 August 1948, for the J.D. Reed Co., Inc. The report indicates that the P-51C was equipped with a Packard V-1650-9. This engine was rated at 1,380 horsepower at 3,000 r.p.m. The Airworthiness Certificate was approved in the Experimental category by C.A.A. Inspector Homer L. Stamets, 29 August 1948, and appropriate limitations were assigned.
During 1948–1949, 42-103757 was radically modified as an Unlimited Class air racer. The lower portion of the P-51’s fuselage was removed and faired over. The radiator and engine oil cooler which had been enclosed in the Mustang’s characteristic belly scoop were relocated to the wingtips. (The Air Force had experimented with a ramjet-powered P-51D, 44-63528. A Marquardt XRJ-30-MA ramjet was placed on each wingtip. The cooling pods on 42-103757 resemble these, though another source says that the cooling pods were made from modified FJ-1 Fury fuel tanks.) No reports of these modifications are found in the airplane’s records with the Federal Aviation Administration, however.
The airplane was named Beguine after a popular song of the time performed by Artie Shaw, Cole Porter’s “Begin the Beguine.” It was painted dark blue and the music from the song was painted in gold along the Mustang’s fuselage, with the race number 7.
The next annual inspection was completed 12 August 1949 by (H.C. Danaher?), Mechanic. The airworthiness certificate was approved by C.A.A. Inspector Ray K. Beckleman.
I bought a Bequine (sp)racing plane in 1949 on the insistence of Bill Odom, a young pilot, who wanted to use it in the Thompson Trophy pylon race in Cleveland. He agreed to take the old number off . . . and paint the lucky 13 in its place. Two days before the race he called me long distance to say that the plane’s paint job was so beautiful that it would be a shame to ruin it repainting a number 13.
— Jackie Cochran: An Autobiography, by Jacqueline Cochran and Maryann Bucknum Brinley, Bantam Books, New York, 1987, at Page 157.
For the 1949 National Air Races, Jackie Cochran bought Beguine for pilot William P. Odom to fly in the Sohio Trophy Race and the Thompson Trophy Race, both pylon races flown over a 15 mile, seven-turn course near the Cleveland Municipal Airport at Cleveland, Ohio
Odom had not flown in a pylon race before, but had gained fame for a number of record flights, including a 78 hour, 55 minute, 6 second around-the-world flight with co-pilot and navigator T. Carroll Sallee in a Douglas A-26 Invader, Reynolds Bombshell, 12–16 April 1947. Jackie also planned to fly Beguine herself in the 1950 Bendix Trophy Race.
Cochran purchased NX4845N from J.D. Reed Co., Inc., for “$10.00 & Other Valuable Considerations” on 22 August 1949. She submitted an Application for Registration to the Civil Aeronautics Administration, but it does not appear that a new Certificate of Registration was ever issued.
Bill Odom won the 105-mile (167 kilometer) Sohio Trophy Race with an average speed of 388.393 miles per hour (625.058 kilometers per hour).
The Thompson Trophy Race on 5 September 1949 was different. Odom had qualified Beguine with a speed 405.565 miles per hour (652.694 kilometers per hour).
At the start of the Thompson race, Odom quickly took the lead. But on the second lap, things went wrong. As it approached Pylon 4, Beguine rolled upside down and then crashed into a house near the airport, setting it on fire.
Air racer Steven Calhoun Beville, flying P-51D Mustang # 77 in the Thompson Race, the closest pilot to Beguine, said that Odom had cut inside Pylon No. 3 and was correcting toward Pylon 4 when the airplane rolled inverted.
[Beville’s Mustang, The Galloping Ghost, NX79111, is the same airplane involved in the catastrophic crash at the National Championship Air Races, Reno, Nevada, 16 September 2011.]
Newspapers reported the crash:
Beville, who finished third in the race, was the closest to Odom when he got in trouble.
“Bill was out too far on the third pylon,” Beville said, “and was trying to correct position too quickly. He turned over in the air and flew along on his back for a short distance, then dived right into a house.”
—The San Bernardino Daily Sun, Vol. LVI, No. 5, Tuesday, 6 September 1949, at Page 2, Column 7
In her autobiography, Jackie Cochran wrote, I was in the judges’ stand handling telephone reports from the back of the stands’ pylons when the flash came through that Bill had crashed. I jumped into a helicopter that was just in front of me on the field and went out to the spot of the accident hoping that something could be done. I found the house on fire, with Bill and the plane, as well as some of the occupants, buried in the wreckage. Some news photographer snapped a picture of me standing there close by. I am in that picture the personification of abject desolation. For three days I stayed in Cleveland doing all that I could to honor Bill Odom’s memory.
— The Stars At Noon, by Jacqueline Cochran, Little, Brown and Company, Boston, 1954, Chapter V at Page 96.
“The house” was a brand new single-family home, located at 429 West Street, Berea, Ohio. The owners, Mr. and Mrs. Bradley C. Laird, had moved in just four days earlier, along with their 5-year-old son, David. Their 13-month-old, Craig, had remained with Mrs. Laird’s parents, but her father, Benjamin J. Hoffman, had brought him to the house in Berea two days earlier.
Jeanne Laird was inside the house when Beguine crashed. She was killed instantly. Mr. Laird, Mr. Hoffman and David were outside watching the airplanes fly overhead, and Craig was in a playpen in the driveway. When the house exploded in flames, Mr. Hoffman rescued Craig, suffering severe burns in doing so. The infant was critically burned, and though Mr. Hoffman drove him to Berea Community Hospital, Craig Hamilton Laird died several hours later.
Bill Odom’s body was so badly burned that it could only be identified by his wristwatch.
“This is a terrible blow to aviation everywhere,” said Jacqueline Cochran, owner of the plane Odom was flying, when she got to the Laird home minutes after the accident. “My heart goes out to the innocent sufferers whose home this was.”
—Chicago Tribune, Vol. CVII–No. 214, Wednesday, 7 September 1949, at Page 1, Column 6.
III. P-51C 2925, NX5528N, THUNDERBIRD, 1949–1953
Having lost her first two Mustangs in tragic accidents, on 19 December 1949 Jackie Cochran bought another P-51 Mustang racer—the 1949 Bendix Trophy Race winner, Thunderbird—from the Academy Award-winning actor and World War II B-24 wing commander, James M. Stewart.
The earliest document in Thunderbird‘s Civil Aviation Administration file, Form ACA 132, contains the hand-written notation, “no service no.” The document states, “THIS AIRCRAFT WAS ASSEMBLED FROM COMPONENTS OF OTHER AIRCRAFT OF THE SAME TYPE.” The aircraft is designated on the form as a North American P-51C, Serial No. 2925.
Thunderbird, made up of salvaged parts, has no known Army Air Corps serial number. No North American Aviation contract number is listed in any document. It has no known history prior to the C.A.A. assigning it the civil registration NX5528N. The serial number 2925 does not conform to any U.S. Army Air Corps serial number sequence for P-51 series aircraft, nor does it conform to any N.A.A. contract number sequence for P-51s. It appears that this serial number was assigned to the P-51 by the Civil Aeronautics Administration.
Various sources attribute U.S.A.A.C. serial numbers to NX5528N, e.g., “43-6822” and “43-6859.” There is nothing in the airplane’s C.A.A. records to substantiate these claims. The record specifically states that there is “no service no.” Some sources also describe Thunderbird as a P-51B or an F-6C photo reconnaissance variant. C.A.A. records specifically identify the airplane as a P-51C.
Thunderbird‘s fuselage was purchased as “salvage & scrap” from the 803rd A.A.F. Specialized Depot, Park Ridge, Illinois, by Allied Aircraft Co., Chicago, Illinois. The transaction is dated 14 January 194_ (the year was left blank on the contract). The purchase price was $27.05. Allied Aircraft Co. was a partnership of Leland H. Cameron and Martha L. Cameron, 5300 W. 63rd Street, Chicago, Illinois.
On 11 February 1948, Cameron purchased a P-51, Serial No. 2925, registration N5528N, from J. Quaine, for $1.00. On 5 April 1948, the Civil Aeronautics Authority (predecessor to the Federal Aviation Administration) registered N5528N to L.H. Cameron, 4619 Sancola Avenue, North Hollywood, California.
Two days later, 7 April 1948, Leland Cameron sold N5528N to Joe De Bona Racing Co., 133 N. Robertson Boulevard, Beverly Hills, California. The purchase price listed on the Department of Commerce Bill of Sale was $10.00. On that date, Joe De Bona applied to have the airplane registered in the name of his racing company.
Interestingly, on De Bona’s Department of Commerce Application for Registration, the serial number of N5528N is listed as “21925.” Information on the application is typewritten with the exception of this serial number, which was handwritten. As above, 21925 does not conform to any Army Air Corps or North American Aviation serial number for P-51B or P-51C Mustangs. This is the only instance in which 21925 appears in the airplane’s C.A.A. records.
The Civil Aeronautics Administration registered N5528N to Joe De Bona Racing Co., 15 April 1948. Joe C. De Bona was an experienced air racer. The company was a partnership between De Bona and James M. (Jimmy) Stewart.
Over the next several months, N5528N, now named Thunderbird, was prepared for the upcoming 1948 Bendix Trophy Race. Unnecessary equipment such as the self-sealing fuel cells, the fuselage fuel tank, etc., were removed to save weight. The airframe seams were filled with putty and sanded smooth. Many coats of primer were applied followed by the the high-gloss “cobalt blue” paint. Gold decorative trim was applied. Thunderbird‘s airworthiness category, EXPERIMENTAL, was painted under the canopy rail on each side. Sponsors’ logos and crew member’s names were painted on the left side of the fuselage beneath the canopy. (The significance of the anvil logo with the numbers “1853” is not known.) The rudder was painted in a checkerboard pattern and the race number 90 applied to both sides of the fuselage. The registration was painted vertically on the fin, the top of the right wing and the bottom of the left wing.
On 31 August 1948, following an airworthiness inspection, C.A.A. Inspector Homer L. Stamets issued an original Airworthiness Certificate to NX5528N. The “Experimental” classification was used as there was no civil Type Certificate for North American’s P-51 fighters, and the C.A.A. had not tested or accepted the aircraft for any civilian use. The Experimental classification placed severe restrictions on De Bona’s use of Thunderbird. In the Operations Authorized section of the certificate it states, “Certificated for the purpose of Racing and Exhibition flights only; flights limited to the Continental limits of the UNITED STATES. Flights prohibited over thickly populated areas or large gatherings of people.” The certificate was valid for one year.
Noted on the Airworthiness Inspection form is that NX5528N was equipped with a Packard V-1650-3 engine. This license-built version of the Rolls-Royce Merlin 63 engine was standard equipment for early production P-51B and P-51C Mustangs. It was rated at 1,380 horsepower at 3,000 r.p.m. and 60 inches of manifold pressure.
The start of the 1948 Bendix Trophy Race took place on 4 September at Van Nuys, California. Joe De Bona was entered with Thunderbird, but was unable to complete the race. Reportedly low on fuel, he landed at Norwalk, Ohio. (As noted above, Jackie Cochran placed 3rd in this race flying NX28388.)
For 1949 Thunderbird‘s engine was upgraded to a Packard V-1650-7. C.A.A. Inspector Stamets again approved its airworthiness inspection and issued another one-year Experimental certificate with same restrictions as previously.
The start of the 1949 Bendix Trophy Race was relocated from Metropolitan Airport at Van Nuys to Rosamond Dry Lake, 40 miles (64.4 kilometers) north of Muroc Air Force Base (renamed Edwards AFB just two months later). This year Joe De Bona was successful. He won the 2,008 mile (3,231.6 kilometers) race to Cleveland, Ohio in an elapsed time of 4:16:17.5, averaging 470.136 miles per hour (756.611 kilometers per hour.) Paul Mantz did not fly in the race but entered two P-51Cs, flown by Stanley H. Reaver and Herman “Fish” Salmon, who placed 2nd and 3rd.
(Leland Cameron, who had sold N5528N to Joe De Bona Racing, also competed in the 1949 Bendix air race. He flew a Martin B-26C-20-MO Marauder medium bomber, serial number 41-35071, N5546N, but he did not finish within the prescribed time limit.)
On 19 December 1949, James Stewart (Sole Owner, for Joe De Bona Racing Co.) sold N5528N to Jacqueline Cochran of Indio, California, for “$1.00 and other consideration.” The C.A.A. issued a new Certificate of Registration to Jackie on 29 December 1949.
That same day Jackie Cochran flew her new airplane, Thunderbird, to two Fédération Aéronautique Internationale (FAI) World Records for Speed Over a 500 kilometer Closed Circuit Without Payload, and a U.S. National Aeronautic Association record, with an average speed of 703.275 kilometers per hour (436.995 miles per hour). (FAI Record File Numbers 4476, 12323)
Thunderbird underwent another airworthiness inspection, completed 10 November 1950 by Patrick J. Kavanaugh, A&E 402226. C.A.A. Inspector H.W. Kattleman issued a new Experimental airworthiness certificate, valid from 10 November 1950 to 10 November 1951. The limitations were identical to the restrictions described above.
Jackie set another Fédération Aéronautique Internationale record on 9 April 1951, flying NX5528N to an average speed of 747.338 kilometers per hour (464.374 miles per hour) over a straight 16 kilometer (9.942 miles) course at Indio, California. (FAI Record File Number 4477)
The next airworthiness inspection of N5528N was completed 26 March 1952 by mechanic James N. Smith. Once again, C.A.A. Inspector H.W. Kattleman issued an Experimental airworthiness certificate, valid from 31 March 1952 to 31 March 1953.
Jackie Cochran had owned Thunderbird for just over three years when, on 20 January 1953, she sold it back to Jimmy Stewart for “$1.00 and other consideration.” The C.A.A. registered N5528N to Stewart at 141 El Camino Drive, Beverly Hills, California, 9 April 1953.
Thunderbird received another engine upgrade, this time to a Packard V-1650-9, serial number V381230. (This engine was rated at 1,380 horsepower at 3,000 r.p.m., but could produce a maximum 2,280 horsepower with water-alcohol injection.) The next airworthiness inspection was completed 31 March 1953 by a mechanic with certificate number M-17807. At the time of this inspection, N5528N had accumulated 76:00 hours total flight time (TTAF). The V-1650-9 engine had only 14:10 hours since new. C.A.A. Aviation Safety Agent Ralph C. Olsen approved the next airworthiness certificate.
On 30 March 1954, another airworthiness inspection was completed by the same mechanic as the 1953 periodic inspection. Once again, the airworthiness certificate was approved by Ralph Olsen. Total flight time for N5528N was now 118:00 hours, with 42:50 on the Merlin engine.
At about this time, N5528N was repainted in a yellow and black scheme, and renamed Mr. Alex in honor of Jimmy Stewart’s father, Alexander Maitland Stewart.
A major event of 1953 was the Coronation of Elizabeth II on 2 June. American television networks CBS and NBC had arranged to have films of the ceremonies flown across the Atlantic to Newfoundland. From there the film would be flown on to the United States by Jimmy Stewart’s P-51 and another owned by Paul Mantz, NX1204, flown by Stanley Reaver.
Jimmy Stewart asked the C.A.A. to temporarily remove the limitations on NX5528N’s airworthiness certificate so that it could be flown out of the United States to pick up the films at Newfoundland and return with them to Boston, Massachusetts. C.A.A. Aviation Safety Agent Ralph C. Olsen approved this request. A second flight to Montreal, Canada was also authorized. The restrictions would resume when the Experimental category Mustang returned to the United States after the Montreal trip.
Joe De Bona was once again in the cockpit of N5528N. He arrived at Boston 24 minutes before his rival, Stan Reaver, but a third network, ABC, was actually the first to broadcast the films of the Coronation.
On 1 September 1954, Jimmy Stewart sold N5528N to Joe De Bona for $1.00 plus a $7,500.00 Chattel Mortgage. On 14 March 1954, the C.A.A. registered the airplane, which they now designated as a North American F-51C, to De Bona at 339 North Beverly Drive, Beverly Hills, California.
An airworthiness inspection was completed 17 March 1955. The mechanic performing the inspection held certificate number M7427. The V-1650-9 had been removed and replaced with a Packard V-1650-300, serial number V350012. This post-war commercial engine was rated at 1,660 horsepower at 3,000 r.p.m. The airframe now had 150:00 hours TTAF, and the new engine had 30:00 hours.
The following day, 18 March 1955, Joe De Bona sold N5528N to James M. Cook of Jacksboro, Texas, for $18,000 plus a $7,000 Chattel Mortgage at 4% interest, payable on or before 1 January 1956. The C.A.A. issued a Certificate of Registration to Cook on 31 March 1955.
On 22 June 1955, North American Aviation P-51C Mustang NX5528N crashed near Scott’s Bluff, Nebraska, while being flown by James Cook. Although an official cause is not available, anecdotally, one of the P-51’s main landing gear failed to retract and Cook bailed out. Although an accident report was completed 13 July 1955, the Federal Aviation Administration currently has no report in its files, nor does the National Transportation Safety Board. The Mustang was deregistered 15 August 1955. (James Cook soon bought another Mustang, P-51D N71L, which he flew for several years as part of the U.S. Weather Bureau’s Thunderstorm Research Airplane Project.)
Warren A. Piestch of Pietsch Aircraft Restoration and Repair, Inc., Minot, North Dakota, purchased a tail wheel assembly and other parts from a wrecked P-51 located in Nebraska, 23 June 1999. He wrote to the F.A.A. and stated that these parts were from P-51 serial number 2925, and that he wanted to rebuild the aircraft. Pietsch requested that ownership of 2925 be assigned to him and that a registration N-number that he had previously reserved, N151LP, be assigned to the airplane. The F.A.A. did as Pietsch requested. This registration was valid until 30 April 2015. The status of Mr. Pietsch’s restoration is not known, and how much of the original Thunderbird he has salvaged, if any, is also not known.
IV. NORTH AMERICAN AVIATION, INC., P-51B and P-51C MUSTANG FIGHTERS
The North American Aviation P-51 Mustang is a single-place, single-engine long range fighter. It is a low-wing monoplane with retractable landing gear and is of all-metal construction. The fighter is powered by a liquid-cooled V-12 engine. It was originally produced for the United Kingdom’s Royal Air Force as the Mustang Mk.I. Two examples were provided to the U.S. Army Air Corps, designated XP-51. This resulted in orders for the P-51A and A-36 Apache dive bomber variant. These early Mustangs were powered by the Allison V-1750 engine driving a three-bladed propeller, which also powered the Lockheed P-38 Lightning and Curtiss P-40 Warhawk.
In 1942, soon after the first production Mustang Mk.I arrived in England, Rolls-Royce began experimenting with a borrowed airplane, AM121, in which they installed the Supermarine Spitfire’s Merlin 61 engine. This resulted in an airplane of superior performance.
In the United States, the Packard Motor Car Company of Detroit, Michigan, had begun building Merlin engines under license from Rolls-Royce. These American engines were designated V-1650. North American modified two P-51s from the production line to install the Packard V-1650-3. These were designated XP-51B. Testing revealed that the new variant was so good that the Army Air Corps limited its order for P-51As to 310 airplanes and production was changed to the P-51B.
The P-51B and P-51C are virtually Identical. The P-51Bs were built by North American Aviation, Inc., at Inglewood, California. P-51Cs were built at North American’s Dallas, Texas plant. They were 32 feet, 2.97 inches (9.829 meters) long, with a wingspan of 37 feet, 0.31-inch (11.282 meters) and overall height of 13 feet, 8 inches (4.167 meters) high. The fighter had an empty weight of 6,985 pounds (3,168 kilograms) and a maximum gross weight of 11,800 pounds (5,352 kilograms).
P-51Bs and Cs were powered by a right-hand tractor, liquid-cooled, supercharged, 1,649-cubic-inch-displacement (27.04-liter) Packard V-1650-3 or -7 Merlin single overhead cam (SOHC) 60° V-12 engine which produced 1,380 horsepower at Sea Level, turning 3,000 r.p.m at 60 inches of manifold pressure (V-1650-3) or 1,490 horsepower at Sea Level, turning 3,000 r.p.m. at 61 inches of manifold pressure (V-1650-7). (Military Power rating, 15 minute limit.) These were license-built versions of the Rolls-Royce Merlin 63 and 66. The engine drove a four-bladed Hamilton Standard Hydromatic constant-speed propeller with a diameter of 11 feet, 2 inches (3.404 meters) through a 0.479:1 gear reduction.
The P-51B/C had a cruise speed of 362 miles per hour (583 kilometers per hour) and the maximum speed was 439 miles per hour (707 kilometers per hour) at 25,000 feet (7,620 meters). The service ceiling was 41,900 feet (12,771 meters). With internal fuel, the combat range was 755 miles (1,215 kilometers).
In military service, armament consisted of four Browning AN/M2 .50-caliber machine guns, mounted two in each wing, with 350 rounds per gun for the inboard guns and 280 rounds per gun for the outboard.
1,988 P-51B Mustangs were built at North American’s Inglewood, California plant and another 1,750 P-51Cs were produced at Dallas, Texas. This was nearly 23% of the total P-51 production.
23 October 1934: At Lago di Garda, Brescia, Italy, Warrant Officer Francesco Agello, Regia Aeronautica, set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 3 Kilometer Course when he flew the Macchi Aeronautica M.C. 72 float plane, serial number MM 181, to an average speed of 709.21 kilometers per hour (440.68 miles per hour).¹
A contemporary news article described the event:
FLYING the Machi-Castoldi 72 seaplane (3,000 h.p. special 24-cyl. Fiat) at Lake Garda on Tuesday of last week, Warrant-Officer Francesco Agello, of the Italian Royal Air Force, raised his own world’s air speed record by putting up a mean speed (subject to homologation) of 709.202 km./hr. (440.677 m.p.h.) for the usual four flights. His previous record stood at 682.403 km./hr. (423.76 m.p.h.)
The weather conditions under which the attempts were made were ideal, there being just sufficient breeze to take the glassiness off the water, so assisting the takeoff. Temperature was suitable, and the air was free from bumps.
Just before 3 p.m. Agello took off and made four runs over the three-kilometre course, clocking as follows:—
After the successful attempt a banquet was held in the Officers’ Mess at Desenzano in Agello’s honour. The speeds were announced, and Col. Bernasconi, who is in command of the High-speed Flight, stated that Signor Mussolini had honoured Warrant-Officer Agello by promoting him to a full lieutenant.
Only a few modifications had been made to the Macchi-Castoldi since the previous attempt, chief among them being the substitution of wooden floats for the metal ones previously used.
As is well known. the most interesting feature of the machine is the extremely unconventional power-unit, the Fiat A.S.6. The problem of frontal area for such a powerful unit as was specified was solved by placing the twenty-four cylinders (totalling in capacity over fifty litres) in two rows, forming a 60 deg. “vee,” and further, arranging them in two mechanically independent groups.
Each group has its own crank shaft, but a single crank case is used for both. The crank shafts, which rotate in opposite directions, are coupled in the centre by spur-gear reduction units, which drive two airscrew shafts. One of these shafts is hollow, and the other operates within it. The two shafts run forward through the “vee” of the front unit, and each carries an airscrew; so that there are two of the latter, close together, but revolving in opposite directions.
Each engine unit has independent camshafts (two per engine), water pump and dual Marelli magnetos, but a common induction system is used, an eight-jet carburetter being mounted behind the rear unit and mixture being drawn from it passed to the cylinders by a supercharger geared up to 20,000 r.p.m. An interesting point is that this supercharger absorbs 200 h.p., and, since it is driven by the rear engine, the blades of the front airscrew (which the rear engine drives) are given different inclination to correct for the slight difference in power.
The power units develop 3,000 h.p. at 3,200 r.p.m., and weighs 2,045lb., giving a weight per h.p. of 0.706lb. The all-up weight of the machine, with pilot and full tanks, is 6,670lb.
British equipment figured in the success, for Castrol oil and K.L.G. plugs were used.
— FLIGHT, The Aircraft Engineer and Airships, No. 1349, Vol. XXVI, November 1, 1934, at Page 1152.
The Macchi-Castoldi M.C.72 was designed by Mario Castoldi for Aeronautica Macchi. It was a single-place, single-engine, low-wing monoplane float plane constructed of wood and metal. It was 8.32 meters (27 feet, 3.5 inches) long with a wingspan of 9.48 meters (31 feet, 1.25 inches) and height of 3.30 meters (10.83 feet). The M.C.72 had an empty weight of 2,505 kilograms (5,512 pounds), loaded weight of 2,907 kilograms (6,409 pounds) and maximum takeoff weight of 3,031 kilograms (6,669 pounds).
It was powered by a 50.256 liter (3,067 cubic inch) liquid-cooled, supercharged Fiat S.p.A. AS.6 24-cylinder 60° dual overhead cam (DOHC) V-24 engine with 4 valves per cylinder. The engine produced 3,100 horsepower at 3,300 r.p.m. and drove two counter-rotating metal two-bladed fixed pitch propellers with a diameter of 8 feet (2.56 meters). The counter-rotating blades cancelled the torque effect of the engine.
Surface radiators were placed on top of each wing and surface oil coolers on the floats.
Five Macchi M.C.72 float planes had been built for the 1931 Schneider Trophy race, but problems with the Fiat AS.6 engine, which was essentially two AS.5 V-12s assembled back-to-back, prevented them from competing.
Four test pilots, including Francesco Agello, had been selected to fly the airplanes for speed record attempts. Two were killed while testing the M.C.72, and the third died when another airplane crashed. The cause of the accidents were explosions within the engines’ intake tract. Though they ran perfectly on test stands, in flight, they began to backfire, then explode.
It was discovered by Rod Banks, a British engineer who had been called in to develop a special high-octane fuel, that the Fiat engineers had overlooked the ram effect of the 400 mile per hour slipstream. This caused the fuel mixture to become too lean, resulting in predetonation and backfiring. A modification was made to the intake and the problem was resolved.
Francesco Agello was twice awarded the Henry De La Vaulx Medal by the Fédération Aéronautique Internationale, and also awarded the Medaglia d’oro al valore aeronautico. In part, his citation read, “A high speed pilot of exceptional courage and, after competition in difficult and dangerous test flights during the development of the fastest seaplane in the world, twice he conquered the absolute world speed record.”
Captain Agello was killed in a mid-air collision, 26 November 1942, while testing a Macchi C.202 Fogore fighter.
13 September 1935: Flying his Hughes H-1 Special, NR258Y, Howard Robard Hughes, Jr. set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 3 Kilometer Course near Santa Ana, California. Making seven passes over the measured course, each in opposite directions, his average speed was 567.12 kilometers per hour (352.39 miles per hour).¹ This was 61.27 kilometers per hour (38.07 miles per hour) faster than the previous record, set by Raymond Delmotte, 25 December 1934, flying a Caudron C.460 Rafale.²
Just after completing the final pass over the course, the airplane’s engine stopped due to fuel starvation. Hughes made a belly landing in a farm field. He was uninjured and the airplane received only minor damage.
The Los Angeles Times reported:
HUGHES WINS SKY RECORD AND CRASHES
Death Escaped in Mishap
Millionaire Flyer Forced Down After Averaging 347 Miles and Hour
Howard Hughes, Millionaire sport flyer, missed death by a narrow margin yesterday morning a few seconds after he brought back to the United States the world’s speed mark for land planes when he averaged 347 miles an hour near Santa Ana.
Official confirmation of the new mark must await calibration of the speed over the measured three-kilometer course, bordering the Eddie Martin Airport, by the Federation Aeronautic Internationale of Paris, France. The figures are to be submitted following a conference between officials of the National Aeronautics Association and representatives of the California Institute of Technology.
“I don’t expect any difficulty in having Hughes’s speed marks officially allowed,” said William R. Enyart, official timer, shortly after the mystery racing plane made a forced landing in a beet field and ploughed a furrow for sixty yards.
Hughes had just completed his seventh lap against the former world record of 314.319 miles an hour, held by Raymond Delmotte of France, when he suddenly lifted the silver monoplane into the air as his fourteen-cylinder Wasp radial air-cooled engine sputtered.
The pilot sought altitude, climbing to 500 feet. Then he turned and headed for the beet field, his engine stopped.
DEAD STICK LANDING
Despite his landing speed of about eighty miles and hour, Hughes made a perfect “dead stick” landing as the ship flattened out on its lower side and slid through the soft ground. A bent propeller and wrenched landing gear were the only visible damage.
“My gas supply in one tank was exhausted,” Hughes said as he stepped unhurt from the racer. When I switched on the other tank the motor didn’t take it. An air lock—pressure built up from the dry tank—had developed in the line and the only thing I could do was attempt a forced landing.”
Hughes received the congratulations of numerous officials gathered to witness the assault on the speed record for his manipulation of the speedy ship and the perfect landing. Amelia Earhart, who had been flying as an observer, was one of the first to praise the pilot.
“The stoppage in gas came so suddenly, Hughes said, “that I did not have time to lower the retractable landing gear. It was only partially down when the plane hit. The force drove it back into the ship and probably aided in preventing additional damage.”
SERIES OF CHECKS
Six record-breaking tests were made as Hughes streaked over the course. An electronic chronograph photographed and clocked each flight. Four are required to officially set a new speed mark.
Determination of Hughes to make his second record-breaking attempt early yesterday morning came as a surprise and after he and his assistants had spent the night checking over difficulties faced in the flight late Thursday afternoon.
Hughes rolled his $120,000, 1000-horsepower, low-winged monoplane from the hangar at Union Air Terminal shortly after daylight and awaited word from officials at the measured course that all was in readiness.
At 6:30 a.m. he flashed into the air and an hour and ten minutes later had made his successful seven flight when halted by the gas supply stoppage.
Hughes and associates announced that the next speed record he will attempt to break in his specially constructed racer will be the flight from Los Angeles to New York. The present time, 10 hours and 2 minutes, is held by Col. Roscoe Turner.
SCENE OF FLIGHT
The record-breaking flight was made over the course on the Irvine ranch surveyed for the late Dr. Albert A. Michelson’s experiments to measure the speed of light. Joe Nikrent and W.H. Hitchman, representing the National Aeronautic Association, helped time the dashes.
In beating the Delmotte record by approximately twenty-nine miles an hour, Hughes brings back to America, the record once held by the late James Wedell. Wedell set a world mark of490.8 kilometers an hour, only to have it bettered by the French flyer last December 24.
—Los Angeles Times, Vol. LIV, Saturday, 14 September 1935, Page 1, Column 4, and Page 3, Columns 3 and 4
The Hughes H-1 (Federal Aviation Administration records identify the airplane as the Hughes Model 1B, serial number 1) was a single-seat, single-engine low-wing monoplane with retractable landing gear. Emphasis had been placed on an aerodynamically clean design and featured flush riveting on the aluminum skin of the fuselage. The airplane was 27 feet, 0 inches long (8.230 meters) with a wingspan of 25 feet (7.6 meters) and height of 8 feet (2.438 meters). (A second set of wings with a span of 31 feet, 9 inches (9.677 meters) was used on Hughes’ transcontinental flight, 19 January 1937). The H-1 has an empty weight of 3,565 pounds (1,617 kilograms) and gross weight of 5,492 pounds (2,491 kilograms).
The H-1 was powered by a air-cooled, supercharged 1,534.943-cubic-inch-displacement (25.153 liter) Pratt & Whitney Twin Wasp Jr. two-row, fourteen-cylinder radial engine. Pratt & Whitney produced 18 civil and 22 military (R-1535) versions of the Twin Wasp Jr., in both direct-drive and geared configurations, rated from 650 to 950 horsepower. According to a 1937 article in Popular Mechanics,
“Hughes’ motor is a stock air-cooled fourteen-cylinder twin-row Pratt & Whitney wasp junior that develops 700 horsepower at 2,500 revolutions per minute at 8,500 feet altitude. The engine has an outside diameter of forty-four and one-eighths inches, a dry weight of 1,060 pounds, and a displacement of 1,535 cubic inches. Compression ratio is 6.7 to one and the supercharger ratio is ten to one. Carburetion and magneto ignition are stock.”
—Popular Mechanics Magazine, Vol. 67, No. 4, April 1937, at Page 502, Column 2
The data cited by Popular Mechanics seems to match the characteristics of P&W’s Twin Wasp Jr. S3A5-G aircraft engine.
¹ FAI Record File Number 8748
² FAI Record File Number 8749: 505.85 kilometers per hour (314.32 miles per hour)
1 September 1953: Captain Harold Edward Collins, United States Air Force, flying North American Aviation F-86D-35-NA Sabre, 51-6145, set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 15/25 Kilometer Straight Course of 1,139.219 kilometers per hour (707.878 miles per hour) at Vandalia, Ohio.¹
This same F-86D (North American Aviation serial number 173-289) flown by Lieutenant Colonel William F. Barnes, set an FAI World Record for Speed Over a 3 Kilometer Straight Course of 715.697 miles per hour (1,151.803 kilometers per hour), 16 July 1953 at the Salton Sea, California. (FAI Record File Number 9868)
The F-86D was an all-weather interceptor developed from North American Aviation F-86 Sabre day fighter. It was the first single-seat interceptor, and it used a very sophisticated—for its time—electronic fire control system. It was equipped with search radar and armed with twenty-four unguided 2.75-inch (69.85 millimeter) Mk 4 Folding-Fin Aerial Rockets (FFAR) rockets carried in a retractable tray in its belly.
The aircraft was so complex that the pilot training course was the longest of any aircraft in the U.S. Air Force inventory, including the Boeing B-47 Stratojet.
The F-86D was larger than the F-86A, E and F fighters, with a longer and wider fuselage. It was also considerably heavier. The day fighter’s sliding canopy was replaced with a hinged “clamshell” canopy. A large, streamlined radome was above the reshaped engine intake.
The F-86D Sabre was 40 feet, 3¼ inches (12.275 meters) long with a wingspan of 37 feet, 1½ inches (11.316 meters), and overal height of 15 feet, 0 inches (4.572 meters). The interceptor had an empty weight of 13,518 pounds (6,131.7 kilograms), and maximum takeoff weight of 19,975 pounds (9,060.5 kilograms). It retained the leading edge slats of the F-86A, F-86E and early F-86F fighters. The horizontal stabilizer and elevators were replaced by a single, all-moving stabilator. All flight controls were hydraulically boosted. A “clamshell” canopy replaced the sliding unit of earlier models.
The F-86D was powered by a General Electric J47-GE-17 engine. This was a single-shaft, axial-flow turbojet with afterburner. The engine had a 12-stage compressor, 8 combustion chambers, and single-stage turbine. The J47-GE-17 was equipped with an electronic fuel control system which substantially reduced the pilot’s workload. It had a normal (continuous) power rating of 4,990 pounds of thrust (22.20 kilonewtons); military power, 5,425 pounds (24.13 kilonewtons) (30 minute limit), and maximum 7,500 pounds of thrust (33.36 kilonewtons) with afterburner (15 minute limit). (All power ratings at 7,950 r.p.m.) It was 18 feet, 10.0 inches (5.740 meters) long, 3 feet, 3.75 inches (1.010 meters) in diameter, and weighed 3,000 pounds (1,361 kilograms).
The maximum speed of the F-86D was 601 knots (692 miles per hour/1,113 kilometers per hour) at Sea Level, 532 knots (612 miles per hour/985 kilometers per hour) at 40,000 feet (12,192 meters), and 504 knots (580 miles per hour/933 kilometers per hour)at 47,800 feet (14,569 meters).
The F-86D had an area intercept range of 241 nautical miles (277 statute miles/446 kilometers) and a service ceiling of 49,750 feet (15,164 meters). The maximum ferry range with external tanks was 668 nautical miles (769 statute miles/1,237 kilometers). Its initial rate of climb was 12,150 feet per minute (61.7 meters per second) from Sea Level at 16,068 pounds (7,288 kilograms). From a standing start, the F-86D could reach its service ceiling in 22.2 minutes.
The F-86D was armed with twenty-four 2.75-inch (69.85 millimeter) unguided Folding-Fin Aerial Rockets (FFAR) with explosive warheads. They were carried in a retractable tray, and could be fired in salvos of 6, 12, or 24 rockets. The FFAR was a solid-fuel rocket. The 7.55 pound (3.43 kilogram) warhead was proximity-fused, or could be set for contact detonation, or to explode when the rocket engine burned out.
The F-86D’s radar could detect a target at 30 miles (48 kilometers). The fire control system calculated a lead-collision-curve and provided guidance to the pilot through his radar scope. Once the interceptor was within 20 seconds of its target, the pilot selected the number of rockets to fire and pulled the trigger, which armed the system. At a range of 500 yards (457 meters), the fire control system launched the rockets.
Between December 1949 and September 1954, 2,505 F-86D Sabres (sometimes called the “Sabre Dog”) were built by North American Aviation. There were many variants (“block numbers”) and by 1955, almost all the D-models had been returned to maintenance depots or the manufacturer for standardization. 981 of these aircraft were modified to a new F-86L standard. The last F-86D was removed from U.S. Air Force service in 1961.
After its service with the United States Air Force, the record-setting Sabre 51-6145 was transferred to a NATO ally, the Ellinikí Vasilikí Aeroporía (Royal Hellenic Air Force).