Tag Archives: Harmon International Trophy

29 October 1953

North American Aviation YF-100A Super Sabre 52-5754 during speed record attempt at the Salton Sea, 29 October 1953. (San Diego Air and Space Museum Archives)
North American Aviation YF-100A Super Sabre 52-5754 during a speed record attempt at the Salton Sea, 29 October 1953. (San Diego Air and Space Museum Archives)

29 October 1953: Lieutenant Colonel Frank Kendall (“Pete”) Everest, United States Air Force, flew a new prototype air superiority fighter, North American Aviation’s YF-100A Super Sabre, serial number 52-5754, over the 3 kilometer and 15 kilometer courses at the Salton Sea, in the Colorado Desert of southeastern California.

Flying four runs over the short course, Everest averaged 757.75 miles per hour (1,219.48 kilometers per hour). Although this was 4.80 miles per hour (7.725 kilometers per hour) faster than the FAI record set three weeks earlier by Lieutenant Commander James B. Verdin, U.S. Navy, with a Douglas XA4D-1 Skyray,¹ it was not fast enough to establish a new world record under FAI rules, which required that a new record exceed the previous record by 1%.

Lieutenant Colonel Frank Kendall Everest, Jr., United States Air Force.

Next came four speed runs over the 15-to-25 kilometer course. All runs were made with the Super Sabre flying within 100 feet (30 meters) of the ground. The official Fédération Aéronautique Internationale (FAI) average speed was 1,215.298 kilometers per hour (755.151 miles per hour)—0.99 Mach. ²

The course at the Salton Sea was used because its surface lies 235 feet (72 meters) below Sea Level. The denser air causes undesired transonic effects to occur at lower speeds, but the higher air temperatures help to delay them, allowing the pilot a greater margin of control during the speed record runs.

Lieutenant Colonel Frank K. Everest and the North American Aviation YF-100A Super Sabre, 52-5754, 29 October 1953. (San Diego Air and Space Museum Archives)

Frank Kendall (“Pete”) Everest, Jr., was born 10 Aug 1920, at Fairmont, Marion County, West Virginia. He was the first of two children of Frank Kendall Everest, an electrical contractor, and Phyllis Gail Walker Everest. Attended Fairmont Senior High School, Fairmont, West Virginia, graduating in 1939. He studied at Fairmont State Teachers College, also in Fairmont, West Virginia, and then studied engineering at the University of West Virginia in Morgantown.

Pete Everest enlisted as an aviation cadet in the United States Army Air Corps at Fort Hayes, Columbus, Ohio, 7 November 1941, shortly before the United States entered World War II. His enlistment records indicate that he was 5 feet, 7 inches (1.703 meters) tall and weighed 132 pounds (59.9 kilograms). He graduated from pilot training and was commissioned as a second lieutenant, Air Reserve, 3 July 1942.

Lieutenant Frank Kendall Everest, Jr. (schultzy)

2nd Lieutenant Everest married Miss Avis June Mason in Marion, West Virginia, 8 July 1942. they would have three children.

He was promoted to 1st Lieutenant, Army of the United States, 11 November 1942. He was assigned as a Curtiss-Wright P-40 Warhawk pilot, flying 94 combat missions in North Africa, Sicily and Italy. He was credited with shooting down two German airplanes and damaging a third. Everest was promoted to the rank of Captain, 17 August 1943.

Pete Everest with his Curtiss-Wright P-40 Warhawk, North Africa, circa 1943.

In 1944, Everest was returned to the United States to serve as a flight instructor. He requested a return to combat and was then sent to the China-Burma-India theater of operations where he flew 67 missions and shot down four Japanese airplanes. Everest was appointed commanding officer of the 29th Fighter Squadron (Provisional), 5th Fighter Group (Provisional) at Chihkiang, China, in April 1945. He was himself shot down by ground fire in May 1945. Everest was captured by the Japanese and suffered torture and inhumane conditions before being freed at the end of the war. He was promoted to the rank of major, 1 July 1945. He was returned to the United States military 3 October 1945.

Following World War II, Major Everest was assigned as a test pilot at Wright-Patterson Air Force Base, Ohio, before going west to the Air Force Flight Test Center at Edwards Air Force Base, California.

Major Everest was returned to the permanent rank of first lieutenant, Air Corps, 19 June 1947, with date of rank retroactive to 3 July 1945.

At Edwards, Pete Everest was involved in nearly every flight test program, flying the F-88, F-92, F-100, F-101, F-102, F-104 and F-105 fighters, the XB-51, YB-52, B-57 and B-66 bombers. He also flew the pure research aircraft, the “X planes:” the X-1, X-1B, X-2, X-3, X-4 and X-5. Pete Everest flew the X-1B to Mach 2.3, and he set a world speed record with the X-2 at Mach 2.9 (1,957 miles per hour, 3,149.5 kilometers per hour) which earned him the title, “The Fastest Man Alive.” He was the test pilot on thirteen of the twenty X-2 flights.

In 1957, Lieutenant Colonel Everest was awarded the Harmon Trophy “for the most outstanding international achievements in the arts and/or science of aeronautics for the preceding year,” and also received the Octave Chanute Award “for an outstanding contribution made by a pilot to the art, science and technology of aeronautics.”

Major Frank Kendall Everest, Jr., U.S. Air Force, with the Bell X-2 supersonic research rocketplane, on Rogers Dry Lake at Edwards AFB, California, 1956. (U.S. Air Force)

Frank Everest returned to operational assignments and commanded a fighter squadron, two combat crew training wings, and was assigned staff positions at the Pentagon. On 20 November 1963, Colonel Everest, commanding the 4453rd Combat Crew Training Squadron, flew one of the first two operational McDonnell F-4C Phantom II fighters from the factory in St. Louis, Missouri, to MacDill Air Force Base, Tampa, Florida.

In 1965, Pete Everest was promoted to the rank of brigadier general. He was assigned as commander of the Aerospace Rescue and Recovery Service. General Everest retired from the Air Force in 1973 after 33 years of service.

Shortly after he retired from the Air Force, on 5 April 1973, Sikorsky Aircraft appointed General Everest its Chief Test Pilot. The manufacturer was developing the S-70 Black Hawk and S-76 commercial helicopters at the time.

During his military career General Everest was awarded the Air Force Distinguished Service Medal; Legion of Merit with two oak leaf clusters (three awards); Distinguished Flying Cross with two oak leaf clusters (three awards); Purple Heart; Air Medal with one silver and two bronze oak leaf clusters (seven awards); Air Force Commendation Medal with one oak leaf cluster (two awards); Presidential Unit Citation with two bronze oak leaf clusters (three awards); Air Force Gallant Unit Citation; Prisoner of War Medal; American Campaign Medal; European-African-Middle Eastern Campaign medal with four bronze stars; Asiatic-Pacific Campaign Medal with two bronze stars; World War II Victory Medal; National Defense Service Medal; Armed Forces Expeditionary Medal; Vietnam Service Medal; Air Force Longevity Service Award with one silver and two bronze oak leaf clusters (seven awards); Air Force Small Arms Expert Marksmanship Ribbon; and the Republic of Vietnam Campaign Medal with 1960– device. General Everest was rated as a Command Pilot, and a Basic Parachutist.

Brigadier General Frank Kendall Everest, Jr. United States Air Force (Retired), died at Tucson, Arizona, 1 October 2004 at the age of 84 years.

Brigadier General Frank Kendall Everest, Jr., United States Air Force

The North American Aviation F-100 Super Sabre was designed as a supersonic day fighter. Initially intended as an improved F-86D and F-86E, the “Sabre 45” soon developed into an almost completely new airplane.

The Super Sabre had a 49° 2′ sweep to the leading edges of the wings and horizontal stabilizer. The total wing area was 385.2 square feet (35.79 square meters). The wings had an angle of incidence of 0°, with no twist or dihedral. The ailerons were placed inboard on the wings and there were no flaps, resulting in a high stall speed in landing configuration. The horizontal stabilizer was moved to the bottom of the fuselage to keep it out of the turbulence created by the wings at high angles of attack. The F-100A had a distinctively shorter vertical fin than the YF-100A. The upper segment of the vertical fin was swept 49° 43′.

There were two service test prototypes, designated YF-100A, followed by the production F-100A series. The first ten production aircraft (all of the Block 1 variants) were used in the flight testing program.

The F-100A Super Sabre was 47 feet, 1¼ inches (14.357 meters) long with a wingspan of 36 feet, 6 inches (11.125 meters). With the shorter vertical fin, the initial F-100As had an overall height of 13 feet, 4 inches (4.064 meters), 11 inches (27.9 centimeters) less than the YF-100A.

North American Aviation Chief Test Pilot George S. Welch in the cockpit of the YF-100A, 52-5754, at Los Angeles International Airport. (North American Aviation, Inc.)
North American Aviation Chief Test Pilot George S. Welch in the cockpit of the YF-100A, 52-5754, at Los Angeles International Airport. (North American Aviation, Inc.)

The F-100A had an empty weight of 18,135 pounds (8,226 kilograms), and its maximum takeoff weight was 28,971 pounds (13,141 kilograms). It had an internal fuel capacity of 744 gallons (2,816 liters) and could carry two 275 gallon (1,041 liter) external fuel tanks.

The new air superiority fighter was powered by a Pratt & Whitney Turbo Wasp J57-P-7 engine. The J57 was a two-spool axial-flow turbojet which had a 16-stage compressor section (9 low- and 7 high-pressure stages) and a 3-stage turbine (2 high- and 1 low-pressure stages). Its continuous power rating was 8,000 pounds of thrust (35.586 kilonewtons). The Military Power rating was 9,700 pounds (43.148 kilonewtons) (30-minute limit). Maximum power was 14,800 pounds (43.148 kilonewtons) with afterburner (5-minute limit). The engine was 20 feet, 9.7 inches (6.342 meters) long, 3 feet, 3.9 inches (1.014 meters) in diameter, and weighed 5,075 pounds (2,303 kilograms). Later production aircraft used a J57-P-39 engine, which had the same ratings.

North American Aviation YF-100 Super Sabre 754 parked on the dry lake at Edwards Air Force Base, California. (U.S. Air Force)

The Super Sabre was the first U.S. Air Force fighter capable of supersonic speed in level flight.

The YF-100A had a maximum speed of 660 miles per hour (1,062 kilometers per hour) at 43,350 feet (13,213 meters). During testing, 52-5754 reached Mach 1.44 in a dive. The service ceiling was 52,600 feet (16,033 meters). Range with internal fuel was 422 miles (679 kilometers).

North American Aviation YF-100A Super Sabre 52-5754 over Edwards Air Force Base, California, 25 May 1953. (North American Aviation, Inc.)

The production F-100 was armed with four M39 20 mm autocannons, capable of firing at a rate of 1,500 rounds per minute. The ammunition capacity of the F-100 was 200 rounds per gun.

North American Aviation built 199 F-100A Super Sabres at its Inglewood, California, plant before production shifted to the F-100C fighter bomber variant. Approximately 25% of all F-100As were lost in accidents.

North American Aviation YF-100A Super Sabre 52-5754 banks away from a chase plane during a flight test. (U.S. Air Force)

¹ FAI Record File Number 9871

² FAI Record File Number 8868

© 2019, Bryan R. Swopes

26 October 1980

THE RESCUE OF THE CREW OF THE SCALLOPER TERRY T

By Sean M. Cross, CAPT, USCG (retired)

“As the basket was lowered a fifth time to pick up the two remaining men, a huge wave hit the awash stern of the TERRY T knocking the last two crewmen – the master and the engineer – into the water downwind of the helicopter and the ship. With the lives of the two crewmen suddenly threatened by the turbulent seas and the ship drifting down upon them…”

TODAY IN COAST GUARD AVIATION HISTORY — 26 OCTOBER 1980: HH-3F assigned to Air Station Cape Cod, MA and crewed by LTJG John P. Currier (AC); LTJG Robert L. Abair (CP); AM1 David L. Seavey and AE2 Gordon R. Warren (AV) was launched at 3:40 AM in response to the 110-foot fishing vessel Terry T out of New Bedford sinking with 10 crewman aboard. The eastern-rigged scallop trawler was 80 miles southeast of Nantucket in 30-foot seas, blowing snow and 60 knot winds gusting to 80 knots. The Terry T reported “4-feet of water in the engine room” (i) and requested dewatering pumps to help control the flooding. (ii)

That weekend, a coastal storm wreaked havoc when high winds and heavy seas lashed the Massachusetts coast line, damaging scores of small work and pleasure craft. (iii) The 31-year-old skipper, Roland Farland, said the Terry T was water tight when it was checked about 10 PM Saturday night as it rode out the severe coastal storm 70 miles east-south east of Nantucket. But when he checked the boat again shortly after midnight, water was flooding the engine room. (iv)

The TERRY T was built by Sturgeon Bay Shipbuilding as hull number 228 and official number 258929. The original name was “Wisconsin” – delivered in 1949 to the original owner John Roen. Records indicate that “John Roen would continue to be a forerunner in maritime accomplishments […] launching an Atlantic fishing fleet out of Boston, which was run from Sturgeon Bay.”
“We got three pumps going but we couldn’t contend with the water,” Farland said. (v)In the Interim, the Terry T had been in frequent radio contact with the Coast Guard through the Nantucket Lightship and by 3:30 AM had informed the Coast Guard they would have to evacuate. (vi) Currier, the most junior Aircraft Commander at the unit, noted he “got stuck” with duty that night because there was a wardroom party planned. It turned into a busy night, The aircrew had already flown on several SAR cases that evening including evacuating Coast Guard members from the Buzzards Bay Entrance Light due to structural concerns caused by the adverse weather. (vii) Currier described their return to base from the last case, “We went back into the air station and I remember shooting an instrument approach at 120 knots indicated airspeed and doing less than 20 knots over the ground.” He added, “We came in, landed and taxied into the lee of the hangar to shut the rotor head down and those guys were taking care of the post-flight and my wife was at the wardroom party. So when we got back into the wardroom at about 8 o’clock at night she said ‘You’re not going out again are you?’ and I said, ‘No way—nobody’s out there.’ ” (vii)
Sikorsky HH-3F Pelican 1484 (Sikorsky S-61R, s/n 61-661) hovers over Lands End with Golden Gate Bridge in background. 1989 photograph.  (U.S. Coast Guard 191114-G-G0000-006/SFO Museum 2012.114.002)

About 3:40 in the morning the aircrew was awakened by Rescue Coordination Center (RCC) Boston saying there was a scalloper taking on water and unable to control flooding about 80 miles southeast of Nantucket. The aircrew described it as an interesting launch because it was still blowing 60 knots (which exceeded the main rotor start limit)—so the duty crew dragged the helicopter about halfway out of the hangar to start the turbine engines and engage the rotor system. They did it in this manner because when a helicopter first starts, the rotors are flexible and droop under their own weight. Strong winds can cause the blades to flap up and down when they are at slow RPM causing them to contact the tail boom or fuselage and do serious damage.

took off and flew toward the last known position (LKP) about 15 miles east of the Nantucket Lightship under instrument flight rules (IFR)—flying in clouds with limited to zero visibility, navigating only by cockpit instruments. The aircraft experienced severe turbulence and Currier remarked, “The crew was holding on for dear life.” (ix)

Approximate route of flight to TERRY T’s last known position “about 70 miles southeast of Nantucket, about 15 miles east of the Nantucket Lightship.”

At 4:54 AM, was approaching the Terry T‘s LKP and Currier further described the situation as, “Pitch black except for the lightning and there was sleet—so we were concerned about icing.” Helicopter pilots avoid icing like dental work. When ice forms on rotor blades, they lose their ability to provide lift, and the aircraft can no longer maintain flight. The aircrew contacted Terry T on the radio and confirmed they still wanted dewatering pumps—they concurred and reported that the fishing boat had lost steering and “was at the mercy of thirty foot seas and fifty knot winds.” (x) However, the master came on the radio a few minutes later as was inbound and said, “We got a fire in the engine room, we can’t control it and I want everybody —there are 10 of us.”

As the water level rose it produced short circuits that caused spontaneous fires in the boat’s electrical system. Farland said the crew had used four fire extinguishers and had nothing left with which to fight the fires. Then radio contact was lost. (xi) From their transit altitude, the aircrew performed an instrument approach to the water astern of Terry T. (xii) The crew used a PATCH or Precision Approach to a Coupled Hover, an autopilot maneuver that transitions the helicopter from forward flight in the clouds down to an automatic hover at 50 feet visual with the water. (xiii) This maneuver can be disorienting in the clouds at night, particularly when low over the water with little room for error. Both pilots must continuously scan and interpret the flight instruments—this is critically important—to confirm the autopilot is flying the correct profile. This maneuver was described as “dicey” due to the HH-3F’s unreliable doppler. The aircrew finally made visual contact with the trawler’s glow as the aircraft descended below 150 feet.

Currier described the challenging situation, “When we arrived in a hover, we turned on the floodlights and neither myself, nor the co-pilot nor the flight mechanic thought we could do it. The tops were blowing off the waves and going over the boat and the boat was dead in the water so it was in the trough—so it was rolling more than rail-to-rail—it was getting green water over each rail as it rolled.” (xiv) With the helicopter pointing into the strong westerly winds—Terry T‘s “bow was pointed to the right (the aircraft’s 3 o’clock position), so I had no place to go to hoist,” added Currier. (xv) Seavey had similar sentiments, “This case was the only time that I had thoughts that I might not be able to complete the hoist [due to] the combination of high winds 50–60 knots or so and 25–30 foot seas.” (xvi) The aircrew was concerned with the extreme pitch and roll of the fishing vessel and height of the rigging and other obstacles, so they initially requested that the Terry T crew disembark the vessel to the life raft. However, when the fishermen inflated the raft, it immediately blew overboard. (xvii) After careful assessment, they decided that hoisting from about 40 feet above the highest waves to an area just aft of the pilot house was their best chance of success.

An MH-65D demonstrates a “trail line hoist” with a Coast Guard small boat. Note the hypotenuse or diagonal formed by the trail line running from the person on deck to the hoist hook. (U.S. Coast Guard)

With no suitable hover reference, Currier was guided only by the voice of his hoist operator, David Seavey. Initial attempts did not go well. The pilot is typically unable to see the hoist area (below and aft of the pilot seat) and must fly exclusively off the flight mechanic’s conning commands—this can be very challenging when the sole hover reference is a raging and turbulent sea surface of 30–35 foot swells. The crew was convinced that a “trail line hoist” was the right tool for the situation as it would allow the helicopter to hoist from a position offset 30–40 feet from the boat and facilitate Currier’s use of the bobbing fishing vessel as a hover reference.

A trail line is a 105-foot piece of polypropylene line (similar to a water ski rope) with a 300-pound weak link at one end and a weight bag at the other. The weight bag end of the trail is paid out below the helicopter and delivered to the persons in distress (usually vertically, but seasoned flight mechanics can literally “cast” the weight bag to a spot). The weak link is then attached to the hoist hook and the helicopter backs away until the pilot can see the hoisting area. The persons in distress can then pull the basket to their location—creating a hypotenuse or diagonal—as opposed to a purely vertical delivery.

Danforth anchor

This was great in theory, but not in practice as Seavey said, “The high winds caused the trail line delivery, even with the heavy weather weight bags (25 pounds) to sail aft and twice get fouled in the rigging. We backed off, discussed the situation and decided to try using the Danforth anchor—which worked.” (xviii) Being an amphibious helicopter, the HH-3F kit included a Danforth anchor (similar to any small recreational boating anchor) with a half-inch line—they used this as an improvised trail line and it worked perfectly—with one exception which would trigger problems later in the evolution. (xix)

Currier was now able to use the vessel’s radio antenna and momentary glimpses of the superstructure for visual reference. (xx) Seavey conducted four hoists with assistance from Warren, taking crewmen in the basket two-at-a-time on each hoist. (xxi) This was unusual but necessary due to fuel concerns, the need to hoist everyone before the trawler sank and the extreme difficulty involved in placing the basket on the vessel each time. Abair added, “While a series of ten one-man hoists could have been successful, it would have more than doubled the difficulty of the rescue and would have likely resulted in loss of life.” (xxii) Between hoists, Warren took the survivors aft in the cabin and provided them with blankets to get warm. Seavey gratefully described Warren’s efforts: “He assisted me during the hoists, was helping out without having to be told what I needed. He anticipated what I needed. He was the extra set of hands getting the rescue basket into the cabin and then clearly directed the survivors to the back of the cabin.” Often forgotten under these conditions was the superlative job done by Abair, a Direct Commission Aviator and veteran Marine Corps helicopter pilot, in his Safety Pilot role. He continuously scanned the system instruments to ensure the aircraft was operating normally and the flight instruments to ensure obstacle clearance and safe altitude—occasionally coming on the controls to assist. He conveyed critical information effectively in a dynamic environment without interfering with Seavey’s commands—the crew said he did a masterful job. (xxiii)

HH-3F #1484’s approximate hoisting position with TERRY T (represented with a generic fishing boat plan of roughly the same arrangement). As Dave Seavey stated, that diagram is accurate, “minus the massive seas, near hurricane force winds, pitch black and the boat being DIW.”

As the basket was lowered a fifth time to pick up the two remaining men, a huge wave hit the awash stern of the Terry T knocking the last two crewmen—the master and the engineer, brothers Roland and Brian Farland—into the water downwind of the helicopter and the ship. (xxiv) “I had one hand on the basket and one hand on my brother,” Farland said. (xxv) With the lives of the two crewmen suddenly threatened by the turbulent seas and the ship drifting down on them, Currier had to reposition the aircraft over the two men with only the conning commands from Seavey to guide him, With Seavey’s instructions, Currier demonstrated extreme skill and daring and maneuvered the basket into a position in the water so that the two men could literally fall into it, and they were lifted to safety—or so they thought.

At this point, the boat actually started to go down by the stern, Seavey had the basket and two men about two-thirds of the way from the boat deck to the helicopter when he realized that earlier in the evolution without aircrew knowledge, the fisherman had tied the trail line off to the pilot house rail. The helicopter was connected to the boat by the anchor line. Seavey shouted, “We’re tied to the boat, we have problems here.” (xxvi) Currier and Abair assessed the sea state then carefully descended from their hoisting altitude of 40 feet to 25 feet creating enough slack in the trail line and allowing Seavey and Warren to bring the basket into the door. At once, Seavey cut the anchor line with a knife and immediately conned, “Up, up, up” for the pilots to immediately pull power. At 25 feet, Seavey could see that the wave tops on either side were level with the helicopter. (xxvii)

After completing the hoists, it took about five minutes to secure the cabin—Seavey and Warren working together—Warren helped the Captain and crew to the rear of the cabin and secured the basket while Seavey was securing the hoist, closing the cabin door and reporting that the cabin was secured and ready for forward flight. As circled the scalloper, it had already began to founder—the decks awash with sea water. (xxviii) The flight mechanic and avionicsman administered first aid to the injured crew on the return flight that landed at 6:52 AM. Throughout the mission, Currier and his crew showed exemplary skill and courage. Currier stated, “We got them off and got back. The helicopter was pretty beat up—they actually had to change the tail rotor because of overstresses.” (xxix)

All 10 men (listed below) were saved from the Terry T—four of the survivors were from the same family. (xxx)

Roland Farland (Captain)
Elmer Beckman (Mate)
Brian Farland (Engineer)
John Santos (cook)
Donald Capps (deckhand)
George Altman (deckhand)
Ronald Charpentier (deckhand)
Stephen Farland (deckhand)
Peter Farland (deckhand)
George Johnston (deckhand) (xxxi)

“It was pretty hairy,” Roland Farland said. “I just have to commend the Coast Guard for doing such a terrific job. It was blowing good,” the New Bedford man said: “Seas were 30 feet and winds were blowing 60 to 65 miles.”

In a post-mission interview, Currier conveyed, “Visibility was about half a mile and it took us five hoists to get 10 people off the boat. We had to hover over it for about an hour. (xxxii) The problem with a situation like that is that you have no point of reference,” he said. “All you can see is the boat and the water, and they are both in motion. You try to keep the helicopter a stable platform, but it’s hard. I’ve been here three years and those were the worst condition I’ve seen.” (xxxiii)

Thirty-five years later, and older and wiser Vice Admiral (VADM) Currier reflected on that night. “This was not a solo pilot operation. This was a reflection of an incredibly talented flight mechanic and a solid co-pilot. Actually, I think that was my co-pilot’s first rescue mission after transitioning from the Marine Corps to the Coast Guard, and I think it was a heck of an eye-opener for him.” VADM Currier added, “In the Coast Guard we have some of the best rotary- and fixed-wing pilots there are. I can say that as the old Coast Guard aviator, but I’ve been around long enough in civil and military aviation to say our people are among the very best. They are challenged on a daily basis with missions that would be a big deal in other services. For us, they’re how we do business—night, offshore, poor visibility, terrible weather. It’s always single-ship, and it’s always single crew. It requires skill, proficiency and individual initiative.” (xxxiv)

For this nearly impossible rescue, Currier earned the Harmon International Aviation Trophy—the only Coast Guard Aviator to warn this distinction. The Harmon Trophy—the aviator’s award—is given for the most outstanding international achievements in the preceding year, with the art of flying receiving first consideration. He joined other winners such as: Colonel Charles A. Lindbergh: General Jimmy Doolittle, Major Charles E. Yeager, Howard Hughes, Major Edwin E. “Buzz” Aldrin and Amelia Earhart.

The Harmon International Trophy at the Smithsonian Institution National Air and Space Museum. The Harmon Trophy (1926) was established by Clifford Harmon, a wealthy balloonist and aviator.  (NASM)

The Harmon Trophy was presented to him at the Old Executive Building across from The White House by Vice President Dan Quayle on 21 June 1991 (11 years after the mission). His name is inscribed on the six foot tall trophy in a glass enclosure in the National Air and Space Museum. Interestingly, Currier was never notified regarding his selection of the award, which has historically been presented by the president. The Reagan assassination attempt by John Hinckley, Jr., on 30 March 1981 wreaked havoc with the President’s schedule and the award presentation was overlooked. His parents while visiting the Smithsonian Institution National Air and Space Museum in Washington, D.C., six years later, reportedly saw his name engraved on the trophy and asked him about it. It took another four years of action by headquarters and the Coast Guard Aviation Association before Currier received the award.

Vice President of the United States James Danforth Quayle congratulates Lieutenant Commander John Philip Currier, U.S. Coast Guard, on the presentation of the Harmon International Aviator Trophy, 21 June 1991.

The aircrew also earned the American Helicopter Society (now, the Vertical Flight Society) Frederick L. Feinberg Award in March 1981—presented to the pilot or crew of a vertical flight aircraft who demonstrated outstanding skills or achievement during the preceding 18 months. (xxxv)

The Frederick L. Feinberg Award (1961) was established by the American Helicopter Society, in memory of an outstanding helicopter test pilot and an exemplary person.

Lieutenant (junior grade) Currier and AM1 Seavey both earned the Distinguished Flying Cross for this mission, while LTJG Abair and AE2 Warren earned the Coast Guard Commendation Medal with Operational Distinguishing Device in a ceremony at Air Station Cape Cod in June 1981. (xxxvi) The Currier and Abair Citations are below. The Seavey and Warren citations have not been located.

Vice Admiral John Philip Currier, Vice Commandant of the United States Coast Guard. Photographed 2009. (U.S. Coast Guard)

Vice Admiral John Philip Currier, United States Coast Guard (Retired), passed away on 01 March 2020 from natural causes at his home in Traverse City, Michigan. His ashes were interred with full military honors at Arlington National Cemetery on 14 September 2021. He is recognized as the “godfather of the Coast Guard’s modern H-60 helicopter program” and received commendations for flying and rescue work over his 38-year career in the Coast Guard. He held assignments as an aviator at Air Stations Cape Cod (MA), Sitka (AK), Traverse City (MI), Astoria (OR), Detroit (MI) and Miami (FL). He held many senior leadership positions including Chief of Operations and Chief of Staff for the Pacific Area; Commander of the Thirteenth District in the Pacific Northwest; Coast Guard Chief of Staff; and finally, Vice Commandant, the Service’s second in command.  From 2008–2012, just prior to his tenure as Vice Commandant, the Coast Guard Aviation community experienced a horrendous series of aircraft accidents that took the lives of 18 Coast Guard aircrewmen. The dilemma weighed heavily on Admiral Currier, but—he was the RIGHT man, in the RIGHT place, at the RIGHT time when the Service needed him most. The Service was searching for solutions—long fatigued and exasperated from attending memorial services, hearing eulogies and listening to “Amazing Grace”—he led us out of that morass to “clearer skies” with a new focus on cockpit leadership, proficiency, risk management and a “back to basics” approach when it came to tactics, techniques and procedures. He guided a structured fleet-wide operational risk assessment and directed corrective actions which yielded a remarkable improvement in aviation professionalism and safety. These efforts added to his already robust Coast Guard Aviation legacy.

***********************

Retired Captain Sean M. Cross served 25 years in the Coast Guard as a helicopter pilot and aeronautical engineer. Flying both the MH-60T and MH-65D, he accumulated over 4,000 flight hours while assigned to Air Stations Clear Water, FL; Cape Cod, MA; San Diego, CA; Elizabeth City, NC and Traverse City, MI, which he commanded.

“There is only one Coast Guard Aviator’s name etched on the Harmon Trophy and the story of HOW it got there should be preserved for posterity.”

i Boston AP article – multiple sources – “The ‘Terry T.” of New Bedford called for help at about 3:30 a m. when its engine room filled with about four feet of water, spokesman Mario Toscano of the Coast Guard’s Boston Rescue Center said.” – available here: https://www.newspapers.com/newspage/439301890/
ii John Currier (HH-3F Aircraft Commander) in video discussion (Exit Interview) with Scott T. Price (Coast Guard Historian) in Washington, D.C. on April 23, 2014.
iii Jack Stewardson, “10 fishermen saved; 2nd trawler overdue,” The Standard-Times, New Bedford, Mass., October 27, 1980, page 1.
iv Jack Stewardson, “It was pretty hairy, but help came for fishing crew,” The Standard-Times, New Bedford, Mass.,, October 28, 1980, page 4.
v Ibid.
vi Ibid.
vii Gordon Warren (HH-3F Avionicsman) in phone interview with the author on September 30, 2021.
viii Currier interview
ix Ibid.
x Barrett Thomas Beard, “Wonderful Flying Machines: A History of U.S. Coast Guard Helicopters,” (Annapolis: Naval Institute Press, 1996), page 146.
xi Ibid
xii Currier interview
xiii Robert Abair (HH-3F Co-Pilot) in email message to author on September 30, 2021. “The term PATCH implies a coupled hover, which was not the case. All hovering was done manually. Because of the heavy seas, it was impossible to couple the aircraft to the radar altimeter. The entire mission from lift off to touch down was hand flown due to turbulence.”
xiv Ibid.
xv Ibid.
xvi David Seavey (HH-3F Flight Mechanic) in email message to author on September 22, 2021.
xvii Currier interview
xviii Seavey email.
xix Currier interview
xx Beard, “Wonderful Flying Machines: A History of U.S. Coast Guard Helicopters,” page 147.
xxi Seavey email.
xxii Abair email.
xxiii Seavey email.
xxiv Staff Writer (1), “Manchester Man Cited by U.S. Coast Guard,” Manchester Evening Herold, June 22, 1981, page 20 – available here: http://www.manchesterhistory.org/News/Manchester%20Evening%20Hearld_1981-06-22.pdf
xxv Stewardson, “It was pretty hairy, but help came for fishing crew,” page 4.
xxvi Currier interview xxvii Ibid
xxviii Seavey email.
xxix Currier interview
xxx Beard, “Wonderful Flying Machines: A History of U.S. Coast Guard Helicopters,” page 147.
xxxi Stewardson, “10 fishermen saved; 2nd trawler overdue,” page 4.
xxxii Staff Writer (2), “CG pulls 10 from blazing trawler,” Cape Cod Times, October 27, 1980, page unknown
(Falmouth Public Library Microfiche retrieved on September 29, 2021 by Sue Henken). xxxiii Ibid
xxxiv American Helicopter Society International – Vertipedia. “Biography, John P. Currier, United States,” Last modified April 14, 2021. https://vertipedia-legacy.vtol.org/milestoneBiographies.cfm?bioID=428
xxxv Vertical Flight Society. “Frederick L. Feinberg Award previous recipients,” Last modified in 2021. https://vtol.org/awards-and-contests/vertical-flight-society-award-winners?awardID=3
xxxvi Staff Writer (1), “Manchester Man Cited by U.S. Coast Guard,” page 20.

© 2021, Sean M. Cross

3 October 1967

Major William J. Knight, United States Air Force, with the North American Aviation X-15A-2, 56-6671. (U.S. Air Force)

3 October 1967: The 188th flight of the X-15 Program was the 53rd for the Number 2 aircraft, 56-6671. It had been extensively modified by North American Aviation to an X-15A-2 configuration following a landing accident which had occurred 9 November 1962. The fuselage was lengthened 28 inches (0.711 meters) to accommodate a liquid hydrogen fuel tank for a scramjet engine that would be added to the ventral fin, a new tank for additional hydrogen peroxide to generate steam for the rocket engine turbo pump, and external propellant tanks to allow the rocketplane to reach higher speeds and altitudes. The entire surface of the X-15 was covered with an ablative coating to protect the metal structure from the extreme heat it would encounter on this flight.

Minor issues delayed the takeoff but finally, after they were corrected, and with Pete Knight in the X-15’s cockpit, it was carried aloft under the right wing of Balls 8, a Boeing NB-52B Stratofortress, 52-008.

At 45,000 feet (13,716 meters) over Mud Lake, Nevada, the X-15 was droppeded at 14:31:50.9 local time. Knight fired the Reaction Motors XLR99-RM-1 rocket engine and began to climb and accelerate. After 60 seconds, the ammonia and liquid oxygen propellants in the external tanks was exhausted, so the the tanks were jettisoned to eliminate their weight and aerodynamic drag.

The X-15A-2 climbed to 102,100 feet (31,120 meters) and Pete Knight leveled off, still accelerating. After 140.7 seconds of engine burn, Knight shut the XLR99 down. He noticed that thrust seemed to decrease gradually and the X-15 continued to accelerate to 6,630 feet per second (2,021 meters per second), or Mach 6.72.

North American Aviation X-15A-2 56-6671 is carried to launch altitude under the right wing of the Boeing NB-52B Stratofortress 52-008. (U.S. Air Force)
North American Aviation X-15A-2 56-6671 is carried to launch altitude under the right wing of the Boeing NB-52B Stratofortress 52-008. The scramjet is attached to the ventral fin. (U.S. Air Force)
North American Aviation X-15A-2 56-6671 immediately after being released from the mothership, Boeing NB-52B Stratofortress 52-008, Balls 8, over Mud Lake, Nevada, 3 October 1967. The steam trail is hydrogen peroxide used to power the rocket engine turbopump. (U.S. Air Force)
North American Aviation X-15A-2 56-6671 immediately after being released from the mothership, Boeing NB-52B Stratofortress 52-008, Balls 8, over Mud Lake, Nevada, 3 October 1967. The steam trail is hydrogen peroxide used to power the rocket engine turbopump. (U.S. Air Force) 
The North American Aviation X-15A-2 56-6671 ignites the XLR99 engine after being released from the mothership, Balls 8, 3 October 1967. (U.S. Air Force)
The X-15A-2’s XLR99-RM-1 rocket engine ignites after release from the mothership, Balls 8, 3 October 1967. (U.S. Air Force) 

Shock waves from the dummy scramjet mounted on the ventral fin impinged on the fin’s leading edge and the lower fuselage, raising surface temperatures to 2,700 °F. (1,482 °C.) The Inconel X structure started to melt and burn through.

Pete Knight entered the high key over Rogers Dry Lake at 55,000 feet (16,764 meters) and Mach 2.2, higher and faster than normal. As he circled to line up for Runway One Eight, drag from the scramjet caused the X-15 to descend faster and this set him up for a perfect approach and landing. Because of heat damage, the scramjet broke loose and fell away from the X-15.

Knight touched down after an 8 minute, 17.0 second flight. His 4,520 mile per hour (7,274 kilometers per hour) maximum speed is a record that still stands.

Firefighters cool down the ventral fin of the North American Aviation X-15A-2 56-6671 after its last landing on Rogers Dry Lake, 3 October 1967.(U.S. Air Force)
Firefighters cool down the ventral fin of the North American Aviation X-15A-2 56-6671 after its final landing on Rogers Dry Lake, 3 October 1967.(U.S. Air Force)

The X-15A-2 suffered considerable damage from this hypersonic flight. It was returned to North American for repairs, but before they were completed, the X-15 Program came to an end. This was 56-6671’s last flight. It was sent to the National Museum of the United States Air Force where it is part of the permanent collection.

In a ceremony at the White House, President Lyndon B. Johnson presented the Harmon International Trophy to Major William J. Knight.

The Harmon International Trophy at the Smithsonian Institution National Air and Space Museum. (NASM)
The Harmon International Trophy at the Smithsonian Institution National Air and Space Museum. (NASM)

© 2016, Bryan R. Swopes

29 May 1951

Charles F. Blair, Jr., standing in the cocpit of his North American Aviation P-51C Mustang, N1202, Excalibur III, 1951. (National Air and Space Museum, Smithsonian Institution.)
Captain Charles F. Blair, Jr., standing in the cockpit of Pan American World Airways’ North American Aviation P-51C Mustang, Excalibur III, Bardufoss, Norway, 29 May 1951. (National Air and Space Museum, Smithsonian Institution.)

29 May 1951: Pan American World Airways Captain Charles F. Blair, Jr., flew a modified North American Aviation P-51C-10-NT Mustang, NX12012, Excalibur III, from Bardufoss, Norway to Fairbanks, Alaska, via the North Pole. He flew the 3,260 miles (5,246.5 kilometers) non-stop in 10 hours, 27 minutes.

After departing Bardufoss at 3:58 p.m., Captain Blair flew north along the E. 20° meridian until crossing the North Pole at an altitude of 22,000 feet (6,706 meters), then south along the W. 160° meridian until reaching N. 70° latitude, and then southeast to Fairbanks.

During the transpolar flight, the Mustang was subjected to air temperatures as low as -25 °F. (-31.6 °C.).

Captain Charles F. Blair, Jr., checks his astrocompass shortly before beginning his transpolar flight, 29 May 1951. (National Air and Space Museum, Smithsonian Institution)
Captain Charles F. Blair, Jr., checks his astrocompass shortly before beginning his transpolar flight, 29 May 1951. ( National Air and Space Museum, Smithsonian Institution)

Captain Blair navigated by using a system of pre-plotted sun lines calculated by Captain Phillip Van Horns Weems, U.S. Navy (Ret.), as a magnetic compass was useless near the Pole and there were no radio navigation aids available.

Charles Blair used this Astrocompass Mark II on his transpolar flight. It is in the collection of the Smithsonian Institution National Air and Space Museum. (NASM2012-02107)

Blair was presented the Harmon International Trophy by President Harry S. Truman, in a ceremony at the White House, 18 November 1952. The Harmon awards are for “the most outstanding international achievements in the art and/or science of aeronautics for the previous year, with the art of flying receiving first consideration.”

Excalibur III being fueled at Bardufoss, Norway, May 1951. (Arkivverkets digitale fotoarkiv)

Charles Blair was commissioned in the United States Naval Reserve in 1931. He was promoted to lieutenant, junior grade, in 1937. During World War II, Blair served as a transport pilot in the U.S. Navy and rose to the rank of captain.

Blair resigned from the Navy in 1952 and the following year accepted a commission in the U.S. Air Force Reserve with the rank of colonel. In 1959 he was promoted to brigadier general.

While serving as a reserve officer, Charlie Blair continued his civilian career as an airline pilot for United Airlines, American Overseas Airlines, and then with Pan American.

Captain Blair was married to actress Maureen O’Hara, whom he had met during one of his 1,575 transatlantic crossings.

Excalibur III is a Dallas, Texas-built North American Aviation P-51C-10-NT Mustang, one of a group of 400 fighters which had been contracted on 5 March 1943. Its North American Aviation serial number is 111-29080, and the U.S. Army Air Forces assigned it serial number 44-10947.

After World War II, 44-10947 was purchased by Paul Mantz, and the Civil Aeronautics Administration registered it as NX1202. Mantz had it painted red and named it Blaze of Noon. Paul Mantz flew NX1202 to win the 1946 and 1947 Bendix Trophy Races. Flown by Linton Carney and renamed The Houstonian, NX1202 placed second in the 1948 Bendix race, and with “Fish” Salmon in the cockpit, it took third place in 1949. Paul Mantz had set several speed records with the Mustang before selling it to Pan American World Airways, Inc., Blair’s employer. Blair named the Mustang Stormy Petrel, but later changed it to Excalibur III.

To increase the Mustang’s range for these long-distance flights, Mantz had removed the standard 90-gallon pressure-molded Firestone self-sealing tanks from each wing and converted the entire wing to a fuel tank (what is known as a “wet wing”).

Test pilot Herman “Fish” Salmon awaits the starter’s signal at the beginning of the 1949 Bendix Trophy Race on Rosamond Dry Lake, California. Paul Mantz had won the 1946 and 1947 races with this P-51C, NX1202, “Blaze of Noon.” (San Diego Air and Space Museum Archive)
Test pilot Herman “Fish” Salmon awaits the starter’s signal at the beginning of the 1949 Bendix Trophy Race on Rosamond Dry Lake, California. Paul Mantz had won the 1946 and 1947 races with this P-51C, NX1202, “Blaze of Noon.” (San Diego Air and Space Museum Archive)

The P-51B and P-51C Mustang 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).

North American Aviation P-51C-10-NT 44-10947, "Excalibur III," at the Steven F. Udvar-Hazy Center, National Air and Space Museum.
North American Aviation P-51C-10-NT 44-10947, “Excalibur III,” at the Steven F. Udvar-Hazy Center, National Air and Space Museum.

P-51Bs and Cs were powered by a right-hand tractor, 1,649-cubic-inch-displacement (27.04-liter) liquid-cooled, supercharged, Packard V-1650-3 or -7 Merlin single overhead cam (SOHC) 60° V-12 engine which produced 1,380 horsepower at Sea Level, at 3,000 r.p.m and 60 inches of manifold pressure (V-1650-3) or 1,490 horsepower at Sea Level, turning 3,000 r.p.m. with 61 inches of manifold pressure (V-1650-7). (Military Power rating, 15 minute limit.) These engines 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), slightly faster than the more numerous P-51D Mustang. The service ceiling was 41,900 feet (12,771 meters). With internal fuel the combat range was 755 miles (1,215 kilometers).

Identical to the Inglewood, California-built North American Aviation P-51B Mustang, this is a Dallas, Texas-built P-51C-1-NT, 42-103023. (North American Aviation, Inc.)
Identical to the Inglewood, California-built North American Aviation P-51B Mustang, this is a Dallas, Texas-built P-51C-1-NT, 42-103023. (North American Aviation, Inc.)

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.

Though the P-51D with its bubble canopy was built in far greater numbers during World War II, the earlier P-51B and P-51C Mustangs were actually faster, so many surplus airplanes were used for racing and record attempts after the war.

In 1952, Pan American World Airways donated Excalibur III to the Smithsonian Institution. Today, completely restored, it is on display at the Steven F. Udvar-Hazy Center in Chantilly, Virginia.

Charles F. Blair, Jr.'s North American Aviation P-51C-10-NT Mustang, Excalibur III, at the Steven F. Udvar-Hazy Center, National Air and Space Museum. (NASM)
North American Aviation P-51C-10-NT Mustang, Excalibur III, at the Steven F. Udvar-Hazy Center, National Air and Space Museum. (NASM)

© 2016, Bryan R. Swopes

18 May 1966–20 June 1966: Sheila Scott

Sheila Scott in the cockpit of her Piper PA-24-260B Comanche G-ATOY, Myth Too, 1966.
Sheila Scott in the cockpit of her Piper PA-24-260 Comanche B, G-ATOY, “Myth Too.

18 May 1966: Sheila Scott (née Sheila Christine Hopkins) departed London Heathrow Airport, London, England, on the first solo around-the-world flight by a British subject, the longest-distance solo flight, and only the third around-the-world flight by a woman. Her airplane was a 1966 Piper PA-24-260 Comanche B, registration G-ATOY, which she had named Myth Too.

Sheila Scott's Piper PA-24-260B Comanche, G-ATOY, Myth II, after her around the world flight. The signatures on the wings and fuselage were collected at stops along the way.
Sheila Scott’s Piper PA-24-260 Comanche B, G-ATOY, “Myth Too,” after her around the world flight. The signatures on the wings and fuselage were collected at stops along the way. (Unattributed)

Departed London, England 18 May 1966
Rome, Italy
Athens, Greece
Damascus, Syria
Barhain
Karachi, Pakistan
Jaipur, India
Delhi, India
Calcutta, India
Rangoon, Burma
Butterworth, Malaysia
Singapore
Bali, Indonesia
Sumbawa, Indonesia
Darwin, Australia
Mount Isa, Australia
Brisbane, Australia
Sydney, Australia
Auckland, New Zealand
Norfolk Island
Nandi, Fiji
Pago Pago, Samoa
Canton Island
Honolulu, HI
San Francisco, CA
Phoenix, AZ
El Paso, TX
Oklahoma City, OK
Louisville, KY
New York, NY
Gander, Newfoundland
Lagens, Azores
Lisbon, Portugal
Arrived London, England 20 June 1966

The Britannia Trophy of the Royal Aero Club of Great Britain.
The Britannia Trophy of the Royal Aero Club of the United Kingdom.

The flight covered approximately 28,658 miles (46,121 kilometers) and took 189 actual flight hours over 33 days.

During her around-the-world flight, Shiela Scott set ten Fédération Aéronautique Internationale (FAI) World Records for Speed Over a Recognised Course: London to Rome, 258.13 kilometers per hour(160.40 miles per hour) (FAI Record File Numbers 4679, 4680); London to Auckland, 41.42 km/h (25.74 mph) #4660, 4661; London to Darwin, 45.67 km/h (28.38 mph) #4666, 4670; London to Fiji Islands, 34.60 km/h (21.50 mph) #4672; 4673; Lisbon to London, 244.00 km/h (151.62 mph) #4956, 4657.

Harmon Aviatrix Trophy (NASM)

For her accomplishments, Ms. Scott was awarded the Silver Medal of the Guild of Pilots; the Brabazon of Tara Award for 1965, 1966 and 1967; the Britannia Trophy of the Royal Aero Club of the United Kingdom, 1968; and the Harmon International Trophy for 1966 and 1970.

Italy gave her the title, Isabella d’Este. Sheila Scott was appointed an Officer of the Most Excellent Order of the British Empire in the New Years Honours List, 1 January 1968.

Sheila Scott flew around the world twice in Myth Too, and a third time in a twin-engine Piper Aztec, Mythre. The Fédération Aéronautique Internationale data base lists 75 records for speed over a recognized course set by Ms. Scott. 31 of these remain current.

In a 1969 interview, Ms. Scott said:

“. . . This must be why I enjoy being in the air alone. But in fact I never feel alone in the air because one has to work so hard and experience such extremes of emotion. The senses, for example, are all highly intensified. The sense of sight. . .when you look down, a pale pink becomes a deep rose; the seas really do look as though they have turquoise gashes in them. . . The sense of smell: . . .up there you can smell everything individually. The people of each country soon learned this on my world flight. It started at Damascus where they filled the plane full of jasmine. . . .”

The Guardian, Saturday, 22 October 1988, Page 39  at Columns 2 and 3

Sheila Christine Hopkins was born 27 April 1922 ¹ at 12 Park Avenue, Worcester, Worcestershire, England. She was the daughter of Harold Reginald Hopkins and Edyth Mary Kenward Hopkins.

Miss Hopkins married Rupert Leamon Bellamy at Kensington, in late 1945. The marriage was dissolved in 1950.

Sheila Scott, Officer of the Most Excellent Order of the British Empire, 12 March 1968. (AP/Worth)

Sheila Scott had been a nurse at Haslar Naval Hospital during World War II. She was an actress on the stage, in films and on television. In 1959 she followed a lifetime ambition and learned to fly. She owned or leased several airplanes which she entered in races or used to establish flight records.

Scott was a commercial pilot, rated in single and multi-engine airplanes, seaplanes and helicopters. She was a member of The Ninety-Nines, founding and serving as governor of the British branch. She was also a member of the Whirly-Girls and the International Association of Licensed Women Pilots.

Sheila Scott was the author of I Must Fly and On Top of the World (Barefoot With Wings in the United States).

Sheila Scott, O.B.E., died of cancer at Royal Marsden Hospital, Chelsea, London, 20 October 1988, at the age of 66 years. ¹

Sheila Scott’s Piper PA-24-260 Comanche B, G-ATOY, “Myth Two,” photographed at Biggin Hill, 15 September 1975. (Photograph © M. West. Used with permission.)

Myth Too was built by the Piper Aircraft Corporation in 1966 and was registered N8893P. It was a PA-24-260B Comanche, an all-metal 4–6 place, single-engine, low-wing monoplane with retractable tricycle landing gear. It is flown by a single pilot and can carry three passengers, though an additional two seats can be mounted at the rear of the passenger cabin.

The airplane is 25 feet, 3-7/16 inches (7.707 meters) long with a wingspan of 35 feet, 11-¾ inches (10.967 meters) with an overall height of 7 feet, 5-11/16 inches (2.278 meters). Empty weight is 1,728 pounds (783.8 kilograms) and maximum gross weight is 3,100 pounds (1,406.1 kilograms).

Piper PA-24-260 Comanche B three view illustration with dimensions in inches.

The Comanche B is powered by an air-cooled, fuel-injected 541.511-cubic-inch-displacement (8.874 liter) Lycoming IO-540-D4A5 6-cylinder overhead valve (OHV) horizontally-opposed engine with a compression ration of 8.5:1, rated at 260 horsepower at 2,700 r.p.m., driving a two-bladed Hartzell constant speed propeller through direct drive. The IO-540-D4A5 weighs 384 pounds (174 kilograms).

Cruise speed is 185 miles per hour (297.7 kilometers per hour). The range is 1,225 miles (1,971.5 kilometers) and the service ceiling is 19,500 feet (5,943.6 meters).

Sheila Scott holds a scale model of her Piper PA-24-260 Comanche B. (Unattributed)

Sheila Scott sold G-ATOY in 1975. It was substantially damaged 6 March 1979 when the engine lost oil pressure then seized after taking off from Elstree Aerodrome, Hertfordshire (EGTR). There were no injuries. The wreck is in the collection of the Scottish National Museum of Flight, East Fortune, East Lothian, Scotland.

The wreck of Myth Too, Piper PA-24-260B Comanche G-ATOY at the Scottish National Museum of Aviation. (Aviation Safety Network)
The wreck of Myth Too, Piper PA-24-260 Comanche B, G-ATOY, at the Scottish National Museum of Aviation. (Aviation Safety Network)

¹ Some sources give her birth year as 1927.

© 2020, Bryan R. Swopes