Category Archives: Aviation

Air Force Cross, Chief Master Sergeant Dennis M. Richardson, United States Air Force.

Retired Brig. Gen. Frank Cardile (left) awards retired Chief Master Sgt. Dennis Richardson the Air Force Cross April 5, 2008 at the Francis S. Gabreski Airport in New York. (Staff Sgt. David J. Murphy, U.S. Air Force)

AIR FORCE CROSS

SERGEANT DENNIS M. RICHARDSON

The President of the United States of America, authorized by Title 10, Section 8742, United States Code, takes pleasure in presenting the Air Force Cross to Chief Master Sergeant (Retired), [then Sergeant] Dennis M. Richardson, United States Air Force, for extraordinary heroism in connection with military operations against an opposing armed force as Flight Engineer of an HH-3E Jolly Green rescue helicopter of the 37th Aerospace Rescue and Recovery Squadron, 3d Air Rescue and Recovery Group, DaNang Air Base, Vietnam, in action in Southeast Asia on 14 March 1968. On that date, Sergeant Richardson flew two sorties in an effort to rescue United States Air Force pilots who were surrounded by enemy troops along the Ho Chi Minh Trail. During the initial rescue attempt another helicopter had been driven off and Sergeant Richardson’s helicopter had itself sustained significant battle damage. Despite their situation, and with complete disregard for their own safety, Sergeant Richardson and his crew elected to return and make a second rescue attempt. Coming to a hover 10 feet above the survivor’s position, Sergeant Richardson stood fully exposed in the helicopter door and began lowering the jungle penetrator with one hand while gripping his M-60 machine gun with the other. Unknown to anyone, the enemy had occupied the area but held their fire, waiting to ambush the helicopter. Suddenly intense enemy fire erupted from all quadrants, resulting in additional damage to “Jolly Green 22” and wounding Sergeant Richardson. In an extraordinary display of courage and valor, Sergeant Richardson, despite his wounds, leaned far outside the door and neutralized charging enemy combatants who appeared intent on boarding the helicopter. Sergeant Richardson continued to lay down an effective blanket of defensive fire which enabled the pilot to maneuver safely out of the area. The selfless actions of Sergeant Richardson undoubtedly saved his helicopter and crew from certain disaster. Through his extraordinary heroism, superb airmanship, and aggressiveness in the face of a determined enemy, Sergeant Richardson reflected the highest credit upon himself and the United States Air Force.

Action Date: March 14, 1968

Service: Air Force

Battalion: 37th Aerospace Rescue and Recovery Squadron

Regiment: 3d Air Rescue and Recovery Group

Division: DaNang Air Base, Vietnam

A Sikorsky HH-3E Jolly Green Giant (66-13290) ot the 37th ARRS, hovering in ground effect at Da Nang, 1968. (U.S. Air Force)

Dennis Martin Richardson was born 29 December 1945 at Queens, New York. He was the son of John Joseph (“Jack”) Richardson and Nora Elizabeth Tuohy Richardson.

Richardson enlisted in the United States Air Force, 12 November 1964. He was trained as a helicopter mechanic, and was assigned as crew chief of a Bell UH-1F Iroquois (“Huey”) at Minot Air Force Base in North Dakota. During 1966, he served in Thailand with the 606th Air Commando Squadron. He was next assigned as flight engineer on the Sikorsky HH-3E Jolly Green Giant with the 37th Aerospace Rescue and Recovery Squadron at Da Nang Air Base, Republic of Vietnam.

Richardson returned to the United States and on 11 October 1968, left active duty.

On 30 January 1970, Richardson married Miss Deidre A. O’Brien at the Sacred Heart Church, Staten Island, New York. They would have five children.

Dennis Richardson joined the New York Air National Guard in 1975, serving as a helicopter flight engineer with the 106th Rescue Wing. He retired in 2005.

In addition to the Air Force Cross, during his service in the Vietnam War, Sergeant Richardson was twice awarded the Distinguished Flying Cross and the Purple Heart.

Chief Master Sergeant Dennis Martin Richardson, United States Air Force, died at Carmel, New York, 1 June 2016 at the age of 70 years. He was buried at the Long Island National Cemetery, East Farmingdale, New York.

This was the helicopter on which Sergeant Richardson served, 14 March 1968. The restored Sikorsky HH-3E Jolly Green Giant, 67-14709, on display at the National Museum of the United States Air Force. (NMUSAF)

The SH-3A Sea King (Sikorsky S-61) first flew 11 March 1959, designed as an anti-submarine helicopter for the U.S. Navy. The prototype was designated XHSS-2 Sea King. In 1962, the HSS-2 was redesignated SH-3A Sea King. Many early production aircraft were upgraded through SH-3D, SH-3G, etc. In addition to the original ASW role, the Sea Kings have been widely used for Combat Search and Rescue operations. Marine One, the call sign for the helicopters assigned to the President of the United States, are VH-3D Sea Kings.

The Sikorsky HH-3E (Sikorsky S-61R) is a development of the SH-3A. It earned the nickname Jolly Green Giant during the Vietnam War. It is a dedicated Combat Search and Rescue (CSAR) helicopter flown by the U.S. Air Force, based on the CH-3C transport helicopter. The aircraft is flown by two pilots and the crew includes a flight mechanic and gunner. It is a large twin-engine helicopter with a single main rotor/tail rotor configuration. It has retractable tricycle landing gear and a rear cargo ramp. The rear landing gear retracts into a stub wing on the aft fuselage. The helicopter has an extendable inflight refueling boom.

A Sikorsky HH-3E Jolly Green Giant refuels in flight from a Lockheed MC-130 Combat Talon. (U.S. Air Force)

The HH-3E is 72 feet, 7 inches (22.123 meters) long and 18 feet, 10 inches (5.740 meters) high with all rotors turning. The main rotor has five blades and a diameter of 62 feet (18.898 meters). Each blade has a chord of 1 foot, 6.25 inches (0.464 meters). The main rotor turns at 203 r.p.m., counter-clockwise, as seen from above. (The advancing blade is on the right.) The tail rotor also has five blades and has a diameter of 10 feet, 4 inches (3.150 meters). The blades have a chord of 7–11/32 inches (0.187 meters). The tail rotor turns clockwise as seen from the helicopter’s left. (The advancing blade is below the axis of rotation.) The tail rotor turns 1,244 r.p.m.

Beginning in 1928, an American food company began using a cartoon figure to advertise its "Green Giant" brand of canned peas. Eventually the mascot represented The Green Giant Company's other canned and frozen vegetables. The character is now owned by General Mills.
Beginning in 1928, an American food company began using a cartoon figure to advertise its “Green Giant” brand of canned peas. Eventually the mascot represented The Green Giant Company’s other canned and frozen vegetables. The character is now owned by General Mills.

The HH-3E has an empty weight of 13,341 pounds (6,051 kilograms). The maximum gross weight is 22,050 pounds (10,002 kilograms).

The Jolly Green Giant is powered by two General Electric T58-GE-5 turboshaft engines, which have a Maximum Continuous Power rating of 1,400 shaft horsepower, each, and Military Power rating of 1,500 shaft horsepower. The main transmission is rated for 2,500 horsepower, maximum.

The HH-3E has a cruise speed of 154 miles per hour (248 kilometers per hour) at Sea Level, and a maximum speed of 177 miles per hour (285 kilometers per hour), also at Sea Level. The service ceiling is 14,000 feet (4,267 meters). The HH-3E had a maximum range of 779 miles (1,254 kilometers) with external fuel tanks.

The Jolly Green Giant can be armed with two M60 7.62 mm machine guns.

Sikorsky built 14 HH-3Es. Many CH-3Cs and CH-3Es were upgraded to the HH-3E configuration. Sikorsky built a total of 173 of the S-61R series.

© 2019, Bryan R. Swopes

14 March 1908

A Voisin-Farman I bis at Le musée de l’Air et de l’Espace. (Wikipedia)
A Voisin-Farman I bis at Le musée de l’Air et de l’Espace. (Wikipedia)

14 March 1908: Henry Farman makes the the first flight in his modified Voisin-Farman I bis, an airplane built by the Appareils d’Aviation Les Frères Voisin, founded by brothers Gabriel and Charles Voisin at Billancourt, a suburb of Paris, France.

The Voisin-Farman I was a single-place, single-engine, two-bay biplane with the elevator forward and a “box kite” tail. It was 10.500 meters (34 feet 5.4 inches) long, with a wingspan of 10.000 meters (32 feet, 9.7 inches). The chord of each wing was 2.000 meters (6 feet, 6.7 inches), and vertical gap between the upper and lower wings was 1.500 meters (4 feet, 11.0 inches). There was no sweep or dihedral.

The complete airplane weighed 530 kilograms (1,169 pounds).

The Voisin-Farman I was modified. The wings’ dihedral was changed to improve stability and the span of the tail reduced. The Antoinette engine was replaced with a Renault rated at 50 horsepower, but was quickly changed back to the Antoinette. A tank containing crushed ice was added to the condensed steam cooling system, increasing the time the engine could be run. The modified airplane is known as the Voisin-Farman I bis (also known as the Henri Farman nº 1).

Two-view illustration of L’Aeroplane Henri Farmin no. 1, with dimensions. (l’Aerophile, 16* Annee, No. 3 1 February 1908, at Page 38/{BnF Gallica}

The airplane was powered by a steam-cooled, direct-injected, 487.14 cubic-inch-displacement (7.983 liter) Société Antoinette 8V 90° V-8 direct-drive engine producing 53 horsepower at 1,100 r.p.m. The engine turned a two-bladed pusher propeller. It was designed by Léon Levavasseur. The engine was 1.120 meters (3 feet, 8 inches) long, 0.630 meters (2 feet, 1 inch) wide and (0.540 meters (1 foot, 9 inches) high. It weighed 95 kilograms (209 pounds).

Charles Voisin and Henry Farman, 1907.
Charles Voisin and Henry Farman, 1907. (Unattributed)

© 2019, Bryan R. Swopes

13 March 1977

The number 2 Sikorsky S-76 makes teh type's first flight, 13 March 1977. (Sikorsky Historical Archives)
The number 2 Sikorsky S-76 prototype, s/n 76002, makes the type’s first flight, 13 March 1977. (Sikorsky Historical Archives)

13 March 1977: The protoype Sikorsky S-76A Spirit made its first flight at the company’s Development Flight Center, West Palm Beach, Florida (06FA). This was the number two aircraft, serial number 76002, registered N762SA. Sikorky’s chief pilot, John Dixson, and S-76 program test pilot Nicholas D. Lappos were in the cockpit.

Test pilot Nick Lappos is congratulated following teh first flight of the Sikorsky S-76, 13 March 1977. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)
Test pilot Nick Lappos is congratulated by His Majesty King Hussein bin Talal of Jordan following the first flight of the Sikorsky S-76, 13 March 1977. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)

The prototype was rolled out 11 January 1977.

The Sikorsky S-76 is a twin-engine medium helicopter designed to carry up to 12 passengers 400 nautical miles (460.3 statute miles, 740.8 kilometers) for the offshore oil industry. It is flown by two pilots and is certified for instrument flight. The helicopter can be configured to carry up to thirteen passengers.

The S-76 is used as a passenger transport, executive or VIP aircraft, and in law enforcement, search and rescue, or military service. It is also widely used as a medical transport helicopter.

Prototype Sikorsky S-76A rollout, 11 January 1977. (Sikorsky Historical Archives)

In 1979, Sikorsky proposed the new helicopter for consideration as the U.S. Coast Guard Short Range Recovery Helicopter, along with competitors Aérospatiale and Bell Helicopter. The S-76 was considered to be the most suitable of the three but the company made a business decision to withdraw before any contract was awarded. The Aérospatiale SA-365 Dauphin variant was finally selected and became the MH-65 Dolphin.

Air Logistics accepted the first Sikorsky S-76A production helicopter 27 February 1979. (Sikorsky, a Lockheed Martin Company)
Air Logistics accepted the first Sikorsky S-76A production helicopter, 27 February 1979. (Sikorsky, a Lockheed Martin Company)

The S-76A has an overall length of 52 feet, 6 inches (16.002 meters) with rotors turning, and overall height of 14 feet, 6 inches (4.420 meters). It had an empty weight of 7,132 pounds (3,235 kilograms) and a maximum gross weight of 10,500 pounds (4,763 kilograms).

The four-bladed, fully-articulated main rotor has a diameter of 44 feet, 0 inches (13.411 meters). The main rotor hub is constructed of forged aluminum and uses elastomeric bearings to allow for blade flapping and lead-lag. The blades are made of composite materials formed around a hollow titanium spar. The blade tips are swept to reduce the formation of blade tip vortices. Each blade is 19 feet, 11¾ inches long (6.090 meters). The main rotor turns counter-clockwise, as seen from above. (The advancing blade is on the right.) At 107% NR, the maximum speed with power on, the rotor turns 313 r.p.m.

A four-bladed tail rotor with a diameter of 8 feet, 0 inches (2.438 meters) is mounted on the left side of a pylon in a pusher configuration. The tail rotor turns clockwise as seen from the helicopter’s left. (The advancing blade is below the axis of rotation.)

A Turboméca-powered Sikorsky S-76C in flight over the City of New York. (Sikorsky, a Lockheed Martin Company)

The S-76A was originally powered by two Allison 250-C30 turboshaft engines mounted side-by-side, behind the main transmission. The engines were rated at 557 shaft horsepower (maximum continuous power). 100% torque is 564 foot-pounds. Later production models have used Turboméca and Pratt & Whitney Canada engines.

The S-76A has a cruise speed and maximum speed (VNE) of 155 knots (178 miles per hour/287 kilometers per hour). (The helicopter’s cruise speed is the same as its maximum.) The service ceiling is 15,000 feet (4,572 meters). The maximum altitude for takeoff and landing is 6,900 feet (2,103 meters).

Over a five-day period, 4–9 February 1982, Sikorsky test pilots Nicholas D. Lappos, William Frederick Kramer, Byron Graham, Jr., David R. Wright, and Thomas F. Doyle, Jr., set a series of twelve Fédération Aéronautique Internationale (FAI) speed, time-to-climb and sustained altitude world records while flying a Sikorsky S-76A helicopter, N5445J, at Palm Beach, Florida. These included an absolute world speed record for helicopters (186.69 knots/214.83 miles per hour/345,74 kilometers per hour). Nine of these records remain current.¹

In April 2020, new FAA regulations requiring crash-resistant fuel tanks for new-production aircraft took effect. Lockheed Martin decided not to invest in the engineering required to update the S-76. As such, the helicopter was no longer allowed to be sold in the United States. New Sikorsky S-76Ds continued to be sold to overseas customers. Later in the year, though, production came to an end.

876 Sikorsky S-76 were built. There were 307 S-76A and S-76A+ variants produced, followed by the S-76B, S-76C, -C+ and -C++. The final production model was the S-76D.

Sikorsky S-76D N7621Y, c/n 761021. (Sikorsky, a Lockheed Martin Company)

¹ See “This Day in Aviation” https://www.thisdayinaviation.com/4-february-1982/

© 2025, Bryan R. Swopes

13 March 1974

First flight, Bell 214A, Fort Worth, TX (Veriflite May/June 1974)

13 March 1974: First flight, Bell Model 214A… Test pilot Louis William Hartwig, co-pilot Bob E. Miller, flight test engineer Ron Magnusson.

The Bell 214A was developed from the prototype Bell 214 Huey Plus (which first flew in October 1970 and was powered by a 1,900-shaft horsepower Lycoming T53-L-702 turboshaft engine) for Imperial Iranian Army Aviation. Bell built three prototype 214As, powered by the Lycoming T55-L7C (2,050 shaft horsepower). One of these was shipped to Iran in August 1972 for evaluation.

The production 214A was powered by the Lycoming LTC4B-8D turboshaft, rated at 2,930 shaft horsepower.

Bell 214A Isfahan of the IRIAF, 6-4878 (MSN 27xxx), photographed at Zahhedan International Airport (ZAH), 20 May 2009. (© A. Mahgoli)

Iran ordered 287 Bell 214As. Iran named the Bell 214, “Isfahan,” after a city in Iran where it was planned to build a Bell helicopter production facility to produce additional 214A/Cs, and as many as 350 of the stretched twin-engine Bell 214STs.

The first production BH 214A, 6-4561 (Bell serial number 27004), was built in Texas and delivered in Iran on 26 April 1975. Three days later, flown by Major General Manucheher Khosrowdad, IIAA, and Bell assistant chief production test pilot Clem A. Bailey, 6-4561 set five FAI world records for time to height and altitude. The Bell 214A climbed to a height of 3,000 meters (9,842.52 feet) in 1 minute, 58 seconds; ¹ 6,000 meters (19,685.04 feet) in 5 minutes, 14 seconds; ² and 9,000 meters (29,527.56 feet) in 15 minutes, 5 seconds; ³ The helicopter reached a peak altitude of 9,071 meters (29,760.5 feet), setting a record for altitude without payload.⁴ It was able to maintain an altitude of 9,010 meters (29,560.4 feet) in horizontal flight.⁵

Bell 214A Isfhahan 6-4656. This is the fifth production BH 214A, manufacturer’s serial number 27009. It was photographed at Tabriz International Airport (TBZ) on 7 March 2023. Note the very large exhuast duct of the Lycoming 4B-8D turboshaft engine. (© Mehdi Piltan. Image used with permission.)

Because of the Iranian revolution of 1978–1979, the Isfahan facility was never built. All of the BH 214A/Cs and BH 214STs for Iran were built in Texas. Santions against the Iran regime have prevented any spare parts for these helicopters being delivered to Iran, but it is believed that that country has produced counterfeit parts. It is not known how many of these helicopters remain in service, but a 2018 estimate suggested just 22.

An unknown number of Bell 214As remain in service with the Islamic Republic of Iran Army Aviation. (Photo by IRIB via Scramble Dutch Aviation Society)

Bell went on to produce a commercial variant of the BH 214A, which it designated the Bell 214B BigLifter. This model received a FAA Type Certificate 27 January 1976. On 3 February 1976, a second model, the BH 214B-1, was also certified. The BH 214B-1 has a lower gross weight than the 214B, but the only actual difference between the two models is the aircraft data plate and the flight manual. This was done due to certification standards of various countries which would place the 214B in a “large helicopter” classification.

A Bell 214B BigLifter. (Business Jet Traveler)

Another commercial BH214 variant was also produced, the 214ST. Initially called the “Stretched Twin,” this helicopter featured two turboshaft engines, a 30-inch ( meters) increase in length, and a larger diameter main rotor system. Marketed as the 214ST SuperTransport, this helicopter could be ordered with either fixed skids or fixed tricycle landing gear. A total of just 96 were built, with 48 for Iran. The others were for commercial customers, or the militaries of several countries.

A Bell 214ST Super Transport, G-BKFN (manufacturer’s serial number 28109), of British Caledonian Helicopters, photographed 8 September 1982. (Wikipedia).

¹ FAI Record File Number 1850

² FAI Record File Number 1849

³ FAI Record File Number 1848

⁴ FAI Record File Number 1879

⁵ FAI Record File Number 9935

© 2024, Bryan R. Swopes

13 March 1928

Eileen Vollick

13 March 1928: At Hamilton, Ontario, Canada, Miss Eileen M. Vollick passed her flight test in a Curtiss JN-4 Canuck, and was issued license number 77. She was the first woman licensed as a pilot in Canada.

The following is an article written by Eileen Vollick, prior to her death in 1968 (photographs are from various other sources):

Owen Sound Sun Times

How I became Canada’s first licensed woman pilot
EILEEN M. VOLLICK
Wednesday, August 6, 2008 10:38:00 EDT AM

“Opportunity” was calling in a thousand forms, in a new and thrilling and expanding industry- viz-commercial aviation, and I felt the urge to fly, to become a pioneer and blaze the trail for the women of my country.

Early in March, 1927, Jack V. Elliot, pioneer of commercial aviation in Canada, opened his school and clubhouse at a place called Ghent’s Crossing, overlooking Hamilton Bay. The story of that flying school and clubhouse, the first of its kind in the Dominion, will be handed down to posterity, not only on account of its pioneer proprietor, but for the reason that in the pages of Canadian Aeronautical history will be found the names of young men and incidentally one woman, whose vocations were founded on faith and the future destiny of aviation in our country’s commercial life.

A Curtiss JN-4 Canuck at the Elliott Air Service hangar, Hamilton, Ontario, Canada. (National Aviation Museum)
A Curtiss JN-4 Canuck at the Elliott Air Service hangar, Hamilton, Ontario, Canada. (National Aviation Museum)

My home at that time was on the Beach, and from my bedroom window I could see the activities going at the aerodrome, the cutting down of trees, the dumping of load after load of cinders, to make the track or runway, the building of the hangars, and finally the installing of the planes. Each day as I drove my car past the aerodrome a small still voice whispered “Go ahead, brave the lion in his den and make known your proposition to him.”

I proposed to learn to fly, and fearful of being turned down or laughed at (women had not then entered into this man’s game in Canada.) I hesitated, wondering how much courage or talent was required to fly an airplane. I have never been afraid to go after anything I wanted and to stay until I got it, so, as “the whispering voices”ne day I ventured into the proprietor’s den, and asked him: — “Can a girl learn to fly.” He simply smiled, thinking doubtless I was looking for a thrill, but I soon convinced him I was in earnest, and later I met the Controller of Civil Aviation, Flt. Lieut. A. T. Cowley of Ottawa, who advised me to write the Government for permission to learn to fly commercially, no woman in Canada had previously made such application, and Mr. Elliot was doubtful of my success. However, on June 14th, 1927, I was advised from Ottawa that the matter had been fully considered and in future certificates would be granted to women providing they passed the necessary tests and had reached the age of 19 years, and though it was through my efforts women were admitted into the flying game at Ottawa, had I not been first, some other enterprising girl would have paved the way to put Canadian women on a par with other countries.

I was only 18 years old at that time and could not qualify but with the official benediction over my head I made arrangements with Mr. Elliot and became an ardent disciple of his school.

Eileen M. Vollick with W. Fleming in a Jack Elliott Air Service airplane at Hamilton, Ontario, Canada, ca. 1927–28. (Canada Aviation Museum)

The instruction planes at the Elliot Air Service have a dual control and by means of specially constructed earphones on the helmet the pilot gives his instructions to the student flyer.

My first flight in the air was an epoch of my life never to be forgotten, no matter what I may achieve in the future the exhilaration of that flight will linger when all others are merely an event.

The pilot who took me aloft thought he would either frighten me or find out how much courage I possessed, for though it is against the rules to “stunt” with a passenger, it is of great value for a student and a necessary adjunctive. By “stunts” I mean “spins,” “loops,” “zooms,” all very thrilling and decidedly the acid test for a new flyer, and I got mine for half an hour, satisfying my instructor as to my flying ability.

Eileen Vollick (Canada Aviation and Space Museum)

DESCRIPTION OF MISS VOLLICK’S FIRST FLIGHT

“As I sat in the cockpit I felt quite at home, fear never entered my head and when I saw the earth recede as the winged monster roared and soared skyward, and the familiar scenes below became a vast panorama of checker- boarded fields, neatly arranged toy houses, and silvery threads of streams, the pure joy of it, gave me a thrill which is known only to the air-man who wings his way among the fleecy clouds. Perhaps the most trying sensation of a flight comes at the close, when the plane glides rapidly earthward and one feels that familiar “elevator” feeling but even that sensitiveness passes away after a few flights. A spin or a loop, though significantly spectacular from below, is a simple stunt to the aeronaut and easy to accomplish. In flying the most important factors are “taking off” and “landing.” Anyone can fly straight and keep towards the horizon, but rising from the ground and returning, is a different matter. These two factors are important tests when the government inspector examines a pilot for his or her license.”

Aviation always had a fascination for me even before I realized what a great thing had been accomplished when a motor driven vehicle could be propelled at great speed through the air, and when I actually became an active member in the field my enthusiasm knew no bounds.

I would like to write here, that, when I entered the school of aeronauts I mixed exclusively with men, no other girl or woman attended the lectures, entered the hangars or worked around the planes but myself, and from the first day when I became a student with the cadets, to the time I received my pilot’s license on March 13, 1928, there was not a man amongst them who failed to remember my sex, nor one who spoke a disrespectful word to me, yet at the same time I was one of them, joined in their discussions, donned overalls and often looked more grimy and greasy than the rest. Truly the air-men are gentlemen. Their ambitions were my ambitions, their success was my success, and each one was as eager as the other to help me in any difficulty, I had confidence in them which was never misplaced, and in the years to come when aeronautics are intelligently understood and acknowledged by the world at large, and I am only one amongst thousands of my sex who are trained flyers, my thoughts will revert to the days when I was a student flyer, and I can say then, with all my heart, “happy days, loyal friends.”

I must mention my first instructor Pilot Earl Jellison, under whose guidance I stored away knowledge which later proved invaluable. Writing from Vancouver where he was stationed Pilot Jellison sent congratulations on my success and wrote as follows: “I was very pleased with your ability last summer, and I think you know something of the confidence I had in you when you walked out on the wing to do your famous ‘parachute jump’ into Hamilton Bay.” This incident happened soon after I started to fly, and it takes a great deal of confidence to walk the wing of an airplane and jump into space, especially when the controls are in the hands of a strange pilot, but I felt no fear and evidently he felt none. A flyer must never make acquaintance with “fear” if he or she wants to become a successful pilot. I have never felt afraid, flying high or low, over land or water, and though I began my flying lessons in summer it was off the ice on Hamilton Bay that I took my solo flight, and passed the government tests. As a proof that my sense of “fear” is small, when I took the parachute jump from the wing of the plane into the waters of Hamilton Bay, from an altitude of 2,800 feet, it was a record, being the first Canadian girl to leap from a plane into water. Parachute work, however, was not my ambition. I wanted to fly.

The first Curtiss JN-4 Canuck built by Canadian Aeroplanes Limited, 1917. (Canada Aviation Museum)
The first Curtiss JN-4 Canuck built by Canadian Aeroplanes Limited, 1917. (Canada Aviation Museum)

The summer months passed too quickly. October came, and flying days were drawing to a close at the airport. Soon, the family of cadets would move from the Beach to the city . . . The first week of the New Year saw me down at the winter quarters, situated at the extreme end of Hamilton Bay, in the north section of the city. And I began the most strenuous hard work I have done during the nineteen years of my life.

The oracle of “early morning flying” is an open sesame if the student-flyer wants to become a real success, and after several flights off the ice on Hamilton Bay, I made arrangements with my instructor Pilot Richard Turner, to fly as early as possible.

This necessitated some of the mechanical crew being down at the airport long before the sun rose in the horizon to fuel the plane and warm up the motor ready for flight. It is said that an aviator or aviatrix must be ready at all times day or night whenever a call comes, and this creed is thoroughly instilled into the minds of each student. So up in the morning early, long before the streets were warmed I left my cozy cot, drove my faithful old Ford down to the airport, donned a flying-suit and with the tang of ice and frost upon pilot, plane and student, we rose from the hardened ground, and winged our way over the icy Bay, across the cold waters of Lake Ontario, back to the city, then after “landing” and “rising” several times, we flew back to port, full of early morning pep, which the sluggard abed can never fully comprehend. Once more aboard my car and back home to breakfast. Eight a. m. found me on my way to the Hamilton Cotton Co., where I was textile analyst and an assistant designer.

Flying is, and always will be, my uppermost thought, yet I never neglected my duties at the office, and when Alan V. Young, President of the Cotton Co. gave me leave of absence to try my examination tests, the time off had been well earned.

Flying in the air is not the only qualification for a pilot, he or she must have a theoretical as well as a mechanical knowledge of aircraft. Lectures for students are given three times weekly at night and students must attend regularly or lose some important part of their training. I never missed a lecture, in fact when the Aero-Club of Hamilton started their lectures at the Technical School, I made a point to attend both. I was out for knowledge on aircraft. Performance is the supreme test, and the time was drawing close when I had to prove my worth or fall down in my tracks. I was ready for a cross-country flight, which is one of the government requirements. Tuesday, February 28th, was a bright, clear, cold day, ideal flying weather, and I was bound on a glorious adventure, my cross-country test flight. Accompanied by Pilot R. Turner, we left Hamilton early in the morning, arrived at St. Thomas; landed safely at McManus Field, refuelled the plane and took off for Hamilton, completing the round trip in 2 hours and 25 minutes. After more landings, a lesson or two on the use of skiis . . . and the eventful day finished.

The government inspector had arrived and the cadets waited anxiously. Before a license can be issued, the pilot must make four landings, from a height of 1,500 feet, within 150 feet of a spot designated on the ground, one landing from 5,000 feet with the motor shut off, five figure 8 (eight) turns between two designated marks, and a 175-miles cross-country flight. The day previous to the tests I had the extreme pleasure of taking Captain G. B. Holmes, Government Inspector, for a flight, and he gave me great credit for the able manner in which I handled the plane. On March 13, 1928, (lucky day for me) along with ten other cadets of the Elliot Flying School, I successfully passed the Government Civil Aviation examination, making three three-point landings on the ice with skiis, in place of wheels, to the utmost satisfaction of Captain Holmes, and the hearty congratulations of my instructors, and fellow students.

They give credit, these loyal air-men, for having an iron nerve, and skill of an old war time pilot, “nerve” is a natural gift from God. “Skill,” I owe to my instructors, I have had three of whom I cannot speak too highly, Pilots Earl Jellison, Lennard Tripp, and Richard Turner whose invaluable assiduous instruction and help, enabled me to earn the proud title of “Canada’s First Licensed Woman Pilot” and made my dreams come true.

http://www.owensoundsuntimes.com/2008/08/06/how-i-became-canadas-first-licensed-woman-pilot

An original 1917 Curtiss JN-4C Canuck
An original 1917 Curtiss JN-4C Canuck. (Unattributed)

Mary Eileen Vane Riley ¹ was born 2 August 1908 at Wiarton, Ontario, Dominion of Canada. She was the daughter of James Henry Riley, a laborer, and Marie Baynes Riley. Mr. Riley was killed in an accident in 1911. Mrs. Riley then married George Vollick. Miss Riley was known by her stepfather’s family name. She would have three step-siblings.

Eileen Vollick attended St. Patrick’s High School in Hamilton, Ontario, then worked as a materials analyst for the Hamilton Cotton Company.

Miss Vollick was 5 feet, 0 inches (1.52 meters) tall with brown hair and eyes, and a medium complexion.

On 28 September 1929, Miss Vollick married James Hopkin, a steamfitter who had been born in Scotland. The Hopkins moved to Elmhurst, Long Island, New York. They would have two daughters, Eileen and Audrey.

Eileen Vollick, as she is best known, died in 1968. She was buried at the Woodlawn Cemetery, Bronx, New York.

¹ Also known as Reilly. She used that version of the surname on an immigration document as she entered the United States the day following her marriage. She also stated that she was unaccompanied; marked “S.”, indicating that she was single (unmarried); and listed her new husband as a “friend” whom she planned to visit in Elmhurst, Long Island, New York.

© 2019, Bryan R. Swopes