Concorde G-BOAG lands at LHR. (www.concordest.com)
24 October 2003: At 4:05 p.m. BST, the final commercial flight of the British Airways Concorde came to an end with the landing of G-BOAG at London Heathrow Airport. It landed third in sequence with G-BOAE and G-BOAF after all three supersonic airliners had made a low pass over London.
G-BOAG had flown from New York under the command of Captain Mike Bannister, with First Officer Jonathan Napier and Engineer Officer David Hoyle. There were 100 celebrity passengers on board.
“Alpha Golf,” British Aerospace serial number 100-214, was the final Concorde built in Britain, and, at its retirement, was the lowest-time Concorde in British Airway’s fleet. It first flew at Filton, 21 April 1978, registered G-BFKW. It was delivered to British Airways 6 February 1980. In 1981, 100-214 was re-registered as G-BOAG. During the early 1980s, it was taken out of service and used as a source for parts for the other Concordes, but returned to airworthy status in 1985.
After a series of farewell flights, G-BOAG was retired to The Museum of Flight, Seattle, Washington. It had flown 16,239 hours, made 5,066 takeoffs and landings and had gone supersonic 5,633 times.
Captain Bannister with Concorde, London Heathrow Airport, 2016. (British Airways)
by Captain Sean M. Cross, United States Coast Guard (Retired)
24 October 1969: During the Vietnam War from 1967–1972, eleven U.S. Coast Guard Aviators voluntarily served with high honor and distinction with the U.S. Air Force Aerospace Rescue and Recovery forces in Southeast Asia in the dual role of aircraft commanders and instructor pilots. They regularly risked their lives flying into harm’s way to save airmen in peril of death or capture. Their significant contributions and exceptional performance were highly commended by the Air Force with the award of four Silver Stars, sixteen Distinguished Flying Crosses, and eighty-six Air Medals, in addition to many other recognitions. The previous accolades did not come without cost —designated Coast Guard Aviator #997, Lieutenant Jack Columbus Rittichier was killed in action while attempting to rescue a downed Marine airman in hostile territory on June 9th, 1968. These Aviators carried out their noble mission with heroism and a focus on duty, honor, country and the Coast Guard. Their actions brought honor on themselves, the United States of America, the U.S. Air Force and the U.S. Coast Guard.
Interesting fact – of the roughly 200 Air Force Cross recipients, only 24 are enlisted rank, of which 12 are Pararescuemen (PJ). Nine PJs were awarded Air Force Crosses for Combat SAR missions in Vietnam…of those nine missions – two had Coast Guard Aviators as Aircraft Commanders – this is one (the other was the SCOTCH 3 mission involving LT Lance Eagan, USCG (CGA ’62) on 02 July 1968).
The goal of the combat rescue and recovery units was to get to those in peril before the enemy could capture of kill them. Whether the mission was an extraction or the pickup of a downed airman, each time they were successful it was a win. When it came to official Air Force data, this was labeled a “save,” but a “save” was much more than a statistic to these men. A “save” was a person, and they took it personally.
At Da Nang Air Base, Republic of Vietnam, the 37th Aerospace Rescue and Recovery Squadron (ARRS) was coming up on their 500th “save” in mid-October 1969. Everyone was looking forward to it. They arrived at number 497, then hit a dry spell for about a week. On 24 October, MISTY 11 went down and through a connected series of events, Coast Guard exchange pilots Lieutenant Richard Victor Butchka retrieved numbers 498, 499, and 500, and Lieutenant (j.g.) Robert T. Ritchie claimed numbers 501 and 502.
Similar to MISTY 11, this North American Aviation F-100F-10-NA Super Sabre, 56-3837, was also a FastFAC. It is in the collection of the National Museum of the United States Air Force, Wright-Patterson AFB, Ohio. (U.S. Air Force)
Northeast of Saravane, Laos, MISTY 11, a U.S. Air Force North American Aviation F-100F Super Sabre “Fast FAC”—a jet Forward Air Controller) was designating targets along the Ho Chi Min Trail for ground interdiction strikes when it experienced engine failure due to antiaircraft fire. The stricken aircraft quickly descended to less than 1,000 feet (305 meters) above the terrain. The approximate time was 8:00 a.m. A MAYDAY was broadcast and the two crewmen ejected at low altitude. They parachuted into the jungle-covered mountainous terrain. MISTY 11 Alpha, 1st Lieutenant Alvin Donald Muller, and MISTY 11 Bravo, Captain Jack K. Clapper, were separated by about 800 yards (732 meters) due to the programmed delay in the ejection sequence between the front and rear ejection seats.
The survivors’ position was in a small valley formed by two ridges about 100 meters long oriented north and south. At the north end where the ridges joined, a road was cut 20 meters from the top of the hill. MISTY 11A was on the east side of the valley and MISTY 11B was on the west side.
Area of operation.
Each was equipped with a battery-powered radio and was contacted by an airborne Forward Air Controller (FAC), a North American Aviation OV-10A Bronco, NAIL 07, who had heard their pre-ejection call and was working in the area. The FAC said that he would notify Search and Rescue. MISTY 11A (Muller) informed MISTY 11B and the FAC that his leg was badly broken. MISTY 11B (Clapper) was unhurt.
Less than two hours from notification, two Douglas A-1 Skyraiders—call signs SANDY 11 and 12—and two Sikorsky HH-3E Jolly Green Giant helicopters—JOLLY 28 and 04—from strip alert in Quang Tri were on scene.
JOLLY 28 (HH-3E #66-13280) crew members: Captain Charles D. Langham, USAF (Pilot); Major Charles W. Bond (Co-Pilot); Staff Sergeant James E. Smith (Flight Engineer); and Technical Sergeant Donald G. Smith (Pararescueman)
JOLLY 04 (HH-3E #66-13290) crew members: Lieutenant Richard Victor Butchka, USCG (Pilot); Captain John K. Coder, USAF (Co-Pilot); Sergeant Joseph J. Vai (Flight Engineer); and Airman 1st Class George P. Hoffman III (Pararescueman)
The helicopters went into orbit. One Jolly Green, referred to as the “low bird,” would make the rescue attempt while the second, the “high bird,” would remain in a 3,000-foot (914 meters) orbit as backup. Before sending in JOLLY 28, the two A-1s trolled the area, but their repeated passes brought no response from enemy ground-fire. It was determined that Muller should be rescued first because of his broken leg and at about 11:00 a.m., JOLLY 28 descended toward MISTY 11A.
A Sikorsky HH-3E Jolly Green Giant, 66-13290, of the 37th ARRS, hovering in ground effect at Da Nang, circa 1968. This helicopter was JOLLY 04, flown by Lt. R. V. Butchka, USCG, on 24 October 1969.(U.S. Air Force)
The terrain in the SAR area was rolling foothills with elevations varying from 1,500 feet MSL (Mean Sea Level: describes height above standard Sea Level) in the ravines, to 2,500 feet MSL on the hilltops (500 to 833 meters). The vegetation on these hills varied from dense triple-layered canopy jungles to open areas with tall jungle grass. The entire immediate area around MISTY 11A and B was defended by heavy small arms and automatic weapons as close as 50 feet to the survivors. The proximity of hostile forces to the survivors severely restricted the type of ordnance which could be delivered to protect them. There were scattered variable broken cumulus build-ups in the area with tops to 9,500 feet MSL and bases varying from 2,000 to 3,000 feet AGL (Above Ground Level: describes height above the ground). Visibility below the clouds was excellent.
Lieutenant Butchka, in the “high bird,” JOLLY 04, watched his good friend, Captain Charles Langham, descend for the recovery. JOLLY 28 entered a hover over MISTY 11A and lowered the “PJ,” Don Smith, by hoist. The PJ immediately had the downed airman on the canopy penetrator and gave the cable-up signal. Less than a minute had elapsed. When the penetrator was approximately 10 feet off the ground, the helicopter came under attack.
Butchka saw three sides of the blind canyon twinkling. It appeared that enemy forces had used the downed F-100F crewman as bait for a “flak trap.” The Skyraiders rushed in to suppress the fire, but the opening enemy volley had shot the hoist assembly off its mounts, sending it crashing into the flight engineer’s chest and dumping the PJ and MISTY 11A back on the ground. Realizing the hoist was inoperative, the flight engineer, SSGT James Smith, hit the switch shearing the hoist cable and yelled to Captain Langham to transition JOLLY 28 to forward flight.
Lieutenant Richard Victor Butchka, United States Coast Guard, in the cockpit of a Sikorsky HH-3E Jolly Green Giant. (Butchka Collection)
Above, Butchka punched off his auxiliary fuel tanks and went into a plunging autorotative descent. Seeing Langham’s aircraft smoking and streaming fluid (was hit in the main gearbox and was losing oil pressure), Butchka told him to put the helicopter on the ground. Langham searched for a clear spot and put the aircraft into a small punch bowl-shaped valley. Langham and crew jumped out of the helicopter into the elephant grass, looking up for high bird. They did not have far to look. Butchka’s helicopter was in a 25-foot hover on the left side of Langham’s helicopter with its hoist cable waiting. Butchka expected ground fire from the enemy at any moment. During the swift pick up, the helicopter shuddered with a jolt to the right side. The aircraft’s skin was holed with a gash eight inches long by two inches wide.
Major Charles W. Bond had the honor of being the 500th save.
With the men safely on board, the next problem was getting out of there. Butchka did not want to go back out the way he came because of heavy enemy fire. Weather was hot and humid, pressure altitude was high, and the only other way out presented him with a vertical face rising about 130 feet. It was decision time. Butchka said; “I headed for the face, pulled every bit of power I could (‘pulled the collective to my arm pit’ was the description in another interview), and with a little bit of airspeed drooped the rotor to 94-percent — and just cleared the top.” As he eased over the ridgeline, the JOLLY immediately came under heavy ground fire from a different direction. SANDY lead hadn’t reported anything because he didn’t know where Butchka was. Miraculously they were not hit. However, JOLLY 04 “caught his blades in some trees and is requesting escort out of the area.” A forward air controller, COVEY 297, escorted JOLLY 04 to Lima Site 61, an Air Force TACAN navigation site at Muang Phalan, Laos.
There were still two MISTY crewmembers and Langham’s PJ on the ground at the initial recovery spot. The PJ, Technical Sergeant Donald G. Smith, using his handheld radio, reported “contact with bad guys 35 meters to my west” and directed air strikes bracketing their position. JOLLY 76, a Sikorsky HH-53C Super Jolly Green Giant from the 40th ARRS at Udorn, Thailand, made three recovery attempts but each time received intense ground fire resulting in extensive battle damage to the helicopter. JOLLY 76 sustained severe battle damage, loss of hydraulic systems and associated tail rotor control problems that forced the aircraft to withdraw. JOLLY 76 was escorted out of the area by JOLLY 72 and A-1s SANDY 01 and 04, and successfully recovered at Lima Site 44, an unimproved covert landing strip near Saravane, Laos.
LT Richard Butchka, USCG is congratulated by CPT Charles Langham, USAF following the recovery of his JOLLY 28 aircrew during the MISTY 11 combat rescue. (Butchka Collection)
JOLLY 76 (Sikorsky HH-53C Super Jolly Green Giant) crewmembers: Captain Donald R. Almanzar (Pilot); Captain Peter L. Fekke (Co-Pilot); Staff Sergeant Harold R. Hailey (Flight Engineer); Sergeant Anthony J. McFarr (Pararescueman); Sgt. Douglas W. Crowder (Pararescueman); and Sergeant Gregory Lee Anderson (Aerial Photographer).
JOLLY 15 (Sikorsky HH-3E Jolly Green Giant) crew members: Coast Guard Lieutenant (j.g.) Robert T. Ritchie, USCG (Pilot); Lieutenant Colonel Sidney S. Sosnow , USAF (Co-Pilot); Technical Sergeant Frank Gaydos, Jr. (Flight Engineer); Staff Sergeant Jon K. Hoberg (Pararescueman); and Sgt. Edward K. Rendle (Pararescueman).
A Douglas A-1H Skyraider dive bombing a target during a close air support mission. (U.S. Air Force)
Later that afternoon the JOLLIES tried again. After multiple A-1 passes dropping CBU-19s ( a 130-pound modified dispenser containing 528 canisters with an incapacitating chemical CS—”tear gas”) SANDY 06 and 05 escorted “low bird” JOLLY 15 with Coast Guard Lieutenant (j.g.) Rob Ritchie into the rescue area.
Rob said; “The previous attempts that day were all into the wind approaches. I chose a downwind approach because all indications were the ‘bad guys’ were set up for us to come into the wind and were waiting.” The SANDYs made suppression runs and laid smoke as had been requested – then they joined in a daisy chain of passes that provided protective fire. Ritchie used the smoke for cover, swooped in fast and quickly put the aircraft into a hover over Smith and MISTY 11A. TSgt. Gaydos fearlessly operated the rescue hoist while completely exposed to the hostile fire impacting about him. His reassuringly calm hover instructions to the pilots, ensured Smith and MISTY 11A were quickly brought on board with only slight damage to the aircraft. During Ritchie’s next approach to pick up MISTY 11B they began taking very heavy ground fire on the way in. The element of surprise was no longer there and the North Vietnamese had repositioned. SANDY Lead called the approach off and both A-1s made several suppression runs.
Ritchie commenced his third approach immediately after the suppression runs. He said it was much quieter this time and he came to a hover over MISTY 11B. As the penetrator went down the ground fire became much heavier and the helicopter was taking numerous hits. The utility hydraulics to the hoist was disabled due to ground fire damage to a pressure line and fluid flow was lost. Unable to complete the pickup Ritchie exited the area. JOLLY 15 notified SANDY 03 that he would be unable to remain in the area and commenced a rendezvous for air refueling with KING 03, a Lockheed C-130 Combat King. JOLLY 15 landed at Lima Site 61 at 3:35 p.m.
1LT Don Muller, USAF, MISTY 11A, is assisted down from LTJG Ritchie’s HH-3E, JOLLY 15. (Rotor Review Magazine, Spring ’19)
Two additional tries to pick up MISTY 11B were made to no avail. A tropical thunderstorm moved in and heavy rain fell for the next 30 minutes. A third attempt was made while the squall was passing through and as the storm began to subside, the winds became relatively calm and the previously laid smoke screen began to envelope the area – adversely impacting the rescue helicopters’ visibility and making it more difficult to locate MISTY 11B.
Fortunately, the survivor’s emergency radio was operational and the pilot knew how to use it. By coordinating voice guidance from MISTY 11B on the ground and SPAD 09 (circling overhead), JOLLY 19, another HH-3E, flew over Clapper and lowered a canopy penetrator to him. He climbed onto the device and the helicopter quickly exited the area as soon as Clapper was clear of the trees. The gunner on the rescue helicopter pulled him in the door and the MISTY 11 rescue was successfully concluded at around 6:00 p.m.
JOLLY 19 (Sikorsky HH-3E Jolly Green Giant) from Detachment 1, 40th Aerospace Rescue and Recovery Squadron. Crewmembers: Major Ted L. Smith (Pilot); Major Edward B. Robbins (Co-Pilot); Staff Sergeant Robert E. Hunt (Flight Engineer); Master Sergeant Paul L. Jenkins (Pararescueman); and Sergeant Leland H. Sorensen (Pararescueman).
The following A-1 SANDY forces participated in the event:
SANDY 01 1st Lieutenant Rex V. Huntsman
SANDY 04 Lieutenant Colonel Dick Michaud
SANDY 03 Major Nelson Moffatt
SANDY 07 1st Lieutenant Noel Frisbie
SANDY 05 Captain Bob Crowder
SANDY 06 Captain Glenn C. Dyer
SANDY 11 Captain Jack L. Hudson
SANDY 12 Lieutenant Colonel George D. Miller
Epilogue: For their efforts during this combat rescue the following medals were awarded:
Master Sergeant Donald G. Smith, United States Air Force.
Technical Sergeant Donald G. Smith, USAF, Pararescueman from JOLLY 28 was awarded the Air Force Cross:
The President of the United States of America, authorized by Section 8742, Title 10, United States Code, awards the Air Force Cross to Technical Sergeant Donald G. Smith for extraordinary heroism in military operations against an opposing armed force as a Pararescueman on a HH-3E Rescue Helicopter in Southeast Asia on 24 October 1969. On that date, Sergeant Smith voluntarily descended to the surface on a forest penetrator to assist a downed pilot. As he and the pilot were being raised, hostile fire rendered the hoist inoperative and the cable was sheared, dropping them fifteen feet to the ground. Sergeant Smith’s position was surrounded by hostile forces, and his helicopter was downed by hostile fire. Remaining exceptionally calm, his resolute and decisive presence encouraged other survivors, while his resourcefulness in controlling and directing the aircraft providing suppressive fire, resulted in the safe recovery of all downed personnel. Through his extraordinary heroism, superb airmanship, and aggressiveness in the face of the enemy, Sergeant Smith reflected the highest credit upon himself and the United States Air Force.
Lieutenant Robert T. Ritchie, USCG, was awarded the Silver Star.
The President of the United States of America takes pleasure in presenting the Silver Star (Air Force Award) to Lieutenant, Junior Grade, Robert T. Ritchie, United States Coast Guard, for gallantry in connection with military operations against an opposing armed force while attached to the 37th Aerospace Rescue and Recovery Squadron (USAF). Lieutenant, Junior Grade, Ritchie distinguished himself as Aircraft Commander of an HH-3E rescue helicopter in Southeast Asia on 24 October 1969. On that date, Lieutenant, Junior Grade, Ritchie repeatedly penetrated an area of intense hostile fire in an effort to rescue three downed airmen before battle damage rendered his aircraft incapable of further rescue operations. By his gallantry and devotion to duty, Lieutenant, Junior Grade, Ritchie has reflected great credit upon himself and the United States Air Force.
CPT Charles D. Langham Silver Star medal ceremony
Captain Charles D. Langham, USAF, earned the Silver Star:
Captain Charles D. Langham distinguished himself by gallantry in connection with military operations against an opposing armed force as Aircraft Commander of an HH-3E helicopter in Southeast Asia on 24 October 1969. On that date, while attempting to recover two downed Air Force pilots., Captain Langham’s aircraft was subjected to intense hostile fire. Displaying superb airmanship, Captain Langham nursed his critically damaged aircraft way from the immediate hostile area and effected an emergency landing in a confined, remote area which saved his crew from probable serious injury or possible death. By his gallantry and devotion to duty, Captain Langham has reflected great credit upon himself and the United States Air Force.
LT Richard V. Butchka, USCG, earned the Distinguished Flying Cross with Combat V.
The President of the United States of America takes pleasure in presenting the Distinguished Flying Cross with Combat “V” (Air Force Award) to Lieutenant Richard V. Butchka, United States Coast Guard, for heroism while participating in aerial flight as aircraft Commander of an HH-3E helicopter, attached to the 37th Aerospace Rescue and Recovery Squadron, United States Air Force, in Southeast Asia on 24 October 1969. On that date, in the face of known hostile forces, who had just shot down another rescue helicopter, Lieutenant Butchka, with complete disregard for his own personal safety, skillfully and expeditiously effected the rescue of three crewmen from the downed helicopter. The outstanding heroism and selfless devotion to duty displayed by Lieutenant Butchka reflect great credit upon himself and the United States Coast Guard.
The following Distinguished Flying Cross recipients were also confirmed for this mission: Major Charles W. Bond; Captain John K. Coder; Technical Sergeant Frank Gaydosl Jr.; Sergaeant Joseph J. Vai; Airman 1st Class George P. Hoffman III; Staff Sergeant Jon K. Hoberg; and Lieutenant Colonel. Sidney S. Sosnow.
Misty #132 Jack K. Clapper left the USAF in 1974, went to law school and is a trial lawyer in Novato, California. Donald G. Smith passed away on 12 March 2016 at the age of 80. Richard V. Butchka passed away 28 July 2007 at the age of 66. Misty #119 Alvin Donald (“Devil”) Muller passed away on 16 November 2010 at the age of 67.
SSGT Gregory Lee Anderson, USAF
Aerial Photographer Staff Sergeant Gregory Lee Anderson, crewman on JOLLY 76, was aboard Jolly Green 71, an HH-53B, when it was shot down over Laos, 28 January 1970. SSGT Anderson is listed as Missing in Action. (Active Pursuit)
HH-3E 66-13280 caught fire in flight, 15 April 1970, and crashed near Kontum, Republic of Vietnam. Two of the five crewmen died.
HH-3E 66-13290 was retired to Davis Monthan Air Force Base, Tucson, Arizona, 18 March 1991. It was withdrawn from storage and placed on display with the New York Air National Guard at Westhampton Beach, New York.
Aircraft
Sikorsky HH-3E Jolly Green
The Sikorsky HH-3E (Sikorsky S-61R) 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.
Sikorsky HH-3E Jolly Green Giant 67-14709 at the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio. (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 rpm., 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 rpm.
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 HH-3E Jolly Green Giant (Sikorsky Historical Archives)
William Harvey Dana, NASA Research Pilot. (National Aeronautics and Space Administration E-5327)
24 October 1968: William Harvey Dana takes the first North America Aviation X-15 hypersonic research rocketplane, 56-6670, for the 199th and final flight of the X-15 program.
Carried aloft by NASA’s Boeing NB-52A Stratofortress mothership, 52-003, the first X-15A was launched over Smith Ranch Dry Lake, about half-way between the city of Reno and the NASA High Range Tracking Station at Ely, Nevada, at 10:02:47.3 a.m., Pacific Daylight Time (17:02:47.3 UTC). Bill Dana started the Reaction Motors XLR99-RM-1 rocket engine for a planned 84 second burn. The flight plan called for the X-15 to reach Mach 5.45 and 250,000 feet (76,200 meters).
The rocketplane’s performance was very close to plan, a tribute to Dana’s piloting skill. The engine burned out after 83.8 seconds. The maximum speed was slightly lower than planned at Mach 5.38, while the peak altitude was a little higher, at 255,000 feet (77,724 meters).
Dana glided back to Edwards Air Force Base. The total duration of the flight was 11 minutes, 28.3 seconds.
Dana made his first flight in the North American Aviation X-15 hypersonic research rocketplane on 4 November 1965. He reached a maximum speed of Mach 4.22, and a peak altitude of 80,200 feet (24,445 meters). He made a total of sixteen flights in the X-15s. Dana’s highest speed was Mach 5.38, and his highest altitude, 306,900 feet, (93,543 meters), on 1 November 1966.
This had been 56-6670’s 81st flight, and the 141st time it had been carried aloft aboard a B-52.
A. Scott Crossfield, wearing a David Clark Co. XMC-2 full-pressure suit, which he helped to design and test, with the first of three North American X-15s, 56-6670. (North American Aviation, Inc.)
56-6670 is the first of three X-15s built by North American Aviation’s Los Angeles Division for NASA, the United States Air Force, and the United States Navy, to investigate the effects of hypersonic flight (Mach 5+). On 8 June 1959, North American Aviation Chief Engineering Test Pilot, and former NACA research test pilot, Albert Scott Crossfield, had made the first glide flight of 56-6670, also launched by 52-003.
NASA Research Pilot William H. Dana with North American X-15A 56-6672 on Rogers Dry Lake. (NASA)
From 8 June 1959 to 24 October 1968, the three X-15s were flown by twelve test pilots, three of whom would qualify as astronauts in the X-15. Two would go on to the Apollo Program, and one, Neil Alden Armstrong, would be the first human to set foot on the surface of the Moon, 20 July 1969. Joe Engle would fly the space shuttle. Four of the test pilots, Petersen, White, Rushworth, and Knight, flew in combat during the Vietnam War, with Bob White being awarded the Air Force Cross. Petersen, Rushworth and White reached flag rank.
Overhead view of X-15A-1 56-6670 shows the rocketplane’s overall fineness ratio and short wings. (North American Aviation, Inc.)
Flown by a single pilot/astronaut, the X-15 is a mid-wing monoplane with dorsal and ventral fin/rudders and stabilators. The wing had no dihedral, while the stabilators had a pronounced 15° anhedral. The short wings have an area of 200 square feet (18.58 square meters) and a maximum thickness of just 5%. The leading edges are swept to 25.64°. There are two small flaps but no ailerons. The entire vertical fin pivots for yaw control.
Above 100,000 feet (30,840 meters) altitude, conventional aircraft flight control surfaces are ineffective. The X-15 is equipped with a system of reaction control jets for pitch, roll and yaw control. Hydrogen peroxide was passed through a catalyst to produce steam, which supplied the control thrusters.
The forward landing gear consists of a retractable oleo strut with steerable dual wheels and there are two strut/skids at the rear of the fuselage. The gear is retracted after the X-15 is mounted on the NB-52 and is extended for landing by its own weight.
The rocketplane’s cockpit featured both a conventional control stick as well as side-controllers. It was pressurized with nitrogen gas to prevent fires. The pilot wore an MC-2 full-pressure suit manufactured by the David Clark Company of Worcester, Massachusetts, with an MA-3 helmet. The suit was pressurized below the neck seal with nitrogen, while the helmet was supplied with 100% oxygen. This pressure suit was later changed to the Air Force-standardized A/P22S.
North American Aviation, Inc. X-15A 56-6670 on Rogers Dry Lake, Edwards Air Force Base, California. (NASA)
The X-15 is 50.75 feet (15.469 meters) long with a wing span of 22.36 feet (6.815 meters). The height—the distance between the tips of the dorsal and ventral fins—is 13.5 feet (4.115 meters). The stabilator span is 18.08 feet (5.511 meters). The fuselage is 4.67 feet (1.423 meters) deep and has a maximum width of 7.33 feet (2.234 meters).
The X-15s were built primarily of a nickel/chromium/iron alloy named Inconel X, along with corrosion-resistant steel, titanium and aluminum. Inconel X is both very hard and also able to maintain its strength at the very high temperatures the X-15s were subjected to by aerodynamic heating. It was extremely difficult to machine and special fabrication techniques had to be developed.
X-15 56-6670 with NB-52A 52-003, 13 April 1960. (NASA)
Since the X-15 was built of steel rather than light-weight aluminum, as are most aircraft, it is a heavy machine, weighing approximately 14,600 pounds (6,623 kilograms) empty and 34,000 pounds (15,422 kilograms) when loaded with a pilot and propellants. The X-15s carried as much as 1,300 pounds (590 kilograms) of research instrumentation, and the equipment varied from flight to flight. The minimum flight weight (for high-speed missions): was 31,292 pounds (14,194 kilograms) The maximum weight was 52,117 pounds (23,640 kilograms) at drop (modified X-15A-2 with external propellant tanks).
Initial flights were flown with a 5 foot, 11 inch (1.803 meters)-long air data boom at the nose, but this would later be replaced by the “ball nose” air sensor system. The data boom contained a standard pitot-static system along with angle-of-attack and sideslip vanes. The boom and ball nose were interchangeable.
Delays in the production of the planned Reaction Motors XLR99 rocket engine forced engineers to adapt two vertically-stacked Reaction Motors XLR11-RM-5 four-chamber rocket engines to the X-15 for early flights. This was a well-known engine which was used on the previous rocketplanes. The XLR11 burned a mixture of ethyl alcohol and water with liquid oxygen. Each of the engines’ four chambers could be ignited individually. Each engine was rated at 11,800 pounds of thrust (58.49 kilonewtons) at Sea Level.
Thiokol Reaction Motors Division XLR99-RM-1 rocket engine. (U.S. Air Force)
The Reaction Motors XLR99-RM-1 rocket engine was throttleable by the pilot from 28,500 to 60,000 pounds of thrust. The engine was rated at 50,000 pounds of thrust (222.41 kilonewtons) at Sea Level; 57,000 pounds (253.55 kilonewtons) at 45,000 feet (13,716 meters), the typical drop altitude; and 57,850 pounds (257.33 kilonewtons) of thrust at 100,000 feet (30,480 meters). Individual engines varied slightly. A few produced as much as 61,000 pounds of thrust (271.34 kilonewtons).
The XLR99 burned anhydrous ammonia and liquid oxygen. The flame temperature was approximately 5,000 °F. (2,760 °C.) The engine was cooled with circulating liquid oxygen. To protect the exhaust nozzle, it was flame-sprayed with ceramic coating of zirconium dioxide. The engine is 6 feet, 10 inches (2.083 meters) long and 3 feet, 3.3 inches (0.998 meters) in diameter. It weighs 910 pounds (413 kilograms). The Time Between Overhauls (TBO) is 1 hour of operation, or 100 starts.
The XLR99 proved to be very reliable. 169 X-15 flights were made using the XLR99. 165 of these had successful engine operation. It started on the first attempt 159 times.
The highest speed achieved during the program was with the modified number two ship, X-15A-2 56-6671, flown by Pete Knight to Mach 6.70 (6,620 feet per second/4,520 miles per hour/ kilometers per hour) at 102,700 feet (31,303 meters). On this flight, the rocketplane exceeded its maximum design speed of 6,600 feet per second (2,012 meters per second).
The maximum altitude was reached by Joe Walker, 22 August 1963, when he flew 56-6672 to 354,200 feet (107,960 meters).
The longest flight was flown by Neil Armstrong, 20 April 1962, with a duration of 12 minutes, 28.7 seconds.
The North American Aviation, Inc., X-15A-1, 56-6670, being brought into the Arts and Industries building, June 1969. (Smithsonian Institution Archives SI-A-4145-23-A)
North American Aviation X-15A-1 56-6670 is on display at the Smithsonian Institution National Air and Space Museum. X-15A-2 56-6671 is at the National Museum of the United States Air Force.
North American Aviation Inc./U.S. Air Force/NASA X-15A 56-6670, hypersonic research rocketplane on display at the National Air and Space Museum. (NASM)
Lieutenant Colonel Francis M. Carney, USAF. (FAI 13135-1.jpg)
18–24 October 1961: Lieutenant Colonel Francis Melvin (“Blackie”) Carney, United States Air Force, flying a Kaman HH-43B Huskie, 60-0263, set a series of four Fédération Aéronautique Internationale (FAI) world flight records at Bloomfield, Connecticut.
On 18 October 1961, Lieutenant Colonel Carney set an FAI World Record for Altitude Without Payload when he flew 60-0263 to 10,010 meters (32,841 feet).¹ The following week, on 24 October 1961, Colonel Carney set three more world records, flying the HH-43B to 3,000 meters (9,853 feet) in 2 minutes, 41.5 seconds;² 6,000 meters (19,685 feet) in 6 minutes 49.3 seconds;³ and to 9,000 meters (29,528 feet) in 14 minutes, 31 seconds.⁴
Kaman HH-53B Huskie 60-0263. *Fédération Aéronautique Internationale 13135-2)
This same helicopter, flown by Captain Walter G. McMeen, set an FAI World Record for Altitude with a 1000 kilogram Payload to an altitude of 8,037 meters (26,368 feet) over the Kaman plant at Bloomfield, Connecticut, 25 May 1961.⁵ The following summer, Captain Richard H. Coan set an FAI World Record for Distance Over a Closed Circuit Without Landing of 1,055.16 kilometers (655.65 miles) at Mono Lake, California;⁶ Captain Chester R. Radcliffe, Jr., set an FAI World Record for Distance Without Landing when he flew it from Hill Air Force Base, Utah, to Springfield, Minnesota, a distance of 1,429.80 kilometers (888.44 miles), 5 July 1962.⁷
Kaman HH-43B Huskie 60-263. (FAI)
In 1962, Lieutenant Colonel Carney, then commanding the 3638th Flying Training Squadron (Helicopter), U.S. Air Force, was awarded the American Helicopter Society (now, the Vertical Flight Society) Frederick L. Feinberg Award “For the establishment of four new world records for helicopters on 18 and 24 October, 1961. The records established were the maximum altitude for a Class EID helicopter and three time-to-climb records for all types of helicopters.”
Francis Melvin Carney was born at Roxborough, Pennsylvania, 14 November 1921. He was the son of Francis Jerome Carney, an electrician, and Maggie May Ferguson Carney. His father died in 1929.
Carney registered for Selective Service (conscription), 16 February 1942. He was described as having a light complexion with brown hair and blue eyes. He was 6 feet (1.83 meters) tall and weighed 165 pounds (73 kilograms). Three days earlier, 13 February 1942, he had enlisted in the Army of the United States (AUS) at the U.S. Customs House, Philadelphia, Pennsylvania.
On 12 March 1942, Carney was assigned as an Aviation Cadet, Air Corps, and began flight training. On completion of training, he was commissioned as a second lieutenant, Air Reserve, 22 April 1943.
Lieutenant Carney married Miss Eleanor May Childs, circa 1944. They would have four children, Eric Lance Carney, Ronald Jerome Carney, Randall Wayne Carney, and Robin Carney.
Lieutenant Carney received a permanent commission as a first lieutenant, Air Corps, United States Army, 10 October 1947, with date of rank retroactive to 22 April 1946. When the United States Air Force was established as a separate military service, 1st Lieutenant Carney was transferred from the U.S. Army to the U.S. Air Force.
In 1952 Captain Carney transitioned to helicopters.
With insufficient fuel to return to Shaw Air Force Base, the two H-19s were refueled at the scene. (U.S. Air Force/The State, 28 March 1955, Page 8-A, Columns 1–3)
On 27 March 1955, Major Carney flew one of two Sikorsky H-19 Chickasaw helicopters of the 363rd Tactical Reconnaissance Wing, Shaw Air Force Base, Sumter, South Carolina, in the nighttime rescue of 93 men, women, and children from several tiny islands in Lake Marion, near Eutawville, South Carolina. A sudden increase in wind raised 4 foot waves on the lake, endangering them. One of the islands was too small to land, so Carney’s co-pilot, Captain Robert L. Hess (also reported as Warren C. Hess), climbed down to help lift victims aboard. Major Carney, Captain Hess, 1st Lieutenant Ronald L. Ingraham, pilot of the second H-19, and several others received the Air Force Commendation Medal, presented 29 March by Major General Edward Julius Timberlake, Jr., commanding Ninth Air Force.
Major Carney climbs down from the cockpit of his Sikorsky H-19, while Captain Robert L. Hess stands at right. (Crowson/ The Sumpter Daily Item, 28 March 1955, Page 6, Columns 7 and 8)
In 1955 Major Carney was assigned as commanding officer, 24th Helicopter Squadron at Sewart Air Force Base, Smyrna, Tennessee, flying the Piasecki H-21B Work Horse, providing troop carrier support to US Army; flew to CA 10 October 1956 deployed to Tachikawa Air Base, Japan, aboard the Casablanca-class utility aircraft carrier USS Corregidor (CVU-58).
Lieutenant Colonel Carney commanded the 3638th Flying Training Squadron (Helicopter), 3635th Combat Crew Training Wing (Advanced) at Stead AFB, Reno, Nevada, 1959–1964. Initially, pilots were trained in the H-19B and H-21B helicopters. In 1964, Carney deployed to Vietnam.
Lieutenant Colonel Carney retired from the U.S. Air Force, 20 September 1965. During his 23 years of military service, he had flown as a fighter pilot in World War II and the Korean War, and a helicopter pilot during the Vietnam War. He had been awarded the Distinguished Flying Cross.
Following his retirement for the Air Force, Carney served as Chief Pilot, Carson Helicopters, Inc., Perkasie, Pennsylvania, then in 1984, he opened a helicopter flight school at Quakertown Airport (UKT), Pennsylvania, using two Hiller UH-12C three-place helicopters.
“Blackie” Carney with a Hiller UH-12C at Quakertown Airport, 1984. (Don Boorse/News Herald, 22 February 1984) columns –6
28 June 1994, Carney was flying his green and white 1947 Piper PA-12 Supercruiser, N3807M (s/n 12-2729). While on approach to the Flying M Aerodrome (P91), Heidelberg Township, Germansville, Pennsylvania, he was caught in a downdraft. His airplane flipped over on landing. Carney suffered one fractured vertebrae in his neck and two in his lower back lower back. He was transported by ambulance and admitted to the Lehigh Valley Hospital, Lehigh Township, Pennsylvania, where he remained in stable condition.
Blackie Carnet’s green and white Piper PA-12 Supercruiser, N3807M, upside down at the Flying M Aerodrome (P91), Heidelberg Township, Pennsylvania, 28 June 1994. (Don Fisher/The Morning Call, 29 June 1994, Page 12, Columns 5–7)
Lieutenant Colonel Carney died at Bedminster, Pennsylvania, 30 July 1996. His remains were interred at White Marsh Memorial Park, Prospectville, Pennsylvania.
The record-setting Kaman HH-43B-KA Huskie, 60-0263, at the National Museum of the United States Air Force. (U.S. Air Force)
The Kaman Aircraft Corporation Huskie was used by the U.S. Air Force, U.S. Navy and Marine Corps, primarily for short range rescue operations. It was operated by two pilots and two rescue crewmen.
A turboshaft engine drove a unique system of counter-rotating and intermeshing rotors to provide lift, thrust and directional control. The counter-rotation cancelled the torque effect so no anti-torque, or tail, rotor was necessary. This allowed all of the engine’s power to drive the main rotor system.
The fuselage of the H-43B was 25 feet, 2 inches (7.671 meters) long. Each rotor had a diameter of 47 feet, 0 inches (14.326 meters). It’s height was 15 feet, 6½ inches (4.737 meters). The helicopter’s empty weight was 4,470 pounds (2,028 kilograms) and its maximum gross weight was 8,800 pounds (3,992 kilograms).⁸
The H-43B was powered by one Lycoming T53-L-1B turboshaft engine, rated at 860 shaft horsepower at 21,510 r.p.m. The engine uses a 5-stage axial-flow, 1 stage centrifugal-flow, compressor with a single stage gas producer turbine and single-stage power turbine. A reverse-flow combustion section allows significant reduction in the the engine’s total length. The power turbine drives the output shaft through a 3.22:1 gear reduction. The T53-L-1 is 3 feet, 11.8 inches (1.214 meters) long and 1 foot, 11.0 inches (0.584 meters) in diameter. It weighs 460 pounds (209 kilograms).
The Huskie’s economical cruise speed was 98 miles per hour (158 kilometers per hour), and the maximum speed was 120 miles per hour (193 kilometers per hour). Its hover ceiling out of ground effect (HOGE) was 18,000 feet (5,486 meters), and in ground effect (HIGE) was 20,000 feet (6,096 meters) and it had a range of 235 miles (378 kilometers).
With the call sign Pedro, the HH-43 was a rescue helicopter that served in combat during the Vietnam War.
The record-setting Kaman HH-43B Huskie 60-0263 was last assigned to Detachment 3, 42nd Aerospace Rescue and Recovery Squadron, Kirtland Air Force Base, New Mexico. It is in the collection of the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio.
¹ FAI Record File Number 1870
² FAI Record File Number 13135
³ FAI Record File Number 13056
⁴ FAI Record File Number 13137
⁵ FAI Record File Number 1258
⁶ FAI Record File Number 13154
⁷ FAI Record File Number 13208
⁸ Maximum overload gross weight is 9,150 pounds (4,150 kilograms) at a load factor of 2.0
Convair YF-102 52-7994 on Rogers Dry Lake, Edwards Air Force Base, California. (San Diego Air and Space Museum Archive)
24 October 1953: At Edwards Air Force Base, California, Richard Lowe Johnson, Chief Test Pilot for the Convair Division of the General Dynamics Corporation, took the first prototype YF-102 Delta Dagger, serial number 52-7994, for its first flight.
The YF-102 was a single-seat, single-engine, delta wing fighter designed as an all-weather, missile-armed, Mach 2 interceptor. It was developed from the earlier, experimental, Convair XF-92 Dart. The F-102 was planned for a Westinghouse XJ67-W-1 engine, but when that was not ready in time, a Pratt & Whitney J57-P-11 afterburning turbojet engine was substituted. The J57 was a two-spool, axial-flow engine with a 16-stage compressor section (9 low- and 7-high-pressure stages) and a 3-stage turbine section (1 high- and 2 low-pressure stages). The J57-P-11 was rated at 10,000 pounds of thrust (44.482 kilonewtons), and 16,000 pounds (71.172 kilonewtons) with afterburner.
The first prototype Convair YF-102 Delta Dagger, 52-7994, was completed at the Convair plant in San Diego, 2 October 1953. (Convair Division of General Dynamics)
The prototype had finished assembly at the Convair plant in San Diego, California, on 2 October 1953. It was then shipped by truck to Edwards Air Force Base in the high desert of southern California where final preparations and testing was carried out.
The National Advisory Committee for Aeronautics (NACA) had tested scale models of the YF-102 in the 8-foot HST wind tunnel at the Langley Memorial Aeronautical laboratory and found that significant shock waves were produced at near-sonic speeds. Surprisingly, shock waves were created at the trailing edge of the delta wing. The shock waves caused very high drag that would keep the aircraft from reaching Mach 1, even with the more powerful engine planned for production models.
Convair YF-102 53-1785 with the original fuselage, photographed 31 December 1954. (NASA)
The Republic YF-105 fighter bomber had similar problems, though it did pass the speed of sound. Both aircraft were significantly redesigned to incorporate the “Area Rule,” developed by NACA aerodynamicist Richard T. Whitcomb. Rather than considering the aerodynamics of the fuselage independently, the frontal area of the wings and tail surfaces had to be included to reduce drag. This produced the “wasp waist” or “Coke bottle” shape that the production models of these two fighters were known for.
Convair built two YF-102s before the design was changed, resulting in the YF-102A prototypes and the production F-102A Delta Dagger.
The first prototype Convair YF-102 Delta Dagger, 52-7994, on Rogers Dry Lake, October 1953. (U.S. Air Force)
Several problems showed up on the YF-102’s first flight. Severe buffeting was encountered at high sub-sonic speed. As predicted by NACA, aerodynamic drag prevented the YF-102 from reaching Mach 1 in level flight. There were also problems with the landing gear, the fuel system, and the J57 engine did not produce the rated power.
The production F-102A was considerably larger than the YF-102. The fuselage was lengthened, the wing area and span were increased, and the vertical fin was taller. A more powerful J57-P-23 engine was used. These and other changes increased the F-102A’s gross weight by nearly 1,800 pounds (815 kilograms).
Convair YF-102 52-7994 parked on the dry lake bed, Edwards AFB, California. (U.S. Air Force)
On 2 November 1953, just nine days after the first flight, the Pratt & Whitney J57-P-11 engine flamed out during a test flight. Dick Johnson was unable to restart it and made a forced landing in the desert. The YF-102 was severely damaged and Dick Johnson badly hurt. The flameout was traced to a problem with the the fuel control system. The prototype was written off.
Convair YF-102 Delta Dagger 52-7994 just before touchdown on Rogers Dry Lake. (U.S. Air Force)Wreck of Convair YF-102 52-7994 near Edwards Air Force Base, 2 November 1953. (U.S. Air Force)
Richard Lowe Johnson ¹ was born at Cooperstown, North Dakota, 21 September 1917. He was the eighth of nine children of Swedish immigrants, John N. Johnson, a farmer, and Elna Kristina Helgesten Johnson, a seamstress.
Dick Johnson attended Oregon State College at Corvallis, Oregon, as a member of the Class of 1943. He was a member of the Sigma Alpha Epsilon (ΣΑΕ) fraternity.
Dick Johnson was a pitcher for the college baseball team, and later, played for the Boston Red Sox “farm” (minor league) system.
On 18 June 1942, Johnson enlisted as a private in the Air Corps, United States Army. On 5 November, he was appointed an aviation cadet and assigned to flight training.
Aviation Cadet Johnson married Miss Juanita Blanche Carter, 17 April 1943, at Ocala, Florida. The civil ceremony was officiated by Judge D. R. Smith.
After completing flight training, on 1 October 1943, Richard L. Johnson was commissioned as a second lieutenant, Army of the United States (A.U.S.).
Lieutenant Johnson was assigned to the 66th Fighter Squadron, 57th Fighter Group, Twelfth Air Force, in North Africa, Corsica, and Italy, flying the Republic P-47 Thunderbolt. He was promoted to first lieutenant, A.U.S., 9 August 1944, and just over three months later, 26 November 1944, to the rank of captain, A.U.S. On 14 May 1945, Captain Johnson was promoted to the rank of major, A.U.S. (Major Johnson was assigned a permanent rank of first lieutenant, Air Corps, United States Army, on 5 July 1946, with a date of rank retroactive to 21 September 1945.)
Republic P-47D-25-RE Thunderbolt 42-26421, assigned to the 66th Fighter Squadron, 57th Fighter group, Twelfth Air Force. This airplane was purchased by the employees of Republic Aviation. (American Air Museum in Britain UPL 25505)
During World War II, Major Johnson flew 180 combat missions with the 66th Fighter Squadron. He is officially credited with one air-to-air victory, 1 July 1944. Johnson was awarded the Silver Star, the Distinguished Flying Cross with two oak leaf clusters (3 awards), and the Air Medal with twelve oak leaf clusters (thirteen awards).
In 1946, was assigned to the Air Materiel Command Engineering Test Pilot School at the Army Air Forces Technical Base, Dayton, Ohio (Wright-Patterson Air Force Base). He was the second U.S. Air Force pilot to be publicly acknowledged for breaking the “sound barrier.”
A few weeks after arriving at Dayton, Major Johnson met Miss Alvina Conway Huester, the daughter of an officer in the U.S. Navy. Dick Johnson and his wife Juanita were divorced 8 January 1947, and he married Miss Huester in a ceremony in Henry County, Indiana, 10 January 1947. They would have three children, Kristie, Lisa and Richard.
Richard L. Johnson waves from the cockpit of the record-setting North American Aviation F-86A-1-NA Sabre, 47-611.
Dick Johnson set a Fédération Aéronautique Internationale (FAI) World Record Speed Over a 3 Kilometer Course,² flying the sixth production North American Aviation F-86A-1-NA Sabre, serial number 47-611, at Muroc Air Force Base, California (renamed Edwards AFB in 1949).
During the Korean War, Major Johnson was sent to the war zone to supervise field installations of improvements to the F-86 Sabre. He was “caught” flying “unauthorized” combat missions and was sent home.
Convair Chief Test Pilot Richard Lowe Johnson. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)
Lieutenant Colonel Johnson resigned from the Air Force in 1953 to become the Chief Test Pilot for the Convair Division of General Dynamics. He made the first flights of the YF-102 and the F-106A Delta Dart, 26 December 1956. He also made the first flight of the F-111 on 21 December 1964.
In 1955, Johnson was one of the six founding members of the Society of Experimental test Pilots.
Dick Johnson was Chief Engineering Test Pilot for the General Dynamics F-111 “Aardvark.” In 1967, the Society of Experimental Test Pilots awarded Johnson its Iven C. Kincheloe Award for his work on the F-111 program. In 1977, Dick Johnson, then the Director of Flight and Quality Assurance at General Dynamics, retired.
In 1998, Dick Johnson was inducted into the Aerospace Walk of Honor at Lancaster, California. His commemorative monument is located in front of the Lancaster Public Library on W. Lancaster Boulevard, just West of Cedar Avenue. ³
Lieutenant Colonel Richard Lowe Johnson, United States Air Force, (Retired), died 9 November 2002 at Fort Worth, Texas. He was buried at Arlington National Cemetery, Arlington, Virginia, on 7 January 2003.
Chief Test Pilot Dick Johnson in the cockpit of a Convair B-58A Hustler. (Courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)
¹ Several sources spell Johnson’s middle name as “Loe.”
² FAI Record File Number 9866
³ Various Internet sources repeat the statement that “Richard Johnson has been honored with. . . the Thompson Trophy, Mackay Trophy, Flying Tiger Trophy, Federation Aeronautique Internationale Gold Medal and Golden Plate Award of the American Academy of Achievement. . . .” TDiA has checked the lists of awardees of each of the appropriate organizations and has not found any support for the statement.
24 October 2003: At 4:05 p.m. BST, the final commercial flight of the British Airways Concorde came to an end with the landing of G-BOAG at London Heathrow Airport. It landed third in sequence with G-BOAE and G-BOAF after all three supersonic airliners had made a low pass over London.
“Alpha Golf,” British Aerospace serial number 100-214, was the final Concorde built in Britain, and, at its retirement, was the lowest-time Concorde in British Airway’s fleet. It first flew at Filton, 21 April 1978, registered G-BFKW. It was delivered to British Airways 6 February 1980. In 1981, 100-214 was re-registered as G-BOAG. During the early 1980s, it was taken out of service and used as a source for parts for the other Concordes, but returned to airworthy status in 1985.
