Harry Tucker’s Lockheed Vega, X4769. (National Archives)
24–25 October 1928: Captain Charles B.D. Collyer, Air Service, United States Army, and Harry J. Tucker flew Tucker’s Lockheed Vega, X4769, from New York to Los Angeles, non-stop, in 24 hours, 55 minutes.
A contemporary newspaper article reported the event:
YANKEE DOODLE SETS NEW MARK
Monoplane Flies Across Continent to Los Angeles in 24 Hours, 55 Minutes
Mines Field, Los Angeles, Oct. 25—(AP)—Setting a new record for a trans-continental non-stop airplane flight from the Atlantic coast to the Pacific, the monoplane Yankee Doodle arrived here at 2:12 p.m. today from New York.
The unofficial time of the flight as announced by Capt. C.D.B. Collyer, pilot and Harry Tucker, owner and passenger, was 24 hours 55 minutes. The best previous time for the westward flight was 26 hours and 50 minutes, made in 1923 by Lieutenants John MacReady [John A. Macready] and Oakley Gelley[Oakley George Kelly].
530 Gallons Carried
The Yankee Doodle hopped off at Roosevelt Field at 4:16:35 p.m. Eastern Standard Time yesterday. The little cigar-shaped white-winged plane was loaded with 530 gallons of gasoline, just about enough for a 24-hour flight, and a check began shortly after landing to determine how much of the fuel was left.
The westward flight covered approximately the course flown over by Col. Arthur Goebel when he piloted his plane to a new West-East non-stop trans-continental record of 18 hours and 55 minutes several weeks ago.
This was the fourth time Tucker has sent his plane into a coast-to-coast grind. The first West to East attempt was unsuccessful but on the second attempt Goebel piloted the machine through to the record.
—The Cornell Daily Sun, Ithaca, New York, Friday, October 26, 1928, Volume XLIX, Number 29 at Page 1, Column 5
Captain Charles B.D. Collyer
Charles Bascum Drury Collyer was born at Nashville, Tennessee, 24 August 1896, the son of Rev. Charles Thomas Collyer. He traveled throughout the world, and lived for a time in Seoul, Korea. Collyer attended Virginia Polytechnic Institute, a military college at Blacksburg, Virginia, as a member of the class of 1919.
Collyer served in the United States Army as a private, first class, being discharged 1 May 1919. He held a commission as a second lieutenant, Aviation Section, Signal Reserve Corps. He was employed as chief pilot, Liberty Flyers, Inc., at Savannah, Georgia.
From 28 June to 22 July 1928, Collyer had flown around the world with John Henry Mears. Collyer was president of the Aviation Services Corporation of New York, which had been formed “to do unusual things in aviation.”
Harry J. Tucker
Harry J. Tucker was variously described as an “auto tycoon” and a “wealthy Santa Monica, California, businessman.” He was born in 1891.
Charles B.D. Collyer and Harry Tucker were killed 3 November 1928 when Yankee Doodle crashed in fog near Venezia, in Yavapai County, Arizona. Collyer was buried at Arlington, National Cemetery, Virginia.
Yankee Doodle was the seventh Lockheed Vega produced (c/n 7). The Vega was a single-engine, high-wing monoplane designed by John Knudsen (“Jack”) Northrop and Gerrard Vultee. The prototype flew for the first time 4 July 1927 at Mines Field, Los Angeles, California.
The Vega was very much a state-of-the-art aircraft for its time. It used a streamlined monocoque fuselage made of strips of vertical-grain spruce pressed into concrete molds and bonded together with cassein glue. These were then attached to former rings. The wing and tail surfaces were fully cantilevered, requiring no bracing wires or struts to support them. They were built of spruce spars and ribs, covered with 3/32-inch (2.4 millimeters) spruce plywood.
Three-view drawing of the Lockheed Vega from a National Advisory Committee for Aeronautics publication. (NASA)
The Lockheed Vega 1 was flown by a single pilot in an open cockpit and could carry up to four passengers in the enclosed cabin. It was 27.5 feet (8.38 meters) long with a wingspan of 41.0 feet (12.50 meters) and height of 8 feet, 6 inches (2.59 meters). The total wing area (including ailerons) was 275 square feet (25.55 square meters). The wing had no dihedral. The leading edges were swept slightly aft, and the trailing edges swept forward. The Vega 1 had an empty weight of 1,650.0 pounds (748.4 kilograms) and a gross weight of 3,200 pounds (1,452 kilograms).
The early Vegas were powered by an air-cooled, normally-aspirated 787.26-cubic-inch-displacement (12.901 liter) Wright Whirlwind Five (J-5C) nine-cylinder radial engine. This was a direct-drive engine with a compression ratio of 5.1:1. The J-5C was rated at 200 horsepower at 1,800 r.p.m., and 220 horsepower at 2,000 r.p.m. It was 2 feet, 10 inches (0.864 meters) long, 3 feet, 9 inches (1.143 meters) in diameter, and weighed 508 pounds (230.4 kilograms).
The Vega had a cruising speed of 110 miles per hour (177 kilometers per hour) with the engine turning 1,500 r.p.m., and a top speed of 135 miles per hour (217 kilometers per hour)—very fast for its time. The airplane had a rate of climb of 925 feet per minute (4.7 meters per second) at Sea Level, decreasing to 405 feet per minute (2.1 meters per second) at 10,000 feet (3,048 meters). Its service ceiling was 15,900 feet (4,846 meters), and the absolute ceiling was 17,800 feet (5,425 meters). The airplane had a fuel capacity of 100 gallons (379 liters), giving it a range of 1,000 miles (1,609 kilometers) at cruise speed.
Twenty-eight Vega 1 airplanes were built by Lockheed Aircraft Company at the factory on Sycamore Street, Hollywood, California, before production of the improved Lockheed Vega 5 began in 1928 and the company moved to its new location at Burbank, California.
The techniques used to build the Vega were very influential in aircraft design. It also began Lockheed’s tradition of naming its airplanes after stars and other astronomical objects.
Lockheed Vega X4769 at NAS San Diego, 1928. (San Diego Air and Space Museum Archives)
First Lieutenant Lowell H. Smith and First Lieutenant John Paul Richter, Air Service, United States Army. (U.S. Air Force)
25 October 1923: First Lieutenant Lowell Herbert Smith and First Lieutenant John P. Richter, Air Service, United States Army, flew a DH-4B from Sumas, Washington, to Tijuana, Mexico, non-stop.
The 1,280 mile (2,060 kilometer) flight was made possible by two air-to-air refuelings from tanker airplanes pre-positioned over Eugene, Oregon, and Sacramento, California. The DH-4B tanker over Eugene was flown by First Lieutenants Virgil Hine and Frank W. Siefert. The Sacramento tanker was flown by Captain Robert J. Erwin and First Lieutenant Oliver R. McNeel. At both locations, Smith and Richter made two refueling contacts before proceeding on their route.
On arrival over Mexico, they circled the Tijuana Customs House, then landed at Rockwell Field, San Diego.
The flight took approximately 12 hours.
On 27 June 1923, Captain Smith and Lieutenant Richter stayed aloft over Rockwell Field, (now, NAS North Island) at San Diego, California, with multiple refuelings. This photograph shows the DH-4B tanker, A.S. 23-467, and receiver on that endurance flight. (U.S. Air Force)
Lowell Herbert Smith was born 8 October 1892 in Santa Barbara County, California. He was the second of four children of Jasper Green Smith and Nora Maude Holland Smith. Beginning in 1915, he flew for the Mexican Army. (Another source says that he flew for the revolutionary bandit, Pancho Villa.) Smith graduated from San Fernando College in 1917. He enlisted in the Aviation Section, Signal Corps, United States Army, 8 June 1917, and attended the Military School of Aeronautics at the University of California. Smith was commissioned as a first lieutenant in the Signal Officers Reserve Corps, 13 December 1917. He was promoted to the rank of captain, Aviation Section, 23 October 1918. On 10 September 1920, that commission was vacated and he was commissioned a captain, Air Service. On 18 November 1922, Smith was discharged as captain and appointed first lieutenant.
On 27 June 1923, Smith and Richter accomplished the first air refueling over Rockwell Field, San Diego, using air techniques that they also used for the border-to-border flight of 25 October 1926. On 28–29 June, Smith and Richter remained airborne over San Diego for 37 hours, 15 minutes, 14½ seconds. For that flight, they were awarded the Distinguished Flying Cross.
From 6 April to 28 September 1924, Lowell Smith was the pilot of Airplane No. 2, the Douglas World Cruiser Chicago, on the first circumnavigation by airplane. After Major Frederick Martin crashed his DWC in Alaska, Smith assumed command of the remaining three aircraft for the rest of the 23,942 nautical mile (44,341 kilometers) flight. For this flight, Smith was awarded the Distinguished Service medal. He was again promoted to captain 4 December 1924.
Smith graduated from the Army Command and General Staff School in 1935. In 1936 he served on a War Department board that established airplane design standards and procedures for the military to order new aircraft. He was promoted to major on 16 June 1936, and to lieutenant colonel on 1 March 1940. Several months later, with the rapid expansion of the Army Air Corps, on 30 August 1940, he was promoted to lieutenant colonel, and then to colonel, 15 March 1941. During World War II, Colonel Smith commanded Davis-Monthan Army Airfield.
Colonel Lowell Herbert Smith, United States Army Air Corps, died as the result of falling from a horse near Tucson, Arizona, 4 November 1945. He was 53 years old. Colonel Smith is buried at the Arlington National Cemetery.
John Paul Richter was born in Virginia, 6 January 1991, the first of five children of Otto Frank Richter, a physician, and Nora Kinney Richter. In 1911 he graduated from the Virginia Agricultural and Mechanical College and Polytechnic Institute with a bachelor of science degree in mechanical engineering. He enlisted in the Aviation Section, Signal Enlisted Reserve Corps 22 May 1917, and was commissioned a first lieutenant 20 November 1917. His commission in the Aviation Section was vacated 12 October 1920 and he was appointed a first lieutenant in the Air Service, effective retroactively to 1 July 1920.
John Richter married Miss Frances K. Fisher in 1925.
Lieutenant Colonel John Paul Richter, United States Army Air Corps, was discharged 31 December 1943. He died 26 April 1964 at the age of 73 years. He is buried at the Gettysburg National Cemetery.
DH-4B A.S. 23-467 (top right) trails a refueling hose for Smith and Richter’s DH-4B near Rockwell Field, San Diego, California, 23 June 1923. (U.S. Air Force)
The Airco DH.4 was a very successful airplane of World War I, designed by Geoffrey de Havilland. The DH.4 (DH-4 in American service) was a two-place, single-engine, two-bay biplane with fixed landing gear. The fuselage and wings were constructed of wood and covered with doped-fabric. The airplane was produced by several manufacturers in Europe and the United States. The DH-4 was 30 feet, 5 inches (9.271 meters) long with a wingspan of 42 feet, 8 inches (13.005 meters) and height of 10 feet, 6 inches (3.200 meters). The DH-4 had an empty weight of 2,391 pounds, (1,085 kilograms) and gross weight of 4,297 pounds (1,949 kilograms). Fuel capacity was 67 gallons (254 liters).
Army Air Service DH-4s were powered by Liberty 12 aircraft engines in place of the Rolls-Royce Eagle VII V-12 of the British-built DH.4 version. The L-12 was water-cooled, normally-aspirated, 1,649.34-cubic-inch-displacement (27.028 liter), single overhead cam (SOHC) 45° V-12 engine. It produced 408 horsepower at 1,800 r.p.m. The L-12 as a right-hand tractor, direct-drive engine and it turned turned a two-bladed fixed-pitch wooden propeller. The Liberty 12 was 67.375 inches (1.711 meters) long, 27.0 inches (0.686 meters) wide, and 41.5 inches (1.054 meters) high. It weighed 844 pounds (383 kilograms).
The Liberty 12 aircraft engine was designed by Jesse G. Vincent of the Packard Motor Car Company and Elbert J. Hall of the Hall-Scott Motor Company. This engine was produced by Ford Motor Company, as well as the Buick and Cadillac Divisions of General Motors, The Lincoln Motor Company (which was formed by Henry Leland, the former manager of Cadillac, specifically to manufacture these aircraft engines), Marmon Motor Car Company and the Packard Motor Car Company. Hall-Scott was too small to produce engines in the numbers required.
The DH-4 had a maximum speed of 124 miles per hour (200 kilometers per hour), service ceiling of 19,600 feet (5,974 meters) and range of 400 miles (644 kilometers).
Many DH-4s were rebuilt as DH-4Bs. These can be identified by the relocated pilot’s cockpit, which was moved aft, closer to the observer’s position. The an enlarged fuel tank was place ahead of the pilot’s cockpit. Following World War II, many were rebuilt with tubular metal frames for the fuselage, replacing the original wooden structure. These aircraft were redesignated DH-4M.
The prototype American DH-4, Dayton-Wright-built airplane, is in the collection of the Smithsonian Institution National Aviation and Space Museum.
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)
