Tag Archives: Combat Search and Rescue

27 September 2008

Sikorsky MH-53M Pave Low IV, 68-8284, “Cowboy 26,” prepares for its final combat mission, Iraq, 27 September 2008. (A1C Jason Epley, U.S. Air Force)

27 September 2008: A United States Air Force Sikorsky MH-53M Pave Low IV special operations helicopter, serial number 68-8284, assigned to the 20th Expeditionary Special Operations Squadron, flew its final combat mission before being withdrawn from service and retired after 40 years and 12,066.6 flight hours.

“Cowboy 26” was flown by Major Philip Cooper, Captain Peter Hettinger, and Colonel Scott Howell, with Technical Sergeant Henry Woodie, Staff Sergeant Shawn Lewis, Senior Airman Eric Harp, and Airman 1st Class Joshua Lucas.

68-8284 was built by the Sikorsky Aircraft Corporation at Bloomfield, Connecticut, as one of 40 HH-53C Super Jolly Green Giants for Combat Search and Rescue (CSAR). It was delivered to the Air Force in August 1968. 68-8284 was assigned to the 40th Air Rescue and Recovery Squadron  at Nakhon Phanom Royal Thai Air Force Base, 1971–1972. It operated as “Jolly Green 55.”

On 5 September 1971, with flight crew Major Jerry R. Thompson, Gary L. Gamble (CP),  FE Raymond Duarte and PJs William D. Brinson and Michael D Vogele, it rescued the survivors of “Knife 33,” a 21st SOS CH-3E that went down in Laos. On 19 December 1971 (Capt Harold O. Jones (P), David G. Daus (CP), FE Jerrold T. Dearmans, with PJs Leon Fullwood and William D. Brinson, the crew of Falcon 74, a 13th TFS/432 TFW F-4D Phantom II which had gone down shot down 17 December by a SAM near Ban Poung Ban in northeastern Laos. Maj. William T. Stanley, Capt. Lester O’Brien were safely recovered.

A U.S. Air Force Sikorsky HH-53C Super Jolly Green Giant hovers to hoist a pararescueman with one downed pilot, while a second waits on the ground, 16 June 1967. The blade tip vortices are visible because of the high humidity. (This image has been reoriented and cropped from the original photograph.) (National Archives at College Park)

8284 was later assigned to the 67th Aerospace Rescue and Recovery Squadron (39th Aerospace Rescue and Recovery Wing) at RAF Woodbridge, Suffolk, England. 68-8284 has been constantly modernized and upgraded. It was initially converted to the MH-53J Pave Low III/Enhanced configuration by the Naval Air Rework Facility, NAS Pensacola, Florida, in the late 1980s. The helicopter was further modified to the MH-53M Pave Low IV configuration at the Naval Air Depot, MCAS Cherry Point, North Carolina.

The MH-53M Pave Low IV is designed for operations in darkness. (Staff Sergeant Aaron Allmon, U.S. Air Force) 080927-F-7823A-433

The MH-53M Pave Low IV is a variant of Sikorsky’s S-65 heavy-lift military transport helicopter series.  The MH-53M is a single main rotor, single tail rotor, twin-engine helicopter. It has a crew of six: 2 pilots, 2 flight engineers and 2 gunners. The Pave Low IV is equipped with Terrain-Following Radar and Forward Looking Infrared (FLIR) for low-level operations in darkness and low visibility.

The MH-53M fuselage is 67 feet, 2.4 inches (20.483 meters) long, and the helicopter has a maximum length of 91 feet, 11.34 inches (28.025 meters) with rotors turning and the refueling boom extended. The height to the top of the main rotor pylon is 17 feet, 1.68 inches (5.224 meters). The maximum height (rotors turning) is 24 feet, 10.88 inches (7.592 meters).

Sikorsky HH-53C 3-view illustration with dimensions. (Sikorsky Historical Archives)

The fully-articulated 6-blade main rotor has a diameter of 72 feet, 2.7 inches (22.014 meters). The main rotor turns counter-clockwise at 185 r.p.m. (100% Nr), as seen from above. (The advancing blade is on the helicopter’s right.) The main rotor blades are built with titanium spars and have -16° of twist. The semi-articulated four-blade tail rotor has a diameter of 16 feet, 0 inches (4.877 meters) and is positioned on the left side of the tail pylon. It turns clockwise at 792 r.p.m., as seen from the helicopter’s left side. (The advancing blade is below the axis of rotation.) The gap between rotor arcs is just 4.437 inches (11.270 centimeters).

Empty, the MH-53M weighs 32,000 pounds (14,515 kilograms). Its maximum takeoff weight is 46,000 pounds (20,865 kilograms).

Its two General Electric T64-GE-100 axial-flow turboshaft engines have a Normal Continuous Power rating of 3,810 shaft horsepower at 85 °F. (30 °C.), Military Power rating of 4,090 shaft horsepower, and a Maximum Power rating of 4,330 shaft horsepower. The T64-GE-100 is 79 inches (2.007 meters) long, 20 inches (0.508 meters) in diameter and weighs 720 pounds (327 kilograms). Output (100% N2) is 13,600 r.p.m.

Two Sikorsky HH-53C Super Jolly Green Giants of the 39th Aerospace Rescue and Recovery Wing fly in formation over Goose Bay, Canada, 11 June 1978. 68-8284 is the ship closest to the camera, painted gray. (TSgt. Robert C. Leach/U.S. Air Force)
Two Sikorsky HH-53C Super Jolly Green Giants of the 39th Aerospace Rescue and Recovery Wing fly in formation over Goose Bay, Labrador, Canada, 11 June 1978. 68-8284 is the ship closest to the camera, painted gray. (TSgt. Robert C. Leach/U.S. Air Force)

The MH-53M has a maximum speed of 196 miles per hour (315 kilometers per hour) and a service ceiling of 16,000 feet (4877 meters). It carries two 450-gallon (1,703 liter) jettisonable fuel tanks under each sponson.

The MH-53M is armed with two M134 7.62mm miniguns and a GAU-18/A .50 caliber machine gun.

A Sikorsky MH-53J Pave Low III Enhanced from the 16th Special Operations Wing ready to refuel from a Lockheed MC-130E Combat Talon, 21 October 2001, classified location Operation Enduring Freedom. (TSGT Scott Reed, USAF) U.S. National Archives 6523525

At the time they were retired, the MH-53Ms were the fastest, heaviest, most powerful helicopters in the United States Air Force inventory.

After leaving Iraq, 68-8284 was transported by C-17 Globemaster III to England. It was loaned to the Royal Air Force Museum Cosford, where it is on display.

Sikorsky MH-53M Pave Low IV 68-8284 with another Pave Low IV on their final mission . 27 September 2008. (U.S. Air Force 080927-F-7823A-409)

Recommended: On a Steel Horse I Ride: A History of the MH-53 Pave Low Helicopters in War and Peace, by Darrel D. Whitcomb. Air University Press, Air Force Research Institute, Maxwell Air Force Base, Alabama, September 2012.

© 2019, Bryan R. Swopes

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26 September 1971: This Day in Coast Guard Aviation History

by Captain Sean M. Cross, United States Coast Guard (Retired)

During the Vietnam conflict 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.

A U.S. Air Force Sikorsky HH-53C Super Jolly Green Giant. (National Archives at College Park)

26 September 1971: A Sikorsky HH-53C Super Jolly Green Giant, crewed by Coast Guard Lieutenant Commander Joseph Lawrence (“Jay”) Crowe, Jr., CGA ‘62 (Pilot), Xxxxxx Hampton (Copilot), William Simm (Flight Engineer), Daniel G. Manion (Pararescue Jumper) and Richard L. Steed (Pararescue Jumper), rescued the crew of a North American Aviation OV-10A Bronco (call sign “RUSTIC 07″), Lieutenant Lansford Elmer Trapp, Jr., and Cambodian observer, Sergeant Chap Khorn, after they ejected from their 12.7mm-damaged aircraft, about 10 miles (16 kilometers) northwest of Kampong Cham, Cambodia.

Lieutenant General Lansford E. Trapp bio: https://www.af.mil/About-Us/Biographies/Display/Article/105437/lieutenant-general-lansford-e-trapp-jr/

Cambodia (Encyclopedia Britannica)

A little more…(much of this content was slightly modified from the book Leave No Man Behind: The Saga of Combat Search and Rescue by George Galdorisi and Thomas Phillips, pages 393 and 394)

To better cover the southern portion of South Vietnam and be closer to the increasing levels of operations in Cambodia, the 37th Aerospace Rescue and Recovery Squadron (ARRS) had for some time maintained a pair of HH-53Cs at Bien Hoa Air Base, about fifteen miles northeast of Saigon.  On September 26, 1971, it was Coast Guard exchange pilot Lieutenant Commander Joseph “Jay” Crowe’s turn to stage at the forward operating location (FOL). Standing the alert with his crew, Hampton, Simm, Manion, and Steed, they were scrambled to rescue of the crew of an OV-10A from the 19th TASS who shared the ramp at Bien Hoa.

A U.S. Air Force North American Aviation OV-10A-5-NH Bronco, 67-14605, fires a white phosphorous rocket. (TSGT Bill Thompson, United States Air Force DFST8505744)

The Rustic FAC, the call sign that any FAC [Forward Air Controller] operating in Cambodia used, regardless of squadron, had fallen victim to a “.50-caliber trap” when it was hit at 3,500 feet (1,067 meters) by converging fire from four 12.7mm AA machine guns ringing the perimeter of a small village about ten miles (16 kilometers) northwest of the Mekong River town of Kampong Cham. When grouped as a battery, the 12.7 mm guns, “heavy guns” of the southern air war (where the heavy AA weapons of Laos and North Vietnam had not yet appeared in large numbers), were still quite deadly. The Bronco pilot, 1st Lieutenant Lansford Trapp, and his observer, Cambodian Sgt. Chap Khom, had parachuted down into the apex of the gun formation, and the hostile forces accompanying the AAA gunners were in no rush to go get them.

In an interview with his grandson recorded in 2018, retired General Lansford E. Trapp described the incident:

“When I was a lieutenant, and this would have been in 1971, I was flying an observation aircraft over in Vietnam. I was on a mission over in Cambodia and we were helping ground forces who were fighting against bad guys over there. That ensuing battle that went on as I was flying over head in my airplane, we actually got hit by ground fire and the left wing of the airplane caught on fire.

“I had a Cambodian interpreter sitting in my back seat, a Sergeant Chung (Khorn), and it was his seventh ride in an airplane. I didn’t even know that the wing was on fire until one of the other airplanes came by and said “hey your left wing is on fire”. So, I looked out, my wing was on fire, and we decided that I was gonna be able to land at one of the airports that was right there. So, we came in and tried to land, but I lost control of the airplane. So, I pushed the power back in and climbed up over the airfield. Then the left wing burned off, and so we started in a pretty good spiral into the wing that had burned off. We ejected from the airplane.

“Sergeant Corn (Khorn) went out first, and then I went out. The craziest thing was that we used to fly with about 250 to 300 big maps, so we could look at the country as we were trying to figure out where we were. Those all came flying out of the cockpit as we ejected. It looked like confetti outside. As we came down sergeant Corn he got burned pretty bad from the wing fire, and I banged my ankle up pretty badly, but we were OK. We got picked up by friendly forces and I got a nice helicopter ride back to home base that night.”

A gunner looks over a General Electric GAU2/A minigun, while his aircraft flies formation with a Sikorsky HH-53C Super Jolly Green Giant over Southeast Asia. (U.S. Air Force)

Crowe’s Jolly approached at 8,000 feet (2,438 meters), safely above the range of the still-active hostile guns, while the A-1H Sandys of the 1st Special Operations Squadron (SOS) went in low to begin their routine of locating the survivors and the hostile guns. In the flat and relatively open terrain of central Cambodia, penetrating the ring of guns was going to be dicey, there not being the ridges, karsts, and dense vegetation of the 37th’s regular operating area to provide a modicum of masking for the helicopter. By this stage of the war, a low, treetop-hugging approach by the rescue helicopter was a well-known procedure, and the enemy gunners would be waiting for it, scanning the low horizon for the rescue helicopter sure to follow on the heels of the tough Skyraiders. Each gun guarded its quadrant of the circle around the downed airmen, waiting.

A Douglas A-1H Skyraider dive bombing a target during a close air support mission. (U.S. Air Force)

Crowe decided to use a variation of the diving spiral approach he had used June 4th with success, rescuing a Covey FAC crew up in southern Laos. Rather than descending some distance away prior to a low-level run-in, he entered an autorotation from directly overhead, copilot Hampton pulling the throttles of the twin engines back, and Crowe lowering the collective stick. Down the helicopter fell, with the rush of air up through the rotors keeping the blades spinning, while the engines idled (relatively quietly). The blades are unloaded in an autorotative descent, so the characteristic whop-whop is virtually eliminated, and with the engines at idle, there is significantly less of the distinctive noises that normally come from the helicopter.

With the Sandys rumbling around, strafing and bombing and attracting the eye of the gunners, the diminished but still telltale sounds made by the falling Jolly were masked.  Crowe kept the helicopter in a steep turn, spiraling down inside the perimeter of the four guns around the downed aircrew, literally behind their backs, careful not to swing out too wide, where he might catch a gunner’s eye. The Jolly would be easily seen should anyone glance straight up, luckily the last place a sane gunner would be looking for a helicopter.  They were falling out of the sky at more than five thousand feet per minute. As the Jolly approached the ground, Crowe began to level off, converting vertical speed to speed across the ground, still spiraling, and then raised the nose to decelerate.

HH-53C (VIRIN: DF-ST-83-02388)

At the same time, Hampton slowly and smoothly pushed the engine throttles forward, to accelerate them back into normal speed and gently engage their drive wheels with the spinning gears of the main rotors. The accelerating engines and the rotors digging into the air as Crowe pulled up on the collective and flared into a quick-stop created loud rotor beats, accenting the whine of jet turbines accelerating to maximum power, announcing their arrival to all. But the helicopter was safely down beneath the trees in a hover, and the telltale was too late to help the gunners acquire their target. This tight spiral autorotative descent and recovery to a hover requires a superior feel for the helicopter, and exquisite coordination with the copilot to return the rotors to engine-driven flight smoothly at just the right instant. Done right, the procedure is a dramatic and breathtaking maneuver and a grand entrance. But the room for error is very small, and a botched maneuver is perilous and very unforgiving.

It was not a gambit to be repeated very often; if the gunners had detected the helicopter, Crowe and company would have found themselves in a deadly crossfire. But this day it was brilliant: a tactical surprise, completely unexpected, and therefore completely effective. The Jolly crew snatched the two men quickly and escaped out of the circle with a low-level departure. A climbing spiral back up from the center of the guns, with the gunners now alerted, was clearly out of the question. The helicopter received only sporadic fire as it left the scene in the typical low-level escape, while taking no casualties.

Epilogue

Lieutenant Commander Joseph Lawrence Crowe, Jr., U.S. Coast Guard. (Sean M. Cross Collection)

After graduation from high school in Weston, Massachusetts in 1958, Jay received an appointment to the U.S. Coast Guard Academy, New London, Connecticut. Commissioned an Ensign in 1962, he served a tour at sea and then was assigned to naval flight training. Receiving his wings in 1965, he served at Coast Guard Air Stations San Francisco, California, Barbers Point, Hawaii; Cape Cod, Massachusetts; Port Angeles, Washington; Annette Island Alaska, and Sitka, Alaska.

He served during the Vietnam War on an exchange tour with the U.S. Air Force as a Combat Rescue Crew commander with the 37th ARRS Jolly Green Giants in Da Nang AB, RVN.

Jay was a 1981 graduate of the Air War College. He served as Commanding Officer Coast Guard Air Station Port Angeles, Washington, and Coast Guard Air Station Cape Cod, Massachusetts. His final assignment before retirement was as Chief, Operations Division, 11th Coast Guard District, Long Beach, California.

During Jay’s distinguished career he was awarded a Legion of Merit, three Distinguished Flying Cross Medals, nine Air Medals, two Meritorious Service Medals. Three Coast Guard Commendation Medals, a Coast Guard Achievement Medal, and a Meritorious Unit Commendation. Hangar 3172 at Air Station Cape Cod, Massachusetts, was named in his honor.

Captain Crowe flew west crossing the bar February 22, 2003. His family was at his side.

Aircraft

Sikorsky HH-53C Super Jolly Green Giant three-view illustration with dimensions. (Sikorsky Historical Archives)

The MH-53M Pave Low IV is a variant of Sikorsky’s S-65 heavy-lift military transport helicopter series.  The MH-53M is a single main rotor, single tail rotor, twin-engine helicopter. It has a crew of six: 2 pilots, 2 flight engineers and 2 gunners. The Pave Low IV is equipped with Terrain-Following Radar and Forward Looking Infrared (FLIR) for low-level operations in darkness and low visibility.

The MH-53M fuselage is 67 feet, 2.4 inches (20.483 meters) long, and the helicopter has a maximum length of 91 feet, 11.34 inches (28.025 meters) with rotors turning and the refueling boom extended. The height to the top of the main rotor pylon is 17 feet, 1.68 inches (5.224 meters). The maximum height (rotors turning) is 24 feet, 10.88 inches (7.592 meters).

The fully-articulated 6-blade main rotor has a diameter of 72 feet, 2.7 inches (22.014 meters). The main rotor turns counter-clockwise at 185 r.p.m. (100% Nr), as seen from above. (The advancing blade is on the helicopter’s right.) The main rotor blades are built with titanium spars and have -16° of twist. The semi-articulated four-blade tail rotor has a diameter of 16 feet, 0 inches (4.877 meters) and is positioned on the left side of the tail pylon. It turns clockwise at 792 r.p.m., as seen from the helicopter’s left side. (The advancing blade is below the axis of rotation.) The gap between rotor arcs is just 4.437 inches (11.270 centimeters).

Empty, the MH-53M weighs 32,000 pounds (14,515 kilograms). Its maximum takeoff weight is 46,000 pounds (20,865 kilograms).

Its two General Electric T64-GE-100 axial-flow turboshaft engines have a Normal Continuous Power rating of 3,810 shaft horsepower at 85 °F. (30 °C.), Military Power rating of 4,090 shaft horsepower, and a Maximum Power rating of 4,330 shaft horsepower. The T64-GE-100 is 79 inches (2.007 meters) long, 20 inches (0.508 meters) in diameter and weighs 720 pounds (327 kilograms). Output (100% N2) is 13,600 r.p.m.

The MH-53M has a maximum speed of 196 miles per hour (315 kilometers per hour) and a service ceiling of 16,000 feet (4877 meters). It carries two 450-gallon (1,703 liter) jettisonable fuel tanks under each sponson.

The MH-53M is armed with two M134 7.62mm miniguns and a GAU-18/A .50 caliber machine gun.

© 2020, Sean M. Cross

For additional reading, see:

Coast Guard Aviation in Vietnam

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18 July 1967

18 July 1967: For the first time, a U.S. Air Force Sikorsky HH-3E Jolly Green Giant combat search and rescue helicopter refueled in flight from a Lockheed HC-130P Combat King command and control aircraft during an actual rescue mission in Southeast Asia.

A Lockheed HC-130P Combat King refuels a Sikorsky HH-3E Jolly Green Giant, with escorting Douglas A-1E and A-1H Skyraiders, Southeast Asia, 1968. (U.S. Air Force)

© 2015, Bryan R. Swopes

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19 June 1968

Lieutenant Clyde Everett Lassen, United States Navy
Lieutenant Clyde Everett Lassen, United States Navy

The MEDAL OF HONOR to

Lieutenant Clyde E. Lassen, United States Navy

For service as set forth in the following

CITATION

For conspicuous gallantry and intrepidity at the risk of his life above and beyond the call of duty on 19 June 1968 as pilot and aircraft commander of a search and rescue helicopter, attached to Helicopter Support Squadron Seven, Detachment One Hundred Four, embarked in USS Preble (DLG 15), during operations against enemy forces in North Vietnam.

Launched shortly after midnight to attempt the rescue of two downed aviators, Lieutenant (then Lieutenant, Junior Grade) Lassen skillfully piloted his aircraft over unknown and hostile terrain to a steep, tree-covered hill on which the survivors had been located.

Although enemy fire was being directed at the helicopter, he initially landed in a clear area near the base of the hill, but, due to the dense undergrowth, the survivors could not reach the helicopter. With the aid of flare illumination, Lieutenant Lassen successfully accomplished a hover between two trees at the survivor’s position. Illumination was abruptly lost as the last of the flares were expended, and the helicopter collided with a tree, commencing a sharp descent.

Expertly righting his aircraft and maneuvering clear, Lieutenant Lassen remained in the area, determined to make another rescue attempt, and encouraged the downed aviators while awaiting resumption of flare illumination. After another unsuccessful, illuminated, rescue attempt, and with his fuel dangerously low and his aircraft significantly damaged, he launched again and commenced another approach in the face of the continuing enemy opposition.

When flare illumination was again lost, Lieutenant Lassen, fully aware of the dangers in clearly revealing his position to the enemy, turned on his landing lights and completed the landing. On this attempt, the survivors were able to make their way to the helicopter. Enroute to the coast, Lieutenant Lassen encountered and successfully evaded additional hostile antiaircraft fire and, with fuel for only five minutes of flight remaining, landed safely aboard USS Jouett (DLG 29).

His courageous and daring actions, determination, and extraordinary airmanship in the face of great risk sustain and enhance the finest traditions of the United States Naval Service.

 

Lieutenant (Junior Grade) Clyde Everett Lassen was the Officer in Charge of Detachment 104 of Helicopter Support Squadron SEVEN (HC-7), the “Sea Devils,” aboard USS Preble (DLG-15). The assignment was Combat Search and Rescue.

McDonnell F-4J-31-MC Phantom II, Bu. No. 153856, of Fighter Squadron Thirty-Three (VF-33) lands aboard USS America (CVA-66) circa 1968. This Phantom is a squadron mate of Root Beer 210. (U.S.Navy)
McDonnell F-4J-31-MC Phantom II, Bu. No. 153856, of Fighter Squadron Thirty-Three (VF-33) “Tarsiers,” lands aboard USS America (CVA-66) circa 1968. This Phantom is a squadron mate of Root Beer 210. (U.S.Navy)

On the night of 18/19 June 1968, a flight of three aircraft from the aircraft carrier USS America (CV-66) were on a bombing mission over North Vietnam. Root Beer 210 was a McDonnell Douglas F-4J-33-MC Phantom II, Bu. No. 155546, flown by Lieutenant Commander John “Claw” Holtzclaw and Lieutenant Commander John A. “Zeke” Burns. Shortly after midnight, two SA-2 surface to air missiles were fired at the Phantom. Holtzclaw and Burns evaded them, but a third missile detonated very close to the fighter bomber, destroying the outer one-third of the right wing. With their airplane critically damaged and on fire, the two naval aviators were forced to eject over enemy territory. They parachuted into a rice paddy and could hear enemy soldiers talking nearby. Burns had suffered a broken leg as well as other injuries.

USS Preble (DLG-15)
USS Preble (DLG-15), a Farragut-class guided missile frigate. (U.S. Navy)

Aboard the guided missile frigate USS Preble (DLG-15), Lieutenant (junior grade) Clyde Lassen and his flight crew were awakened and assigned to rescue the crew of Root Beer 210, 70 miles (113 kilometers) away in total darkness. Lassen and his co-pilot, Lieutenant (j.g.) LeRoy Cook and gunners Aviation Electrician’s Mate 2nd Class (AE2) Bruce Dallas and Aviation Machinist’s Mate 3rd Class (ADJ3) Don West, took off from Preble at 0022 hours aboard their Kaman SH-2A Seasprite helicopter, call sign Clementine Two, and were vectored by radar to the location of the downed aircrew. The glow of the burning Phantom could be seen from 30 miles (48 kilometers) away. They arrived on scene at 0141 hours. Holtzclaw and Burns were in immediate need of rescue as the enemy was closing in.

The crew of Clementine 2, left to right, Lt. (j.g.) Clyde E. Lassen, AE2 Bruce Dallas, ADJ3 Don West, Lt. (j.g.) LeRoy Cook. (U.S. Navy)
The crew of Clementine Two, left to right, Lt. (j.g.) Clyde E. Lassen, AE2 Bruce Dallas, ADJ3 Don West, Lt. (j.g.) C. LeRoy Cook. (U.S. Navy)

Holtzclaw and Burns were on a hillside covered with very tall trees, making it impossible for the Seasprite to land. Parachute flares dropped by supporting aircraft illuminated the area. The pickup would have to be made using a “jungle penetrator” attached to the helicopter’s rescue hoist. But the single-engine helicopter was already fully loaded with its four-man crew and their weapons and ammunition. It could not pick up both fliers while hovering out of ground effect above the trees. Lassen ordered his co-pilot to dump fuel to reduce the weight.

As Lassen hovered into position to make the hoist pickup, the overhead flares went out, leaving the jungle totally dark. Unable to see, Lassen collided with a tree causing damage to the horizontal stabilizer and the right side cabin door. He narrowly avoided a crash.

Clementine Two moved away while they awaited the arrival of another flare aircraft. They were soon engaged by enemy ground fire and the helicopter gunners returned fire with their M-60 machine guns.

On several occasions, Lassen landed the SH-2A in a rice paddy to pickup Holtzclaw and Burns, but enemy gunfire prevent them from reaching the helicopter, which repeatedly had to pull back.

Finally, the crew of Root Beer 210 found their way to the bottom of the slope and Clementine Two landed in a rice paddy about 60 yards (55 meters) away. A fierce firefight between the North Vietnamese soldiers and the gunners of the Navy helicopter took place. Lassen held the Seasprite in a hover to prevent it from sinking into the mud. The gunners jumped down to assist Holtzclaw and Burns aboard. As soon as they were loaded, Lassen immediately took off and left the area, climbed to 4,000 feet (1,220 meters) and headed toward the South China Sea, twenty miles (32 kilometers) away. The helicopter had only thirty minutes of fuel remaining. During the flight, the right cabin door, which had been damaged when the helicopter hit the tree, came off and fell away into the darkness.

USS Jouett (DLG-29)
USS Jouett (DLG-29), a Belknap-class guided missile frigate. (U.S. Navy)

Clementine Two was too far away to make it back to Preble, so they turned toward USS Jouett (DLG-29). Commander Destroyer Squadron One, Captain Robert Hayes, commanding Jouett, turned his ship toward the shore and proceeded at full speed, turning on all of the ship’s lights so that Lassen would be able to find it. Jouett came within 3 miles (4.8 kilometers) of the beach. With almost no fuel remaining, Lassen made a straight-in approach and landing.

Lieutenant Commander John A. Burns aboard USS Jouett. (U.S. Navy)

For his actions on 19 June 1968, Lieutenant Clyde Everett Lassen was awarded the Medal of Honor. Lieutenant (j.g.) LeRoy Cook received the Navy Cross. AE2 Bruce Dallas and AE3 Don West each received the Silver Star.

Kaman UH-2A Seasprite Bu. No. 149764, photographed November 1967. Lieutenant (j.g.) Clyde Everett Lassen flew this helicopter during the rescue of 19 January 1968. (U.S. Navy)
Kaman UH-2A Seasprite Bu. No. 149764, photographed November 1967. Lieutenant (j.g.) Clyde Everett Lassen flew this helicopter during the rescue of 19 January 1968. (U.S. Navy)

Clementine Two was a Kaman SH-2A Seasprite, Bu. No. 149764 (c/n 66). The SH-2A is 52 feet, 2.2 inches (15.905 meters) long with rotors turning, with an overall height of 14 feet, 8.6 inches (4.486 meters). The four-bladed main rotor has a diameter of 44 feet, 0 inches (13.411 meters) and rotates counter-clockwise, as seen from above (the advanicng blade is on the helicopter’s right). The blades are controlled by Kaman’s unique servo flap system. The three-bladed tail rotor is mounted on the left side of a pylon and rotates clockwise, as seen from the helicopter’s left (The advancing blade is below the axis of rotation). The helicopter’s main landing gear was retractable. The SH-2A has and empty weight is 6,110 pounds (2,771 kilograms) and maximum takeoff weight is 10,000 pounds (4,536 kilograms).

The SH-2A is powered by a single General Electric T58-GE-8B turbine engine.  The T58 is a free power turboshaft, with a 10-stage axial-flow compressor section, an annular combustion chamber with 16 burner nozzles, and a 3-stage turbine (2 gas-generator stages and a single power-turbine stage). The T58-GE-8B has a Normal Power rating of 1,050 shaft horsepower at 19,500 r.p.m. at Sea Level, and Military Power rating of 1,250 shaft horsepower at 19,500 r.p.m. The engine is 1 foot, 8.9 inches (0.531 meters) in diameter, 4 feet, 11.0 inches (1.499 meters) long, and weighs 305 pounds (138 kilograms).

The SH-2A Seasprite has a Hover Ceiling Out of Ground Effect (HOGE) of 4,600 feet (1,402 meters). With a crew of four, the hover ceiling is reduced to 2,800 feet (853 meters). Its service ceiling is 15,000 feet (4,572 meters).

The SH-2A has a cruise speed of 125 knots (144 miles per hour/232 kilometers per hour) and a maximum speed of 140 knots (161 miles per hour/259 kilometers per hour) at Sea Level. Its combat radius is 125 nautical miles (144 miles/232 kilometers). The maximum range is 465 nautical miles (535 miles/861 kilometers).

Clementine 2 was armed with two M60 7.62 mm machine guns.

88 UH-2As were built 1959-1960, before production shifted to a twin-engine variant.

Seasprite 149764 was lost in the South China Sea, 7 January 1969.

President Lyndon Johnson congratulates Lieutenant Clyde Everett Lassen on the award of the Medal of Honor, 16 January 1969.

Clyde Everett Lassen was born at Fort Myers, Florida, 14 March 1942. He graduated from Venice High School, Englewood, Florida, in 1960.

Lassen enlisted in the United States Navy, 14 September 1961. He served as an Aviation Electronics Technician, 3rd Class (AT3). In 1964, he was accepted as a Naval Aviation Cadet at NAS Pensacola. On completion of flight training, Lassen was commissioned an ensign and awarded the wings of a Naval Aviator.

Ensign Lassen married Miss Linda Barbara Sawn in October 1965.

Lt. Clyde E. Lassen, USN, 1968

He was promoted to lieutenant (junior grade), 16 December 1966, and to lieutenant, 1 July 1968.

President Lyndon Johnson presented the Medal of Honor to Lieutenant Lassen at a ceremony at The White House, 16 January 1969.

Lieutenant Lassen was promoted to the rank of lieutenant commander 1 August 1972, and to commander, 1 July 1975. Commander Lassen retired from the U.S. Navy in December 1982.

Commander Lassen donated his Medal of Honor to the National Naval Aviation Museum 19 June 1993.

Commander Clyde Everett Lassen, United States Navy, died 1 April 1994 at Pensacola, Florida. He was buried at the Barrancas National Cemetery at Pensacola.

USS Lassen (DDG-82)
USS Lassen (DDG-82). (U.S. Navy)

Highly recommended: “Clementine Two: U.S. Navy night rescue over North Viet Nam,” by C. LeRoy Cook, at http://www.vhpa.org/stories/clem2.pdf

USS Lassen (DDG-82. (United States Navy)

© 2018, Bryan R. Swopes

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21–25 April 1944

First Lieutenant Carter Harman, United States Army Air Corps. (U.S. Army)
Second Lieutenant Carter Harman, United States Army Air Corps. (U.S. Army)

21 April 1944: The first military helicopter combat rescue began with Lieutenant Carter Harman, 1st Air Commando Group, being ordered to proceed from Lalaghat, India with his Vought-Sikorsky YR-4B, 43-28247, 600 miles (965 kilometers) to Taro in northern Burma.

Technical Sergeant Ed “Murphy” Hladovcak, pilot of a Stinson L-1A Vigilant liaison airplane, had crashed in the jungle behind Japanese lines while transporting three wounded British soldiers. Lieutenant Harman was assigned to attempt to rescue the four men. It would be a marathon operation.

The first Stinson O-49 liaison airplane, 40-192. The type was redesignated L-1A Vigilant in April 1942. (U.S. Air Force)
The first Stinson O-49 liaison airplane, 40-192. The type was redesignated L-1A Vigilant in April 1942. The L-1A was expensive to manufacture, but had excellent short field performance. (U.S. Air Force)

It took Harman and his Sikorsky 24 hours to arrive at Taro. After a brief rest and dip in the river to cool off, he continued for another 125 miles (202 kilometers) to an airstrip in the jungle called “Aberdeen” which was well behind the enemy lines. It was from here that Sgt. Hladovcak had been operating, flying out wounded soldiers. From Aberdeen, Harman was led to the location of the downed men by another liaison airplane. The survivors were surrounded by Japanese soldiers who had found the crashed airplane and were trying to locate the four men.

Lt. Carter Harman hovering in ground effect with Sikorsky YR-4B Hoverfly 43-28247 at Lalaghat, India, March 1944. This is the helicopter with which he made the first combat rescue, 21–25 April 1944. (U.S. Air Force)
Lt. Carter Harman hovering in ground effect with Sikorsky YR-4B 43-28247 at Lalaghat, India, March 1944. This is the helicopter with which he made the first combat rescue, 21–25 April 1944. (U.S. Air Force)

Because of the high heat, elevation and humidity, which increased the density altitude, the YR-4B’s air-cooled engine was unable to produce its full rated power. Also, the helicopter’s rotor blades were not as effective as they would have beeen at lower density altitudes.

Harman planned to lift one of the survivors out of the clearing in the jungle and fly a short distance to a sand bank where other L-1 or L-5 liaison airplanes could pick them up and fly them back to Aberdeen. He would repeat the operation until all four men had been rescued. However, it took the rest of the day to airlift just the first two wounded and very sick soldiers.

Distinguished Flying Cross

On the second flight, the helicopter’s engine was overheating and on landing it seized and could not be restarted. Sergeant Hladovcak and the remaining soldier were still in the jungle, Lieutenant Harman was stuck by the river bank and Japanese soldiers were everywhere.

On the morning of 25 April Lieutenant Harman was able to get the helicopter’s engine to start, and again, one at a time, he rescued the two remaining survivors. A liaison plane flew out the wounded soldier while Hladovcak rode along with Harman back to Aberdeen. He had never seen a helicopter before.

For his actions, Lieutenant Carter Harman was awarded the Distinguished Flying Cross.

Sikorsky YR-4B 43-28247 was condemned 31 December 1944.

Lieutenant Carter Harman (standing, left), 1st Air Commando Group, with Sikorsky YR-4B-8-SI 43-28223, Burma, 26 April 1944. (U.S. Air Force)
Lieutenant Carter Harman, 1st Air Commando Group, (standing, left) with Sikorsky YR-4B 43-28223, Burma, 26 April 1944. The other officer standing next to Harman is Lieutenant Frank Peterson. Harman’s crew chief, Sergeant Jim Phelan, is kneeling at right. (U.S. Air Force)

The Sikorsky YR-4B was a two-place, single-engine helicopter with a single main rotor and an anti-torque tail rotor. The fuselage was 35 feet, 8.375 inches (10.881 meters) long with a main rotor diameter of 38 feet, 0 inches (11.582 meters). The tail rotor was 8 feet, 2.25 inches (2.496 meters) in diameter. Its overall length, with rotors turning, was 48 feet, 3.375 inches (4.716 meters). The helicopter had an overall height of 12 feet, 5 inches (3.785 meters). The empty weight was 2,020 pounds (916 kilograms) and maximum takeoff weight of 2,540 pounds (1,152 kilograms). The helicopter’s fuel capacity was 30 gallons (113.6 liters)

The main rotor consisted of three tapered, fully-articulated blades built of chrome-molybdenum steel spars and spruce plywood ribs, with laminated spruce, balsa and mahogany forming the leading edge and a flexible cable forming the trailing edge. The blades were covered with two layers of doped fabric. The three-bladed semi-articulated tail rotor was built with a spruce spar and alternating laminations of maple and mahogany, covered with fabric. Both the main and tail rotors had a thin brass abrasion strip covering the leading edges. The main rotor turned counter-clockwise, as seen from above. (The advancing blade is on the helicopter’s right.) The tail rotor was mounted on the helicopter’s right side in a tractor configuration. It turned clockwise as seen from the helicopter’s left. (The advancing blade is below the axis of rotation.)

Lieutenant Carter Harmon in the cockpit of Sikorsky YR-4B 43-28223, Burma, 1945.

The YR-4B was powered by an air-cooled, direct-drive 555.298-cubic-inch-displacement (9.100 liter) Warner Super Scarab SS185 (R-550-3) seven-cylinder radial engine with a compression ratio of 6.20:1. The R-550-3 was rated at 185 horsepower at 2,175 r.p.m. at Sea Level, and 200 horsepower at 2,475 r.p.m (five minute limit) for takeoff. The engine was placed backwards in the aircraft with the propeller shaft driving a short driveshaft through a clutch to a 90° gear box and the transmission. The R-550-3 weighed 344 pounds (156 kilograms).

The R-4B had a cruise speed of 65 miles per hour (105 kilometers per hour) and maximum speed of 82 miles per hour (132 kilometers per hour). The service ceiling was 12,000 feet (3,658 meters) and range was 157 miles (253 kilometers).

The YR-4B was equipped with bomb racks. It could carry three 125 pound (56.7 kilogram) demolition bombs or one 325 pound (147 kilogram) depth bomb. The equipment was deleted for the R-4B.

Sikorsky built 27 YR-4Bs and 100 R-4B helicopters. Of these, 40 were assigned to the Army Air Corps, 19 to the Navy and Coast Guard, and 41 were sent to the Royal Air Force and Royal Navy.

Sikorsky YR-4B 43-28225 in the NACA full scale wind tunnel, Langley Field, Virginia, 1944. A technician is preparing strobes to take stop-motion photographs of the helicopter's rotor blades while they turn at normal operating r.p.m. (NASA)
Sikorsky YR-4B 43-28225 in the NACA full scale wind tunnel, Langley Field, Virginia, 1944. A technician is preparing strobes to take stop-motion photographs of the helicopter’s rotor blades while they turn at normal operating r.p.m. (NASA)

Carter Harman was born at Brooklyn, New York, 14 June 1918, the son of Steven Palmer Harman, a newspaper editor, and Helen F. Doremus Harman.

Before the war, Harman had been a musician and author. He assisted Duke Ellington write an autobiography. Harman earned a bachelor’s degree in music composition from Princeton University, Princeton, New Jersey, in 1940. While at Princeton, Harman was a member of the Dial Lodge, American Whig Society, Princeton University Band, and the Princeton University Choir.

Harman enlisted as a private in the United States Army at Hew York City on 1 April 1942, and was assigned to the Air Corps. Enlistment records indicate that he was 5 feet, 7 inches (170.2 centimeters) tall and weighed 125 pounds (57 kilograms).

After World War II ended, Harman returned to his musical studies at Columbia University, New York City, receiving a master’s degree in 1949.

Harman worked as a music critic for The New York Times and Time Magazine, and also continued writing books, as well as composing for ballet and opera. He was also a music producer and became executive vice president of CRI Records (Composers Recordings, Inc.).

Harman was married three times. He married Miss Nancy Hallinan, 5 February 1946, however they later divorced. His second wife was Helen Scott. They had four children together. His third wife was Wanda Maximilien.

Carter Harman died at Berlin, Vermont, 23 January 2007 at the age of 88 years.

© 2018, Bryan R. Swopes

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