24 November 1971

This photograph shows Northwest Orient Airlines' Boeing 727, N467US, on teh ramp at Seattle-Tacoma International Airport on the evening of 24 November 1971. (Unattributed; probable news agency photo)
This photograph shows Northwest Orient Airlines’ Boeing 727, N467US, on the ramp at Seattle-Tacoma International Airport on the evening of 24 November 1971. (Unattributed; probable news agency photograph, via Check-Six.com)

24 November 1971: Early Wednesday afternoon, a man who gave the name “Dan Cooper” purchased a one-way ticket for Northwest Orient Airlines Flight 305, a non-stop flight from Portland, Oregon, to Seattle, Washington. Flight 305 departed on schedule at 2:50 p.m., PST, with a crew of 6 and 37 passengers, including Cooper. Captain William A. Scott was in command with First Officer William Rataczack as co-pilot and Second Officer Harold E. Anderson, flight engineer.

The airliner was a six-year-old Boeing 727-51, c/n 18803, registered N467US. On this flight, it was approximately one-third full. The trip from PDX to SEA was estimated to take 30 minutes.

Shortly after takeoff, Cooper gave a handwritten note to Florence Schaffner, a flight attendant who was seated nearby. The note read that the airliner was being hijacked and that Cooper had a bomb in his briefcase. Schaffner asked Cooper to show her the bomb. He opened the brief case and she later described having seen eight red cylinders with red-insulated wires attached, and a cylindrical battery. Cooper closed his briefcase and gave Schaffner his demands: $200,000 in United States currency, four parachutes and a fuel truck to be standing by on their arrival at Seattle. She then relayed Cooper’s demands to the flight crew.

The Federal Bureau of Investigation released these artists sketches of the suspect in the hijacking of Flight 305. (FBI)
The Federal Bureau of Investigation released these artist’s sketches of the suspect in the hijacking of Flight 305. (Federal Bureau of Investigation)

Once over Seattle, Flight 305 circled for approximately two hours while officials on the ground arranged to comply with Cooper’s demands. The 727 landed at SEA at 5:39 p.m. Ransom money had been gathered by the FBI from several Seattle area banks and consisted of 10,000  $20 bills. The notes were not marked but all were photographed to record their serial numbers.

The money was carried to the airliner by a Northwest employee, along with the requested parachutes. These were given to flight attendant Tina Mucklow at the 727’s aft boarding stairs. She carried these to Cooper, who satisfied that his demands had been met, allowed the 36 other passengers, as well as flight attendants Schaffner and Alice Hancock, to leave the airplane.

Refueling was delayed because of trouble with the fuel truck, and eventually three trucks were used.

Cooper informed the flight crew that he wanted them to fly the 727 south to Mexico, and gave very specific instructions. He told them to fly as slow as possible, to leave the landing gear extended, flaps lowered to 15°, and to remain below 10,000 feet (3,048 meters) with the cabin unpressurized. He also demanded that the airliner takeoff with its ventral stairs lowered but this was refused as being unsafe.

At 7:40 p.m., N467US took off from SeaTac with the flight crew and cabin attendant Mucklow still on board. Cooper required that Mucklow remain with him in the passenger cabin. It was followed by two Convair F-106 Delta Dart interceptors from McChord Air Force Base.

An intermediate fuel stop had been planned for Reno, Nevada, and the airliner headed in that direction, flying along a standard airway, Victor 23.

Cooper told Mucklow to go forward and join the rest of the crew in the cockpit. At 8:00 p.m., a warning light in the cockpit came on indicating that the ventral stairs had been activated. At 8:13 p.m., the aircraft pitched nose down, and required that the flight controls be re-trimmed for a level attitude. At 10:15 p.m., the airliner landed at Reno. After a search, it was determined that Cooper, the money and two parachutes were no longer aboard.

Flight 305 crew at Reno, Nevada. Captain William A. Scott, First Officer William Rataczack, Flight Attendant Tina Mucklow, and Second Officer Harold E. Anderson.

In 1978, a hunter discovered a placard from a 727’s aft stairs near the known path of the hijacked 727. In 1980, a young boy found three deteriorated packets containing $5,800 in $20 bills along the banks of the Columbia River, downstream from Vancouver, Washington. The serial numbers matched currency included in the ransom.

Dan Cooper has never been located. There have been a number of persons considered as suspects, however it is possible that Cooper did not survive the jump from Flight 305.

Northwest Boeing 727-51 N467US at Reno, Nevada. (Federal Bureau of Investigation)

N467US remained in service with Northwest Orient Airlines until June 1978, when it was sold to Piedmont Airlines, re-registered N838N, and christened Mt. Mitchell Pacemaker. From 1982 through 1984, it was operated by United Technologies Flight Dynamics, testing navigational equipment. In September 1984 the 727 was again sold, this time to Key Airlines, with a third registration N29KA. During this period, c/n 18803 was operated on daily charter flights from Nellis Air Force Base to the Tonapah Test Range, a restricted Department of Energy installation located about 125 nautical miles (144 statute miles/232 kilometers) northwest of Las Vegas, Nevada. Later, the 727 was placed in storage at Greenwood-Leflore Airport (GWO) near Greenwood, Mississippi. It was scrapped in 1996.

Boeing 727-51 c/n 18803, now in Piedmont Airlines livery and registered N838N, at Chicago O’Hare, 1979. (RuthAS)

C/n 18803, a Boeing 727-51, is now considered to be a 727-100, a medium-range civil transport. It was operated by a flight crew of three and could carry up to 131 passengers. The airliner was 133 feet, 2 inches (40.589 meters) long with a wingspan of 108 feet, 0 inches (32.918 meters), and overall height of 34 feet, 0 inches (10.363 meters). Empty weight was 87,696 pounds (39,778 kilograms) and maximum ramp weight was 170,000 pounds (77,111 kilograms). Usable fuel capacity was 8,090 gallons (30,624 liters).

Power was supplied by three Pratt & Whitney JT8D-7 turbofan engines. The JT8D-7 was a two-spool engine with a 2-stage fan section, 13-stage compressor (6 low- and 7 high-pressure stages), nine combustion chambers, and a 4-stage turbine (1 high- and 3 low-pressure stages). The JT8D-7 had a maximum continuous power rating of 12,600 pounds of thrust (56.048 kilonewtons) at Sea Level, and 14,000 pounds (62.275 kilonewtons) for takeoff. It was 3 feet, 6.5 inches (1.080 meters) in diameter, 10 feet, 3.5 inches (3.137 meters) long, and weighed 3,096 pounds (1,404 kilograms). Two of the engines were in nacelles at either side of the aft fuselage, and the third was mounted in the tail. Its intake was above the rear fuselage at the base of the vertical fin.

The Boeing 727s were very fast airliners with a maximum speed in level flight of 549 knots (632 miles per hour/1,017 kilometers per hour). The Design Cruise Speed (VC) was 530 knots (610 miles per hour/981 kilometers per hour) at 25,000 feet (0.88 Mach). The airplane was certified with a Maximum Mach Number (MMO) of 0.92 Mach (this was later reduced to 0.90 Mach). (During flight testing, a Boeing 727 achieved 0.965 Mach in level flight.) The airliner’s service ceiling was 37,400 feet (11,400 meters) and the range was 2,600 nautical miles (2,992 statute miles/4,815 kilometers).

Boeing built 572 of the 727-100 series and 1,260 of the longer 727-200 variant from 1963 to 1984.

Boeing 727-51 c/n 18803, carrying registration N29KA, awaits scrapping at Greenwood-Leflore Airport, Greenwood, Mississippi. (Jim Newton Photography)
Boeing 727-51 c/n 18803, carrying registration N29KA, awaits scrapping at Greenwood-Leflore Airport, Greenwood, Mississippi. (Jim Newton Photography)

© 2018, Bryan R. Swopes

24 November 1969

Apollo 12 command modules just before splashdown 10:58 a.m., local time, 24 November 1969. (U.S. Navy)
Apollo 12 command module just before splashdown 10:58 a.m., local time, 24 November 1969. (U.S. Navy)

24 November 1969: The Apollo 12 command module Yankee Clipper, carrying astronauts Charles “Pete” Conrad, Jr., Mission Commander; Richard F. Gordon, Jr., Command Module Pilot; Alan L. Bean, Lunar Module Pilot; landed in the Pacific Ocean at 20:58:24 UTC, approximately 500 miles east of American Samoa. Mission Time: 244:36:23.

Apollo 12 command module Yankee Clipper splashed down within approximately 2.5 nautical miles of the primary recovery ship. It is in the foreground of this photograph, with a Sikorsky SH-3D Sea King and USS Hornet (CVS-12), approximately 11:00 a.m., local time, 24 November 1969. (U.S. Navy)
Apollo 12 command module Yankee Clipper splashed down within approximately 2.5 nautical miles of the primary recovery ship. It is in the foreground of this photograph, with a Sikorsky SH-3D Sea King and USS Hornet (CVS-12), approximately 11:00 a.m., local time, 24 November 1969. (U.S. Navy)

© 2015, Bryan R. Swopes

24 November 1959

Trans World Airlines’ Lockheed L-1049H Super Constellation N102R at Frankfurt, Germany, 1959. (Erich Marek)

24 November 1959: At 5:35 a.m., Central Standard Time, Trans World Airlines Flight 595, a Lockheed L-1049H Super Constellation freighter, N102R, crashed into a residential area about ¼-mile (0.4 kilometer) to the southeast of Midway Airport (MDW), Chicago, Illinois.

“How disabled plane, whose pilot tried to return to airport, crashed into homes on southwest side in holocaust of destruction.” —Chicago Tribune, Vol. CXVIII, No. 282, Wednesday, 25 November 1959, Page 3, columns 5–8)
(L–R) Auge, Helwig, Watters.

N102R had departed Midway Airport at approximately 5:31 a.m., Central Standard Time (11:31 UTC), en route to Los Angeles, California. The flight crew were Captain Claude Wilbert Helwig, First Officer Delmas Earl Watters, and Flight Engineer Aerion Lyman Auge, Jr.

A weather observation made ten minutes before takeoff reported the sky partially obscured, scattered clouds at 600 feet (183 meters), measured 900 foot (274 meters) overcast; visibility 3 miles (4.8 kilometers), with light rain, fog and smoke. The wind was 10 knots (5.14 meters per second) temperature 39 °F. (3.8 °C.) and dew point 38 °F. (3.3 °C.).

1 minute, 20 seconds after takeoff, the flight crew reported to the control tower that that they had a fire warning for the airplane’s number 2 engine (inboard, left wing) and that they would return to the airport. The tower cleared Flight 595 to land on Runway 31L. [Today, this runway is 31C.] The controller asked if they wanted to use a localizer approach, and received the answer, “I think we’ll make it VFR, OK,” meaning that the crew intended to remain in visual conditions below the overcast.

Ground track of TWA Flight 595, 24 November 1959. (Civil Aeronautics Board)

According to the accident investigation report,

      In the turn to final approach to runway 31 the aircraft banked in excess of 45 degrees during which it developed an excessive rate of sink. When the aircraft reached the tops of the trees its wings were nearly level and its nose was raised in a climbing attitude; however, the descent continued. The wing flaps were being retracted during the last 5 to 10 seconds of the final descent and were found to be symmetrically extended at 24 percent upon impact.

A controller saw the airplane crash into the residential area. The time was established by the time of the power failure caused when the Super Constellation hit the Commonwealth Edison Company power lines.

The three members of the flight crew and 11 people of the ground were killed. Another 11 people were injured.

Investigators found that the number 2 engine had been shut down and its propeller feathered, but there was no evidence of any inflight fire.

The investigative board found the the flight crew’s decision to remain below the clouds was reasonable under the circumstances.

     In anticipation of landing, a gear-down, flap-extended configuration was established on the downwind portion of the traffic pattern. The wing flaps were at least in the takeoff position of 60 percent and had been allowed, presumably to remain so extended since takeoff, because less than one minute had elapsed from the start of the takeoff roll until the fire warning, and at that time the captain planned to return to land. The track over the ground on the “downwind” curved toward the runway. When the aircraft was positioned to start the turn to final approach a sharp turn was needed to avoid overshooting the extended centerline of runway 31L.

     The Board believes the captain attempted such a turn, and in doing so combined a very steep bank with high gross weight ¹ and three-engine aircraft configuration in such a manner that the aircraft entered a regime of flight describable as being on the backside of the power curve. More power and altitude than was available to him was needed to safely recover the aircraft At some point in this turn the captain very probably decided to discontinue the landing approach and attempted to “go-around.” Hence, he called for gear up at or near this same point, but for an unexplained reason the wing flap controls were positioned for flap retraction.

The nose landing gear and left main gear assemblies were found to be in the up position but unlocked, and the right main gear was up and locked. The wing flaps were extended symmetrically at about 24 percent of their full travel. The flap control valve and follow-up mechanism were positioned to raise the flaps. The cockpit flap control lever was found to be about 1/8-inch (3.2 millimeters) aft of the full up position, with the lever bent over 80 degrees to the left. There was no indication that the lever had been forcibly moved fore or aft.

Wreckage of Lockheed L-1049H Super Constellation N102R in a hangar at Chicago Midway Airport 25 November 1959. (Civil Aeronautics Board)

The Civil Aeronautics Board determined that the Probable Cause of the accident was

     . . . the maneuvering of the aircraft in a manner that caused it to develop an excessive rate of sink in the turn to final approach.

Lockheed L-1049 Super Constellation three-view illustration with dimensions. (Lockheed Aircraft Corporation)

The L-1049 series was 18 feet, 4 inches (5.588 meters) longer than the preceding L-749 Constellation, with cylindrical “plugs” installed fore and aft of the wing. The L-1049H was the final commercial variant of the Super Constellation series. It could be converted from a passenger airliner to an air freighter configuration in a few hours. The L-1049 was 113 feet, 3.7 inches (34.536 meters) long, with a wingspan of 123 feet, 0 inches (37.490 meters), and overall height of 24 feet, 9.5 inches (7.557 meters). The fuselage had a maximum diameter of 11 feet, 7½ inches ( meters).

The total wing area was 1,650 square feet (153.3 square meters). The wings’ leading edges were swept aft 7° 28.7′, while the trailing edges swept forward 3° 13′. They had 7° 36.6′ dihedral.

Factory cutaway Wright Aeronautical Division 988TC18 turbocompound engine. (Aircraft Engine Historical Society)

N102R was powered by four air-cooled, direct-fuel-injected, 3,347.662 cubic-inch-displacement (54.858 liters) Wright Aeronautical Division 988TC18EA3 Duplex Cyclone turbocompound engines with a compression ratio of 6.70:1. The turbocompound engine used captured exhaust gases to drive three Power Recovery Turbines. These PRTs were coupled to the engine’s crankshaft. This system added approximately 450 horsepower to the engine’s total power output.

The 988RC18EA3 had Normal Power ratings of 2,860 horsepower at 2,650 r.p.m. at Sea Level; 2,920 horsepower at 2,650 r.p.m. at 4,800 feet (1,463 meters); 2,450 horsepower at 2,600 r.p.m. at 16,400 feet (4,999 meters). Its Maximum Power ratings were 3,400 horsepower at 2,900 r.p.m. to 4,000 feet (1,219 meters) for Take Off; and 2,600 horsepower at 2,600 r.p.m. at

The engines turned three-bladed Hamilton Standard propellers through a 0.4375:1 propeller gear reduction. The reduction gears were strengthened to support 4,000 horsepower. The Wright 988TC18EA3 was 7 feet, 5.53 inches (2.274 meters) long, 4 feet, 8.59 inches (1.473 meters) in diameter, and weighed 3,640 pounds, ± 1% (1,651 kilograms).15,200 feet (4,633 meters). 115/145-octane aviation gasoline was required.

The L-1049 had a maximum speed for normal operations (VNO) of 260 knots (299 miles per hour/482 kilometers per hour) and a maximum speed (VNE) of 293 knots (337 miles per hour/543 kilometers per hour) up to 11,000 feet (3,353 meters). VNO was reduced by 9 knots, and VNE reduced by 11 knots, for each 2,000 foot (610 meters) increase in altitude above 11,000 feet.

The maximum operating altitude for the L-1049 was 25,000 feet (7,620 meters). Its maximum range was 4,140 miles (6,663 kilometers).

N102R had a manufacture date of 6 June 1957. When it went through a scheduled overhaul 8 March 1959, it had accumulated 3,432:08 hours of flight time.

Claude Wilbert Helwig was born 9 July 1919 in San Francisco, California. He was the son of Henry Wilbert Helwig, a truck driver, and Mina Helwig Borchard. He attended Balboa High School in San Francisco, graduating in 1937.

Helwig enlisted in the United States Army Air Forces 12 March 1941. He had brown hair, gray eyes, a light complexion, was 5 feet, 8 inches (178 centimeters) tall and weighed 133 pounds (60 kilograms). Helwig was honorably discharged 9 March 1943 and was commissioned as a second lieutenant, Air Corps, Army of the United States (AUS), 10 March 1943. he was assigned to in the 14th Troop Carrier Squadron, 61st Troop Carrier Group.

Lieutenant Helwig married Miss Josephine Crull at Crow Creek Township, North Carolina, 20 May 1943. The ceremony was performed by J.W. Johnson, Justice of the Peace.

Following World War II, Helwig remained in the U.S. Air Force Reserve, serving with the rank of captain. He was discharged 1 April 1953. Captain Helwig had been awarded the Air Medal with 13 oak leaf clusters (14 awards). Captain Helwig’s remains were interred at Glen Oaks Memorial Park, Chico, California.

Delmas Earl Watters was born at Estill Springs, Tennessee, 30 November 1922. He was the son of Earl Watters, a locomotive fireman,  and Annabelle Smith Watters.

He attended Tennessee Technological University, Cookeville, Tennessee.

Watters enlisted as an aviation cadet in the United States Navy, 9 December 1942, at Atlanta, Georgia. He entered pre-flight school at Athens, Georgia, 1 May 1942, then underwent flight training at Corpus Christi, Texas. His enlistment was terminated to accept a commission as an ensign, United States Navy Reserve, 26 December 1944.

Ensign Watters married Miss Theda Jeanne McMillan in King County, Washington, 30 December 1945. The ceremony was performed by J. Robert Walter of the Central Presbyterian Church, Seattle, Washington. They later divorced.

Ensign Watters was promoted to the rank of lieutenant (junior grade), 1 January 1947.

Watters later transferred to the United States Air Force with the rank of first lieutenant. During the Korean War, he was awarded the Distinguished Flying Cross with one oak leaf cluster (two awards).

Watters married Miss Jean Ruth Cleere at the Chapel of Roses, Pasadena, California, California, 30 December 1951. They would have one son.

First Officer Watters’ remains were interred at the Mountain View Cemetery and Mausoleum, Altadena, California.

Aerion Lyman Auge, jr., was born 8 June 1924 in Jefferson, Kentucky. He was the son of Aerian Lyman Auge, an electrician, and Isabelle Veronica Jahn Auge.

Auge served in the United States Navy during World War II.

Auge married Yvonne Easton in Pierce County, Washington, 19 April 1946. They would have three daughters. Flight Engineer Auge’s remains were interred at the Inglewood Park Cemetery, Inglewood, California.

Thanks to TDiA reader George Firis for suggesting this subject. Mr. Firis’s aunt lived in an apartment building that was destroyed.

¹ The computed allowable gross takeoff weight for this flight was 127,400 pounds (57,788 kilograms). At departure, the aircraft weighed 126,606 pounds (57,428 kilograms). The allowable landing weight was 115,000 pounds (52,163 kilograms).

© 2024, Bryan R. Swopes

23 November 2002, 00:49:47 UTC, T minus Zero

Space Shuttle Endeavour (STS-113) lifts off from LC-39A, 7:49:47 p.m., Eastern Standard Time, 23 November 2002. (NASA)

23 November 2002, 00:49:47 UTC, T minus Zero: Space Shuttle Endeavour (OV-105) lifted off from Launch Complex 39A, Kennedy Space Center, Cape Canaveral, Florida, on mission STS-113.

The mission commander, Captain James D. Wetherbee, United States Navy, was on his sixth space flight and shuttle pilot Lieutenant Colonel Paul S. Lockhart, United States Air Force, was on his second. Mission Specialist Captain Miguel López-Alegría, USN,  was on his third space flight while Commander John B. Harrington, USN, was on his first.

Flight crew of Space Shuttle Endeavour, STS-113), left to right, LCOL Paul S. Lockhart, USAF; CAPT Michael E. Lopez-Alegria, USN; CDR John B. Herrington, USN; CAPT James D. Wetherbee, USN. (NASA)
Flight crew of Space Shuttle Endeavour (STS-113), left to right, LCOL Paul S. Lockhart, USAF; CAPT Michael E. López-Alegría, USN; CDR John B. Herrington, USN; CAPT James D. Wetherbee, USN. (NASA)

STS-113 delivered the P1 truss (the Port Side Thermal Radiator Truss), a major structural component of the International Space Station, into orbit, while also carrying the three members of Expedition 6, who were to spend the next four months on board the space station: Captain Kenneth D. Bowersox, USN, was on his fifth space flight; Test Cosmonaut Nikolai Mikhailovich Budarin (Николай Михайлович Бударин), Russian Federal Space Agency (RKA), on his third flight; and Donald R. Pettit, Ph.D., NASA, was on his first. ISS Expedition 5 members Colonel Valery Grigoryevich Korzun (Валерий Григорьевич Корзун), Soviet Air Force, Peggy Annette Whitson, Ph.D., NASA, and Sergei Yevgenyevich Treshchov (Сергей Евгеньевич Трещёв), RSC Energia, having completed their assignments to the ISS, were returned to Earth aboard Endeavour.

Endeavour landed at the Shuttle Landing Facility (LSF), Kennedy Space Center, at 19:38:25 UTC, 7 December 2002. The duration of mission STS-113 was  13 days, 18 hours, 48 minutes, 38 seconds.  Endeavour remained docked with the ISS for 6 days, 22 hours, 51 minutes, 00 seconds. While in orbit, NASA astronauts López-Alegría and Herrington performed three EVAs (Extravehicular Activity, of “space walks”).

Space Shuttle Endeavour (OV-105) in Earth orbit, photographed from the International Space Station. The P1 Truss is in the open cargo bay. (NASA)
Space Shuttle Endeavour (OV-105) in Earth orbit, photographed from the International Space Station, 25 November 2002. The P1 Truss is in the open cargo bay. (NASA)

© 2018, Bryan R. Swopes

23 November 1959

Boeing 720-022 c/n 17907, N7201U. (Boeing)
Boeing 720-022 c/n 17907, N7201U, parked on the taxiway at the south shore of Lake Washington. (Boeing)

23 November 1959: The first Boeing 720 airliner, a 720-022, registered as N7201U, made its first flight at Renton, Washington. The 720 was a development of the 707 and no prototype was built. N7201U was used by Boeing for flight testing and was then delivered to United Airlines, 1 October 1960. The airline named the new 720 Jet Mainliner Capt. F. M. Crismore. Over the next two years, United acquired 29 Boeing 720s.

N7201U was sold to Contemporary Entertainment, owned by singer Bobby Sherman and his manager, Ward Sylvester, in January 1973. It was repainted in a gold and black livery and christened The Starship. As a VIP transport, it was used by such rock bands as Led Zeppelin, Deep Purple, The Rolling Stones, Alice Cooper and Elton John. It was last chartered by Peter Frampton.

N7201U was withdrawn from service in 1977 and after being stored for several years, was broken up at Luton Airport near London, England, in 1982.

The Boeing 720 was a variant of the Model 707, intended for short to medium range flights. It had 100 inches (2.54 meters) removed from the fuselage length and improvements to the wing, decreasing aerodynamic drag.

Boeing built 154 720 and 720B airliners from 1959 to 1967.

The Boeing 720 was operated by a flight crew of four and could carry up to 149 passengers. It was 136 feet, 2 inches (41.25 meters) long with a wingspan of 130 feet, 10 inches (39.90 meters) and overall height of 41 feet, 7 inches (12.65 meters). The airplane had an empty weight of 103,145 pounds (46,785 kilograms) and Maximum Takeoff Weight of 220,000 pounds (100,800 kilograms).

The Boeing 720 was powered by four Pratt & Whitney Turbo Wasp JT3C-7 turbojet engines, a civil variant of the military J57 series. The 720B was equipped with the more efficient P&W JT3D-1 turbofan engines. The JT3C-7 was a “two-spool” axial-flow engine with a 16-stage compressor (9 low- and 7 high-pressure stages), 8 combustion tubes, and a 3-stage turbine (1 high- and 2 low-pressure stages). It was rated at 12,030 pounds of thrust (53.512 kilonewtons) for takeoff.

The JT3D-1 was a dual axial-flow turbofan engine, with a 2-stage fan section 13-stage compressor (6 low- and 7 high pressure stages), 8 combustion chambers and a 4-stage turbine (1 high- and 3 low-pressure stages). This engine was rated at 14,500 pounds of static thrust (64.499 kilonewtons) at Sea Level, and 17,000 pounds (75.620 kilonewtons), with water injection, for takeoff (2½ minute limit). Almost half of the engine’s thrust was produced by the fans. Maximum engine speed was 6,800 r.p.m. (N1) and 10,200 r.p.m. (N2). It was 11 feet, 4.64 inches (3.471 meters) long, 4 feet, 5.00 inches (1.346 meters) wide and 4 feet, 10.00 inches (1.422 meters) high. It weighed 4,165 pounds (1,889 kilograms). The JT3C could be converted to the JT3D configuration during overhaul.

The maximum cruise speed was 611 miles per hour (983 kilometers per hour) and maximum speed was 620 miles per hour (1,009 kilometers per hour). Range at at maximum payload was 4,370 miles (7,033 kilometers).

The last flight of a Boeing 720 was on 9 May 2012, when a 720B aircraft used by Pratt and Whitney Canada as a test aircraft was placed in the National Air Force Museum of Canada at Trenton, Ontario.

United Airlines' Boeing 720-022, N7201U. (Unattributed)
United Airlines’ Boeing 720-022, N7201U. The airliner’s name, “Jet Mainliner Capt. F. M. Crismore,” is visible under the cockpit windows. (Bill Larkins via Wikipedia)

© 2018, Bryan R. Swopes