Tag Archives: Boeing

10 November 2005

Aviation, , , , , , , , , , , ,
Boeing lead test pilot for the 777, Captain Suzanna Darcy-Henneman, in the left seat of a Boeing 777-200LR. (Smithsonian Institution National Air and Space Museum L60826)

10 November 2005: Captain Suzanna Darcy-Henneman set a Fédération Aéronautique Internationale (FAI) world record for distance flown by a commercial aircraft when she and a crew of 7 additional pilots flew a Boeing 777-200LR Worldliner, N6066Z, non-stop from Hong Kong (HKG) to London Heathrow (LHR), a distance of 21,601.33 kilometers (13422.44 miles), in 22 hours, 22 minutes.¹ During the flight, Captain Darcy-Henneman also set two speed records. The 777 averaged 981.57 kilometers per hour (609.92 miles per hour) from Los Angeles to New York,² and 910.54 kilometers per hour (565.78 miles per hour) from New York to London.³

The record-setting Boeing 777-200LR touches down at Heathrow. (Boeing)

Suzanna Darcy joined Boeing’s engineering department in 1974. She learned to fly with the Boeing Employees Flying Association. Darcy graduated from the University of Washington in 1981 with a Bachelor of Science degree in Aeronautics and Aeronautical Engineering. She then became a ground school instructor for Boeing’s Model 757 and 767 airliners.

In 1985, Boeing assigned Darcy-Hanneman as a production test pilot, the first woman to hold that position with the company. She was also the first woman to earn a captain’s rating on the 747-400, and is also rated on the 737, 757, 767 and 777.  She performed flight testing on the 737-300 and was the project test pilot for the 777-200LR.

“Capt. Suzanna Darcy-Hennemann, the first female test pilot of Boeing, peers from the cockpit of a 777-200LR at Everett’s Boeing Plant in 2005.” (Mike Siegel / The Seattle Times)

In 2008, Captain Darcy-Hanneman became Chief Pilot, Boeing Commercial Airplane Services. She is a member of the Society of Experimental Test Pilots, and was inducted into the Women in Aviation Pioneer Hall of Fame in 2010. She retired from Boeing in 2015.

Boeing 777-200LR N6066Z. (Unattributed)
Boeing 777-200LR N6066Z. (Unattributed)

The Boeing 777-200LR was designed for very long distance airline routes. It is operated by two pilots, and can carry a maximum 317 passengers. The airplane is 209 feet, 1 inch (63.729 meters) long with a wingspan of 212 feet, 7 inches (64.795 meters) and overall height of 61 feet, 1 inch (18.618 meters). It has an empty weight of 320,000 pounds (145,150 kilograms), and maximum takeoff weight of 766,000 pounds (347,452 kilograms).

The 777-200LR is powered by two General Electric GE-90-110B1 or -115B engines. The engine is dual rotor axial-flow high bypass turbofan. It has a single fan stage; 4-stage high pressure- and 9-stage low pressure compressor section; with a 2-stage high- and 6-stage low-pressure turbine. The high pressure rotor turns 9,332 r.p.m., and the low-pressure rotor turns 2,355 r.p.m. The engine is 286.67 inches (7.281 meters) long and weighs 19,316 pounds (8,761.590 kilograms). The fan has a diameter of 128 inches (3.251 meters). The GE90-115 produces a maximum 115,300 pounds of thrust (156.326 kilonewtons).

The 777-200LR has a maximum speed (MMO) of 0.89 Mach. Its maximum operating altitude is 43,100 feet (13,137 meters).

As of September 2020, Boeing had delivered sixty 777-200LRs.

¹ FAI Record File Number 12181

² FAI Record File Number 12182

³ FAI Record File Number 12183

© 2020, Bryan R. Swopes

9 November 1967, 12:00:01.263 UTC, T plus 0.263

Space Flight, , , , , , , , , , , , , , , , , , , , , ,
Apollo 4 Saturn V (AS-501) on the launch pad at sunset, the evening before launch, 8 November 1967. (NASA)
Apollo 4 Saturn V (AS-501) on the launch pad at sunset, the evening before launch, 8 November 1967. (NASA)

9 November 1967: The first flight of a Saturn V took place when the unmanned Apollo 4/Saturn V (AS-501) was launched from Pad 39A at the Kennedy Space Center, Cape Canaveral, Florida. The rocket lifted off at 12:00:01.263 UTC.

AS-501 consisted of the first Saturn V launch vehicle, SA-501, with Apollo Spacecraft 017 (a Block I vehicle with Block II upgrades), and included the Launch Escape Tower, Command Module, Service Module, Lunar Module Adapter, and Lunar Module Test Article LTA-10R).

The Saturn V rocket was a three-stage, liquid-fueled heavy launch vehicle. Fully assembled with the Apollo Command and Service Module, it stood 363 feet, 0.15 inches (110.64621 meters) tall, from the tip of the escape tower to the bottom of the F-1 engines. The first and second stages were 33 feet, 1.2 inches (10.089 meters) in diameter. Fully loaded and fueled the rocket weighed 6,200,000 pounds (2,948,350 kilograms).¹ It could lift a payload of 260,000 pounds (117,934 kilograms) to Low Earth Orbit.

The first stage was designated S-IC. It was designed to lift the entire rocket to an altitude of 220,000 feet (67,056 meters) and accelerate to a speed of more than 5,100 miles per hour (8,280 kilometers per hour). The S-IC stage was built by Boeing at the Michoud Assembly Facility, New Orleans, Louisiana. It was 138 feet (42.062 meters) tall and had an empty weight of 290,000 pounds (131,542 kilograms). Fully fueled with 203,400 gallons (770,000 liters) of RP-1 and 318,065 gallons (1,204,000 liters) of liquid oxygen, the stage weighed 5,100,000 pounds (2,131,322 kilograms). It was propelled by five Rocketdyne F-1 engines, producing 1,522,000 pounds of thrust, each, for a total of 7,610,000 pounds of thrust at Sea Level.² These engines were ignited seven seconds prior to lift off and the outer four burned for 168 seconds. The center engine was shut down after 142 seconds to reduce the rate of acceleration. The F-1 engines were built by the Rocketdyne Division of North American Aviation at Canoga Park, California.

A Rocketdyne F-1 engine is being installed on a Saturn S-IC first stage. (NASA)

The S-II second stage was built by North American Aviation at Seal Beach, California. It was 81 feet, 7 inches (24.87 meters) tall and had the same diameter as the first stage. The second stage weighed 80,000 pounds (36,000 kilograms) empty and 1,060,000 pounds loaded. The propellant for the S-II was liquid hydrogen and liquid oxygen. The stage was powered by five Rocketdyne J-2 engines, also built at Canoga Park. Each engine produced 232,250 pounds of thrust, and combined, 1,161,250 pounds of thrust.³

The Saturn V third stage was designated S-IVB. It was built by Douglas Aircraft Company at Huntington Beach, California. The S-IVB was 58 feet, 7 inches (17.86 meters) tall with a diameter of 21 feet, 8 inches (6.604 meters). It had a dry weight of 23,000 pounds (10,000 kilograms) and fully fueled weighed 262,000 pounds. The third stage had one J-2 engine and also used liquid hydrogen and liquid oxygen for propellant.⁴ The S-IVB would place the Command and Service Module into Low Earth Orbit, then, when all was ready, the J-2 would be restarted for the Trans Lunar Injection.

Eighteen Saturn V rockets were built. They were the most powerful machines ever built by man.

Apollo 4 Saturn V AS-501 lifts off at 12:00:01 UTC, 9 November 1967. (NASA)
Apollo 4 Saturn V (AS-501) lifts off at 12:00:01 UTC, 9 November 1967. (NASA)

¹ The AS-501 total vehicle mass at First Motion was 6,137,868 pounds (2,784,090 kilograms).

²  Post-flight analysis gave the total thrust of AS-501’s S-IC stage as 7,728,734.5 pounds of thrust (34,379.1 kilonewtons).

³ Post-flight analysis gave the total thrust of AS-501’s S-II stage as 1,086,396 pounds of thrust (4,832.5 kilonewtons).

⁴ Post-flight analysis gave the total thrust of AS-501’s S-IVB stage as 222,384 pounds of thrust (989.2 kilonewtons) during the first burn; 224,001 pounds (996.4 kilonewtons) during the second burn.

© 2017, Bryan R. Swopes

31 August 1956

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Dix Loesch climbs aboard City of Renton while Tex Johnston waits. (Boeing)

31 August 1956: The first production Boeing KC-135A Stratotanker, 55-3118, named City of Renton, made its first flight with company test pilots Alvin Melvin (“Tex”) Johnston and Richards Llewellyn (“Dix”) Loesch, Jr., on the flight deck.

City of Renton, the first Boeing KC-135A Stratotanker, 55-3118, takes off for the first time. (Seattle Post Intelligencer)

Built as an aerial refueling tanker to support the U.S. Air Force fleet of B-52 strategic bombers, an initial order for 29 tankers was soon followed by three additional orders, bringing the total to 275 airplanes by the end of Fiscal Year 1958.¹ Eventually 732 KC-135As were built by Boeing, and an additional 81 of other versions.

KC-135 City of Renton. (Seattle Post-Intelligencer)
Boeing KC-135A Stratotanker 55-3118, City of Renton, just prior to touchdown. (Seattle Post-Intelligencer)

With the company internal designation of Model 717, the KC-135 was developed from the Model 367-80 proof-of-concept prototype, the “Dash Eighty.” The Stratotanker is very similar in appearance to the Model 707 and 720 airliners but is structurally a different aircraft. It is also shorter than the 707 and has a smaller diameter fuselage.

Boeing Aircraft Co. President Bill Allen talks to test pilots Tex Johnston and Dix Loesch after first flight of the Model-367-80 prototype. (Seattle Post-Intelligencer)
Boeing Aircraft Co. President Bill Allen talks to test pilots Tex Johnston and Dix Loesch after first flight of the Model 367-80, prototype of the KC-135A Stratotanker. (Seattle Post-Intelligencer)

The Stratotanker was originally operated by a flight crew of four: pilot, co-pilot, navigator, and refueling boom operator. Upgrades over the decades have simplified operation and the crew has been reduced to two pilots and the boom operator. The tanker’s maximum transfer fuel load is 200,000 pounds (90,719 kilograms). The KC-135 can carry 83,000 pounds (37,648 kilograms) of cargo, and up to 37 passengers.It can also be configured to carry cargo or up to 32 passengers.

The KC-135A is 136 feet, 3 inches (41.529 meters) long, with a wingspan of 130 feet, 10 inches (39.878 meters) and overall height of 41 feet, 8 inches (12.700 meters). The Stratotanker’s maximum takeoff weight is 322,500 pounds (146,284 kilograms).

The KC-135A was powered by four Pratt & Whitney J57-P-59W turbojet engines. The J57 was a two-spool, axial-flow engine with a 16-stage compressor section (9 low- and 7-high-pressure stages) and a 3-stage turbine section (1 high- and 2 low-pressure stages). These engines were rated at 13,750 pounds of thrust (61.16 kilonewtons), each. The J57-P-59W was 183.5 inches (4.661 meters) long, 38.9 inches (0.988 meters) long and weighed 4,320 pounds (1,920 kilograms).

The Stratotanker fleet has been re-engined with more efficient CFM International CFM56 turbofan engines which produce 21,634 pounds of thrust (96.23 kilonewtons), each. The upgraded aircraft are designated KC-135R.

Boeing KC-135A Stratotanker 55-3118, City of Renton, escorted by the “Dash 80.” (Flight Global)

The tanker has a cruise speed of 530 miles per hour (853 kilometers per hour) at 30,000 feet (9,144 meters). The service ceiling was 50,000 feet (15,240 meters). Its range is 1,500 miles (2,414 kilometers) when carrying 150,000 pounds (68,039 kilograms) of transfer fuel, and the maximum ferry range is 11,015 miles (17,727 kilometers).

Of the 803 KC-135 aircraft built, 396 remain in service with the U.S. Air Force (as of 14 May 2018). It is estimated that the fleet is 33% through their design lifetime limits.

The first production airplane, 55-3118, was used for flight testing. It was later modified into an EC-135K Head Dancer airborne command post. Today, the first Stratotanker is on display at the front gate of McConnell Air Force Base, Kansas.

Boeing KC-135A-BN Stratotanker 55-3118, City of Renton, refuels B-52C-50-BO Stratofortress 54-2676. (U.S. Air Force)

¹ KC-135A-BN: 57-1418–57-1514; 57-2589–57-2609; 58-0001–58-0130; total: 275

© 2018, Bryan R. Swopes

12 August 1977

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Space Shuttle prototype Enterprise separates from NASA 905 for its first free flight, 12 August 1977. (NASA)

12 August 1977: At Edwards Air Force Base, California, the prototype Space Shuttle Oriter, Enterprise, (OV-101) was mated to the Boeing 747-100 Shuttle Carrier Aircraft, N905NA, call sign NASA 905, for the first of five approach and landing test flights. On Enterprise‘ flight deck were astronauts Fred Haise and Gordon Fullerton. The crew of NASA 905 were NASA test pilots Fitz Fulton and Tom McMurty with Vic Horton and Skip Guidry as flight engineers.

Space Shuttle Enterprise during the first free flight, 12 August 1977. (NASA)

An estimated 65,000 people had come to Edwards to watch and at 8:00, Fitz Fulton began the take off roll down Runway 22. For the next 38 minutes the spacecraft/aircraft combination climbed together into the desert sky. After reaching an altitude of 24,100 feet (7,346 meters), Fulton put the Shuttle Carrier Aircraft into a shallow dive. At 8:48 a.m., Fred Haise fired the seven explosive bolts holding the two craft together. The 747 entered a descending left turn while Haise banked Enterprise away to the right.

Space Shuttle Orbiiter Enterprise during a glide test. (NASA)
Space Shuttle Orbiter Enterprise during a glide test. (NASA)

As Enterprise made its gliding descent, Haise and Fullerton experimented with the prototype’s flight characterisics and handling. The Shuttle Orbiter touched down on Rogers Dry Lake at 185 miles per hour (297.7 kilometers per hour), and rolled for two miles (3.22 kilometers) before coming to a complete stop.

The first free flight of Enterprise lasted 5 minutes, 21 seconds.

Space Shuttle Enterprise banks to the left to line up with the runway on Rogers Dry Lake. (NASA)
Space Shuttle Enterprise banks to the left to line up with the runway on Rogers Dry Lake. (NASA)

© 2019, Bryan R. Swopes

6 August 1955

Aviation, , , , , , , , , , , ,
Looking out across the right wing of the Boeing 367–80, inverted, at the city of Seattle, 6 August 1955. (Bill Whitehead/Boeing)

6 August 1955: Boeing’s Chief of Flight Test, Alvin M. “Tex” Johnston, barrel-rolled the Model 367-80, prototype of the KC-135 Stratotanker and 707, over Lake Washington.

Twice.

This photograph was taken by the flight test engineer, Bill Whitehead.

© 2023, Bryan R. Swopes