Tag Archives: Airliner

21 August 1961

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Douglas DC-8-43 N9604Z is accopmanied by a U.S. Air Force Lockheed F-104A Starfighter, near Edwards Air Force base, California.
Douglas DC-8-43 N9604Z is accompanied by a U.S. Air Force Lockheed F-104A-10-LO Starfighter, 56-749, near Edwards Air Force Base, California. (NASA test pilot Milt Thompson was forced to eject from this airplane 20 December 1962. The Starfighter was destroyed.) (Douglas Aircraft Co.)

On 21 August 1961, a Douglas DC-8-43, N9604Z, c/n 45623, Line Number 130, flown by Chief Test Pilot William Marshall Magruder, Paul Patten, Joseph Tomich and Richard H. Edwards climbed to 50,090 feet (15,267 meters) near Edwards Air Force Base. Placing the DC-8 into a dive, it reached Mach 1.012 (668 miles per hour/1,075 kilometers per hour) while descending through 41,088 feet (12,524 meters). The airliner maintained this supersonic speed for 16 seconds. This was the first time that a civil airliner had “broken the Sound Barrier.”

An Air Force F-100 Super Sabre and F-104 Starfighter were chase planes for this flight. Reportedly, the F-104 was flown by the legendary test pilot, Colonel Chuck Yeager.

Canadian Pacific Douglas DC-8-43 CF-CPG, Empress of Montreal. (Photograph © Peter Scharkowski. Used with permission)

The Douglas DC-8 is a commercial jet airliner, a contemporary of the Boeing 707 and Convair 880. It was operated by a flight crew of three and could carry up to 177 passengers. The DC-8 was powered by four turbojet or turbofan engines mounted on pylons suspended below the wings. The wings’ leading edges were swept to 30°, as was the vertical fin and horizontal tailplane.

The DC-8-40 series is 150 feet, 6 inches (45.872 meters) long with a wingspan of 142 feet, 5 inches (43.409 meters) and overall height of 42 feet, 4 inches (12.903 meters). It had an empty weight of 124,790 pounds (56,604 kilograms) and maximum takeoff weight of 315,000 pounds (142,882 kilograms).

The DC-8-40 series had a cruising speed of 0.82 Mach (542 miles per hour/872 kilometers per hour) at 35,000 feet (10,668 meters). Its maximum range was 5,905 nautical miles (6,795 statute miles, 10,936 kilometers).

N9604Z was powered by four Rolls-Royce Conway RCo.12 Mk 509 two-shaft axial-flow turbofan engines, rated at 17,500 pounds of thrust (77.844 kilonewtons) at 9,990 r.p.m. The 509 is 11 feet, 3.9 inches (3.452 meters) long, 3 feet, 6.2 inches (1.072 meters) in diameter, and weighs 4,542 pounds (2,060 kilograms).

N9604Z was delivered to Canadian Pacific Airlines 15 November 1961, re-registered CF-CPG, and named Empress of Montreal. It later flew under CP Air as Empress of Buenos Aires. The DC-8 was scrapped at Opa Locka Municipal Airport, north of Miami, Florida, in May 1981.

© 2016, Bryan R. Swopes

15 August 1962

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An American Airlines Boeing 707-023B Astrojet (720B) at Los Angeles International Airport, 26 December 1962. (Photograph courtesy of Jon Proctor)
An American Airlines Boeing 707-023B Astrojet (720B) at Los Angeles International Airport, 26 December 1962. (Photograph used with the permission of Jon Proctor)

15 August 1962: American Airlines’ Captain Eugene M. (“Gene”) Kruse set two National Aeronautic Association Class C-1 records for Speed Over a Commercial Air Route, East to West Transcontinental, when he flew a Boeing 720B Astrojet from New York to Los Angeles, 2,474 miles (3,981.5 kilometers), in 4 hours, 19 minutes, 15 seconds, at an average speed of 572.57 miles per hour (921.46 kilometers per hour). 61 years later, these records still stand.

Screen Shot 2015-01-02 at 12.22.27 The National Aeronautic Association has placed Captain Kruse’s records on its “Most Wanted” list: long-standing flight records that it would like to see challenged. Rules require that a new record exceed the old by at least a 1% margin. The performance needed to establish a new record would be 578.30 miles per hour (930.68 kilometers per hour).

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.

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).

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

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.

© 2018, Bryan R. Swopes

2 August 1947

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British South American Airways’ Avro Lancastrian Mk.III, G-AGWH, R.M.A. Star Dust. (SDASM)

2 August 1947: At 1:46 p.m., British South American Airways Flight CS59 departed Buenos Aires, Argentina enroute Santiago, Chile. The airliner was an Avro Lancastrian Mk.III, registration G-AGWH, named R.M.A. Star Dust. The flight was under the command of Captain Reginald J. Cook, D.S.O., D.F.C., D.F.M., with First Officer Norman Hilton Cook, Second Officer Donald S. Checklin, Radio Operator Dennis B. Harmer and “Stargirl” Iris Morcen Evans. On this flight, in addition to the five-person airline crew, there were just six passengers.

Captain Reginald J. Cook, D.S.O., D.F.C., D.F.M.

At 5:41 p.m., Santiago airport received a routine Morse code signal from G-AGWH indicating the flight would arrive in four minutes:

ETA SANTIAGO 17.45 HRS STENDEC

The radio operator at Santiago did not understand “STENDEC” and asked the airliner’s radio operator to repeat it, which he did, twice. The airliner never arrived. A five-day search was unsuccessful. The meaning of the last word in the message has never been determined.

The fate of Star Dust remained a mystery until 1998, when two mountain climbers on Mount Tupungato—at 21,555 feet (6,570 meters), one of the highest mountains in South America—50 miles east of Santiago, found a wrecked Rolls-Royce Merlin aircraft engine in the ice of a glacier at the 15,000 foot level (4,572 meters). A search of the glacier in 2000 located additional wreckage and it was confirmed that this was the missing Lancastrian. The crash site is at S. 33°22’15.0″, W. 69°45’40.0″.

Investigators determined that the airliner had flown into the glacier at high speed and the crash caused an avalanche which buried the wreckage.

In 2002 the remains of eight persons were recovered from the glacier, five of which were identified through DNA.

Volcan Tupungato, 21,560 feet (6,570 meters). (Diode via Wikipedia)
1948 B.S.A.A. advertisement.

The Avro 691 Lancastrian Mk.III was a four-engine civil transport based on the World War II very long range heavy bomber, the Avro Lancaster. The Mk.III variant was built specifically for the British South American Airways Corporation by A.V. Roe & Co. Ltd, at Woodford, Cheshire, England, and was an improved version of the British Overseas Airways Corporation Lancastrian Mk.I. Eighteen Mk.IIIs were built for BSAAC. G-AGWH, serial number 1280, was the second of this series. It first flew on 11 November 1945 and was registered to BSAAC 16 January 1946.

The airliner was operated by a flight crew of four and carried one flight attendant. It could carry up to thirteen passengers. The Lancastrian Mk.III was 76 feet, 10 inches (23.419 meters) long with a wingspan of 102 feet (31.090 meters) and overall height of 19 feet, 6 inches (5.944 meters). The empty weight was 30,220 pounds (13,707.6 kilograms) and gross weight was 65,000 pounds (29,483.5 kilograms).

Avro Lancastrian Mk.III, G-AGWH, R.M.A. Star Dust

The Lancastrian Mk.III was powered by four 1,648.9-cubic-inch-displacement (27.04 liter) liquid-cooled, supercharged, Rolls-Royce Merlin T24/2 ¹ single overhead camshaft (SOHC) 60° V-12 engines producing 1,650 horsepower and turning three bladed propellers.

These gave the airplane a cruise speed of 245 miles per hour (394.3 kilometers per hour) and a maximum speed of 315 miles per hour (506.9 kilometers per hour). The service ceiling was 25,500 feet (7,772 meters) and the range was 4,150 miles (6,679 kilometers).

Site of the wreck of Avro Lancastrian G-AGWH, S. 33°22’15.0″, W. 69°45’40.0″. (Google Maps)

¹ Two of G-AGWH’s Merlin T24/2 engines had been completely overhauled and converted to the Merlin 500-2 configuration. One engine was converted to a Merlin 502. The fourth engine remained as a T24/2. All engines had less than 1,200 hours total time since new (TTSN) and the converted engines were approximately 500 hours since overhaul (TSOH).

© 2018, Bryan R. Swopes

23 July 1983

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Air Canada Flight 143, a Boeing 767-200, C-GAUN, after emergency landing at Gimli, Manitoba, 23 July 1983. (Wayne Glowacki / Winnipeg Free Press)
Air Canada Flight 143, a Boeing 767-200, C-GAUN, after emergency landing at Gimli, Manitoba, 23 July 1983. (Wayne Glowacki / Winnipeg Free Press)
Captain Robert Pearson
Captain Robert Pearson

23 July 1983: Air Canada Flight 143 was a Boeing 767-200, registration C-GAUN, enroute from Montreal to Edmonton, with a stop at Ottawa. On board were 61 passengers and a crew of eight. On the flight deck were Captain Robert Pearson and First Officer Maurice Quintal.

At 1:21 p.m., at 41,000 feet (12,497 meters) over Red Lake, Ontario, the 767 ran out of fuel and both engines stopped. This caused a loss of electrical and hydraulic power to the aircraft. The 767 was equipped with a “glass cockpit” and the pilots lost most of their instrumentation. The airliner became very difficult to fly without the hydraulic system functioning, and flaps and landing gear were inoperative.

Unable to reach Winnipeg for an emergency landing, Captain Pearson turned toward a closed airport, the former RCAF Station Gimli. First Officer Quintal had been stationed there during his military service.

Pearson had extensive experience flying gliders and used this knowledge to extend the glide of the 767. The airliner touched down on a closed runway that was being used as a race track. The nose gear, which had not locked when dropped by gravity, collapsed, and the airliner suffered some damage as it slid to a stop.

Of those aboard, there were ten people injured. The airliner was forever after known as “The Gimli Glider.”

The investigation of the accident faulted the airline for not reassigning the responsibility for calculating the fuel load when use of a flight engineer became unnecessary with the new Boeing 767, which was designed to be flown by a two-pilot crew. Also, the recent change from the Imperial measurement system to metric resulted in a series of miscalculations as to how much fuel was actually aboard the aircraft before the flight.

In 2008, C-GAUN was retired to The Boneyard at Mojave, California. Captains Pearson and Quintal and several of the Flight 143 flight attendants were aboard on her final flight.

Air Canada’s Boeing 767-200, C-GAUN, “The Gimli Glider,” in storage at Mojave. (Akradecki via Wikipedia)

© 2016, Bryan R. Swopes

23 July 1970

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McDonnell Douglas DC-10 rollout at Long Beach, 23 July 1970. (Boeing)

23 July 1970: At Long Beach, California, the first McDonnell Douglas DC-10 airliner was rolled out. A DC-10-10, serial number 46500 with FAA registration N10DC, this aircraft was used for flight testing and Federal Aviation Administration certification. It made 989 test flights, accumulating 1,551 flight hours. It was put into commercial service with American Airlines 12 August 1972, re-registered as N101AA.

The DC-10 was a wide-body commercial airliner designed for medium to long range flights. It was flown by a crew of three and depending on the cabin arrangement, carried between 202 and 390 passengers. The DC-10-10 was 170 feet, 6 inches (51.968 meters) long with a wingspan of 155 feet, 4 inches (47.346 meters) and overall height of 58 feet, 1 inch (17.704 meters). The airliner had an empty weight of 240,171 pounds (108,940 kilograms) and maximum takeoff weight of 430,000 pounds (195,045 kilograms). It was powered by three General Electric CF6-6D turbofan engines, producing 40,000 pounds of thrust, each. These gave the DC-10 a maximum cruise speed of Mach 0.88 (610 miles per hour, 982 kilometers per hour). Its range is 3,800 miles (6,116 kilometers) and the service ceiling is 42,000 feet (12,802 meters).

In production from 1970 to 1988, a total of 386 DC-10s were built in passenger and freighter versions. 122 were the DC-10-10 variant. Another 60 KC-10A Extender air refueling tankers were built for the U.S. Air Force and 2 KDC-10 tankers for the Royal Netherlands Air Force.

The first McDonnell Douglas DC-10 was in service with American Airlines from 12 August 1972 to 15 November 1994 when it was withdrawn from service and placed in storage at Tulsa, Oklahoma. The 24-year-old airliner had accumulated 63,325 flight hours.

After three years in storage, the first DC-10 returned to service flying for Federal Express. In 1998 it was modernized as an MD-10 and re-registered again, this time as N530FE. It was finally retired from service and scrapped at Goodyear, Arizona in 2002.

© 2015, Bryan R. Swopes