Aero Commander 500 family

Aero Commander 500 family
695A Jetprop 1000
General information
TypeUtility and business aircraft
National origin
United States
ManufacturerAero Design and Engineering Company
Aero Commander
Rockwell-Standard Corporation
North American Rockwell
Rockwell International
Gulfstream Aerospace
StatusActive
Number built~2,902 (1951 piston-engined, 951 turboprops)
History
Manufactured1951–1986
Introduction date
October 1952
First flight23 April 1948 (Model L3085)
Developed into
IAI Westwind

The Aero Commander 500 family (also known as the Twin Commander) is a series of light twin piston-engined and turboprop aircraft designed and originally produced by the Aero Design and Engineering Company in the late 1940s, renamed the Aero Commander company in 1950, and later a division of Rockwell International in 1965. Final production occurred in 1986 under the Gulfstream Aerospace name.

The initial production version, which was first delivered in 1951, was the 200 mph (320 km/h; 170 kn), seven-seat Aero Commander 520. Numerous early aircraft were sold to military operators, including the United States Air Force and the United States Army. One was used as the presidential transport aircraft, Air Force One, for Dwight D. Eisenhower between 1956 and 1960. The Belgian Air Force also flew one as the personal transport of Baudouin of Belgium between 1961 and 1973. The Aero Commander was also operated by various types of civil operators, including as a business aircraft and cargo aircraft. During its later service life, the Federal Aviation Administration (FAA) looked into the aircraft's main wing spar, which was believed to be susceptible to stress fatigue and subsequent cracking, thus allegedly resulting in several fatal crashes.

Further development of the Aero Commander proceeded throughout the type's production life of almost 40 years. In 1967, an improved version of that aircraft, the 500S Shrike Commander, was launched. Several of the larger variants have been given their own model names and designations, ranging up to the 330 mph (530 km/h; 290 kn), 11-seat Model 695B/Jetprop 1000B turboprop.

Design and development

The first model, the five-seat 520, was certified in January 1952 with two 260 HP Lycoming GO-435s

The concept for the Commander light business twin was conceived by Ted Smith, a project engineer at the Douglas Aircraft Company. Working part-time after hours throughout 1944, a group of engineers that worked on the Douglas A-20 Havoc came together to form the Aero Design and Engineering Company with the goal of designing and producing this envisioned aircraft, which would have a layout similar to their A-20 bomber. Originally, the new company was going to build three pre-production aircraft, but as the first aircraft was being built, they decided to build just one prototype. The final configuration was completed in July 1946 and was designated the Model L3805.

Registered NX1946, the prototype first flew on 23 April 1948. The L3805 accommodated up to five people and was powered by a pair of Lycoming O-435-A piston engines. It was an all-metal high-wing monoplane with retractable undercarriage and used several components sourced from a Vultee BT-13 Valiant. The market segment planned for this aircraft included small feeder airliners, aided by its range of 1,000 miles; however, in practice, the majority of customer demand came from the private business aircraft sector as well as military operators. Walter Beech test flew the aircraft in 1949 and expressed interest in buying the project, but ultimately chose to pass on the aircraft to instead develop the Beechcraft Twin Bonanza. Fairchild Aircraft also evaluated the prototype at its headquarters in Hagerstown, Maryland.

The prototype successfully validated the aircraft's design. The company secured a lease on a new 26,000 square feet (2,400 m2) factory at Bethany near Oklahoma City to build a production version, which was certified on 30 June 1950. Nearly 10,000 hours of redesign work took place to produce the initial production aircraft, which was equipped with more powerful Lycoming GO-435-C2 engines, which had a combined rating of 520 horsepower (390 kW). The first of these production aircraft, which was named the Commander 520, was rolled out of the Bethany factory in August 1951. Serial number 1 was briefly used as a demonstrator before being sold in October 1952 to the Asahi Shimbun Press Company of Tokyo.[citation needed]

In terms of its general configuration, the Aero Commander 500 is an all-metal twin-engined light transport aircraft, fitted with a high-mounted cantilever wing and furnished with retractable landing gear. The aircraft is primarily composed of aluminium and uses semi-monocoque construction. Later-built models, such as the Shrike Commander 500S, were outfitted with an avionics suit to facilitate all-weather flight, and could be optionally equipped with deicing boots for use in cold climates. The Shrike Commander model could accommodate a seven-seat cabin configuration if a rear bench seat was fitted. Numerous amenities could also be fitted in the cabin, including curtains, a fold-away desk, and storage cabinets. On later models, the fuselage was stretched, the gross weight increased, and more powerful engines were fitted.

While not a typical use of the type, the aircraft's favourable handling capabilities at both high and low speeds, even when flow with a single working engine, led to it being occasionally performing aerobatic manoeuvress. While such display aircraft did not typically require without major modifications, they were sometimes fitted with propeller unfeathering systems as well as smoke generators. As all of the fuel tanks are interconnected, there was no need for pilots to perform either tank selection or cross-feeding. The landing gear had been designed for use on aircraft twice the size of the Aero Commander, making it relatively sturdy and well-suited to use from unprepared airstrips.

Operational history

Special mission cabin for the NOAA

In US military service, it was initially designated the L-26, though in 1962 this was changed to U-4 for the United States Air Force and U-9 for the United States Army.

Under ownership of Rockwell in the 1960s, World War II pilot R. A. "Bob" Hoover demonstrated the Shrike Commander 500S for decades in a variety of "managed energy" routines, including single-engine and engine-out aerobatics. His Shrike Commander is displayed in the colors of his last sponsor, Evergreen International Aviation, at the Steven F. Udvar-Hazy Center of the Smithsonian National Air and Space Museum. Bob Odegaard continued the tradition in 2012, flying a 1975 Shrike 500S in a Bob Hoover tribute routine.

One U-4B was operated as Air Force One, the presidential transport aircraft, for Dwight D. Eisenhower between 1956 and 1960. Often personally flown by Eisenhower, it was the first presidential aircraft to be powered by only two engines as well as the first to wear the now-familiar blue-and-white livery. Also used to transport other senior politicians, such as the Secretary of Defense and the Secretary of the Air Force, it was later transferred to the USAF Academy’s skydiving team. This aircraft is now owned by the Commemorative Air Force.

By 2004, numerous Shrike Commanders remained in service with the United States Customs Service, United States Coast Guard, and United States Forest Service.

A single 560F was operated by the Belgian Air Force as the personal transport of the late king Baudouin of Belgium between 1961 and 1973.

According to the July 1, 1968, Frontier Airlines system timetable, series 500 aircraft were being operated on scheduled passenger flights by Combs Aviation on behalf of Frontier via a contract agreement with service to several smaller communities in Montana and Wyoming at this time.

The unpressurized, long-fuselage 680FL was operated as a small package freighter by Combs Freightair in the 1970s and 1980s, and by Suburban Air Freight in the 1980s and 1990s. The aircraft was popular with pilots, because it was extremely "pilot friendly" and with its 380 hp (280 kW) supercharged engines did well in icing meteorological conditions. A number are still operated on contracts for cargo and fire control applications, as their piston engines offer good fuel specifics at low altitudes and longer loiter times. Suburban retired their last 680FLs in the first half of 2024.

Wing spar fatigue

In June 1991, senior company engineers met with Federal Aviation Administration (FAA) officials to discuss concerns over the Aero Commander's main wing spar, which was believed to be susceptible to stress fatigue and subsequent cracking, and was believed to have resulted in a number of fatal crashes. From approximately 1961 to 1993, 24 aircraft crashed when spar failures caused the loss of the wing in flight. 35 more spars were found cracked during inspections.

Single-engine safety

In 1950, when the developers were working to satisfy Civil Aeronautics Authority (CAA) regulations for certification of the 500, they chose a novel method of demonstrating its single-engine safety and performance: they removed one of the two-bladed propellers, secured it in the aft cabin, and flew from Bethany to Washington, D.C., on one engine. There they met with CAA personnel, then replaced the propeller and returned to Oklahoma in the conventional manner. The flight received nationwide coverage in the press.

In 1979, the National Transportation Safety Board reviewed light-twin engine-failure accidents, involving the 24 most popular model-groups of light twins between 1972 and 1976. They found that the piston-engined twin-Commanders had averaged slightly over 3.4 engine-failure accidents per hundred-thousand hours, the second worst number of all aircraft under review. The most engine failures were suffered by the small-engine versions of the Piper Apache, at 6.9 failures per hundred thousand hours; the third-worst, the Beechcraft Travel Air, averaged 2.9 failures; the average for all models was only 1.6.

Countering the statistical evidence, Rockwell demonstration pilot Bob Hoover's airshow stunt routine, with the Shrike Commander, included a full aerobatic routine performed first with both engines, then with one engine out (and the critical engine, at that), then both engines out, and gliding. Then in his final airshow performance, in a demonstration of conservation of momentum, he landed. The Shrike Commander dead stick (engines off), coasted the airplane down the runway then from the runway and taxied to the audience.

The turboprop twin-Commanders—with much more powerful engines (and most with longer bodies, allowing greater rudder leverage, critical for single-engine control) – came out on the opposite end of the rankings, with one of the lowest rates of engine-failure accidents of all "light" twins examined, at only 0.4 per hundred-thousand hours.

Variants

Type certificate data sheet 6A1 and 2A4
modelnameapprovedTCenginespowerMTOWceilingseatsfuelbuilt
L-3805 1
520 1952-01-316A12× GO-435-C2/C2B2× 2605500-57005145150
560 1954-05-286A12× GO-480-B/B1C2× 2706000714580
520 with more power, increased weight, swept tail, plus revised wing, landing gear, fuselage, and primary control system
560A 1955-07-016A12× GO-480-D/C/G2× 27560007156
560 with longer fuselage, revised engine installation, wing, landing gear, fuel and oil systems
560E 1957-02-216A12× GO-480-C/G2× 2956500722393
560A with Larger wings and greater payload, revised engine installation, wing, wheel and brake installation, fuel system with outboard tanks, and landing gear location
560F 1961-02-082A42× IGO-540-B2× 35075007223
680F with normally aspirated engine and reduced gross weight
360 2× 18041
Lightened 560E
500 1958-07-246A12× O-540-A2B2× 25060007156101
560E with decreased gross weight, powerplants, and 560A landing gear
500A Aero Commander1960-04-076A12× IO-470-M2× 2606000715699
500 with new nacelles, fuel injected Continental engines and new landing gear
500B 1960-07-136A12× IO-540-B/E2× 29067507156217
500A with Lycoming engines and 3-bladed props.
500U Shrike Commander1964-12-116A12× IO-540-E2× 2906750715656
500B with pointed nose and squared off tail.
500S Shrike Commander1968-03-156A12× IO-540-E2× 29067507156316
500U with minor changes[page needed]
680 Super L-26C → U-4B
L-26C → U-9C
1955-10-142A42× GSO-480-A1A62× 34070007223254
supercharged 560A
680E 1958-06-192A42× GSO-480-B1A62× 34075007223100
680 with Lightened 560E/560A type undercarriage, extended wing and increased maximum weight
720 AltiCruiser1958-12-052A42× GSO-480-B1A62× 3407500622313
Pressurized 680-E, structural modifications to the fuselage, extended wing and increased maximum weight
680F 1960-08-232A42× IGSO-540-B2× 38080007223126
680E with fuel injection engine, new nacelles, new main gear and increased maximum weight
680FP 2× 38022326
Pressurized 680F
680FL Grand Commander1963-05-242A42× IGSO-540-B2× 3807000-850011223157
680F with larger tail, 2 built for the US Army as the RL-26D → RU-9D with SLAR, Courser Commander after 1967; stretched
680FL(P) Grand Commander1964-10-082A42× IGSO-540-B1A/B1C2× 38085001122337
pressurized 680FL
680T Turbo Commander1965-09-152A42× TPE-331-432× 575895025,000 ft11286.556
680FL/P turboprop
680V Turbo Commander1967-06-132A42× TPE-331-432× 575940025,000 ft11286.536
680T with slightly improved cargo capacity
680W Turbo II Commander1968-02-052A42× TPE-331-43BL2× 575940025,000 ft11286.546
680V with pointed nose. squared off fin, one panoramic and two small cabin windows and weather radar
681 Hawk Commander1969-03-202A42× TPE-331-43BL2× 575940025,000 ft11286.543
680W with improved pressurisation, air conditioning system and nose
681B Turbo Commander25,000 ft29
Marketing designation for economy version of the 681
685 Commander1971-09-172A42× GTSIO-520-F/K2× 435900025,000 ft9256-32266
690 powered by piston engines
690 Commander 6901971-07-192A42× TPE-331-52× 717.51025025,000 ft1138479
681 with new wing centre section and engines moved further outboard
690A Commander 690A1973-04-252A42× TPE-331-52× 717.51025031,000 ft11384245
690 with changed flightdeck layout and increased pressurisation
690B Commander 690B1976-10-052A42× TPE-331-52× 717.51032531,000 ft10384217
690A with improved soundproofing and internal lavatory
690C Jetprop 8401979-09-072A42× TPE-331-52× 717.51032531,000 ft11384136
690B with increased wingspan, wet wing fuel tanks and winglets
690D Jetprop 9001981-12-022A42× TPE 331-52× 7481070031,000 ft11425-47442
690C with internal rear cabin extension, improved pressurisation and five square cabin windows
695 Jetprop 9801979-11-012A42× TPE-331-102× 7331032531,000 ft11425-47484
more powerful 690C
695A Jetprop 10001981-04-302A42× TPE-331-102× 8201120035,000 ft11474101
more powerful 690D with higher takeoff weight, built for the NOAA
695B Jetprop 1000B1984-02-152A42× TPE-331-102× 8201175035,000 ft114746
695A with minor changes

Operators

Islamic Republic of Iran Army Aviation 690A
Argentine Air Force 500U

Government operators

Military operators

 Algeria
 Angola
 Argentina
 Bahamas
 Benin
 Bolivia
 Burkina Faso
 Colombia
 Costa Rica
 Cuba
 Dominican Republic
 Greece
 Guatemala
 Honduras
 Indonesia
 Iran
 Ivory Coast
 Kenya
Laos Kingdom of Laos
 Republic of Korea
 Mexico
 Nicaragua
 Niger
 Pakistan
 Panama
 Philippines
 Thailand
 United States
 Venezuela

Civil operators

 Samoa

Notable accidents


Specifications (Rockwell Aero Commander 500S)

3-view line drawing of the Aero Commander L-26B
3-view line drawing of the Aero Commander L-26B

Data from Jane's all the world's aircraft 1976–77.

General characteristics

Performance

See also

References

Notes

  1. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 [citation needed]
  2. ↑ 2 built for the US Air Force
  3. ↑ 4 built for the US Army

Citations

  1. 1 2 3 "President Eisenhower's Twin-Engine Air Force One". Ike's Bird. Archived from the original on 27 October 2020.
  2. 1 2 3 "Rockwell U-9A Aero Commander". March Field Air Museum. Archived from the original on 18 August 2007. Retrieved 1 August 2007.
  3. 1 2 3 4 5 Collman, B.J. (May–June 1973). "The Aero Commander Twins". Air-Britain Digest. 15 (3): 79–86.
  4. 1 2 Twombly, Ian J. (1 June 2020). "Airplanes we love: Twin Commander 500S". Aircraft Owners and Pilots Association.
  5. 1 2 Williams, Nicholis M (Spring 1990). "The Aero Commander 520". AAHS Journal.
  6. ↑ Welsh, Jonathan (13 March 2024). "This 1974 Aero Commander 500S Is a Pioneer Light Twin and an 'AircraftForSale' Top Pick". flyingmag.com.
  7. ↑ "What's New in Aviation: Feederliner Makes Debut". Popular Science. Vol. 153, no. 2. August 1948. p. 90.
  8. 1 2 3 4 "North American Rockwell Shrike Commander 500S, Robert A. "Bob" Hoover". National Air and Space Museum.
  9. ↑ "This 1960 Aero Commander 500 Is a Pioneering 'AircraftForSale' Top Pick". flyingmag.com. 24 October 2024.
  10. ↑ "ROCKWELL COMMANDER "SHRIKE"(AERO COMMANDER 500)". planeandpilotmag.com. 13 March 2009.
  11. ↑ "Shrike Commander". Flying. July 1972. pp. 72–73, 76.
  12. ↑ Collins, Richard L. (January 1999). "Grand Renaissance: The rebirth of the tough bird". Flying. Vol. 126, no. 1. pp. 80–83.
  13. ↑ "missing". Sport Aviation: 30. June 2011.
  14. 1 2 "Aero Commander U-4B". National Museum of the United States Air Force. Retrieved 11 October 2026.
  15. ↑ Suciu, Peter (22 June 2020). "Did You Know: Any Plane Carrying President Trump Is Technically 'Air Force One'". nationalinterest.org.
  16. ↑ "Aerocommander 560f". Archived from the original on 17 February 2010.
  17. ↑ "fl6807-1 JPG file".
  18. ↑ "fl6807-4 JPG file".
  19. 1 2 3 Swift, S. J. (1 May 1995), The Aero Commander chronicle (PDF), Civil Aviation Safety Authority, retrieved 1 August 2007
  20. ↑ Harris, Richard. "The Aero Commander Line – A short history". Archived from the original on 13 July 2011. Retrieved 13 August 2011.
  21. 1 2 Smith, Thomas Motley (1981). Multiengine Airplane Rating: A Guide to the FAA Oral and Flight Tests. Pan American Navigation Service. ISBN 0-87219-003-X. OCLC 7958067.
  22. 1 2 3 "Special Study: "Light Twin-Engine Aircraft Accidents Following Engine Failures, 1972–1976 NTSB-AAS-79-2" (PDF). Washington, D.C.: National Transportation Safety Board. 1979. Retrieved 16 May 2017.
  23. 1 2 Ibold, Ken, ed. (2001). Aviation Consumer's Used Aircraft Guide. Vol. 2 (9 ed.). Greenwich, Connecticut: Belvoir Publications.
  24. ↑ Cochrane, Dorothy (20 February 2014). "Robert A_ "Bob" Hoover, The Greatest Stick and Rudder Man, is Honored in Hollywood". Smithsonian National Air and Space Museum. Washington, D.C. Retrieved 16 May 2017.
  25. ↑ "Bob Hoover flies west". GeneralAviationNews.com. 25 October 2016. Retrieved 29 August 2020.
  26. ↑ "Bob Hoover's Last Air Show". 15 June 2015 – via YouTube.
  27. ↑ "Checkout in a Multiengine Airplane". Flight Training Handbook Advisory Circular 61-21A. Federal Aviation Administration.
  28. ↑ "Type Certificate data sheet No. 6A1" (PDF). FAA. 25 September 2015. Archived from the original (PDF) on 19 June 2022. Retrieved 27 January 2022.
  29. ↑ "Type Certificate data sheet No. 2A4" (PDF). FAA. 25 September 2015. Archived from the original (PDF) on 2 November 2016.
  30. ↑ Simpson 1995
  31. ↑ "Aircraft History". TxDPS. Archived from the original on 28 August 2018. Retrieved 27 August 2018.
  32. ↑ Seymour, Paul (28 December 2018). "AERO COMMANDER 560A, P-2001 / 310-73, INDONESIAN POLICE / POLISI". ABPIC. Retrieved 1 April 2021.
  33. ↑ Flight International 29 November 1986, p. 32
  34. ↑ Flight International 29 November 1986, p. 33
  35. ↑ Andrade 1982, p. 12
  36. ↑ Andrade 1982, p. 13
  37. ↑ "Royal Bahamas Defence Force (RBDF) – Air Wing". LA MILITARY. 9 April 2016.
  38. ↑ Andrade 1982, p. 26
  39. ↑ Flight International 29 November 1986, p. 37
  40. ↑ Flight International 29 November 1986, p. 39
  41. ↑ "World Air Forces 2022". FlightGlobal. 2022. Retrieved 17 July 2022.
  42. ↑ "División de Aviación Asalto Aéreo incorpora nuevo avión Turbo Commander 690D". webinfomil.com. 10 March 2014. Retrieved 19 December 2016.
  43. ↑ Hagedorn 1993, p. 128
  44. ↑ Hagedorn 1993, p. 18
  45. ↑ Flight International 29 November 1986, p. 49
  46. ↑ Andrade 1982, p. 94
  47. ↑ Hagedorn 1993, p. 55
  48. 1 2 "World Air Forces 2021". FlightGlobal. 4 December 2020. Retrieved 10 August 2021.
  49. ↑ Andrade 1982, p. 106
  50. ↑ Andrade 1982, p. 107
  51. ↑ Andrade 1982, p. 109
  52. ↑ Andrade 1982, p. 110
  53. ↑ Andrade 1982, p. 126
  54. ↑ Andrade 1982, p. 141
  55. ↑ "Royal Lao Air Force Aircraft Types". aeroflight.co.uk. Retrieved 19 December 2016.
  56. ↑ Andrade 1982, p. 143
  57. ↑ Andrade 1982, p. 156
  58. ↑ Hagedorn 1993, p. 42
  59. ↑ Andrade 1982, p. 167
  60. ↑ Andrade 1982, p. 172
  61. ↑ Andrade 1982, p. 173
  62. ↑ Hagedorn 1993, p. 120
  63. ↑ "World Air Forces 2025". Flightglobal Insight. 2024. Retrieved 10 December 2024.
  64. ↑ Flight International 29 November 1986, p. 92
  65. ↑ "Thai Military Aircraft Designations". designation-systems.net. Retrieved 18 March 2025.
  66. 1 2 Andrade 1979, p. 134
  67. ↑ "When in Samoa, fly with Talofa and its Twin Commanders". Flight Levels Online. 21 (3). 2016. Archived from the original on 17 April 2023. Retrieved 27 May 2021.
  68. ↑ "Teddy's Ordeal". Time. 26 June 1964. Retrieved 23 May 2008.{{cite magazine}}: CS1 maint: deprecated archival service (link)
  69. ↑ "The Luck of the Kennedys". Check-Six.com. 8 May 2008. Archived from the original on 1 February 2009. Retrieved 24 February 2009.
  70. ↑ "John F. Kennedy Jr. – Timeline: Misfortunes of a Family". CNN. July 1999. Archived from the original on 23 March 2008. Retrieved 23 May 2008.
  71. ↑ Swidey, Neil (16 February 2009). "Chapter 2: The Youngest Brother: Turbulence and tragedies eclipse early triumphs". The Boston Globe. Archived from the original on 22 February 2009. Retrieved 24 February 2009.
  72. ↑ "Biography for Audie Murphy". IMDb. 1 August 2007. Retrieved 1 August 2007.
  73. ↑ "Crash of a Rockwell Aero Commander 560F in Granada Hills: 1 killed". Bureau of Aircraft Accidents. Retrieved 16 July 2021.
  74. ↑ "INVESTIGATION REPORT 9402804 Rockwell Commander 690B VH-SVQ en route Williamtown to Lord Howe Island New South Wales 2 October 1994" (PDF). Bureau of Air Safety Investigation. Retrieved 12 October 2024.
  75. ↑ Delgado, Ray (12 August 2002). "Galen Rowell 1940–2002". San Francisco Chronicle. Hearst Communications Inc. Retrieved 27 November 2016.
  76. ↑ Ranter, Harro. "Accident Rockwell Aero Commander 690C Jetprop 840 C-FNRP, Wednesday 24 June 2026". aviation-safety.net. Retrieved 30 June 2026.
  77. ↑ Taylor 1976, pp. 346–347

Bibliography