| Aero Commander 500 family | |
|---|---|
695A Jetprop 1000 | |
| General information | |
| Type | Utility and business aircraft |
National origin | United States |
| Manufacturer | Aero Design and Engineering Company Aero Commander Rockwell-Standard Corporation North American Rockwell Rockwell International Gulfstream Aerospace |
| Status | Active |
| Number built | ~2,902 (1951 piston-engined, 951 turboprops) |
| History | |
| Manufactured | 1951–1986 |
Introduction date | October 1952 |
| First flight | 23 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.

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.

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.
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.
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.
| model | name | approved | TC | engines | power | MTOW | ceiling | seats | fuel | built |
|---|---|---|---|---|---|---|---|---|---|---|
| L-3805 | 1 | |||||||||
| 520 | 1952-01-31 | 6A1 | 2× GO-435-C2/C2B | 2× 260 | 5500-5700 | 5 | 145 | 150 | ||
| 560 | 1954-05-28 | 6A1 | 2× GO-480-B/B1C | 2× 270 | 6000 | 7 | 145 | 80 | ||
| 520 with more power, increased weight, swept tail, plus revised wing, landing gear, fuselage, and primary control system | ||||||||||
| 560A | 1955-07-01 | 6A1 | 2× GO-480-D/C/G | 2× 275 | 6000 | 7 | 156 | |||
| 560 with longer fuselage, revised engine installation, wing, landing gear, fuel and oil systems | ||||||||||
| 560E | 1957-02-21 | 6A1 | 2× GO-480-C/G | 2× 295 | 6500 | 7 | 223 | 93 | ||
| 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 | 1961-02-08 | 2A4 | 2× IGO-540-B | 2× 350 | 7500 | 7 | 223 | |||
| 680F with normally aspirated engine and reduced gross weight | ||||||||||
| 360 | 2× 180 | 4 | 1 | |||||||
| Lightened 560E | ||||||||||
| 500 | 1958-07-24 | 6A1 | 2× O-540-A2B | 2× 250 | 6000 | 7 | 156 | 101 | ||
| 560E with decreased gross weight, powerplants, and 560A landing gear | ||||||||||
| 500A | Aero Commander | 1960-04-07 | 6A1 | 2× IO-470-M | 2× 260 | 6000 | 7 | 156 | 99 | |
| 500 with new nacelles, fuel injected Continental engines and new landing gear | ||||||||||
| 500B | 1960-07-13 | 6A1 | 2× IO-540-B/E | 2× 290 | 6750 | 7 | 156 | 217 | ||
| 500A with Lycoming engines and 3-bladed props. | ||||||||||
| 500U | Shrike Commander | 1964-12-11 | 6A1 | 2× IO-540-E | 2× 290 | 6750 | 7 | 156 | 56 | |
| 500B with pointed nose and squared off tail. | ||||||||||
| 500S | Shrike Commander | 1968-03-15 | 6A1 | 2× IO-540-E | 2× 290 | 6750 | 7 | 156 | 316 | |
| 500U with minor changes[page needed] | ||||||||||
| 680 Super | L-26C → U-4B L-26C → U-9C | 1955-10-14 | 2A4 | 2× GSO-480-A1A6 | 2× 340 | 7000 | 7 | 223 | 254 | |
| supercharged 560A | ||||||||||
| 680E | 1958-06-19 | 2A4 | 2× GSO-480-B1A6 | 2× 340 | 7500 | 7 | 223 | 100 | ||
| 680 with Lightened 560E/560A type undercarriage, extended wing and increased maximum weight | ||||||||||
| 720 | AltiCruiser | 1958-12-05 | 2A4 | 2× GSO-480-B1A6 | 2× 340 | 7500 | 6 | 223 | 13 | |
| Pressurized 680-E, structural modifications to the fuselage, extended wing and increased maximum weight | ||||||||||
| 680F | 1960-08-23 | 2A4 | 2× IGSO-540-B | 2× 380 | 8000 | 7 | 223 | 126 | ||
| 680E with fuel injection engine, new nacelles, new main gear and increased maximum weight | ||||||||||
| 680FP | 2× 380 | 223 | 26 | |||||||
| Pressurized 680F | ||||||||||
| 680FL | Grand Commander | 1963-05-24 | 2A4 | 2× IGSO-540-B | 2× 380 | 7000-8500 | 11 | 223 | 157 | |
| 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 Commander | 1964-10-08 | 2A4 | 2× IGSO-540-B1A/B1C | 2× 380 | 8500 | 11 | 223 | 37 | |
| pressurized 680FL | ||||||||||
| 680T | Turbo Commander | 1965-09-15 | 2A4 | 2× TPE-331-43 | 2× 575 | 8950 | 25,000 ft | 11 | 286.5 | 56 |
| 680FL/P turboprop | ||||||||||
| 680V | Turbo Commander | 1967-06-13 | 2A4 | 2× TPE-331-43 | 2× 575 | 9400 | 25,000 ft | 11 | 286.5 | 36 |
| 680T with slightly improved cargo capacity | ||||||||||
| 680W | Turbo II Commander | 1968-02-05 | 2A4 | 2× TPE-331-43BL | 2× 575 | 9400 | 25,000 ft | 11 | 286.5 | 46 |
| 680V with pointed nose. squared off fin, one panoramic and two small cabin windows and weather radar | ||||||||||
| 681 | Hawk Commander | 1969-03-20 | 2A4 | 2× TPE-331-43BL | 2× 575 | 9400 | 25,000 ft | 11 | 286.5 | 43 |
| 680W with improved pressurisation, air conditioning system and nose | ||||||||||
| 681B | Turbo Commander | 25,000 ft | 29 | |||||||
| Marketing designation for economy version of the 681 | ||||||||||
| 685 | Commander | 1971-09-17 | 2A4 | 2× GTSIO-520-F/K | 2× 435 | 9000 | 25,000 ft | 9 | 256-322 | 66 |
| 690 powered by piston engines | ||||||||||
| 690 | Commander 690 | 1971-07-19 | 2A4 | 2× TPE-331-5 | 2× 717.5 | 10250 | 25,000 ft | 11 | 384 | 79 |
| 681 with new wing centre section and engines moved further outboard | ||||||||||
| 690A | Commander 690A | 1973-04-25 | 2A4 | 2× TPE-331-5 | 2× 717.5 | 10250 | 31,000 ft | 11 | 384 | 245 |
| 690 with changed flightdeck layout and increased pressurisation | ||||||||||
| 690B | Commander 690B | 1976-10-05 | 2A4 | 2× TPE-331-5 | 2× 717.5 | 10325 | 31,000 ft | 10 | 384 | 217 |
| 690A with improved soundproofing and internal lavatory | ||||||||||
| 690C | Jetprop 840 | 1979-09-07 | 2A4 | 2× TPE-331-5 | 2× 717.5 | 10325 | 31,000 ft | 11 | 384 | 136 |
| 690B with increased wingspan, wet wing fuel tanks and winglets | ||||||||||
| 690D | Jetprop 900 | 1981-12-02 | 2A4 | 2× TPE 331-5 | 2× 748 | 10700 | 31,000 ft | 11 | 425-474 | 42 |
| 690C with internal rear cabin extension, improved pressurisation and five square cabin windows | ||||||||||
| 695 | Jetprop 980 | 1979-11-01 | 2A4 | 2× TPE-331-10 | 2× 733 | 10325 | 31,000 ft | 11 | 425-474 | 84 |
| more powerful 690C | ||||||||||
| 695A | Jetprop 1000 | 1981-04-30 | 2A4 | 2× TPE-331-10 | 2× 820 | 11200 | 35,000 ft | 11 | 474 | 101 |
| more powerful 690D with higher takeoff weight, built for the NOAA | ||||||||||
| 695B | Jetprop 1000B | 1984-02-15 | 2A4 | 2× TPE-331-10 | 2× 820 | 11750 | 35,000 ft | 11 | 474 | 6 |
| 695A with minor changes | ||||||||||



Data from Jane's all the world's aircraft 1976–77.
General characteristics
Performance
{{cite magazine}}: CS1 maint: deprecated archival service (link)A rugged high-performance airplane with more than just a face lift
Decades after its introduction, it remains rugged, capable… and cool