Aero Commander 500

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Aero Commander 500
Aero Commander.jpg
Aero Commander 690A
Type: Business jet
Design country:

United StatesUnited States United States

Manufacturer:

Aero Design and Engineering Company , Rockwell

First flight:

April 23, 1948

Production time:

1948-1985

Number of pieces:

approx. 2000

The Aero Commander 500 is a light twin-engine propeller-driven aircraft that was developed by the Aero Design and Engineering Company in the late 1940s . The company was taken over by Rockwell in 1958 . In 1967 the model was renamed the Shrike Commander .

history

The idea for this aircraft came from two employees of the Douglas Aircraft Company , who founded their own company in 1944 to make the model a reality. The designers designed an all-metal aircraft that was designed as a shoulder- wing wing and had a retractable nose wheel landing gear . The aircraft had space for five people and was powered by two piston engines.

The first prototype flew on April 23, 1948 under the designation L-3085 . In the following 37 years, twenty-nine versions were created based on the Aero Commander 520 . Some variants received turboprop drives and were then called Turbo Commander or Jetprop Commander . The last models had up to eleven seats in the stretched trunk, some of them had a pressurized cabin . After about two thousand aircraft, production ceased in 1985.

variants

Aero Commander 500A
Aero Commander L-3805
Prototype, one copy built.
Aero Commander 520
First production version, a developed L-3805 with a larger vertical tail unit and a larger cabin with two 260 hp Lycoming GO-435-C engines , 150 units built.
Aero Commander 560
Model 520 with swept tail unit, increased take-off weight, seven seats, more powerful engines (two Lycoming GO-480B engines) and improved wings, 80 units built.
Aero Commander 560A
New landing gear, extended fuselage and numerous other improvements, 99 units built.
Aero Commander 560E
Enlarged wings and a larger payload, 93 units built.
Aero Commander 360
Light version of the 560E with four seats and two 180 hp engines, one copy built.
Aero Commander 500
Economy version introduced in 1958, as the 560E with 250 hp Lycoming O-540-A engines , 101 units built.
Aero Commander 500A
First Aero Commander model - new nacelles with injection engines, 99 pieces built.
Aero Commander 500B
560E with injection engines Lycoming IO-540 engines, 217 pieces built.
Aero Commander 500U / Shrike Commander
500B with a pointed nose and modified rear end, two 290 hp Lycoming IO-540 engines, replaces 500A, 500B, 560F and 680F, 56 units built.
Aero Commander 680 Super
Further development of the 560A with supercharged 340 hp Lycoming GSO-480-A engines and increased fuel capacity, 254 units built.
Aero Commander 680E
Light-weight 560E with 560A-type chassis, 100 pieces built.
Aero Commander 680F
680E with new landing gear and charged injection engines Lycoming IGSO-540 and new nacelles, 126 pieces built.
Aero Commander 680PF
Version of the 680F with pressurized cabin , 26 units built.
Aero Commander 680FL Grand Commander
680F with an extended fuselage and a larger tail unit, 157 units built. Named Courser Commander after 1967 .
Aero Commander 680FL / P Grand Commander
Version of the 680FL with a pressurized cabin, 37 units built.
Aero Commander 680T Turbo Commander
680FL / P with Garrett TPE331-43 - turboprop engines built 56 pieces.
Aero Commander 680V Turbo Commander
680T with increased take-off mass and slightly improved loading capacity, 36 units built.
Aero Commander 680W Turbo II Commander
680V with a pointed nose, modified tail unit, a panorama and two small cabin windows and weather radar, 46 pieces built.
Rockwell Commander 681 Hawk
680W with improved pressurized cabin, air conditioning and nose, 43 pieces built.
Rockwell 681B Turbo Commander
Marketing term for economy version of the 681, 29 units built.
685 Rockwell Commander
Version of the 690 built from 1972 onwards, powered by two 435 hp Continental GTSIO 520k piston engines, 66 units built.
Commander 690
681 with new wing center section and new motors moved further outwards, two AirResearch TPE331-5-521 turboprops, 79 units built.
Commander 690A
690 with modified cabin design and increased pressurization, 245 units built.
Commander 690B
690A with improved sound insulation and internal toilet, 217 pieces built.
690C Jetprop840
690B with enlarged wingspan, wing fuel tanks and winglets, two 840 HP TPE331-5-254K turboprops, 136 pieces built.
690D Jetprop900
Similar to 690C with extended aft cab, improved pressurization and five square windows, 42 pieces built.
695 Jetprop 980
Similar to the 690C with 735 hp TPE331-10-501K engines, 84 built.
695A Jetprop 1000
690D with higher takeoff weight and more powerful TPE331-10-501K motors, 101 units built.
695B Jetprop 1000B
695A with minor changes, six built.
Aero Commander 720 AltiCruiser
Pressurized cabin version of the 680, 13 units built.
YL-26 → YU-9A
Aero Commander 520 tested by the US Army, three pieces built.
YL-26A
Aero Commander 560 tested by the US Air Force, one copy built.
L-26B → U-4A
Aero Commander 560A sold to the US Air Force, 14 units built.
L-26B → U-9B
Aero Commander 560A sold to the US Army, 1 piece built.
L-26C → U-4B
Aero Commander 680 Super sold to the US Air Force, 2 pieces built.
L-26C → U-9C
Aero Commander 680 Super sold to the US Army, 4 pieces built.
RL-26D → RU-9D
Commander 680 for the US Army with SLAR ( side view radar ), two pieces built.
NL-9D → NU-9D
One copy built

use

The versions used by the military were initially named L-26 in the system used by the US Air Force and US Army until 1962 . In the common designation system for aircraft of the US armed forces in force from 1962 , the former USAF aircraft were then designated as U-4 and the former US Army aircraft as U-9 .

An L-26C served Dwight Eisenhower as a presidential aircraft from 1956 to 1960, making it the smallest Air Force One . It was also the first with the typical blue and white paintwork. The Prime Minister of Australia also used this type of aircraft at times.

Military users

ArgentinaArgentina Argentina
BelgiumBelgium Belgium
BeninBenin Benin
Burkina FasoBurkina Faso Burkina Faso
Dominican RepublicDominican Republic Dominican Republic
HondurasHonduras Honduras
GreeceGreece Greece
  • air force
  • marine
GuatemalaGuatemala Guatemala
IndonesiaIndonesia Indonesia
  • air force
  • army
IranIran Iran
  • air force
  • army
  • marine
KenyaKenya Kenya
LebanonLebanon Lebanon
MexicoMexico Mexico
  • air force
  • marine
PakistanPakistan Pakistan
PeruPeru Peru
Korea SouthSouth Korea South Korea
Vietnam SudSouth Vietnam South Vietnam
  • air force
ThailandThailand Thailand
United StatesUnited States United States
UruguayUruguay Uruguay
  • air force

Civil users

GermanyGermany Germany
United StatesUnited States United States

Technical specifications

Parameter Data Rockwell Aero Commander 500S Data Rockwell Jetprop Commander 1000
span 14.95 m 15.89 m
length 11.22 m 13.10 m
height 4.56 m 4.56 m
payload 961 kg
Takeoff mass 3060 kg 5080 kg
Passengers 5 6-10
crew 1 1-2
Cruising speed 312 km / h 474 km / h
Top speed 346 km / h 571 km / h
Service ceiling 5,915 m 10,000 m
Range 1915 km 2430 km
Engines 2 × Lycoming IO-540 -E1B5 piston motors with 214 kW (290 PS) each 2 × Turboprop Garrett TPE331-10-501K with 610 kW (830 PS) each

Incidents

See also

Web links

Individual evidence

  1. To the renaming
  2. Michael Gasser: The drama about flight "Rheintal 102". In: Vorarlberger Nachrichten. February 15, 2014, accessed July 15, 2015 .