Difference between revisions of "Piper PA-50 Cayuga"

From Shipbucket Wiki
Jump to: navigation, search
(Created page; Categorized page; Added infobox)
 
m
 
(4 intermediate revisions by the same user not shown)
Line 1: Line 1:
 
{|{{Infobox aircraft begin
 
{|{{Infobox aircraft begin
 
  |name= Piper PA-50 Cayuga
 
  |name= Piper PA-50 Cayuga
−
  |image=[[image:Piper PA-50R-300 Cayuga (Blank).png|300]]
+
  |image=[[image:Piper PA-50R-300 Cayuga (Blank).png|thumb]]
 
  |caption= Piper PA-50R-300
 
  |caption= Piper PA-50R-300
 
}}{{Infobox aircraft type
 
}}{{Infobox aircraft type
Line 14: Line 14:
 
  |primary users= {{wp|United States Army}}
 
  |primary users= {{wp|United States Army}}
 
  |more users = {{wp|Philippine Air Force}}, {{wp|Mexican Air Force}}
 
  |more users = {{wp|Philippine Air Force}}, {{wp|Mexican Air Force}}
−
  |produced= 1969-1972
+
  |produced= 1968-1972
−
  |number built= 5
+
  |number built= 37
 
  |developed from= {{wp|Piper PA-28 Cherokee|Piper PA-28R Arrow}}
 
  |developed from= {{wp|Piper PA-28 Cherokee|Piper PA-28R Arrow}}
 
  |variants with their own articles=   
 
  |variants with their own articles=   
Line 21: Line 21:
 
}}
 
}}
 
|}
 
|}
 +
The Piper PA-50 Cayuga was an American single-engined training monoplane designed by Piper for military and commercial markets.
 +
==Development==
 +
The PA-50 grew out of Piper’s exploration into two-seat trainers in the late-1950s and early-1960s that initially culminated in the PA-29 Papoose. The Papoose proved that the PA-28 airframe could be successfully adapted into a two-seat trainer, but the all-composite construction proved to be too expensive for serial production and Piper quietly discontinued the project. In 1965, company executives decided to restart design work on a similar trainer, this time intended for the military market. The US Air Force had just recently decided to retire the T-34 Mentor and Piper’s management saw an opening for a similar aircraft with the USAF and foreign T-34 operators. Desperate to avoid the skyrocketing costs that the PA-29 experienced, the new design was to be all-metal and retain as much of the existing PA-28 airframe as possible. The PA-28R-180 Arrow, which was also currently on the drawing board, was determined to be the perfect starting point for the new aircraft (soon designated PA-50).
 +
 +
==Design==
 +
Designers began by removing the four-place cabin and replacing it with a sliding bubble canopy seating student and instructor in a side-by-side configuration. The landing gear was strengthened to support repeated hard landings by new student pilots and the fuselage was reinforced to increase G limits to +6/-3. The 180 horsepower Lycoming IO-360-B1E engine from the Arrow was quickly identified as too weak and Piper chose to fit the 300 horsepower Lycoming IO-540-K1A5 engine from the PA-32-300 instead. This engine gave the PA-50 excellent performance for an aircraft its size and gave it speed comparable to that of the T-34 it was intended to replace.
 +
 +
==Operational History==
 +
The first PA-50 rolled out of Piper’s Lock Haven facility in April 1969 and took flight on 1 June. Test pilots reported excellent visibility and an aircraft that was both stable and responsive. Marketing tours began in the fall and both the USAF and USN tested the aircraft in early 1970. The USAF, however, was not interested in purchasing the design as the Cessna T-37B had already become their standard primary trainer and replaced the T-34. Piper was simply too late to the party. The US Navy was similarly uninterested, having decided to retain the T-34 and develop the turboprop-powered T-34C. This left Piper without obvious domestic operators and focus shifted to foreign markets. Orders finally came in the summer of 1970, with Mexico placing an initial order for 15 aircraft and the Philippines ordering 48 aircraft to replace their T-34s. The line at Lock Haven went into full swing in early 1971 and serial production aircraft began rolling off the line in the summer. The US Army approached Piper in August 1971 about purchasing a small handful of aircraft to provide fixed-wing training for their pilots, a role that was at the time being fulfilled by the USAF. An order was finalized in early September for five PA-50s, to be operated by the US Army Aviation Center at Fort Rucker.
 +
 +
The US Army and Mexican Air Force orders were complete by spring 1972, but the larger Filipino order was still underway in early June when disaster struck. Torrential rains from Hurricane Agnes caused massive flooding along the Susquehanna River which drowned Piper’s facility in over 16 feet of water and destroyed over 100 aircraft. Tooling for several aircraft was completely destroyed, including equipment for the PA-24 Comanche and the PA-50 Cayuga. Production never resumed, and the Philippine Air Force sold their incomplete order to civilian operators and smaller militaries including several African nations. The Mexican Air Force and US Army remained the only original military operators of the PA-50, though Mexico retired their aircraft by 1980 in favor of a larger order of SIAI-Marchetti SF.260s. The US Army flew the type well into the early 1990s, before they too divested their fleet. Only 37 PA-50s were ever built.
 +
 +
==Variants==
 +
* '''PA-50R-300''' – Production Version (37 built)
 +
* '''PA-50-235''' - Fixed-Gear Version for the civilian market (Never Built)
 +
* '''PA-50-301''' - Stretched version with tapered wing from PA-28R-201 (Never Built)
 +
 +
==Operators==
 +
;{{wp|United States}}
 +
* {{wp|United States Army}}
 +
[[image:Piper PA-50R-300 Cayuga (US Army).png]]
 +
;{{wp|Philippines}}
 +
* {{wp|Philippine Air Force}}
 +
[[image:Piper PA-50R-300 Cayuga (Philippines).png]]
 +
;{{wp|Mexico}}
 +
* {{wp|Mexican Air Force}}
 +
[[image:Piper PA-50R-300 Cayuga (Mexico).png]]
 +
;Various Civilian Operators
 +
[[image:Piper PA-50R-300 Cayuga (US Civilian).png]]
 +
[[image:Piper PA-50R-300 Cayuga (UK Civilian).png]]
 +
 +
==Specifications (PA-50R-300)==
 +
'''General Characteristics:'''
 +
<br>Crew: One
 +
<br>Capacity: One Passenger
 +
<br>Length: 7.5 meters
 +
<br>Wingspan: 9.2 meters
 +
<br>Height: 2.9 meters
 +
<br>Wing Area: 15 square meters
 +
<br>Airfoil: NACA 65sub2-415
 +
<br>Empty Weight: 1,605 lb
 +
<br>Gross Weight: 2,650 lb
 +
<br>Max Takeoff Weight: 2,650 lb
 +
<br>Powerplant: 1x Lycoming IO-540-K1A5 6-cylinder air-cooled horizontally-opposed piston engine, 300 hp
 +
<br>Propeller: 2-blade constant speed propeller
 +
 +
<br>'''Performance:'''
 +
<br>Never-Exceed Speed (Vne): 215 knots
 +
<br>Cruise Speed: 165 knots
 +
<br>Stall Speed, Landing Configuration (Vso): 55 knots
 +
<br>Range: 375 nmi
 +
<br>Service Ceiling: 15,200 ft
 +
<br>Rate of Climb: 1,230 ft/min
 +
 +
 +
==See also==
 +
'''Related Development'''
 +
* {{wp|Piper PA-28 Cherokee}}
 +
'''Similar Aircraft'''
 +
* {{wp|SIAI-Marchetti SF.260}}
 +
* {{wp|PZL M26 Iskierka}}
 +
 +
 +
[[Category:The Sprinklez]]
 +
[[Category:Alternate Universe drawings]]
 +
[[Category:United States]]
 +
[[Category:FD scale]]

Latest revision as of 03:50, 28 January 2024

Piper PA-50 Cayuga
Piper PA-50R-300 Cayuga (Blank).png
</div>
Piper PA-50R-300
Role Primary Trainer
National origin United States of America
Manufacturer Piper Aircraft
First flight 1 June 1969
Introduction 1971
Retired 1993 (US Army)
Status Limited service
Produced 1968-1972
Number built 37
Developed from Piper PA-28R Arrow

The Piper PA-50 Cayuga was an American single-engined training monoplane designed by Piper for military and commercial markets.

Development

The PA-50 grew out of Piper’s exploration into two-seat trainers in the late-1950s and early-1960s that initially culminated in the PA-29 Papoose. The Papoose proved that the PA-28 airframe could be successfully adapted into a two-seat trainer, but the all-composite construction proved to be too expensive for serial production and Piper quietly discontinued the project. In 1965, company executives decided to restart design work on a similar trainer, this time intended for the military market. The US Air Force had just recently decided to retire the T-34 Mentor and Piper’s management saw an opening for a similar aircraft with the USAF and foreign T-34 operators. Desperate to avoid the skyrocketing costs that the PA-29 experienced, the new design was to be all-metal and retain as much of the existing PA-28 airframe as possible. The PA-28R-180 Arrow, which was also currently on the drawing board, was determined to be the perfect starting point for the new aircraft (soon designated PA-50).

Design

Designers began by removing the four-place cabin and replacing it with a sliding bubble canopy seating student and instructor in a side-by-side configuration. The landing gear was strengthened to support repeated hard landings by new student pilots and the fuselage was reinforced to increase G limits to +6/-3. The 180 horsepower Lycoming IO-360-B1E engine from the Arrow was quickly identified as too weak and Piper chose to fit the 300 horsepower Lycoming IO-540-K1A5 engine from the PA-32-300 instead. This engine gave the PA-50 excellent performance for an aircraft its size and gave it speed comparable to that of the T-34 it was intended to replace.

Operational History

The first PA-50 rolled out of Piper’s Lock Haven facility in April 1969 and took flight on 1 June. Test pilots reported excellent visibility and an aircraft that was both stable and responsive. Marketing tours began in the fall and both the USAF and USN tested the aircraft in early 1970. The USAF, however, was not interested in purchasing the design as the Cessna T-37B had already become their standard primary trainer and replaced the T-34. Piper was simply too late to the party. The US Navy was similarly uninterested, having decided to retain the T-34 and develop the turboprop-powered T-34C. This left Piper without obvious domestic operators and focus shifted to foreign markets. Orders finally came in the summer of 1970, with Mexico placing an initial order for 15 aircraft and the Philippines ordering 48 aircraft to replace their T-34s. The line at Lock Haven went into full swing in early 1971 and serial production aircraft began rolling off the line in the summer. The US Army approached Piper in August 1971 about purchasing a small handful of aircraft to provide fixed-wing training for their pilots, a role that was at the time being fulfilled by the USAF. An order was finalized in early September for five PA-50s, to be operated by the US Army Aviation Center at Fort Rucker.

The US Army and Mexican Air Force orders were complete by spring 1972, but the larger Filipino order was still underway in early June when disaster struck. Torrential rains from Hurricane Agnes caused massive flooding along the Susquehanna River which drowned Piper’s facility in over 16 feet of water and destroyed over 100 aircraft. Tooling for several aircraft was completely destroyed, including equipment for the PA-24 Comanche and the PA-50 Cayuga. Production never resumed, and the Philippine Air Force sold their incomplete order to civilian operators and smaller militaries including several African nations. The Mexican Air Force and US Army remained the only original military operators of the PA-50, though Mexico retired their aircraft by 1980 in favor of a larger order of SIAI-Marchetti SF.260s. The US Army flew the type well into the early 1990s, before they too divested their fleet. Only 37 PA-50s were ever built.

Variants

  • PA-50R-300 – Production Version (37 built)
  • PA-50-235 - Fixed-Gear Version for the civilian market (Never Built)
  • PA-50-301 - Stretched version with tapered wing from PA-28R-201 (Never Built)

Operators

United States

Piper PA-50R-300 Cayuga (US Army).png

Philippines

Piper PA-50R-300 Cayuga (Philippines).png

Mexico

Piper PA-50R-300 Cayuga (Mexico).png

Various Civilian Operators

Piper PA-50R-300 Cayuga (US Civilian).png Piper PA-50R-300 Cayuga (UK Civilian).png

Specifications (PA-50R-300)

General Characteristics:
Crew: One
Capacity: One Passenger
Length: 7.5 meters
Wingspan: 9.2 meters
Height: 2.9 meters
Wing Area: 15 square meters
Airfoil: NACA 65sub2-415
Empty Weight: 1,605 lb
Gross Weight: 2,650 lb
Max Takeoff Weight: 2,650 lb
Powerplant: 1x Lycoming IO-540-K1A5 6-cylinder air-cooled horizontally-opposed piston engine, 300 hp
Propeller: 2-blade constant speed propeller


Performance:
Never-Exceed Speed (Vne): 215 knots
Cruise Speed: 165 knots
Stall Speed, Landing Configuration (Vso): 55 knots
Range: 375 nmi
Service Ceiling: 15,200 ft
Rate of Climb: 1,230 ft/min


See also

Related Development

Similar Aircraft

Retrieved from "http://shipbucket.com/wiki/index.php?title=Piper_PA-50_Cayuga&oldid=15284"