Piper J-5: Difference between revisions

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{|{{Infobox Aircraft Begin
{|{{Infobox Aircraft Begin
|name= J-5
|name= J-5 Cub Cruiser
|image=File:G-BTKA (19839711909).jpg
|image=Piper J-5AX O-M category C-GZHU 01.JPG
|caption=
|caption=Piper J-5
}}{{Infobox Aircraft Type
}}{{Infobox Aircraft Type
|type=Multipurpose light civil aircraft
|type=Multipurpose light civil aircraft
Line 12: Line 12:
|produced=1940-1946
|produced=1940-1946
|number built=1,507
|number built=1,507
|unit cost={{AircraftCost|USA|1798|year=1940|ref=<ref>{{cite magazine|title=Piper Cub: 3-place cruiser|magazine=[[Aviation Week & Space Technology|Aviation]]|date=January 1940|volume=39|issue=1|page=54|url=http://archive.aviationweek.com/issue/19400101#!&pid=54|url-access=registration }}</ref>}}
|unit cost=[[United States dollar|US$]]1,995 (1947)
|variants with their own articles= [[Piper J-3]] <br />[[Piper PA-12]]
|developed from=[[Piper J-3 Cub]]
|variants with their own articles= [[Piper PA-12]]
}}
}}
|}
|}
The '''Piper J-5 'Cub Cruiser'''' was a larger, more powerful version of the basic [[Piper J-3|Piper J-3 Cub]]. It was designed just two years after the J-3 Cub, and differed by having a wider fuselage with the pilot sitting in the front seat and two passengers sitting in the rear seat. Equipped with a 75-hp [[Continental engine]] the plane's cruising speed was 75 mph. Though officially a three-seater, it would be more accurately described as a "two-and-a-half-seater", as two adults would find themselves quite cramped in wider rear seat. The Cruiser sold for $1,995 when it was first designed.{{Citation needed|date=June 2012}}


The '''Piper J-5 Cub Cruiser''' was a larger, more powerful version of the basic [[Piper J-3 Cub]]. It was designed just two years after the J-3 Cub, and differed by having a wider fuselage with the pilot sitting in the front seat and two passengers sitting in the rear seat. Equipped with a 75-hp [[Continental engine]] the plane's cruising speed was 75&nbsp;mph. Though officially a three-seater, it would be more accurately described as a "two-and-a-half-seater", as two adults would find themselves quite cramped in the wider rear seat. The Cruiser sold for $1,798 when it was first designed.
Production of the three models of the J- (-A, -B, -C), fall into two categories that differ considerably. The obvious difference can be seen in the landing gear. Early versions, of which 783 were built between 1940 and early 1942, have external bungee's. Those built from 1944 to 1946 included design changes developed for the United States Navy HE-1 flying ambulance, and these models have internal bungees. Currently over 500 J-5s remain on the FAA registry.{{Citation needed|date=June 2012}}


Production of the three models of the J-5 (-A, -B, -C), fall into two categories that differ considerably. The obvious difference can be seen in the landing gear. Early versions, of which 783 were built between 1940 and early 1942, have external bungees. Those built from 1944 to 1946 included design changes developed for the United States Navy HE-1 flying ambulance, and these models have internal bungees. In August 2018, 327 J-5s remained on the [[Federal Aviation Administration]] registry.<ref>{{cite web |url=http://registry.faa.gov/aircraftinquiry/AcftRef_Results.aspx?Mfrtxt=PIPER&Modeltxt=J-5&PageNo=1 |title=FAA Registry : Piper J-5 |work=[[Federal Aviation Administration]] |date=21 August 2018 |access-date=21 August 2018 |archive-date=22 August 2018 |archive-url=https://web.archive.org/web/20180822150016/http://registry.faa.gov/aircraftinquiry/AcftRef_Results.aspx?Mfrtxt=PIPER&Modeltxt=J-5&PageNo=1 |url-status=dead }}.</ref>
==History==
[[Image:Piper AE-1 N203SA 30274 KEM 09.05.09R edited-3.jpg|thumb|right|Ex US Navy Piper AE-1 showing the hinged rear decking for access for ambulance work]]
Throughout World War II, Piper modified the basic structure of the '''J-5A'''. The '''J-5B''' had a 75 h.p. [[Lycoming O-145|Lycoming GO-145-C2]] engine. The later '''J-5C''' also built as the '''HE-1''' (later '''AE-1''') ambulance for the U.S. Navy with rear hinged fuselage decking, used the fully cowled 100 h.p. [[Lycoming O-235|Lycoming Military O-235-2 or Civilian O-235-B]] engine with an electrical system, and redesigned landing gear.<ref name="Peperell1987p43">Peperell, 1987, p. 43</ref> <ref name=FAA ATC 725>
[[Image:Piper J-5A Cub Cruiser N41236 N.Perry FL 03.87.jpg|thumb|right|Piper J-5A Cub Cruiser with wing endplates and banner-towing gear at North Perry airport, Florida, in March 1987]]


==Design and development==
After the war, Piper dropped the J- designation system in exchange for the PA- system, and the J-5C became the [[Piper PA-12|PA-12 "Super Cruiser"]]. The Super Cruiser was more popular than the basic J-5A, with 3,759 being built.<ref name="Simpson2005p430">Simpson, 2005, p. 430</ref>
Throughout World War II, Piper modified the basic structure of the '''J-5A'''. The '''J-5B''' had a 75 h.p. [[Lycoming O-145|Lycoming GO-145-C2]] engine. The later '''J-5C''' also built as the '''HE-1''' (later '''AE-1''') ambulance for the U.S. Navy with rear hinged fuselage decking, used the fully cowled 100 h.p. [[Lycoming O-235|Lycoming Military O-235-2 or Civilian O-235-B]] engine with an electrical system, and redesigned landing gear.<ref name="Peperell1987p43">Peperell, 1987, p. 43, FAA ATC 725</ref>


Piper also produced a four-seat variant of the Super Cruiser with a 115-hp engine. It was designated the [[PA-14 Family Cruiser]]. It was the least successful of the three Cruiser designs in terms of aircraft sold, with 238 being built in 1948/49,<ref name="Simpson2005p430" /> and only about one hundred remain in existence.
After the war, Piper dropped the J- designation system in exchange for the PA- system, and the J-5C became the [[Piper PA-12|PA-12 "Super Cruiser"]]. The Super Cruiser was more popular than the basic J-5A, with 3,759 being built.<ref name="Simpson2005p430">Simpson, 2005, p. 430</ref>

Piper also produced a four-seat variant of the Super Cruiser with a 115-hp engine. It was designated the [[PA-14 Family Cruiser]]. It was the least successful of the three Cruiser designs in terms of aircraft sold, with 238 being built in 1948/49,<ref name="Simpson2005p430" /> and only about one hundred remain in existence.{{cn|date=November 2022}}


==Variants==
==Variants==
;J-5
;J-5
:75hp Continental A-75-8 powered variant.
:75hp Continental A-75-8 powered variant.
[[File:Piper J-5A Cub Cruiser N41236 N.Perry FL 03.87.jpg|thumb|right|Piper J-5A Cub Cruiser with wing endplates and banner-towing gear at North Perry airport, Florida, in March 1987]]
;J-5A
;J-5A
:Continental A-75-9 powered variant.
:Continental A-75-9 powered variant.
;J-5A-80
;J-5A-80
:J-5As modified with a 80hp Continental A-80-8 engine.
:J-5As modified with an 80hp Continental A-80-8 engine.
;J-5B
;J-5B
:75hp Lycoming O-145-B powered variant.
:75hp Lycoming O-145-B powered variant.
;J-5C
;J-5C
:100hp Lycoming O-235-C powered variant.
:100hp Lycoming O-235-B powered variant.
;J-5CA
;J-5CA
:Prototype ambulance variant produced as the HE-1 for the United States Navy.
:Prototype ambulance variant produced as the HE-1 for the United States Navy.
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;YL-14
;YL-14
:Prototype liaison aircraft for the United States Army Air Force, five built.
:Prototype liaison aircraft for the United States Army Air Force, five built.

[[File:Piper L-14 Army Cruiser. Festival Aéreo Internacional De Gijón. Gijón 2016. (28639109032).jpg|thumb|A restored Piper L-14 over the [[Gijón]] International Air Festival, 2016]]
;L-14
;L-14
:Production variant of the YL-14, order for 845 cancelled and nine under construction completed for the civilian market.
:Production variant of the YL-14, order for 845 cancelled and nine under construction completed for the civilian market.
Line 64: Line 67:


==Specifications (J-5)==
==Specifications (J-5)==
[[File:Piper L-14 3-view line drawing.png|frameless|right|3-view line drawing of the Piper L-14]]

{{Aircraft specs
{{Aircraft specs
|ref=Peperell, 1987, p. 43
|ref=Peperell, 1987, p. 43
Line 173: Line 178:
|lists=
|lists=
|see also=
|see also=

}}
}}

==References==
==References==
;Notes
===Notes===
{{reflist}}
{{reflist}}

;Bibliography
===Bibliography===
{{refbegin}}
*{{cite book|last=Peperell|first=Roger|title=Piper Aircraft and their forerunners|year=1987|publisher=Air-Britain (Historians) Ltd|isbn=0-85130-149-5}}
*{{cite book|last=Peperell|first=Roger|title=Piper Aircraft and their forerunners|year=1987|publisher=Air-Britain (Historians) Ltd|isbn=0-85130-149-5}}
*{{cite book|last=Simpson|first=Rod|title=Airlife's World Aircraft|year=2001|publisher=Airlife Publishing Ltd|isbn=1-84037-115-3}}
*{{cite book|last=Simpson|first=Rod|title=Airlife's World Aircraft|year=2001|publisher=Airlife Publishing Ltd|isbn=1-84037-115-3}}
{{refend}}


==External links==
==External links==
{{commonscat|Piper J-5}}
{{commons category|Piper J-5}}
*[http://www.a2oxford.info/pages/spain/piperl14/ Detailed photos - Piper L-14 Army Cruiser]
*[https://web.archive.org/web/20110719103124/http://www.a2oxford.info/pages/spain/piperl14/ Detailed photos - Piper L-14 Army Cruiser]


{{Piper aircraft}}
{{Piper aircraft}}
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{{USAF liaison aircraft}}
{{USAF liaison aircraft}}
{{USAF transports}}
{{USAF transports}}
{{Aircraft manufactured in Canada}}
{{Aviation lists}}


[[Category:United States civil utility aircraft 1940–1949]]
[[Category:1930s United States civil utility aircraft]]
[[Category:High-wing aircraft]]
[[Category:High-wing aircraft]]
[[Category:Single-engined tractor aircraft]]
[[Category:Single-engined tractor aircraft]]
[[Category:Piper aircraft|J-5]]
[[Category:Piper aircraft|J-5]]
[[Category:Aircraft first flown in 1939]]

Latest revision as of 02:58, 16 November 2023

J-5 Cub Cruiser
Piper J-5
Role Multipurpose light civil aircraft
Manufacturer Piper Aircraft
First flight July 1939
Produced 1940-1946
Number built 1,507
Developed from Piper J-3 Cub
Variants Piper PA-12

The Piper J-5 Cub Cruiser was a larger, more powerful version of the basic Piper J-3 Cub. It was designed just two years after the J-3 Cub, and differed by having a wider fuselage with the pilot sitting in the front seat and two passengers sitting in the rear seat. Equipped with a 75-hp Continental engine the plane's cruising speed was 75 mph. Though officially a three-seater, it would be more accurately described as a "two-and-a-half-seater", as two adults would find themselves quite cramped in the wider rear seat. The Cruiser sold for $1,798 when it was first designed.

Production of the three models of the J-5 (-A, -B, -C), fall into two categories that differ considerably. The obvious difference can be seen in the landing gear. Early versions, of which 783 were built between 1940 and early 1942, have external bungees. Those built from 1944 to 1946 included design changes developed for the United States Navy HE-1 flying ambulance, and these models have internal bungees. In August 2018, 327 J-5s remained on the Federal Aviation Administration registry.[1]

Design and development[edit]

Throughout World War II, Piper modified the basic structure of the J-5A. The J-5B had a 75 h.p. Lycoming GO-145-C2 engine. The later J-5C also built as the HE-1 (later AE-1) ambulance for the U.S. Navy with rear hinged fuselage decking, used the fully cowled 100 h.p. Lycoming Military O-235-2 or Civilian O-235-B engine with an electrical system, and redesigned landing gear.[2]

After the war, Piper dropped the J- designation system in exchange for the PA- system, and the J-5C became the PA-12 "Super Cruiser". The Super Cruiser was more popular than the basic J-5A, with 3,759 being built.[3]

Piper also produced a four-seat variant of the Super Cruiser with a 115-hp engine. It was designated the PA-14 Family Cruiser. It was the least successful of the three Cruiser designs in terms of aircraft sold, with 238 being built in 1948/49,[3] and only about one hundred remain in existence.[citation needed]

Variants[edit]

J-5
75hp Continental A-75-8 powered variant.
Piper J-5A Cub Cruiser with wing endplates and banner-towing gear at North Perry airport, Florida, in March 1987
J-5A
Continental A-75-9 powered variant.
J-5A-80
J-5As modified with an 80hp Continental A-80-8 engine.
J-5B
75hp Lycoming O-145-B powered variant.
J-5C
100hp Lycoming O-235-B powered variant.
J-5CA
Prototype ambulance variant produced as the HE-1 for the United States Navy.
J-5CO
Prototype observation variant, later modified as the L-4X to be a prototype for the military L-14 version.
J-5D
1946 built aircraft with a 125hp Lycoming engine.

Military designations[edit]

YL-14
Prototype liaison aircraft for the United States Army Air Force, five built.
A restored Piper L-14 over the Gijón International Air Festival, 2016
L-14
Production variant of the YL-14, order for 845 cancelled and nine under construction completed for the civilian market.
AE-1
HE-1 redesignated in 1943 in the Ambulance category.
HE-1
Hospital variant for the United States Navy with hinged fuselage top for stretcher access, 100 built later re-designated AE-1.
UC-83
Four J-5A aircraft impressed into military service in Panama later becoming the L-4F.
L-4F
Four UC-83s re-designated and an additional 39 J-5As impressed.
L-4G
J-5B impressed into military service, 34 aircraft.

Specifications (J-5)[edit]

3-view line drawing of the Piper L-14
3-view line drawing of the Piper L-14

Data from Peperell, 1987, p. 43

General characteristics

  • Crew: one
  • Capacity: two passengers
  • Length: 22 ft 6 in (6.86 m)
  • Wingspan: 35 ft 6 in (10.82 m)
  • Height: 6 ft 10 in (2.08 m)
  • Empty weight: 830 lb (376 kg)
  • Gross weight: 1,450 lb (658 kg)
  • Powerplant: 1 × Lycoming GO-145-C2 four cylinder, horizontally-opposed aircraft engine, 75 hp (56 kW)
  • Propellers: 2-bladed wooden

Performance

  • Maximum speed: 96 mph (154 km/h, 83 kn)
  • Cruise speed: 86 mph (138 km/h, 75 kn)
  • Stall speed: 42 mph (68 km/h, 36 kn)
  • Range: 430 mi (690 km, 370 nmi)
  • Service ceiling: 10,200 ft (3,100 m)
  • Rate of climb: 460 ft/min (2.3 m/s)

See also[edit]

Related development

References[edit]

Notes[edit]

  1. ^ "FAA Registry : Piper J-5". Federal Aviation Administration. 21 August 2018. Archived from the original on 22 August 2018. Retrieved 21 August 2018..
  2. ^ Peperell, 1987, p. 43, FAA ATC 725
  3. ^ a b Simpson, 2005, p. 430

Bibliography[edit]

  • Peperell, Roger (1987). Piper Aircraft and their forerunners. Air-Britain (Historians) Ltd. ISBN 0-85130-149-5.
  • Simpson, Rod (2001). Airlife's World Aircraft. Airlife Publishing Ltd. ISBN 1-84037-115-3.

External links[edit]