Consolidated PT-11
{{Infobox aircraft
|name = PT-11
|image = Consolidated Y1PT-11.jpg
|caption = Consolidated Y1PT-11
|type = Primary trainer
|manufacturer = Consolidated Aircraft Company, Fleet Aircraft
|designer =
|first_flight =
|introduction = 1931
|retired =
|status =
|primary_user = United States Army Air Corps
|more_users = United States Coast Guard
|produced =
|number_built = 41"U.S. Army Aircraft 1908-1946" by James C. Fahey, 1946, 64pp.{{Cite web|url=http://aerofiles.com/_fleet.html|title = Fleet}}
|variants =
}}
The Consolidated Model 21 was an American two-seat training aircraft built by the Consolidated Aircraft Company. It was used by the United States Army Air Corps with the designation PT-11 and the United States Coast Guard under the designation N4Y.
Design and development
The Model 21 was an aerodynamic cleaned up version of the Model 12/PT-3, one of the distinguishing features being curved instead of angular tail surfaces. The aircraft was a single-engined biplane with fixed tailwheel landing gear and accommodation for two in open cockpits.
Operational history
Designated the PT-11 by the United States Army Air Corps it progressed through a number of trial variants but was not built in large numbers. 11 Examples of the model 21-C were built in Canada as the 21-M for Mexico but none were built for local use.
Variants
;XPT-933
: (Model 21A). Prototype powered by {{convert|170|hp|kW|abbr=on}} Kinner engine, first flew February 1931.Wegg 1990, p. 64.
;YPT-11
:Evaluation aircraft for US Army based on the Model 21A with a {{convert|165|hp|kW|abbr=on}} Continental R-545-1 engine, four built.
;PT-11A
:One YPT-11 was re-engined with a {{convert|175|hp|kW|abbr=on}} Curtiss R-600-1 Challenger engine, originally as Y1PT-11A, later converted to PT-11C standard.
;Y1PT-11B
:One YPT-11 was re-engined with a {{convert|210|hp|kW|abbr=on}} Kinner YR-720-1 engine and designated Y1PT-11B. 5 production aircraft for US Army with another for the United States Coast Guard and designated N4Y-1.Wegg 1990, p. 65.
;PT-11C
:PT-11A re-engined with a {{convert|180|hp|kW|abbr=on}} Lycoming YR-680-1 engine. One or two converted for US Army, with 18 new-build aircraft for Colombia.Wegg 1990, pp. 64–65.
;PT-11D
:Production version with {{convert|220|hp|kW|abbr=on}} R-680-3 engine, originally designated Y1PT-11D. 21 new-built, plus five conversions from Y1PT11-Bs and two from Y1PT-11s.
;PT-12
:A version of the PT-11 with a 300hp R-985-1 engine and detailed changes, ten built later redesignated BT-7.
;Y1BT-6
:One YPT-11 was re-engined with a 300hp R-985-1
;BT-6
:Redesignation of Y1BT-6.
;BT-7
:PT-12 aircraft redesignated.
;XN4Y-1
:Evaluation aircraft for the United States Coast Guard, three built.
;N4Y-1
:One YPT-11B for the USCG, later modified to the same standard as the XN4Y-1
Operators
;{{USA}}
;{{COL}}
- Colombian Air Force (PT-11C).
;{{PAR}}
- Paraguayan Air Arm (Model 21-C).
;{{MEX}}
- Mexican Air Force (Model 21-M).
Specifications (PT-11D)
{{Aircraft specs
|prime units? = imp
|ref="The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)" Orbis Publishing
|crew= two
|length ft= 26
|length in= 11
|length m= 8.20
|span ft= 31
|span in= 7
|span m= 9.63
|height ft= 9
|height in= 8
|height m= 2.95
|wing area sqft= 280
|wing area sqm= 26.01
|empty weight lb= 1,918
|empty weight kg= 870
|max takeoff weight lb= 2,585
|max takeoff weight kg= 1173
|eng1 name= Lycoming R-680A
|eng1 type= radial piston
|eng1 number= 1
|eng1 hp= 200
|eng1 kw= 149
|max speed mph= 118
|max speed kmh= 190
|ceiling ft= 13,700
|ceiling m= 4175
}}
See also
References
{{commons category|Consolidated PT-11}}
{{reflist}}
- {{cite book |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|publisher= Orbis Publishing}}
- {{cite book|last=Wegg|first=John|title=General Dynamics Aircraft and their Predecessors|year=1990|publisher=Putnam Aeronautical Books|location=London|isbn=0-85177-833-X}}
{{Consolidated aircraft}}
{{USAF trainer aircraft|uncollapsed}}
{{USN trainer aircraft}}
{{Wright Field project numbers}}
Category:Single-engined tractor aircraft