Pilatus B-4
{{Infobox aircraft
| name=B4-PC11
| image=Pilatus B4-PC11 AF D-3993.jpg
| caption=
| type=Club-class glider
| national_origin=Switzerland
| manufacturer=Pilatus
| designer=Ingo Herbst, Manfred Küppers and Rudolf Reinke
| first_flight=7 November 1966
| introduction=
| retired=
| status=
| primary_user=
| number_built=322
| developed_from=
| variants=
}}
The Pilatus B4-PC11 (also known as the PC-11 in the Pilatus numbering sequence) is an all-metal intermediate glider built by Pilatus Aircraft of Switzerland.[https://sagach.ch/pilatus-b4-pc11/]Good 2016 description of B-4 by Swiss Aerobatic Gliding Association 9 April 2025
The B4-PC11 is designed to Standard Class specifications, meaning that it has a 15-metre wingspan and no wing flaps. Air brakes are provided on the top surface of each wing for glidepath control. Construction is aluminium, with foam ribs in the mainplane, fin and tailplane.
Development
The design of this glider originated in the 1960s, when the company Firma Rheintalwerke G. Basten [https://flickr.com/photos/vlk77/albums/72177720316670870]D-7201 photo 9 April 2025(from which the "B" in the original designation is derived) manufactured the first two prototypes. The designers were Ingo Herbst, Manfred Küppers and Rudolf Reinke. The first flight of the first prototype took place on 7 November 1966. However, no series production was started.
In 1972 Pilatus bought the manufacturing licence for the B-4 and renamed it the B4-PC11. In the spring of the same year the first production example (numbered HB-1100) made its first flight.
A total of 322 B4-PC11s of all versions were built by Pilatus by 1980, when the license to manufacture the craft was sold to Nippi Corporation of Japan, who built only 13 gliders, plus one two-seater prototype designated the Nippi B4T.[https://www.nippi.co.jp/jp/nippi_history.html] B-4 and B4T in History of Nippi Corporation (in Japanese: Click 1980 icon then find the photos under 1980 and 1983) 9 April 2025
Subsequently, in 1994, EWMS Technomanagement GmbH, which was founded in 1994 at Fribourg, Switzerland and was deregistered in 2024,[https://business-monitor.ch/en/companies/185887-ewms-technomanagement-gmbh-in-liquidation] business-monitor [https://www.northdata.com/EWMS%20Technomanagement%20GmbH,%20Oberschrot/CHE-107.579.211] [https://www.yelp.com/biz/ewms-technomanagement-leibnitz] 9 April 2025 bought the rights to produce and service the B4-PC11. This company also specialized in renovating and upgrading older B4-PC11 craft. In addition, it manufactured a motorized B4-PC11.
Variants
;B4-PC11: Permitted to fly a number of aerobatic manoeuvres, it was not permitted to do inverted loops or flick/snap/quick maneuvers. The B4-PC11 was available with either fixed or retractable landing gear.
;B4-PC11A: developed to perform inverted loops and was also able to handle higher g-forces.
;B4-PC11AF: File:CC-K17W (pilatus B4).jpgreleased in 1975, with full aerobatic capabilities. Nippi Corporation in Japan produced 13 pieces with Japanese Type Certificate Nippi-Pilatus B4-PC11AF (1978-1994). Then the rights were transferred to EWMS Technomanagement.
; Nippi B4TTeikyo Univ.: [https://www.teikyo.jp/utsunomiya/public_relations/pdf/t_kouku.pdf], Photo of B4T. 9 April 2025: One prototype tandem was made by Nippi in 1983.
;Lynch B4M1: a motor glider conversion in Australia by John F. Lynch, powered by a {{convert|17.9|kW|hp|abbr=on}} König SC 430 engine.{{cite book |title=Jane's All the World's Aircraft 1987–88 |year=1987 |publisher=Jane's Information Group |location=London |isbn=9780710608505 |editor=John W.R. Taylor |url-access=registration |url=https://archive.org/details/janesallworldsai0000unse }}
The changes in construction from B4-PC11 through A and AF variants were to add extra ribs through the fuselage section (increasing torsional rigidity, only AF variant), and to modify the control column stops and shorten the rudder, giving greater control surface deflection.
Specifications
{{Aircraft specs
|ref=
|prime units?=met
|genhide=
|crew=one
|length m=6.57
|span m=15
|height m=1.57
|wing area sqm=14
|aspect ratio=16
|airfoil=NACA 64(3)-618
|empty weight kg=230
|gross weight kg=350
|more general=
|never exceed speed kmh=240
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|g limits=
;PC-11:+5.3 -3
;PC-11A:+6.5 -4
;PC-11AF:+7 -5
|glide ratio=35:1 (Measurements performed by Idaflieg suggest 30)
|sink rate ms=0.63
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|more performance=
|avionics=
}}
See also
{{aircontent
|see also=
|related=
|similar aircraft=
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References
{{Commons category|Pilatus PC-11}}
{{reflist}}
- Hardy, M. Gliders & Sailplanes of the World. Ian Allan, 1982
{{Pilatus aircraft}}
Category:1960s Swiss sailplanes