BGA glider data sheet - Pilatus B4-PC11 (& -A & -AF) Data source: Manufacturer’s Manual Date of issue: Dec 1974 Manufacturer: Pilatus Aircraft ltd, Stans, Switzerland. Manufactured under licence by Nippy in Japan since 1978 as the NP-100 Albatross. Weighing Data: Control deflections in mm Kg Pounds Up Down Measuring point Max weight 350 772 BGA concession non-aerobatic max weight [+3%] Max pilot weight (seat load) 360 795 114 252 mm Inches Forward C of G limit (aft of datum) 280 Aft C of G limit (aft of datum) 420 Pilot position (forward of datum) 610 Min weight pilot sat fully forward Pilot position (forward of datum) 531 Max weight pilot sat fully back 11.0 16.5 24 20.9 Ailerons 120 ± 5 58 ± 5 TE inboard end Elevator 100 ± 5 70 ± 5 TE centre PC11 Elevator 100 ± 5 85 ± 5 TE centre PC11A & AF Rudder Left & right TE bottom 230 ± 10 Airbrakes. 7.25 to 8.25 pounds force required to unlock the mechanism on each wing. Longitudinal datum: Wing root LE Horizontal datum: Rear fuselage top 1000:80 tail down The fixed main wheel is 147mm (5.79”) aft of datum. Distance between wheels is 3368mm (132.6”). The retractable main wheel is 164mm (6.46”) aft of datum. Distance between wheels is 3351mm (131.9”). Maximum speeds Knots Kph Knots Kph VNE 130 240 Aerotow 88 163 Rough air 88 163 Winch / auto tow 70 130 Manoeuvre 88 163 Airbrakes open 130 240 Max winch weak link: 550 kg (Tost white) BGA concession 600 Kg (Tost blue) Tyre pressure: Main 27 psi (1.9 bar) Tail 25 psi (2.5 bar) Pilatus B4-PC11- Semi aerobatic, cloud flying permitted. Pilatus B4-PC11-A - Fully aerobatic (+ 7.00, -4.79 g). Cleared for inverted flying, rolling manoeuvres and outside loops. Structurally as B4-PC11 but with toe straps, 5-point harness and increase down elevator travel. Pilatus B4-PC11-AF - Fully aerobatic. Cleared as “A” model and for flick manoeuvres. As B4-PC11-A model but with rear fuselage strengthening to cater for flick manoeuvres. Strengthening may be factory fitted internally or external, fitted as a modification. Span 15 meters This sheet compiled by: Tim Macfadyen Last updated 3 Aug 2008 Distances from wheel to datum and pilot positions corrected as per Manual revisions 01473 & 01574E Page 180 of 227