BGA glider data sheet - Pegasus - Centrair 101 & 101A

Data source: Manufacturers‟ Handbook Date:1987

Manufacturer: Centrair

e mail: sncentrair@aol.com

UK Agent:

Web site:

Phone:

Fax:

Link to mandatory mods:

Weighing Data:

Kg Pounds

Max weight (dry) no tanks in wings 363 800

BGA concession non-aerobatic max weight (dry) without tanks [+3%]

374

Max weight dry with tanks in wings 368

BGA concession non-aerobatic

379

max weight (dry) with tanks [+3%]

Max weight with water

455

Max weight of non lifting 235 components (everything except wings)

824
811 836
1003 518

BGA concession non-aerobatic max weight of non lifting components [+5%] Max pilot weight (seat load)

247 110

mm

Forward C of G limit (aft of datum) 230

Aft C of G limit (aft of datum)

375

Pilot position (forward of datum) 650

544
242 Inches 9.06 14.76 25.59

Control deflections in degrees

Up Down Distance - Max

hinge to

free

measuring point

play

Ailerons 22 ±2

14 ±2

Elevator 22 ±3.5
Rudder Left 30±3

18 ±2
Right 30±3

Rudder Ailerons Elevator

Controls mass & moment limits

Mass Kg

Balance KgCm

Longitudinal datum: Wing root LE (not the fairing).

Horizontal datum: Rear fuselage top 1000:45 tail down

Maximum speeds

Kph Knots

Kph Knots

VNE

250 135

Aerotow

170 92

Rough air *

170* 92*

Winch / auto tow 120 65

Manoeuvre

170 92

U/C down

163 88

*Serial Nos 101001 to 101039 plus 101041, which have not had Centrair Major Mod 101-02, ( DGAC AD 93-145(A)) incorporated, have Vra, decreased to 163kph / 88kt.

Max winch weak link: 600 Kg [Blue]

Tyre pressure:2.6 - 3.4 Bars

Semi aerobatic. Cloud flying permitted.

Notes: -

Each 1Kg lead weight in the nose reduces the min pilot weight by 2 Kg.

Span 15 meters

This sheet compiled by: Tim Macfadyen

Last update: 4 Nov 2007 (Speeds corrected)

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