ANNEX A TO BGA AMP LEAFLET 4-1

WEIGHING RECORD - SINGLE SEATERS AND SIDE-BY-SIDE TWO SEATERS

Glider Type:

BGA Cof No:

Serial No:

LEADING PARTICULARS EXTRACT

Datum Point : Levelling Means :

Fwd CofG Limit (Xfl) : Aft CofG Limit (Xal) : Pilot(s) CofG (Xpl) : Baggage CofG (Xb) :

mm aft. Max All Up Weight (Dry) (Wd) : mm aft. Max All Up Weight (Wet) (Ww) : mm fwd. Max Weight Non-Lift Parts (Wn) : mm aft. Max Baggage Weight (Wb) :

Kg Kg Kg Kg

EMPTY WEIGHT AND CofG POSITION

Weight on Front Support (Wf) = Weight on Rear Support (Wr) = Weight of Port Wing (Wp) = Weight of Starboard Wing (Ws) =

kg kg kg kg

Empty Glider Weight Weight Non-Lifting Parts

(We) = Wf + Wr = (Wnl) = We - Wp - Ws =

kg kg

Displacement of Front Support Displacement of Rear Support

(Xfs) = (Xrs) =

mm fwd (-ve if aft of datum) mm aft

Empty Glider CofG Displacement (Xe) = (Wf x Xfs) - (Wr x Xrs) We

=

= mm aft

MINIMUM AND MAXIMUM COCKPIT LOADS

Minimum Cockpit Load

CofG Based We(Xe - Xa1) + Wb(Xb - Xa1) (Xp1 + Xa1) (Xp1 + Xa1)

= = kg ( lb).

AMP 4-1A/Dec00

BGA AMP Part 4, Leaflet 4-1A, Page 1

Maximum Cockpit Load

a. CofG Based:

We(Xe - Xf1) + Wb(Xb - Xf1) (Xp1 + Xf1) (Xp1 + Xf1)

=

= kg

b. Max AUW Based:

Wd - We - Wb

=

= kg

c. Max Non-Lift Based:

Wn - Whl - Wb

=

= kg

d. Flight Manual Limitation:

= kg

The Max (Dry) Cockpit Weight is the LEAST value of a. to d:

= kg (

Maximum Total Loading - Wet

Total weight of pilot(s) plus water must not exceed:

Ww - We - Wb

=

kg

lb)

NOTES:

Date:

Name:

Signature:

BGA Insp Auth:

AMP 4-1A/Dec00

BGA AMP Part 4, Leaflet 4-1A, Page 2