Limitations - LIM-11 Weight and Centre of Gravity Limits

Question 1

002- Centre Of Gravity Limits

LIM-11

Answer 1

• CG Limits are Given in % of the Reference Chord

Length Aft of the Leading Edge.

• The CG Must Always be Within Nominal Reference Chord

Length and the Reference Chord Aft of the Aircraft Nose

Regardless of Fuel Load.

Question 2

003- Weight Limitations

B-HTJ, B-HTK

LIM-11

Answer 2

Maximum Taxi Weight — 89 400 kg

Maximum TakeOff Weight (Brake Release) — 89 000 kg Maximum Landing Weight — 77 800 kg

Maximum Zero Fuel Weight — 73 800 kg

Minimum Weight — 47 500 kg

Question 3

004- Weight Limitations

B-HSQ to B-HSU

LIM-11

Answer 3

Maximum Taxi Weight — 77 400 kg

Maximum TakeOff Weight (Brake Release) — 77 000 kg

Maximum Landing Weight — 66 000 kg

Maximum Zero Fuel Weight — 62 500 kg

Minimum Weight — 37 230

Question 4

005- Weight Limitations

B-HSD to B-HSP

LIM-11

Answer 4

Maximum Taxi Weight — 75 900 kg

Maximum TakeOff Weight (Brake Release) — 75 500 kg

Maximum Landing Weight — 64 500 kg

Maximum Zero Fuel Weight — 61 000 kg

Minimum Weight — 37 230 kg

Question 5

006- Weight Limitations

B-HTD to B-HTI

LIM-11

Answer 5

Maximum Taxi Weight — 89 400 kg

Maximum TakeOff Weight (Brake Release) — 89 000 kg

Maximum Landing Weight — 75 500 kg

Maximum Zero Fuel Weight — 71 500 kg

Minimum Weight — 47 500 kg