NATOPS Flashcards
T/O weight normal
164,000 lbs
T/O weight alternate
175,000 lbs
Landing weight recommended
142,000 lbs
Landing weight normal
164,000 lbs
Landing weight alternate
175,000 lbs
Fuel tank limits 1,4 2,3 ext aux
1,4 = 8310 2,3 = 7,650 Ext = 8,900 Aux = 5,810
Takeoff and Landing Fuel Management
- Max usable fuel weights in fuel weight limits
- # 1/#4 500-1000# more than #2/#3
- Main tanks are full, except for fuel used to taxi, t/o, and climb but not less than 7,060 in 1/4 and not less than 6,410 in 2/3 when ext contain usable fuel
- Fuel unbalance w/in limits
- refer to charts
Enroute fuel management
seeks to maximize the weight in the outboard fuel tanks as long as possible but does not take mission constraints into consideration while doing so. Improves wing-loading and efficiency during long transit legs; it also extends airframe service life, especially with medium to heavy cargo loads.
10% flaps
220 kias
20% flaps
210 kias
30% flaps
200 kias
40% flaps
190 kias
50% (takeoff/approach)
183 kias
60% flaps
165 kias
70% flaps
155 kias
80% flaps
150 kias
90% flaps
145 kias
100% flaps (landing)
145 kias
Landing gear extended
168 kias
Landing lights extended
250 kias
Cargo door open and locked; ramp up and locked
250 kias
Cargo door (all positions and motions)
250 kias
Ramp (all positions and motions)
250 kias
Paratroop air deflectors open
150 kias