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AFI 11-2C-130v3 - BITS

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212 <strong>AFI</strong><strong>11</strong>-<strong>2C</strong>-130V3 23 APRIL 2012<br />

14.5.4.1. A multi-leg fuel plan becomes necessary when a mission includes multiple<br />

stops where fuel is unavailable. Use the following procedure for multi-leg fuel planning,<br />

assume a three leg mission with legs labeled 1, 2, and 3:<br />

14.5.4.1.1. Begin with the last leg (3) and fuel plan as normal to obtain required ramp<br />

fuel.<br />

14.5.4.1.2. Next, determine the fuel required for leg 2. Include the required ramp fuel<br />

from leg 3 as identified extra fuel for leg 2. Do not plan for contingency, reserve or<br />

alternate/missed approach fuel for leg 2 unless those totals exceed the required ramp<br />

fuel for leg 3. If this occurs, add the difference in the identified extra block for leg 2.<br />

Use 1,000 lbs. for approach and landing.<br />

14.5.4.1.3. Plan leg 1 using the same procedures you used for leg 2.<br />

14.5.4.2. Fuel requirements must be verified at each stopover airfield. Requirement must<br />

be recomputed whenever the planned burnoff changes; for example, enroute altitude<br />

changes, actual cargo/passenger load differs from the estimate, holding is accomplished,<br />

diversion to alternate is required, etc.<br />

14.5.4.3. Regardless of the number of mission segments involved, fuel planning is<br />

always accomplished by planning the last leg‗s requirements first. The remaining leg<br />

requirements are planned in the reverse order to be flown until the refueling airfield is<br />

reached.<br />

Table 14.1. Fuel Load Components.<br />

1. ENROUTE Fuel for flight time from departure to overhead destination or initial<br />

penetration fix at cruise altitude (including time for planned orbit, escort,<br />

search, recovery, appropriate climb, weather recon, etc. when applicable).<br />

2. RESERVE 45 minutes (2+00 hrs for remote destinations). Reserve fuel will be<br />

computed using consumption rates providing maximum endurance fuel flow<br />

at 10,000 MSL (20,000 MSL for remote destinations). For gross weight, use<br />

end cruise gross weight (ECGW) from section II of the AF Form 4<strong>11</strong>6. If<br />

an alternate is required, compute using weight at alternate destination.<br />

3. CONTINGENCY 15 minutes. Use same fuel flow as reserve fuel above. (Not required for<br />

4. ALTERNATE AND<br />

MISSED<br />

APPROACH<br />

local training missions)<br />

Alternate: Fuel for flight time from overhead destination or initial<br />

penetration fix to alternate, or most distant alternate when two are required.<br />

Compute at terminal fuel flow. Required whenever alternate must be filed.<br />

Missed Approach: 2,200 lbs. Required if destination is below ceiling<br />

minimums but above visibility minimums for planned destination approach.<br />

5. APPROACH/LANDING Approach: 1,000 lbs (2,000 lbs for high altitude approach). Entry always<br />

required.<br />

Minimum Landing Fuel: 4,000 lbs. Entry always required. This accounts<br />

for gauge error. Do not include this 4,000lbs of fuel in the reserve and<br />

6.<br />

IDENTIFIE<br />

D EXTRA<br />

STORED FUEL<br />

contingency fuel calculations.<br />

Ramp fuel for succeeding legs without refueling.<br />

THUNDERSTORM 1,500 lbs if forecast thunderstorms are scattered or numerous along the route<br />

AVOIDANCE of flight. Will be based on the DD Form 175-1 or equivalent.<br />

ICING 1,000 lbs if route of flight has forecast or known icing conditions. Will be<br />

based on the DD Form 175-1 or equivalent.

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