1
1. Operating wt. = approx. 375m
2. Each pax = 241 lbs (73 pax = 17.6m)
3. Check winds valid for T/O time. If not valid, update and spin new times
4. T/O wt = ramp wt – 3000 lbs
5. Use overhead temp dev to find highest acceptable FL
BLOCK
1. Time from T/O to BDP
2. 10% of Cat 1 route, 1 hour max
3. Total of 1 & 2
4. Use overhead dest wt. Use time to most distant alternate if 2 are required. Add 8,000 lbs fuel if dest. Wx is vis only.
5. Use overhead alternate wt. Use 45 min at 10,000 ft unless alternate is unavail., located in Alaska, lat > 59 deg, remote or island dest. Then use 1+15 min at 20,000 ft.
6. 7,000 lbs, 2,000 for descent, 5,000 for app & landing
7a. Off course maneuvering = 600# /min for
climbout, 400# /min for cruise, 5,000#
for unreliable nav aids. Known holding
delays
7b. Tankered fuel for subsequent mission
segments. Hyd cooling if needed
8. Total 3 + 4 + 5 + 6 + 7a & 7b
9. STTO = 3,000 lbs or 120 lbs /min for a
Max of 5,000 lbs
10. Block 10 is required ramp, block 8 is required for flight.
11. Actual fuel on aircraft
12. 10 – 11 = 5,000 lbs normally. Not required to defuel for standard load.
13. Block 4 + 5 + 6. As technique write actual sum so FE can use on fuel log. If less than 25,000 lbs add difference to block 7b stored fuel.
Missions will normally be planned for a step-climb profile, choose the most fuel conservative profile to accomplish mission requirements.
Cruise Ceiling: Used to determine initial level off/highest acceptable FL, known as cruise-climb altitude (300 FPM rate of climb at NRT).
Cruise Speed: Normal cruise speed is 300 KCAS / 0.77 M, whichever is less.
Fuel Requirements: If decompression would cause descent to an altitude resulting in fuel consumption exceeding planned fuel, add fuel to recover at a suitable airfield from ETP at the appropriate altitude. This is not required if the aircraft can recover at a suitable airfield at FL 250 at LRC speed from ETP.
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