t-39 - Chief of Naval Air Training
t-39 - Chief of Naval Air Training
t-39 - Chief of Naval Air Training
Create successful ePaper yourself
Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.
T-<strong>39</strong> FLIGHT PREPARATION STUDENT GUIDE<br />
2-14<br />
60 2 gauges = 1800<br />
30 1 gauge = 900<br />
45 1 gauge + 1/2 other gauge = 1350<br />
20 2/3 <strong>of</strong> 1 gauge = 600<br />
15 1/2 <strong>of</strong> 1 gauge = 450<br />
10 1/3 <strong>of</strong> 1 gauge = 300<br />
5 1/2 <strong>of</strong> 1 gauge divided by 3 = 150<br />
1 1800/60 = 30.0<br />
Wings Level: 106 min = 60 + 45 + 1 = both gauges + 1 gauge + 1/2 <strong>of</strong> 1 gauge + 1<br />
= 1800 + 900 + 450 + 30<br />
6040 # - 3180 # = 2860# at the IAF<br />
(4) Pounds per nautical mile method<br />
Determine fuel flow in terms <strong>of</strong> pounds per NM by dividing fuel flow (#/hr) by<br />
estimated ground speed to IAF (NM/hr). Multiply the result by the distance remaining to<br />
IAF.<br />
1800 #/hr ÷ 420 NM/hr (estimated) = 4.3 #/NM<br />
Wings level: 742 nm x<br />
6040 – 3180 = 2860 # at IAF<br />
COMPARISONS:<br />
Method Advantage Disadvantage<br />
Pounds Per Minute (1). Once fuel flow/min is<br />
determined, multiply by time<br />
remaining.<br />
(2). In-flight re-planning<br />
Matrix (1). Uses addition instead <strong>of</strong><br />
multiplication<br />
(2). Accurate<br />
(1). Requires accurate ETEs;<br />
preflight winds must be<br />
reasonably accurate (+ 10-20<br />
kts and 10-20 o )<br />
(2). Must recompute when<br />
fuel flow changes<br />
(3). Math intensive<br />
(1). Requires new matrix if<br />
fuel flow changes.<br />
(2). Also dependent on<br />
accurate ETEs