03.03.2013 Views

t-39 - Chief of Naval Air Training

t-39 - Chief of Naval Air Training

t-39 - Chief of Naval Air Training

SHOW MORE
SHOW LESS

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

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!