t-39 - Chief of Naval Air Training

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T-39 FLIGHT PREPARATION STUDENT GUIDE G-10 THIS PAGE INTENTIONALLY LEFT BLANK
APPENDIX H FLIGHT PLANNING DATA T-39 NORMAL THRUST CLIMB TWO ENGINES T-39 FUEL FLOW TWO ENGINES ALT TAS PPH SL 300 3000 10,000' 300 2400 15,000' 300 2200 360 2300 20,000' 360 2000 23,000' 360 1900 390 2100 420 2200 25,000' 360 1800 390 1950 420 2100 27,000' 360 1750 390 1850 420 2000 29,000' 360 1650 420 1900 31,000' 360 1500 390 1650 420 1800 33,000 420 1750 35,000' 390 1550 420 1650 37,000' 390 1500 420 1600 39,000' 390 1450 420 1550 41,000' 390 1350 420 1450 43,000' 420 1300 45,000' 420 1200 ALT TIME FUEL DIST (1000's) (mins) (lbs.) (nm) 10 3 200 12 15 5 350 22 20 7 430 32 21 8 480 38 23 9 500 40 25 10 600 48 27 12 650 57 30 13 780 72 33 16 800 80 35 18 920 102 37 20 1000 118 39 26 1150 147 41 31 1500 233 43 37 1680 265 45 44 1800 305 1. START/TAXI/TAKEOFF CONSUMES 400# (JP-5) AND IS NOT INCLUDED IN ABOVE FIGURES. 2. FUEL REQUIRED FOR APPROACH: 400#. 3. RESERVE FUEL COMPUTED AT 175 KIAS, 10K MSL, 1800 PPH FOR A 14,000# AIRCRAFT IS 600#. 4. TOTAL FUEL: 7200# (JP-5), 6900# (JP-4) 3+10 FOR VNAV AND 4+00 FOR INAV. 5. DESCENT: ALLOW 30#, 2 MINUTES, AND 10 NM PER 5000 FEET OF ALTITUDE. 6. ENROUTE BETWEEN LOW-LEVELS: 10.5K, 300 KTAS, 2400 PPH 16.5K, 300 KTAS, 2000 PPH H-1
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NAVAL AIR TRAINING COMMAND NAS CORP
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t-39 - Chief of Naval Air Training

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