Page 554 - (KU)01-75GAJ-1.5 - Change 1

INTRO

EP'S (KU)01-75GAJ-1.5 FIGURES

TORQUE METER SHAFT ACAWS
HORSEPOWER REQUIRED
MODEL: C-130J
AE2100D3 ENGINES FOR TAKE-OFF
DATE: SEPTEMBER 1998 4 ENGINES NORMAL BLEED
DATA BASIS: FLIGHT TEST GROUND

TAKEOFF POWER
5.0 TAKEOFF

FIRE/SMK
NORM 4.5

PRES/OXY

-30 -20 PRESS ALT - 1,000 FT 4.0
-45 -40 -10 ENG/PROP
0
-2
3.5
10 SL FUEL
1
2
4 TORQUE SHAFT HORSEPOWER - 1,000 HORSEPOWER PER ENGINE
20
DEV FROM
6 AAR
STD DAY - °C
3.0
8
30 10
SPEC NOT FOR FLIGHT ELEC
12
40 14 2.5
45 16
HYD

2.0 FLT CTRL
BASELINE

1.5 GEAR
-70 -60 -50 -40 -30 -20 -10 0 10 20 30 40 50 60 70 0 50 100 150 200
OUTSIDE AIR TEMPERATURE - °C CALIBRATED
AIRSPEED - KNOTS
3278W-03-05-006 DOR/RMP
PERF

JETTISON
FIGURE 4-3

TORQUE METER SHAFT HORSEPOWER REQUIRED
FOR TAKEOFF LANDING

DITCHING

BAILOUT

OPER FAULT LG

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