Page 552 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

4.6 CHARTS
ACAWS

MODEL: C-130J CROSSWIND CHART
AE2100D3 ENGINES
DATE: MARCH 1998 TAKEOFF GROUND
DATA BASIS: FLIGHT TEST

TAKEOFF

NOTE
THE MAXIMUM ALLOWABLE INCREASE IN ROTATION SPEED FIRE/SMK
NORM IS 10 KNOTS. RECOMPUTE TAKEOFF GROUND RUN WHEN
ROTATION SPEED IS INCREASED.
PRES/OXY
60 150
RECOMMENDED NOT RECOMMENDED

15 ENG/PROP
WIND ANGLE - DEGREES 50 45 PROHIBITED 130 FUEL
50 30 CAUTION WIND VELOCITY 140
- KNOTS
60

RUNWAY COMPONENT - KNOTS 30 30 60 120 MINIMUM ROTATION SPEED - KNOTS INDICATED HYD
FOR TAKE-OFF
40
AAR

SPEC NOT FOR FLIGHT ELEC
40

20
20
75 110 FLT CTRL

10 100 GEAR
0
DOR/RMP
CAUTION
0 90
PERF 0 10 20 30 40 50 60
JETTISON
CROSSWIND COMPONENT - KNOTS
POWER RESTRICTED TO 2500 HORSEPOWER WHEN LESS THAN 35 KNOTS
AIRSPEED FOR WIND ANGLES BETWEEN 45° AND 315° AND CROSSWIND LANDING
COMPONENTS BETWEEN 15 AND 35 KNOTS. ADD 200 FEET TO THE
TABULAR REFUSAL DISTANCE FOR THIS CONDITION.

DITCHING
3278-QRH-03-07-011
FIGURE 4-1
BAILOUT
CROSSWIND CHART, TAKEOFF
OPER FAULT LG

4 - Use, copying and/or disclosure is
governed by the statement on the
BACK title page of this document. CHARTS