Page 574 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

ACAWS

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

NOTE
THE MAXIMUM ALLOWABLE INCREASE IN TOUCHDOWN SPEED FIRE/SMK
NORM IS 10 KNOTS. RECOMPUTE LANDING GROUND ROLL WHEN
TOUCHDOWN SPEED IS INCREASED.
PRES/OXY
60 150
RECOMMENDED NOT RECOMMENDED
15 ENG/PROP
WIND ANGLE - DEGREES 50 45 130 FUEL
50 30 CAUTION 60 140
- KNOTS
WIND VELOCITY

RUNWAY COMPONENT - KNOTS 30 NOT FOR FLIGHT 120 MINIMUM TOUCHDOWN SPEED - KNOTS INDICATED
40
AAR

40
SPEC 30 60 ELEC

20

20
75 110 HYD
FLT CTRL
10 100
0
GEAR

CAUTION
0 90
0 10 20 30 40 50 60
DOR/RMP
CROSSWIND COMPONENT - KNOTS
PERF
JETTISON

LANDING
3278_QRH-09-01-011
FIGURE 4-18
CROSSWIND CHART, LANDING DITCHING

BAILOUT

OPER FAULT LG

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