Flight Procedures
Instrument Flight
AUTO
SCL
AUTO
SCL
SEQ
SEQ
W
W
80
80
T
T
Y
Y
C
C
P
P
1 5 0 /6 7 .0
0 3 0 /4 4 .0
1 7 0 /4 2 .0
0 1 0 /5 2 .0
N
N
33
3
T
T
1 6 :2 4
0 9 :4 8
1 0 :0 6
1 2 :3 0
N
6
N
30
V030
V010
V
V
O
3
O
E
33
W
R
R
0
0
P
P
30
12
24
6
L
L
A
A
N
N
245 G S
250 G S
W 0 3 0 /2 5
W 0 3 0 /2 8
C
W
15
C
21
E
D
D
I
I
C
S
24
C
12
S
R
R
S
A
21
S
A
15
D
D
030
I
030
330
I
030
HDG
DATA
AFT
MENU
CRS
HDG
DATA
AFT
MENU
CRS
E
D
AUTO
SCL
SEQ
W
80
T
Y
C
P
1 8 0 /4 0 .0
0 0 0 /5 5 .0
N
W
T
0 8 :5 3
1 2 :0 9
30
24
V030
V
O
33
21
R
030
0
P
N
S
L
A
N
270 G S
E.
W 0 3 0 /2 8
A . T u n e a n d id e n tify s ta tio n
C
15
3
D
I
B . S e t d e s ir e d c o u r s e
C
12
6
R
in c o u r s e s e le c t w in d o w
S
A
E
D
270
I
030
C. L
o o k fro m
des
ir e d c o u r s e to th e
HDG
DATA
AFT
MENU
CRS
h
ead ofbe
a r in
g p o in te r a n d
C
3
0 d e g re e
s be
y o n d to d e te r m in e
in
te rc e p t h
ead
in g
D . T u r n to in te r c e p t h e a d in g
D.
R -2 1 0
E . M a in ta in h e a d in g to le a d p o in t
a n d th e n c o m p le te in te r c e p t
A.
C.
B.
Figure 17: 30-DEGREE METHOD
(4-01) Original
Page 67
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