——— ——— ——— ——— ——— ——— ——— ——— ——— ,.— _ _,
10J1W1W2E
(
FMS
VEFIT SPEED
‘m
VPATH
● =
i
“--+:1 lcq
I
L
‘scB”Om’Am
——————
r
FMS
MACH/lAS
+
(
FMS
TAS GAIN
1+
LIMIT
PROGRAMMER
TO SH7
TO SH7
~TosH3
r
——————
M2-SZO
NAV COMPUTER
M
121J1N121J1B
I
(
10
ASCB“A-
OATA ,,
I
ASCS “B- llATA
(
‘e
31
L
———. ——
I
I
b
ALTRATE
T
SELECTED
MACWIAS
1;:
ARWW:OI
TAS
TO SH3
ASCS ‘~
PITCH RATE
TO S“7
NORMAL
ACCEL
TO SH3
I
r
——— ——— .
u-m
OADC
I
ASCB “A” tAATA
(
I
ASCB “W OATA
(
L —————— .
(
TAS
+
)
SPEE~oRATE
ZEW
+
+
vER~{~cAmm
ALTITuOE RATE
CONVERTER
10 SH7
l— —11
0 SH3
NOTE 1 (SH1)
r
——
IRS
I
I
—
—
———
M
(
14
ASCS”A” OATA ,5
(
12
ASCB “B” OATA
13
———
L ——
F=
AS’SW
PITCH RATE
TAS
AIRSPEECV
MACH
RR-l
-r-
r
——— ———
SG-S94SVMSOLGENERATOR
T
SsJ
1’
(
ASC8
“A” OATA 16
17
I
ASCB “B- OATA
1
(
CdTi
i==
ASCB “W
INTERFACE
I
l-m
A—————— A
r
——— .—— —,
GP-S20
FLIGHT
1
GUIDANCECONTROLLER
1 m
I
I~-lxt-
1
IASIMACH
SPEED
TACH
KNOS
1
GEN
L————— —d
VPATH, VFLCH, AND FLCH MOOES
——— ——— ——. — ——— ——.. ——— ——— —.—— __
——— ——— ——— ——— ——— ——— ———
AD13.sw~
F1ight Director/Autopilot
Pitch Channel Mode Flow-Diagram
Figure 260 (Sheet 3)
22-14-00
Page 298.131/298.132
Aug 15/91
Use or disclosure of information on Ihm page m subpct 10 the restrlchons on the title page of Ihm document,