Honeywell SPZ-8000 - Page 603

C1OJ2B
— 10
——— ———
=4=mGHT GUIDANCS COMPUTER
AVERAGED
——
——— ——— ——— ——. ——— ——— ——— ——— ———
(
PITCH ATT
~
/1
1
2
0
14
Is
M
)5
1
2
F
,m CROSS
r
——— ——— SIOE
PC4B0 TURN PITCH
1~ FGC
CONTROLLER
129J1
PITCH WHEEL
(
+ 18
TACH NO 1
- 19
TAS GAIN
TO SH7
PROGRAMMER
t
~
PITCH HOLD +(AP ENGo~
●NO VERT F D MODE)
I
I
NOTE 4
I
-{ PITCH ATTITUOE ~ TO SH1 AND SH7
\
/
TO SH7
TO SH 1
l-~ ‘OsH’
u
---F==l
A
-v
A
v
NOTES
1. THE FOLLOWING ASCB ‘A- AND “B- DATA (SH1
THRU 10) IS AVERAGED IN THE FZ.S2rl
● ROLUPITCH ATTITUDE
r-==-TO”’
r
——————
IRS
I
ASCB
“A” DATA
(
14
15
I
( ~
12
ASCB ‘%” DATA
13
1-
——— ———
d
. PITCH RATE
● TAC
ASCB “A
I
,--
● LONGITUDINAL ACCEL
● NORMAL ACCEL
● VERTICAL SPEEO
(NOTE 1)
ASCB B
I
THE FOLLOWING ASCB “A” OR 4’0”MTA (SH1
TliRu 6 ) IS PROVIDED
FROMTHECOLAPLEDSIOE:
● AIRSPEEDfMACH
● FMS SEL MACH/lAS
● ALTITUDEIPRESELECT ALTITUDE
● ALTITUDE RATE
—
r
SG
I
I
L
——— ———
-SM SYMBOL GENERATOR
M
S5JlA/SSJ2B
(
ASCB“A”DATA 16
17
ASCB‘%”DATA
(
16
17
——— ———
● MIDDLE MARKER
● GLIDE SLOPE DEVIATION
● FMS PRESLECT ALTITUDE
● FMS CMD VS
IF ONE OF THE SIGNALS IS INVALID AND AVERAG-
ING IS NOT POSSIBLE. THEN THE SY3TEM
--Ed
SWITCHES TO SINGLE SIDE OPERATION USING
THE SIGNAL FROM THE VALID SENSOR.
I NOTE 1
2. THE SWITCH NOMENCLATURE CAUSES THE
SWITCH TO CHANGE FROM STATE SHOWN.
3. POLARITY SIGNS AT SUMMATION POINTS
DENOTE SIGNAL RELATIONSHIPS.
r
——— ——— —
AZ-81ODADC
I
ASCB “W OATA
(
0!!
9JlA/9JlB
11
12
13
i4
55
56
FIAP
HANDLE
57
SWITCH
58
4. ROTATING THE PITCH WHEEL F%l@lDES BOTH
TACH OUTPUTS AT THE SAME TIME.
I
ASCB‘“WDATA
(
I
I
(
0’
FLAP POSITION ~,
I
39
LIFT
COMPENSATION
+
1- COS OF
TO SH7
ROLL ANGLE
L ——
——— —.
G=-=DE&
PITCH HOLD MODE AND LIFT COMPENSATION
!——— ——— ——— ——— —
——— ——— ——
AD.13664 ~ 433
F1ight Director/Autopilot
Pitch Channel Mode Flow Diaaram
Figure 260 (Sheet 1) “
22-14-00
Page 298.127/298~128
Aug 15/91
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