Cessna 402C - Page 321

Hohcrtson 402C
ALTIMETER CORRECTION
ALTERNATE STATIC SOURCE
POHS 82-2
Paie 5-5
-
t. Add cor reeL 1.on to indicat~J .. ltimeter reading.
2. TIlt' follow1ng calibrationa are valid for pilot's and co-
pl1ot'~ altlmetere when the atandard atatic aystem i.
1l'1Udhd.
J. An .1.1ternate stati(: sow-c. ia not available tor co-pUot's
inatrlAel1Ca WhiH'I the opt1o~1 Jual atatic syate_ 18 lnllt.ll.d.
4. Refer to basic POR foJr sear up, flapa 0
0
c.onf1j.urat10n.
JW!
Al!{
COt;TROL
IN ANtJ PILOT'S W!NOOW
CLOSED
ALTITUDE SEA-LEVF.L
10 000 TEET
,
N
FU.PS
JOO
30·
10° 30°
KIAS
I'f.ET
FEET FEET
FEn
70 -h
b
-8
8
80
-7
7 -10 10
'0
-,
0
-11
0
lor)
-.
c -12 0
110
-20 0
-27 0
120
-22 0
-29
0
11.1
-
0 -
0
140
-25
-
-34
-
lbO
-44 -
-59
-
173 -48
-
-b4
-
KA."I AlIt CONTROL OUT AND PILOT'S WINDOW CLOSED
70 12 19
17
25
8(,
14 21
19 29
90 16 lb
22 22
lUil
•
18
12 24
llfi !"J 20 13
27
lW
1,
22
15 29
III
-
22 -
29
J 4('
0
-
0
-
1M'
0
-
0
-
I 7{r
0 -
0
-
RA!'l
AI'
Cu;-.iTROL
OliT
ANO PILOT'S
WINDOW OPEN
]0 -}l
-25
-42 -)4
,,,
-36
-29
-48
-)9
'J!I -40
-40 -54 -54
100
-45
i
-4> -61 -61
llr,
_. ~9
-49
-80 -67
1211
-1,5
I
-54 -88
-73
t25
-
-68
-
-92
14(1 -7t·
- -103
-
lbO
-lO~
-
-1309
-
170 -109
-
-147
-
,