Cessna 402B 1973 - Single-Engine Climb Data; Single-Engine Service Ceiling

SINGtE
ENGINE
CLIIAB
DATA
GrGs
Weight
Pouds
EA LEVEL
59"F
5000 r'r
41-F 10,000
FT 23'F 15,
OOO
FT
5.6" F 20,000
rT
-12'F
Best
CIidb
IAS
MPH
Rate
OI
CLiEb
FtlMin
Best
CIimb
IAS
MPH
Rate
or
UITMD
FtlMin
Best
Climb
IAS
MPH
Rate,
ot
Climb
FtlMin
Best
Climb
IAS
MPII
Rate
of
CliEb
FtlMin
Best
Climb
IAS
MPH
Rate
ot
Climb
FtlMitr
6300
5800
5300
4800
4300
18
08
02
97
225
350
499
680
908
l',l
12
07
c2
96
t41
2'.17
430
615
850
11?
tLz
10?
101
?0
202
360
550
790
116
111
106
101
v)
128
289
484
731
t ld
109
to4
99
94
-278
U
192
4
NOTE: FI,APS
AND
GI'AR
RETRACTED.
INOPERATIIT
PROPELLER
.
FEAT}IERED,
WING BANKED
5.
TOIilARD OPERATTVE
ENGINE,
COWL FI"{P
CLOSED
ON
INOPERATIVE
ENGINN,
34. 5
IN.
HG. M.
P.,
TO 16,000
FT.,
PLAOARD I!l- P.
ABOVE 16,000 I'T.
,
2?00
RPM, lvtrlfl'URF-AT
RECOMMENDED
FUEL FTOW. DECREASE
RATE OF CUMD
15 FTlMiN FOR
EACII 10"F
ABOVE STANDARD TEMPERJTIIRE
FOR
A
PARTICUI,AR
ALTITIJDE.
Figure
6-?
SINGTE
ENGINE
SERVICE
CEIIING
BEST CLIMB SPEED
APPROXIT4ATELY
110 MPH
IAS
(
R/C
=
50 FPM)
GROSS
WEIGHT
POUNDS
6300
5800
5300
4800
4300
OUTSIDE
AIR TEMPFRATURE
.
F
-10
10
20
30
40
t4,zoo
1?,300
19,450
21,
?00
24,40O
13,250
16,950
19,100
2t,3OO
24,OOO
72,2O0
16,
?oo
18,700
20,900
23,650
11,150
16,350
18,400
20, 600
23,250
10,100
15,8OO
18,000
20,2OO
22,850
9,050
14, ?50
1?,
600
19,800
22,450
7,950
13,
?00
1?,300
19,450
22,050
NOTE:
TABLE PROVIDES
PERFORMANCE INIORMATION
TO AID IN ROUTE
SELECTION
WHXN OPERATDIG
UNDER
FAR
135.
145
AND
FAR
91.119
REQUIREMENTS
-
INCRXASE
INDICATED SERVICE CEILINGS
1OO
FEET FOR
EACH O.
10
INCII IIG. ALTIMETER
SETTING
GREATER
THAN 29.92.
DECREASE
INDICATED
SERVICE CEILINGS
1OO FEET FOR
EACH
O' 10
INCH
iIG.
ALTIMETER
SETTING LESS
THAN
29.92.
Figure
6-8
6-1