Cessna 402B 1973 - Cruise Performance: Sea Level

CRUISE
PERFORMANCE
WIIH
NORMAT
IEAN
MIXTURE AT
sEA
tEVEt
RPM
MP
%BHp
TAS
Lb/Hr
Enduance
600
Lb
Rarge
600 Lb
Endu&ce
840
Lb
Range
840
Lb
Endur&ce
1080
Lb
'
Range
r080.
Lb
2450
25
23
?1.9
65, ?
59.2
195
18?
1?9
L10
188.4
t12.8
r42.8
3.18
3.41
3.82
4.20
621
649
683
4.46
4. 86
5.34
5.88
869
909
956
1000
6,25
6. 8?
7.56
t1t
169
230
285
2300
29
25
23
65.
?
60.2
54. 3
48.4
187
180
172
163
112.8
159.0
145.8
133.2
3. 47
3.77
4.12
4. 50
649
6?9
?08
?34
,1.86
5.28
5.
?6
6.31
909
951
s91
1028
6. 25
6.
?9
'1.47
8.11
.169
222
.215
2200
29
23
62,1
56.6
45- I
183
1?5
165
r59
.63.8
.27.8
3.66
3.9?
4. 33
4. 69
670
694
746
5.13
6.
06
6.
5?
938
I't2
1000
to44
8. 45
1206
1250
1285
t344
2100
29
27
25
23
27
19
ca-o
52.3
47.4
42.2
31.2
32.0
1?6
169
153
L42
126
r$.0
141.6
131.4
120.6
111.6
102.0
3.92
4.24
4.5',1
4. 98
5.37
5. 88
690
?16
744
?61
764
741
5.
49
5.93
6. 39
6.
9?
8.24
966
1002
1036
1065
10?0
103?
?.06
?.63
8.22
8.96
9.68
10. 59
1243
1289
1332
13?1
13?5
1334
NOTE:
CRU]SE
PERFORMANCE
E BASED ON
STANDARD
CON'DITIONS
(59'F),
ZERO
WIND,
600, 840,
ed 1080
pouNDs
oF FUEL
(NO
RESERVE).
SEE RANGE
PROFII,E FIGI'RE
6-10
FOR RANGE
INCLIIDING
CLIMB.
CR,UISE
PERFORMANC
WITH
NORMAT
TEAN
MIXTURE
AT 5OOO
FI
RPM
MP
%BHP TAS
Lb/Ht 600
Lb
600
Lb
840
Lb
Range
840
r.b
Enquroce
1080
Lb
Rangs
1080
rb
2450
29
27
?1.9
65.
?
53,3
204
196
186
1?8
r88.4
L72.8
157,8
r43.4
3.18
3.41
3.80
4.18
650
681
707
745
4.46
4. 86
5. 32
5.86
910
953
990
1043
D.
''J
6.25
6. 84
1169
1225
t27 2
1340
2300
29
27
oo. a
60.5
54.9
49. I
196
189
180
1?1
!72.8
160.2
L4'1.6
134.4
3,41
3. ?5
4. O7
4,
46
681
?08
732
?63
4.86
5, 69
6.25
991
1025
1068
6.25
6.
?4
7.32
8.04
1225
.
L27
4
1318
13?5
2200
29
23
56, I
46.4
1S1
183
167
151.8
140.4
129.0
3,
64
3.95
4. 65
695
't48
1't7
5.
Oll
5.
53
5,98
6.51
Lot2
to4'l
1088
6. 55
?.11
7. 69
8.
3?
251
301
346
398
2100
29
27
23
21
58.5
48.
1
4ta
37.9
32.7
185
1?8
169
159
L41
124
155.4
L43.4
132.6
L22.4
112.8
103.2
3.
86
4.18
4,52
4. 90
5.32
5. 81
714
745
?65
't19
782
727
5.41
5.86
6.33
6.86
?.45
8.
1?
.000
.043
.0?1
.091
.095
.009
6.
95
?.53
8.14
8. 82
9.5?
LO,41
.286
340
.3?6
.Q2
.407
298
CRUEE PERTORMANCE
IS BASED
ON
STANDARD
CONDTUONS (41"F),
ZEROwrND,1600,
a40,
ad 1Os0
poUNDsOF
FUEL.(NoREseRvii
-,,
NOTE:
SEn RANGE
PROTTL+
FIGUR5
6_10 rOR
RANGE
INCLUDING
CLIMB,
6-8
Figure
6-9
(Sheet
1
of
B)