Cessna 402B 1973 - Page 75

CRUISE PERFORTVIANCE
WIIH
NOR'YIAt
IEAN
'VIIXIURE
AI
2O,OOO
]I
RPM MP %sHP
TAS
LblHr
EDqUbCe
600
Lb
xrnge
600 Lb
840
rb
&nge
840
Lb
1080
Lb
1080
!t
2450
29
21
25
72.3
66.
4
60.
8
54.9
233
223
215
204
19?,4
L82,4
169, I
156-
6
3.04
3.53
3.83
708
734
?60
182
4.29
4. 61
4,
95
5.36
991
1028
1064
1095
5, 47
5.
92
6.36
6.90
1215
1320
1367
1408
2300
29
zt
23
66. 4
61.1
55.9
50. 4
223
215
205
193
182.4
1?0.4
158,4
146.4
3.29
3.52
3. ?9
4.
10
734
777
?91
4.61
4.
93
5. 30
5.
?4
1028
1060
1088
1107
5.92
6,
34
6.
82
?.38
320
363
398
424
2200 27 58. 2
53.0
2r0
200
186
163.8
rcl.
u
141,0
3.66
3.95
4.26
?69
791
791
5. 13
5.53
I077
110?
1107
6. 59
7.66
1384
L422
L425
2100 25
24
50.0
47.1
44.8
193
186
1??
145.8
141.0
135.6
4. L2
4.26
442
794
?91
783
5.76
5.96
6.
19
LLL2
1109
1096
1, 47
?. 96
1430
1425
1409
CRIIISE
PERFORMANCE
trS
BASED ON
STANDARD
CONDITIONS
(.12"F),
ZERO MN'D, 600; 840, aud 1080
pOIJNDS
Or' FITEL
(NO
RISERVE).
NOTE:
SEE RANGE
PROFIIE
TICUFE 6-10 FOR
RANGE
INCI,IIDING
CLIMB.
CRUISE
PERFOR'\AANCE
IWIIH
NORTVIAt
LEAN
tvllXTURE
AT 25,000;I
RPM MP %BHP
TAS
LblHr
Enduruce
600
Lb
600
Lb
Encunnce
840 Lb
fiatrge
840.Lb
fnftlraEce
1080 Lb 1080
Lb
2450 23
20
55.6
52,6
49,4
47.r
z|z
205
L94
184
158.4
LAL. Z
744,6
139.8
|
;:;;
4.15
| 4.29
803
8t4
80b
?90
5. 30
5.56
5. 81
6.01
tz4
14t)
106
6.82
7. ?3
1446
L464
1449
t422
2300 23
22
51,0
48.4
45. 5
200
173
148.2
L42.8
136.8
4,05
4.20
4.39
810
803
759
o. ot
5.
88
6.14
1134
t124
1063
1458
L444
1365
2200 2X
22
48. I 190
L72
L42.2
136.8
4r,
4.39
BO2
754
5. 91
6,14
IT23
1056
7.59
?.89
I442
135?
CRUISE PERFO4MANCE 15 BASED ON
STANDARD
CONDITIONS
(.30"F),
ZERO WIND,
600, 840, ud
1080
POUNDS OF FrrEL
(No
RnsERyE).
Figlure 6-9
(Sheet
3 of
3)
6-10