~'-PIi_()T'S
OPERATING
1978
HANDBOOKL'
J£RFORMANCESPECIFICATIONS
CESSNA MODEL 152
'SPEED: t S
11 10
r a
Range Time Time Range
NOTS NOTS NOTS NO TS
350NM .4 .5 2 H
Time SE IC ILIN ILIN TA EOFF EOFF PERF PERFOR ORMA MANC NCE: E:
.7 PM 14,7 14 ,700 00 FT
1340 13 40 FT LAND LANDIN IN
PERF PERFOR OR
ANCE AN CE 1200 12 00 FT OT OT 1670 16 70 LB
TA
PT
IG T: 1081 LB 1081 1118 11 18 LB
IM
EF 89 LB
AG AG PO
LO
ALLO ALLO IN
ANCE AN CE /H
12 LB 10.5 15.2 L. L.
OI
CAPA CA PACI CITY TY 0-235-L2C
installed.
OT
OP RA
N G H AN D
Cessna.
152
COPYRIGHT
1977
MP
D1107·2·13-RPC-5,OOO-11178
OOK
CONGRATULATIONS
CESSNA 52
CONGRATULATIONS so
Dealers: sa
workmanship.
Company.
es
er
CESSNA
ENTS ENTS
SECTION
WEIGHT
BALANCE/
AIRPLANE
SYSTEMS
SERVICE SUPPLEMENTS (Opt (O ptio iona na
yste ys te
escr es crip iptio tio
If
CESSNA MODE 152
SECT SECTIO IO GENERAL
GENERAL
Page
. . , A
dS
e P tA dB
1-1
CESSNA
GENERAL
NOTES:
1.
Wing
sp
Maxi Maximu mu
hown hown
it
trob trob
ligh lights ts in tall talled ed
heig height ht shown
pressed,
flat flated ed an
flas flashi hing ng beac beacon on inst instal alle led. d.
length th is 58". 58". base leng ll 5.
Wing
ro
le
16 square feet.
in outboard wing tip)
1'1--
3
1
Figure 1-1. Thre Thre -2
is 12",
iv ",
in to
CESSNA EL
GENERAL
INTRODUCTION ls
in
tain tain
su
le
ta
ly
ESCR ESCRIP IPTI TI
AT
ENGINE in in in
Av -2 -a
-L
in t-
displacement.
-c
iz
ta 3c
0r
PROPELLER ro
ll
r: lAl0 lAl0 /T inim inim
.5 in
FUEL
Fuel Fuel Ca Capa paci city ty St rd
s: .5
lo 1-
CESSNA MODE MODE 15
GENERAL
Tota Tota
sa le
.5
ll
5g
s.
NOTE
capacity.
OIL Oi
ra
(Spe (Spe ific ificat atio io ):
io
iliz iliz NOTE
is
SA IL-L IL-L-2 -2
it
1-
ratu ratu
tw -1 (O F) lo -1 F) 1A le is
-1 Oi Ca Capa paci city ty
fo
(7 l: )a
F)
IO GENERAL
CESSNA MODE MODE 15
IG in ig in
lb 0lb
tm
t:
NOTE 0l
TA
AI
EI II
BAGG BAGGAG AG
SPAC SPAC
1l
8lb
DI ENSI ENSION ON
SPEC SPECIF IFIC IC LO LOAD ADIN INGS GS in
5l 2lb /h
TERMINOLOGY
KCAS
airspe peed ed co corr rrec ecte te indicated airs
1-5
CESSNA MODE MODE 15
GENERAL KIAS KTAS ltit ltit
te
ratu rature re
position.
NE
METEO METEORO ROLO LOGIC GICAL AL TERMINO TERMINOLO LOGY GY OA
Standard Temperature Pressure Altitude
-6
0f
EC IO GENERAL
CESSNA MODEL 52
EN IN
OWER OWER TE
INOL INOLOG OG
BR RPM Static RPM
stationary.
TERMINOLOGY Demonstrated Crosswind Velocity sa le Fuel Fuel Unusable Fuel PR NMPG tion.
IN Reference Datum
purposes.
Station Arm Moment 1-
SECTlONl
CESSNA
GENERAL
1000
Gravity (C.G.)
C.G. rm C.G. Limits
iv
ig t.
Standard Empty Weight lu Useful Load Gross (Loaded) Weight Maximum Takeoff Weight Maximum Landing Weight Tare
1-
SECT SECTIO IO LIMITATIONS
CESSNA MODE MODE 15
Page
Airs Airspe peed ed Li itat itatio ions ns rs In ic Po er Pl Li it ti
Fuel Fuel Li itat itatio ions ns
rkin rkin
2222-
2-5 2-5 2-5
22-
2-1 (2-2bla (2-2 blank) nk)
SECT SECTIO IO LIMITATIONS
CESSNA ODEL OD EL 15
INTRODUCTION
REMARKS
SPEED VNE
an
oper operat atio ion. n.
VNO
VA
VFE
, a
Mane Maneuv uver erin in
Spee Speed: d: 101 96
104' 98'
o n
d t
Speed
Speed
139
143
wi
ws
n.
2-
CESSNA MODE MODE 15
IO LIMITATIONS
MARKING Whit Whit
KIAS KIAS VALU VALU
SIGNIFICANCE
rc
flap flap exte extend nded ed
laps laps etra etract cted ed
Oper Operat atio ions ns must must be on uc
Yell Yellow ow Ar
PO
ER PLAN PLAN
LI
ITAT ITATIO IONS NS
-2
NOTE
pst,
Pr
ll
l0 /T inim inim
2-
.5 in
pp
im
it
SECT SECTIO IO LIMITATIONS
CESSNA MODE MODE 15
INSTRUMENT
MINIMUM LIMIT
Tachometer 245°F
Oi Temp Temper erat atur ur l P
ig ig
0lb 0l
in 1(o lo
NOTE 0l
0i
5in
0l
2-5
CESSNA ODE~ OD E~ 15
LIMITATIONS
NE
St Spins
im
ta
ER
IMIT IMIT
.9 .9 .9
ig ts rn
thin thin
,-
2-
ts ts ot
CESSNA MODEL 15
SECT SECTIO IO LIMITATIONS
issuance.
FUEL FUEL LIMITA LIMITATIO TIONS NS Stan Stan ar Ta Tota Tota Fuel Fuel
13
sa le Fuel Fuel Tota Tota Fuel Fuel 39
24.5 1. 19.5
37.5 U.S. U.S. gallon gallons. s.
sa le Fuel Fuel 1.5 NOTE
capacity. NOTE tank).
LGr Fo
ly
iati iati /1
Fu
lu
iati iati
Fu
2-
SECT SECTIO IO LIMITATIONS
CESSNA MODEL MODEL 15
PLACARDS in ivid ividua ua
plac placar ards ds
1.
equipped.)
104knots 16701bs +4.4,-1.76
EXCE EXCE Maneuver Chandelles Laz 'Eights 'Eights St Turn Turn
In
2-
io
THOS THOS
95 kn knot ot 95 kn knot ot 95 kn knot ot
in
it
ft.
LIST LIST
EL
St ll (e hi stal stalls ls). ). Slow Slow De Dece cele lera rati tion on
4k ro te
lt tu
loss loss
CESSNA LIMITATIONS
L/
IN
FUEL
IA IO
FUEL
SO IN
IO
0U
SPIN SPIN RECO RECO ER 1.
STALL
2-9/(2 2-9 /(2-10 -10 blank blank
SECT SECTIO IO EMERGENCY EMERGENCY PROCEDURES PROCEDURES
CESSNA MODE MODE 15
Page 3-
OPERATIO OPERATIONAL NAL CHECK CHECKLIST LIST
d L
in In
3-6 3-6
ir te
Icin Ic in
te
AMPLI AMPLIFIE FIE
Land Landin in
itho ithout ut Elev Elevat ator or-C -Con ontr trol ol
PROCED PROCED RE
3-10 3-10 3-10
SE TI EMERG EMERGENC ENC
PROCEDU PROCEDURES RES
CESSNA MODE MODE 15
Page
y F r L
. . . . . . . . . . . e O
3-
SE TION TION EMERG EMERGENCY ENCY PROCEDU PROCEDURES RES
CESSNA MODE MODE 15
INTRODUCTION
te
erin erin 0L
is
Sp
te
ld
is
60
IA
104KIAS 98 IA 93 IAS 60 IA 55 IA 65 60
IA IA
1.
3-3
IO EMERG EMERGENC ENC
CESSNA MODE MODE 15
PROCED PROCED RES
1.
FO CE
LAND LANDIN IN
1.
-- SLIG SLIG
S.
S.
3-
--
IL
IO
CESSNA MODEL 15
IO EMERG EMERGEN ENCY CY PROCED PROCED RES
DITCHING -intentions.
121. 12 1.
z,
3.
SWELLS. 5.
-opened,
FIRES
1.
in
st ts 0R
installed).
1.
-5
SECT SECTIO IO EMERG EMERGENC ENC
PROCED PROCEDURE URE
5K mixture). it
En in
Po er). er).
1.
WARNING
flight:
co plete pletely ly ex extin tingu guish ished ed
1.
WARNING te
3-
CESSNA MODE MODE 15
SECT SECTIO IO EMERGEN EMERGENCY CY PROCEDURE PROCEDURE
CESSNA MODEL MODEL 15
NOTE to
retracted.
ICING
to
tsid tsid
ir te
tu
"o
ness.
impr improv oved ed visib visibili ility ty
essa essary ry fo
accumulation.
3-
IO EMERG EMERGENC ENC
CESSNA MODE MODE 15
PROCED PROCEDUR URES ES
1.
DT
MALFUNCTIONS OVER OVER-V -VOL OLTA TA
LI
ILLU ILLU INAT INATES ES
1.
IS 1.
3-
ffl
CESSNA
EMER EMER ENCY ENCY PROC PROCED ED RE
AMPL AMPLIF IFIE IE IN
ROCE ROCE URES URES
IL
3- shou should ld be failure. th ec list list
10,000 8000
be
I---I---l~-+---+--+---+--t--:.-..!~ --
4 - - • •
(!)
2000
PROP PROPEL ELLE LE
WIND WINDMI MILL LLIN IN
14
16
18
20
3-
IO EMERG EMERGENC ENC
PROCED PROCEDUR URES ES
lo
te io
ti
CESSNA DE 52
5K ti
trim
iv ly
FIRES if
3-10
SECT SECTIO IO EMERGENCY EMERGENCY PROCEDURE
CESSNA MODEL MODEL 15
he inadv inadver erten tently tly tr ly-p ly-p le ly
EC
ic
tu
in tr
in
in
iv
th
il
180
IN
1.
airplane. 4. accurately. tr l.
ib
itio itio
in
id
rc
le
trol trolli li
in
fel fth
th
tr
th
ll
1.
3-11
CESSNA MODE MODE 15
SECT SECTIO IO EMERGENCY EMERGENCY PROCEDUR PROCEDURES ES
th
1.
ttle ttle
ri
li
stra straig ig
IG
in
IN
IN
IT An inad inadve vert rten en
icin icin
enco en co nter nter
cond co nditi ition ons. s.
SPINS should be used: IL
1.
TION TION 3-12
IN
POSI POSI IO
,HOLD FULL FULL RUDD RUDDER ER
ROTA RO TATI TI N.
PPOS PPOSIT IT
TO TH
DIRE DI RECC-
SE TI EMERG EMERGENCY ENCY PROCEDU PROCEDURES RES
CESSNA MODE MODE 15
ery. SMOO SMOOTH TH RECO RECO ER
FROM FROM TH
RESU RESULT LTIN IN
IVE. IVE.
NOTE
POWER
th
in
ti
depostts,
Ht
3-13
SECT SECTIO IO EMERGENCY EMERGENCY PROCEDURE PROCEDURE
CESSNA MODE MODE 15
igni igniti tion on po posi siti tion on
MA NETO NETO
ALFU ALFUNC NCTI TION ON Hto if continued
OW OI
PR SS
th touc touchd hdow ow
is
spot spot
MALFUNCTIONS io
te situation.
3-14
lo
lf ib
th
CESSNA MODEL MODEL 15
SECT SECTIO IO EMERG EMERGENCY ENCY PROCEDU PROCEDURES RES
voltage if
th
In io
ti
3-15/(3-16
blank)
CESSNA
NORMA NORMA
SE IO PROCED PROCED RES
Page 4-3
CHECK CHECKLIST LIST PROCED PROCEDUR URES ES
in
efor efor
Land Landin in in
al ed La di Se
ring ring Airp Airpla la AMPL AMPLIFIE IFIE
PROC PROCED ED RE 4-11 4-11
4-1
NORM NO RMAL AL PROCED PROCED RES
CESSNA EL
Page
Warm-Up to
ross ross in
Nois No is
4-
Ta
ff
lked lked La in th ti Abat Ab atem emen en
4-13 4-13 4-13 4-13 4-14 4-14 4-14 4-15 4-15 4-15 4-16 4-17 4-17 4-19 4-19 4-20 4-20 4-20 4-22
IO NORMAL NORMAL PROCEDU PROCEDURES RES
CESSNA MODE MODE 15
INTRODUCTION
0p Takeoff:
65-7 KIA 54 IA 70-8 KIA 67 IA 61 IA 55 IA
0F Land Landin in
Appr Ap proa oach ch
60-70 IAS 60-70 55-6 KIA 54 IA
al ed Land Landin ing: g:
55
1670Lbs im
tr te
in
it
IA
104KIAS 98 IA IA 12 NO NOTS TS
4-
CESSNA EL
NORM NO RMAL AL PROC PROCED ED RES
NOTE
lk-a lk-aro roun un
insp inspec ecti ti n. In ls
-4
th
EC IO NORMAL NORMAL PROCEDU PROCEDURES RES
CESSNA MODE MODE 15
IS
IG
IN
EC IO
G)CABIN 1.
®EMPENNAGE 1.
n -
RIGH RIGH
IN
Tr ilin ilin Ed
1.
RIGH RIGH 1.
in
IN Ti -D
--
ISCO ISCO
EC
®NOSE 1.
If water
4-5
CESSNA MODE MODE 15
SE IO NORMAL NORMAL PROCEDUR PROCEDURES ES
fore foreig ig
tter tter
stoppage. @LEFTWING 1.
1.
operation.
1.
1.
1.
li
In
--
IO NORM NO RMAL AL PROCED PROCED RES
CESSNA MODE MODE 15
0R
BEFO BEFORE RE TAKE TAKEOF OF
--
0R
required.
TAKEOFF _1
NORMA NORMA
CESSNA ODEL OD EL
PROCED PROCED RES
0f
NOTE
300 feet. feet.
CRUISE 0R
1.
AN
LANDING NO
4-8
AL LAND LANDIN IN
CESSNA MODE MODE 15
NORMA NORMA
PROCED PROCED RES
to
ALKE ALKE
ANDI ANDING NG
1.
to 20°.
AFTE AFTE
LAND LANDIN IN
SECU SECU IN
AI PLAN PLAN
1.
4-9/(4-10blank)
CESSNA DE
NORMA NORMA
PROCED PROCEDUR URES ES
0R NOTE
exhaust
stack
NOTE
TAXIING
CESSNA
NORM NO RMAL AL PROC PROCED ED RE
CODE
NOTE
ainta aintain in dire directi ction on
Figure 4-2. Taxi Taxiin in 4-12
Diag Diagra ra
SECT SECTIO IO NORMAL NORMAL PROCEDU PROCEDURES RES
CESSNA MODE MODE 15
be
WARM-UP
ig itio itio
it 5R
ir
0R .Ne
to to th
Hpo itio itio
RP
to th
osit ositio io op sh ld
be
4-13
CESSNA ODEL OD EL
NORM NO RMAL AL PROCE PROCEDU DURE RE
TAKEOFF
_1 10
4-14
CESSNA ODEL OD EL
NORMA NORMA
SE TI PROCEDU PROCEDURES RES
attitude.
0f
to
CRUISE %a
%p inSect Sectio io
NOTE %to
%p
cylinders.
4-15
SECT SECTIO IO NORMAL NORMAL PROCEDU PROCEDURES RES
ALTITUDE
CESSNA MODE MODE 15
KTAS
Se Leve Leve
100
16.4
94
103
17.0
97
18.4
107
17.6
100
18.9
KTAS
NMPG
89
19.8
0R
to
operation.
re 4-16
SECT SECTIO IO NORMAL NORMAL PROCED PROCEDUR URES ES
CESSNA MODE MODE 15 1.
%to appr ap pr xi at ly
ar
il 22 0- 250R 250RPM PM). ).
ic
le
ls
%o
power. NOTE 0R
mixture.
STALLS
SPINS .B
th
belt
4-17
CESSNA MODEL MODEL 15
SECT SECTIO IO NORMAL NORMAL PROCEDU PROCEDURES RES should be
ig
lt tu
are co
0f
be
plet pleted ed 40 4000 00fe feet et or
li or ab abov ov
be
1-
be 6000 be
0f
91.71.
orientation. As
th
be be
inadvertent nose no se-d -dow ow
spir spiral al NOTE tt
ti
ld be
2t
1to
==.
4-18
CESSNA MODE MODE 15
SECTION· NORMAL NORMAL PROCEDU PROCEDURES RES IL ITIO ITIO
IN ID
FULL HOLD FULL
IO
AFTER CONT CO NTRO RO
4.
ER
IO
EE
TO
IR
BRISKLY
IN
HOLD
PP SI
IL
IO
ery. SM OT
RECO RECO ER
FROM FROM TH
RESU RESULT LTIN IN
IVE. IVE.
NOTE
fl
/win /win
tr
tu
LANDING be
0to
is
SH
it 5to 5K
-o
-o
imin iminis is
FI LD LA
IN
4-19
CESSNA
NORM NO RMAL AL PROCED PROCED RES
be
conditions.
AL ED LAND LANDIN IN
be
NOTE
ith Prehe Preheat at
SECT SECTIO IO NORMAL NORMAL PROCEDU PROCEDURES RES
CESSNA MODE MODE 15
NOTE
9.
0t
0R
0o
Without Preheat:
be
NOTE
th
in
0R
in
SE IO NORMA NORMA
CESSNA MODE MODE 15
PROCEDU PROCEDURES RES
conditions.
1.
NOTE
if
fo
2a
im
CESSNA ODEL OD EL 52
SE IO PERFORMANCE
PERFORMANCE
Page
Takeoff
.A
5555555555-10 5-11
.R .C
5-12 5-13 5-14 5-15 5-16 5-17 5-18 5-19
5-1/(5 5-1 /(5-2 -2 blank blank
CESSNA
PERFORMANCE
INTRODUCTION to
techniques.
%o
to illus-
LE
IRPL IR PL
LE
ff
CO FI ig
TA EOFF EOFF CO
ITIO ITIO
RA IO
1610Pound 1610 Pound 24.5 24 .5 allons allons
1500 15 00 Feet
Temperature ie
le
3500 35 00 Fee
in
-3
CESSNA PERFORMANCE CR IS CO COND NDIT ITIO IONS NS Tota Tota ista ista ce
5500 55 00 Fee
Temperature LAND LANDIN IN
ot
COND CO NDIT ITIO IONS NS
ea
in
2000 Fee 2000 25°C 3000 30 00 Fee
Temperature
TAKEOFF
this this pa part rtic icul ul th
foll follow owin ing: g:
0f 98 Feet Feet 182 Feet
12
Decrease (980 (980 feet feet
nots nots ts
100/0
130/0)
Decrease tota tota ista ista (1820 (1820 fee 13%)
13
Decrea Dec rease se
12 85 Feet Feet
1820
158 Fee
5-
CESSNA
PERFORMANCE
CRUISE
5-9.
0f
37 (3. ho hours urs te
in
0f pond to Power Tr irsp irsp
64 99 no nots ts 5.2GPH
to
FUEL FUEL REQU REQUIR IRED ED
0fe
0fe
1g -5
CESSNA EL
PERFORMANCE
%f
16°C 100C 10 0C )(1 0 0 / 0
(1.0 (1.0)( )( 16
to
16
on-s on -sta ta da dard rd
Increa Inc rease se
te pe pera ratu ture re
0. 1.2 Gallon Gallon 0na
to
miles.
Tota Tota Clim Clim Cr is
ista ista ista istanc nc ista ista
32 -1
99 -1 89
89
.5 5-
1.
rs )( .2
nots no ts
3.
nots no ts
ll
s/
ti
ours ou rs
18.2Gallon 18.2 Gallon
il
CESSNA
SECl'ION5 PERFORMANCE
foll foll
requincI
Th
taxi. an '-keoff
Climb
Cruise
.2 18.2
2ii:2 Gallons
required
This will
s:
of:
24.5
-20.2 Ts'Gallons
underway. ground speed checks will required
LANDING be used fo airport. Figure 5-10
to
are
rt foll foll
te s:
iq roll roll
stim stim ti ts
2000 fe
is
tob
in
30°C
Feet 1300 Feet 53
be
-7
SECTIONS PERFORMANCE
CESSNA
CONDITION: Power
rated RP
KIAS KCAS
dive dive
90 69
10 KIAS KCAS
80 44
52
70
85
--
FLAPS KIAS KCAS
85
Fi
5-8
re
-1 Airs Airs
--
Ca ibra ibra io
--
--
--
CESSNA
PERFORMANCE
10
80
..
40
CI
20
-2
-4 -4
20
20
EG
40
60
CE SI
5-
CESSNA
PERFORMANCE
CONDITIONS: Power Of NOTE:
data with
WEIGHT
FLAP
UP
rP
46
36
49 46
·3
44
WEIGHT LBS
FLAP DEFLECTION
49
44
rP
6rP
KIAS UP
1670
40 40
52
46
49 46
5-10
58
42
49
CESSNA
PERFORMANCE 0:(1)
_I«Ill t-_lt-
0011..
'E
t-oo t-Ill
'5
(!Ja: a: I) _I«1Il
.5 :! a..
-_lt-
0011..
'-~'-·NNNC")MV
(!Ja: a: I) _I«1Il
GJ
-_lt-
0011..
t-oo t-Ill (!Ja: a: I) _ I « Il Il l
...I
-_lt-
..
0011..
t-oo
a:
(!Ja: a: I) _ I « Il Il l t-_lt-
0011..
LO
II I I I I 1 11 11 0 10 ,...COIOCOalN,...q-qalC»O-Nq-IO,...C»
-_..-
........
--
~~~~~!ElIRIR18 q-COalONlllalN,...
f )
t-oo t-Ill
:::J
LL LL
IIIl
100~lOi~lOallll
~~5Hi~al~IR~~ alalC»O-Mq-CO,...
-- ................
~~~R~~~~~ ~~~~~~~~~
101ll0§81ll1ll~1ll , .. . . .a . a lC l C » - NM N M qq- C
-- ........ --
,It)
~~IO~~i~:g~ N q. - l. 8. " ". C ». _. M ". " ~. . . . . . . . .
~18S1!El~!El~~!El CO,...alC»O_NMIll
....
..-
............
00108IOo8°~ _Mq-CO,...C»Nq-
t-oo t-Ill (!Ja:
OIllIllIOOOIllOIO ~g:::::g~~:!~i ...--
........
-!§§§~§§§8
a : « II II .
e,
II..
11..0(1)
t-t: 10
~a..~
«(I)
t-u..
11..11..
(!Jill
,...
co
!!
5-11
SECTIONS PERFORMANCE
CESSNA
MAXIMUM CONDITIONS:
Ful Thro Thrott ttle le NOTE:
Mixt Mixtur ur
lean leaned ed above
WEIGHT LBS
1670
PRESS ALT
F C
- F
SPEED
400c
-:woC S.L
4000 6000 8000
12.000
5-12·
fo
67
535
65 62
60
440 340
20 285
230
355 265
85
CESSNA PERFORMANCE.
IMAXIMUM RATE
CONDITIONS:
Full Full Thro Thrott ttle le Stan Standa dard rd Temp Temper eratu ature re NOTES: 1.
3.
.8 of
Incr Increa ease se time time
WEIGHT LBS
1670
above 3000 feet
PRESSURE ALTITUDE
FT
distance by based
TEMP
°c
takeoff allov.nce.
start.
SPEED KIAS
fo each
standard temperature.
CLIMB FPM
NM
S.L
66 2000
66
3000
65
590
4000
65
550
5000
64
.2 .4
6000
.7 8000
-1
62
380
9000
-3
62
340
-7
12.000
-9
Figure 5-6.
.3
300
-5 11.000
17
25 60
.0
29
.4
34
to Climb
5-13
CESSNA PERFORMANCE
CONDITIONS: 1670 1670 Poun Pounds ds Reco Reco mend mended ed Lean Lean Mixt Mixtur ur NOTE: Cruise speeds by appro approxi xima matel tel
2400 2300 2200 2100
71
97
55
87
5.7 5.1 4.5 4.1
67 60 53
2300 46
2550
5.4 4.8 4.4 3.9
96 91 86
55
2500
2450 2200
5.8 5.2 4.6 4.2 3.8
101 96 90 85
80
--
51
56
51
46
96 91 86
80
5.4 4.8 4.3 3.9
95 90 85
80
5.1 4.6 4.2 3.8
67 60
63
56
90
46
79
51
67 60 49
45
57 52
49
89 84
79
4.4 4.0 3.7
75
107
6.1
99 94
71 67
4.7
55
83
3.9
46
45
68
83 101 99 93 88 82
5.3 5.0 4.6 4.2 3.9
58 52
56 51
46
62
59
49
45
is
85
102
89
93 88 82 97 92 87 81
4.5 4.2 3.9 4.8 4.4 4.1 3.8
48 44
58 53
49
45
59 56
52 48
44
4.6 4.2 3.8 5.7.
95 89 84 78
4.9 4.4 4.0 3.7
94 88 83
5.2 4.7 4.3 3.9 3.6
71
75
5.8 5.3 4.7 4.3 4.0
95 90 84 105 99 94
65
63
71
-7 5-14
47
6.2 5.5 5.0 4.5 4.1
105
2400 2200
66 59
75
--
2000
BHP
BHP
2450
2000
12,000
speeds
2 ( J O c ABOVE
STANDARD TEMPERATURE
BHP
2300 2200 2100
10,000
th
ox,.
2000
8000
e)
with speed
20
FT
4000
on
two knots.
PRESSURE
2000
(See
77
106 103 98
93 87
5.7 5.4 4.~ 4.5 4.2 3.8
97 92 86 81
4.8 4.4 4.0 3.8
99 96 91 85
4.8 4.6 4.3 4.0 3.7
79
CESSNA
PERFORMANCE
CONDITIONS: 1670 Pounds
Stan Standa dard rd Temp Temper erat atur ur NOTES:
2. 3.
chart allows fo th fuel used fo engine start,
Reserve
Performance is shown fo an airp airp an
equi equipp pp th cruise speeds by approximately two knots.
12,000
~,
10,000
:::>
fair fairin ings gs whic whic
incr increa ease se
l_~
If'
8000
speed
I
,
K,- r A• S ,
1""102KTAS
It(,
1~7 , 1 C ' f A ; ~ ' ..... 10 KT
6000
i= ..J
.8 KTAS KTAS
4000
a:::
I-w
a::: r-a:::
1-3:
2000
I-~ I-~
1-100 -KT~~
S.L.3OQ
~~
r-3: 10
87 :g KT~
a:
-~ -~
-~ 450
5-15
CESSNA
PERFORMANCE
CONDITIONS:
Recommended lean Stan Standa dard rd Temp Temper erat atur ur Zero Wind NOTES:
1.
fo engine start, taxi This chart allows fo th taxi take takeof of an climb, and th distance duri 5-6. during ng clim clim based 45 2.8 gallons. Performance is sh wn fo an airp airp an quip quip ed with speed ai in hich hich ncre ncreas as th cruise speeds by approximately two knots.
12,000
r-r-"",,,,,,,,,,,,""""-.--r--r-r-.--r---."'-K'"""r-r-,....,...-,,....,
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10,000 l-+...,j--1f-+,,~
'---
--
~~~~ ~~~~'f'f-I4 I41I 1I -+---+---I-I-- -+-H -+-H --t-I--t-I--t-t- --l
L......L-l...J1I!107
~ 10 10 0
+f
1--+-+-IH.... C:rAS ~KTAS 1--+-H~1-+-I-~~-+-~91 6OOO1--t~~r+~~-+;-ttl,KT~B-~~+4
1f
79
~IKTASI-I-
1--+~+-I-+-H'+--l~-+-~89 1--t~+4--+-~I--t-t-~~KTAS--~-I-~
4000~~~~~~+4_.~~~~~~ lU
I-
M03
VTAS
lU
~97
I-f-D::
'--I
I-f-:=
KTAS
KTAS
.:iI-I-
f-I-f-;#! 10 f-I-+ f-I-+-IO -IO
87
. S.L. " " H . : . ... . ... . . . . . .AS...I~.....IIIl~,KT_._AS~rn--LIif~"K_TL..AS~;tL...K.t; ... K_T~_AS ......-I-~
5-16
CESSNA
PERFORMANCE
24.5 CONDITIONS: 1670 Pounds
Recommended Lean Mixture fo Cruise Stan Standa dard rd Temp Temper erat atur ur chart allows fo th 2.
Reserve
taxi. takeoff and climb. and th
5-6.
at
based
12.000
al
and
f-+--~Sl
r-+-1-t.."1 10.000
r-I- ~I r-r-~ 'r-C"-..JI
'r
8000
-ec:
'I
u..
6000
..J
4000
2000
_CJ:
f-I--ffi -~ f - f - ~ c-f-2 CJ
-..,_ -..,_
,... f--IS
~~
1-1-
-CJ:
..,_-
5-17
CESSNA
PERFORMANCE
37.5 CONDITIONS:
1670
Stan Standa dard rd Temp Temper erat atur ur NOTES:
takeof of start, ta i, take
fuel
12,000
10,000
8000
an
im
th
I~
J...~ f-~ f--r-.;::,'7
1--«
u.
::::>
6000
t:
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4000 --0::
2000
-i-w
-1-2
r-r'--I-
-r-~ t-~ t-l:!!
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5-18
1-1- -0::
'--+-
-2
e,
e,
t---
10
CESSNA PERFORMANCE
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SECT SECTIO IO WEIGHT BALANCE EQ IPMEN IPMEN LIS
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INTRODUCTION
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NOTE In ad addi diti tion on to
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