Academy of Carver Aviation Aviation Pvt. Ltd.
QUESTION
What is the max speed of a Cessna 152A at sea level What is the cruise speed of a Cessna 152A @5! po"er and at 8500 ft What is the endurance of a Cessna 152A @5! po"er and at 8500 ft #standard tank$ What is the endurance of a Cessna 152A @5! po"er and at 8500 ft #lon* ran*e tank$ What is the max ran*e of a Cessna 152A @ 10(000 ft #standard tank$ What is the max ran*e of a Cessna 152A @ 10(000 ft #lon* ran*e tank$ What is the rate of clim, of a Cessna 152A at sea level What is service ceilin* of a Cessna 152A What is the takeoff performance- *round roll What is the takeoff performance- over 50 ft o,stacle What is the landin* performance- *round roll What is the landin* performance- over 50 ft o,stacle What is the stall speedflaps up( po"er off What is the stall speedflaps do"n( po"er off What is the max ramp "ei*ht What is the max takeoff.landin* "ei*ht What is the standard empt/ "ei*ht What is the max useful load
Cessna 152A
A
B
C
D
ANS
108 knots
106 knots
112 knots
109 knots
A
105 knots
108 knots
118 knots
109 knots
A
%10 &'( %)0hrs)
%12 &'( %)2hrs
%06 &'( %)15hrs)
%10 &'( %)1hrs
A
5%0 &'( 5)2hrs
6%0 &'( 5)2hrs
5%0 &'( 5)1hrs
520 &'( 5)0hrs
A
%65 &'( +)1hrs
%0 &'( +hrs
%65 &'( +)2hrs
%60 nm( +)%hrs
A
615 nm( 6)9hrs
610 nm( 6)5hrs
615 nm( 6)8hrs
610 &'( 6)hrs
A
15 fpm
10 fpm
12 fpm
+5 fpm
A
1+(00 ft
12(00 ft
1+(000 ft
1%(00 ft
A
25 ft
%0 ft
10 ft
15 ft
A
1%+0 ft
1%20 ft
1%25 ft
2%25 ft
A
+5 ft
+25 ft
+15 ft
++5 ft
A
1200 ft
125 ft
1215 ft
12%+ ft
A
+8 knots
+% knots
++ knots
+6 knots
A
+% knots
+8 knots
+6 knots
++ knots
A
165 l,
110 l,
160 l,
115 l,
A
160 l,
165 l,
110 l,
5++ l,
A
11%1 l,
11%0 l,
5++ l,
111 l,
A
5++ l,
5+0 l,
11%1 l,
500 l,
A
1
Academy of Carver Aviation Aviation Pvt. Ltd.
What is the diameter of the propeller he aircraft commonl/ called Cessna 152A is certified under AA t/pe certificate num,er he vne of Cessna 152A is
he vno of Cessna 152a is
he va of Cessna 152A is
he vfe of Cessna 152A is
he "indo" open speed of Cessna 152A is
69 inches %A19 as Cessna model num,er A152 168 knots #kcas$ and 12 knots #kias$ 122 knots #kcas$ and 125 knots #kias$ 106 knots #kcas$ and 108 knots #kias$ 8 knots #kcas$ and 85 knots #kias$ 1+5 knots #kcas$ and 1+9 knots #kias$
he "hite arc on the A34 of Cessna 152A is
from vso to vne
he *reen arc on the A34 of Cessna 152A is
from vso to vne
he /ello" arc on the A34 of Cessna 152A is
from vso to vne
he red line on the A34 of from vso to Cessna 152A is vne he name of the en*ine manufacturer is he en*ine model num,er is he en*ine ,hp is he maximum en*ine speed for all operations
Cessna 152A
68 inches 19A% as Cessna model num,er A152 186 knots #kcas$ and 182 knots #kias$ 121 knots #kcas$ and 122 knots #kias$ 160 knots #kcas$ and 180 knots #kias$ 8 knots #kcas$ and 58 knots #kias$ 15+ knots #kcas$ and 19+ knots #kias$ from %5 knots to 85 knots #kias$ from +0 knots to 125 knots #kias$ from %5 knots to 125 knots #kias$ from %5 knots to 125 knots #kias$
2 inches
1 inches
%A19 as %A91 as Cessna Cessna model model num,er 152A num,er A152A 12 knots 182 knots #kcas$ and #kcas$ and 168 knots 121 knots #kias$ #kias$ 125 knots 152 knots #kcas$ and #kcas$ and 152 knots 121 knots #kias$ #kias$ 108 knots 180 knots #kcas$ and #kcas$ and 106 knots 160 knots #kias$ #kias$ 58 knots 85 knots #kcas$ and #kcas$ and 8 knots 8 knots #kias$ #kias$ 1+9 knots 19+ knots #kcas$ and #kcas$ and 1+5 knots 15+ knots #kias$ #kias$ full flap and C are operatin* correct ran*e from vs to maximum and C are structural correct cruisin* speed from from 125 knots to +0 knots to 12 knots 125 knots #kias$ #kias$ from 125 12 knots knots to 12 #kias$ knots #kias$ accessor/ 'cCaule/ division accessor/ from division 'cCaule/
A
A
A
A
A
A
A
C
Avco 7/comin*
7/comin* Avco
02%5&2C
02%%)%&2C
02%5'2C
0255&2C
A
180 ,hp
108 ,hp
2%%)% ,hp
2%5 ,hp
2550 revolutions per minute
2505 revolutions per minute
2055 revolutions per minute
5250 revolutions per minute
A
A
2
Academy of Carver Aviation Pvt. Ltd.
he static rpm is checked "ith
car,uretor heat on( full throttle( and full mixture
car,uretor heat off( throttle lean to max rpm( and full mixture
car,uretor heat off( full throttle ( and mixture lean to max rpm
car,uretor heat off( full throttle ( full ,reaks unapplied( and mixture lean to max rpm
What is the "in* loadin* factor
10)5 l,s.s)ft
105 l,s.s)ft)
15)5 l,s.s)ft)
15 l,s.s)ft
A
What is the po"er loadin* factor
15)5 l,s.hp
10)5 l,s.hp
10)5 l,s.s)ft
10 l,s.s)ft
A
What is the total fuel capacit/ #standard$
26 *al
%9 *al
1% *al
18)5 *al)
A
26 *al
%9 *al
1% *al
18)5 *al
uarts
8 uarts
)5 uarts
6 uarts
A
continue crankin*
throttle full open
mixtureidle cut off
all of the a,ove
airspeed 65 kias
airspeed 5 kias
airspeed 85 kias
none of the a,ove
C
up
20:
%0:
as desired
What should the first step ,e for a ca,in fire
fire extin*uisher activate
vents ca,in airclosed
master s"itch on
none of the a,ove
What is the total ,a**a*e allo"ance
120 l,
+0 l,
60 k*
120 k*
A
'ark the correct statement
;A is installed in the left "in* root ventilator
;A is installed in the ri*ht "in* root ventilator
ans #A$ and cali,rated in centi*rade and fahrenheit
;A is installed on ri*ht tail cone
h/draulic
pneumatic
mechanical
none of the a,ove
5 to 10 knots
10 to 15 knots
at stall
none of the a,ove
A
What is the total fuel capacit/ #lon* ran*e$ What is the total oil capacit/ What should the initial action ,e for an en*ine fire on *round "ith the en*ine failin* to restart What speed should ,e maintained for an en*ine fire in fli*ht What should the flaps ,e "hile landin* "ith a flat main tire
3tall "arnin* s/stem is of<<<<
Cessna 152A
C
3
Academy of Carver Aviation Pvt. Ltd.
he value of static rpm at sea level under standard conditions is
22502%50
2%502+50
22802%80
2%802880
Amon* the follo"in*( "hich en*ine oil is used
'47l6082 aviation *rade strai*ht mineral oil '47l22851 aviation *rade ashless dispersant oil
'47l6082 aviation *rade strai*ht mineral oil '47l22815 aviation *rade ashless dispersant oil
'47l22851 aviation *rade strai*ht mineral oil '47l6082 aviation *rade ashless dispersant oil
'47l6082 aviation *rade strai*ht mineral oil '47l2851 A aviation *rade ashless dispersant oil
he propeller is
manufactured ,/ 'c caule/ accessor/ division
ans #A$ and has the maximum diameter of 69
ans #A$ and has a model num,er 1A10%.C' 6958
ans #A$ and can ,e moved onl/ at the speed of 2550 rpm #maximum en*ine speed$
C
100: 2+5: and 255: respectivel/
200: 2+5: and 255: respectivel/
115: 2+5: and 2+5: respectivel/
100:2+5: and 2+5: respectivel/
2)5 psi( 6)09)0 psi( 11)5 psi
25 psi( 6090 psi( 115 psi
25 psi( 60190 psi( 2+5 psi
125 psi( 160190 psi( 2+5 psi
&ormal and maximum oil temperature limits are 'inimum( normal and maximum limits for oil pressure are What is the fuel uantit/ left in the left tank "hen the fuel level indicator for the left tank is at = he normal operatin* ran*e for the suction *au*e is et"een "hat stations area is ,a**a*e area 1 and ,a**a*e area 2 At "hich speed are chandelles done What does the ori*inal air"orthiness certificate of the Cessna 152A state
Cessna 152A
C
)5 *allons of usa,le fuel
)5 *allons of unusa,le fuel
1)5 *allons of unusa,le fuel
)5 *allons for standard tanks and )95 *allons for lon*ran*e tanks
+)+ to 5)5 inches of >*
5)5 to +)5 inches of >*
+)5 to 5)+ inches of >*
+)5 to 5)6 inches of mercur/
C
station 506 and station 69+
station 52+ and station 6%92
station 506 and station 69+
station 50+ and station +92
C
105 kias
115 kias
108 kias
1%0 kias
A
A? &4>
B 4
A? &4> B 4B
A? &4> BB D ?BB
C
4
Academy of Carver Aviation Pvt. Ltd. 'aximum *lide speed( and "hich of the follo"in* take place at 60 knots What is the manoeuvrin* speed at all "ei*hts =n*ine failure durin* take off roll( the first three precautionar/ steps for x are he correct seuence of actions for en*ine failure immediatel/ after take offE are maintain airspeed 60 knots( mixture idle cut off and
precautionar/ landin* "ith en*ine po"er
landin* "ithout en*ine po"er flaps up
landin* "ithout en*ine po"er flaps do"n
none of the a,ove
C
108 kias
106 kcas
,oth A and are correct
all of the a,ove are "ron*
C
,rakes appl/( throttle idle( "in* flaps retract
throttle idle( ,rakes appl/( i*nition s"itch off
,rakes appl/( throttle idle( mixture idle cut off
throttle idle( ,rakes appl/( "in* flaps retract
i*nition s"itch off
master s"itch off
fuel shut off valveoff
"in* flapsas reuired
C
=n*ine failure durin* fli*ht is the restart procedure for x airspeed 60 kias
primer in and locked( fuel shutoff valve off( mixture rich
car,uretor heat on( fuel shutoff valve off( mixture rich
car,uretor heat on( primer in and locked( fuel shutoff valve off
none of the a,ove
=mer*enc/ landin* "ithout en*ine po"er is the first step for
seats( seat ,elts( shoulder harnesses secure
mixtureidle
fuel shutoff valveoff
"in* flapsas reuired
A
65 kias #flaps up$
55 kias #flaps do"n$
60 kias #flaps up$
,oth and C are correct
A
airspeed 60 kias( "in* flaps 20:
airspeed 60 kias( "in* flaps %0:
airspeed 55 kias( "in* flaps 20:
none of the a,ove
A
master s"itch off
i*nition s"itch off
radio and electrical s"itches off
fuel shutoff valve off
200 ft.min
%00 ft.min
+00 ft.min
150 ft.min
1200
100
2280
2250
What is the airspeed durin* emer*enc/ landin* "ithout en*ine po"er What is the airspeed and flaps settin* for a precautionar/ landin* "ith en*ine po"er Frecautionar/ landin* "ith en*ine po"erE select the incorrect step urin* ditchin*( "hat should the rate of descent ,e urin* an en*ine fire on *round "ith the en*ine runnin* "hat should the
Cessna 152A
5
Academy of Carver Aviation Pvt. Ltd.
rpm ,e
Cessna 152A
6
Academy of Carver Aviation Pvt. Ltd.
What manoeuvre should one perform durin* "in* fireG 3tate "hether true or false- durin* "in* fire( land "ith flaps do"n What should the first step ,e durin* an inadvertent icin* condition encounter What should the airspeed ,e durin* a landin* approach in an icin* condition What should the first step ,e if the ammeter sho"s an excessive rate of chan*e
loop
side slip
true
false
turn ,ack or chan*e altitude
pull ca,in heat control full out
pitot heat s"itch on
none of the a,ove
C
65 to 5 kias
60 to 0 kias
0 to 80 kias
55 to 65 kias
A
nonessential electrical euipmentoff
none of the a,ove
fli*ht terminate as soon as practical
non essential electrical euipmentoff
alternator alternator circuit ,reaker off pull
face the "ind
roll
When an ammeter sho"s excessive rate of chan*e choose the incorrect alternative
alternatoroff
alternator circuit ,reaker push
What should the first step ,e if the lo" volta*e li*ht illuminates durin* fli*ht
alternator circuit ,reaker check in
master s"itchoff
alternatoroff
alternatoroff
What should the airspeed ,e "hen landin* "ithout elevator control
50 kias
55 kias
60 kias
65 kias
0:
10:
20:
%0:
C
attitude indicator
turn coordinator
directional indicator
none of the a,ove
60 seconds
%0 seconds
90 seconds
120 seconds
A
%00 to 500 ft.min
500 to 800 ft.min
500 to 00 ft.min
550 to 50 ft.min
55 kias
60 kias
65 kias
0 kias
keep hands off control "heel
none of the a,ove
What de*ree of flaps is used "hen landin* "ithout elevator control Which instrument should the pilot rel/ on "hen the vacuum s/stem fails in clouds While executin* a 180: turn in clouds "hen there is a vacuum s/stem failure( ho" lon* should it take What is the rate of descent durin* an emer*enc/ descent throu*h clouds What is the descent airspeed durin* an emer*enc/ descent throu*h clouds What is the first step durin* an emer*enc/ descent throu*h clouds
Cessna 152A
full full car,uretor rich heat mixture
7
Academy of Carver Aviation Pvt. Ltd.
adHust trimmer to normal fli*ht
use opposite aileron and rudder
throttle open
none of the a,ove
55 kias
60 kias
65 kias
0 kias
not permitted
prohi,ited
not approved
permitted
throttle idle
ailerons neutral
full opposite rudder
none of the a,ove
car,uretor icin*
spark plu* foulin*
ma*neto malfunction
none of the a,ove
car,uretor icin*
spark plu* foulin*
ma*neto malfunction
none of the a,ove
A
car,uretor icin*
spark plu* foulin*
ma*neto malfunction
none of the a,ove
C
oil pressure *au*e failure
oil relief valve failure
leak in the line to the *au*e
all of the a,ove
a vacuum s/stem failure
an en*ine failure
loss of h/draulic pressure
loss of rpm
overheat
evaporate the electrol/te
melt
,oth A and
What is the first step durin* a ,ail out
release seat ,elt and shoulder harness
pull emer*enc/ d rin*
unlatch door
none of the a,ove
C
What is the first step "hen "indshield dama*e has occurred
open the side "indo"s
reduce airspeed
open door
none of the a,ove
A
en*ine failure
loss in rpm
odour of ,urnin* insulation
increase in oil temperature
C
level altitude
nose do"n altitude
tail do"n altitude
none of the a,ove
A
normal procedures
performanc e
limitations
none of the a,ove
What is the first step durin* recover/ from a spiral dive What is the airspeed "hile recoverin* from a spiral dive li*ht into icin* condition is What is the first step in a spin recover/ What is the pro,a,le cause for a sli*ht en*ine rou*hness in fli*ht What is the pro,a,le cause for a *radual loss of rpm and eventual en*ine rou*hness What is the pro,a,le cause for a sudden en*ine rou*hness of misfirin* What is the pro,a,le cause for a drop in oil pressure( accompanied ,/ normal oil temperature What is the pro,a,le cause "hen a total loss in oil pressure is accompanied ,/ a rise in oil temperature What should happen to the ,atter/ if the char*in* rate "ere to remain in excess of the rate of char*e
What is the initial indication of an electrical fire What aircraft altitude should ,e used for landin* in icin* conditions What does section % deal "ith
Cessna 152A
8
Academy of Carver Aviation Pvt. Ltd. 4n temperatures near freeIin*( upto ho" man/ strikes of the primer ma/,e necessar/ rpm drop should not exceed <<<< rpm on either ma*neto or sho" *reater than <<<< rpm differential ,et"een ma*netos urin* an alternator check( it is prefera,le that <<<<< li*hts ,e used instead of <<<<<< li*hts What is the rpm ran*e "ith car,uretor heat off and mixture leaned to maximum rpm in po"er check ,efore take off ull throttle run ups over loose *ravel is especiall/ harmful to "hich of the follo"in* Jsin* 10 de*ree "in* flaps reduces the total distance over an o,stacle ,/ approximatel/ ho" much percent ;n a short field( "hat de*ree "in* flaps and an o,stacle clearance speed of ho" much kias should ,e used or the ,est com,ination of performance( visi,ilit/ and en*ine coolin*( speeds should ,e ho" man/ knots hi*her than the ,est rate of clim, 7eanin* is not recommended until a total of the follo"in* hours is accumulated 4n order to ensure proper settin* of the piston rin*s( the follo"in* should ,e done
Cessna 152A
2
%
+
1
125(50
50(125
125(100
125(5
A
taxi( landin*
landin*( taxi
stro,e( taxi
readin*( landin*
A
2%80 to 2550
2200 to 2550
2280 to 2%80
2180 to 2280
C
car,uretor
"in*s
propeller
air cooler
C
15
20
5
10
10: and 55 kias
10: and 5+ kias
20: and 60 kias
20: and 5+ kias
5 to 12 knots
10 to 12 knots
10 to 15 knots
5 to 10 knots
25 hrs
100 hrs
50 hrs
5 hrs
C
cruise at 5! po"er
ans #A$ and until a total of 50 hrs has accumula ted
ans #A$ and until a total of 25 hrs has accumulated
ans #C$ and it is applica,le to ne" en*ines as "ell
9
Academy of Carver Aviation Pvt. Ltd. o achieve the recommended lean mix fuel consumption fi*ures( the mix should ,e leaned until the en*ine rpm peaks and drops <<<<<<< to <<<<<<<
50 5 rpm
15 25 rpm
25 50 rpm
10 25 rpm
he stall "arnin* horn produces a si*nal <<<<<<< to<<<<<< knots ,efore actual stall is reached
05 10 knots
10 15 knots
0 05 knots
15 20 knots
A
or a short field landin* in smooth air make an approach at
6+ knots and 20 de*rees
60 knots and 20 de*rees
5+ knots and %0 de*rees
55 knots and %0 de*rees
C
4n a ,alked landin*( "in* flap settin* should ,e reduced to
10 de*rees
20 de*rees
%0 de*rees
none of the a,ove
18:C and :C
0:C and 20:c
18: and :
,oth and C are correct
A
6%)% d,
6%)6 d,
66)% d,
66)6 d,
C
immelmann
spiral dive
cu,an ei*ht
none of the a,ove
ailerons neutral
appl/ and hold rudder in the direction of rotation
throttle idle
as in A and C
,arrel roll
loop
snap roll
aileron roll
,arrel roll
loop
snap roll
aileron roll
A
105 knots
100 knots
115 knots
1%0 knots
C
Freheat is *enerall/ reuired "ith ;A ,elo" <<<<<< KC and recommended in temperature ,elo" <<<< KC he certified noise level for 152A at 160 l,) is A prolon*ed stall that results in a nose do"n rapid rotation of the aircraft follo"in* a helical path ollo"in* steps should ,e done to recover from a spin A %60 de*ree turn executed in a vertical plane A coordinated manoeuvre in "hich the aircraft is rolled %60 de*ree alon* the lon*itudinal axis of the aircraft =ntr/ speed for the ,arrel roll is
Cessna 152A
10
Academy of Carver Aviation Pvt. Ltd. A coordinated manoeuvre in "hich aircraft is rolled %60 de*ree alon* the lon*itudinal axis ,ut is ti*hter than the ,arrel roll An accelerated stall manoeuvre in "hich /a" from full rudder deflection produces
cu,an ei*ht
loop
snap roll
aileron roll
,arrel roll
loop
snap roll
aileron roll
C
=ntr/ to the snap roll is done at <<<<<<<< kias
105 knots
100 knots
80 knots
1%0 knots
C
<<<<< manoeuvre is approx) L of the normal loop and a divin* M roll in the opposite direction ,/ another L of a loop and M roll
cu,an ei*ht
loop
snap roll
aileron roll
A
Cu,an ei*ht is done at
+)0 to +)5 * at 115 knots
%)5 to +)0 * at 115 knots
+)0 to +)5 * at 1%0 knots
%)5 to +)0 * at 1%0 knots
immelmann
loop
cu,an ei*ht
vertical reversement
A
immelmann
loop
cu,an ei*ht
vertical reversement
60 0: at 80 knots
60 0: at 110 knots
50 60: at 105 knots
50 60: at 100 knots
A
25 ft approx
26 ft approx
25 ft 1 inch approx
26 ft 1 inch approx
C
Win* flap s/stem is
dou,le slot "ith maximum deflection of %0K
sin*le slot "ith maximum deflection of 10K
dou,le slot "ith maximum deflection of 10K
sin*le slot "ith maximum deflection of %0K
Wheel ,ase len*th is
55 inches
56 inches
5 inches
58 inches
Win* span "ith conical cam,er "in* tip and stro,e li*hts is
2+ ft 1 inch
%%ft + inches
%2 ft 8 M inches
%2 ft M inches
Win* area is
159 M s) ft
156 M s) ft
158 N s) ft
156 N s) ft
A
Avco 7/comin* 02%5&2C is
2%%)% cu) in displacement "ith 108 ,hp at 2550 rpm
2%%)5 cu) in displaceme nt "ith 108 ,hp at 2550 rpm
2%5 cu) in displacement "ith 108 ,hp at 2550 rpm
2%% cu) in displacement "ith 108 ,hp at 2550 rpm
he com,ination of a M loop follo"ed ,/ M roll he manoeuvre "hich is M snap roll from a steep turn in one direction to steep turn in opposite direction he entr/ speed for a vertical reversement is 'inimum turnin* radius of the airplane durin* taxi usin* differential ,rakin* and nose "heel steerin* is
Cessna 152A
11
A
Academy of Carver Aviation Pvt. Ltd. standard tanks 1% *al and 0)5 unusa,le maximum uarts minimum 6 uarts
standard tanks 26 *al and 1)5 unusa,le maximum uarts minimum + uarts
standard tanks 19)5 *al and 0)5 unusa,le maximum 6 uarts minimum + uarts
1200 ft
1260 ft
%10 nm in % hrs of time
standard tanks 19)5 *al and 1)5 unusa,le
A
maximum 6 uarts minimum 5 uarts
1%60 ft
1%+0 ft
%00 nm in %)10 hrs of time
615 nm in +)1 hrs of time
615 nm in 6)9 hrs of time
A
160 l,
165 l,
11%1 l,
5++ l,
C
7andin* performance minimum *round roll
25 ft
1%+0 ft
+5 ft
1200 ft
C
otal unusa,le fuel after a lon* cross countr/ of total fl/in* time of % hrs is
0)5 *al
0)5 litres
1)5 litres
1)5 *al
tric/cle t/pe "ith steera,le nose "heel
t"o main "heels havin* tire pressure of 21 psi
shock a,sorption ,/ tu,ular sprin* steel main landin* *ear
all the a,ove
none of the a,ove
C
aft of rudder ,ase
uel capacit/ in port "in* tank
;il capacit/ ake off performance "ith 50 ft o,stacle 'inimum ran*e "ith 5! po"er at 8500 ft) "ith standard tanks 3tandard "ei*ht of empt/ aircraft
he landin* *ear of aircraft is
10 ampere 5 ampere circuit circuit ,reaker ,reaker aft of main aft of landin* *ear elevator
15 ampere circuit ,reaker aft of aileron
if char*e volta*e reaches %1)5 volts #approx)$ en*ine produces maximum po"er at level
if char*e volta*e reaches 2+ volts #approx)$
if char*e volta*e reaches %0 volts #approx)$
if char*e volta*e reaches 12 volts #approx)$
A
en*ine is set at ,est mixture ratio
en*ine is ne" to set
en*ine failure
&ose "heel is turned ,/ a sprin*loaded steerin* ,un*ee
an arc of approx) 8)0K each side of centreline
an arc of approx) )K each side of centreline
an arc of approx) 8)5K each side of centreline
an arc of approx) 8)5K
C
'aHor en*ine accessories are
;B( A and > transceiver
first aid ,ox and fire extin*uisher
flap motor and trim ta,
starter( alternator( oil cooler
he "in* flap s/stem circuit protected ,/ he *round adHusta,le trim ta, is at he alternator control unit protected ,/ overvolta*e sensor "hich trips out the circuit at 4f total loss of oil pressure is accompanied ,/ a rise in oil temperature
Cessna 152A
12
Academy of Carver Aviation Pvt. Ltd.
'aHor en*ine instruments A34( 34 and are altimeter he aircraft en*ine is euipped "ith <<<<<<< car,uretor Jse of full car,uretor heat at full throttle "ill *ive 4*nitions and starter operation is controlled ,/ a rotar/ t/pe s"itch la,elled #clock "ise$
4( compass( clock
tachometer( oil temperature( oil pressure *au*es direct fuel inHection s/stem
ammeter and lo" volta*e li*hts
C
updraft( float t/pe
A
rpm remains unchan*ed
the value ma/ var/ up to 1000 rpm
off start r l ,oth
off r l ,oth start
fuel strainer and suppl/ direct to car,uretor
C
updraft( float t/pe fix Het extra rpm a,out 150 #approx)$
do"n draft( float t/pe fix Het loss of rpm a,out 150 #approx)$
off r l start ,oth
r l start ,oth off
he prime dra"s its fuel from
left fuel tanks and inHect c/linder intake ports
ri*ht fuel tank and suppl/ direct to car,uretor
fuel strainer
uel uantit/ meter is
electricall/ operated
h/draulicall/ operated
thermo sensor mechanicall/ t/pe operated
A
Airplane is euipped "ith
28 volts C electrical s/stem
2+ volts ,atter/ mounted on ri*ht for"ard fire"all
a ,elt driven 60 amp alternator
all the a,ove
he master s"itch is a t/pe
split rocker( left half is alt and ri*ht half is ,at
split rocker( left half is ,at and ri*ht half is alt
,oth half is ,at and alt
none of the a,ove
A
15)5 l,s).s ft at sea level CautionO remove ,efore movin* a.c
10)5 l,s).s ft at sea level CautionO remove ,efore fli*ht
10)5 l,s).hp at sea level CautionO remove ,efore en*ine start
15)5 l,s).hp at sea level
CautionO remove ,efore take off
C
he aircraft is certified for follo"in* fli*ht operations A? &4> as of date of ori*inal B 4B air"orthiness certificate
A? &4> B ;&7?
A? &4> D 4B ;&7?
AW& J3 B 4B
A
Centre of *ravit/ ran*e #front face of fire "all as reference datum$
aft %6)5K at all "ei*hts
aft %6)0K at all "ei*hts
aft %5)5K at all "ei*hts
aft %5)0K at all "ei*hts
A
Fick the odd one out
'ax) ramp "ei*ht 165 l,s
'ax) landin* "ei*ht 160 l,s
'ax) useful load 11%1 l,s
sae 50
sae 60
C
Win* loadin* of aircraft is
;n control lock its printed
Jse multiviscosit/ oil at all temperatures a,ove
Cessna 152A
sae %0
'ax) ,a**a*e "ei*ht 120 l,s sae +0
13
Academy of Carver Aviation Pvt. Ltd.
60K What is the s/m,ol for minimum stead/ fli*ht at "hich the aircraft is controlla,le in the landin* confi*uration at most for"ard c) *) he point at "hich an aircraft or euipment "ould ,alance if suspended( its distance from reference datum is found ,/ dividin* the total movement ,/ total "ei*ht of aircraft
va
vno
vs
vso
c)*) arm
arm
station
centre of *ravit/
&ever exceed speed in an/ operations #kias$
12 kts under 43A conditions
125 kts under 43A conditions
1+9 kts under 43A conditions
168 kts under 43A conditions
A
'ax) speed "ith flaps do"n #extended$ kias
85 kts
8 kts
108 kts
125 kts
A
12512 kias onl/ in smooth air
+0125 kias onl/ in nil "ind conditions
+0125 kias onl/ in smooth air
+)55)+ in h* in maximum limit of red arc
+)55)+ in h* in normal limit of *reen arc
+)55)+ in h* in normal limit of "hite arc
C
?ello" arc speed operation must ,e conducted "ith caution and 3uction *au*e reads in
12512kias onl/ in nil "ind conditions +)55)+ in h* in minimum limit of /ello" arc
White arc of A43 starts from
vso vfe
vso vs
va vso
does not have a limit
A
'aximum oil temperature ran*e is
118: C
108: C
180: C
80: C
A
4nvert fli*ht is prohi,ited
due to hi*h "in* construction and *ravit/ feed fuel s/stem
due to fixed pitch propeller and conventiona l car,uretor
it is not prohi,ited ,ut not approved due to *ravit/ feed fuel s/stem and conventional car,uretor
due to "et sump of oil and actual minimum + uarts of oil is al"a/s reuired
C
he structure meet or exceeds desi*n load ,/ 150! of fli*ht load factor
flap up P % * to Q%)5 *
flap up P % * to Q6)0 *
flap do"n P % * to Q6)0 *
flap do"n P % * to Q%)5 *
010 de*ree other then landin* confi*uration
1020 de*ree other then landin* confi*uratio n
20%0 de*ree other then landin* confi*uration
none of the a,ove as use of flap durin* aero,atics is strictl/ prohi,ited
Jse of flap is restricted in aero,atics fli*ht up to a limit of
Cessna 152A
14
Academy of Carver Aviation Pvt. Ltd. 4n case of en*ine failure durin* take off role( application of full
throttle is reuired
flaps are reuired
,rakes are reuired if alternator is "orkin* and electrical load in excess the output of alternator( ammeter sho"s ,atter/ dischar*e rate lo" volta*e li*ht "ith ammeter dischar*e ,oth lo"
mixture is to ,e rich
C
all a,ove options are correct
lo" vacuum li*ht "ith lo" volta*e
he ammeter indicates the amount of current in amperes from
alternator to ,atter/
,atter/ to the aircraft electrical s/stem
urin* lo" rpm condition
lo" volta*e li*ht "ill illuminate
ammeter indicates dischar*e
electrical circuits in Cessna 152A aircraft is protected ,/
push to restart t/pe
pull off t/pe
,oth
none of the a,ove
C
he stall "arnin* s/stem of this aircraft is euipped "ith a stall "arnin* s/stem that is
pneumatic t/pe "hich sounds "arnin* at 5 10 kts a,ove stall "arnin* s/stem
electric t/pe "hich indicates stall "arnin* ,/ li*ht
,oth this s/stem "orks to*ether
none of the a,ove
A
7andin* "ithout elevator control reuire
trim for vertical fli*ht ,/ throttle and elevator trim
trim for horiIontal fli*ht ,/ throttle and elevator trim
trim aircraft ,/ usin* desired flap settin*
aircraft cannot ,e controlled "ithout elevator
continue crankin*- fire "ill "hip out of its o"n
shut do"n en*ine
continue crankin* to *et a start( then po"er to 100 rpm and then shut do"n the en*ine
continue crankin* the en*ine till it starts
C
60 0 kts
0 80 kts
60 55 kts
50 55 kts
C
appl/ ,rakes
cut throttle
cut mixture
fuel shut off valveoff
=n*ine fire durin* fli*ht
mixture idle cut off
fuel flo" valve to ,e off
throttle to idle
;pen "indo"s and inspect first
A
What topics does section 8 cover
handlin* and service mainte nance
emer*en cies
*eneral
limitations
A
urin* start on *round( if fire occurs from en*ine
orced landin* "ith en*ine po"er( airspeed must ,e =n*ine failure durin* take off roll( first action ,/ F4C is to
Cessna 152A
15
Academy of Carver Aviation Pvt. Ltd.
What information is displa/ed on the identification plate of the aircraft
o"ners name and address
serial no) model no) production certificate no) R t/pe certificate no
Where is the identification plate located
outside left door on fusela*e
on fire"all at rear of en*ine
manufacturers name and address
ca,in floor ,elo" the on instrument left rear corner panel of pilotSs seat )
none of the a,ove
C
air"orthiness certificate ( re*istration certificate ( a.c radio station license
What is to ,e displa/ed on the aircraft at all times
fuel consump tion
fli*ht plan
address of air"orthiness office
What is to ,e carried on the aircraft at all times
pilotSs operatin* hand,ook( "ei*ht and ,alance euipment list
operations manual
ualit/ assurance manual
none of the a,ove
A
certificate of air"orthiness
airplane lo*,ook( en*ine lo*,ook
certificate of re*istration
"ei*ht schedule
%0T either side of centre
+5T either side of centre
60T either side of centre
90T either side of centre
A
fli*ht release certificate
rudder lock
pitot cover
certificate of re*istration
head into the "ind
,roadside facin* "ind
C
,/ appl/in* pressure on the elevators
none of the a,ove
A
What can ,e availa,le on reuest While to"in* ( "hat an*le of nose *ear should not ,e exceeded "hile turnin* What should ,e removed from the aircraft ,efore to"in* With respect to the "ind direction ( ho" should the aircraft ,e parked While pushin* the tail cone ( ho" can ,ucklin* of the skin ,e avoided What levellin* is accomplished ,/ placin* the levellin* scre"s on stations 9+)6% R 1%2)9% 7on*itudinal levellin* can ,e accomplished ,/ placin* the levellin* scre"s on stations <<< R <<<
Cessna 152A
tail into the "ind ,/ appl/in* pressure on ,ulkhead
irrespective of "ind direction ,/ steerin* nose "heel throu*h %0K onl/
horiIontal levellin*
lon*itudinal levellin*
vertical levellin*
three dimensional levellin*
9+)6% R 1%2)9+
95)6% R 1%%)9+
9+)6% R 1%%)9+
95)6% R 1%2)9+
A
16
Academy of Carver Aviation Pvt. Ltd. or ho" man/ da/s can the aircraft ,e stored in non operational condition ;n ever/ th da/ of stora*e( ho" man/ times should the propeller ,e rotated ,/ hand
%0 da/s
60 da/s
90 da/s
+5 da/s
A
10 revolutions
25 revolutions
5 revolutions
15 revolutions
C
What are the oil specifications
'477608% '47722851
'4776082 '477 22851
'4776082 '47722852
'477602 '47722851
he aircraft should not ,e operated "ith less than <<<< uarts of oil
+
8
6)5
5
6
+
8
A
5
6
+
onl/ at overhaul
C
or normal fli*hts of less than % hrs( ho" man/ uarts of oil is reuired or extended fli*hts of more than % hrs( ho" man/ uarts of oil is reuired When should the oil chan*e ,e made
ever/ 100 hours
never
1st chan*e after 25 hrs ( then after ever/ 50 hrs
After "hat time duration should the oil filter ,e chan*ed
% months
6 months
9 months
at en*ine overhaul
A and UF5
100ll *rade aviation fuel #,lue$( 100.1%0 *rade aviation fuel # *reen$)
UF5( UF and mo*as
C
What are the approved fuel *rades
100ll and A
<<< R <<< can ,e added to fuel suppl/ in uantities less than 1! to 15 ! ,/ volume
fuel should not ,e adulterated
mo*as
UF5 and UF
isoprop/l alcohol or eth/lene *l/col monometh/l ether
What is the capacit/ of standard fuel tanks
15 *allons
1% *allons
29 *allons
20 *allons
What is the capacit/ of lon* ran*e tanks
25 *allons
19)5 *allons
1% *allons
20 *allons
What is the antiicin* fluid called
'475566
='=
'47>5606
none of the a,ove
A
With "hat apparatus can the concentration of "ater ,e checked
inclinometer
chamois leather
differential refractometer
differential pressure *au*e
C
What is the nose "heel tire pressure
20 psi
21)5 psi
%0 psi
25 psi
C
Cessna 152A
17
Academy of Carver Aviation Pvt. Ltd.
'ain "heel tire pressure
25 psi
21 psi
%0 psi
25)% psi
What is the ,rake fluid *rade
"120
"100
milh5606
none of the a,ove
C
kerosene
stoddard solvent
100ll
petrol
isoprop/l alcohol
kerosene
petrol
turpentine
A
What are the replacea,le door post map li*ht ,ul, num,ers
322+%1 R 322+%2
322+21 R 322+%2
322+%1 R 322+22
322++1 R 322+%2
A
What topic does section 9 cover
limitations
3upple ments
*eneral
emer*enc/ procedures
What is the t/pe of clock installed in the Cessna 152A
titan uartI
rolex chrono meter
astro teach 7C2 uartI chronometer
none of the a,ove
C
>o" is the intensit/ of the ,ackli*ht of the clock controlled
push pull s"itch
radio lt rheostat
5 amp circuit ,reaker
10 amp circuit ,reaker
What is displa/ed "hen operatin* in the clock mode
time of da/ in hours and minutes
date and time of da/
time of da/ in hours( minutes and seconds
none of the a,ove
A
At "hat intervals does the colon ,link
15 seconds
10 seconds
1 second
1)5 seconds
4n ho" much time does the clock mode return from the date displa/ mode automaticall/
1 second
1)5 seconds
2)5 seconds
15 seconds
Jsin* "hich ,utton on the aircraft clock can the timer ,e set to S0S
ri*ht hand ,utton
upper ,utton
left hand ,utton
centre ,utton
C
Where is the *round service plu* receptacle located
,ehind a door adHacent to the fire"all on the left side of the upper co"l
,ehind a door adHacent to the fire"all on the ri*ht side of the upper co"l
,et"een the pilot and copilot seats
at location 5%0
A
C
;il and *rease stains can ,e removed ,/ What "ill remove ice accumulation satisfactoril/ "ithout dama*in* paint
4s usin* a *round service plu* receptacle recommended for char*in* a dead ,atter/
/es
no
onl/ in cold "eather
onl/ after rotatin* the propeller 5 times
Where is the stand,/ vacuum pump located
under the co"l aft of the starter
next to the fuel drain plu*
mounted aft side of fire"all ,ehind instru ment panel
there is no stand,/ vacuum pump
Cessna 152A
18
Academy of Carver Aviation Pvt. Ltd.
4s 4B fli*ht recommended "ith an inoperative en*ine driven vacuum pump At "hat altitude does the suction *au*e indicate ,elo" +)5 in) h* and is still normal and operational At "hat temperature should the "interiIation kit ,e installed When is the =7 activated
no
/es
onl/ "hen clearance is o,tained from the control to"er
15(000 ft
1+(00 ft
10(000 ft
1%(000 ft
A
,elo" 20KC
,elo" 10K
,elo" %0K
,elo" 20K
impact of 1*
impact of 5* and a,ove international distress freuencies of 2+%)0 '>I) or 121)5 '>I
durin* a steep turn
"hen exceedin* vne
the freuenc/ currentl/ in use
on all militar/ freuencies
"ith special permission A from the CA
What freuencies does the =7 operate on
an/ preset freuenc/
What is the ran*e of transmission of the =7 follo"in* a crash landin*
100 miles at 10(000 ft
10 miles at 5(000 ft
50 miles at 5(000 ft
100 miles at 5(000 ft
A
What is the po"er output and for ho" much time does the =7 transmit
25 m") rated po"er output( +8 hrs
5 m") rated po"er output( +8 hrs
5 m") rated po"er output( 2+ hrs
15 m") rated po"er output( %6 hrs
C
What is the temp ran*e of transmission of the =7
10KC to 25KC
0KC to 100KC
20KC to 50KC
+KC to 1%1K
red( under pilots seat
/ello"( on the for"ard ,ulk head
,lack( alon* "ith the first aid kit
A
200 k>I to 1699 k>I
200 k>I to 500 k>I
50 k>I to 00 k>I
receiver( ,earin* indicator and sense antenna 118)000 to 1%5)95 '>I) in 50 k>I steps
receiver( ,earin* indicator( loop antenna( sense antenna
receiver and ,earin* indicator
C
118)000 to 1%5)95 '>I) in 5 k>I steps
118)000 to 1%5)95 '>I) in 5 k>I steps
A
What colour is the =7 unit and "here is it installed What is the freuenc/ ran*e of the A
,ri*ht oran*e( ,ehind ,a**a*e compartment "all in tail cone 100 k>I to 1000 k>I
What is the s/stem of the A comprised of
receiver( ,earin* indicator and loop antenna
What is the operational ran*e of nav.com
118)000 to 1%5)95 '>I) in 25 k>I steps
Cessna 152A
19
Academy of Carver Aviation Pvt. Ltd. et"een "hat freuencies does the navi*ation receiver receive si*nals
108)00 to 11)95 '>I in 25 k>I steps
;n "hat freuencies does the transponder transmit and receive si*nals on
transmits on 10%0 '>I and receives on 1090 '>I
What is the no) of channels the *lide can receive 473 *lide slope si*nals
+0 channels
What is the spacin* ,et"een channels and operational ran*e of the *lide slope
spacin* 250 k>I apart( ran*e %29)15 to %%5 '>I
When is the *lide slope indicator unusa,le A,ove "hat altitude is the transponderSs altitude reportin* capa,ilities availa,le
"hen 3 fla* is visi,le or *lide slope is off a,ove 5000 ft) and in 100 ft) increments
108)00 to 11)95 '>I in 50 k>I steps transmits on 1000 '>I and receives on 10%0 '>I %0 channels spacin* 100 k>I apart( ran*e %29)15 to %%5 '>I "hen circuit ,reaker pops out a,ove 1000 ft and in 100 ft increments formed sheet metal ri,s R Vv t/pe corru*ated aluminium skin Hoined to*ether at the leadin* ed*e
108)00 to 11)95 '>I in 5 k>I steps
108)00 to 11)95 '>I in 5 k>I steps
transmits on 1090 '>I and receives on 10%0 '>I
transmits on 900 '>I and receives on 10%0 '>I
C
20 channels
10 channels
A
spacin* 150 k>I apart( ran*e %29)15 to %%5 '>I
spacin* 150 k>I apart( ran*e %00 to %50 '>I
C
indicator never fails
none of the a,ove
A
a,ove 1000 ft and in 1000 ft increments
a,ove 10(000 ft and in 100 ft increments
contain ,alance "ei*hts
none of the a,ove
C
'ark the correct statement re*ardin* ailerons
the/ are dou,leslotted
What effect "ill the for"ard motion of the trim "heel have
have no effect
trim nose up
trim nose do"n
cause aircraft to /a"
C
/rooperated fli*ht instruments are
arran*ed side ,/ side to left of control column
side ,/ side sli*htl/ to the ri*ht of control column
one a,ove another sli*htl/ to the left of control column
one a,ove another sli*htl/ to the ri*ht of control column
C
left
ri*ht
a,ove
A
Avionics euipment are stacked approx on<<<
Cessna 152A
20
Academy of Carver Aviation Pvt. Ltd. achometer( ammeter( econom/ mixture indicator and additional instruments are on the<<<<
left
ri*ht
centre
lo"er half
&ose "heel can ,e turned ,/ a to" ,ar ,/
%0 de*rees
15 de*rees
20 de*rees
+5 de*rees
A
8)5( %0
%0( 8)5
25( )5
)5( 25
A
25 feet 1 inch
%0 feet 2 inches
25 feet 2 inches
10 feet 2 inches
A
ans #A$ and deflection of 10K up R 20K do"n
ans #$ and deflection of %0K
When rudder pedals are pressed the nose "heel turns throu*h an arc of approx) <<<< and "hen ,rakes applied<<<<< 'inimum turnin* radius of the airplane is Win* flaps are
dou,le slotted
sin*le slotted
Win* flap s/stem is protected ,/ a<<<<
15 amp
25 amp
10 amp
%0 amp
A
he airplane has<<<<<,rake s/stem
h/draulicall/ actuated
pneumatic
air pressured
none of the a,ove
A
A control lock is provided to prevent dama*e caused ,/ "ind ,uffetin* "hen the aircraft is parked to the
ailerons onl/
ailerons R elevator
rudders R elevators
rudders R ailerons
'aHor en*ine accessories include
elevator( rudders R ailerons
tachometer( car,uretor R ammeter
none of the a,ove
C
tachometer is cali,rated in 100 increments
ans #A$ R is en*ine mechanical driven
starter( ,eltdriven alternator R oil cooler ans #$ R indicates en*ine and propeller speed
ans #C$ R maximum speed of 2550 rpm
start,othlr off
offlr,oth start
offrlstart ,oth
offrl,othstart
rise in rpm ,/ approx) 50
loss in rpm ,/ approx) 150
loss in rpm ,/ approx) 50
rise in rpm ,/ approx) 150
updraft( float t/pe R idle cutoff mechanism
fixed Het( pneumatic t/pe
,oth
all are correct
A
'ark the most correct statement 4*nition starter s"itch is la,elled Jse of full car,uretor heat at full throttle "ill cause Car,uretor is of the t/pe
Cessna 152A
21
Academy of Carver Aviation Pvt. Ltd.
=n*ine is cooled ,/
ram air
en*ine cooler
avionics fan
all the a,ove
A
Fropeller of the aircraft is
sin*le,laded( fixed pitch( t"opiece for*ed aluminium propeller
t"o,laded( fixedpitch( onepiece for*ed aluminium propeller
t"o,laded( varia,le pitch( onepiece for*ed aluminium propeller
none of the a,ove
=lectrical s/stem of the airplane consists of
28 volt C and 2+ volt ,atter/
2+ volt C and 28 volt ,atter/
ans #A$ and ,elt driven alternator of 15 amp
Ans #$ and ,elt driven alternator of 60 amp
A
7o" volta*e li*ht illuminates
ammeter sho"s dischar*e
under lo" rpm R ammeter sho"s dischar*e
due to excess volta*e on the ,atter/
all the a,ove
he colour of the lo" volta*e li*ht is
flashin* *reen
series of /ello" flashes
red
"hite
C
=lectrical circuits are protected ,/
pushtoreset t/pe
pulloff t/pe
,oth
none of the a,ove
C
Badio lt controls
intensit/ of the radio li*hts
intensit/ of instrument R panel li*hts
all are "ron*
C
Fitot heat s"itch is protected ,/ a
60 amp alternator
15 amp circuit ,reaker
flip s"itch
C
4f the vacuum s/stem fails( then the */ro instrument that "ill still operate
turn R slip coordinator
suction *a*e
artificial horiIon
A
lo" vacuum in the suction *au*e
lo" rpm conditions
+)0 inches h*
+)1 inches h*
C
Q5* to Q10*
0 to Q10*
7o" vacuum li*ht indicates
ammeter sho"s dischar*e
3uction *au*e "ill read<<<<
+)5 inches h*
Accelerometer is cali,rated from
5* to Q5*
Cessna 152A
intensit/ of static interference in radio 5 amp circuit ,reaker directional indicator lo" vacuum condition existin* in the vacuum s/stem +) inches h* 5* to Q10*
22
Academy of Carver Aviation Pvt. Ltd.
Cessna 152A
23
