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C172R by me > Quick Rev > Flashcards

Quick Rev Flashcards

1
Q

MAX RAMP WT FOR NORMAL CATEGORY A/C is

And for UTILITY CATEGORY is

A

For normal
2457lbs

For utility
2207lbs

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2
Q

WITH THE ALTERNATOR SIDE OF MASTER SWITCH OFF MAX COMPASS DEVIATION MAY OCCUR UPTO

A

25deg

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3
Q

MAX SLIP OR SKID DURATION WITH ONE TANK DRY is

A

30 sec

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4
Q

TEMP DECREASES BY ______ FOR EACH 1000ft ALTITUDE

A

2deg Celsius per 1000ft alt

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5
Q

MAX OIL PRESSURE is

A

115 psi

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6
Q

MAX WINDOW OPEN SPEED in KIAS is

A

163 KIAS

160 KCAS ( additional fact )

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7
Q

MAX TURNING RADIUS (pivot pt to outbound using tip)

A

27feet 5.5inches

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8
Q

UNUSABLE FUEL QUANTITY IN EACH TANK is

A

1.5 gallon

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9
Q

MAX VENTILATION CAN BE ACHIEVED BY

A

Cabin air knob pull out and
Cabin heat knob is pushed in

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10
Q

In voltmeter /OAT operation/ CLOCK by pushing the upper control button will sequence the window from

A

E-F-C-E
( empty full centre empty)

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11
Q

PROP GROUND CLEARANCE

A

11feet 1/4th inches ie 11.25inches

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12
Q

Ignition operation is controlled by a rotary switch which is labeled

A

Right, left , both, start

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13
Q

BEST FUEL ECONOMY CAN BE ACHIEVED AT

A

OPERATION AT PEAK EGT

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14
Q

Weak intermittent firing followed by puffs of black smoke from the exhaust stock indicates

A

Over priming

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15
Q

WHEN SHOULD FUEL EXAMINATION FOR CONTAMINATION AND GRADE BE DONE

A

1) Before first flight of each day
2) after refuelling

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16
Q

Oil Px gauge marking indicates

A

Red line for minimum permissible idling pressure

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17
Q

VSI indicates airplanes ____

A

ROC or ROD in ft per min

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18
Q

There was obvious power loss when ignition switch was momentarily turned from “both” to “L” position. The cause is____

A

LEFT magneto problem

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19
Q

To apply parking brakes what all steps are to be followed

A

1) Set the brake with rudder pedal
2) pull the handle aft
3) rotate the handle 90 deg down

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20
Q

The engine driven vacuum system provides the

A

Suction necessary to operate

directional indicator and attitude indicator

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21
Q

Centre area of instrument panel contains ___

A

Static px alternate source valve

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22
Q

_____ of ldg gear is of ____ shock strut

A

Nose
Air/oil

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23
Q

Colour of 100LL grade aviation fuel is

A

BLUE

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24
Q

DiEGME( Diethyl glycol monomethyl ether) mixed w fuel tot fuel volume in concentration is b/w ??

A

0.10% to 0.15%

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25
Q

ELT enunciator illuminates when rocker switch in cockpit is placed to ____

A

Forward position

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26
Q

Left rudder pedal pressed to left side so nose wheel can be turned to ____ deg max

A

10deg max

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27
Q

Avionics eqpt 3 points

A

The aviation cooling fan operates when avionics power switch is put on.

Volume and output of overhead speaker is controlled through the audio selector .

Avoid covering opening on back side of microphone for optimum noise cancelling

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28
Q

An open alternate air door will result in an approx ____ power loss at full throttle

A

10% power loss

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29
Q

To permit heavier cabin loading filling of usable fuel in each tank must not be less than ____

A

17.5 gallons

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30
Q

Yellow arc on ASI reponds to ___

A

129 to 163 kts (smooth air)

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31
Q

Abrupt use of controls is prohibited above ___

A

99kts

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32
Q

The digital clock / OAT is tested by ___

A

Holding control button for 3 sec

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33
Q

Audible stall warning horn comes at ____

A

5-10 kts above stall in all flight conditions

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34
Q

In pitot/ static system of the static system becomes blocked what will happen to the ASI

A

ASI will still function but will give erroneous readings

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35
Q

Carburettor ice is detected by ___

A

1) Drop in engine RPM in fixed pitch propeller aircraft

2) drop in manifold Px in constant speed prop a/c

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36
Q

To improve engine cooling in en route climb, a short duration climb can be made at what V speed and

at what engine power

A

Vy - best rate of climb speed

Until engine has accumulated 50hrs or 80% of engine power

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37
Q

Vy at sea level with max weight of 2450lbs

A

79KIAS

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38
Q

Recommended starter duty cycle is

A

10sec on
20sec off
Max 3 times
10min gap for cooling
Repeat 3 times

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39
Q

During engine starting, if engine floods what should be done

A

Mixture in idle cut off

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40
Q

3 statements of compass

A

A knob on the lower left edge of the instrument is used to adjust the compass card

A compass card must be readjusted on extended flights and

a knob on the lower right edge of the instrument for the heading bug

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41
Q

The transmitter of bendix /king XX 155 Anav/comm system stops transmitting if microphone is keyed continuously for greater than ___ sec

A

33 sec

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42
Q

Flap switch level mechanical stops are provided at

A

10,20 and 30deg positions

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43
Q

Red oil Px illuminates when Px is below ___ psi

A

20psi

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44
Q

Annunciator located above altimeter provides caution and warning msgs for ?

A

Fuel quantity
Oil Px
Low vaccum
Low voltage situation

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45
Q

Alternator must be switched off manually if voltage indicates beyond ____V

A

31.5V

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46
Q

In every cold wx condition after starting the engine , if oil Px gauge does not read Px within _____ sec then stop the engine and investigate

A

Within 60 sec

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47
Q

Max airspeed and altimeter variation over the normal operating range window(s) closed and alternator switched off is ____ & _____??

A

4knots
30ft

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48
Q

To apply parking brakes

A

Set brake with rudder paddle
Pull handle aft
Rotate 90deg down

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49
Q

____ is not marked on each side of the central marking of an attitude indicator

A

40deg

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50
Q

In long flt which is the maximum deviation in compass for precession error

A

30 deg max deviation

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51
Q

ELT annunciator does not activate on ____

A

Low fuel flow

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52
Q

In the event of alternate static door open what will be the margin of error in ASI

A

ASI will give error of 7kts

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53
Q

Min oil Px of a/c

A

20psi

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54
Q

DGI (or compass) has to be aligned regularly on long flights for ___

A

Precession

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55
Q

Compass error upto 25deg may come in the event of alternator ____

A

Switched off

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56
Q

MIN AND MAX oil quantity for extended flights is

A

MIN 5 quarts
fill upto
MAX 8 quarts

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57
Q

Conc of isopropyl alcohol ___

A

1%

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58
Q

Which oil is to be used after 50 hrs of engine running or when the oil consumption has been stabilised

A

MIL- L -22851
&
SAE J1899 aviation grade ash-less dispersant oil

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59
Q

Max deflection of nose wheel by use of rudder paddle on ground is ___

A

10deg to either side

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60
Q

Mechanical stops on flaps are at____

A

10deg
20deg
30deg

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61
Q

Shock absorption on nose wheel

A

Air and oil system

62
Q

(Vy) Best rate of climb speed at sea level is

A

79 knots

63
Q

Shock absorption on main wheel___

A

tubular spring

64
Q

Min turning radius during taxi using differential braking and nose wheel steering ___

A

27feet

65
Q

If engine floods
Right 3 steps for course of action

A

Turn off auxiliary fuel pump and place mixture in idle cut off

Open half throttle and crank engine when engine fires

Advance mixture to fuel rich and retard throttle properly

66
Q

Starter cycle for engine is

A

10sec ON
&
3times and then 10min gap for cooling to be given

67
Q

Enroute climb speed is 5 to 10kts above best rate of climb speed for ___

A

Best visibility
Best performance
Best cooling

68
Q

Until 50hrs has been accumulated engine should be run at ___

A

80% power on cruise

69
Q

Nose gear shock strut pressure

A

45 psi

70
Q

OAT/volt gauge select switch may be used by putting the select button down off

A

3 sec to start

71
Q

If the PTT button of microphone is kept pressed more than 33 sec in continuous then the transmission is ___

A

Automatically terminated

72
Q

Max fuel capacity of each tank is

A

28 US GALLONS

73
Q

Spark plug fault causes

A

Loss of RPM

74
Q

Magneto malfunction causes

A

Misfiring

75
Q

Brake of A/C model

A

MIL-H-5606

76
Q

Tyre Px of nose wheel tyre

A

34 psi

77
Q

Tyre Px of main wheel tyre

A

29 psi

78
Q

Nose wheel strut length

A

2 inches

79
Q

Propeller diameter

A

75 inches

80
Q

Engine model number

A

IO - 360- L2A

81
Q

Std empty wt of a/c

A

1639 lbs

82
Q

Baggage compartment contains

A

Compartment 1 has allowance of 120lbs (fwd)

Compartment 2 has allowance of 50 lbs (aft)

Tot baggage compartment allowance is 120 lbs (combined)

83
Q

Max useful load of a/c

A

818 lbs (NORMAL CATEGORY)

And for utility category = 564 lbs

84
Q

Wing loading of a/c

A

14.1 lbs / sq ft

85
Q

Power loading of a/c

A

15.3 lbs /Hp

86
Q

Wing area of A/c

A

174sq ft

87
Q

Elevator span of a/c

A

11 ft 4 inches

88
Q

Wheel base length of a/c

A

65 inches

89
Q

Max Horse power rating and engine power ( RPM)

A

160BHP
2400 RPM

90
Q

Prop model no. of a/c

A

IC235/LFA7570

91
Q

Airspeed when ENGINE FAILS after t/o

A

Flaps up 65 KIAS
Flaps down 60KIAS

92
Q

Landing with a flat main tyre , flaps will be ___

A

30deg

93
Q

Landing with a flat nose tyre, flaps will be ___

A

As required

94
Q

Engine failure during t/o roll the first action will be

A

Throttle idle

95
Q

If fire occurs during start on ground the throttle and mixture will be ___

A

Throttle full open
Mixture idle cut off

96
Q

Magneto check should be made at ___

A

At 1800RPM

97
Q

Descending through clouds to go around against spiral dive and due to changing bank angle what to do to minimise compass card swings ?

A

Choose an easterly hdg
&
Choose a westerly hdg

98
Q

A/c is equipped with DC electrical system of ?

A

28Volt DC ie direct current electric system

99
Q

Electrical system of a/c is powered by

A

34 V , DC electrical system

100
Q

Desired vacuum range of a/c is

A

4.5 to 5.5 inches of mercury

101
Q

Communication receiver transmitter receives and transmits signals b/w

A

B/w 118.06 and 136.972MHz with 25Hz spacing

102
Q

Nav receiver receives VOR and localiser signals

A

B/w 108 and 117.95MHz in 50KHz steps

103
Q

Aircraft has ____ clock model

A

The davtron model 803 digital clock

104
Q

Clock of a/c combines the feature of
___, ____ and _____

A

A clock
OAT gauge
Voltmeter

105
Q

T/o speed for normal climb

A

70-80 KIAS

106
Q

Enroute climb at sea level airspeed is

A

75-85 KIAS with flaps UP

107
Q

Engine manufacturer of a/c

A

Textron Lycoming

108
Q

Engine type of a/c

A

Four cylinder engine
Horizontally opposed
Fuel injection
Air cooled

109
Q

MIL-L-6082 or SAE J1966 aviation grade straight mineral oil is used

A

To replenish the supply during first 25hrs
&
Use until total of first 50 hrs

110
Q

At 10,000ft best angle of climb speed

A

65 KIAS

111
Q

Max oil temp in Celsius and Fahrenheit

A

118 deg Celsius
245 Fahrenheit

112
Q

Landing apch speed

A

Normal apch speed at 65-75 KIAS FLAPS UP

FLAPS DOWN 30deg at 60-70 KIAS

short field apch Flaps FULL (62KIAS)

113
Q

Max flap extended speed of a/c

A

110 kias for 10 deg flaps
&
85 kias for 10deg to 30 deg flaps

114
Q

Vne of a/c

A

160kcas or 163kias

115
Q

Max structural cruising speed of aircraft

A

126 KCAS or 129 KIAS

116
Q

While ditching transmit mayday on _____ giving location and intention and squawk ____

A

121.5MHz
Squawk 7700

117
Q

The set of radio contains

A

760 channels of VHF comm receiver
200 channels of VHF nav rcvr

118
Q

Which of the following statement is incorrect
A) No aerobatic maneuvers approved
B) Acrobatic maneuvers approved
C) DAY – NIGHT – VFR – IFR approved
D) Flight into icing condition prohibited

A

D) Flight into icing condition prohibited

119
Q

If alternator shuts down due to over-voltage, when will
you
restart it?

A

only on ground

120
Q

Full flowmeter range
and Cruising full flow

A

0 to 11 gph ie gallons per hr (GREEN ARC)

and
5.6 to 9.3 gph depending on ht , power and oat

121
Q

The VSI testing ELT, what will you

do with the rubber arm?

A

press forward ON
press backward RESET

122
Q

aircraft tyres are ___ ply rated.

A

6 ply rated

123
Q

Pitot-static system provides pressure to ____ & static to ___, ___, ___.

A

pitot static to ASI

static to ASI
VSI
ALTIMETER

124
Q

when flying through clouds at night or when____ or ____ are ON, it can cause vertigo and loss of orientation

A

flashing beacon or lights

125
Q

Dimensions in terms of
Length
Wing span
Height

A

Length 27ft 2 inches
Wing span 36 ft 1 inch
Height 8ft 11 inches

126
Q

Service ceiling

A

13,500ft

127
Q

Stall speed
FLAPS UP
POWER OFF and

FLAPS DOWN
POWER OFF

A

51KCAS FLAPS UP power off

47KCAS FLAPS DOWN power off

128
Q

Cruise 80% power
Airspeed and
Range

A

122 kts
580Nm

129
Q

SAE stands for

A

Society of automotive engineers

130
Q

Speed fairing inc speed of a/c by ____

A

2kts

131
Q

Max t/o and ldg wt for normal ops and for utility category

A

For normal = 2450lbs
For utility = 2200lbs

132
Q

Attitude indicator bank marking at an increment of ___

A

10,20,30,60,90 degrees

133
Q

ELT is operated by ____ and ____

A

Control panel and forward fairing/facing

134
Q

Beta rays fit fine

A

thrust reverse

135
Q

In case of engine fire in flt,
_____ kts airspeed is advised to maintain

A

100kts

136
Q

In case of ditching
Flap setting
Apch speed
ROD
is advised to mntn

A

Flap setting 20 deg
ROD 300 fpm
Apch speed 55kts

137
Q

In case of flames from left fuel tank, side slip to ____

A

Right

138
Q

With ice accumulation of _____ on wing leading edges, be prepared for significant
high power requirement, high approach speed and high stall speed.

A

0.25inches or more

139
Q

Fuel saving procedure for flight training operations provide fuel saving in excess of ___ when compared
to mixture rich operations.

A

5%

140
Q

Operating at peak EGT provides best fuel economy, results in ___ greater range and ___ decrease
in speed.

A

4% greater range
3kts dec in speed

141
Q

Low vacuum annunciatorshows in Amber light twhen vacuum pressure drops below ___

A

3.4 inch of Hg

142
Q

digital display of annuciator shows red colour annunciator in tachometer when rpm exceeds___ and indicates engine speed more than the limit

A

2472 rpm and above

143
Q

Max. Limit range of float travel _____to indicate fuel remaining in tanks

A

0-24 Us Gallon

144
Q

Low volt annunciator is when voltage goes below___

A

24.5V

145
Q

T/o performance

Ground roll
Tot distance over 50ft obstacle

A

Ground roll 945 ft

Tot distance over 50ft obstacle 1685ft

146
Q

Landing performance

Ground roll
Tot distance over 50ft obstacle

A

550 ft

1295ft

147
Q

Fuel capacity
Tot in both tanks
Tot usable in both tanks

A

56 US GALLONS

53 US GALLONS

148
Q

Tot fuel capacity in each tank
Tot usable fuel capacity in each tank

A

28 US GALLONS in one tank

26.5 US GALLONGS in one tank

149
Q

Max glide at ___ KIAS

A

65 KIAS

150
Q

Va at 2450 lbs

A

97KCAS
99KIAS

151
Q

Va at 2200lbs

A

93KCAS
94 KIAS

152
Q

Va at 1600 lbs

A

82KCAS
82KIAS

C172R by me (1 decks)

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