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
2
Q
WITH THE ALTERNATOR SIDE OF MASTER SWITCH OFF MAX COMPASS DEVIATION MAY OCCUR UPTO
A
25deg
3
Q
MAX SLIP OR SKID DURATION WITH ONE TANK DRY is
A
30 sec
4
Q
TEMP DECREASES BY ______ FOR EACH 1000ft ALTITUDE
A
2deg Celsius per 1000ft alt
5
Q
MAX OIL PRESSURE is
A
115 psi
6
Q
MAX WINDOW OPEN SPEED in KIAS is
A
163 KIAS
160 KCAS ( additional fact )
7
Q
MAX TURNING RADIUS (pivot pt to outbound using tip)
A
27feet 5.5inches
8
Q
UNUSABLE FUEL QUANTITY IN EACH TANK is
A
1.5 gallon
9
Q
MAX VENTILATION CAN BE ACHIEVED BY
A
Cabin air knob pull out and
Cabin heat knob is pushed in
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)
11
Q
PROP GROUND CLEARANCE
A
11feet 1/4th inches ie 11.25inches
12
Q
Ignition operation is controlled by a rotary switch which is labeled
A
Right, left , both, start
13
Q
BEST FUEL ECONOMY CAN BE ACHIEVED AT
A
OPERATION AT PEAK EGT
14
Q
Weak intermittent firing followed by puffs of black smoke from the exhaust stock indicates
A
Over priming
15
Q
WHEN SHOULD FUEL EXAMINATION FOR CONTAMINATION AND GRADE BE DONE
A
1) Before first flight of each day
2) after refuelling
16
Q
Oil Px gauge marking indicates
A
Red line for minimum permissible idling pressure
17
Q
VSI indicates airplanes ____
A
ROC or ROD in ft per min
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
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
20
Q
The engine driven vacuum system provides the
A
Suction necessary to operate
directional indicator and attitude indicator
21
Q
Centre area of instrument panel contains ___
A
Static px alternate source valve
22
Q
_____ of ldg gear is of ____ shock strut
A
Nose
Air/oil
23
Q
Colour of 100LL grade aviation fuel is
A
BLUE
24
Q
DiEGME( Diethyl glycol monomethyl ether) mixed w fuel tot fuel volume in concentration is b/w ??
A
0.10% to 0.15%
25
ELT enunciator illuminates when rocker switch in cockpit is placed to ____
Forward position
26
Left rudder pedal pressed to left side so nose wheel can be turned to ____ deg max
10deg max
27
Avionics eqpt 3 points
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
28
An open alternate air door will result in an approx ____ power loss at full throttle
10% power loss
29
To permit heavier cabin loading filling of usable fuel in each tank must not be less than ____
17.5 gallons
30
Yellow arc on ASI reponds to ___
129 to 163 kts (smooth air)
31
Abrupt use of controls is prohibited above ___
99kts
32
The digital clock / OAT is tested by ___
Holding control button for 3 sec
33
Audible stall warning horn comes at ____
5-10 kts above stall in all flight conditions
34
In pitot/ static system of the static system becomes blocked what will happen to the ASI
ASI will still function but will give erroneous readings
35
Carburettor ice is detected by ___
1) Drop in engine RPM in fixed pitch propeller aircraft
2) drop in manifold Px in constant speed prop a/c
36
To improve engine cooling in en route climb, a short duration climb can be made at what V speed and
at what engine power
Vy - best rate of climb speed
Until engine has accumulated 50hrs or 80% of engine power
37
Vy at sea level with max weight of 2450lbs
79KIAS
38
Recommended starter duty cycle is
10sec on
20sec off
Max 3 times
10min gap for cooling
Repeat 3 times
39
During engine starting, if engine floods what should be done
Mixture in idle cut off
40
3 statements of compass
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
41
The transmitter of bendix /king XX 155 Anav/comm system stops transmitting if microphone is keyed continuously for greater than ___ sec
33 sec
42
Flap switch level mechanical stops are provided at
10,20 and 30deg positions
43
Red oil Px illuminates when Px is below ___ psi
20psi
44
Annunciator located above altimeter provides caution and warning msgs for ?
Fuel quantity
Oil Px
Low vaccum
Low voltage situation
45
Alternator must be switched off manually if voltage indicates beyond ____V
31.5V
46
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
Within 60 sec
47
Max airspeed and altimeter variation over the normal operating range window(s) closed and alternator switched off is ____ & _____??
4knots
30ft
48
To apply parking brakes
Set brake with rudder paddle
Pull handle aft
Rotate 90deg down
49
____ is not marked on each side of the central marking of an attitude indicator
40deg
50
In long flt which is the maximum deviation in compass for precession error
30 deg max deviation
51
ELT annunciator does not activate on ____
Low fuel flow
52
In the event of alternate static door open what will be the margin of error in ASI
ASI will give error of 7kts
53
Min oil Px of a/c
20psi
54
DGI (or compass) has to be aligned regularly on long flights for ___
Precession
55
Compass error upto 25deg may come in the event of alternator ____
Switched off
56
MIN AND MAX oil quantity for extended flights is
MIN 5 quarts
fill upto
MAX 8 quarts
57
Conc of isopropyl alcohol ___
1%
58
Which oil is to be used after 50 hrs of engine running or when the oil consumption has been stabilised
MIL- L -22851
&
SAE J1899 aviation grade ash-less dispersant oil
59
Max deflection of nose wheel by use of rudder paddle on ground is ___
10deg to either side
60
Mechanical stops on flaps are at____
10deg
20deg
30deg
61
Shock absorption on nose wheel
Air and oil system
62
(Vy) Best rate of climb speed at sea level is
79 knots
63
Shock absorption on main wheel___
tubular spring
64
Min turning radius during taxi using differential braking and nose wheel steering ___
27feet
65
If engine floods
Right 3 steps for course of action
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
Starter cycle for engine is
10sec ON
&
3times and then 10min gap for cooling to be given
67
Enroute climb speed is 5 to 10kts above best rate of climb speed for ___
Best visibility
Best performance
Best cooling
68
Until 50hrs has been accumulated engine should be run at ___
80% power on cruise
69
Nose gear shock strut pressure
45 psi
70
OAT/volt gauge select switch may be used by putting the select button down off
3 sec to start
71
If the PTT button of microphone is kept pressed more than 33 sec in continuous then the transmission is ___
Automatically terminated
72
Max fuel capacity of each tank is
28 US GALLONS
73
Spark plug fault causes
Loss of RPM
74
Magneto malfunction causes
Misfiring
75
Brake of A/C model
MIL-H-5606
76
Tyre Px of nose wheel tyre
34 psi
77
Tyre Px of main wheel tyre
29 psi
78
Nose wheel strut length
2 inches
79
Propeller diameter
75 inches
80
Engine model number
IO - 360- L2A
81
Std empty wt of a/c
1639 lbs
82
Baggage compartment contains
Compartment 1 has allowance of 120lbs (fwd)
Compartment 2 has allowance of 50 lbs (aft)
Tot baggage compartment allowance is 120 lbs (combined)
83
Max useful load of a/c
818 lbs (NORMAL CATEGORY)
And for utility category = 564 lbs
84
Wing loading of a/c
14.1 lbs / sq ft
85
Power loading of a/c
15.3 lbs /Hp
86
Wing area of A/c
174sq ft
87
Elevator span of a/c
11 ft 4 inches
88
Wheel base length of a/c
65 inches
89
Max Horse power rating and engine power ( RPM)
160BHP
2400 RPM
90
Prop model no. of a/c
IC235/LFA7570
91
Airspeed when ENGINE FAILS after t/o
Flaps up 65 KIAS
Flaps down 60KIAS
92
Landing with a flat main tyre , flaps will be ___
30deg
93
Landing with a flat nose tyre, flaps will be ___
As required
94
Engine failure during t/o roll the first action will be
Throttle idle
95
If fire occurs during start on ground the throttle and mixture will be ___
Throttle full open
Mixture idle cut off
96
Magneto check should be made at ___
At 1800RPM
97
Descending through clouds to go around against spiral dive and due to changing bank angle what to do to minimise compass card swings ?
Choose an easterly hdg
&
Choose a westerly hdg
98
A/c is equipped with DC electrical system of ?
28Volt DC ie direct current electric system
99
Electrical system of a/c is powered by
34 V , DC electrical system
100
Desired vacuum range of a/c is
4.5 to 5.5 inches of mercury
101
Communication receiver transmitter receives and transmits signals b/w
B/w 118.06 and 136.972MHz with 25Hz spacing
102
Nav receiver receives VOR and localiser signals
B/w 108 and 117.95MHz in 50KHz steps
103
Aircraft has ____ clock model
The davtron model 803 digital clock
104
Clock of a/c combines the feature of
___, ____ and _____
A clock
OAT gauge
Voltmeter
105
T/o speed for normal climb
70-80 KIAS
106
Enroute climb at sea level airspeed is
75-85 KIAS with flaps UP
107
Engine manufacturer of a/c
Textron Lycoming
108
Engine type of a/c
Four cylinder engine
Horizontally opposed
Fuel injection
Air cooled
109
MIL-L-6082 or SAE J1966 aviation grade straight mineral oil is used
To replenish the supply during first 25hrs
&
Use until total of first 50 hrs
110
At 10,000ft best angle of climb speed
65 KIAS
111
Max oil temp in Celsius and Fahrenheit
118 deg Celsius
245 Fahrenheit
112
Landing apch speed
Normal apch speed at 65-75 KIAS FLAPS UP
FLAPS DOWN 30deg at 60-70 KIAS
short field apch Flaps FULL (62KIAS)
113
Max flap extended speed of a/c
110 kias for 10 deg flaps
&
85 kias for 10deg to 30 deg flaps
114
Vne of a/c
160kcas or 163kias
115
Max structural cruising speed of aircraft
126 KCAS or 129 KIAS
116
While ditching transmit mayday on _____ giving location and intention and squawk ____
121.5MHz
Squawk 7700
117
The set of radio contains
760 channels of VHF comm receiver
200 channels of VHF nav rcvr
118
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
D) Flight into icing condition prohibited
119
If alternator shuts down due to over-voltage, when will
you
restart it?
only on ground
120
Full flowmeter range
and Cruising full flow
0 to 11 gph ie gallons per hr (GREEN ARC)
and
5.6 to 9.3 gph depending on ht , power and oat
121
The VSI testing ELT, what will you
do with the rubber arm?
press forward ON
press backward RESET
122
aircraft tyres are ___ ply rated.
6 ply rated
123
Pitot-static system provides pressure to ____ & static to ___, ___, ___.
pitot static to ASI
static to ASI
VSI
ALTIMETER
124
when flying through clouds at night or when____ or ____ are ON, it can cause vertigo and loss of orientation
flashing beacon or lights
125
Dimensions in terms of
Length
Wing span
Height
Length 27ft 2 inches
Wing span 36 ft 1 inch
Height 8ft 11 inches
126
Service ceiling
13,500ft
127
Stall speed
FLAPS UP
POWER OFF and
FLAPS DOWN
POWER OFF
51KCAS FLAPS UP power off
47KCAS FLAPS DOWN power off
128
Cruise 80% power
Airspeed and
Range
122 kts
580Nm
129
SAE stands for
Society of automotive engineers
130
Speed fairing inc speed of a/c by ____
2kts
131
Max t/o and ldg wt for normal ops and for utility category
For normal = 2450lbs
For utility = 2200lbs
132
Attitude indicator bank marking at an increment of ___
10,20,30,60,90 degrees
133
ELT is operated by ____ and ____
Control panel and forward fairing/facing
134
Beta rays fit fine
thrust reverse
135
In case of engine fire in flt,
_____ kts airspeed is advised to maintain
100kts
136
In case of ditching
Flap setting
Apch speed
ROD
is advised to mntn
Flap setting 20 deg
ROD 300 fpm
Apch speed 55kts
137
In case of flames from left fuel tank, side slip to ____
Right
138
With ice accumulation of _____ on wing leading edges, be prepared for significant
high power requirement, high approach speed and high stall speed.
0.25inches or more
139
Fuel saving procedure for flight training operations provide fuel saving in excess of ___ when compared
to mixture rich operations.
5%
140
Operating at peak EGT provides best fuel economy, results in ___ greater range and ___ decrease
in speed.
4% greater range
3kts dec in speed
141
Low vacuum annunciatorshows in Amber light twhen vacuum pressure drops below ___
3.4 inch of Hg
142
digital display of annuciator shows red colour annunciator in tachometer when rpm exceeds___ and indicates engine speed more than the limit
2472 rpm and above
143
Max. Limit range of float travel _____to indicate fuel remaining in tanks
0-24 Us Gallon
144
Low volt annunciator is when voltage goes below___
24.5V
145
T/o performance
Ground roll
Tot distance over 50ft obstacle
Ground roll 945 ft
Tot distance over 50ft obstacle 1685ft
146
Landing performance
Ground roll
Tot distance over 50ft obstacle
550 ft
1295ft
147
Fuel capacity
Tot in both tanks
Tot usable in both tanks
56 US GALLONS
53 US GALLONS
148
Tot fuel capacity in each tank
Tot usable fuel capacity in each tank
28 US GALLONS in one tank
26.5 US GALLONGS in one tank
149
Max glide at ___ KIAS
65 KIAS
150
Va at 2450 lbs
97KCAS
99KIAS
151
Va at 2200lbs
93KCAS
94 KIAS
152
Va at 1600 lbs
82KCAS
82KIAS
