Cessna 152 Flashcards
(86 cards)
1
Q
Engine
A
Avco Lycoming O-235-L2C Horizontally Opposed
2
Q
Maximum engine power
A
110 BHP
3
Q
Maximum engine speed
A
2550 RPM
4
Q
Propeller
A
McCauley Accessory Division
5
Q
Propeller Dimensions
A
69 inches max., 67.5 inches min., 12inches ground clearance
6
Q
Wing area surface
A
160 ft2
7
Q
Wing span
A
33 ft 4 in
8
Q
Maximum height
A
8ft 6 in
9
Q
Maximum width
A
24 ft 1 in
10
Q
Service ceiling
A
14,700 ft
11
Q
Rate of climb at sea level
A
715 FPM
12
Q
Maximum weight
A
1670 LBS
13
Q
Standard empty weight
A
1081 LBS
14
Q
Maximum useful load payload and fuel
A
589 LBS
15
Q
Maximum takeoff weight
A
1670 LBS
16
Q
Maximum landing weight
A
1670 LBS
17
Q
Baggage allowance, area 1 and area 2
A
120 LBS
18
Q
Fuel capacity - standard tanks
A
26 gallons
19
Q
Fuel Capacity - Usable
A
24.5 gallons
20
Q
Fuel capacity - Unusable
A
1.5 gallons
21
Q
Fuel capacity - long range tanks
A
39 gallons
22
Q
Oil capacity:
A
6 quarts, 7 quarts (with filter)
23
Q
Oil Grade - first 50 hours
A
MIL - L - 6082
24
Q
Oil Grade - After 50 Hours
A
MIL - L - 22851
25
Take-off performance: ground roll
725 feet
26
Take off: total distance over 50ft obstacle
1340 feet
27
Landing performance: ground roll
475 feet
28
Landing: Total distance over 50ft obstacle
1200 ft
29
Stall speed (CAS) Flaps up, power off
48 knots
30
Stall speed (CAS) Flaps down, power off
43 knots
31
Vx
55 knots
32
Vy
67 knots
33
Maximum demonstrated crosswind
12 knots
34
Maneuvering speed
95 knots
35
Tire pressure nosewheel
30 PSI
36
Tire pressure mainwheel
21 PSI
37
Battery
24 volts, 14 ampere
38
Alternator
28 volt, 60 ampere
39
Approved fuel grade and color
100LL Blue;
100 (Former 100/130) Green
40
Flight load factors, flaps up
+4.4g, -1.76g
41
Flight load factor, flaps down
+3.5 g
42
Wing loading
10.5 lbs/ft2
1670 lbs / 160ft2
43
Power loading
15.2 lbs/hp
1670 lbs/110hp
44
White arc
035-085 knots
45
Green arc
040-111 knots
46
Yellow arc
111-149 knots
47
Red line
149 knots
48
Maneuver - chandelles
95
49
Maneuver - lazy eights
95
50
Maneuver - steep turns
95
51
Maneuver - spins
Use slow deceleration
52
Maximum gross weight
1670 lbs
53
Maximum useful weight
589 lbs
54
Standard Empty Weight
1081 lbs
55
Maximum baggage capacity
120 lbs
56
Fuel Capacity - Standards Tanks
26 gallons
57
Fuel Capacity - Optional Long range tanks
39 gallons
58
Standard total usable fuel
24.5 gallons
59
Maximum range, long range tanks - 10,000 ft
690 NM, 8.7HRS
60
Maximum range, standard tanks - 10,000 ft
415 NM, 5.2 HRS
61
Use of flaps 10
Shorten ground run by 10%
62
Emergency Landing without engine power
60 KIAS (flaps down), 65 KIAS (flaps up)
63
Ditching
Flaps 30, 300ft/m descent, 55 KIAS
64
Oil pressure gauge should begin to show pressure in
30 seconds in summer time and twice as long in very cold weather
65
Maxim speed at which you may use abrupt control travel
Va - 95 KIAS
66
Cruise power
1900-2550 RPM
67
Primary Flight Instrument for bank reference
Use heading indicator for primary check, turn coordinator for supporting check
68
Static RPM power check
2280 - 2380 RPM
69
Maximum Cruise speed, sea level
70
If erroneous readings of the static source instruments (airspeed, altimeter, and rate of climb) are suspected, __________________, thereby applying static pressure to these instruments from the cabin
The alternate static source valve should be pulled on
71
Normal take-off airspeed
65-75 KIAS
72
Short fiel takeoff
54 KIAS, Flaps 10, speed at 50 ft
73
Climb Flaps up, Normal airspeed
70 - 80 KIAS
74
Landing, Normal Approach Flaps up
60 - 70 KIAS
75
Landing, Normal Approach Flaps 30
55 - 65 KIAS
76
Landing, Short field approach Flaps 30
54 KIAS
77
Balked Landing, Maximum Power, Flaps 20
55 KIAS
78
Spiral dive
Adjust elevator trim control to maintain a 70 kts glide
79
Primary Flight Instrument for nose up and nose down reference
Altimeter for primary check, VSI for supporting check
80
Level the nose should restore power within _____ to raise air temp - 1/4 - 1/2
20 seconds
81
Change in engine oil
Every 6 months of every 100 hrs whichever comes first
82
Cruise speed at sea level, 75%
100 KTAS
83
Flight instrument for primary check for power
Use airspeed indicator for primary check, tachometer for support or confirm power settings
84
Prior to starting on a cold morning, it is advisable to pull the propeller through several times by hand to
"break loose" or "limber" the oil, thus conserving battery energy
85
If erroneous instrument readings are suspected due to water or ice in static pressure lines
The static pressure alternate source valve control knob located below the wing flap switch should be opened
86
Engine Failure After Take off
Flaps up - 65 KIAS
Flaps down - 60 KIAS
Max Glide - 60 KIAS
