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Cessna 172 Systems And Limitations > Systems And Limitations > Flashcards

Systems And Limitations Flashcards

1
Q

What does the Accessory Kit (L2A) consist of?

A

Starter, Belt-Driven Alternator, Dual Magnetos, Vacuum Pump, Engine-Driven Fuel Pump, Full-Flow Oil Filter

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2
Q

What are the components of the ignition system?

A

Magnetos (2), Spark Plugs (8), High-tension leads, Ignition switch, Starter, Pinion gear/flywheel, Main battery, Impulse coupler

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3
Q

Maximum Engine Speed

A

2700RPM

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4
Q

Static RPM range at full throttle

A

2300-2400RPM

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5
Q

Maximum Oil Temperature

A

245°F

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6
Q

Minimum Oil Pressure

A

20 PSI

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7
Q

Maximum Oil Pressure

A

115 PSI

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8
Q

Engine Oil for the first 50 hours

A

Aviation Grade Straight Mineral Oil

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9
Q

Engine Oil after the first 50 hours

A

Aviation Grade Ashless Dispersant Oil

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10
Q

Green Arc on the tachometer at sea level

A

2100-2500RPM

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11
Q

Green Arc on the tachometer at 5,000ft

A

2100-2600RPM

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12
Q

Green Arc on the tachometer at 10,000ft

A

2100-2700RPM

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13
Q

Green Arc for CHT

A

200 to 500°F

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14
Q

Green Arc on Oil Temperature

A

100 to 245°F

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15
Q

Green Arc on Oil Pressure

A

50-90 PSI

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16
Q

Green Arc on Fuel Quantity

A

5-24 gal

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17
Q

Green Arc on Fuel Flow

A

0-12 GPH

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18
Q

Green Arc on Vacuum Indicator

A

4.5-5.5 in. Hg.

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19
Q

What kind of propellor do we have?

A

McCauley, two-bladed, fixed pitch, one-piece forged aluminum alloy propeller

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20
Q

Maximum Propeller Diameter

A

76 inches

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21
Q

Minimum Propeller Diameter

A

75 inches

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22
Q

Propeller ground clearance

A

11.25 inches

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23
Q

Normal Category Maximum Ramp Weight

A

2558lbs

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24
Q

Normal Category Maximum Takeoff Weight

25
Normal Category Maximum Landing Weight
2550lbs
26
Maximum Weight in Baggage Area A: Normal Category
120lbs
27
Maximum Weight in Baggage Area B: Normal Category
50lbs
28
Maximum Allowable Combined Weight in Areas A and B: Normal Category
120lbs
29
Utility Category Maximum Ramp Weight
2208lbs
30
Utility Category Maximum Takeoff Weight
2200lbs
31
Utility Category Maximum Landing Weight
2200lbs
32
Maximum Weight in Baggage Compartment: Utility Category
Baggage compartment must be empty and rear seat must not be occupied
33
Normal Category CG Range: Forward
35 inches at 1950lbs or less and 41 inches at 2550lbs
34
Normal Category CG Range: Aft
47.3 inches at all weights
35
Utility Category CG Range: Forward
35 inches at 1950lbs or less and 37.5 inches at 2200lbs
36
Utility Category CG Range: Aft
40.5 inches at all weights
37
Normal Category Load Factor: Flaps Up
+3.8g, -1.52g
38
Normal Category Load Factor: Flaps FULL
+3.0g
39
Utility Category Load Factor: Flaps Up
+4.4g, -1.76g
40
Utility Category Load Factor: Flaps FULL
+3.0g
41
Fuel Limitations
1. Park plane in a wings level, normal attitude with the fuel selector on left or right 2. Takeoff and land with fuel selector on both 3. Maximum slip or skid duration with one tank dry is 30 seconds 4. Operation on either the left or right tank is limited to level flight only 5. With 1/4 tank or less, prolong uncoordinated flight is prohibited when on the left or right tank 6. Fuel remaining in the tank after the fuel quantity indicator reads 0 (red line) cannot be safely used in flight 7. 100LL (blue) and 100 (green)
42
Flap Limitations: Approved Takeoff Range
UP to 10°
43
Flap Limitations: Approved Landing Range
UP to FULL
44
Fuel Indicating System
Green: 5-24 gal per tank Yellow: 0-5 gal per tank Red: 0 gal per tank
45
Minimum Amount of Oil
5 quarts
46
HIGH VOLTS
M Bus or E Bus is above 32V
47
LOW VOLTS
M Bus or E Bus is below 24.5V
48
STBY BATT
Discharge rates are greater than 0.5 amps for more than 10 seconds
49
LOW FUEL
When fuel quantity is less than 5 gallons indicated for more than 60 seconds
50
OIL PRESSURE
When oil pressure is between 0 and 20 PSI
51
LOW VACUUM
When vacuum pressure is below 3.5 in. Hg.
52
CO LVL HIGH
When CO level is 50 parts-per-million or higher
53
Minimum Turning Radius
27 feet, 5.5 inches
54
Nose-wheel Turning Radius
Without brakes: 10° each side of center With brakes: 30° each side of center
55
When will RPM flash
2780RPM or more
56
When does the standby battery have little or no capacity remaining?
20V
57
Nose Wheel PSI
45 PSI
58
Main Wheel PSI
42 PSI

Cessna 172 Systems And Limitations (1 decks)

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