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| What is the engine model number for the 1978 Cessna 152? | The engine model is Avco Lycoming O-235-L2C. |
| What is the horsepower rating and engine speed for the Cessna 152's O-235-L2C engine? | The engine is rated for 110 BHP at 2550 RPM. |
| What are the two approved fuel grades for the 1978 Cessna 152? | 100LL Grade Aviation Fuel (Blue) and 100 (Formerly 100/130) Grade Aviation Fuel (Green). |
| What is the total usable fuel capacity of a Cessna 152 with standard tanks? | The total usable fuel is 24.5 gallons. |
| What is the total usable fuel capacity of a Cessna 152 equipped with long-range tanks? | The total usable fuel is 37.5 gallons. |
| What is the oil sump capacity of the Cessna 152's engine? | The sump capacity is 6 quarts. |
| What are the maximum certificated takeoff and landing weights for the Cessna 152? | The maximum takeoff and landing weight is 1670 lbs. |
| What is the maximum combined weight capacity for baggage areas 1 and 2 in the Cessna 152? | The maximum combined weight capacity is 120 lbs. |
| The white arc on the airspeed indicator of a Cessna 152 represents the _____. | Full Flap Operating Range (35-85 KIAS). |
| What is the significance of the green arc on the Cessna 152's airspeed indicator? | It indicates the Normal Operating Range (40-111 KIAS). |
| Operations in the yellow arc (111-149 KIAS) on the airspeed indicator must be conducted with caution and only in _____. | smooth air. |
| What is the Never Exceed Speed ($V_{NE}$) for the Cessna 152? | The $V_{NE}$ is 149 KIAS (145 KCAS). |
| What is the Maximum Structural Cruising Speed ($V_{NO}$) for the Cessna 152? | The $V_{NO}$ is 111 KIAS (108 KCAS). |
| What is the Maneuvering Speed ($V_A$) for the Cessna 152 at its maximum weight of 1670 lbs? | The $V_A$ at 1670 lbs is 104 KIAS (101 KCAS). |
| What is the Maximum Flap Extended Speed ($V_{FE}$) for the Cessna 152? | The $V_{FE}$ is 85 KIAS (87 KCAS). |
| What is the static RPM range at full throttle for the Cessna 152? | The static RPM range is 2280 to 2380 RPM. |
| What is the normal operating range for oil pressure in the Cessna 152? | The normal oil pressure range is 60-90 psi (green arc). |
| What is the maximum oil temperature for the Cessna 152's engine? | The maximum oil temperature is 118°C (245°F). |
| What are the flight load factor limits for the Cessna 152 with flaps up? | The limits are +4.4g and -1.76g with flaps up. |
| What is the flight load factor limit for the Cessna 152 with flaps down? | The limit is +3.5g with flaps down. |
| According to the placards, are intentional spins with flaps extended permitted in the Cessna 152? | No, intentional spins with flaps extended are prohibited. |
| What are the first two steps in the spin recovery procedure for a Cessna 152? | 1. Verify ailerons are neutral and throttle is closed. 2. Apply full opposite rudder. |
| What is the recommended airspeed for a maximum glide in a Cessna 152 during an emergency? | The recommended maximum glide speed is 60 KIAS. |
| In an engine failure immediately after takeoff, what is the first action regarding airspeed? | The first action is to establish an airspeed of 60 KIAS. |
| What is the procedure for an engine fire in flight regarding the mixture and fuel shutoff valve? | Set the mixture to IDLE CUT-OFF and the fuel shutoff valve to OFF. |
| During an electrical fire in flight, what is the first immediate action? | The first action is to turn the Master Switch OFF. |
| If you inadvertently encounter icing conditions, what should you do with the pitot heat and cabin heat controls? | Turn the pitot heat switch ON and pull the cabin heat control full out for maximum defroster air. |
| During an inadvertent icing encounter with 1/4 inch or more of ice, what should you do with the wing flaps for landing? | Leave the wing flaps retracted. |
| What is the first step in the procedure for an engine failure during the takeoff run? | The first step is to move the throttle to IDLE. |
| In a spin recovery, after applying full opposite rudder, what is the next step involving the control wheel? | Move the control wheel briskly forward to break the stall. |
| What is the maximum demonstrated crosswind velocity for the Cessna 152? | The maximum demonstrated crosswind velocity is 12 knots. |
| What is the best rate-of-climb speed ($V_Y$) for a Cessna 152 at sea level? | The best rate-of-climb speed at sea level is 67 KIAS. |
| What is the best angle-of-climb speed ($V_X$) for a Cessna 152? | The best angle-of-climb speed is 55 KIAS from sea level through 10,000 feet. |
| What is the recommended short field approach speed with 30° flaps? | The recommended short field approach speed is 54 KIAS. |
| During the preflight inspection, how do you check the stall warning system? | Place a clean handkerchief over the vent opening and apply suction; a sound from the horn confirms operation. |
| During the engine run-up, what is the maximum allowable RPM drop when checking magnetos? | The RPM drop should not exceed 125 RPM on either magneto. |
| What is the maximum allowable RPM differential between magnetos during the run-up check? | The RPM differential between magnetos should not exceed 50 RPM. |
| For a short field takeoff in a Cessna 152, what flap setting should be used? | A 10° flap setting should be used for a short field takeoff. |
| In a balked landing (go-around), what is the first action regarding the wing flaps after applying full power? | The wing flaps should be immediately retracted to 20°. |
| Normal cruising in the Cessna 152 is performed between what power settings? | Normal cruising is performed between 55% and 75% power. |
| How is the fuel mixture leaned for best economy during cruise? | The mixture should be leaned until the engine RPM peaks, and then drops 25-50 RPM. |
| What is the stall warning system designed to do? | It produces a steady audible warning 5 to 10 knots before the actual stall is reached. |
| For a short field landing, what flap setting is recommended? | A 30° flap setting is recommended for a short field landing. |
| What action should be taken immediately after touchdown during a short field landing to maximize braking effectiveness? | Retract the flaps and hold full nose-up elevator. |
| When taxiing in a strong quartering tailwind, what aileron and elevator inputs are required? | Use down aileron on the upwind wing and down elevator. |
| According to the performance charts, decreasing takeoff distance by 10% corresponds to what headwind component? | A 10% decrease in takeoff distance corresponds to a 9-knot headwind. |
| According to the performance charts, what is the effect on landing ground roll of operating on a dry, grass runway? | For operation on a dry, grass runway, increase the ground roll distance by 45%. |
| What is the Reference Datum for weight and balance calculations on the Cessna 152? | The Reference Datum is the front face of the firewall. |
| What is the construction of the Cessna 152 fuselage described as? | The fuselage construction is a conventional formed sheet metal bulkhead, stringer, and skin design known as semimonocoque. |
| How are the wing flaps on the Cessna 152 operated? | The flaps are extended or retracted by an electrically operated switch lever on the instrument panel. |
| The shock absorption for the main landing gear is provided by what component? | Shock absorption is provided by the tubular spring-steel main landing gear struts. |
| The shock absorption for the nose gear is provided by what type of strut? | The nose gear uses an air/oil shock strut. |
| How is engine power controlled in the Cessna 152? | Engine power is controlled by a throttle located on the lower center portion of the instrument panel. |
| The mixture control is in the _____ position when fully aft. | idle cut-off |
| What does the engine-driven vacuum system power in the Cessna 152? | It provides suction to operate the attitude indicator and the directional indicator. |
| What is the desired suction range for the vacuum system, as shown on the suction gage? | The desired suction range is 4.6 to 5.4 inches of mercury. |
| The Cessna 152 electrical system is a _____-volt, direct-current system. | 28 |
| What component powers the Cessna 152's electrical system? | The system is powered by an engine-driven, 60-amp alternator and a 24-volt battery. |
| What does illumination of the red 'HIGH VOLTAGE' warning light indicate? | It indicates that an over-voltage condition has occurred and the alternator has shut down. |
| The pitot-static system supplies ram air pressure to which instrument? | The pitot-static system supplies ram air pressure only to the airspeed indicator. |
| The pitot-static system supplies static pressure to which three instruments? | It supplies static pressure to the airspeed indicator, rate-of-climb indicator, and altimeter. |
| How is fuel delivered from the tanks to the carburetor in the Cessna 152? | Fuel is delivered by gravity flow from the wing tanks to the carburetor. |
| How is the fuel system vented to the atmosphere? | The left tank is vented overboard through a vent line, and the right tank filler cap is also vented. |
| On airplanes not equipped with an oil filter, how often should the engine oil be drained and the pressure screen cleaned? | The oil should be drained and the screen cleaned every 50 hours of operation. |
| What is the recommended tire pressure for the main wheels of a Cessna 152? | The recommended pressure is 21 PSI for the 6.00-6, 4-ply rated main wheel tires. |
| What is the recommended air pressure for the nose gear shock strut? | The nose gear shock strut should be inflated with air to 20 PSI. |
| What is the function of the Emergency Locator Transmitter (ELT)? | It is a self-contained radio transmitter that activates on impact to emit a distress signal on 121.5 and 243.0 MHz. |
| What does the 'AUTO' position on the ELT function selector switch do? | It sets the ELT to activate automatically only when the 'g' switch receives an impact of 5g or more. |
| What special transponder code is selected to indicate an emergency? | The code 7700 is selected to indicate an emergency. |
| What special transponder code is selected to indicate a loss of all communications? | The code 7600 is selected to indicate a loss of communications. |
| When the transponder function switch is in the 'ALT' position, what information can it transmit? | It can transmit either Mode A (aircraft identification) or Mode C (altitude reporting) pulses. |
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