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1.5.1.2.7.B.1
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CGX
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Knowledge Code: A20
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To act as pilot in command of a glider, using self-launch procedures, that person must hold a pilot certificate with a glider rating and have accomplished
| | A) ground and flight training in self-launch procedures and operations, and possess a logbook endorsement from a flight instructor certifying such proficiency. |
| | B) a competency flight check given by an authorized flight instructor. |
| | C) appropriate flight training and meet recent experience in self-launch operations. |
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1.5.1.2.8.B.1
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CAX CBG CBH CGX CLA CRG CRH MCA MCH
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Knowledge Code: A21
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To act as pilot in command of a tailwheel airplane, without prior experience, a pilot must
| | A) pass a competency check and receive an endorsement from an authorized instructor. |
| * | B) receive and log flight training from an authorized instructor as well as receive a logbook endorsement from an authorized instructor who finds the person proficient in a tailwheel airplane. |
| | C) log ground and flight training from an authorized instructor. |
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1.5.1.2.9.B.1
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CAX CBG CBH CGX CLA CRG CRH MCA MCH
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Knowledge Code: B12
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No person may operate an aircraft that has an experimental airworthiness certificate
| | A) when carrying property for hire. |
| * | B) when carrying persons or property for hire. |
| | C) under instrument flight rules (IFR). |
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2.5.1.5.1.A.1
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CAX CBG CBH CGX CLA CRG CRH MCA MCH
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Knowledge Code: H303
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The ratio between the total airload imposed on the wing and the gross weight of an aircraft in flight is known as
| | A) aspect load and directly affects stall speed. |
| | B) load factor and has no relation with stall speed. |
| * | C) load factor and directly affects stall speed. |
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2.5.1.5.2.A.1
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CAX CBG CBH CGX CLA CRG CRH MCA MCH
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Knowledge Code: H303
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Load factor is the lift generated by the wings of an aircraft at any given time
| | A) multiplied by the total weight of the aircraft. |
| * | B) divided by the total weight of the aircraft. |
| | C) divided by the basic empty weight of the aircraft. |
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2.5.1.5.3.A.1
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CAX CBG CBH CGX CLA CRG CRH MCA MCH
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Knowledge Code: H303
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For a given angle of bank, in any airplane, the load factor imposed in a coordinated constant-altitude turn
| | A) varies with the rate of turn. |
| | B) is constant and the stall speed decreases. |
| * | C) is constant and the stall speed increases. |
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2.5.1.5.4.A.1
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CAX CBG CBH CGX CLA CRG CRH MCA MCH
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Knowledge Code: H303
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Airplane wing loading during a level coordinated turn in smooth air depends upon the
| * | A) angle of bank. |
| | B) true airspeed. |
| | C) rate of turn. |
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2.5.1.5.5.A.1
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CAX CBG CBH CGX CLA CRG CRH MCA MCH
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Knowledge Code: H303
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In a rapid recovery from a dive, the effects of load factor would cause the stall speed to
| | A) decrease. |
| | B) not vary. |
| * | C) increase. |
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2.5.1.5.6.A.1
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CAX CBG CBH CGX CLA CRG CRH MCA MCH
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Knowledge Code: H303
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If an aircraft with a gross weight of 2,000 pounds was subjected to a 60° constant-altitude bank, the total load would be
| | A) 12,000 pounds. |
| | B) 3,000 pounds. |
| * | C) 4,000 pounds. |
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2.5.1.5.8.A.1
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CAX CBG CBH CGX CLA CRG CRH MCA MCH
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Knowledge Code: H300
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Lift on a wing is most properly defined as the
| | A) differential pressure acting perpendicular to the chord of the wing. |
| | B) reduced pressure resulting from a laminar flow over the upper camber of an airfoil, which acts perpendicular to the mean camber. |
| * | C) force acting perpendicular to the relative wind. |
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