TEST en vol multi Flashcards

(32 cards)

1
Q

Définition de la Vso

A

vitesse de décrochage en configuration d’atterrissage (VSO) à la masse maximale d’atterrissage

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2
Q

Vso PA31 pour UMQ et RKG

A

73 RKG et 82 UMQ (vortex)

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3
Q

Définition VYSE

A

vitesse correspondant à la vitesse ascensionnelle maximale, un moteur en panne (VYSE)

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4
Q

VYSE PA31

A

110

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5
Q

définition VXSE

A

vitesse correspondant à la pente de montée maximale, un moteur en panne (VXSE)

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6
Q

VXSE PA31

A

106

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7
Q

vitesse de manœuvre (VA) PA31

A

183 selon POH (check-list différent)

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8
Q

Définition de la vitesse de manœuvre (VA)

A

la vitesse maximale à laquelle une déflexion complète et brusque des commandes n’entraînera pas de surcharge structurelle excessive.

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9
Q

vitesse minimale de contrôle (VMC) PA31 UMQ et RKG

A

85 POH et RKG, 87 UMQ

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10
Q

Il y a combien de critères pour calculer la VMC et énumère les

A

11, -Maximum Takeoff Power
-Critical Engine Inoperative
-Inoperative Engine Windmilling
-Sea Level Conditions
-Most Adverse Legal Weight
-Most Adverse Legal C of G
-5 degrees of Bank into the Operative Engine
-Gear Up
-Flaps in the Takeoff Position
-Cowl Flaps Open
-Out of Ground Effect

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11
Q

Définition VMC

A

the speed at which the rudder no longer has the authority to overcome the yaw caused by the critical engine being inoperative

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12
Q

Explique comment La puissance maximum au décollage affecte la VMC? Est-ce que c’est bon?

A

Mauvais The more power on the operating engine, the greater the force pulling toward the dead engine. The greater the force, the earlier the rudder will lose control. The minimum controllable airspeed will be higher with greater power.

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13
Q

Explique comment CRITICAL ENGINE INOPERATIVE affecte la VMC? Est-ce que c’est bon?

A

CRITICAL ENGINE INOPERATIVE - BAD for Vmc
The critical engine is the engine that has the most adverse affect on control of the plane. By failing this engine, the rudder has more force to overcome than if the R-engine was failed, therefore Vmc will be higher.

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14
Q

Explique comment INOPERATIVE ENGINE WINDMILLING affecte la VMC? Est-ce que c’est bon?

A

INOPERATIVE ENGINE WINDMILLING - BAD for Vmc
A windmilling prop creates more drag than a feathered prop. Increased drag on the inoperative engine will create a stronger yaw toward the dead engine. Therefore, the rudder has to overcome more force, raising Vmc.

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15
Q

Explique comment SEA LEVEL CONDITIONS affecte la VMC? Est-ce que c’est bon?

A

SEA LEVEL CONDITIONS - BAD for Vmc
At sea level the dense air allows the operating engine and prop to produce maximum thrust. Since there is more thrust, there is a greater force toward the dead engine for the rudder to overcome, therefore Vmc is higher.

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16
Q

Explique comment LIGHTEST WEIGHT affecte la VMC? Est-ce que c’est bon?

A

MOST UNFAVORABLE LEGAL WEIGHT (LIGHTEST WEIGHT) - BAD for Vmc
Vmc increases as weight is reduced so the lightest legal weight is most unfavorable. The lightest weight provides the aircraft the least momentum. The heavier the aircraft, the more likely its inertia will carry it forward and help prevent the yaw and roll associated with a failed engine.

17
Q

Explique comment MOST UNFAVORABLE LEGAL CENTER OF GRAVITY affecte la VMC? Est-ce que c’est bon?

A

MOST UNFAVORABLE LEGAL CENTER OF GRAVITY (AFT CG) - BAD for VMC
Vmc increases as the C of G is moved aft (arrière). The further aft the C of G, the shorter the rudder’s arm is. The shorter the arm, the less effective the rudder. Vmc will be higher since the rudder produces less force at any speed than if the C of G was forward

18
Q

Explique comment OUT OF GROUND EFFECT affecte la VMC? Est-ce que c’est bon?

A

An aircraft in ground effect is “cushioned”, with less drag and greater lift. So in ground effect, Vmc decreases. As the aircraft lifts out of ground effect, it loses that lift and increases its drag, thereby increasing the Vmc.

19
Q

Explique comment GEAR POSITION affecte la VMC? Est-ce que c’est bon?

A

GEAR RETRACTED - BAD for Vmc
When the gear is down it acts as a keel (like on a boat) which aids in directional stability and decreases Vmc. With the gear up the keel effect is removed and it cannot help keep the aircraft straight.

20
Q

Explique comment COWL FLAPS POSITION affecte la VMC? Est-ce que c’est bon?

A

COWL FLAPS OPEN - GOOD for Vmc
With the cowl flaps open the operating engine’s prop will push air into the cowl flaps resulting in increased drag. Increased drag on the operating engine decreases Vmc since it assists in counteracting the yaw toward the dead engine.

21
Q

Explique comment un 5 DEGREES OF BANK INTO THE OPERATING ENGINE affecte la VMC? Est-ce que c’est bon?

A

5 DEGREES OF BANK INTO THE OPERATING ENGINE - GOOD for Vmc The horizontal component of lift generated by bank assists the rudder in counteracting the yaw from the inoperative engine. Vmc is reduced considerably with bank angle so the FAA limits the bank during testing to 5 degrees.

22
Q

Explique comment take-off flaps affecte la VMC? Est-ce que c’est bon?

A

Extended flaps will increase both drag and lift. The increased drag from the extended flap behind the operating engine may tend to oppose the yawing motion of that engine, requiring less rudder to counteract that yaw. So Vmc will be lower with flaps extended, and higher with flaps retracted (the take-off position for this aircraft).

23
Q

définition VLE

A

vitesse maximale, train d’atterrissage sorti (VLE)

24
Q

VLE PA31?

25
Définition Vlo
vitesse maximale d'opération du train d'atterrissage(VLO)
26
Vlo PA31
150
27
Définition VFE
vitesse maximale, volets sortis (VFE
28
VFE 0 to 15 PA31
175
29
VFE 15 to full
150 POH et RKG, 161 UMQ
30
définition VSSE
La VSSE est la vitesse minimale sécuritaire recommandée pour effectuer une panne moteur simulée sur un bimoteur. Elle est plus élevée que la Vmc et permet de prévenir une perte de contrôle lors de l'entraînement ou des vérifications en vol.
31
VSSE UMQ et RKG
97 UMQ et 95 RKG c'est VMC plus 10
32
explique moi brièvement le moteur critique
Le moteur critique est défini comme le moteur dont la panne produit les effets les plus défavorables sur le contrôle et la performance de l’avion, notamment en ce qui concerne la maîtrise du lacet asymétrique. Sur les bimoteurs conventionnels à hélices tournant vers la droite (sens horaire), il s’agit du moteur gauche, car la perte de ce moteur amplifie le bras de levier du moteur droit encore en marche, ce qui accroît le couple de lacet vers le moteur inopérant. Cette situation est aggravée par des facteurs comme le P-factor, l’effet d’ascenseur spirale et l’asymétrie de souffle de l’hélice, rendant la gouverne de direction moins efficace pour contrer le lacet.