Piper Seneca III PA-34 Flight Quiz
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Questions and Answers

What is the one engine inoperative air minimum control speed (VMCA)?

  • 66 KTS (correct)
  • 82 KTS
  • 92 KTS
  • 75 KTS

The propeller can be feathered when the engine is rotating below 600 RPM.

False (B)

What is the usable fuel tank capacity of the standard tank?

93 US Gallons

In case of engine failure during take-off at 82 KTS, close throttle immediately, apply maximum brakes, switch off __________ and continue straight ahead to stop.

<p>battery</p> Signup and view all the answers

Match the following actions with their corresponding speeds:

<p>One engine inoperative best rate of climb speed = 92 KTS One engine inoperative air minimum control speed = 66 KTS Manual gear extension speed = 85 KIAS Action to recover from spin = Throttle to idle</p> Signup and view all the answers

The landing gear warning will sound when the gear is down and locked.

<p>False (B)</p> Signup and view all the answers

What should be the immediate action to recover from an unintentional spin?

<p>Retard throttle to idle, apply full opposite rudder, control wheel forward, and aileron neutral.</p> Signup and view all the answers

What should a pilot do in the event of propeller over speed?

<p>Retard throttle to full aft and decrease RPM (C)</p> Signup and view all the answers

The normal Cylinder Head Temperature (CHT) range is from 160° F to 460° F.

<p>False (B)</p> Signup and view all the answers

What is the maximum landing gear operating speed for extension?

<p>130 KIAS</p> Signup and view all the answers

The maximum flaps extended speed (VFE) is ____ KIAS.

<p>115</p> Signup and view all the answers

Match the aircraft component with its corresponding specification:

<p>Nose Gear Tire Pressure = 40 PSI Main Gear Tire Pressure = 55 PSI Maximum Take-off RPM = 2800 RPM for 5 minutes One Engine inoperative Air Minimum Control Speed = 66 KIAS</p> Signup and view all the answers

Which of the following describes the nose landing gear's steerable limit?

<p>27° either side of center (D)</p> Signup and view all the answers

The design maneuvering speed increases with lighter weight of the aircraft.

<p>False (B)</p> Signup and view all the answers

What is considered the never exceed speed (VNE)?

<p>205 KIAS</p> Signup and view all the answers

What is the altitude limit for the operation of the Combustion Heater?

<p>Above 25,000 feet (C)</p> Signup and view all the answers

The hydraulic pressure for the landing gear is provided by a manually operated hydraulic pump.

<p>False (B)</p> Signup and view all the answers

What prevents shimming of the nose landing gear?

<p>Centering spring</p> Signup and view all the answers

The starter cranking is limited to ____ seconds.

<p>30</p> Signup and view all the answers

Match the following indicators with their meanings:

<p>Upper red radial line = Never exceed speed (VNE) 205 KIAS Blue radial line = One engine inoperative best rate of climb speed (VYSE) 92 KIAS Lower red radial line = One engine inoperative air minimum control speed (VMCA) 66 KIAS Yellow arc = Caution range of speed (may be used in smooth air only)</p> Signup and view all the answers

How many fuel tank vents are provided?

<p>Two (C)</p> Signup and view all the answers

The stabilator incorporates an anti-servo tab that moves in the opposite direction of the stabilator.

<p>False (B)</p> Signup and view all the answers

What is the type of brake system used in the aircraft?

<p>Separate hydraulic reservoir, 2 single disc, double puck brake assemblies</p> Signup and view all the answers

What is the wing loading of the aircraft?

<p>22.8 Lbs/Sq Ft (C)</p> Signup and view all the answers

The stall warning sound occurs 5 to 10 knots after the stall.

<p>False (B)</p> Signup and view all the answers

What type of propeller is described in the content?

<p>Three blade, constant speed, hydraulically activated, controllable pitch and full feathering Mc Cauley</p> Signup and view all the answers

The fuel selector during single engine operations for the operating engine should be set to _____ and for the inoperative engine to _____.

<p>X-FEED, OFF</p> Signup and view all the answers

Match the following limitations with their descriptions:

<p>Continuous ground operation limitation above 32&quot; of Hg = Avoid continuous operation between 2000 and 2200 RPM Continuous ground operation limitation in X-wind = Avoid continuous operation between 1700 and 2100 RPM Propeller overspeed action = Reduce throttle and maintain 2600 RPM Alternate air usage on ground = Not to be used on ground</p> Signup and view all the answers

What are the consequences of towing an airplane with secured controls?

<p>Damage to the nose gear steering assembly may occur (B)</p> Signup and view all the answers

The basic empty weight includes unusable fuel and full oil.

<p>True (A)</p> Signup and view all the answers

What should be done if the primary air source is blocked?

<p>The automatic alternate air door opens.</p> Signup and view all the answers

What should a pilot do in case of engine failure during take-off with speed more than 85 KTS?

<p>Maintain directional control and close throttle immediately (C)</p> Signup and view all the answers

The maximum drop allowed during feathering check is 400 RPM.

<p>False (B)</p> Signup and view all the answers

What is the stall speed in landing configuration referred to as?

<p>VSO</p> Signup and view all the answers

In the event of hydraulic failure, landing gear will __________.

<p>free fall</p> Signup and view all the answers

What is the correct propeller setting on final approach?

<p>Full forward for a possible go around (C)</p> Signup and view all the answers

Match the following procedures with their descriptions:

<p>Flap position for short-field take-off = 25° Emergency gear extension = Aided by aerodynamic forces and springs Vacuum system = One vacuum pump for each engine Oxygen system malfunction indication = Red pellets are visible</p> Signup and view all the answers

What is the yellow arc on the tachometer indicative of?

<p>2600 to 2800 RPM (B)</p> Signup and view all the answers

What is the maximum landing weight for the aircraft?

<p>4513 Lbs</p> Signup and view all the answers

Flashcards

VMCA (One Engine Inoperative Air Minimum Control Speed)

The minimum airspeed required for control with one engine inoperative.

VYSE (One Engine Inoperative Best Rate of Climb Speed)

The best rate of climb speed with one engine inoperative.

Feathering the Propeller

The process of feathering the propeller to reduce drag when the engine is inoperative. This can only be performed while the engine is rotating above 600 RPM.

Landing Gear Warning

An alert that sounds when the landing gear is not down and locked at low throttle settings.

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Manual Landing Gear Extension

A procedure to extend the landing gear manually in flight. Maintain speed below 85 KIAS, select gear down, and pull the emergency gear extension knob.

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Total Fuel Tank Capacity

The total fuel capacity of the standard tank is 98 US Gallons.

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Usable Fuel Tank Capacity

The usable fuel capacity of the standard tank is 93 US Gallons.

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Engine Failure During Takeoff

A procedure to minimize damage after an engine failure during takeoff. Close throttle, apply brakes, switch off battery, and switch off fuel selector.

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VLE (Maximum Landing Gear Extended Speed)

The maximum speed at which the aircraft can be safely operated with the landing gear extended.

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VLO (Maximum Landing Gear Operating Speed)

The maximum speed at which the aircraft can be safely operated with the landing gear retracted (in the up position).

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VNE (Never Exceed Speed)

The maximum speed at which the aircraft can be operated without being damaged.

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VNO (Maximum Structural Cruising Speed)

The maximum speed at which the aircraft can be safely operated in smooth air. It's the speed at which the aircraft can be safely flown in normal cruising conditions.

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VFE (Maximum Flaps Extended Speed)

The maximum speed at which the aircraft can safely be operated with the flaps fully extended.

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Maximum Take-off RPM

The maximum speed at which the propeller can be operated for 5 minutes. This is not a continuous operating speed.

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Design Maneuvering Speed

A speed that decreases with lighter weights and is the speed at which the aircraft can be safely maneuvered without exceeding structural limits.

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What is engine prime time?

The engine prime time is the amount of time it takes for the engine to start and reach a stable operating condition. It typically varies depending on the ambient temperature.

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How is the landing gear retracted?

The landing gear is retracted into the fuselage using hydraulic pressure.

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What is the function of the Squat Switch?

The Squat Switch prevents the landing gear from retracting when the aircraft is on the ground. It is located on the left main landing gear.

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What is the altitude limit for operating the Combustion Heater?

The Combustion Heater is not approved to be used above 25,000 feet.

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What is the datum of the aircraft?

The datum is a reference point on the aircraft used for measuring distances and locations. For this aircraft, the datum is located 78.4 inches ahead of the wing leading edge at the inboard edge of the inboard fuel tank.

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How is the magnetic drop carried out?

The magnetic drop is a test used to check the health of the engine's magnetos. It involves running the engine at 2000 RPM and measuring the change in RPM when the magnetos are disconnected.

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What happens in case of a Combustion Heater overheat?

The Combustion Heater has a safety feature that automatically cuts off fuel, air, and ignition to the Heater in case of overheating.

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What is the maximum time allowed for starter cranking?

The starter cranking is limited to 30 seconds to prevent damage to the starter motor.

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Stall speed (VSO)

The minimum steady speed at which the aircraft is controllable in the landing configuration.

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Feathering Procedure

Feathering a propeller involves decreasing the pitch, reducing the drag and preventing the propeller from windmilling in case of engine failure.

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Engine Operating Limits

The engine operating limits for your aircraft are 40 inches of manifold pressure (MAP), 2800 RPM, and 220 BHP for a maximum of 5 minutes.

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Yellow Arc on Tachometer

The yellow arc on the tachometer indicates the RPM range for take-off, which is 2600 to 2800 RPM for a maximum of 5 minutes.

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Auxiliary Fuel Pump

The auxiliary fuel pump is used to supply fuel in case of failure of the engine-driven pump and for vapour suppression.

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Vacuum System

The vacuum system in the aircraft is powered by one vacuum pump per engine and includes plumbing and regulating equipment.

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Maximum Landing Weight

The maximum landing weight for your aircraft is 4513 lbs.

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LO BUS Voltage Annunciator

The LO BUS voltage annunciator will illuminate when the total BUS voltage falls below approximately 25 volts DC.

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Wing Loading

The weight of the aircraft divided by the wing area. It indicates how much weight each square foot of the wing needs to support.

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Power Loading

The weight of the aircraft divided by the engine horsepower. It tells us how much weight each horsepower needs to push.

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Stall Warning

A warning system that alerts the pilot when the aircraft is approaching a stall. It sounds 5 to 10 knots before the actual stall, accompanied by mild airframe buffeting and gentle pitching.

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Stall Warning Type

The type of stall warning system used in this aircraft. It uses a continuous horn, distinct from the landing gear warning horn which has a faster beep.

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Towing the Aircraft

The process of moving the aircraft on the ground. It can be done using the nose wheel steering bar stored in the baggage compartment or with specialized towing equipment. Do not tow with the controls secured.

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Propeller Type

The type of propeller used in this aircraft. It is a three-blade, constant speed propeller with hydraulic activation. It has a controllable pitch and full feathering capabilities and is directly connected to the crankshaft.

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Fuel Selector for Single-Engine Operations

The fuel selector position setting for single-engine operations. The operating engine is selected to X-FEED, and the inoperative engine is set to OFF.

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Alternate Air

The alternate air system is designed to provide air to the engine if the primary air source is blocked. However, the alternate air is unfiltered and should not be used on the ground.

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Study Notes

Piper Seneca III PA-34 220T Questions

  • One Engine Inoperative Air Minimum Control Speed (VMCA): 66 KTS
  • One Engine Inoperative Best Rate of Climb Speed (VYSE): 92 KTS
  • Engine Failure Below 66 KTS: Apply rudder towards operative engine, retard throttle to stop yaw forces.
  • Propeller Feathering: Only possible while engine rotates above 600 RPM.
  • Landing Gear Warning Sound: Occurs at low throttle setting when gear is not down and locked.
  • Manual Landing Gear Extension: Maintain speed below 85 KIAS, switch to gear down, and use emergency gear extension knob.
  • Standard Fuel Tank Capacity: 98 US Gallons
  • Usable Fuel Tank Capacity: 93 US Gallons
  • Battery Type: 24 Volt, 65 Amp (19 AH)
  • Alternator Type: 2 x 28 Volt 60 Amperes
  • Engine Controls: Throttle lever, Mixture control lever, and Propeller control lever
  • Unintentional Spin Recovery: Retard throttle to idle, apply full opposite rudder, and control wheel forward with aileron neutral.
  • Nose Landing Gear Extension Assist: Aerodynamic load and springs
  • Propeller Overspeed Procedure: Retard throttle to full aft and move propeller control to full decrease RPM
  • Nose Landing Gear Steerability: 27° either side of center
  • Center of Gravity Limit (3400 kg): 94.6"
  • Engine Failure Identification: Loss of thrust and yaw towards inoperative engine
  • Normal CHT Range: 240° to 460° F
  • Normal EGT Range: 1200° to 1525° F
  • Design Maneuvering Speed: 140 KIAS, decreases with lighter aircraft weight
  • Main Gear Tyre Pressure: 55 PSI
  • Nose Gear Tyre Pressure: 40 PSI
  • Maximum Flaps Extended Speed (VFE): 115 KIAS
  • Maximum Landing Gear Extended Speed (VLE): 130 KIAS
  • Maximum Landing Gear Operating Speed (VLO): Extension: 130 KIAS; Retraction: 108 KIAS
  • Never Exceed Speed (VNE): 205 KIAS
  • Maximum Structural Cruising Speed (VNO): 166 KIAS
  • Maximum Take-off RPM: 2800 RPM for 5 minutes
  • Oil Viscosity (Below 40°F): 1065 (Aviation Grade), SAE 30
  • Oil Viscosity (Above 40°F): 1100 (Aviation Grade), SAE 50
  • Wing Loading: 22.8 Lbs/Sq Ft
  • Power Loading: 10.8 Lbs/HP
  • Engine Stall Warning: 5 to 10 knots prior to actual stall, with mild buffeting and pitching
  • Stall Warning Type: Continuous horn, different from landing gear warning horn (90 cycles/second)
  • Aircraft Towing: Using nose wheel steering bar, or power equipment avoiding nose gear stress.
  • Propeller Type: Three blade, constant speed, hydraulically activated, controllable pitch
  • Fuel Selector During Single Engine Operations: Selector for operating engine: X-FEED; Selector for inoperative engine: OFF
  • Alternate Air Use: Not permitted on ground
  • Basic Empty Weight: Standard empty weight + optional equipment + unusable fuel + oil + unusable fluids
  • Continuous Ground Operation Limitation (Above 32") Between 2000 and 2200 RPM
  • Continuous Ground Operation Limitation (X-Wind/Tail Wind): Between 1700 and 2100 RPM
  • Propeller Overspeed Procedure: Reduce throttle to reduce RPM (do not feather) if propeller governor malfunctions, check control availability, decrease airspeed
  • Alternate Air Source: Automatic alternate air door opens; if primary air source is blocked it is unfiltered, so should not be used for ground operations
  • Engine Failure During Take-off (Speed > 85 KTS): Maintain directional control, immediately close throttle, land if airborne, stop straight ahead, and apply brakes
  • Feathering Procedure: Throttle retard, verifying propeller feathering at > 800 RPM, mixture to idle cutoff, cowl flaps closed, alternator off, fuel selector off, reduce electrical load and cross-feed
  • Emergency Gear Extension Aid: Aerodynamic forces and springs
  • Engine Operating Limits: 40" Hg MAP/2800 RPM/220 BHP for 5 minutes
  • Yellow Arc on Tachometer: 2600 to 2800 RPM (take-off RPM for 5 minutes)
  • Prime Time/Ambient Temperature Relationship: Prime time increases if ambient temperature decreases
  • Maximum Feathering Drop: 300 RPM
  • Normal Take-off Procedure: RPM 2800 before releasing brakes < full throttle, 40″ of Hg MAP
  • Flap Position for Short Field Take-off: 25°
  • Hydraulic Failure in Landing Gear: Landing gear will free fall
  • Final Propeller Setting: Full forward
  • Vacuum System: One vacuum pump per engine; plumbing and regulating equipment
  • Oxygen System Malfunction Indicator: Visible red pellets
  • Propeller Setting for Taxi: High RPM low pitch
  • Emergency Gear Extension Knob Action: Releases hydraulic pressure on the landing gear.
  • Auxiliary Fuel Pump Function: Provides fuel supply in case of engine driven pump failure, and ensures vapor suppression
  • Minimum Controllable Speed (VSO): Minimum steady flight speed in landing configuration
  • Maximum Landing Weight: 4513 lbs

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Piper Seneca III PA-34 220T Questions PDF

Description

Test your knowledge on the Piper Seneca III PA-34 220T with this quiz. Topics include engine performance, emergency procedures, and aircraft specifications. Perfect for both aspiring pilots and aviation enthusiasts!

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