Podcast
Questions and Answers
What is the maximum KIAS speed for flap extension?
What is the maximum KIAS speed for flap extension?
- 103 KIAS (correct)
- 100 KIAS
- 160 KIAS
- 126 KIAS
What is the never exceed speed (VNE) in KCAS?
What is the never exceed speed (VNE) in KCAS?
- 122 KCAS
- 100 KCAS
- 153 KCAS (correct)
- 160 KCAS
What is the minimum fuel pressure?
What is the minimum fuel pressure?
- 25 PSI
- 8 PSI
- 5 PSI
- 0.5 PSI (correct)
What range should you expect to see when checking the vacuum gauge during the ground check?
What range should you expect to see when checking the vacuum gauge during the ground check?
What are the static RPM limits at maximum permissible throttle setting, sea level, and ISA for the 74DM6-0-60 propeller?
What are the static RPM limits at maximum permissible throttle setting, sea level, and ISA for the 74DM6-0-60 propeller?
What is the oil capacity of the engine in the PA-28-161 Warrior II?
What is the oil capacity of the engine in the PA-28-161 Warrior II?
The PA-28-161 Warrior II is approved for acrobatic maneuvers in the normal category.
The PA-28-161 Warrior II is approved for acrobatic maneuvers in the normal category.
What is the maximum demonstrated crosswind velocity for the PA-28-161 Warrior II?
What is the maximum demonstrated crosswind velocity for the PA-28-161 Warrior II?
The unusable fuel for this airplane is 5.0 gallon.
The unusable fuel for this airplane is 5.0 gallon.
Which aviation fuel grade is approved for use in the PA-28-161 Warrior II?
Which aviation fuel grade is approved for use in the PA-28-161 Warrior II?
What is the engine rotation speed (RPM) limit?
What is the engine rotation speed (RPM) limit?
What is the minimum and maximum propeller diameters in inches?
What is the minimum and maximum propeller diameters in inches?
This airplane may only be operated in day VFR if all equipment required for the operation is installed and operable.
This airplane may only be operated in day VFR if all equipment required for the operation is installed and operable.
What is the maximum oil temperature?
What is the maximum oil temperature?
What is the Utility Category Maximum Takeoff Weight?
What is the Utility Category Maximum Takeoff Weight?
What is the Normal Category Maximum Ramp Weight?
What is the Normal Category Maximum Ramp Weight?
In utility category operation, no aft passengers and baggage are allowed.
In utility category operation, no aft passengers and baggage are allowed.
The datum used to determine the weight and center of gravity is how many inches ahead of the wing?
The datum used to determine the weight and center of gravity is how many inches ahead of the wing?
What is the entry speed into steep turns?
What is the entry speed into steep turns?
Approved maneuvers for bank angles exceeding 60° in the utility category include?
Approved maneuvers for bank angles exceeding 60° in the utility category include?
What is the maximum positive load factor in Normal category?
What is the maximum positive load factor in Normal category?
What is the maximum positive load factor in Utility category?
What is the maximum positive load factor in Utility category?
This airplane is approved for inverted maneuvers in utility category.
This airplane is approved for inverted maneuvers in utility category.
The usable fuel in this airplane has been determined as how many gallons in each wing?
The usable fuel in this airplane has been determined as how many gallons in each wing?
The noise level of this aircraft is?
The noise level of this aircraft is?
When the air conditioner is installed, it must be off to ensure normal takeoff climb performance.
When the air conditioner is installed, it must be off to ensure normal takeoff climb performance.
To close the cabin door in flight the maximum speed in KIAS is:
To close the cabin door in flight the maximum speed in KIAS is:
What should you do with the strobe lights when in close proximity to the ground or during flight through cloud, fog or haze?
What should you do with the strobe lights when in close proximity to the ground or during flight through cloud, fog or haze?
During power off landing procedure what will be the trim setting KIAS?
During power off landing procedure what will be the trim setting KIAS?
What is the U.S. gallon capacity of the fuel tanks in the piper warrior?
What is the U.S. gallon capacity of the fuel tanks in the piper warrior?
With no flaps, what airspeed should be maintained with an engine power loss?
With no flaps, what airspeed should be maintained with an engine power loss?
In normal procedures what should be the rate of climb in KIAS?
In normal procedures what should be the rate of climb in KIAS?
In normal procedures what is the best angle of climb airspeed in KIAS?
In normal procedures what is the best angle of climb airspeed in KIAS?
During a normal descent what is the recommended power setting?
During a normal descent what is the recommended power setting?
During a normal descent what airspeed should be used?
During a normal descent what airspeed should be used?
During approach and landing what should you trim to in KIAS?
During approach and landing what should you trim to in KIAS?
During approach and landing what is the final approach speed used with flaps extended to 40 degrees in KIAS?
During approach and landing what is the final approach speed used with flaps extended to 40 degrees in KIAS?
The electric fuel pump should be turned OFF during normal takeoff.
The electric fuel pump should be turned OFF during normal takeoff.
While performing short field takeoff what airspeed should you lift off at in KIAS?
While performing short field takeoff what airspeed should you lift off at in KIAS?
When comitted to landing, at lowest possible airspeed, what procedure should you do?
When comitted to landing, at lowest possible airspeed, what procedure should you do?
What is the first action to a carburetor icing problem that is indicated by a drop in RPM and may be accompanied by a slight loss of airspeed or altitude?
What is the first action to a carburetor icing problem that is indicated by a drop in RPM and may be accompanied by a slight loss of airspeed or altitude?
What is the rated horsepower of the Lycoming O-320-D2A or O-320-D3G engine used in the PA-28-161 Warrior II?
What is the rated horsepower of the Lycoming O-320-D2A or O-320-D3G engine used in the PA-28-161 Warrior II?
The PA-28-161 Warrior II has a useable fuel capacity of 50 U.S. gallons.
The PA-28-161 Warrior II has a useable fuel capacity of 50 U.S. gallons.
What is the maximum oil temperature as indicated by the red line on the oil temperature gauge?
What is the maximum oil temperature as indicated by the red line on the oil temperature gauge?
What is the minimum fuel grade (AVGAS) approved for use in the PA-28-161 Warrior II?
What is the minimum fuel grade (AVGAS) approved for use in the PA-28-161 Warrior II?
The maximum allowable baggage weight in the baggage compartment is 250 lbs.
The maximum allowable baggage weight in the baggage compartment is 250 lbs.
What is the maximum permissible rotation speed (RPM) for the engine?
What is the maximum permissible rotation speed (RPM) for the engine?
What is the never exceed speed (VNE) in knots calibrated airspeed (KCAS) for the PA-28-161?
What is the never exceed speed (VNE) in knots calibrated airspeed (KCAS) for the PA-28-161?
What is the maximum flap extended speed (VFE) in knots indicated airspeed (KIAS)?
What is the maximum flap extended speed (VFE) in knots indicated airspeed (KIAS)?
What is the minimum propeller diameter allowed, in inches?
What is the minimum propeller diameter allowed, in inches?
What is the design maneuvering speed ($V_A$) at 2440 lbs gross weight, in knots indicated airspeed (KIAS)?
What is the design maneuvering speed ($V_A$) at 2440 lbs gross weight, in knots indicated airspeed (KIAS)?
Which of the following maneuvers are prohibited in the normal category?
Which of the following maneuvers are prohibited in the normal category?
Approved maneuvers for the utility category involving bank angles exceeding 60° require an entry speed of:
Approved maneuvers for the utility category involving bank angles exceeding 60° require an entry speed of:
What is the allowable fuel imbalance between tanks during flight operations?
What is the allowable fuel imbalance between tanks during flight operations?
What action should be taken if an alternator overload is observed (more than 20 amps above known electrical load)?
What action should be taken if an alternator overload is observed (more than 20 amps above known electrical load)?
When operating with light electrical load and a fully charged battery, the Alternator Inop. light may flicker due to excessive alternator output.
When operating with light electrical load and a fully charged battery, the Alternator Inop. light may flicker due to excessive alternator output.
What is the procedure for a spin recovery?
What is the procedure for a spin recovery?
Carburetor heat should only be used when ice is present or suspected, as it reduces engine output.
Carburetor heat should only be used when ice is present or suspected, as it reduces engine output.
Below what Outside Air Temperature ($OAT$) should the oil cooler winterization plate be installed, in degrees Fahrenheit?
Below what Outside Air Temperature ($OAT$) should the oil cooler winterization plate be installed, in degrees Fahrenheit?
The air conditioning must be off to insure
The air conditioning must be off to insure
What is the demonstrated crosswind velocity (knots) with flaps?
What is the demonstrated crosswind velocity (knots) with flaps?
Match the airspeed with the action
Match the airspeed with the action
If an electrical wire is present and indicted in the cabin, what position should the Master switch be?
If an electrical wire is present and indicted in the cabin, what position should the Master switch be?
If an engine fire is present, what position should the fuel selector?
If an engine fire is present, what position should the fuel selector?
If there is too much ice is allowered accumulate what could occur?
If there is too much ice is allowered accumulate what could occur?
To close the door in flight: Slow airplane to ______ KIAS
To close the door in flight: Slow airplane to ______ KIAS
Tachometer Green Arc (Normal Operating Range
Tachometer Green Arc (Normal Operating Range
Tachometer Red Line (Maximum Continuous Power)
Tachometer Red Line (Maximum Continuous Power)
Maximum Weight (lbs), Normal
Maximum Weight (lbs), Normal
Maximum Weight (lbs), Utility
Maximum Weight (lbs), Utility
Is it important to make sure the airplane that the airplane is properly loaded?
Is it important to make sure the airplane that the airplane is properly loaded?
Normal max power
Normal max power
NORMAL Throttle
NORMAL Throttle
NORMAL Airspeed
NORMAL Airspeed
NORMAL Mixture
NORMAL Mixture
NORMAL Carburetor heat settting only required if required
NORMAL Carburetor heat settting only required if required
Best angle of climb speed
Best angle of climb speed
Best rate of climb
Best rate of climb
Vso speed (knots)
Vso speed (knots)
Is it permissible, or not, to perform a preflight outside a hanger?
Is it permissible, or not, to perform a preflight outside a hanger?
What is the rated horsepower of the Lycoming engine used in the PA-28-161 Warrior II?
What is the rated horsepower of the Lycoming engine used in the PA-28-161 Warrior II?
What is the maximum rotation speed (RPM) for the PA-28-161's engine?
What is the maximum rotation speed (RPM) for the PA-28-161's engine?
What is the maximum oil temperature for the PA-28-161 Warrior II?
What is the maximum oil temperature for the PA-28-161 Warrior II?
What is the minimum fuel pressure for the PA-28-161 Warrior II?
What is the minimum fuel pressure for the PA-28-161 Warrior II?
What is the Never Exceed Speed (VNE) in KIAS for the PA-28-161?
What is the Never Exceed Speed (VNE) in KIAS for the PA-28-161?
The maximum baggage weight in the baggage compartment of the PA-28-161 Warrior II is 220 lbs.
The maximum baggage weight in the baggage compartment of the PA-28-161 Warrior II is 220 lbs.
What is the fuel capacity (U.S. gallons total) for the PA-28-161 Warrior II?
What is the fuel capacity (U.S. gallons total) for the PA-28-161 Warrior II?
What is the utility category maximum takeoff weight (lbs) for the PA-28-161 Warrior II?
What is the utility category maximum takeoff weight (lbs) for the PA-28-161 Warrior II?
What is the normal category maximum takeoff weight (lbs) for the PA-28-161 Warrior II?
What is the normal category maximum takeoff weight (lbs) for the PA-28-161 Warrior II?
The usable fuel for the PA-28-161 is 1.5 gallons in each wing.
The usable fuel for the PA-28-161 is 1.5 gallons in each wing.
What are maneuvers for bank angles exceeding 60° approved to perform in Utility Category entry speeds for Steep Turns, Lazy Eights and Chandelles?
What are maneuvers for bank angles exceeding 60° approved to perform in Utility Category entry speeds for Steep Turns, Lazy Eights and Chandelles?
What is the total amount of unusable fuel in the PA-28-161?
What is the total amount of unusable fuel in the PA-28-161?
The maximum structural cruising speed (VNO) - Do not exceed this speed except in smooth air and then only with caution, is ____________ KCAS.
The maximum structural cruising speed (VNO) - Do not exceed this speed except in smooth air and then only with caution, is ____________ KCAS.
What are the propeller models used?
What are the propeller models used?
What kind of grade the fuel must be for the PA-28-161 Warrior II aircraft?
What kind of grade the fuel must be for the PA-28-161 Warrior II aircraft?
Match the following terms with their descriptions:
Match the following terms with their descriptions:
What instruments are required by the FAA for day VFR flight?
What instruments are required by the FAA for day VFR flight?
How do you check if the stall warning system is working properly?
How do you check if the stall warning system is working properly?
When operating in the Utility category what acrobatic maneuvers are authorized?
When operating in the Utility category what acrobatic maneuvers are authorized?
Flashcards
VNE (Never Exceed Speed)
VNE (Never Exceed Speed)
Maximum speed; exceeding it could cause structural damage.
VNO (Maximum Structural Cruising Speed)
VNO (Maximum Structural Cruising Speed)
Maximum structural cruising speed; exceeding it should be done with caution.
VS (Stalling Speed)
VS (Stalling Speed)
Stalling speed; minimum steady flight speed at which the airplane is controllable.
VSO (Stalling Speed Landing Configuration)
VSO (Stalling Speed Landing Configuration)
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VX (Best Angle-of-Climb Speed)
VX (Best Angle-of-Climb Speed)
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VY (Best Rate-of-Climb Speed)
VY (Best Rate-of-Climb Speed)
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VFE (Maximum Flap Extended Speed)
VFE (Maximum Flap Extended Speed)
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VA (Design Maneuvering Speed)
VA (Design Maneuvering Speed)
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ISA standard temperature
ISA standard temperature
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OAT (Outside Air Temperature)
OAT (Outside Air Temperature)
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Indicated Pressure Altitude
Indicated Pressure Altitude
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Pressure Altitude
Pressure Altitude
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Station Pressure
Station Pressure
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Takeoff Power
Takeoff Power
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Maximum Continuous Power
Maximum Continuous Power
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Maximum Climb Power
Maximum Climb Power
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Maximum Cruise Power
Maximum Cruise Power
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Climb Gradient
Climb Gradient
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Demonstrated Crosswind Velocity
Demonstrated Crosswind Velocity
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Accelerate-Stop Distance
Accelerate-Stop Distance
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Reference Datum
Reference Datum
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Station
Station
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Arm
Arm
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Moment
Moment
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Center of Gravity (C.G.)
Center of Gravity (C.G.)
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C.G. Arm
C.G. Arm
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C.G. Limits
C.G. Limits
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Usable Fuel
Usable Fuel
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Unusable Fuel
Unusable Fuel
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Standard Empty Weight
Standard Empty Weight
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Payload
Payload
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Maximum Ramp Weight
Maximum Ramp Weight
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Maximum Takeoff Weight
Maximum Takeoff Weight
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Maximum Landing Weight
Maximum Landing Weight
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Maximum Zero Fuel Weight
Maximum Zero Fuel Weight
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Airspeed indicator markings KIAS
Airspeed indicator markings KIAS
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Airspeed indicator markings KCAS
Airspeed indicator markings KCAS
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Normal operating range in rpm
Normal operating range in rpm
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Maximum continueous RPM
Maximum continueous RPM
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Normal Operating rang for oil tempertures
Normal Operating rang for oil tempertures
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Maximum, Red Line for Temperature on engine oil
Maximum, Red Line for Temperature on engine oil
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Limits for Optimal preasure in PSI
Limits for Optimal preasure in PSI
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Total capasity
Total capasity
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un useable capacity
un useable capacity
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Airspeeds for safe operartions
Airspeeds for safe operartions
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Best rate (Flaps up)
Best rate (Flaps up)
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best ancel flapped up
best ancel flapped up
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Study Notes
Warrior II PA-28-161: Study Notes
Speeds
- Never Exceed Speed (VNE) is 160 KIAS or 153 KCAS; this speed must never be exceeded.
- Maximum Structural Cruising Speed (VNO) is 126 KIAS or 122 KCAS; this speed should not be exceeded except in smooth air and even then, with caution.
- Maximum Flaps Extended Speed (VFE) is 103 KIAS or 100 KCAS; this speed should not be exceeded when flaps are extended.
- Design Maneuvering Speed (VA) at 2440 lbs GW is 111 KIAS.
- Design Maneuvering Speed (VA) At 1531 lbs GW is 88 KIAS.
- Maneuvering speed decreases as weight decreases due to more pronounced aerodynamic forces, maneuvering speed should not be exceeded during rough air.
- Best rate of climb w/ flaps up is 79 KIAS
- Best angle of climb w/ flaps up is 63 KIAS
- Enroute climb is 87 KIAS
- Landing final approach speed (Flaps 40°) 63 KIAS
- Turbulent Air Operating Speed is 111 KIAS.
Operating Limits
- This Warrior II PA-28-161 airplane is FAA-approved for normal and utility categories
- The airplane must be operated in compliance with the operating limitations stated in the form of placards, markings, and manuals.
- Acrobatic maneuvers, including spins, are prohibited in the normal category.
- Approved Maneuvers for the Utility Category with bank angles beyond 60° are steep turns, lazy eights, and chandelles, and entry speed for each maneuver is 111 KIAS.
Capacities
- Total fuel capacity is 50 US gallons.
- Usable fuel is 48 US gallons, determined as 24.0 gallons available in each wing.
- Unusable fuel is 2 US gallons, determined as 1.0 gallon in each wing in critical flight attitudes.
- Oil capacity is 8 US quarts.
Weight Limits
- Maximum Takeoff Weight (Normal Category): 2,440 lbs.
- Maximum Takeoff Weight (Utility Category): 2,020 lbs.
- Maximum Ramp Weight (Normal Category): 2,447 lbs.
- Maximum Ramp Weight (Utility Category): 2,027 lbs.
- Maximum Landing Weight (Normal & Utility Category): 2,440 lbs. or 2,020 lbs.
- Maximum Weight in Baggage Compartment: 200 lbs. In normal category, 0 lbs. in utility category.
Power Plant and Instrument Markings
- The aircraft is powered by a Lycoming O-320-D2A or O-320-D3G engine.
- The engine is a four-cylinder, direct drive, horizontally opposed, air-cooled type.
- Maximum horsepower is 160.
- Maximum rotation speed is 2700 RPM.
- Maximum oil temperature is 245°F.
- Minimum oil pressure is 25 PSI.
- Maximum oil pressure is 100 PSI.
- Minimum fuel pressure is 0.5 PSI; maximum fuel pressure is 8 PSI.
- Tachometer green arc (normal operating range) is 500 to 2700 RPM.
- The red line (maximum continuous power) on the tachometer is 2700 RPM.
- Oil temperature green arc (normal operating range) is 75° to 245°F.
- Oil temperature red line (maximum) is 245°F.
- Oil pressure green arc (normal operating range) is 60 PSI to 90 PSI.
- Oil pressure yellow arc (caution range, idle) is 25 PSI to 60 PSI; yellow arc (ground warm-up) from 90 PSI to 100 PSI.
- Oil pressure red line (minimum) is 25 PSI; red line (maximum) is 100 PSI.
- Fuel pressure green arc (normal operating range) is 0.5 PSI to 8 PSI.
- Fuel pressure red line (minimum) is 0.5 PSI; red line (maximum) is 8 PSI.
- Propeller Model Numbers are 74DM6-0-60 or 74DM6-0-58,.
- Propeller static rpm at maximum permissible throttle setting, Sea Level, ISA: 74DM6-0-60 must not be above 2430 RPM and not below 2330 RPM,. test procedure to determine approved static rpm under non standard conditions in airplane maintenance manual --static rpm at maximum permissible throttle setting: 74DM6-0-58 must not be above 2465 RPM and not below 2365 RPM,., under non standard conditions same as above
Limitations
- Approved fuel is AVGAS only, minimum grade 100 or 100LL Aviation Grade.
Placards
- Examples of required are: to "Operate This Airplane as a Normal Or Utility Category Airplane" or "All Markings And Placards As A Utility Category Airplane",
- Baggage limits are 200lbs, or in utility mode - No Aft Passengars Allowed etc.
Flight Load Factors
- Normal category- Positive (Up) 3.8 G, Negative (Down) - No Inverted Manuevers Allowed
- Utility Category Positive (Up) 4.4G Negative (Down)- No Inverted Manuevers Allowed
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