Exams4Pilots Logo


  Quick Links   
Take a Practice Exam
Contribute to the Site
About this Site
Privacy Policy
Terms & Conditions
New User
Log In
Examine My Cookies
Contact WebMaster
  FAA Written Test Prep   
for Windows PCs
for Mac
for iPhone and iPad
for Android
MP3 Audio
 

 
Showing results 161 - 170 of 981 total.
prev 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 next

1.5.1.2.7.B.1
CGX
Knowledge Code: A20
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.
view comments
Modified: 7/26/2004 kapatten
Comments: 0
make comment

1.5.1.2.8.B.1
CAX CBG CBH CGX CLA CRG CRH MCA MCH
Knowledge Code: A21
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.
view comments
Modified: 7/16/2004 kip
Comments: 1
make comment

1.5.1.2.9.B.1
CAX CBG CBH CGX CLA CRG CRH MCA MCH
Knowledge Code: B12
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).
view comments
Modified: 7/24/2004 kapatten
Comments: 0
make comment

2.5.1.5.1.A.1
CAX CBG CBH CGX CLA CRG CRH MCA MCH
Knowledge Code: H303
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.
view comments
Modified: 7/26/2004 kapatten
Comments: 0
make comment

2.5.1.5.2.A.1
CAX CBG CBH CGX CLA CRG CRH MCA MCH
Knowledge Code: H303
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.
view comments
Modified: 7/26/2004 kapatten
Comments: 1
make comment

2.5.1.5.3.A.1
CAX CBG CBH CGX CLA CRG CRH MCA MCH
Knowledge Code: H303
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.
view comments
Modified: 7/26/2004 kapatten
Comments: 1
make comment

2.5.1.5.4.A.1
CAX CBG CBH CGX CLA CRG CRH MCA MCH
Knowledge Code: H303
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.
view comments
Modified: 7/26/2004 kapatten
Comments: 1
make comment

2.5.1.5.5.A.1
CAX CBG CBH CGX CLA CRG CRH MCA MCH
Knowledge Code: H303
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.
view comments
Modified: 7/26/2004 kapatten
Comments: 0
make comment

2.5.1.5.6.A.1
CAX CBG CBH CGX CLA CRG CRH MCA MCH
Knowledge Code: H303
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.
view comments
Modified: 7/26/2004 kapatten
Comments: 1
make comment

2.5.1.5.8.A.1
CAX CBG CBH CGX CLA CRG CRH MCA MCH
Knowledge Code: H300
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.
view comments
Modified: 7/26/2004 kapatten
Comments: 1
make comment

Showing results 161 - 170 of 981 total.
prev 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 next