Flaps at landing position - Study guides, Class notes & Summaries

Gleim Private Pilot FAA Knowledge Test Guide Gleim Private Pilot FAA Knowledge Test Guide What is one purpose of wing flaps? To enable the pilot to make steeper approaches to a landing without increasing the airspeed. One of the main functions of flaps during approach and landing is to: Increase the angle of descent without increasing the airspeed. What is the purpose of the rudder on an airplane? To control yaw. Which is not a primary flight control surface? A. Flaps B. Stabilat...

Datum Line - ANSWER Imaginary point on the aircraft picked by the manufacturer to measure CG Arm - ANSWER Horizontal distance (in) from datum to CG CG range - ANSWER the distance between forward and aft CG position limits to retain airplane controllability Floor load limit - ANSWER The maximum weight the floor can sustain per square inch/foot as provided by the manufacturer. fuel load - ANSWER usable fuel Empty Weight - ANSWER Weight of plane excluding people and luggage Max ramp weight...

What are the full names of the following airports? STN PIK CIA MAD NYO - Answer- STN - London Stansted PIK - Glasgow Preswick CIA - Ciampino MAD - Madrid NYO - Stockholm Skavsta Explain the following terminology? AFT IAA Ditching PA THOB - Answer- AFT - Towards the tail of the ac IAA - Irish Aviation Authority Ditching - Emergency landing on water PA - Passenger announcement THOB - Total Heads on board How many CC are required on a Boeing 737-800 ac? Explain. - Answer- 4...

1. While approaching the airport, you are 15 miles from the runway at 3,000 AFL. As you begin to configure the aircraft for landing, when would you expect the hydraulic ACMP's 1 and 2 to turn on? - ️️When the flaps are selected to any position greater than 0 10. In the event of a total loss of hydraulic systems 1 and 2 the only way to stop the aircraft is with reverse thrust? - ️️False 100. What is the minimum fuel temperature for the ERJ-175? - ️️-37C 101. Prior to pushback, yo...

24 ft 10 in/24 ft 1 in/24 ft 1 in CORRECT ANSWER-1. What is the height of the tail? 700/900/900EP 42,000 lbs/45,000 lbs/45,000 lbs CORRECT ANSWER-2. Minimum Flight weight? 700/900/900EP 10 kts CORRECT ANSWER-3. Max Tailwind for Takeoff and Landing? 182 ktg/195 ktg/ 195 ktg CORRECT ANSWER-4. Max Tire Speed? 700/900/900EP All aircraft types: 19,594 lbs Total/7,492 lbs Mains/4610 lbs Center CORRECT ANSWER-5. Max Refueling Fuel Pressurized 700/900/900EP Parking brake . . . . . . . . ....

Maximum start EGT is ___ -Correct Answer 725 C The maximum runway slope allowed for P-8A operations is ___ -Correct Answer +/- 2% Maximum takeoff and landing tailwind component is ___ -Correct Answer 15 knots Maximum operating altitude is ___ -Correct Answer 41,000' MSL Maximum takeoff and landing altitude is ___ -Correct Answer 8,400' MSL For RVSM operations, when field elevation is between sea level and 5,000', the maximum allowable difference between PFD altitude displays is...

Horizontal Stabilizer - ANSWERSWhat aircraft part is the letter 1? Fuselage - ANSWERSWhat aircraft part is number 2? Landing Flaps - ANSWERSWhat aircraft part is number 3? Rudder - ANSWERSWhat aircraft part is number 4? Leading Edge, Left Wing - ANSWERSWhat aircraft part is number 5? Vertical Stabilizer - ANSWERSWhat aircraft part is number 6? High wing-externally braced; Tricycle type landing gear - ANSWERSThe airplane in the diagram may best be described as? Nose Wheel - A...

fixed-wing aircraft structure 1. Fuselage 2. Wings 3. Tail assembly or empennage 4. Landing gear 5. Powerplant 6. Flight instruments/controls and control surfaces fuselage body of an airplane. Contains the cockpit, the cabin, the cargo area if there is one, and attachment points for other major airplane components, such as wings, tail section, and landing gear. cockpit from which the pilots and the flight crew control the aircraft's operations Two design types of ...

Pilots shall not exchange seats during flight if only two pilots are aboard the airplane correct answers True Verbal coordination between applicable crewmembers will be required when: correct answers A. Control of the airplane is transferred between pilot and copilot or when an autopilot mode or axis is engaged. B. Repositioning fuel panel valves and switches or when an electrical power source is changed. C. A crewmember leaves position or leaves interphone or goes on or off oxygen. D. Any...

PSA Airlines Study Questions And Answers 100% Guaranteed Success. Lowest CAT 1 ILS Visibility - correct answer. 1800RVR First officer low time minimum visibility - correct answer. 4000RVR or 3/4 sm Lowest visibility OPSPEC - correct answer. 500' 500' 500 How many transmitometers needed for below 1600rvr - correct answer. 2 When do we need a take off alternate - correct answer. Cannot get back to the departure airport on lowest CAT 1 ap...