Tailwind component - Study guides, Class notes & Summaries

High min CA - Answer-Must make all T/O & Landing Mins increase by 100' n 1/2 m vis above MDA and can't go no lower that 300/1 F/O Restriction - Answer-CA will make all TO n Land when: Wx <cat 1 IFR min RWY shorter than 4,500' Braking less than Fair When he determine conditions need it FO restriction <100hr - Answer-CA will make all TO n Land when: Special use airport When vis at or lower 3/4:RVR 4000 RWY contaminate do:Water snow slush etc Braking less than Good 15 knot ...

SUU AVIATION EOC Exam Questions and Answers What is the maximum demonstrated crosswind component for your aircraft? Can you legally land with a crosswind stronger than max demonstrated? - Answer- How does density altitude effect aircraft performance? - Answer- What is an accelerate stop distance? How do you use an accelerate stop distance in your preflight planning? - Answer- What is the glide ratio of your aircraft? How do you use this information in flight? - Answer- What is the ...

ATR 72-600 Exam Questions And Answers Maximum Operating Altitude 25,000 feet Maneuvering Limit Load Factors, gear and flaps retracted -1 (g) gees, to 2.5 (g) gees Brainpower Read More Previous Play Next Rewind 10 seconds Move forward 10 seconds Unmute 0:01 / 0:15 Full screen Maneuvering Limit Load Factors, gear and/or flaps extended 0 (g) gees, to 2.5 (g) gees Cargo door crosswind component limitation Do not operate cargo door with a crosswind component of ...

GoJet CRJ-700 Flight Safety PowerPoint Question and answers 100% correct 2023/2024What is the minimum air temperature for flight - correct answer -70 degrees centigrade What is the turbulence penetration airspeed - correct answer 280 KIAS/ .75 MACH What is the maximum tailwind component - correct answer 10 Knots What is the minimum pavement for and 180 degree turn - correct answer 75 feet Door support cable must be installed when moving the aircraft with the passenger door open or th...

Maximum 90 degree crosswind for takeoff and landing - Answer 27 knots Maximum 90 degree crosswind landing for Category II Approach - Answer 15 knots Maximum headwind for landing from a Category II Approach - Answer 16 knots Maximum Tailwind Component for Takeoff/Landing - Answer 10 knots Maximum runway slope approved for takeoff and landing - Answer +2.0% (uphill) -2.0% (downhill)

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...

MESA Airlines E-175 Study Guide (Limitations)Engine Starter Duty Cycle Limits How many attempts and Limits? - correct answer (5) Attempts, First 2 Attempts, (Ground) 90 sec ON/10 sec OFF (Airborne) 120sec ON/10 sec OFF Attempts 3,4,5 (Ground) 90 sec ON/5 min OFF (Airborne) 120 sec ON/5 min OFF Types of Operations - correct answer Visual (VFR). Instrument (IFR). Icing conditions. Category I and II. Maximum Ramp Weight (MRW) - correct answer 85,870 Maximum Take...

Maximum Ramp Weight correct answers 100,000 lbs Maximum Takeoff Gross Weight correct answers 99,600 lbs Maximum Landing Weight correct answers 83,500 lbs Maximum Zero Fuel Weight correct answers 60,500 lbs Maximum Usable Fuel Weight correct answers 44,200 lbs Maximum Operating Altitude correct answers 51,000 ft Maximum Operating Altitude (Single Pack) correct answers 48,000 ft Maximum Airport Elevation correct answers 15,000 ft Maneuvering Speed (Va) correct answers 206 K...

IATRA – Questions And Answers A balanced field length means the length of the runway: a. required to accomodate the take-off of a heavy aircraft when the runway maximum weight-bearing capacity is reached. b. Required for an aircraft to accelerate to computed rotation speed (Vr), experience an engine failure and to come to a complete stop on the runway remaining. c. Required for an aircraft to accelerate to critical engine failure speed, experience an engine failure and to either conti...

Maximum start EGT is ______ Degrees C A. 725 B. 750 C. 925 D. 950 A1-P8AAA-NFM-000 4-6  A The maximum runway slope allowed for P-8A operation is A. +-1% B. +-2% C. +-3% D. +-4% A1-P8AAA-NFM-000 4-2 2 0 2 4 /2025 | © copyright | This work may not be copied for profit gain Excel! 1 | P a g e | G r a d e A + | 2 0 24 / 2 0 2 5  B Maximum takeoff and landing tailwind component is A. 15 knots B. 5 knots C. 20 knots D. 10 knots A1-P8AAA-NFM-000 4-2  A Maximum operating...