293 Oral Exam Review (Gamma / Wheels Up) Exam Questions And Answers Latest Update

293 Oral Exam Review (Gamma / Wheels
Up) Exam Questions And Answers Latest
Update

293 Oral Exam Review (Gamma / Wheels Up)
mn mn mn mn mn mn mn




1.
mn What is the maximum ramp weight for the G280?
mn mn mn mn mn mn mn mn




a)
mn 35,500 lbs mn




b) 36,000 lbs
mn mn




c)
mn 36,100 lbs mn




d) 37,000 lbs
mn mn




2.
mn What is the maximum takeoff weight (MTOW) for the G280?
mn mn mn mn mn mn mn mn mn




a)
mn 35,500 lbs mn




b) 35,800 lbs
mn mn




c)
mn 35,900 lbs mn




d) 36,100 lbs
mn mn




3. What is the maximum landing weight (MLW) for the G280?
mn mn mn mn mn mn mn mn mn mn




a) 30,900 lbs
mn mn




b) 31,500 lbs
mn mn




c) 32,000 lbs
mn mn




d) 33,000 lbs
mn mn




4.
mn What is the maximum zero fuel weight (MZFW) for the G280?
mn mn mn mn mn mn mn mn mn mn




a)
mn 22,000 lbs mn




b) 22,500 lbs
mn mn




c)
mn 23,500 lbs mn




d) 24,000 lbs
mn mn




5. What is the maximum operating altitude for the G280?
mn mn mn mn mn mn mn mn mn




a) 41,000 feet
mn mn




b) 45,000 feet
mn mn




c) 47,000 feet
mn mn




d) 49,000 feet
mn mn




6. How many independent hydraulic systems are on the G280?
mn mn mn mn mn mn mn mn mn




a) 1
mn




b) 2 mn

,c) 3
mn




d) 4
mn




7. What is the normal operating pressure of the hydraulic systems?
mn mn mn mn mn mn mn mn mn mn




a) 2,500 psi
mn mn




b) 3,000 psi
mn mn




c) 3,500 psi
mn mn




d) 4,000 psi
mn mn




8. The landing gear and flaps on the G280 are operated by which hydraulic system?
mn mn mn mn mn mn mn mn mn mn mn mn mn mn




a) System 1
mn mn




b) System 2
mn mn




c) Both System 1 and 2
mn mn mn mn mn




d) Neither, they are electrically operated
mn mn mn mn mn




9. How is the primary flight control actuation achieved on the G280?
mn mn mn mn mn mn mn mn mn mn mn




a) Mechanical cables
mn mn




b) Hydraulic actuators (Hydro-mechanical)
mn mn mn




c) Electrical motors
mn mn




d) Pneumatic servos
mn mn




10. How many Engine-Driven Pumps (EDPs) are on the G280?
mn mn mn mn mn mn mn mn mn




a) One (Left Engine)
mn mn mn




b) One (Right Engine)
mn mn mn




c) Two (One on each engine)
mn mn mn mn mn




d) Four
mn




11. How many AC power generators are installed on the G280?
mn mn mn mn mn mn mn mn mn mn




a) One
mn




b) Two (One per engine)
mn mn mn mn




c) Three
mn




d) Four
mn




12. What is the output voltage of the main AC generators?
mn mn mn mn mn mn mn mn mn mn




a) 28V DC
mn mn




b) 115/200V AC, 400 Hz
mn mn mn mn




c) 28V AC
mn mn




d) 12V DC
mn mn




13. In flight, which generator is the primary source for the AC bus?
mn mn mn mn mn mn mn mn mn mn mn mn




a) The left engine generator
mn mn mn mn




b) The right engine generator
mn mn mn mn




c) The APU generator
mn mn mn




d) The Emergency generator
mn mn mn

, 14. What is the function of the Emergency Generator (EMER GEN)?
mn mn mn mn mn mn mn mn mn mn




a) It provides power for the galley
mn mn mn mn mn mn




b) It powers the landing lights
mn mn mn mn mn




c) It is deployed by the RAT to power essential flight instruments and systems in an emerge
mn mn mn mn mn mn mn mn mn mn mn mn mn mn mn mn




ncy
d) It charges the main batteries
mn mn mn mn mn




15. How many batteries does the G280 have?
mn mn mn mn mn mn mn




a) One (Main)
mn mn




b) Two (Main and APU)
mn mn mn mn




c) Three
mn




d) Four
mn




16. What type of engines power the G280?
mn mn mn mn mn mn mn




a) Pratt & Whitney PW305A
mn mn mn mn




b) Honeywell HTF7250G
mn mn




c) Rolls-Royce BR710
mn mn




d) General Electric CF34
mn mn mn




17. What is the thrust rating of each HTF7250G engine?
mn mn mn mn mn mn mn mn mn




a) 6,500 lbf
mn mn




b) 6,900 lbf
mn mn




c) 7,624 lbf
mn mn




d) 8,500 lbf
mn mn




18. The FADEC (Full Authority Digital Engine Control) system on the G280 provides wh
mn mn mn mn mn mn mn mn mn mn mn mn mn




at type of control?
mn mn mn




a) Manual mechanical control only
mn mn mn mn




b) Limited envelope protection
mn mn mn




c) Full digital control and monitoring of the engine from start to shutdown
mn mn mn mn mn mn mn mn mn mn mn mn




d) Only fuel metering
mn mn mn




19. How many independent bleed air systems are on the G280?
mn mn mn mn mn mn mn mn mn mn




a) Two (One per engine)
mn mn mn mn




b) One (Shared)
mn mn




c) Three
mn




d) Four
mn




20. The bleed air from the engines is primarily used for:
mn mn mn mn mn mn mn mn mn mn




a) Thrust reversal
mn mn




b) Fuel heating
mn mn




c) Pressurization and air conditioning
mn mn mn mn




d) Hydraulic pressurization
mn mn