Psa Airlines Flight Correct Exams Answers And Questions Set A.pdf

PSA AIRLINES FLIGHT CORRECT EXAMS ANSWERS
AND QUESTIONS SET A+
✔✔PSA CRJ 701: Maximum transient Oil Pressure after cold start(10 minutes
maximum) - ✔✔182 psi or amber dashes

✔✔*After cold start, engine must remain __ ____until oil pressure returns to normal
range. - ✔✔After cold start, engine must remain at idle until oil pressure returns to
normal range.

✔✔**Continuous engine ignition must be used during the following: - ✔✔• Takeoff and
landing on contaminated runways
• Takeoff with high crosswind components (15 knots or greater)
• Flight through moderate or heavier intensity rain
• Flight through moderate or heavier intensity turbulence
• Flight in the vicinity of thunderstorms

✔✔*CRJ 700 and 900: Engine Starter Cranking Limitations: - ✔✔PSA CRJ 700 and
900:
• 1st start 90 Seconds on Followed by 10 sec OFF
• 2nd start 90 Seconds on Followed by 10 sec OFF
• 3rd and Subsequent starts 90 Seconds on Followed by 5 Minutes OFF

✔✔Thrust reversers are approved for ground use only. T/F - ✔✔True, Thrust reversers
are approved for ground use only.

✔✔The thrust reversers are intended for use during ____ ____ landings. Do not attempt
a go-around maneuver after deployment of the thrust reversers. - ✔✔The thrust
reversers are intended for use during full stop landings. Do not attempt a go-around
maneuver after deployment ofthe thrust reversers.

✔✔What thrust reverser condition will prohibit takeoff? - ✔✔Takeoff with any thrust
reverser lights ON, icons, or EICAS messages displayed is prohibited.

, ✔✔**During landing, maximum reverse thrust is prohibited below____, and reverse idle
should be achieved by____ - ✔✔75 knots. reverse idle should be achieved by 60 knots

✔✔Can power-back the aircraft up with thrust reversers? - ✔✔Backing-up (power-back)
using thrust reversers is prohibited.

✔✔**PSA CRJ 701: Engine Operating Limits Due to Wind Direction. Within 30° on
either direction of the airplane nose-no windspeed limit -OR- >30° in either direction of
the airplane nose- <5 knots windspeed - ✔✔**PSA CRJ 701: No limitations - TOGA
thrust may be applied before brakes released.

✔✔**PSA CRJ 701: Engine Operating Limits Due to Wind Direction >30° in either
direction of the airplane nose-between 5 and 30 knots windspeed - ✔✔**PSA CRJ 701:
Apply maximum of 75% N1 before brake release, then TOGA thrust.

✔✔**PSA CRJ 701: Engine Operating Limits Due to Wind Direction. >30° in either
direction of the airplane nose >30 knots windspeed - ✔✔**PSA CRJ 701: Apply
maximum of idle/taxi thrust before brake release, then TOGA thrust

✔✔**CRJ 700 and 900: Maximum permissible fuel imbalance between the left and right
wing tanks for takeoff: - ✔✔**PSA CRJ 701: 300 lbs

✔✔**CRJ 700 and 900: Maximum permissible fuel imbalance between the left and right
wing tanks for all other phases of flight: - ✔✔**PSA CRJ 701: 800 lbs

✔✔CRJ 700:Fuel Quantities Left Wing and Right Wing Tank Pressure Refuel: - ✔✔PSA
CRJ 701: Left Wing and Right Wing Tank Pressure Refuel: 7,492 lbs

✔✔PSA CRJ 701:Fuel Quantities Center Tank Pressure Refuel: - ✔✔PSA CRJ 701:
Center Tank Pressure Refuel: 4,610 lbs

✔✔**CRJ 700 and 900: Fuel Quantities Total Fuel Pressure Refuel: - ✔✔19,594 lbs

✔✔*Takeoff with a fuel load in excess of ___ lbs. in the center tank is not permitted
unless each wing tank is above_____ lbs. - ✔✔Takeoff with a fuel load in excess of 500
lbs. in the center tank is not permitted unless each wing tank is above 4,400 lbs.

✔✔What is the minimum fuel quantity for go-around per wing tank (with the airplane
level) and assuming a maximum airplane climb attitude of 10° nose up? - ✔✔The
minimum fuel quantity for go-around per wing tank (with the airplane level) and
assuming a maximum airplane climb attitude of 10° nose up:
PSA CRJ 200: 450 lbs.
PSA CRJ 701: 600 lbs.