ENVOY AIR ERJ 170/175 WEEK 3 ACTUAL EXAM PAPER
2026 QUESTIONS WITH ANSWERS GRADED A+
● ERJ 170/175 Engines. Answer: Two General Electric CF34-8E engines, each producing
approximately 14,200 lbs of thrust.
● V1. Answer: Takeoff decision speed; if an engine fails before V1 the takeoff must be
rejected.
● VR. Answer: Rotation speed; the speed at which the pilot applies back pressure to lift the
nose.
● V2. Answer: Takeoff safety speed; minimum airspeed to maintain with one engine
inoperative after liftoff.
● Vref. Answer: Reference landing speed; typically 1.3 times stall speed in landing
configuration.
● Maximum Takeoff Weight (ERJ 175). Answer: Approximately 82,000 lbs (37,200 kg).
● Maximum Landing Weight (ERJ 175). Answer: Approximately 74,000 lbs (33,600 kg).
● Maximum Zero Fuel Weight. Answer: Approximately 70,548 lbs (32,000 kg) for the ERJ
175.
● Pressurization System. Answer: The ERJ 170/175 maintains cabin altitude at
approximately 6,000 feet at maximum cruise altitude.
● Maximum Operating Altitude. Answer: 41,000 feet (FL410) for the ERJ 170/175.
● APU (Auxiliary Power Unit). Answer: Provides electrical power and bleed air for
environmental systems when engines are not running.
● FADEC. Answer: Full Authority Digital Engine Control; manages engine parameters
automatically for optimal performance.
● Fly-By-Wire. Answer: The ERJ 170/175 uses an electronic flight control system rather than
direct mechanical linkage.
2026 QUESTIONS WITH ANSWERS GRADED A+
● ERJ 170/175 Engines. Answer: Two General Electric CF34-8E engines, each producing
approximately 14,200 lbs of thrust.
● V1. Answer: Takeoff decision speed; if an engine fails before V1 the takeoff must be
rejected.
● VR. Answer: Rotation speed; the speed at which the pilot applies back pressure to lift the
nose.
● V2. Answer: Takeoff safety speed; minimum airspeed to maintain with one engine
inoperative after liftoff.
● Vref. Answer: Reference landing speed; typically 1.3 times stall speed in landing
configuration.
● Maximum Takeoff Weight (ERJ 175). Answer: Approximately 82,000 lbs (37,200 kg).
● Maximum Landing Weight (ERJ 175). Answer: Approximately 74,000 lbs (33,600 kg).
● Maximum Zero Fuel Weight. Answer: Approximately 70,548 lbs (32,000 kg) for the ERJ
175.
● Pressurization System. Answer: The ERJ 170/175 maintains cabin altitude at
approximately 6,000 feet at maximum cruise altitude.
● Maximum Operating Altitude. Answer: 41,000 feet (FL410) for the ERJ 170/175.
● APU (Auxiliary Power Unit). Answer: Provides electrical power and bleed air for
environmental systems when engines are not running.
● FADEC. Answer: Full Authority Digital Engine Control; manages engine parameters
automatically for optimal performance.
● Fly-By-Wire. Answer: The ERJ 170/175 uses an electronic flight control system rather than
direct mechanical linkage.
