Embraer 170 - 175 Limitations
BY AOM PART 1!
- 1.What is the Max Landing Weight (MLW)?
- A.
36150 KG
- B.
35990 KG
- C.
32800 KG
- D.
30140 KG
- 2.What are the MAC Limits for Takeoff?
- A.
31% aft / 10% fwd
- B.
30% aft / 10% fwd
- C.
31% aft / 12% fwd
- D.
30% aft / 12% fwd
- 3.What is the VLO for retraction?
- A.
230 Kts
- B.
250 Kts
- C.
320 Kts
- D.
215 Kts
- 4.What is the Max. Ramp Weight (MRW)?
- A.
35990 KG
- B.
36150 KG
- C.
32800 KG
- D.
30140 KG
- 5.What is the Max altitude to start the APU?
- A.
30000 ft
- B.
33000 ft
- C.
41000 ft
- D.
25000 ft
- 6.What is the VLO for extension?
- A.
320 Kts
- B.
215 Kts
- C.
235 Kts
- D.
250 Kts
- 7.What is the Max negative pressure?
- A.
- 0,5 PSI
- B.
- 0,2 PSI
- C.
- 0,1 PSI
- D.
- 0,6 PSI
- 8.What is the Max Zero Fuel Weight (MZFW)?
- A.
30140 KG
- B.
32800 KG
- C.
35990 KG
- D.
36150 KG
- 9.What is the VRA (Turbulent Air Penetration) at or above 10000 ft?
- A.
270 Kts
- B.
265 Kts
- C.
320 Kts
- D.
M .82
- 10.Which flap speeds are correct? Check the box when all flap speeds are correct.
- A.
Flaps 1 = 230 Kts Flaps 2 = 215 Kts Flaps 3 = 215 Kts Flaps 4 = 200 Kts Flaps 5 = 180 Kts Flaps Full = 165 Kts
- B.
Flaps 1 = 230 Kts Flaps 2 = 215 Kts Flaps 3 = 200 Kts Flaps 4 = 180 Kts Flaps 5 = 180 Kts Flaps Full = 165 Kts
- C.
Flaps 1 = 230 Kts Flaps 2 = 215 Kts Flaps 3 = 200 Kts Flaps 4 = 180 Kts Flaps 5 = 180 Kts Flaps Full 160 Kts
- 11.What is the Max Tailwind component?
- A.
12 Kts
- B.
9 Kts
- C.
11 Kts
- D.
10 Kts
- 12.What is the Max Takeoff Weight (MTOW)?
- A.
30140 KG
- B.
32800 KG
- C.
35990 KG
- D.
36150 KG
- 13.What is the Max altitude that the APU can provide Electrical power?
- A.
30000 ft
- B.
41000 ft
- C.
33000 ft
- D.
21000 ft
- 14.What is the Max / Min Temp to start the APU?
- A.
-62°C / ISA +35°C
- B.
-60°C / ISA +35°C
- C.
-56°C / ISA +35°C
- D.
-54°C / ISA +35°C
- 15.What is the Max Crosswind (By Company)?
- A.
Dry RWY = 35 Kts Wet RWY = 25 Kts
- B.
Dry RWY = 38 Kts Wet RWY = 31 Kts
- 16.What is the Max over pressure?
- A.
8,3 PSI
- B.
8,4 PSI
- C.
8,6 PSI
- D.
8,7 PSI
- 17.What is the Max diff. pressure below 37000 ft?
- A.
8,3 PSI
- B.
7,8 PSI
- C.
8,4 PSI
- D.
7,6 PSI
- 18.What is the Max RWY slope deviation?
- A.
-2% / +2%
- B.
-1,8% / +2%
- C.
-2% / +1,8%
- D.
-2% / + 2,1%
- 19.What is the Max Contaminant depth?
- A.
25,4 mm
- B.
22 mm
- C.
25,1 mm
- D.
19 mm
- 20.What is the Max usable fuel per wing?
- A.
4713 Kg
- B.
4714 Kg
- C.
4715 Kg
- D.
4712 Kg
- 21.During Takeoff and Go-Around the Max ITT temp is?
- A.
875°C
- B.
945°C
- C.
990°C
- D.
1032°C
- 22.What is the MAX N1 Rating in %? (CF34-8E5)
- A.
99,4%
- B.
99,5%
- C.
99,3%
- D.
99,6%
- 23.What is the Maximum Altitude For Flap Extension?
- A.
41000ft
- B.
21000ft
- C.
20000ft
- D.
15000ft
- 24.What is the Unusable fuel per wing?
- A.
43 kg
- B.
34 kg
- C.
46 kg
- D.
36 kg
- 25.What is the Max Tire Speed?
- A.
200 Kts
- B.
165 Kts
- C.
160 Kts
- D.
195 Kts
Questions: 36 | Attempts: 2763 | Last updated: Mar 22, 2022
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Sample QuestionBoth IDGs and the APU generator are rated at _______________________ , three-phase.
Questions: 22 | Attempts: 1851 | Last updated: Mar 20, 2022
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Sample QuestionThe Auxiliary Power Unit (APU) is a gas turbine engine located in the airplane tailcone, which provides pneumatic and electrical AC power. The pneumatic power is used for engine starting and to supply bleed air to the air conditioning packs of the Environmental Control System (ECS). An electrical AC generator supplies _____________ to the electrical system.
Questions: 29 | Attempts: 1789 | Last updated: Mar 22, 2022
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Sample QuestionFuel is stored in____ integral wing tanks, interconnected by a crossfeed valve.
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