Embraer Jet 170/190 Limitations
Just before flight mental quiz for embraer pilots
- 1.Max allowable runway slope?
- A.
-2% to +2%
- B.
-2.1% to +2%
- C.
-2.1% to -2.1%
- D.
2% to -2.1%
- 2.What is the max contaminant depthnfor take off operations?
- A.
25.4mm
- B.
19.0mm
- C.
24.5mm
- D.
10.9mm
- 3.Which of the following is not an EGPWS limitation
- A.
Navigation to be predicated on use of TAWS
- B.
Use of predictive EGPWS function manually inhibited on airports not on database
- C.
Pilots allowed to deviate from atc to comply with EGPWS warning
- D.
Terrain display intended to be used as a situational tool only and maynot provide accuracy or fidelity on which to base terrain avoidance manoeuvring
- 4.As far as TCAS is concerned deviation from ATC assigned altitude authorised
- A.
To change altitude in controlled airspace
- B.
Only to extent neccesary to comply with TCAS RA
- C.
To climb or descend due turbulence
- D.
Manourvres must not be based solely on information displyed on traffic displa
- 5.Maximum fuel per tank
- A.
1474
- B.
4741
- C.
4714
- D.
4174
- 6.Unusable fuel per tank
- A.
34kg
- B.
43kg
- C.
42kg
- D.
33kg
- 7.Max fuel imbalance
- A.
360kg
- B.
306kg
- C.
630kg
- D.
036kg
- 8.Fuel low warning comes when you get to______________kgs of fuel remaining?
- A.
300kg
- B.
310kg
- C.
301kg
- D.
130kg
- 9.On the Embraer 190/195 the maximum usable fuel quantity per tank is?
- A.
6550kg
- B.
6055kg
- C.
6505kg
- D.
5605kg
- 10.E190 unusable fuel per tank amounts to?
- A.
46kg
- B.
64kg
- C.
45kg
- D.
54kg
- 11.APU min max start limits are?
- A.
-54`c to ISA +35
- B.
-54`c to ISA +34
- C.
-53`c to ISA +36
- D.
-53`c to ISA +35
- 12.Maximum altitude for APU start
- A.
15000
- B.
21000
- C.
33000
- D.
30000
- 13.APU operational limitations ; max altitude for operation
- A.
15000
- B.
33000
- C.
30000
- D.
21000
- 14.APU operational limitation; Electrical generator
- A.
33000
- B.
30000
- C.
21000
- D.
15000
- 15.APU operational limitation;altitude to supply bleed for aircon
- A.
33000
- B.
30000
- C.
21000
- D.
15000
- 16.APU operational limitation; altitude to assist engine start
- A.
21000
- B.
210000
- C.
20100
- D.
20010
- 17.max APU rotor speed
- A.
106%
- B.
108%
- C.
160%
- D.
107%
- 18.Max start and continuos EGT for the APU
- A.
1032`c and 717`c
- B.
717`c and 1032`c
- C.
990`c and 1016`c
- D.
1032`c and 990`c
- 19.Starter limitation during APU start 1st and second start
- A.
30s off 30s on
- B.
40s off 40s on
- C.
60s off 60s on
- D.
20s on 20s off
- 20.CF34- 8E5A max N1 is
- A.
99.3%
- B.
99.5%
- C.
99.4%
- D.
99.2%
- 21.CF34-8E5A min and max N2
- A.
58.4%, 99.5%
- B.
58.5%, 99.5%
- C.
58.5%, 99.4%
- D.
55.8%, 94.9%
- 22.CF34-8E5A max ITT start
- A.
875`c
- B.
740`c
- C.
815`c
- D.
1006`c
- 23.CF34-8E5A Normal TOGA
- A.
965`c , 949`c
- B.
945`c , 954`c
- C.
954`c, 949`c
- D.
945`c , 949`c
- 24.CF34-8E5A maximum takeoff go around
- A.
1006`c , 990`c
- B.
990`c , 1006`c
- C.
1006`c , 960`c
- D.
1032`c , 717`c
- 25.CF34-8E5A max continuos ITT
- A.
990`c
- B.
989`c
- C.
960`c
- D.
940`c
Questions: 36 | Attempts: 2849 | Last updated: Mar 22, 2022
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Sample QuestionBoth IDGs and the APU generator are rated at _______________________ , three-phase.
Questions: 22 | Attempts: 1886 | 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: 1832 | 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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