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Ejet E179 > Limitations > Flashcards

Limitations Flashcards

(89 cards)

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1
Q

E1

Max Taxi​ &​ Ramp

Weight

A

50,950 kg

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2
Q

E2

Max Taxi​ &​ Ramp

Weight

A

61,700 kg

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3
Q

E1

Max​ Takeoff

Weight

A

50,790 kg

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4
Q

E2

Max​ Takeoff

Weight

A

61,200 kg

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5
Q

E2

Max​ Landing

Weight

A

54,000 kg

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6
Q

E1

Max​ Landing

Weight

A

45,000 kg

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7
Q

E1

Max​ Zero Fuel

Weight

A

42,500 kg

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8
Q

E2

Max​ Zero Fuel

Weight

A

51,850 kg

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9
Q

E1/E2

Max Headwind (for CAT II and LVO)

Operational Limits

A

25 kts

AOM Vol 1 - Limitations

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10
Q

E1/E2

Max 90 degree crosswind (including gusts) for CAT II and LVO

Operational Limits

A

15 kts (AD)

AOM Vol 1 - Limitations

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11
Q

E1/E2

Max 90 degree crosswind component (STEADY)
Takeoff - DRY

Operational Limits

A

25 kts

AOM Vol 1 - Limitations

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12
Q

E1/E2

Max 90 degree crosswind component (STEADY)
Landing - DRY

Operational Limits

A

25 kts

AOM Vol 1 - Limitations

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13
Q

E1/E2

Max 90 degree crosswind component (STEADY)
Takeoff - WET

Operational Limits

A

20 kts

AOM Vol 1 - Limitations

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14
Q

E1/E2

Max 90 degree crosswind component (STEADY)
Landing - WET

Operational Limits

A

15 kts

AOM Vol 1 - Limitations

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15
Q

E1/E2

Max 90 degree crosswind component (STEADY)

Landing - DRY​ RWY​ or TAXIWAYS (1700m X40m or​ less)

Operational Limits

A

15 kts

AOM Vol 1 - Limitations

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16
Q

E1/E2

Max 90 degree crosswind component (STEADY)

Takeoff - DRY​ RWY​ or TAXIWAYS (1700m X40m or​ less)

Operational Limits

A

15 kts

AOM Vol 1 - Limitations

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17
Q

E1/E2

Max 90 degree crosswind component (STEADY)

Takeoff - WET​ RWY​ or TAXIWAYS (1700m X40m or​ less)

Operational Limits

A

05 kts

AOM Vol 1 - Limitations

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18
Q

E1/E2

Max 90 degree crosswind component (STEADY)

Landing - WET​ RWY​ or TAXIWAYS (1700m X40m or​ less)

Operational Limits

A

05 kts

AOM Vol 1 - Limitations

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19
Q

E1/E2

Max 90 degree crosswind component (STEADY)
Takeoff and Landing
STANDING WATER
GROOVED​ RWY

Operational Limits

A

10 kts

AOM Vol 1 - Limitations

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20
Q

E1/E2

Max 90 degree crosswind component (STEADY)
Takeoff and Landing
STANDING WATER
NON-GROOVED​ RWY

Operational Limits

A

05 kts

AOM Vol 1 - Limitations

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21
Q

E1/E2

Max takeoff and landing tailwind component

Operational Limits

A

10 kts (AD)

AOM Vol 1 - Limitations

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22
Q

E1/E2

Max takeoff tailwind component for LVO

Operational Limits

A

05 kts (AD)

AOM Vol 1 - Limitations

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23
Q

E1/E2

Maximum wind for passenger door operation

Operational Limits

A

40 kts

AOM Vol 1 - Limitations

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24
Q

E1/E2

Maximum wind for cargo door opening

Operational Limits

A

40 kts

AOM Vol 1 - Limitations

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25
# **E1/E2** Max Runway Slope (up hill, down hill) | Runway Slope
+/- 2.0% | AOM Vol 1 - Limitations
26
# **E1/E2** Min fuel temperature | Fuel
\- 37 °C | AOM Vol 1 - Limitations
27
# **E1/E2** Max fuel imbalance | Fuel
360 kg | AOM Vol 1 - Limitations
28
# **E1/E2** How the CROSSFEED switch must be for takeoff and landing? | Fuel ## Footnote XFEED Switch must be set to ____ for takeoff and landing
OFF | AOM Vol 1 - Limitations
29
# **E1/E2** Max operating airspeed | Speeds
Vmo | AOM Vol 1 - Limitations
30
# **E1/E2** Max operating mach​ number | Speeds
.82 (Mmo)
31
# **E1/E2** Max airspeed​ for RAT​ operation | Speeds
Vmo or Mmo
32
# **E1/E2** Max Turbulent airspeed below 10,000​ ft | Speeds
250 kts
33
# **E1/E2** Max Turbulent airspeed at or above 10,000​ ft | Speeds
270 kts or M.76
34
# **E1/E2** Tire limit ground speed | Speeds
195 kts
35
# **E1/E2** Max​ speed​ with​ windshield wiper​ failed​ in non-parked position​ | Speeds
320 kts
36
# **E1/E2** Max windshield wiper operation speed | Speeds
250 kts
37
# **E1/E2** Max speed Flap 1 | Speeds
230 kts
38
# **E1/E2** Max speed Flap 2 | Speeds
215 kts
39
# **E1/E2** Max speed Flap 3 | Speeds
200 kts
40
# **E1/E2** Max speed Flap 4 | Speeds
180 kts
41
# **E1/E2** Max speed Flap 5 | Speeds
180 kts
42
# **E1/E2** Max speed Flap FULL | Speeds
165 kts
43
# **E1/E2** Design maneuvering speed | Speeds
240 kts
44
# **E1/E2** Max​ operating altitude | Altitudes
41,000 fts
45
# **E1/E2** Max​ takeoff​ and landing altitude | Altitudes
10,000 fts
46
# **E1/E2** Max​ flap extension altitude | Altitudes
20,000 fts
47
# **E1/E2** Max​ ambient temperature for​ takeoff and landing | Temperatures
52 °C
48
# **E1/E2** Min​ ambient temperature approved​ for takeoff | Temperatures
\- 54 °C
49
# **E1/E2** Max​ altitude​ for single pack operation | Pneumatics
31,000 ft
50
# **E1/E2** Max​ differencial pressure | Pneumatics
8.4 psi
51
# **E1/E2** Max​ negative differential pressure​ | Pneumatics
\- 0.5 psi
52
# **E1** Max gear retraction speed VLO | Speeds
235 kts
53
# **E1/E2** Max differential pressure for takeoff & landing​ | Pneumatics
0.2 psi
54
# **E1** Max gear extension speed VLO | Speeds
265 kts
55
# **E1** Max​ gear extended speed​ V​LE | Speeds
265 kts
56
# **E1** Min altitude​ for​ autopilot​ use precision approach | Autoflight
50 ft below DH/DA
57
# **E1/E2** Min altitude​ for​ autopilot​ use nonprecision approach | Autoflight
MDA
58
# **E1** Min altitude​ for​ autopilot​ use enroute | Autoflight
500 ft AGL
59
# **E1** Min altitude​ for​ autopilot​ use Visual​ Approach​ not​ backed up by instrument procedure | Autoflight
500 ft AGL
60
# **E1/E2** Min Engagement Height Takeoff | Autoflight
Acceleration Altitude
61
# **E1/E2** Min Engagement Height other than Takeoff | Autoflight
400 ft AGL
62
# **E1/E2** Limit Maneuvering Load Factors Flaps Up | Autoflight
\- 1.0G to + 2.5G
63
# **E1/E2** Limit Maneuvering Load Factors Flaps​ down (1, 2, 3, 4, 5 and​ full) | Autoflight
0.0G to + 2.0G
64
# **E1/E2** Max N1 | Engine
100%
65
# **E1/E2** Max N2 | Engine
100%
66
# **E1** Max ITT​ During engine start (on ground) | Engine
740 °C
67
# **E1** Max ITT​ During engine start (in flight) | Engine
875 °C
68
# **E1** Max ITT​ Takeoff and Go-Around​ | Engine
983 °C
69
# **E1** Max Continuous ITT | Engine
960 °C
70
# **E1** Min Oil Pressure | Engine
25 PSI
71
# **E1** Max Oil Temperature​ | Engine
155 °C
72
# **E1** Min temperature for operations | APU
\- 54 °C
73
# **E1** Max​ altitude for​ Start | APU
30,000 ft
74
# **E1/E2** Max​ temperature for operations | APU
ISA + 35 °C
75
# **E1** Max​ altitude for​ electrical​ supply | APU
33,000 ft
76
# **E1** Max​ altitude to assist​ engine start​ | APU
21,000 ft
77
# **E1** Max​ EGT​ Continuous | APU
717 °C
78
# **E1/E2** Max​ altitude for​ bleed​ supply | APU
15,000 ft
79
# **E1/E2** Max​ rotor speed | APU
108 %
80
# **E1/E2** Max​ EGT​ start | APU
1032 °C
81
# **E1/E2** The T/O DATASET MENU on the MCDU​ must be set to EN​G in the following cases | Anti-Ice System
- when​ OAT is between 5ºC and 10ºC and; - if​​ there is any possibility of encountering visible moisture​ up to 1700 ft AFE.
82
# **E1/E2** The T/O DATASET MENU on the MCDU​ must be set to ALL in the following cases | Anti-Ice System
- when​ OAT is below 5ºC and; - if​​ there is any possibility of encountering visible moisture​ up to 1700 ft AFE.
83
# **E1/E2** Do​ not hold \_\_\_\_\_\_\_\_ with slats/flaps​ extended. | Anti-Ice System
in icing conditions
84
# **E1** Maximum fuel capacity | Fuel
13,192​ kg
85
# **E2** Maximum fuel capacity | Fuel
13,690 kg
86
# **E1/E2** Do not attempt a go-around​ maneuver after \_\_\_\_ | Thrust Reversers
deployment of the thrust ​reversers
87
# **E1** Maximum value​ for​ Last Minute Change | LMC
225 kg
88
# **E1** Engine Warm-up | Engine
two​ (2) minutes
89
# **E1** Engine Shutdown | Engine
two​ (2) minutes

Ejet E179 (2 decks)

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