Limitations Flashcards

0
Q

Emergency Equipment

A
Protective Breathing Equipment (PBE) 
Fire Extinguishers 
Crash Axe 
Life Vests 
Escape Ropes 
Flashlights
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1
Q

Type of engine?

A

High-bypass and dual rotor turbofan fully integrated and thrust reverse General Electric CF34-10E5

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2
Q

Max Ramp Weight (MRW)

A

111,245 lb

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3
Q

Maximum Altitude For Flap Extension

A

20,000 ft

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4
Q

VLO for retraction

A

235 KIAS

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5
Q

Maximum Speed to Open the Direct Vision Window

A

160 KIAS

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6
Q

VLO for extension

A

265 KIAS

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7
Q

VMO/MMO

A

320 KIAS / 0.82 M

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8
Q

Maximun Flap Extended Speed (VFE) Flaps 2

Structural/Manuvering

A

215/160 KIAS

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9
Q

Max. Landing Weight (MLW) (lb)

A

94,798 lb

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10
Q

Maximun Flap Extended Speed (VFE) Flaps 3

Structural/Manuvering

A

200/150 KIAS

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11
Q

Maximun Flap Extended Speed (VFE) Flaps 5

Structural/Manuvering

A

180/140 KIAS

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12
Q

Max. Zero Fuel Weight (MZFW) (lb)

A

89,948 lb

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13
Q

Maximun Flap Extended Speed (VFE) Flaps Full

Structural/Manuvering

A

165/130 KIAS

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14
Q

maximum fuel capacity TOTAL

A

4268 gal 29083 lb

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15
Q

Max. Takeoff Weight (MTOW) (lb)

A

110,230 lb

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17
Q

Maximum tire ground speed

A

225 mph / 195 kts

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18
Q

Maximum Recommended Crosswind Dry Runway Pista Seca

A

38 kt

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19
Q

VLE

A

265 KIAS

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20
Q

Maximum Recommended Crosswind Wet Runway Pista Mojada

A

31 kt

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21
Q

Load factor limits Flaps down (1,2,3,4,5 full)

A

2g positivas 0g negativas

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22
Q

runway slope y surface

A

entre -2% y 2% superficie pavimentada

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23
Q

fuel tank temperature

A

minimum -40 C

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24
Q

maximum usable fuel per wing tank

A

2134 gal 14440 lb

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25
Maximun Flap Extended Speed (VFE) Flaps 1 | Structural/Manuvering
230/180 KIAS
25
unusable fuel per wing
15 gal 101.5 lb
26
Maximun Flap Extended Speed (VFE) Flaps 4 | Structural/Manuvering
180/140 KIAS
27
maximum fuel imbalance
794 lb
28
Max Engine (powerplant) ITT inflight start
875 C
29
crossfeed operations
off during takeoff and landing
30
APU Max EGT start
1032 C
31
Maximum Recommended Crosswind compacted snow runway nieve compactada
20 kt
33
APU start temperature
-54 C e ISA + 35
34
APU max Start altitude
30,000 ft
35
Max Engine (powerplant) ITT takeoff and go around
983 C
36
FADEC automatically shutsdown the APU on ground:
- overspeed - underspeed - FADEC critical fault - APU fire - APU EGT overtemp - APU high oil temp - APU low oil pressure - Sensor fail
37
Max Engine (powerplant) ITT continuous
960 C
38
max differential overpressure
8,77 psi
39
Maximum Recommended Crosswind ice pista con hielo congelada
12 kt
40
APU max operational alt
33,000 ft
41
Load factor limits Flaps up
2.5g positivas -1g negativas
42
FADEC automatically shutsdown the APU in flight when:
- overspeed - underspeed - FADEC critical fault
43
APU max altitude bleed
15,000 ft
44
Normal Engine (powerplant) ITT takeoff and go around
945 C for 5 min
45
APU max altitude to assist engine start
21,000 ft
46
APU max rotor speed
108%
47
max differential pressure hasta 37,000
7,8 psi
48
APU Max EGT continuous
717 C
49
Taxi Speed | Turns/Wet or Contaminated
5KT
50
Max Engine (powerplant) limitation N1
100%
51
Engine (powerplant) oil press
min 25 psi
52
Max Engine (powerplant) ITT ground start
740 C
53
Engine (powerplant) limitation N2
min 59.3% max 100%
54
max differential pressure arriba de 37,000
8,34 psi
55
Engine (powerplant) oil temp
155 C
56
Maximum Recommended Crosswind standing water /slush/ wet snow/ dry snow
18 kt
57
Powerback
Prohibited
57
Cuanto tiempo de carga tienen las baterías?
10 minutos
58
max differential negative pressure
-0,5 psi
59
Autopilot minimum engage height y minimum use height
400 ft / 50 ft
60
Windshield wiper operation
253 KIAS
61
Stabilized idle indications:
N1=27% ITT=460 N2=62% Fuel Flow=600PPH
62
Taxi Speed | Straight/Dry
30KT
63
Max Airspeed For windshield wiper operation
253 KIAS
64
APU Cooling Periods
First and second attempt 60 secs OFF | Third attempt 5 min OFF
65
Taxi Speed | Straight/Wet or Contaminated
10KT
66
APU max electrical generation alt
33,000 ft
67
Taxi Speed | Turns/Dry
10KT
68
max differentia pressure for takeoff and landing
0,2 psi