Limitations Flashcards
Emergency Equipment
Protective Breathing Equipment (PBE) Fire Extinguishers Crash Axe Life Vests Escape Ropes Flashlights
Type of engine?
High-bypass and dual rotor turbofan fully integrated and thrust reverse General Electric CF34-10E5
Max Ramp Weight (MRW)
111,245 lb
Maximum Altitude For Flap Extension
20,000 ft
VLO for retraction
235 KIAS
Maximum Speed to Open the Direct Vision Window
160 KIAS
VLO for extension
265 KIAS
VMO/MMO
320 KIAS / 0.82 M
Maximun Flap Extended Speed (VFE) Flaps 2
Structural/Manuvering
215/160 KIAS
Max. Landing Weight (MLW) (lb)
94,798 lb
Maximun Flap Extended Speed (VFE) Flaps 3
Structural/Manuvering
200/150 KIAS
Maximun Flap Extended Speed (VFE) Flaps 5
Structural/Manuvering
180/140 KIAS
Max. Zero Fuel Weight (MZFW) (lb)
89,948 lb
Maximun Flap Extended Speed (VFE) Flaps Full
Structural/Manuvering
165/130 KIAS
maximum fuel capacity TOTAL
4268 gal 29083 lb
Max. Takeoff Weight (MTOW) (lb)
110,230 lb
Maximum tire ground speed
225 mph / 195 kts
Maximum Recommended Crosswind Dry Runway Pista Seca
38 kt
VLE
265 KIAS
Maximum Recommended Crosswind Wet Runway Pista Mojada
31 kt
Load factor limits Flaps down (1,2,3,4,5 full)
2g positivas 0g negativas
runway slope y surface
entre -2% y 2% superficie pavimentada
fuel tank temperature
minimum -40 C
maximum usable fuel per wing tank
2134 gal 14440 lb
Maximun Flap Extended Speed (VFE) Flaps 1
Structural/Manuvering
230/180 KIAS
unusable fuel per wing
15 gal 101.5 lb
Maximun Flap Extended Speed (VFE) Flaps 4
Structural/Manuvering
180/140 KIAS
maximum fuel imbalance
794 lb
Max Engine (powerplant) ITT inflight start
875 C
crossfeed operations
off during takeoff and landing
APU Max EGT start
1032 C
Maximum Recommended Crosswind compacted snow runway nieve compactada
20 kt
APU start temperature
-54 C e ISA + 35
APU max Start altitude
30,000 ft
Max Engine (powerplant) ITT takeoff and go around
983 C
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
Max Engine (powerplant) ITT continuous
960 C
max differential overpressure
8,77 psi
Maximum Recommended Crosswind ice pista con hielo congelada
12 kt
APU max operational alt
33,000 ft
Load factor limits Flaps up
2.5g positivas -1g negativas
FADEC automatically shutsdown the APU in flight when:
- overspeed
- underspeed
- FADEC critical fault
APU max altitude bleed
15,000 ft
Normal Engine (powerplant) ITT takeoff and go around
945 C for 5 min
APU max altitude to assist engine start
21,000 ft
APU max rotor speed
108%
max differential pressure hasta 37,000
7,8 psi
APU Max EGT continuous
717 C
Taxi Speed
Turns/Wet or Contaminated
5KT
Max Engine (powerplant) limitation N1
100%
Engine (powerplant) oil press
min 25 psi
Max Engine (powerplant) ITT ground start
740 C
Engine (powerplant) limitation N2
min 59.3% max 100%
max differential pressure arriba de 37,000
8,34 psi
Engine (powerplant) oil temp
155 C
Maximum Recommended Crosswind standing water /slush/ wet snow/ dry snow
18 kt
Powerback
Prohibited
Cuanto tiempo de carga tienen las baterías?
10 minutos
max differential negative pressure
-0,5 psi
Autopilot minimum engage height y minimum use height
400 ft / 50 ft
Windshield wiper operation
253 KIAS
Stabilized idle indications:
N1=27%
ITT=460
N2=62%
Fuel Flow=600PPH
Taxi Speed
Straight/Dry
30KT
Max Airspeed For windshield wiper operation
253 KIAS
APU Cooling Periods
First and second attempt 60 secs OFF
Third attempt 5 min OFF
Taxi Speed
Straight/Wet or Contaminated
10KT
APU max electrical generation alt
33,000 ft
Taxi Speed
Turns/Dry
10KT
max differentia pressure for takeoff and landing
0,2 psi