Limitations Flashcards
Max Ramp weight
(MRW) lb
190 Lr- 111,245
190 Ar-114,552
Max Takeoff weight
(MTOW)
190 LR-110,892
190 Ar-114,199
Max landing weight
(MLW)
190 Lr-94,798
199 Ar- 97,003
Max zero fuel weight
(MZFW)
190 Lr-89,948
190 Ar- 90,169
Max altitude for flap extended
20,000 ft
Minimum crew
2 pilots
Load factor limit positive
Flaps up 2.5 g
Flaps down 2.0 g
Load factor limit negative
Flaps up -1.0 g
Flaps down 0 g
Runway slope
-2% to +2%
Runway surface type
Paved
Towing
Towbarless towing is prohibited, unless it is conducted in accordance with the procedures presented in the AMM chapter 9
Max tire ground speed
225 mph (195 kt)
Wind limitations
Max t/o and landing tailwind component 10 kt
Max recommended crosswind
-Dry runway 38kt
-Wet rwy 31 kt
-Rwy whit frost 31 kt
-Rwy whit compacted snow 20kt
-Specially prepared winter rwy (RWYCC 4) 20kt
-Rwy whit standing water/slush/wet snow/dry snow 18kt
-slippery when wet rwy 15kt
-specially prepared winter rwy (RWYCC 3) 15kt
-rwy whit ice 12kt
Maximum usable quantity per wing tank
2134 gal
14,440 lb
Unusable quantity per wing tank
15 gal
101.5 lb
Max fuel capacity
4298 gal
29,083 lb
Max permitted imbalance between wing tanks
794 lb
Fuel specifications
Brazilian specification QAV1
ASTM specification D1655-JET A AND JET A-1
American specification MIL-T-83133A-JP8
Fuel tank temperature
Minimum -37 Celsius
Crossfeed operation
Crossfeed selector knob must be set OFF during takeoff and landing
APU starter limits
Cooling period after each starting attempt
First and second attempt 60s off
Third attempt 5min off
Engine
Two General Electric CF34-10E6
Take off thrust
Hasta 20,000 lb