Limitations Flashcards
Max ramp weight
84,450 lb (LL) 85,870 lb (LR)
Max T/O weight
85,098 lb (LL), 85,517 lb (LR)
Max Landing weight
74,957 lb
Max Zero Fuel weight
69,467 lb (LL), 69,886 lb (LR)
Min Runway Width
100 ft (SKW)
Min Taxiway Width
50 ft (SKW)
Wing Span
93 ft 11 in
Aircraft Length
103 ft 11 in
Tail Height
32 ft 4 in
Max Ops Alt
41,000 ft
Max T/O & Land Alt
10,000 ft
Max Temp T/O & Land
ISA +35C (52C)
Min Temp T/O & Land
-40*C
Runway Slope
+/- 2%
Max tailwind
15 knots
Max single pack operations (altitude)
31,000 ft
Vmo SL - 8000’
300 knots
Vmo 10,000 ft - Mach Transition
320
Mmo
0.82
Va
240
Vlo ext
250
Vle ret
250
Vle
250
Vtire
195
V rat deploy max
Vmo/Mmo
Vmin (to provide electrical power)
130
Vb (below 10,000 ft)
250
Vb (10,000 ft and above)
270/0.76M (whichever is lower)
V wiper ops max
250 (SKW)
Vwindow
160
Vfe 1
230
Vfe 2
215
Vfe 3
200
Vfe 4
180
Vfe 5
180
Vfe FULL
165
Crosswind limitation; dry runway
38 kt (SKW)
Crosswind limitation; wet
31 kt (SKW)
Crosswind limitation; compact snow
20 kt (SKW)
Crosswind limitation T/O; dry snow, wet snow, slush, standing water
18 kt (SKW)
Crosswind limitation T/O; ice and wet ice
12 kt (SKW)
Max Alt Flaps/Slats Extended
20,000 ft
CAT II Approach flap setting
Mandatory Flaps 5
Min battery voltage
22.5V
Engine Start Max ITT
815*C
Starter cranking limits: Engine start on the ground
Start 1&2: 90 seconds ON, 10 seconds OFF. Start 3-5: 90 seconds ON, 5 minutes OFF.
Starter cranking limits: engine start in flight
Start 1&2: 120 seconds ON, 10 seconds OFF. Start 3-5: 120 Seconds ON, 5 minutes OFF.
Dry motoring duty cycle limits
Motoring #1: 90 seconds ON, 5 minutes OFF. Motoring #2-5: 30 seconds ON, 5 minutes OFF. After this the process may be repeated following a 15 minute cool down period.
Max fuel capacity
20,935 lb.
Max fuel imbalance
794 lb
Min fuel tank temperature
-37* C
How long to wait before starting the APU after EICAS is energized?
30 seconds.
Simultaneous use of the APU bleed and the HP cart?
Prohibited.
APU starter duty cycle
Start attempt 1&2: 60 seconds OFF. Start attempt 3: 5 minutes OFF.
APU min and max temp: start
-54*C -/ ISA+35
APU start max altitude
30,000 ft
APU continuous operation min/max temp
-54C / ISA+35 (52C)
APU continuous operation max altitude
33,000 ft
APU continuous operation electrical generator use max altitude
33,000 ft
APU continuous operation engine start max altitude
21,000 ft
APU continuous operation max altitude bleed use
15,000 ft
Max Differential Pressure
8.4 psi
Max Differential Overpressure
8.8 psi
Max Differential Negative Pressure
-0.5 psi
Max Differential Pressure for T/O and Landing
0.2 psi
Min hydraulic reservoir temp for engine start
-18*C
Go-around after deployment of thrust reversers?
Prohibited
When must the TO DATASET MENU be set to ENG?
OAT is from 5C to 10C, there is possibility of encountering visible moisture up to 1700 ft AFE , and when operating on ramps, taxiways, runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engines, nacelles, or engine sensor probes. TO DATASET MENU on the MCDU must be set to ENG.
When must TO DATASET MENU on the MCDU must be set to ALL?
OAT is less than 5*C, there is possibility of encountering visible moisture up to 1700 ft AFE , and when operating on ramps, taxiways, runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engines, nacelles, or engine sensor probes. TO DATASET MENU on the MCDU must be set to ALL.
AP minimum engagement height
400 ft
AP minimum use height
50 ft
AP minimum use height - Non-Precision Approach
MDA
When are TAS, TAT and SAT information valid?
Only valid above 60 knots
When is the standby magnetic compass indication not valid?
While transmitting in VHF1.
What to verify prior to joining a published segment of an instrument approach?
Verify the NAVAID identification visually displayed matches the chart being used. When the identification is not visually displayed, very that the ID matches the chart being used.
