Limitations Flashcards
Max T/O wt
85,517
Max landing wt
74,957
Max zero fuel wt
69,886
Max Ramp weight
85,870
Max aft cargo
2,535
Max fwd cargo
3,306
Min rwy width SKW
100 ft
Wing span
93’11”
Aircraft length
103’11”
Main to main distance
17’1”
Tail height
32’4”
Max operating altitude
41,000
Max T/O and landing altitude
8,000 ft
Max temp T/O & landing
ISA + 35C
Min. Temp T/O and landing
-40C
Rwy slope
+/- 2%
Max tail wind
15kt
Max altitude single pack
31,000
Vmo SL-8,000ft
300
Vmo 10,000 -Mach transition
320
Mmo
.82
Va
240
Vlo ext
250
Vle ret
250
Vle
250
V tire
195
V rat deploy max
Vmo/Mmo
Vmin rat
130
Vb below 10,000
250
Vb above 10,000
270/.76 Mach whichever is lower
V wiper max
250 SKW
V window
160
Vfe 1
230
Vfe 2
215
Vfe 3
200
Vfe 4
180
Vfe 5
180
Vfe full
165
Dry runway max crosswind
38kt
Wet runway max cross wind
31kt
Runway with compacted snow max cross wind
20kt
Runway with standing water/slush/wet snow/dry snow max cross wind
18 kt
Runway with ice max cross wind
12kt
Max crosswind static take off
30 kt
Max alt flaps/slats extended
20,000ft
Enroute ops flaps/slats
Prohibited
Min spoiler speed
180 kt
Cat. II approach
Mandatory flaps 5
Landing flaps full
Go-around flaps 4
Landing flaps 5
Go-around flaps 2
Min battery voltage
22.5
Max engine start temp
815C
Min temp engine start
-40C
Min oil pressure start
25 psi
Starter limit 1 & 2
90s on, 10 sec off
Starter limit 3-5
90s on, 5 min off
Starter limit inflight 1 & 2
120s on, 10s off
Starter limit inflight 3-5
120s on, 5 min off
Dry motoring attempt 1
90s on, 5 min off
Dry motoring limit 2-5
30s on, 5 min off
Start with tailwind must be….
Manually aborted
ATTCS off is…..
Not authorized
Max fuel capacity
20,935
Max fuel imbalance
794 pounds
Min fuel tank temp
-40C
Crossfeed must be…..
Off for take-off and landing
Apu start attempt 1 & 2
60s off
Apu starter duty cycle attempt
5 min off
APU start temperature range
-54C to ISA + 35
APU max start altitude
30,000ft
APU continuous temp range
-54C to ISA + 35C
APU continuous max altitude
33,000ft
APU continuous electric gen use
33,000ft
Apu max continuous altitude bleed use
15,000ft
APU continuous altitude engine start
21,000ft
Max differential pressure up to 37,000ft
7.8
Max differential pressurization above 37,000ft
8.34
Max differential over pressure
8.77
Max diff neg pressure
-.5
Max diff press t/o and lnd
.2
Min reservoir temp for eng start
-18C
Temp 5 to 10 OAT
Eng must be selected if moisture below 1,700 ft or
Contaminated surfaces
Temp below 5C OAT
All must be selected with moisture below 1,700 AFE or
Contaminated surfaces
In flight with either 1 or 2 ice detectors failed
Temp below 10 TAT A/I on
Min autopilot engagement height
400ft
Min autopilot use height
50ft
Min autopilot us non-precision appoach
MDA
