Limitations Flashcards
(66 cards)
1
Q
Max Ramp Weight
A
48,500
2
Q
Max Takeoff Weight
A
48,300
3
Q
Max Landing Weight
A
42,000
4
Q
Max Zero Fuel Weight
A
30,864
5
Q
Min Flight Weight
A
20,700
6
Q
Datum
A
25% MAC or station 420.43
7
Q
Baggage total weight
A
2,866
8
Q
Payload
A
5,990
9
Q
VMO / MMO
A
VMO 370 kts
MMO .87
10
Q
Maneuvering Speed
A
Va 228kts
11
Q
Slats out Flaps 7•
A
200 kias
12
Q
Slats out flaps 20•
A
190 kias
13
Q
Slats out flaps 40•
A
180 kias
14
Q
VLO
Safety speed for extending & retracting
A
190 kias or .70 Mach
15
Q
VLE
A
245 kias or .75 Mach
16
Q
VMCA
A
85.2 KCAS
17
Q
All Engines Operative
VMCL
A
85 KCAS
18
Q
One engine inoperative Vmcl
A
83 KCAS
19
Q
Vmcg
A
88.9 KCAS
20
Q
V wwo
A
215 KCAS
21
Q
V window
A
215 KCAS
22
Q
Max Tire Speed
A
195 kts
23
Q
Runway Slop limitations
A
+/- 2.5%
24
Q
Airport Pressure Altitude
A
-1,000 ft / +14,000 ft
25
Max Tailwind Takeoff & Landing
10 kts
26
Runway
Paved and Hard Surface
27
Max Operating Altitude
51,000
28
Cabin Pressure Differential
9.6 psi
29
Max Negative Pressure Differential
-0.29
30
Cabin Pressure Dump
14,500 ft + / - 500 ft
31
Autopilot min height to engage after t/off
400 ft
32
Autopilot min height for operation except during approach and climb
1,000 ft
33
Autopilot coupled approach
| ILS with radio altimeter
80 ft
34
Coupled ILS no radio altimeter
150 ft
35
Autopilot coupled non-precision approach
250 ft
36
Auto throttle min height to engage in climb
400 ft
37
Auto throttle min to disengage during descent
80 ft
38
DC Voltage limits
32V
39
Engine Gen Max
Transient
Up to 43,000 ft
Above 43,000 ft
350A
300A
260A
40
Battery Limits
Amber 120•F
| Red 160•F
41
Max Speed with Arthur inop
260 kias or .76 Mach
42
Max altitude for slats and flaps
20,000
43
Fuel:
Engine 1
Engine 2
Engine 3
Engine 1: 1,050. (7,036 lbs)
Engine 2: 1,027. (6,885 lbs)
Engine 3: 1,056.5. (7,079 lbs)
Total: 3,133.5 (21,000 lbs)
44
Hydraulic Fluid
5606
45
Engine Anti-Ice
During climb and cruise it must be used below +10•C TAT
| and above -40•C SAT and in visible moisture
46
Wing Anti-Ice
Do not use with a TAT above 10•C / 50•F
Do not use on the ground
47
Landing Lights
Ground operation limited to 15 min with 45 min cooling between use
48
Max N1 speed
110%
49
Passenger Door
Max weight on door
One step
On baggage door
1200 lbs
440 lbs
220 lbs
50
Max thrust takeoff
5,000 lbs (N1)
51
Max Continuous Thrust
4,525 lb (N1)
52
Max Engine Rotor Speed Takeoff
| N1
100% takeoff max continuous
| 100.5% transient one second max
53
N2 Max Continuous
Takeoff 100%
| Transient 101.5% 1 second max
54
Max ITT
Ground Start 994•C
Air Start 994•C
T/Off 5 min max 1,022•C
Max Continuous 991•C
55
Starting Time
| Ground & Starter assist air start
10 seconds max
56
Starting time
Windmilling air start
60% N2
45 seconds max
57
Starter
Ground start
Light off to idle
60 seconds max
58
Oil Pressure
| Max Continuous
Min pressure 65 psi
| Max pressure 80 psi
59
Oil Pressure
| Idle
Min 60 psi
| Max 80 psi
60
Oil Pressure
| Transient
100 psi less than 3 min
61
Red Oil Pressure Lights come up on panel when?
Below 50 psi
| All Engines
62
Oil Temp
| SL - 30,000 ft
127•C max
63
Oil Temp
| Above 30,000 ft
140•C max
64
Oil Temp
| Transient all altitudes
149•C
| Less than 2 minutes
65
Oil temp
| Min for exceeding idle power
30•C
66
Max Standing Water
.5"
