All Limitations Flashcards

1
Q

Max Ramp Weight

A

85870

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2
Q

Max T/O Weight

A

85517

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3
Q

Max Landing Weight

A

74957

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4
Q

Max Zero Fuel Weight

A

69886

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5
Q

Max Forward Baggage Weight

A

3306

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6
Q

Max Aft Baggage Weight

A

2535

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7
Q

Static Wicks on Wing tips

A

6 installed, 5 required

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8
Q

Static Wicks on Ailerons

A

3 installed 2 required

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9
Q

Static Wicks on Elevators

A

4 installed 3 required

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10
Q

Static Wicks Rudder/Stabilizer

A

5 installed 4 required

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11
Q

Max Runway Slope

A

+/-2 degrees

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12
Q

Max Latitude Alignment

A

N 78.25 degrees

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13
Q

Max T/O and Landing Altitude

A

10,000 Feet

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13
Q

Max T/O and Landing Temperature

A

52 C
ISA + 35 C

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13
Q

Min ambient temp for operations

A

-54 C

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13
Q

Minimum T/O and Landing Altitude

A

-1000

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14
Q

If landing below this temperature you may not takeoff
without maintenance inspection

A

-40 C

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15
Q

Gravity Load Factor with Flaps Up

A

+2.5/-1.0

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16
Q

Gravity Load Factor Flaps Down (All)

A

+2.0/-0.0

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17
Q

Max Altitude for Flap Operations

A

20,000

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18
Q

Flaps speeds

A

Flaps 1 230
Flaps 2 215
Flaps 3 200
Flaps 4 180
Flaps 5 180
Flaps Full 165

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19
Q

Approved Airplane Operations

A

VFR & IFR
Icing Conditions
CAT I & II
Extended Overwater Ops
RVSM
RNP

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20
Q

CAT II Demonstrated Headwind, tailwind, and Crosswind

A

Headwind: 25 kts
Crosswind: 12 kts
Tailwind: 10 kts

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21
Q

Gusts Limit on Pax Service Door Open/Closed

A

40 kts

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22
Gusts Limit Pax Service Door Open & Locked
65 kts
23
Max Speed Direct Vision Window
160 kts
24
Oxygen Requirement for 3 Crew Members
3 Green 1150
25
Oxygen Requirement for 2 Crew Members
2 Blue 842
26
Max Crosswind for Dry or Wet Runway
28 kts
27
Max Crosswind for Static T/O
25 kts
28
Max Crosswind for Compacted Snow
20 kts
29
Max Crosswind Standing Water/Slush/Wet Snow/Dry Snow
18 kts
30
Max Crosswind Ice (inc wet ice)
12 kts
31
Max N1 with Brakes Applied
60%
31
Max Fuel
20,935 lbs
32
Fuel Per Tank Usable
10,392.50 lbs
33
Unsuable Fuel per Tank
75 lbs
34
Maximum Fuel Imbalance
794 lbs
35
Maximum Fuel Imbalance Warning
800 lbs
36
Minimum Fuel Tank Temp
-37 C
37
Fuel Low Level Sensor In Collector Box
660 lbs
38
Max Operating Airspeed
320 kts
39
Max Operating MACH Number
.82
40
Min Airspeed RAT operation
130 kts
41
Max Wiper Speed
253 kts
42
Max Tire Ground Speed
195 kts
43
Turbulent Airspeed Below 10,000 Ft
250
44
Max Differential Pressure
8.4 psi
44
Turbulent Airspeed Above 10,000 Ft
270/.76
45
Max Differential Overpressure
8.8 psi
46
Positive Pres Relief Valve Opens
8.6 psi
47
Max Differential Negative Pressure
-.5 psi
48
Max Differential Pressure for T/O and Landing
.2 psi
49
Single Pack Operation Limit
31,000
50
Speed at which TAT, TAS, and SAT become valid
60 kts
51
Taxi Speeds Dry Straight Dry Turning Wet Straight Wet Turning
Dry Straight: 20 kts Dry Turning: 10 kts Wet Straight: 10 kts Wet Turning: 5 kts
52
Min APU Start Temp
-54 C
53
Max APU Start Temp
1032 C
54
APU Continuous Temp
717 C
55
APU Start Limitations
1st & 2nd attempt: 60 seconds off 3rd attempt: 5 minutes off
56
Max Engine ITT Start Temp on ground vs air
815 C on ground 927 C in the air
57
ITT Max T/O & GA
Max ITT 990 C. Can be exceeded up to 1006 C during the first 2 minutes. 2 Engine Max 5 mins. 1 Engine Max 10 min.
58
Max Continuous ITT
960 C
59
N1 Max
99.50%
60
N2 Min / Max
58.5% / 99.4%
61
Oil Pressure Min / Max
25 psi / 95 psi
62
Oil Temp Continuous
155 C
63
Oil Temp Max Transient
163 C limited to 15 mins
64
Engine Starter Duty Cycle 1-2
Max 90 seconds on ground; 120 seconds in flight. 10 seconds off
65
Engine Starter Duty Cycle 3-5
Max 90 seconds on ground; 120 seconds in flight. 5 minutes off
66
Engine Dry Motor Limits Cycle 1
Max 90 seconds on, 5 minutes off
67
Engine Dry Motor Limits Cycle 2-5
Max 30 seconds on, 5 minutes off
68
Minimum Auto Pilot Use Height
50 feet
69
What are the requirements for RVSM
1 Auto pilot 1 Altitude alert system 2 Altitude reporting transponders of which 1 must be operational 2 Air data computers both of which have to be operational