Limitations Memory Flashcards

(85 cards)

1
Q

Maximum headwind for Cat II approaches

A

25 knots

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2
Q

Maximum crosswind for landing vis less than 4000 RVR or 3/4

A

15 knots

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3
Q

Maximum takeoff and landing tailwind component

A

10 knots

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4
Q

Maximum crosswind for takeoff on dry runway

A

35 knots

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5
Q

Maximum crosswind for takeoff Wet runway

A

30 knots

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6
Q

Maximum operating altitude

A

41,000 feet

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7
Q

Maximum altitude with flaps extended

A

20,000 feet

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8
Q

Maximum operating airspeed (Vmo)

A

320

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9
Q

Maximum operating Mach number (Mmo)

A

.82

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10
Q

Turbulent airspeed (below 10,000 feet)

A

250 knots

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11
Q

Turbulent airspeed (at or above 10,000 feet)

A

270 KIAS/.76

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12
Q

Maximum airspeed for windshield wiper operation

A

250 Knots

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13
Q

Eng. Starter duty cycles

1st and 2nd

A

Maximum 90 seconds on (ground)120 seconds on (in flight)

Followed by 10 seconds off

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14
Q

Eng. Starter Duty Cycle
3rd though 5th

A

Maximum 90 seconds on (ground)120 seconds on (in flight)

Followed by 5 minutes off

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15
Q

Eng. Dry-Motoring Cycle
1st start 90 seconds on
2nd though 5th start 30 seconds on

A

Followed by 5 minutes off

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16
Q

Reverse Thrust is used….

A

For ground use only

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17
Q

Landing with reverse thrust..

A

Maximum reverse thrust is not permitted at air speeds below 60 knots.
Below 60 Knots set reverse thrust to idle.

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18
Q

Apu starter limits
1st and 2nd attempt

A

60 seconds off

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19
Q

Apu Starter Limits
3rd attempt

A

5 minutes off

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20
Q

Apu maximum altitude for APU start

A

30,000 feet

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21
Q

Apu maximum altitude for electrical use

A

33,000 feet

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22
Q

Apu maximum altitude for bleed use

A

15,000 feet

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23
Q

Apu maximum altitude for assist engine start

A

21,000 feet

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24
Q

Aircraft Dimensions

A
  • Length – 103’ 11” (104’)
  • *Width – 93’ 11 ” (94’)
  • Height – 32’ 4” (33’)
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25
Cabin Loading
• Max PAX - 76 | 12 First / 64 Coach
26
Minimum Crew
• Left Seat Pilot and Right Seat Pilot (i.e. Captain and First Officer)
27
Aircraft Operations
``` • Day & Night • VFR & IFR • Icing Conditions • CAT I & CAT II • RVSM Extended over water operations if equipped ```
28
Max Cabin Differential Over-pressure
8.8 psi
29
Max Cabin Differential Pressure (Above FL370)
8.4 psi
30
Max Cabin Differential Negative Pressure
-0.5 psi
31
Max Cabin Differential for Takeoff/Landing
0.2 psi
32
Max Altitude Depressurized
10,000’ or MEA whichever is Higher
33
Vmo (Below 10,000’)
250 *FAA Regulatory Speed / Structural Speed Limit is 300 KIAS
34
Va
240
35
Vle
250
36
Vlo
250
37
Vlr
250
38
Vfe1
230
39
Vfe2
215
40
Vfe3
200
41
Vfe4
180
42
Vfe5
180
43
VfeFull
165
44
Max Crosswinds for Landing
Braking action/Max crosswind 6/38 5/31 4/20 3/15 2/12 1/8
45
Max DV Window Operation
160 KIAS
46
Max Tire Speed
195 KIAS
47
Max Windshield Wiper Speed
250 KIAS
48
MAX Takeoff/Landing Altitude
10,000
49
MIN Takeoff/Landing Altitude
-1,000’
50
Min Takeoff /Landing Temperature (SAT)
-40°C Note: In the event of a landing below -40°C, the Airplane may not takeoff without further maintenance inspection.
51
APU Brand
Sundstrand APS 2300
52
APU Minimum Operation Temperature
-54°C
53
APU Maximum Operation Temperature
ISA + 35°C
54
APU EGT (Start)
1032°C
55
APU EGT (Continuous)
717°C Note: No time limit in amber on the ground/in-flight from 662°C to 717°C
56
APU Max Rotor Speed
108%
57
Autopilot Minimum Engagement Altitude on Takeoff or Go Around
400 Feet
58
Autopilot Minimum Engaged Altitude during Landing
Above 50 Feet
59
Engine Type
GE CF34-8E5
60
N1 Max
99.5%
61
N2 Max
99.4%
62
Max Start ITT
815°C
63
Max Normal T/O ITT
965°C (2 min.) / 949°C (3 min.) [Total – 5 min.]
64
Max T/O & G/A ITT
1006°C (2 min.) / 990°C (3 min.) [Total – 5 min.]
65
Max Continuous ITT
960°C
66
Min/Max Oil Pressure
25 psi / 95 psi
67
Continuous Oil Temperature
155°C
68
Transient Oil Temperature
163°C (15 min. limit)
69
Engine Thrust T/O-1
13,000 lbs. / OEI ATTCS = 14,200 lbs
70
Engine Thrust T/O-2
11,800 lbs. / OEI ATTCS = 13,000 lbs
71
Fuel Types Allowed
* Brazilian – QAV1 * ASTM – Jet A or A1 * American – JP8
72
Maximum Fuel Capacity
20,934 lbs. (10,467 lbs. per tank)
73
Maximum Useable Quantity
20,784 lbs. (10,392 lbs. per tank)
74
Unusable Quantity
150 lbs. (75 lbs. per tank)
75
Maximum Fuel Imbalance
794 lbs.
76
Minimum Fuel Tank Temperature
-37°C
77
Crossfeed Operation
Crossfeed Knob must be OFF for Takeoff and Landing
78
Max difference allowed between FO and CA altimeter in RSVM is:
180 ft.
79
Aircraft Dimensions
Length – 103’ 11” (104’) • Width – 93’ 11” (94’) (Wingspan) • Height – 32’ 4” (33’)
80
Cargo Compartment Max Weight Limits
* FWD – 3,306 lbs. * AFT – 2,535 lbs
81
Max Ramp Weight
85800
82
Max Takeoff Weight
85500
83
Zero Fuel Weight
69800
84
Max Landing Weight
74900
85
Max Takeoff/Landing Tempature SAT
52°C