Limitations Flashcards

(79 cards)

1
Q

Aircraft Length

A

103’ 11” (104’)

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2
Q

Aircraft Width

A

93’ 11” (94’)

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3
Q

Aircraft Height

A

32’ 4” (33’)

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4
Q

Max Passengers

A

76 (12 First, 64 Coach)

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5
Q

Cargo Compartment - FWD

A

3,306 lbs

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6
Q

Cargo Compartment - AFT

A

2,535 lbs

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7
Q

Minimum Crew

A

Left Seat Pilot and Right Seat Pilot

Captain and First Officer

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8
Q

Aircraft Operations

A
  • Day and Night
  • VFR and IFR
  • Icing Conditions
  • CAT I and CAT II
  • RVSM
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9
Q

Max Cabin Differential Overpressure

A

8.7 psi

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10
Q

Max Cabin Differential Pressure

Above FL370

A

8.3 psi

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11
Q

Max Cabin Differential Pressure

At or Below FL370

A

7.8 psi

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12
Q

Max Cabin Differential Negative Pressure

A

-0.5 psi

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13
Q

Max Cabin Differential for Takeoff and Landing

A

0.2 psi

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14
Q

Max Altitude Depressurized

A

10,000’ or MEA whichever is higher

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15
Q

Mmo (Above FL280)

A

0.82

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16
Q

Vmo (Above 10,000’ to FL280)

A

320 KIAS

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17
Q

Vmo (Below 10,000’)

A

250 KIAS (FAA Regulatory Speed, Structural Speed Limit is 300 KIAS)

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18
Q

Va

A

240 KIAS

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19
Q

Vle

A

250 KIAS

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20
Q

Vlo

A

250 KIAS

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21
Q

Vlr

A

250 KIAS

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22
Q

Vfe1

A

230 KIAS

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23
Q

Vfe2

A

215 KIAS

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24
Q

Vfe3

A

200 KIAS

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25
Vfe4
180 KIAS
26
Vfe5
180 KIAS
27
VfeFull
165 KIAS
28
Max Turbulent Airspeed | Below 10,000'
250 KIAS
29
Max Turbulent Airspeed | 10,000' and Above
270 KIAS or .76 Mach
30
Max Crosswind for takeoff (Dry/Wet)
35 kts Dry, 30 kts Wet
31
Max Crosswinds for Landing
``` Poor: 8kts Medium to Poor: 12kts Medium: 15kts Good to Medium: 20kts Good: 31kts 38kts ```
32
Max Tailwind
10 kts
33
Max DV Window Operation
160 KIAS
34
Max Tire Speed
195 KIAS
35
Max Windshield Wiper Speed
250 KIAS
36
Max Operating Altitude
41,000'
37
Max Altitude with Flaps Extended
20,000'
38
Max Takeoff and Landing Elevation
8,000'
39
Min Takeoff and Landing Elevation
-1,000'
40
Min/Max Takeoff and Landing | Temperature (SAT)
-40 degrees C / 52 degrees C
41
APU name
Sundstrand APS 2300
42
APU Starting limits
1st and 2nd Start Attempt - START/ON then 60 sec. OFF | 3rd Start Attempt - START/ON then 5 min. OFF
43
APU Min Operation Temp
-54 degrees C
44
APU Max Operation Temp
ISA +35 degrees C
45
APU EGT (Start)
1032 degrees C
46
APU EGT (Continuous)
717 degrees C | Note: No time limit in amber on the ground/inflight from 662C to 717C
47
APU Max Operation Altitude | Electrical
33,000'
48
APU Max Start Altitude
30,000'
49
APU Max Operation Altitude | Eng. Start Assist
21,000'
50
APU Max Operation Altitude | ECS Bleed
15,000'
51
APU Max Rotor Speed
108%
52
Autopilot Min Engagement Alt
Above 400'
53
Autopilot Min Engaged Alt
Above 50'
54
Engine name
GE CF34-8E5
55
Engine max N1
100%
56
Engine max N2
100%
57
Engine Max Start ITT
815 degrees C
58
Engine Max Normal T/O ITT
965C (2 min) / 949C (3 min) [Total - 5 min]
59
Engine Max T/O and G/A ITT
1006C (2 min) / 990C (3 min) [Total - 5min]
60
Engine Min/Max Oil Pressure
25 psi / 95 psi
61
Engine Continuous Oil Temp
155 degrees C
62
Engine Transient Oil Temp
163 degrees C (15 min limit)
63
Engine Thrust: T/O-1 / OEI ATTCS
T/O-1 = 13,000 lbs / OEI ATTCS = 14,200 lbs
64
Engine Thrust: T/O-2 / OEI ATTCS
T/O-2 = 11,800 lbs / OEI ATTCS = 13,000 lbs
65
Fuel types
- Brazilian - QAV1 - ASTM - Jet A or A1 - American - JP8
66
Max Fuel Capacity
20,934 lbs (10,467 lbs per tank)
67
Max Useable Fuel Quantity
20,784 lbs (10,392 lbs per tank)
68
Unusable Fuel Quantity
150 lbs (75 lbs per tank)
69
Maximum Fuel Imbalance
800 lbs
70
Minimum Fuel Tank Temp
-40 degrees C
71
Crossfeed Operation
Crossfeed Knob must be OFF for Takeoff and Landing
72
Starter Limits (Dry Motor)
1st - Max 90 sec, 5 min cooldown 2nd to 5th - Max 30 sec, 5 min cooldown (After 5 seq dry motors, 15 min cooldown)
73
Starter Limits (Normal)
1st and 2nd - 90/120sec (Grd/Flt), 10 sec Cool-down | 3rd to 5th, 90/120sec (Grd/Flt), 5 min Cool-down
74
Taxi and Ramp Weight
85,800
75
Takeoff Weight (MTOW)
85,500
76
Landing Weight (MLW)
74,900
77
Zero Fuel Weight (MZFW)
69,800
78
Maximum allowable in-flight difference between Captain and FO altimiters for RVSM
200ft
79
Max reverse thrust is not permitted below __ KIAS during normal operations
60