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Envoy > Limitations > Flashcards

Limitations Flashcards

1
Q

Aircraft dimensions
Length

A

103’ 11” (104’)

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2
Q

Aircraft dimensions
Width

A

93’ 11” (94’) (Wingspan)

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3
Q

Aircraft Dimensions
Height

A

32’ 4” (33’)

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4
Q

Cabin Loading
Max Pax

A

76

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5
Q

Cabin loading
First

A

12

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6
Q

Cabin Loading
Coach

A

64

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7
Q

Cargo Compartment Max Weight
FWD

A

3307 lbs

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8
Q

Cargo Compartment Max Weight Limits
AFT

A

2535 lbs

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9
Q

Aircraft Weights
MRW

A

85,800 lbs

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10
Q

Aircraft weights
MTOW

A

85,500 lbs

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11
Q

Aircraft weights
MLW

A

74,900 lbs

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12
Q

Aircraft Weights
MZFW

A

69,800 lbs

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13
Q

Minimum Crew

A

Left seat pilot and Right seat pilot (Captain & First Officer)

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14
Q

Aircraft Operations (5)

A
  • Day & Night
  • VFR & IFR
  • Icing Conditions
  • CAT I & CAT II
  • RVSM
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15
Q

Max Cabin Differential Overpressure (Safety Valve)

A

8.8 PSI

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16
Q

Max Cabin Differential Pressure
Above FL370

A

8.4 PSI

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17
Q

Max Cabin Differential Pressure
T/O & Landing

A

0.2 PSI

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18
Q

Max negative Cabin Differential Pressure

A

-0.5 PSI

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19
Q

Max Altitude Depressurized

A

10,000’ or MEA whichever is Higher

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20
Q

Max Altitude for Single Pack Operation

A

31,000

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21
Q

Airspeed
MMO Above FL280

A

0.82M

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22
Q

Airspeed
VMO 10,000’ to FL280

A

320 KIAS

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23
Q

Airspeed
VMO Below 10,000’

A

250 KIAS*
- *FAA Regulatory Speed
- Structural Speed Limit 300 KIAS

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24
Q

Airspeed
VA

A

240 KIAS

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25
Airspeed VLE
250 KIAS
26
Airspeed VLO
250 KIAS
27
Airspeed VLR
250 KIAS
28
Airspeed VFE1
230 KIAS
29
Airspeed FE2
215 KIAS
30
Airspeed VFE3
200 KIAS
31
Airspeed VFE4
180 KIAS
32
Airspeed VFE5
180 KIAS
33
Airspeed VFEFULL
165 KIAS
34
Max Turbulent Airspeed Below 10,000’
250 KIAS
35
Max Turbulent Airspeed 10,000’ and Above
270 KIAS or .76M
36
Max Crosswind for Takeoff (Dry)
35 kts
37
Max Crosswind for Takeoff (Wet)
30 kts
38
Max Crosswinds for landing
See AOM 1 Limitations
39
Max Tailwind
10 KT
40
Max Headwind for CAT II Operations
25 KT
41
Max Crosswind for Landing < RVR 4000 or 3/4
15 KT
42
Max DV (Direct View)Window Operation
160 KIAS
43
Max Tire Speed
195 KIAS
44
Max Windshield Wiper Speed
250 KIAS
45
Max Operating Altitude
41,000’
46
Max Flaps Extended Altitude
20,000’
47
Max Takeoff & Landing Altitude
10,000’
48
Min Takeoff & Landing Altitude
-1,000’
49
Minimum and Maximum Takeoff & Landing Temperature (SAT)
— 40 degrees C to 54 degrees C Note: in the event of a landing below - 40 degrees C, takeoff not authorized without further maintenance inspection
50
Max Altitude Display Difference in flight for RVSM
180 ft
51
APU First & Second Start Attempts
START/ON then 60 sec OFF
52
APU Third Start Attempt
START/ON then 5 min OFF
53
APU Brand Name
Sunstrand APS 2300
54
APU Minimum Starting Temperature
-54 degrees C
55
APU Maximum Operation Temperature
ISA + 39 degrees C Supplemental information applicable > ISA + 35 degrees C
56
APU EGT (Start) temperature
1032 degrees C
57
APU EGT (Continuous) temperature
717 degrees C No time limit in Amber on ground/inflight between 662-717 degrees C
58
APU Max Rotor Speed
108%
59
APU Max starting altitude ___________ ft Max Electrical Altitude __________ ft
30,000’ 33,000’
60
APU Max ENG Start Assist Altitude
21,000’
61
APU Max ECS Bleed Altitude
15,000’
62
Autopilot Min Engagement Altitude on Takeoff or Go Around
Above 400’
63
Autopilot Min Engaged Altitude during Landing
Above 50’
64
Engine Type
GE CF34-8E5
65
Engine Max N1 RPM
99.5%
66
Engine Max N2 RPM
99.4%
67
Engine Max Start ITT
815 degrees C
68
Engine max normal T/O ITT
2 minutes at 965 degrees 3 minutes at 949 degrees [Total 5 min]
69
Engine max T/O ITT Engine max G/A ITT
2 minutes at 1006 degrees C 3 minutes at 990 degrees C [Total 5 min]
70
Engine Max Continuous ITT
960 degrees C
71
Engine Min/Max Oil Pressure
25 PSI - 95 PSI
72
Engine Continuous Oil Temperature
155 degrees C
73
Engine Transient Oil Temperature
163 degrees C (15 min limit)
74
Engine Thrust T/O-1
13,000 lbs / OEI ATTCS = 14,200 lbs
75
Engine Thrust T/O-2
11,800 lbs / OEI ATTCS = 13,000 lbs
76
Brazilian Fuel type
QAV1
77
ASTM fuel type
Jet A or A1
78
American military Fuel Type
JP8
79
Fuel Capacity
20,934 lbs (10,467 lbs / tank)
80
Useable fuel
20,784 lbs (10,392 lbs/tank)
81
Unusable Fuel
150 lbs (75 lbs/tank)
82
Imbalance fuel
794 lbs
83
Min fuel tank temp
-37 degrees C
84
Fuel Crossfeed Operation must be ______ for takeoff and landing
OFF
85
Engine 1st & 2nd Starter Time GND
90 sec START / 10 Sec cool down
86
Engine 1st & 2nd Starter time FLT
120 sec START / 10 sec cool down
87
Engine 3rd-5th Starter time GND
90 sec START / 5 min cool down
88
Engine 3rd-5th Starter time FLT
120 sec START / 5 min cool down
89
1st Dry Motor Starter Time
Max 90 sec followed by 5 min cool down
90
2nd-5th Dry Motor Starter Time
Max 30 sec followed by 5 min cool down Note: after 5 sequential Dry Motoring Cycles, the sequence may be repeated following a 15 min cool down period

Envoy (20 decks)

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