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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
Q

Airspeed
VLE

A

250 KIAS

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26
Q

Airspeed
VLO

A

250 KIAS

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27
Q

Airspeed
VLR

A

250 KIAS

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28
Q

Airspeed
VFE1

A

230 KIAS

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29
Q

Airspeed
FE2

A

215 KIAS

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30
Q

Airspeed
VFE3

A

200 KIAS

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31
Q

Airspeed
VFE4

A

180 KIAS

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32
Q

Airspeed
VFE5

A

180 KIAS

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33
Q

Airspeed
VFEFULL

A

165 KIAS

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34
Q

Max Turbulent Airspeed
Below 10,000’

A

250 KIAS

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35
Q

Max Turbulent Airspeed
10,000’ and Above

A

270 KIAS or .76M

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36
Q

Max Crosswind for Takeoff
(Dry)

A

35 kts

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37
Q

Max Crosswind for Takeoff
(Wet)

A

30 kts

38
Q

Max Crosswinds for landing

A

See AOM 1 Limitations

39
Q

Max Tailwind

A

10 KT

40
Q

Max Headwind for CAT II Operations

A

25 KT

41
Q

Max Crosswind for Landing
< RVR 4000 or 3/4

A

15 KT

42
Q

Max DV (Direct View)Window Operation

A

160 KIAS

43
Q

Max Tire Speed

A

195 KIAS

44
Q

Max Windshield Wiper Speed

A

250 KIAS

45
Q

Max Operating Altitude

A

41,000’

46
Q

Max Flaps Extended Altitude

A

20,000’

47
Q

Max Takeoff & Landing Altitude

A

10,000’

48
Q

Min Takeoff & Landing Altitude

A

-1,000’

49
Q

Minimum and Maximum Takeoff & Landing Temperature (SAT)

A

— 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
Q

Max Altitude Display Difference in flight for RVSM

A

180 ft

51
Q

APU
First & Second Start Attempts

A

START/ON then 60 sec OFF

52
Q

APU
Third Start Attempt

A

START/ON then 5 min OFF

53
Q

APU Brand Name

A

Sunstrand APS 2300

54
Q

APU
Minimum Starting Temperature

A

-54 degrees C

55
Q

APU
Maximum Operation Temperature

A

ISA + 39 degrees C

Supplemental information applicable > ISA + 35 degrees C

56
Q

APU
EGT (Start) temperature

A

1032 degrees C

57
Q

APU EGT (Continuous) temperature

A

717 degrees C

No time limit in Amber on ground/inflight between 662-717 degrees C

58
Q

APU
Max Rotor Speed

A

108%

59
Q

APU
Max starting altitude ___________ ft
Max Electrical Altitude __________ ft

A

30,000’
33,000’

60
Q

APU
Max ENG Start Assist Altitude

A

21,000’

61
Q

APU
Max ECS Bleed Altitude

A

15,000’

62
Q

Autopilot
Min Engagement Altitude on Takeoff or Go Around

A

Above 400’

63
Q

Autopilot
Min Engaged Altitude during Landing

A

Above 50’

64
Q

Engine Type

A

GE CF34-8E5

65
Q

Engine Max N1 RPM

A

99.5%

66
Q

Engine Max N2 RPM

A

99.4%

67
Q

Engine Max Start ITT

A

815 degrees C

68
Q

Engine max normal T/O ITT

A

2 minutes at 965 degrees
3 minutes at 949 degrees [Total 5 min]

69
Q

Engine max T/O ITT
Engine max G/A ITT

A

2 minutes at 1006 degrees C
3 minutes at 990 degrees C [Total 5 min]

70
Q

Engine Max Continuous ITT

A

960 degrees C

71
Q

Engine Min/Max Oil Pressure

A

25 PSI - 95 PSI

72
Q

Engine Continuous Oil Temperature

A

155 degrees C

73
Q

Engine Transient Oil Temperature

A

163 degrees C (15 min limit)

74
Q

Engine Thrust
T/O-1

A

13,000 lbs / OEI ATTCS = 14,200 lbs

75
Q

Engine Thrust
T/O-2

A

11,800 lbs / OEI ATTCS = 13,000 lbs

76
Q

Brazilian Fuel type

A

QAV1

77
Q

ASTM fuel type

A

Jet A or A1

78
Q

American military Fuel Type

A

JP8

79
Q

Fuel Capacity

A

20,934 lbs (10,467 lbs / tank)

80
Q

Useable fuel

A

20,784 lbs (10,392 lbs/tank)

81
Q

Unusable Fuel

A

150 lbs (75 lbs/tank)

82
Q

Imbalance fuel

A

794 lbs

83
Q

Min fuel tank temp

A

-37 degrees C

84
Q

Fuel Crossfeed Operation must be ______ for takeoff and landing

A

OFF

85
Q

Engine 1st & 2nd Starter Time GND

A

90 sec START / 10 Sec cool down

86
Q

Engine 1st & 2nd Starter time FLT

A

120 sec START / 10 sec cool down

87
Q

Engine 3rd-5th Starter time GND

A

90 sec START / 5 min cool down

88
Q

Engine 3rd-5th Starter time FLT

A

120 sec START / 5 min cool down

89
Q

1st Dry Motor Starter Time

A

Max 90 sec followed by 5 min cool down

90
Q

2nd-5th Dry Motor Starter Time

A

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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