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Envoy E175 > Limitations > Flashcards

Limitations Flashcards

1
Q

Max Ramp Weight (MRW)
170/170/175
Std / LR

A

79,696 / 82,364 / 85,870

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2
Q

Max Takeoff Weight (MTOW)
170/170/175
Std / LR

A

79,344 / 82,011 / 85,517

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3
Q

Max Landing Weight (MLW)
170/170/175
Std / LR

A

72,310 / 72,310 / 74,957

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4
Q

Max Zero Fuel Weight (MZFW)
170/170/175
Std / LR

A

65,256 / 65,256 / 69,886
66,446 / 66,446

66,446 is aircraft post-mod SB 170-00-0024

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5
Q

Max Cargo Weight (FWD)
170/170/175
Std / LR

A

3,020 / 3,020 / 3,307

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6
Q

Max Cargo Weight (AFT)
170/170/175
Std / LR

A

2,271 / 2,271 / 2,535

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7
Q

Length

A

103 Ft. 11 in.

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8
Q

Height

A

32 Ft. 3 in.

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9
Q

Width w/ enhanced winglets

A

93 Ft. 11 in.

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10
Q

Max turning width for 180 deg. turn

A

59 ft. 2 in.

Envoy uses 60 ft for conservative planning

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11
Q

Cabin Configuration?

A

Dual cabin
12 First Class Seats
64 Coach Seats

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12
Q

Each fuel tank holds ___ lbs. of usable fuel
_____ lbs. total
_____ gal. total

A

10,392 lbs. of usable fuel per tank
20,784 lbs. total
3094 gal. total

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13
Q

Fuel density

A

6.77 lbs/US gal.

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14
Q

___ lbs. unusable per tank

A

75 lbs.

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15
Q

Max Thrust

A

14,200 lbs

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16
Q

Type of engine

A

GE CF34-8E5

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17
Q

Service Ceiling

A

41,000

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18
Q

Maximum operating Mach number (Mmo)

A

Mach .82

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19
Q

Nose gear maximum steering angle

A

76 deg.

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20
Q

ELT Battery lifespan

A

~72 Hours

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21
Q

Maximum headwind for Cat II approaches

A

25 kts

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22
Q

Maximum crosswind for landing vis < 4000 or 3/4

A

15 kts (E)

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23
Q

Maximum takeoff and landing tailwind component

A

10 kts

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24
Q

Maximum crosswind for takeoff (dry)

A

35 kts (E)

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25
Q

Maximum crosswind for takeoff (wet)

A

30 kts (E)

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26
Q

Maximum altitude with flaps extended

A

20,000 ft

27
Q

Maximum operating airspeed (Vmo)

A

320

28
Q

Turbulent airspeed (below 10,000)

A

250 KIAS

29
Q

Turbulent airspeed (at or above 10,000)

A

270 KIAS / .76M

Whichever is lower

30
Q

Maximum airspeed for windshield wiper operation

A

250 KIAS

31
Q

Minimum Fuel temperature

A

-37C

32
Q

Maximum permissible fuel imbalance between left and right tanks

A

794 lbs

33
Q

Maximum altitude for single pack operation

A

31,000 ft

34
Q

Starter cycle limits

A

1st and 2nd starts: 90 seconds on ground… 120 seconds in air… 10 seconds off
3rd through 5th starts: 90 seconds on ground… 120 seconds in air… 5 minutes off

35
Q

Dry motoring starter cycle limits

A

1st start: 90 seconds on… 5 minutes off
2nd through 5th starts: 30 seconds on… 5 minutes off

** After five sequential motorings, cycle may be repeated following a 15 minute cool down period

36
Q

Application of maximum reverse thrust is not permitted at airspeeds below ____ kts during normal operations. Below ____ kts reduce thrust to idle

A

60 kts

60 kts

37
Q

APU starter cycle limits

A

1st and 2nd cycle: START/ON followed by 60 seconds of

3rd cycle: START/ON followed by 5 minutes off

38
Q

Max altitude for APU start

A

30,000 ft

39
Q

Max altitude for APU operation - Electrical

A

33,000 ft

40
Q

Max altitude for APU operation - Bleed

A

15,000 ft

41
Q

Max altitude for APU operation - to assist in engine start

A

21,000 ft

42
Q 
Max operating speed for flaps:
1 = 
2=
3=
4=
5=
FULL =
A 
Max operating speed for flaps:
1 = 230 KIAS
2= 215 KIAS
3= 200 KIAS
4= 180 KIAS
5= 180 KIAS
FULL = 165 KIAS
43
Q

Max DV window speed

A

160 KIAS

44
Q

Cabin Altitude HI / Rapid Decompression

A

Oxygen Masks ……. CR …… ON, 100%

45
Q

Jammed control column - pitch

A

Elevator Disconnect …… CR …… PRESS and PULL

46
Q

Jammed control wheel - roll

A

Aileron Disconnect …… CR …… PRESS and PULL

47
Q

Pitch Trim Runaway

A

AP/TRIM Disconnect …… PRESS and HOLD

TRIM PITCH SYS 1 & 2 CUTOUT …… Push In

48
Q

Roll or Yaw trim runaway

A

AP/TRIP Disconnect …… PRESS and HOLD

49
Q

Nosewheel steering runaway

A

Steering Disconnect …… PRESS

50
Q

Aborted Engine Start

A

Associated Thrust Lever …… IDLE

Associated START/STOP …… STOP

51
Q

Icing conditions definition

A

OAT (on the ground and for
takeoff) or TAT (inflight) is 10°C or below and;
• Visible moisture in any form is present such as clouds, fog (one mile or
less visibility), rain, snow, sleet and ice crystals, or
• When operating on ramps, taxiways, or runways where surface snow, ice,
standing water, or slush may be ingested by engines, freeze on engines,
nacelles, or engine sensor probes.

52
Q

Max tire ground speed

A

195 kts

53
Q

Max crosswind for landing on a dry runway

A

38 kts

54
Q

The normal straight ahead taxi speed on dry pavement SHOULD not exceed _____?

A

30 kts

55
Q

The normal straight ahead taxi speed on wet pavement SHOULD not exceed _____?

A

10 kts

56
Q

What is VLE?

A

250 kts

57
Q

MAX differential pressure

A

8.4 PSI

58
Q

MAX differential over pressure

A

8.8 PSI

59
Q

What is the MAX differential pressure for takeoff and landing?

A

0.2 PSI

60
Q

What is MAX continuous ITT?

A

960 C

61
Q

What is the minimum BATT 2 Temperature for APU starting?

A

-20C

62
Q

Maximum negative differential pressure

A

-0.5 PSI

63
Q

Engine limitation colors

Red / Amber / Green

A

Maximum and minimum limitations
Caution range
Normal operating range

Envoy E175 (22 decks)

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