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RJET E-170 Validation Guide > Limitations > Flashcards

Limitations Flashcards

1
Q

Types of Operations

A
  1. VFR
  2. IFR
  3. Icing conditions
  4. CAT I
  5. CAT II
  6. RVSM
  7. EOW; E175 when properly equipped

SOP 3-2

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2
Q

Max ramp weight

A

82,364

SOP 3-3

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3
Q

Max Takeoff weight

A

82,011

SOP 3-3

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4
Q

Max landing weight

A

72,310

SOP 3-3

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5
Q

Max zero fuel weight

A

65,256
66,446 for N646RW and above

SOP 3-3

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6
Q

Min crew

A

pilot and copilot

SOP 3-4

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7
Q

Max t/o and landing tailwind

A

10 knots

SOP 3-4

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8
Q

Max runway slope

A

+/- 2.0 %

SOP 3-4

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9
Q

Runway surface type

A

Paved

SOP 3-4

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10
Q

Flaps up maneuvering G load

A

-1.0G to +2.5G

SOP 3-4

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11
Q

Flaps down maneuvering G load

A

0.0G to +2.0G

SOP 3-4

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12
Q

Max operating altitude

A

41,000 ft

SOP 3-4

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13
Q

Max T/O and landing altitude

A

8,000 ft

SOP 3-4

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14
Q

Max ambient temp t/o and landing

A

+52C

SOP 3-4

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15
Q

TAS, TAT and SAT valid above speed

A

60 knots

SOP 3-13

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16
Q

Mag compass not valid when…

A

Transmitting on VHF #1

SOP 3-13

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17
Q

All CAT I approaches must use…

A

BARO altimeter mins

SOP 3-13

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18
Q

Back course ILS prohibited when…

A

On IESS

SOP 3-13

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19
Q

A/P min engagement height for takeoff

A

400 ft

SOP 3-18

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20
Q

A/P min height for approach on coupled ILS

A

50 ft

SOP 3-18

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21
Q

Max operating airspeed

A

VMO

tbd

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22
Q

Max operating mach number

A

.82M (MMO)

tbd

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23
Q

Max A/S for RAT operation

A

VMO/MMO

tbd

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24
Q

Turbulent air A/S below 10,000ft

A

250KIAS

SOP 3-6

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25
Q

Turbulent air A/S above 10,000 ft

A

270KIAS
.76M

SOP 3-6

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26
Q

Max tire ground speed

A

195 knots

SOP 3-6

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27
Q

Max windshield wiper operation speed

A

250 KIAS

SOP 3-9

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28
Q

Max gear extension/extended/retraction speed

A

250 KIAS

SOP 3-6

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29
Q

Design maneuvering speed

A

240 KIAS

SOP 3-8

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30
Q

VFE1 (structural/republic)

A

230 KIAS

To extend the life of the flaps, the flaps should be extended as much as possible below max flap extension speed, but in no case below green dot

SOP 3-6

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31
Q

VFE2 (structural/republic)

A

215 KIAS

To extend the life of the flaps, the flaps should be extended as much as possible below max flap extension speed, but in no case below green dot

SOP 3-6

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32
Q

VFE3 (structural/republic)

A

200 KIAS

To extend the life of the flaps, the flaps should be extended as much as possible below max flap extension speed, but in no case below green dot

SOP 3-6

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33
Q

VFE4 (structural/republic)

A

180 KIAS

To extend the life of the flaps, the flaps should be extended as much as possible below max flap extension speed, but in no case below green dot

SOP 3-6

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34
Q

VFE5 (structural/republic)

A

180 KIAS

To extend the life of the flaps, the flaps should be extended as much as possible below max flap extension speed, but in no case below green dot

SOP 3-6

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35
Q

VFE full (structural/republic)

A

165 KIAS

To extend the life of the flaps, the flaps should be extended as much as possible below max flap extension speed, but in no case below green dot

SOP 3-6

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36
Q

Max operating speed SL-8,000ft

A

300 KIAS

SOP 3-7

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37
Q

Max operating speed 8K-10K

A

300-320 KIAS

SOP 3-7

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38
Q

Max operating speed 10K-FL290

A

320 KIAS

SOP 3-7

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39
Q

Max operating speed FL290-FL410

A

.82M

SOP 3-7

40
Q

Definition of icing conditions

A

When SAT on ground or TAT in flight is:

  1. 10C or below; and
  2. Visible moisture is present in any form, such as clouds, fog with vis
41
Q

Engine and wing anti-ice system operation on ground

A

During taxi and takeoff the MCDU DATASET MENU must be set to ALL when SAT is 10C or below and icing conditions exist or are anticipated

SOP 3-9

42
Q

Engine and wing anti-ice systems operations in flight

A

The engine and wing anti-ice systems operate automatically in case of ice encounter when the ICE PROTECTION Mode Selector is in AUTO. If either one or both ice detectors are failed, the crew must set the mode selector to ON when icing conditions exist or are anticipated at or below 10°C TAT with visible moisture.

SOP 3-9

43
Q

Max fuel capacity

A

20,935 lbs

SOP 3-10

44
Q

Unusable fuel quantity per tank

A

75 lbs

SOP 3-10

45
Q

Min fuel tank temp

A

-40C

SOP 3-10

46
Q

Max fuel imbalance

A

790 lbs

SOP 3-10

47
Q

X-Feed operations for t/o and landing

A

Must be set to OFF

SOP 3-10

48
Q

Max differential pressure up to 37,000ft

A

7.8 PSI

SOP 3-11

49
Q

Max differential pressure 37,000-41,000 ft

A

8.3 PSI

SOP 3-11

50
Q

Max differential overpressure

A

8.7 PSI

SOP 3-11

51
Q

Max differential negative pressure

A

-0.5 PSI

SOP 3-11

52
Q

Max differential pressure for t/o and landing

A

0.2 PSI

SOP 3-11

53
Q

Max altitude single pack operation

A

31,000 ft

SOP 3-11

54
Q

Max flap extension altitude

A

20,000 ft

SOP 3-12

55
Q

Thrust reverser limitations

A

a. Ground use only
b. Rejected takeoffs and full stop landings only
c. Do not attempt go-around after deployment
d. Power-back prohibited
e. Must be stowed below 60KIAS
f. After use, do not move TLs to forward range until REV turns amber or green on EICAS

SOP 3-12

56
Q

Max APU rotor speed (%)

A

108%

SOP 3-23

57
Q

Max APU ITT start

A

1032C

SOP 3-23

58
Q

Max APU continuous ITT

A

717C

SOP 3-23

59
Q

Max APU start altitude

A

30,000ft

SOP 3-23

60
Q

Max APU electrics-only altitude

A

33,000 ft

SOP 3-23

61
Q

Max APU electric and pneumatics altitude

A

15,000 ft

SOP 3-23

62
Q

Max APU assist engine start altitude

A

21,000ft

SOP 3-23

63
Q

Min outside APU operation temp

A

-62C

SOP 3-23

64
Q

Max outside APU operation temp

A

ISA +35C

SOP 3-23

65
Q

APU starter duty cycle

A

2 X (60 on, 60 off) + 60 on, 5 mins off

SOP 3-23

66
Q

Do not takeoff when brake temp is…

A

In the amber range

67
Q

Max CAT II x-wind

A

12 knots

SOP 3-19

68
Q

Are manual FD director CAT II approaches authorized?

A

No

SOP 3-19

69
Q

Max N1 speed

A

99.5%

SOP 3-20

70
Q

Min N2 speed

A

58.5%

SOP 3-20

71
Q

Max N2 speed

A

99.4%

SOP 3-20

72
Q

Max engine start ITT

A

815C

SOP 3-20

73
Q

Max engine inflight start ITT

A

815C

SOP 3-20

74
Q

Max NORMAL engine TOGA ITT and time limits

A

965C for 1st 2 mins, then:
949C for following 3 mins

SOP 3-20

75
Q

Max MAX TOGA ITT and time limits

A

1006C for 1st 2 mins, then:
990C for following 3 mins

SOP 3-20

76
Q

Max continuous engine ITT

A

960C

SOP 3-20

77
Q

Engine oil pressure range

A

25-95PSI

SOP 3-20

78
Q

Max continuous engine oil temp

A

155C

SOP 3-20

79
Q

Max transient oil temp

A

163C for up to 15 mins

SOP 3-20

80
Q

EICAS color markings

A

Red - max and min limitations
Amber - caution range
Green - normal operating range

SOP 3-21

81
Q

Max thrust reduction with FLEX

A

25%

SOP 3-21

82
Q

When is FLEX prohibited?

A

On runways contaminated with standing water, slush, snow, or ice and are not allowed on wet runways unless suitable performance accountability is made for the increased stopping distance.

SOP 3-21

83
Q

Engine starter duty cycle on ground

A

1st and 2nd attempt: 90 sec ON, 10 secs OFF
3rd-5th attempts: 90 secs ON, 5 mins OFF

SOP 3-22

84
Q

Engine start duty cycle in flight

A

1st and 2nd attempt: 120 secs ON, 10 secs OFF
3rd-5th attempt: 120 secs ON, 5 mins OFF

SOP 3-22

85
Q

Engine start dry motoring duty cycle

A

1st attempt: 90 secs ON, 5 mins OFF
2nd-5th attempt: 30 secs ON, 5 mins OFF
after 5th attempt: 15 mins OFF

SOP 3-22

86
Q

What are the five factors that can limit takeoff weight?

A
  1. Max takeoff weight (climb limited)
  2. Max field length limited takeoff weight
  3. Max certified takeoff weight
  4. Obstacle clearance, enroute and landing limitations
  5. Brake energy limit weights

SOP 3-2

87
Q

What factors determine max landing weight?

A
  1. Max approach and landing weight (runway length plus obstacle, altitude, and temp and including limitations for inoperative equipment)
  2. Max landing weight (climb limited)
  3. Max certified landing weight

SOP 3-2

88
Q

Forward cargo compartment weigh limit

A

3,020 lbs

SOP 3-3

89
Q

Aft cargo compartment weight limit

A

3,307 lbs

SOP 3-3

90
Q

Max recommended crosswind, all conditions

A 
Dry - 38 KIAS
Wet - 31 KIAS
Compact snow - 20 KIAS
Standing water/Slush - 18 KIAS
Wet ice - 12 KIAS

SOP 3-4

91
Q

Max direct vision window opening speed

A

160 KIAS

92
Q

Other than speed and altitude, what are the flap operating limitations?

A

No enroute use, no holding in icing conditions with flaps extended, do not use flaps 4 for approach and landing

93
Q

RVSM Min Equipment Required

A
  • 2 ADS
  • 1 Autopilot, engaged, with ALT mode operative
  • 1 Altitude Alerter
  • 1 Transponder

SOP 3-14

94
Q

Under what conditions is ADS 3 non-RVSM compliant?

A

In case of loss of sideslip compensation. “ADS3 SLIPCOMP FAIL”)

SOP 3-14

95
Q

A ___ cool down must be observed prior to shutting down an engine

A

2 minute

SOP 3-20

RJET E-170 Validation Guide (7 decks)

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