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E175 (Envoy) > Limitations > Flashcards

Limitations Flashcards

1
Q

max ramp weight

A

85800

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2
Q

Max takeoff weight

A

85500

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3
Q

Max Landing weight

A

74900

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4
Q

max zero fuel

A

69,800

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5
Q

fwd cargo weight

A

3306

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6
Q

aft cargo weight

A

2535

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7
Q

max headwind cat II

A

25 knots

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8
Q

max crosswind dry

A

35 (Mark said 38)

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9
Q

max crosswind less than 4000 and 3/4

A

15 (e)

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10
Q

max crosswind takeoff (wet)

A

30 (e)

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11
Q

max runway slope

A

+/- 2°

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12
Q

max maneuvering load limits flaps up

A

-1.0 to +2.5

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13
Q

Max maneuvering load limit flaps down

A

-0 to +2.0

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14
Q

maximum operating altitude

A

41,000’

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15
Q

Max T/O and LDG alt

A

8000

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16
Q

MAX SAT FOR T/O LDG/ GND START

A

52C

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17
Q

max alt with flaps extended

A

20,000

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18
Q

max operating latitude

A

78N (E)

78S (E)

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19
Q

Min SAT for T/O LDG and GND Start

A

-40C

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20
Q

Max Crosswind Code 6 breaking action (-)

A

38 knots

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21
Q

Max Crosswind Code 5 breaking action (good)

A

31

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22
Q

Max Crosswind Code 4 breaking action (good to medium)

A

20

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23
Q

Max Crosswind Code 3 breaking action (Medium)

A

15

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24
Q

Max Crosswind Code 2 breaking action (medium to poor))

A

12

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25
Q

Max Crosswind Code 1 breaking action (Poor)

A

8

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26
Q

What are all winds based limits based on

A

Peak Gust Value

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27
Q

Min operating speed limit

A

Intentional operation below onset of stall warning (stick shaker) is prohibited unless specifically authorized for flight test.

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28
Q

Max Opp Airspeed

A

320

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29
Q

Max Mach

A

.82

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30
Q

Max RAT airspeed

A

Vmo Mmo

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31
Q

Turbulent Airspeed below 10,000

A

250

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32
Q

Turbulent Airspeed above 10,000

A

270/.76M

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33
Q

Tire Limit Groundspeed

A

195 knots

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34
Q

Max speed windshield wiper operation

A

“Hi”

-Jason Vandergriff (hahaha)

(250 knots)

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35
Q

Max speed windshield wiper failed not in non-parked position

A

320KIAS

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36
Q

MAX SPEED FLIGHT DECK WINDOW OPEN

A

160 KIAS

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37
Q

MAX GEAR (Retraction, extension, extended)

A

250 KIAS

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38
Q

Flaps 1 MAX SPEED

A

230

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39
Q

Flaps 2 MAX SPEED

A

215

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40
Q

Flaps 3 MAX SPEED

A

200

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41
Q

Flaps 4 MAX SPEED

A

180

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42
Q

Flaps 5 MAX SPEED

A

180

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43
Q

Flaps FULL MAX SPEED

A

165

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44
Q

Min Controllable Speed

A

Vapp +10, refer to QRH

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45
Q

Design Maneuvering Speed

A

Full application of rudder and aileron controls, as well as maneuvers that involve angles of attach near stall must be confined to speeds at or below 240 KIAS

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46
Q

Definition of Ice

A

OAT or TAT (in flight) of 10C or below AND:

  • Visible moisture (precipitation or visibility of less than 1 mile)
  • operating on surfaces covered in snow, ice, slush, or standing water
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47
Q

Engine and Wind Anti-Ice temp limit in Auto

A

There is no temperature limit in the AUTO position

48
Q

Engine and Wing Anti-ice operations

A

must be set to “ALL” when 10C or below and icing conditions exist

49
Q

Approved Fuels

A

Jet-A and A-1
JP-8
QAV-1

When using JET-A with a temp below -30C, the fuel temp prior to flight must be verified to be above -29C

50
Q

Fuel density

A

6.77 lbs/gal

51
Q

Max fuel Capacity

A

10,392lbs per tank (20,734 total usable)

75lbs unusable fuel per tank

52
Q

Min Fuel Temp

A

-37C

53
Q

Max Fuel Imbalance

A

800lbs

54
Q

Crossfeed Operation for Takeoff and Landing

A

Crossfeed OFF for Takeoff and Landing

55
Q

APU Start Limit 1st/2nd cycle

A

60 seconds off per start

56
Q

APU Start Limit 3rd cycle

A

5 minutes off

57
Q

APU MIN/MAX temp for operation

A

-54C to ISA+35C

58
Q

MAX APU START ALT

A

30,000

59
Q

MAX APU OPERATION (ELECTRICAL)

A

33000

60
Q

MAX APU OPERATION (BLEED)

A

15,000

61
Q

MAX APU OPERATION (ENGINE START)

A

21,000

62
Q

MAX APU ROTOR SPEED

A

108%

63
Q

MAX APU EGT START

A

1032C

64
Q

MAX APU EGT CONTINUOUS OPERATION

A

717

65
Q

MAX SINGLE PACK ALT

A

31,000

66
Q

MAX DIFF PRESSURE (UP TO 37,000)

A

7.8

67
Q

MAX DIFF PRESSURE (ABOVE 37,000)

A

8.3

68
Q

MAX DIFF OVERPRESSURE

A

8.7

69
Q

MAX NEG DIFF PRESSURE

A

-0.5

70
Q

MAX DIFF PRESSURE FOR T/O AND LDG

A

.2

71
Q

OZONE CONCENTRATION LIMITS

A

REFER TO TABLE IN LIMITATIONS SECTION OF AOM 1

72
Q

BRAKE TEMP limit for Takeoff

A

DO NOT TAKE OFF WITH BRAKE TEMPS IN THE AMBER.

73
Q

FLAPS ENROUTE

A

ENROUTE USE OF FLAPS/SLATS IS PROHIBITED

74
Q

MAX ALTITUDE WITH FLAPS/SLATS EXTENDED

A

20,000

75
Q

AUTOPILOT MIN ALT

A

TAKEOFF- 400’

LANDING- 50’

76
Q

TCAS DEVIATIONS

A

DEVIATIONS FROM ATC CLEARANCES ARE AUTHORIZED TO COMPLY WITH TCAS RA

77
Q

TCAS DEVIATIONS BASED SOLELY ON NAV DISPLAY

A

MANEUVERS MUST NOT BE BASED SOLELY ON INFORMATION PRESENTED ON NAV DISPLAY

78
Q

IS COMPLIANCE WITH A TCAS RA REQUIRED

A

YES, UNLESS PIC DETERMINES DOING SO WOULD JEOPARDIZE SAFE OPERATION OF FLIGHT

79
Q

CAN YOU NAVIGATE WITH EGPWS DISPLAY

A

NO, NAV MUST NOT BE PREDICATED ON EGPWS DISPLAY

80
Q

ARE DEVIATIONS FROM ATC CLEARANCES PERMITTED TO COMPLY WITH EGPWS WARNINGS?

A

YES

81
Q

WHEN SHOULD THE PILOT MANUALLY INHIBIT TERRAIN/OBSTACLE AWARENESS ALERTING?

A

WITHIN 15 MILES ON APPROACH TO AN AIRPORT NOT IN THE EGPWS AIRPORT DATABASE

82
Q

HOW WILL CREWS KNOW AN AIRPORT IN NOT IN THE EGPWS DATABASE

A

IT WILL BE NOTED IN THE F4 MESSAGES OF THE RELEASE

83
Q

BANK ANGLES ON FMS LNAV

A

THERE IS NOT AUTOMATIC BANK ANGLE PROTECTION FOR SINGLE ENGINE OPERATIONS WHEN IN FMS LNAV

84
Q

TAS TAT AND SAT ARE ONLY VALID ABOVE WHAT AIRSPEED?

A

60 KNOTS

85
Q

WHAT TYPE OF ENGINE DO WE HAVE

A

GE CF34-8E5

86
Q

WHAT INFORMATION IS USED TO DETERMINE WHETHER WE ARE WITHIN ENGINE LIMITATIONS

A

THE MARKINGS ON THE EICAS

87
Q

MAX AND MIN ENGINE LIMITATIONS ARE DEPICTED ON THE EICAS HOW?

A

IN RED

88
Q

ENGINE CAUTION RANGE IS DEPICTED ON THE EICAS HOW?

A

AMBER

89
Q

ENGINE NORMAL OPERATING RANGE IS DEPICTED ON THE EICAS HOW?

A

GREEN

90
Q

NORMAL AND MAXIMUM TAKEOFF AND GO AROUND TEMPERATURES ARE LIMITED TO _____MINUTES DURING A ____ MINUTE PERIOD

A

5, 10

91
Q

NORMAL TAKEOFF AND GO AROUND TEMP/TIME LIMIT

A

965 (2 MIN)

949 (3MIN)

92
Q

MAX TAKEOFF AND GO AROUND TEMP/TIME LIMIT DURING WINDSHEAR OR OEI WITH THRUST LEVERS IN TOGA

A

1006 (2 MIN)

990 (3 MIN)

93
Q

MAX CONTINUOUS ENGINE TEMP LIMIT

A

960

94
Q

ENGINE START TEMP LIMIT

A

815

95
Q

ENGINE N1 MAX RPM

A

100% N1

96
Q

ENGINE N2 MAX RPM

A

100% N2

97
Q

MAX ENGINE OIL TEMP (TIME)

A

163C FOR 15 MINUTES

98
Q

MAX ENGINE OIL PRESSURE (TIME)

A

95PSI FOR 25 MIN

99
Q

ENGINE START CYCLE LIMIT GROUND (1ST AND SECOND)

A

90 SEC ON, 10 SECONDS OFF

100
Q

ENGINE START CYCLE LIMIT GROUND (3RD-5TH)

A

90 SEC ON, 5 MIN OFF

101
Q

ENGINE START CYCLE LIMIT FLIGHT (1ST AND 2ND)

A

120 SEC ON ON, 10 SEC OFF

102
Q

ENGINE START CYCLE LIMIT FLIGHT (3RD-5TH))

A

120 SEC ON, 5 MIN OFF

103
Q

ENGINE MOTORING LIMIT (AIR AND GND) (1ST)

A

90 SEC ON, 5 MIN OFF

104
Q

ENGINE MOTORING LIMIT (AIR AND GND) (2ND-5TH)

A

30 SEC ON, 5 MIN OFF

105
Q

AFTER 5 MOTORINGS, HOW MUCH TIME BEFORE CYCLE CAN BE REPEATED

A

15 MIN

106
Q

CAN WE GO AROUND AFTER DEPLOYING REVERSER

A

NO

107
Q

CAN WE BACK UP WITH REVERSE THRUST

A

NO

108
Q

CAN WE USE REVERSE THRUST IN THE AIR

A

NO

109
Q

MIN SPEED FOR FULL REVERSE THRUST

A

60 KIAS

110
Q

FUEL CIRCUIT BREAKER RESET (EVER?)

A

NO: “RESETTING A FUEL BOOST PUMP, OR FUEL INDICATING SYSTEM CIRCUIT BREAKER IS PROHIBITED.”

“THERE IS NO OPERATIONAL SITUATION IN WHICH IT WOULD BE NECESSARY TO RESET A TRIPPED FUEL BOOST PUMP OR FUEL INDICATING SYSTEM CIRCUIT BREAKER”

111
Q

MIN BATTERY TEMP FOR APU STARTING

A

-20C, THIS DOES NOT PROHIBIT STARTING THE APU VIA DC POWER IF A DC GPU IS AVAILABLE AND UTILIZED

112
Q

WHEN MUST THE FLIGHT DECK DOOR ACCESS SYSTEM BE TESTED

A

PRIOR TO THE FIRST FLIGHT OF THE DAY

113
Q

WHEN MUST THE ESCAPE SLIDES BE ARMED?

A

WHENEVER OCCUPANTS ARE IN THE CABIN, THE ESCAPE SLIDE MUST BE ARMED FOR TAXI, TAKEOFF, AND LANDING.

FOR DOOR ARMING REQUIREMENTS ON FERRY, TRAINING, AND CHARTER FLIGHTS, REFER TO FM-1 (E)

114
Q

ALTIMETER TOLERANCES (STBY ALT)

A

STBY ALTIMETERS DO NOT MEET ACCURACY REQUIREMENTS OF RVSM

115
Q

MAX ALLOWABLE IN FLIGHT DIFFERENCE BETWEEN CAPT AND FO ALTITUDE DISPLAY FOR RVSM?

A

200 FEET

116
Q

length
width
height

A

104
94
32

117
Q

certified operations

A 
day/night
VFR/IFR
ICING
CAT I
CAT II
RVSM

E175 (Envoy) (3 decks)

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