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E175 Systems > Aircraft Limitations > Flashcards

Aircraft Limitations Flashcards

1
Q

Types of Operations

A

VFR
IFR
Icing Conditions
CAT I and II
RVSM
RNP
Extended Overwater EOW

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2
Q

LR Maximum Ramp Weight (MRW)

A

85,870 lbs

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3
Q

LR Maximum Takeoff Weight (MTOW)

A

85,517 lbs

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4
Q

LR Maximum Landing Weight (MLW)

A

74,957 lbs

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5
Q

LR Maximum Zero Fuel Weight (MZFW)

A

69,886 lbs

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6
Q

Minimum Flight Crew

A

Pilot and Copliot

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7
Q

Max Takeoff and Landing Tailwind Component

A

10 knots

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8
Q

Max Runway Slope

A

+/-2%

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9
Q

Runway Surface Type

A

Paved

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10
Q

Flap Maneuvering Load Acceleration Limit - Flaps Up

A

-1.0 G to +2.5 G

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11
Q

Flap Maneuvering Load Acceleration Limit - Flaps Down
(1, 2, 3, 4, 5 and Full)

A

0.0 G to +2.0 G

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12
Q

Max Operating Altitude

A

41,000’

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13
Q

Max Takeoff and Landing Altitude

A

10,000’

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14
Q

Min Takeoff and Landing Altitude

A

-1,000’

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15
Q

Max Ambient Air Temperature for takeoff, landing and ground starts (decreases with altitude)

A

52 degrees C

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16
Q

Max Flap Extension Altitude

A

20,000’

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17
Q

Max Latitude for Stationary Alignment

A

78.25 degrees North
78.25 degrees South

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18
Q

Minimum Takeoff Temperature / Landing Below __ degrees C, you may not takeoff without further maintenance inspection

A

-40 degrees C SAT

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19
Q

Minimum Ambient Temperature for Operation on Ground

A

-54 degrees C

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20
Q

Temperature Compensation Baro-VNAV Operation Must Be:

A
  1. Coordinated with ATC
  2. Used for operation outside the temperature limits published the approach procedure
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21
Q

Max Operating Airspeed Abbreviation

A

Vmo

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22
Q

Max Operating Mach Number Mmo

A

.82M

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23
Q

Maximum Airspeed for RAT Operation

A

Vmo / Mmo

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24
Q

Max Windshield Wiper Operation Speed

A

253 KIAS

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25
Q

Max Gear Extension Speed Vloe

A

250 KIAS

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26
Q

Max Gear Extended Speed (Vle)

A

250 KIAS

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27
Q

Max Gear Retraction Speed (Vlor)

A

250 KIAS

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28
Q

Flaps 1

A

230 KIAS

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29
Q

Flaps 2

A

215 KIAS

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30
Q

Flaps 3

A

200 KIAS

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31
Q

Flaps 4

A

180 KIAS

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32
Q

Flaps 5

A

180 KIAS

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33
Q

Flaps Full

A

165 KIAS

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34
Q

Max Operating Speed Up to 8,000’

A

300 KIAS

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35
Q

Max Operating Speed 8,000’-10,000’

A

300 to 320 KIAS Increases Linearly

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36
Q

Max Operating Airspeed 10,000’ - FL290

A

320 KIAS Vmo

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37
Q

Max Operating Airspeed FL290 - FL410

A

.82M Mmo

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38
Q

Define Icing Conditions

A

OAT on the ground or TAT inflight is 10 degrees C or less with visible moisture in any form

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39
Q

Maximum Fuel Capacity

A

20,935 lbs Total

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40
Q

Unusable Fuel Quantity per Tank

A

75 lbs

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41
Q

Maximum Fuel Imbalance

A

794 lbs

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42
Q

Minimum Fuel Tank Temperature

A

-37 degrees C

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43
Q

Crossfeed Operation Limitation

A

Must be OFF for takeoff and landing

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44
Q

Max Differential Pressure

A

8.4 PSI

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45
Q

Max Differential Overpressure

A

8.8 PSI

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46
Q

Max Differential Negative Pressure

A

-0.5 PSI

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47
Q

Max Differential Pressure for Takeoff and Landing

A

0.2 PSI

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48
Q

Max Altitude for Single Pack Operation

A

FL310

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49
Q

Brake Temperature Limitation

A

Do not takeoff with brake temperatures in the amber

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50
Q

Thrust Reverser Limitations

A

DIMPFNG

Do not attempt a go-around (after deployment)
Idle thrust by 30 KIAS (translating cowl closed)
Min reverse thrust by 60 KIAS (translating cowl open)
Power back prohibited
Full Stop Landings
Not Authorized while Taxiing
Ground Use Only

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51
Q

Autopilot Minimum Engagement Height (Takeoff) per AFM

A

400’AGL per AFM (1,000’ per Mesa CFM)

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52
Q

Engine Model

A

CF34-8E5

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53
Q

Engine Takeoff/TOGA Thrust Time Limit

A

Time limited to 5min with all engines operative. This limit is extended to 10min with one engine inoperative for airplanes with Post-Mod 17073-0002 (which we have) or equipped with an equivalent modification factory incorporated.

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54
Q

Engine Start ITT Limitations (Min and Max)

A

Min: None, Max: 815deg C

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55
Q

EICAS Red Markings

A

Max and Min Limitations

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56
Q

EICAS Amber Markings

A

Caution Range

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57
Q

EICAS Green Markings

A

Normal Operating Range

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58
Q

FLEX Takeoff Reduction Limitaion

A

Must not exceed 25% full takeoff thrust

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59
Q

Can FLEX Takeoff be used on Contaminated Runways?

A

No. The FAA defines that a runway is contaminated whenever standing water, ice, snow, slush, frost in any form, heavy rubber or other substances are present. So “Good to Medium” reported.

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60
Q

ATTCS (Automatic Takeoff Thrust Control System) (selects RSV power for engine failures based on system logic)

A

Must be ON for all takeoffs and landings

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61
Q

Engine Starter Duty Cycle Limits - On Ground

A

Attempt 1,2: 90 sec ON / 10 sec OFF
Attempt 3,4,5: 90 sec ON / 5min OFF

For ground starts the max cumulative starter run time per start attempt is 90sec

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62
Q

Engine Starter Duty Cycle Limits - In Flight

A

Attempt 1-2: 120 sec ON / 10 sec OFF
Attempt 3-5: 120sec ON / 5min OFF

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63
Q

Dry Motoring Duty Cycle Limits (used to remove heat and fuel that was introduced but not ignited - only use for hot starts)

A

Attempt 1: 90 sec ON / 5 min OFF
Attempt 2-5: 30 sec ON / 5 min OFF
After 5, the cycle can be repeated after 15min

So in a scenario, you would attempt an engine start for 90sec ON, then 10sec OFF after it didn’t start. Then, if it is a hot start, you would dry motor the engine for 90sec ON max (QRH calls for 30sec), followed by 5min off. Then you could try starting the engine again on attempt 2 for 90sec ON, 10sec OFF. If you have to dry motor again, you will be on dry motoring attempt 2 so 30sec ON, 5min off. Then attempt an engine start for the 3rd time so then 90sec ON, 5min off. Maintenance must be called if the third attempt doesn’t work per the CFM.

For HOT Starts, the FADEC commands an automatic abort when ITT is 10°C lower than the engine hot start limit. This will prevent ENG EXCEEDANCE EICAS message to be displayed. In this case, two additional engine starts are allowed without any cause investigation.

If both the following conditions occur, only one additional engine start is allowed:
a. Engine start is manually aborted due to no ITT indication 15 seconds after fuel is reapplied, and
b. “ENG 1(2) NO DISPATCH” or “ENG 1(2) SHORT DISPATCH” EICAS messages are not displayed.

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64
Q

APU Starter Duty Cycle Limits

A

Attempt 1,2: 1min ON / 1min OFF
Attempt 3: 1min ON / 5min OFF

(The 1min ON shutoff function is automatically provided by the APU FADEC)

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65
Q

APU Start Min Temperature

A

-54 degrees C

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66
Q

APU Start Max Temperature

A

APU Temperature matches the Airplane Operational Envelope temperature (52deg C on the ground)

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67
Q

APU Start Max Altitude

A

30,000’

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68
Q

APU Operation Min Temperature

A

APU Temperature matches the Airplane Operational Envelope temperature (-54 deg C on the ground)

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69
Q

APU Operational Max Temperature

A

APU Temperature matches the Airplane Operational Envelope temperature (52deg C)

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70
Q

APU Operation Max Altitude

A

33,000’

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71
Q

APU Operation Max Electrical Gen Altitude

A

33,000’

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72
Q

APU Operational Max Bleed Altitude

A

15,000’

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73
Q

APU Operation Max Altitude to Assist Engine Start

A

21,000’

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74
Q

Is there an automatic in-flight shutdown if the APU EGT exceeds limits?

A

No

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75
Q

At what speed are the TAS, TAT, and SAT valid?

A

Above 60 KIAS

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76
Q

When is the standby magnetic compass not valid?

A

While transmitting on VHF #1

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77
Q

What kind of minimums must be used for all CAT I approaches?

A

Baro Minimums

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78
Q

Are pilots advised to deviate from their current ATC clearance to the extent necessary to comply with a RA?

A

Yes

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79
Q

Can you fly a LOC Back Course approach using IESS?

A

No

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80
Q

How many lbs of fuel are used for taxi?
About how many gallons is this?

A

353 lbs
~52 Gallons

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81
Q

How many lbs are a Gallon of Jet Fuel

A

6.8 lbs per Gallon

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82
Q

Is unusable fuel included in the Maximum Zero Fuel Weight?

A

Yes

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83
Q

What is the purpose of the MZFW Maximum Zero Fuel Weight?

A

Structural Limitation
Wings are subjected to upward bending stress that is counteracted by the weight of the fuel
If the fuel level becomes low and the aircraft weight is high, the wings may be subject to too much lift production
This could result in the wings becoming over-stressed in flight

84
Q

Max Fuel Capacity Per Tank

A

10,392.5 lbs per Tank (doesn’t include unusable fuel)

85
Q

Minimum Engagement Height (Takeoff) per GOM

A

1,000’AGL per GOM

86
Q

Minimum Use Height (Coupled ILS Approach)

A

50’AGL

87
Q

Fwd baggage compartment capacity

A

3,306lbs

88
Q

AFT baggage compartment capacity

A

2,535 lbs

89
Q

Max alt for flaps extended

A

20,000’

90
Q

Max speed to open the direct vision window

A

160KIAS

91
Q

Max crosswind takeoff on dry runway

A

38kts

92
Q

Max crosswind takeoff on wet runway

A

31kts

93
Q

Max crosswind takeoff on rwy with compacted snow

A

20kts

94
Q

Max crosswind takeoff on rwy with standing water/slush/wet snow/dry snow

A

18kts

95
Q

Max crosswind takeoff on rwy with ice/wet ice

A

12kts

96
Q

Due to compressor stall possibility, static takeoff is not recommended with crosswinds greater than

A

25kts

97
Q

What fuel weight was used for the fuel capacity info in the CFM

A

6.767 lbs/gal

98
Q

What is the maximum thrust with brakes applied?

A

60% N1

99
Q

What is the N1 limit?

A

99.5%

100
Q

What is the N2 min and max limit?

A

58.5 - 99.4% N2

101
Q

What is the max ITT for TOGA thrust? Is there a time limit?

A

990 deg C limited to 5min
or 10min with one engine inop (we have the Postmod)

can be exceeded up to 1006 deg C during first 2 min

102
Q

Max Continuous Thrust (CON) ITT limit

A

960deg C

(Max Continuous Thrust CON is the highest thrust that does not require maintenance to inspect the engine earlier than planned. It is used in emergency situations and is 12,800lbs. The highest possible thrust is TO-1 RSV or GA RSV, RSV meaning that ATTCS is activated. TO-1 RSV and GA RSV produce 14,200lbs of thrust or 13,000lbs SE)

103
Q

Engine Oil Pressure Min and Max Limits

A

25psi - 95psi

104
Q

Max Continuous (engine) Oil Temperature

A

155deg C

(Max Continuous Thrust CON is the highest thrust that does not require maintenance to inspect the engine earlier than planned. (Up to the red line) It is used in emergency situations and is 12,800lbs. The highest possible thrust is TO-1 RSV or GA RSV, RSV meaning that ATTCS is activated. TO-1 RSV and GA RSV produce 14,200lbs of thrust or 13,000lbs SE)

105
Q

Max Transient Oil Temperature

A

above 155deg C (max continuous) is limited to 15min up to 163deg C (max transient oil temp)

(Max Continuous Thrust CON is the highest thrust that does not require maintenance to inspect the engine earlier than planned. (N1 to the red line) It is used in emergency situations and is 12,800lbs. The highest possible thrust is TO-1 RSV or GA RSV, RSV meaning that ATTCS is activated. TO-1 RSV and GA RSV produce 14,200lbs of thrust or 13,000lbs SE) So Max Transient must be RSV thrust.

106
Q

When must the TO DATSET MENU on the MCDU be set to ENG

A

when OAT is 5-10deg C and there is a possibility of encountering moisture up to 1,700’ AFE or water/snow/ice on airport surfaces

107
Q

When must the TO DATASET MENU on the MCDU be set to ALL?

A

when OAT is below 5deg C and there is a possibility of encountering moisture up to 1,700’ AFE or water/snow/ice on airport surfaces

108
Q

Autopilot minimum use height per AFM

A

50’

109
Q

What flap setting must be used for a CAT II approach?

A

flaps 5

110
Q

What is the demonstrated headwind component for CAT II?

A

25kts

111
Q

What is the demonstrated tailwind component for CAT II?

A

10kts

112
Q

What is the demonstrated crosswind component for CAT II?

A

12kts

113
Q

What kind of FMS do we have?

A

Honeywell Primus Epic II

114
Q

What equipment is required for RVSM operations?

A

1 autopilot, altitude alerting system, 2 transponders (1 must be operational), 2 ADCs (both operational)

115
Q

Aircraft Wingspan

A

93’ 11”

116
Q

Tail Height

A

32’ 4”

117
Q

Aircraft Length

A

103’ 11”

118
Q

Max Ambient Air Temp for Takeoff and Landing

A

52 deg C

119
Q

What is the minimum oxygen required for dispatch? Max, Green, Blue, Amber

A

Max - 1664psi
Green for 3 - 1150psi
Blue for 2 - 842psi
Amber - No Dispatch

120
Q

Fuel Tanks Red

A

660lbs

121
Q

Fuel Tanks Amber

A

1320lbs

122
Q

180 Degree Turn Radius (Wheel to Wingtip)

A

57’ 10”

123
Q

180 Degree Turn Tail Clearance (Wheel to Tail)

A

57’ 3”

124
Q

Pavement Required for 180 Degree Turn (Min Rwy Length)

A

59’ 2”

125
Q

Max Fuel Capacity

A

20,935lbs

126
Q

Useable fuel per side

A

10392.5lbs

127
Q

Unusable Fuel per side

A

75lbs

128
Q

What is max thrust limited to?

A

14,200lbs for SE or 13,000 with both engines

129
Q

LL MRW, MTOW, MLW, MZFW

A

MRW 85,450 (420lbs less)
MTOW 85,098 (419lbs less)
MLW 74,957 (same)
MZFW 69,467 (419lbs less)

130
Q

APU Amber range (no time operating limit in amber in flight or on the ground)

A

662-717deg C

131
Q

5G Limitation - autothrottles

A

For all approaches in VMC or IMC, the Auto -Throttles will be turned off by 500ft AGL

132
Q

5G Abnormal EICAS Messages on Takeoff

A

On takeoff above 80 knots or on landing below 60 knots, messages may appear that are normally inhibited. Some of these messages are related to hydraulic and brakes failure.

If Caution and/or Advisory messages are displayed above 80 KIAS, continue the takeoff, except for ENG 1 (2) FAIL Caution messages up to V1.

133
Q

How could 5G affect TCAS?

A

During normal operation, TCAS will switch to TA only mode below 900ft during descent and 1000ft during climb. This operation could be affected by 5G interference where an RA descent could occur below 900ft.

134
Q

What is the APU oil capacity?

A

4.12 Quarts

135
Q

Maximum Tire Ground Speed

A

195

136
Q

What fuel weight are the fuel limits based on?

A

6.75lbs/gal

137
Q

Max N1 with brakes applied

A

60%

138
Q

Is there a temperature limitation for anti-icing system AUTO operation?

A

No

139
Q

Can the aircraft be operated within the north and south magnetic polar cut-out regions?

A

Yes. The airplanes may be operated within the North and South magnetic polar cut- out regions specified in the “North and South Magnetic Polar Cut-Out Regions” table below, but IRS magnetic Heading and track angle magnetic data will not be available.

Whenever operating within North or South magnetic polar cut-out regions, current airplane Heading must be referenced to true Heading, if not already selected. Otherwise, the Heading Failure Indication flag will be displayed.

See table for latitude longitude coordinates.

This is not the same as maximum latitude for stationary alignment.

140
Q

Minimum Equipment Required for CAT II

A
  1. Two Inertial Reference Systems.
  2. Two Flight Director Systems.
  3. Two Primary Flight Displays (PFD).
  4. Windshield Wipers.
  5. Two VOR/ILS NAV System.
  6. One VHF/COMM System.
  7. Cat II Engagement Logic.
  8. One Radio Altimeter.
  9. One Ground Proximity Warning System (EGPWS).
  10. Two Air Data System (ADS).
  11. One Autopilot System Channel.
  12. Rudder in Normal Mode.
  13. SPOILER FAULT message not presented.
141
Q

What flap setting must be used with CAT II?

A

Flap 5 Only

142
Q

What is the maximum ozone criteria?

A

The Maximum Ozone Criteria is the limiting altitude for every flight and does not depend on flight time.

143
Q

What is the Time weighted average TWA ozone criteria?

A

The Time Weighted Average (TWA) Ozone Criteria tables do not represent the ceiling altitude, but the altitude above which the airplane should not fly for more than three continuous hours (14 CFR 25.832 (a)(2)). This means that the TWA ozone chart shall only be considered if both of the following conditions are met:
a. The airplane is flying in a latitude range at or above the minimum indicated in the table with an actual limitation (not a dash).
b. The flight will be conducted at or above FL270 in that latitude range for three or more hours.

C. If the latitude considered is in between the ones presented in the table, the altitude value may be interpolated. For calculation purposes, the dashes in the table should be considered the maximum altitude presented in the approved operational envelope (FL410).

D. For example, during flight on the west side of the longitude reference line (100°W) at any latitude above 45°N up to 50°N in January, the maximum flight level shall be limited to 407 (Maximum Ozone Criteria), but the airplane shall not be above flight level 338 for more than three hours (TWA Ozone Criteria).

The tables show altitude limitations calculated for constant ozone concentration and cabin stabilized at 8,000 ft. However, ozone tables shall still be considered regardless of the actual cabin altitude attained during a given flight.

144
Q

What types of non-precision approaches does the FMS support?

A

a. GPS only (type III FAA overlay definition);
b. RNAV (including type II or type III FAA overlay definition);
c. VOR; VOR-based Approaches include FAA type II GPS overlays.
d. VOR-DME;

145
Q

What non-precision GPS approach minima are supported by the FMS?

A

LNAV.
LNAV/VNAV.
RNP-APCH.

146
Q

Can pilots conduct RNP AR or RNP RF Legs?

A

Mesa Airlines, Inc. does not have Operations Specifications authorization to conduct RNP AR or RNP RF Legs operations. Flight crews shall not conduct RNP AR operations until Operations Specifications approval is authorized.

147
Q

When must an IRS be operational?

A

Operation above 72° 30.0’ north latitude and below 59° 30.0’ south latitude is prohibited due to unreliable magnetic Heading, unless at least one Inertial Reference System (IRS) is verified operational as a sensor to the FMS. In this case, the system will automatically switch to TRUE.

148
Q

Can FMS Performance Management calculations be used for load planning or airplane range predictions?

A

* FMS performance management calculations have not been certified by the Airworthiness Authority. FMS performance management information is advisory information only, and may not be used as a basis for fuel load planning or airplane range predictions.*

149
Q

What is required when inserting a hold on a waypoint through the FMS?

A

The use of the FMS default option (if presented) is required when inserting a hold on a waypoint.
The selection of a database defined hold option on the FMS select hold page is prohibited.

150
Q

RVSM Tolerances

A

A. Total Vertical Error
Equal to, or greater than, +/- 300 ft. Vertical geometric difference between the actual pressure altitude flown by an aircraft and its assigned pressure altitudes.

B. Altimetry System Error
Equal to, or greater than, +/- 245 ft. Any system which is designed to automatically control the aircraft to a referenced pressure altitude.

C. Assigned Altitude Deviation
Equal to, or greater than, +/- 300 ft. Difference between the transponder Mode C altimeter and the assigned altitude/flight level.

151
Q

RVSM Required Equipment

A

(1) Autopilot - Must be operational
Altitude Alerting System - Must be operational
(2) Altitude Reporting Transponders - One must be operational
(2) Air Data Computers (ADC) - Two must be operational

152
Q

Flaps 1 Pitch

A

11deg

153
Q

Flaps 2 pitch

A

10deg

154
Q

Flaps 4 pitch

A

12deg

155
Q

What is the demonstrated crosswind for takeoff and for landing? Is this considered limiting?

A

The maximum 90° crosswind component for which adequate control of the airplane during Takeoff and Landing was actually demonstrated during certification tests. The maximum demonstrated crosswind component for Takeoff (at 33 ft (10 meters) tower height) is 28 knots and is to be considered limiting. The maximum demonstrated crosswind component for Landing (at 33 ft (10 meters) tower height) is 30 knots and is to be considered limiting.
In high crosswind conditions, rudder effectiveness may be limited after Landing with maximum reverse thrust selected.

156
Q

Per GOM can the takeoff, approach and landing wind components published as demonstrated, recommended or limiting be exceeded?

A

The takeoff, approach and landing wind components published in the appropriate aircraft CFMs and listed as demonstrated, recommended, or limiting will not be exceeded.

157
Q

Do wind gusts affect the crosswind limitations?

A

No

158
Q

APU Max Rotor Speed

A

108%

159
Q

APU EGT for start

A

1032deg C

160
Q

APU EGT for continuous operation

A

717deg C

161
Q

In flight, will the APU shut down if the EGT limit is exceeded?

A

No.

162
Q

Is there a time limitation for operating the APU on the ground or in flight in the amber range between 662deg and 717deg C?

A

No

163
Q

What emergency equipment is located on the flight deck?

A

1 PBE
1 Halon Fire Extinguisher
2 Flashlights
3 Life Vests
3 Oxygen Masks
1 Crash Axe
2 Escape Ropes
1 Thermal Containment Gloves

164
Q

The originating/receiving checklist requires logbook, forms and manuals to be checked. What are you looking for?

A

Name the 15 required manuals and docs

165
Q

What emergency equipment is located in the LR cabin and where are they located?

A

FWD Lav (left):
- Halon Fire Extinguisher (1/5) + 1 on flight deck

FWD FA Station (left):
- Life Vest (1/2)
- Flashlight (1/2)
- MRT Manual Release Tool (1/2)

Wardrobe (right):
- Thermal containment gloves and bag

FWD Galley Bulkhead (right):
- Halon Fire Extinguisher (2/5)
- PBE Portable Breathing Equipment (1/3)
- POB Portable Oxygen Bottle (1/2)
- FAK First Aid Kit (1/2)

Row 1 Overhead Bin (left):
- Demo Equipment
- Seat Belt Extensions
- Extra Passenger Briefing Safety Information Cards

Row 23 Overhead Bin (left):
- Portable ELT

Row 24 Overhead Bin (left):
- AED Automated External Defibrillator
- EEMK Enhanced Emergency Medical Kit
- 8 Infant Life Vests

Doghouse (left):
- Halon Fire Extinguisher (3/5)
- PBE (2/3)
- POB (2/2)
- FAK (2/2)

AFT FA Station (left):
- Life Vest (2/2)
- Flashlight (2/2)
- MRT (2/2)

AFT Lav (left):
- Halon Fire Extinguisher (4/5)

Doghouse (right):
- Halon Fire Extinguisher (5/5)
- PBE (3/3)
- Water Fire Extinguisher
- Megaphone

Behind Galley Carts (right):
- Wheelchair

166
Q

What emergency equipment is in the LL cabin and where is it located? What are the major differences?

A

Major Differences:
- 3 MRT instead of 2
- 3 POB instead of 2
- Life vests under each seat
- AFT wardrobe (right) instead of doghouse (right)
- Row 22 Overhead Bin (right) instead of 23 and 24 (left)
- AFT Additional Jumpseat (right)

FWD Lav (left):
- Halon Fire Extinguisher (1/5) + 1 on flight deck

FWD FA Station (left):
- Life Vest (1/3)
- Flashlight (1/2)
- MRT Manual Release Tool (1/3)

Wardrobe (right):
- Thermal containment gloves and bag

FWD Galley Bulkhead (right):
- Halon Fire Extinguisher (2/5)
- PBE Portable Breathing Equipment (1/3)
- POB Portable Oxygen Bottle (1/3)
- FAK First Aid Kit (1/2)

Row 1 Overhead Bin (left):
- Demo Equipment
- Seat Belt Extensions
- Extra Passenger Briefing Safety Information Cards

Life Vest Under Each Passenger Seat

Doghouse (left):
- Halon Fire Extinguisher (3/5)
- PBE (2/3)
- POB (2/3)
- FAK (2/2)

AFT Lav (left):
- Halon Fire Extinguisher (4/5)

AFT FA Station (left):
- Life Vest (2/3)
- Flashlight (2/2)
- MRT (2/3)

AFT Wardrobe (right):
- Halon Fire Extinguisher (5/5)
- PBE (3/3)
- POB (3/3)

Row 22 Overhead Bin (right):
- Portable ELT
- 8 Infant Life Vests
- EEMK
- AED
- Megaphone

AFT Additional Jumpseat (right):
- Life Vest (3/3)
- Flashlight (2/2)
- MRT (3/3)

Behind Galley Carts (right):
- Wheelchair

167
Q

Turbulent Airspeed Below 10,000’

A

250kts

168
Q

Turbulent Airspeed at or above 10,000’

A

270kts or .76M, whichever is lower

169
Q

Max Range

A

2,000NM

170
Q

Min Airspeed for RAT Operation

A

130kts

171
Q

Certification Category

A

Transport

172
Q

Headsets must be worn below what altitude?

A

FL180

173
Q

Max Ambient Air Temperature for Operation at FL410

A

-21.5deg C

174
Q

Min Ambient Air Temperature for Operation at FL410

A

-65deg C

175
Q

GOM Recommended Max Taxi Speed - Straight, Dry Pavement

A

20kts

176
Q

GOM Recommended Max Taxi Speed - Straight, Wet Pavement

A

10kts

177
Q

GOM Recommended Max Taxi Speed - Turns, Dry Pavement

A

10kts

178
Q

GOM Recommended Max Taxi Speed - Turns, Wet Pavement

A

5kts

179
Q

Max Recommended Crosswind for Landing - Dry

A

38kts

180
Q

Max Recommended Crosswind for Landing - Wet “Good”

A

31kts

181
Q

Max Recommended Crosswind for Landing - Compacted Snow “Good to Medium”

A

20kts

182
Q

Max Recommended Crosswind for Landing - Standing Water / Wet/Dry Snow “Medium”

A

15kts

183
Q

Max Recommended Crosswind for Landing - Water/Slush “Medium to Poor”

A

12kts

184
Q

Max Recommended Crosswind for Landing - Ice “Poor”

A

8kts

185
Q

Max Recommended Crosswind for Landing - “Nil”

A

Not Approved

186
Q

PAX Cabin Door Max Wind Gusts - Partially Open

A

40kts

187
Q

PAX Cabin Door Max Wind Gusts - Open and Locked

A

65kts

188
Q

Cargo Door Max Wind Gusts - Partially Open

A

40kts

189
Q

Cargo Door Max Wind Gusts - Open and Locked

A

60kts

190
Q

Cabin Alt High Warning Occurs When

A

Cabin Alt is 9,700’ or higher
OR
Cabin Alt > 500’ above LFE, for LFE above 9,400’

191
Q

When should the Hot Weather Checklist be used?

A

Above 30deg C or 86deg F

192
Q

AP Coupled Go-Around Height Loss

A

May be 50’

193
Q

Batt 2 Minimum Temperature for APU Start

A

-20deg C

194
Q

VDC Required for APU Start

A

22VDC

195
Q

BATT 1(2) OVERTEMP trigger

A

70deg C for 2 sec

196
Q

VDC Required to Close the battery contactor during APU start

A

18VDC

197
Q

What is required to start the APU below -20deg C or below 22VDC

A

The battery must be charged or the DC GPU can be used.

198
Q

DC GPU Voltage Output Required

A

24-29 VDC

199
Q

IDG HOT Trigger

A

> 168deg C

200
Q

IDG LOP Trigger

A

< 140PSI

201
Q

NiCad Batteries Supply Power for

A

10min

202
Q

TOGA ITT Can be exceeded up to ___deg for ___min

A

1006deg C for 2min

203
Q

ITT Limit for engine start logic

A

120deg C for igniters to come on

204
Q

Hydraulic System Pressure

A

3,000 PSID

205
Q

HYD 1/2/3 HI TEMP Trigger

A

100deg C

206
Q

HYD SOV automatically closes for systems 1 and 2, or for system 3 pumps 3A and 3B turn off at ____deg C

A

125deg C

207
Q

HYD 1/2/3 OVERHEAT Trigger

A

145deg C

E175 Systems (18 decks)

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