Limitations Flashcards

1
Q

Tire speed

A

204 kts

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2
Q

Runway slope

A

+/- 2%

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3
Q

Maximum Takeoff and Landing Tailwind

Component

A

15 knots

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4
Q

Maximum Operating Altitude

A

45,100 feet pressure altitude

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5
Q

Maximum Takeoff and Landing Altitude

A

10,000 feet pressure altitude

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6
Q

Maximum Field Elevation

A

9,500 feet

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7
Q

Maximum speed operating in RVSM airspace

A

0.90 Mach

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8
Q

Ground wind limits for all doors

A
  • 40 knots while opening or closing

* 65 knots while open

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9
Q

Takeoff/Landing Crosswind Guidelines (including peak gust): Good
Dry
Wet

A

Dry 30/30

Wet 25/25

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10
Q

Takeoff/Landing Crosswind Guidelines (including peak gust)

Medium - Poor

A

15/10

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11
Q

Maximum Taxi Weight

A

395.9

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12
Q

Maximum Takeoff Weight

A

394.6

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13
Q

Maximum Landing Weight

A

295.7

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14
Q

Maximum Zero Fuel Weight

A

276.6

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15
Q

Minimum Flight Weight

A

166.6

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16
Q

Maximum differential pressure (relief valves)

A

9.4 psi

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17
Q

Maximum allowable cabin pressure differential for

takeoff and landing

A

0.11 psi

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18
Q

The autopilot must not be engaged below ___ feet after takeoff

A

250

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19
Q

The autopilot must not be engaged below ___ feet during enroute operation.

A

500

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20
Q

The autopilot must be disengaged below ___ feet in a single channel ILS approach

A

150

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21
Q

The autopilot must be disengaged below ___ feet in a non-precision approach.

A

360

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22
Q

Do not use FLCH on final approach below ___ feet airport field elevation

A

1,000

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23
Q

Autoland - Flaps

A

25 or 30 only

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24
Q

Autoland - Glideslope Angle

A

Maximum 3.25º

Minimum 2.5º

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25
Automatic landings require _ operating hydraulic systems
4
26
Autoland - Maximum Wind Component Headwind Tailwind Crosswind
25 knots 15 knots 25 knots
27
Do not operate HF radios during ___
refueling operations
28
Do not operate the weather radar (3)
in a hangar within 50 feet of any personnel within 50 feet of a fuel spill
29
Remove any power cords from all flight deck PC power outlets before ____
using a hand microphone
30
Desired Oxygen Pressures - Crew/Pass system
1,200/1,200
31
Personnel entering main cargo deck during flight ____
will carry a portable oxygen bottle
32
The smoke barrier door must be closed during ____
taxi, takeoff, flight and landing
33
EGT Limits - Starting Takeoff Continuous
750 (870 - 40 sec) 960 (5 min) 925
34
Minimum Oil Pressure
10 psi
35
Max Oil Temperature - Continuous Transient (15 min)
160º C | 175º C
36
Continuous ignition must be ON encountering: (5)
* heavy rain * severe turbulence * volcanic ash * icing conditions * standing water or slush on runway
37
``` APU Limits - Between starts wait: 1 and 2 __ min 2 and 3 __ min 3 and 4 __ min ```
Between battery starts wait: 1 minute 1 minute 75 minutes
38
The maximum altitude with flaps extended is ______ feet
20,000
39
Flight Maneuvering Load Acceleration Limits - Flaps Up Flaps Down
+2.5g to -1.0g | +2.0g to 0.0g
40
Use of speed brakes in flight with flaps extended past __ is not recommended
20
41
From engine start until shutdown at the completion of flight, _______ are the primary means of alerting the flight crews to non-normal conditions or improper configuration
EICAS Alert messages (Warning, Caution, Advisory)
42
Maximum speed in RVSM Airspace
0.90 Mach
43
The maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operations is ______
200 feet
44
The maximum allowable on-the-ground altitude display difference for RVSM between Captain and First Officer -
SL to 5,000 ft - 35 feet | 10,000 ft - 40 feet
45
The maximum allowable on-the-ground altitude display difference for RVSM operations between CA/FO and Field Elevation -
75 feet
46
IFR approach procedures using VNAV to a DA(H) are not authorized if the path angle is less than ____ or more than ____ degrees
2. 75 | 3. 50
47
Do not extend or retract the flaps between positions __ and __ during fuel jettison
1 and 5
48
The use of ___ and ___ fuels are prohibited
Jet B and JP4
49
In-flight tank fuel temperature must be maintained at least ___ above the fuel freezing point of the fuel being used
3° C
50
Jet A Freeze Point -
- 40 C
51
Jet A1 Freeze Point -
-47 C
52
Nacelle anti-ice must be ON during all ground and flight operations when icing conditions exist or are anticipated, except when the temperature is below ____
-40°C OAT
53
Icing conditions exist when the OAT on the ground or TAT in-flight, is (4)
10°C or below, and; * visible moisture in any form is present * When operating on ramps, taxiways or runways with snow, ice, standing water or slush * When the difference between the temperature and dew point is less than 3°C
54
Do not use anti-ice if OAT or TAT exceeds ____
10°C
55
Ice crystal conditions exist when in visible moisture and one or more of the following indications are present: (4)
* Amber or red weather radar returns below the airplane. * Appearance of liquid water on the windshield at temperatures too cold for rain (the sound is different than rain). * The autothrottle is unable to maintain the selected airspeed. * TAT indication on EICAS remains near 0°C.
56
TAT should normally increase approximately __°C per ___ feet of descent
2°C per 1,000 feet
57
``` Flap Placard Speed (VFE) 1 5 10 20 25 30 ```
``` 1 - 280 5 -260 10 - 240 20 -230 25 -205 30 -180 ```
58
Landing Gear Operating Speeds: Retract or Extend (VLO/MLO) - Extended (VLE/MLE) -
270/0.82 | 320/0.82
59
The total number of persons carried, including crew, shall not exceed __
10
60
Access to the cargo compartment during ___, ___, ___, and ___ is prohibited
Taxi, Takeoff, Flight, and Landing
61
Mode 4 of the GPWS must be determined to be operational before takeoff by verifying that a ____ status message is not displayed on EICAS before engine start, and a ____ advisory message is not displayed on EICAS after engine start and before takeoff
GND PROX SYS | GND PROX SYS
62
Above _______ full maneuver capability is not attained until reaching __________
309,000 kgs VREF 30 + 100 knots.