Limitations Flashcards

(48 cards)

1
Q

The Turbulent Air penetration -400 (Severe Turbulent Air Penetration -8) speed is?

A

-400: 290-310 KIAS / .82-.85 Mach Whatever is lower
-8: 310 KIAS / .83 Mach Whatever is lower

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2
Q

Max Operating Altitude? 400/-8?

A

400: 45100 PA
-8: 43100 PA
LCF: 43100 PA

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3
Q

Max Altitude for T/O and Landing?

A

400: 10000 PA
-8: 10000 PA
LCF: 7300 PA

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4
Q

Maximum Field Elevation?

A

400: 9500 MSL
-8: 9500 MSL
LCF: 7300 MSL

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5
Q

Max T/O and Landing Tailwind component?

A

400: 15
-8: 15
LCF: 10

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6
Q

Max Runway Slope?

A

All: 2%

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7
Q

Max speed in RVSM Airspace?

A

400: 0.9 mach
-8/LCF: NA

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8
Q

Main Deck Cargo Compartment Access; If there is no MAIN DECK SIGNALING/ALERT SYSTEM

A

Supernumeraries are prohibited from accessing the main deck cargo compartment any time the aircraft is moving.

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9
Q

Main Deck Cargo Compartment Access; If there is a MAIN DECK SIGNALING/ALERT SYSTEM

A

WITH Main Deck Signaling/Alert System
(main deck occupancy placard on the smoke barrier door)
Supernumeraries are prohibited from accessing the main deck cargo compartment
during taxi, takeoff, and landing.
A maximum of 3 supernumeraries are allowed access to the main deck cargo
compartment in-flight for cargo or live animal operations.
Supernumeraries must be signaled to return to their seats at the onset of a smoke,
fire, or pressurization event, turbulence, and prior to landing.
There must be at least one portable oxygen unit with a full face mask attached to it
provided for each supernumerary allowed to enter the main deck cargo
compartment during flight.
The supernumeraries must be trained in the use of the oxygen units and making
the determination whether oxygen is being delivered to the dispensing units.
During flight, the supernumerary must carry the portable oxygen unit whenever he
or she is in the main deck cargo compartment.
400F
For aircraft without an automatic aural and visual system installed,
supernumeraries must also don the full-face mask and initiate the oxygen flow
whenever the main deck cargo compartment is accessed during flight. See placard
on the smoke barrier door to determine requirement status.

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10
Q

Max Demonstrated takeoff and landing crosswing?

A

30 kts, not limiting

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11
Q

Do not operate HF radios when?

A

During refueling

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12
Q

Avoid weather radar operation when/where?

A

In a hangar and when people are within the area normally enclosed by the aircraft radome

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13
Q

Without Cabin Crew on board can ACMs and Supernumeraries sit downstairs at all times?

A

No, restricted to the upper deck for taxi, takeoff and landing.

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14
Q

Do the standby Altimeters meet the accuracy requirements for RVSM airspace?

A

No

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15
Q

Max allowable in-flight difference between CA and FO altitude displays for RVSM is what?

A

200 ft

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16
Q

The maximum allowable on-the-ground altitude display differences for RVSM
operations are what?

A

Seal Level to 5000ft: 35 ft between CA and FO, 75 ft between CA/FO and Field elevation
5001-9500ft: 50ft between CA and FO, 75ft between CA/FO and Field elevation.

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17
Q

Target Oxygen Pressures (PSI)

A

Crew system: Land 950, Ocean 1200
Pass system: Land 1200, Ocean 1200

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18
Q

AFM limits weight

A

Max Taxi: 397800* if zfw is above 276691kg max taxi weight is max TO weight + 1360 KG

MAX TO: 396893
MAX landing wieght: 302092
Max ZFW: 288031

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19
Q

Max differential pressure (relief valves)

A

9.4 PSI

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20
Q

Max allowable cabin pressure differential for TO and Landing

21
Q

Air conditioning (A/C) PACKS OFF for takeoff or go-around is (BLANK).
Takeoff and go-around must be performed with at least (BLANK) A/C pack on.

A

not permitted/ 1

22
Q

Nitrogen Generation System (NGS)
400P
If Pack 3 is available, do not move the Pack 3 Control selector to (BLANK) during
normal ground operations unless Pack 1 and Pack 2 selectors are (Blank).

23
Q

Use of aileron trim with the autopilot engaged is?

24
Q

The autopilot must not be engaged below what altitude after takeoff?

25
The autopilot must be disengaged before the airplane descends more than (BLANK) below minimums unless it is coupled to an ILS glideslope and localizer or in the go-around mode.
50ft
26
Without LAND 2 or LAND 3 annunciated, the autopilot must not remain engaged below BLANK feet RA.
100ft
27
Max allowable wind speeds for Autoland
headwind: 25 kts Tailwind: 15 kts // 10kts for LCF Crosswind: 25 kts Crosswind CAT 2/3: 15 kts
28
Min/Max glideslope?
2.5-3.25
29
Auto land landing must be made with what flap settings
25 or 30
30
Do not use FLCH on final approach below BLANK AFE
1000
31
What are the limitations of CNS/RVSM required equipment?
CNS = Communication/navigation/surveillance RVSM = reduced vertical separation minimums. This section in the limitations provides guidance on what is required for these two.
32
Engine Limit Display Markings?
Red = Min/Max limits Caution limits are amber
33
Engine Oil System; PRATT Oil temperature must be greater than BLANK degrees C before advancing thrust levers to takeoff power.
50
34
When must continuous ignition be on?
* heavy rain * severe turbulence * volcanic ash * icing conditions * standing water or slush on runway
35
Intentional selection of reverse thrust in flight is Blank?
Prohibited
36
Backing the airplane with use of reverse thrust is Blank?
Prohibited
37
If engine vibration indications are available and above 4 units, do not Blank? -8
Takeoff
38
Do not operate the APU below Blank feet pressure altitude.
-1000
39
-8: Engines must be shut down when the 90 degree crosswind component exceeds Blank Kts
55
40
APU start cycle restrictions are?
Battery: 1 min / 1 min / 75 mins TR: 1 min / 10 mins / 75 mins
41
Avoid Blank and Blank alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g., large side slip angles) as they may result in structural failure at any speed, including below VA.
Rapid, Large
42
The maximum altitude with flaps extended is?
20,000ft
43
Use of speedbrakes in flight with flaps extended past Blank is not recommended
20
44
QFE operations are prohibited on what sub fleet?
LCF
45
IFR approach procedures using VNAV to a DA(H) are not authorized if the path angle is less than bLANK or more than bLANK degrees.
Less than 2.75 and more than 3.5
46
maximum tank fuel temperature is?
54C
47
What fuel type is prohibited?
Jet B and JP4
48
In-flight tank fuel temperature must be maintained at least BLANK C above the fuel freezing point of the fuel being used
3