Limitations Flashcards
Limitations
RVSM
Prior to takeoff, what is the maximum allowable difference between CPT’s or F/O’s altitude display and field elevation ?
75 feet
Limitations
RVSM
Does the standby altimeter meet RVSM altimeter accuracy requirements ?
NO ➞ Do not fly in RVSM airspace on ISFD alone.
Limitations
RVSM
ARE RVSM operations allowed when conducting landing gear extended operations ?
NO.
RVSM operations are prohibited when conducting landing gear extended operations.
Limitations
NON-ETOPS Flights
Non-ETOPS area is defined by the maximum distance from an adequate airport flown at the N-1 cruise speed for how long ?
60 minutes
Limitations
NON-ETOPS Flights
Non-ETOPS area is defined by the maximum distance from an adequate airport flown in 60 mn at the N-1 cruise speed.
What distance does that represent ?
420 NM
Limitations
MTAW
Maximum Taxi Weight ?
253 558 Kg
Limitations
MTOW
Maximum Takeoff Weight ?
252 650 Kg
Limitations
MLW
Maximum Landing Weight ?
192 776 kg
Limitations
MZFW
Maximum Zero Fuel Weight ?
181 436 Kg
Limitations
O₂
Below which pressure does the EICAS advisory message CREW OXYGEN LOW display ?
Below 500 PSI
Only 15 minutes breathing protection for 2 crew members left
Limitations
O₂
What breathing protection is left when the EICAS advisory message CREW OXYGEN LOW is displayed ?
15 minutes breathing protection for 2 crew members.
Message is displayed below 500 PSI
Limitations
Autoflight
Lowest altitude for autopilot engagement after takeoff ?
200 feet AGL
Limitations
Autoflight
How low can the autopilot stay engaged without LAND 2 or LAND 3 annunciated ?
135 feet AGL
Limitations
Autoflight
# With LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25 °, when must the autopilot be disengaged ?
below 100 feet AGL
Limitations
Autoflight
If the glide path angle for approach is greater than 3.77 °,
when must the autopilot be disengaged ?
no later than 50 feet below the DA(H)/MDA
Limitations Low Visibility (HUD) Takeoff
Maximum Headwind component ?
25 kt
Limitations Low Visibility (HUD) Takeoff
Maximum Crosswind component ?
20 kt
Limitations Low Visibility (HUD) Takeoff
Maximum Tailwind component ?
15 kt
Limitations
Automatic Landing
Maximum Headwind component ?
25 kt
Limitations
Automatic Landing
Maximum Crosswind component ?
25 kt
Limitations
Automatic Landing
Maximum Tailwind component ?
15 kt
Limitations
Automatic Landing
Maximum glideslope angle ?
3.25 °
Limitations
Automatic Landing
Minimum glideslope angle ?
2.5°
Limitations
Automatic Landing
Maximum field elevation for Autoland ?
8400 feet
Limitations
Max Runway slope ?
+/- 2 %
Limitations
Maximum Takeoff and Landing Tailwind Component ?
15 knots
Limitations
Maximum Operating Altitude ?
43 100 ft pressure altitude
Limitations
Maximum Takeoff and Landing Altitude ?
14 000 ft pressure altitude
Limitations
Turbulent Air Penetration Speed ?
290 KIAS < 25 000 feet ≤ 310 KIAS / .84 Mach (whichever is lower)
Limitations
O₂
Required minimum pressure (PSI) for dispatch from CDG ?
1000 PSI at 21°C (FWD Cargo temperature).
Varies with temperature.
Limitations
Lowest Oil temperature for Engine start ?
- 40 °C
Limitations
Engine Oil Quantity
Lowest Oil quantity (liters) ?
12 liters
If the indicated oil level is 12 L or less, the engine oil tank must be filled.
Limitation
Engine Oil Quantity
Which quantity should the EICAS display when the oil tank is full ?
20 L or more
Limitations
Integrated Approach Navigation (IAN)
Is IAN authorized on RNP AR approaches ?
NO
Limitations
Integrated Approach Navigation (IAN)
Is IAN authorized on NON straight-in approaches ?
NO
A NON straight-in approach = final approach course > 30° from the runway centerline
Limitations
Integrated Approach Navigation (IAN)
Is IAN authorized on approaches with published glide path > 3.77° ?
NO
Limitations
Audio Control Panel (ACP)
Can the CPT’s or F/O’s ACP be used to establish a SATCOM/cabin conference ?
NO, it is prohibited.
Limitations
Can reverse thrust be used to back up the aircraft?
NO, backing the airplane with use of reverse thrust is prohibited.
Limitations
What is the max thrust setting for a standing takeoff prior to brake release ?
55% N1
Limitations
Minimum time for the engine to be run at idle or taxiing power prior to takeoff ?
3 minutes
Limitations
Ground wind operating envelope
Max N1 for crosswinds greater than 40 knots ?
Setting normally used for taxi : 45% N1
Limitations
Ground wind operating envelope
Max N1 thrust for tailwind component > 5 knots and winds > 35 knots ?
Setting normally used for taxi : 45% N1
Limitations
Ground wind operating envelope
Max N1 thrust for winds greater than 55 knots ?
IDLE
Limitations
Maximum altitude with flaps extended ?
20,000 feet
Limitations
Maximum tank fuel temperature at takeoff for Jet A, Jet A-1, JP-5, JP-8 or TS-1 ?
49°C (120°F)
Limitations
Max Inflight fuel temperature for Jet A, Jet A-1, JP-5 or JP-8 ?
65°C (150°F)
Limitations
Minimum tank fuel temperature prior to takeoff ?
-29°C (-20°F)
Limitations
What is the margin from freezing temperature that the fuel has to be maintained at?
3°C
In-flight tank fuel temperature must be maintained at least 3° C above the freezing point of the fuel being used. The use of Fuel System Icing Inhibitor additives does not change the minimum fuel tank temperature limit
Limitations
Fuel Loading
Limitation on Main tanks if center tank is used ?
Main tanks must be scheduled to be full if center tank fuel is loaded.
Note:
The center tank may contain up to 10 T of fuel with less than full main tanks provided center tank fuel weight plus actual zero fuel weight does not exceed the maximum zero fuel weight (181,4 T), and CG limits are observed.
Limitations
Can HF radios be operated while refueling ?
NO
Operational limitation
Limitations
What are the limitations for weather radar operation on the ground ?
- not in a hangar
- not within 50 feet of fueling operations or a fuel spill.
Limitations
Can FLCH be used below 1000 ft on final approach ?
NO
Limitations
Can reverse thrust be used in flight ?
NO, intentional selection of reverse thrust in flight is prohibited.
Limitations
Can rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g. large side slip angles) be done ?
No, it SHOULD be avoided.
Duh !
