Global Limitations Flashcards
MAXIMUM WEIGHTS
Taxi and Ramp Weight………………………………………………. ?
Takeoff Weight………………………………………………………….. ?
Landing Weight………………………………………………………… ?
Zero Fuel Weight………………………………………………………. ?
Taxi and Ramp Weight………………………………….. 96,250 lb.
Takeoff Weight……………………………………………… 96,000 lb.
Landing Weight……………………………………………. 78,600 lb.
Zero Fuel Weight………………………………………….. 56,000 lb.
TAKEOFF ON RUNWAYS
NEAR BODIES OF WATER
For takeoff at weights above the maximum landing weight,
OUTFLOW VLV 2 must be closed and one air-conditioning
pack must be shutdown for takeoff.
LANDING ON RUNWAYS
NEAR BODIES OF WATER
LANDING ON RUNWAYS
NEAR BODIES OF WATER
For forced/emergency landing at weights above the maximum
landing weight, OUTFLOW VLV 2 must be closed and
one air-conditioning pack must be shutdown for landing.
MENU
MAXIMUM AIRPORT PRESSURE ALTITUDE Maximum Airport Pressure Altitude for Takeoff and Landing......................................... ? MENU
Maximum Airport Pressure
Altitude for Takeoff and Landing……………………… 10,000 ft.
MAXIMUM AIRPORT
PRESSURE ALTITUDE
Maximum airport pressure altitude for takeoff and landing
with Supplement 20 ____________________________ .
MENU
Maximum airport pressure altitude for takeoff and landing
with Supplement 20 13,700 feet Pressure Altitude.
MAXIMUM OPERATING ALTITUDE
51,000 ft.
MAXIMUM AMBIENT
AIR TEMPERATURE
Maximum Ambient Air Temperature
Approved for Takeoff and Landing……………………………….. ?
+50°C (122°F)
MINIMUM AMBIENT
AIR TEMPERATURE
Minimum Ambient Air Temperature
Approved for Takeoff………………………………………………….. ?
–40°C (–40°F)
COWL ANTI-ICE SYSTEM
Takeoff:
During takeoff, use of cowl anti-ice in ______ mode is
prohibited.
Takeoff:
During takeoff, use of cowl anti-ice in AUTO mode is
prohibited.
COWL ANTI-ICE SYSTEM
Ground Operations:
The cowl anti-ice system must be ON when the OAT is
________ or below and visible moisture in any form is present
(such as fog with a visibility of 1,500 meters (one mile) or
less, rain, snow, and ice crystals).
Ground Operations:
The cowl anti-ice system must be ON when the OAT is
10°C (50°F) or below and visible moisture in any form is
present (such as fog with a visibility of 1,500 meters (one
mile) or less, rain, snow, and ice crystals).
COWL ANTI-ICE SYSTEM
Ground Operations:
The cowl anti-ice must also be ON when the OAT is
________ or below when operating on runways, ramps,
or taxiways where surface snow, ice, standing water, or slush
is present.
Ground Operations:
The cowl anti-ice must also be ON when the OAT is
10°C (50°F) or below when operating on runways, ramps,
or taxiways where surface snow, ice, standing water, or
slush is present.
COWL ANTI-ICE SYSTEM
Flight Operations:
The engine cowl anti-ice system must be ON, when in ____
________ , or when ____ is annunciated by the ice detection
system.
Flight Operations:
The engine cowl anti-ice system must be ON, when in icing
conditions, or when ICE is annunciated by the ice detection
system.
NOTE
Icing conditions exist in flight at a TAT of 10°C (50°F)
or below, and visible moisture in any form is encountered
(such as clouds, rain, snow, sleet, or ice crystals),
except when the SAT is –40°C (–40°F) or below.
WING ANTI-ICE SYSTEM
Takeoff:
During takeoff, use of the wing anti-ice system in ______
is prohibited.
Takeoff:
During takeoff, use of the wing anti-ice system in AUTO
is prohibited.
WING ANTI-ICE SYSTEM
Takeoff:
The wing anti-ice system must also be ON for takeoff when
the OAT is ________ or below and the runway is contaminated
with surface snow, slush, or standing water.
Takeoff:
The wing anti-ice system must also be ON for takeoff when
the OAT is 5°C (41°F) or below and the runway is contaminated
with surface snow, slush, or standing water.
WING ANTI-ICE SYSTEM
Ground Operations:
The wing anti-ice system must be ON for takeoff when the
OAT is ________ or below and visible moisture in any form
is present (such as fog with visibility of 1,500 meters (one
mile) or less, rain, snow, sleet, and ice crystals).
Ground Operations:
The wing anti-ice system must be ON for takeoff when the
OAT is 5°C (41°F) or below and visible moisture in any form
is present (such as fog with visibility of 1,500 meters (one
mile) or less, rain, snow, sleet, and ice crystals).
WING ANTI-ICE SYSTEM
Flight Operations:
The wing anti-ice system must be ON, when in _____
_________ , or when ____ is annunciated by the ice
detection system.
Flight Operations:
The wing anti-ice system must be ON, when in icing
conditions, or when ICE is annunciated by the ice
detection system.
WING ANTI-ICE SYSTEM
Flight Operations:
Do not hold in icing conditions with the _____________.
Flight Operations:
Do not hold in icing conditions with the slats extended.
WING ANTI-ICE SYSTEM
Flight Operations:
When in icing conditions, maintain a minimum engine
speed of _________.
Flight Operations:
When in icing conditions, maintain a minimum engine
speed of 76% N2.
NOTE
Icing conditions exist in flight at a TAT of 10°C (50°F)
or below, and visible moisture in any form is encountered
(such as clouds, rain, snow, sleet, or ice crystals),
except when the SAT is –40°C (–40°F) or below.
TAKEOFF LIMITATIONS
Maximum Runway Slopes
Approved for Takeoff and Landing…………………………………. ?
Maximum Tailwind Component
Approved for Takeoff and Landing…………………………………. ?
Maximum Runway Slopes
Approved for Takeoff and Landing…………………. +2% (uphill)
–2% (downhill)
Maximum Tailwind Component
Approved for Takeoff and Landing………………………10 knots
COLD WEATHER OPERATIONS
Minimum Ambient Temperature
Approved for Takeoff………………………………………………….. ?
−40°C (−40°F)
COLD WEATHER OPERATIONS
For Takeoff and landing operations below ____________
refer to FCOM Volume 1, Chapter 7 SUPPLEMENTARY
PROCEDURES—Cold Weather Operations, Cold Soak
Limitations.
0°C (32°F)
WARM WEATHER OPERATIONS
Ground operation of the Display Units with flight compartment
temperatures in excess of _______________, for greater
than ___ minutes, is prohibited.
Ground operation of the Display Units with flight compartment
temperatures in excess of 40°C (104°F), for greater
than 30 minutes, is prohibited.
APPROACH
Flying an approach with a published glidepath angle of
___________________ is prohibited.
Flying an approach with a published glidepath angle of
4.5 degrees or greater is prohibited.
APPROACH
Approaches with published glidepath angles greater than
_________ must be flown in accordance with Supplement 29,
Approaches With Published Glidepath Angles Greater Than
3.5 Degrees.
3.5 degrees
ENGINE OPERATING LIMITS
TAKEOFF THRUST LIMITATIONS
5 minutes with all engines operating.
10 minutes in the event of an engine failure.
ENGINE OPERATING LIMITS
Static ground operation in the range of ____% to ____% N1
is prohibited.
66% to 80% N1
ENGINE OPERATING LIMITS
Maximum Wind Speed and Direction:
Engine starts are not permitted when tailwinds component
exceeds ___ knots.
20 knots
ENGINE OPERATING LIMITS
Maximum Wind Speed and Direction:
Anytime there is an external or EICAS indication of N1
rotation due to tailwinds, the engine must be cranked for
___ seconds and must be followed immediately by an
AUTO start.
30 seconds
ENGINE OPERATING LIMITS
Maximum Wind Speed and Direction:
When the takeoff crosswind component exceeds ___ knots,
do not exceed _______ below ___ KIAS.
Maximum Wind Speed and Direction:
When the takeoff crosswind component exceeds 20 knots,
do not exceed 66% N1 below 30 KIAS.
STARTER CRANKING LIMITS
(GROUND AND AIR)
The starter must not be used if indicated rpm exceeds
________.
The starter must not be used if indicated rpm exceeds
42% N2.
ENGINE START
START CYCLE
Normal Engine Start:
__ consecutive engine start cycles of __ minutes each with
__ seconds cooling between cycles.
After __ attempts, a __ minute cooling period is required.
Normal Engine Start:
3 consecutive engine start cycles of 3 minutes each with
15 seconds cooling between cycles.
After 3 attempts, a 15 minute cooling period is required.
