Limitations Flashcards
Flight maneuvering load acceleration limits
Clean config
-1g to +2.5g
Flight maneuvering load acceleration limits
Other config
0g to +2g
Environmental envelope
Max alt
41450ft
Environmental envelope
Takeoff and landing altitude
-2000 to 8500ft
Environmental envelope
Minimum TAT
-53 degC
Airport operations and wind limitations
Runway slope
+-2%
Airport operations and wind limitations
Runway altitude
8000ft
Airport operations and wind limitations
Nominal runway width
45m
Airpprt operations and wind limitations
Maximum certified crosswind for takeoff
30kt (gust included)
Airport operations and wind limitations
Maximum certified crosswind for landing
35kt (gust included)
Airport operations and wind limitations
Maximum tailwind for takeoff
15kt
Airport operations and wind limitations
Maximum tailwind for landing
15kt
Airport operations and wind limitations
For landing with tailwind greater than __, FLAPS FULL is recommended
10kt
Airport operations and wind limitations
Maximum wind for passenger door operation
40kt (or 50kt if the aircraft nose is into the wind)
Airport operations and wind limitations
Maximum wind for FWD and AFT cargo doors operation
40kt (or 50kt, if the aircraft nose is into the wind)
Airport operations and wind limitations
Passenger and cargo doors must be closed before the wind speed exceeds __
60kt
Runway surface condition: Good
Max crosswind for takeoff
30kt
Runway surface condition: Good
Max crosswind for landing
35kt
Runway surface condition: Good to Medium
Max crosswind for takeoff and landing
27kt
Runway surface condition: Medium
Max crosswind for takeoff and landing
20kt
Runway surface condition: Medium to Poor
Max crosswind for takeoff and landing
20kt
Runway surface condition: Poor
Max crosswind for takeoff and landing
15kt
Airport operations and wind limitations
Max flight path angle during approach
-4deg
Cockpit window open maximum speed
230kt
Maximum flaps/slats speeds
Config 1
240kt
Maximum flaps/slats speeds
Config 1 + f
215kt
Maximum flaps/slats speeds
Config 1*
205kt
Maximum flaps/slats speeds
Config 2
196kt
Maximum flaps/slats speeds
Config 3
186kt
Maximum flaps/slats speeds
Config FULL
180kt
Vmo
330kt
Mmo
0.86 mach
Maximum speed with landing gear extended (Vle)
250kt / 0.55
Maximum speed with the landing gear operating - extension and retraction (Vlo)
250kt / 0.55
Maximum speed for landing gear gravity extension
200kt
Maximum tire speed
204kt
Minimum control speed for landing (Vmcl)
126kt
Vmcg at 0 ft
131kt
Vmca at 0 ft, config 1 + f
128kt
Vmca at 0 ft, config 2
127kt
Vmca at 0 ft, config 3
124kt
Wipers maximum operating speed
230kt
Maximum taxi weight
242 900 kg
Maximum takeoff weight (brake release)
242 000 kg
Maximum landing weight
191 000 kg
Maximum zero fuel weight
From 177 000 kg to 181 000 kg
Maximum zero fuel weight at MTOW 238 000 kg
181 000 kg
Maximum zero fuel weight at MTOW 242 000 kg
177 000 kg
With passengers on board, it is not recommended to exceed __ without air conditioning supply.
20min
Maximum positive differential pressure
9.25psi
Maximum negative differential pressure
-0.73psi
Safety relief valve setting
8.85psi
Max norm cabin alt
8000ft
Outflow valve closure (cabin alt)
15000ft
AP must not be used in approach and autoland with an aft CG at or above __
35% MAC
Autopilot at takeoff
100ft AGL and at least 5 s after liftoff
Autopilot in approach with F-G/S mode
200ft AGL
Autopilot in approach with FINAL APP, V/S, or FPA mode
250ft AGL
Autopilot in circling approach
500ft AGL
Autopilot in ILS approach when CAT1 is diaplayed on the FMA
160ft AGL
Autopilot in ILS approach when CAT2 or CAT3 (single or dual) is displayed on the FMA
0ft AGL if autoland
Autopilot after a manual go-around
100ft AGL
Autopilot in all other phases
500ft AGL
RNP accuracy with GPS PRIMARY
With AP ON
Enroute, terminal, approach
1nm, 0.5nm, 0.3nm
RNP accuracy with GPS PRIMARY
With AP OFF and FD ON
Enroute, terminal, approach
1nm, 0.51nm, 0.3nm
RNP accuracy with GPS PRIMARY
With AP OFF and FD OFF
Enroute, terminal, approach
1.1nm, 0.51nm, 0.3nm
ILS CATEGORY II
Minimum decision height
100ft
ILS CATEGORY III FAIL PASSIVE (SINGLE)
Minimum decision height
50ft
ILS CATEGORY III FAIL OPERATIONAL (DUAL)
Alert height
200ft
CAT III without DH
Minimum runway visual range
75m
Maximum wind conditions for ILS CAT II or CAT III
AEO
Headwind, Tailwind, Crosswind
25kt, 10kt, 20kt
Maximum wind conditions for ILS CAT II or CAT III
OEI
Headwind, tailwind, crosswind
20kt, 10kt, 10kt
Automatic landing is demonstrated:
Glide slope angle between __ and __
-2.5deg and -3.5deg
Automatic landing is demonstrated:
For airfield elevation below __
5750ft
Automatic landing is demonstrated:
For weights above __
140 000 kg
Automatic landing is demonstrated:
With aircraft weight below __
The maximum landing weight
Automatic landing is demonstrated:
Depending on the aircraft situation and provided that the runway is approved for automatic landing, the flight crew can decide to perform an autoland up to __
251T
Autoland must not be used with an aircraft CG forward of __
15% MAC
APU START
After three consecutive APU start attempts, the flight crew must wait __ before a new start attempt
60min
APU max N speed
107%
APU max EGT for APU start
1250degC
APU max EGT for APU running
650degC
APU Battery Restart Limit (elec emer config)
25000ft
APU BLEED
Max altitude to assist engine start
20000ft
APU BLEED
Max altitude for airconditioning and pressurization (single pack operation)
22500ft
APU BLEED
Max altitude for air conditioning and pressurization (dual pack operation)
17500ft
ENG EGT LIMIT
Takeoff and go-around
900degC
ENG EGT LIMIT
MCT
850degC
ENG EGT LIMIT
Starting on ground
700degC
ENG EGT LIMIT
Starting in flight
900degC
ENG max N1
101.5%
ENG max N2
103.5%
ENG max N3
101.5%
ENG max oil temp continuous operation
191degC
ENG max oil temp transient operation (limited to 15 min during takeoff)
196degC
ENG min oil temp for starting
-40degC
ENG min oil temp before takeoff
40degC
ENG oil min quantity
Flight time below 10h
15qt
ENG oil min quantity
ETOPS, or flight time at or above 10h
16qt
ENG oil minimum pressure
30psi
ENG starter
Extended cycle: one continuous operation cycle of __
5mins
ENG starter
Normal cycle: Two consecutive start attempts of __ maximum, plus __ continuous operation
3min, 1min
ENG starter
High tailwinds (higher than __) may have an adverse effect on start. It may be necessary to reposition the airplane into the wind
15kt
ENG starter
No running engagement of the starter when the N3 is above __ on ground, or __ in flight
10%, 30%
FLEX TAKEOFF
TFLEX cannot be higher than TMAXFLEX, equal to ISA + __
60degC
ENG crosswind limit for landing
35kt (gust included)
Maximum altitude flaps/slats extended
20000ft
Maximum fuel temperature
55degC
Minimum fuel temperature
The highest of freezing point or __ below 30000ft or __ above 30000ft, in inner tank
-44degC, -54degC
Maximum allowed fuel imbalance
Inner tanks (outer balanced)
Heavier tank full
2900kg
Maximum allowed fuel imbalance
Inner tanks (outer balanced)
Heavier tank 17000kg
4800kg
Maximum allowed fuel imbalance
Inner tanks (outer balanced)
Heavier tank 7500kg
7500kg
Maximum allowed fuel imbalance
Outer tanks (inner balanced)
Heavier tank full
1480kg
Maximum allowed fuel imbalance
Outer tanks (inner balanced)
Heavier tank 2400kg
1580kg
Maximum allowed fuel imbalance
Outer tanks (inner balanced)
Heavier tank 1730kg
1730kg
Minimum fuel quantity for takeoff
5200kg
Severe ice accretion on airframe, thickness
5mm (0.2in) or more
Maximum brake temperature for takeoff (brake fans off)
300degC
NWS limit angle
72deg
Taxi with deflated or damaged tires
Maximum one tire per gear is deflated (consider three gears)
Max taxi speed
7kt
Taxi with deflated or damaged tires
Two tires are deflated on the same main gear (maximum one main gear)
Max taxi speed, max nws angle
3kt, 30deg
Ground alignment of the IRS is possible in lattitudes between __ North and __ South
82deg, 82deg
Minimum flight crew oxygen pressure
30deg, CAPT or FO
540psi
Minimum flight crew oxygen pressure
30deg, 3rd or 4th occupant
750psi
The predictive GPWS functions should be inhibited when the aircraft position is less than __ from the airfield
15nm
