Limitations Flashcards
Kind of operations
‐ VFR and IFR ‐
Extended overwater flight ‐
Flight in icing conditions
FLIGHT MANEUVERING LOAD ACCELERATION LIMITS
Clean configuration –1 g to +2.5 g
Other configurations 0 g to +2 g
WEIGHT LIMITATIONS
A4O-DA, A4O-DC, A4O-DF, A4O-DG
Max taxi weight. 233900kg Max takeoff weight. 233000kg Max landing weight. 182000kg Max zero fuel weight 170000kg Min weight 116000kg
Weight limitations
A4O-DB, A4O-DD, A4O-DE
Max taxi weight. 233900 Max takeoff weight. 233000kg Max landing weight. 187000kg Max zero fuel weight 175000kg Min weight 121000kg
Weight limitations
A4O-DH, A4O-DI, A4O-DJ
Max taxi weight. 235900 Max takeoff weight. 235000kg Max landing weight. 187000kg Max zero fuel weight 173000kg Min weight 121000kg
Runway slope
+-2%
Runway altitude
12500ft
Max certified crosswind for takeoff
32kt (gust included)
Max tailwind takeoff
A4O-DA, A4O-DB, A4O-DC, A4O-DD, A4O-DE, A4O-DF, A4O-DG
10kts
Autopilot minimum engagement height
100 ft AGL or 5 s after liftoff.
In approach using F-LOC , F-G/S
200ft AGL
Autopilot cat 1
160fr AGL
Autopilot GLS
160ft AGL
Autopilot after a go around
100ft
Maximum wind for auto land cat II and III
Headwind: 35 kt Tailwind : 10 kt Crosswind: 20 kt
Auto land glide slope
-2.5 ° and -3.25 °
For airfield elevation below 9200ft
Weight limitations autoland
- For weights below maximum landing weight
- For weights above 116 000 kg (255 737 lb)
Nominal Runway Width
45 m
Max tailwind takeoff
A4O-DH, A4O-DI, A4O-DJ
15kts
Max crosswind for landing
A4O-DA, A4O-DC, A4O-DF, A4O-DG
45kts
Max crosswind for landing
A4O-DB, A4O-DD, A4O-DE, A4O-DH, A4O-DI, A4O-DJ
40kts
Max tailwind landing
10kts
The maximum wind for passenger door operation
40 kt or 50 kt if the aircraft nose is into the wind
Takeoff is not recommended on the following runway conditions
‐ Wet ice,
‐ Water on top of Compacted Snow,
‐ Dry Snow or Wet Snow over Ice.
COCKPIT WINDOW OPEN MAXIMUM SPEED
230 kt
Max VMO/MMO
330kts/ m0.86
Maximum speed with landing gear extended (VLE
250 kt/0.55
Maximum speed with the landing gear operating - extension and retraction (VLO)
250 kt/0.55
Maximum ground speed tire speed
204kts
WIPERS MAXIMUM OPERATING SPEED
230 kt
Maximum positive differential pressure
9.25 PSI
Maximum negative differential pressure
.-0.73 PSI
Safety relief valve setting
8.85 PSI
APU start attempts
After three consecutive APU start attempts, the flight crew must wait 60 min before a new start attempt.
APU max rotor speed
107 %
Maximum EGT for APU start
1 250 °C
Maximum EGT for APU running
650 °C
APU bleed air and elec power
25000ft
APU elec power only
41450 ft
When JET B or JP4 is used, APU operation is limited to
25 000 ft
Maximum N1
Maximum N2
Maximum N3
99 %
103.3 %
100 %
OIL TEMPERATURE Maximum continuous temperature
190 °C
Minimum oil temperature before takeoff
20 °C
Minimum oil pressure
25 PSI
STARTER
‐ Starter maximum continuous operation is 5 min . ‐ Two 3 min duty cycles and a consecutive 1 min cycle is permitted with run down to zero N3 between each cycle. ‐ After one continuous operation, or the three cycles wait 30 min to allow the starter to cool. ‐ No running engagement of the starter when the N3 is above 10 % on ground, or 30 % in flight.
REVERSE THRUST
Maximum reverse should not be used below 70 kt. Idle reverse is permitted down to aircraft stop.
Maximum operating altitude with slats and/or flaps extended
20 000 ft
Minimum fuel quantity for takeof
5 200 kg
Maximum brake temperature for takeoff (brake fans off)
300 °C
If maximum one tire per gear is deflated (consider three gears) Maximum taxi speed during turn
7kts
If two tires are deflated on the same main gear (maximum one main gear) Maximum taxi speed
3 kt
For the nosewheel steering (NWS) angle Maximum NWS angle
30 °
APU bleed and elec
22500ft
APU battery restart limit
25000ft
APU ground operation
14600ft
APU normal start
41450ft
Max fuel temp
55 degrees for jet a1
Starter
‐ Starter maximum continuous operation is 5 min .
‐ Two 3 min duty cycles and a consecutive 1 min cycle is permitted with run down to zero N3 between each cycle.
‐ After one continuous operation, or the three cycles wait 30 min to allow the starter to cool. ‐ No running engagement of the starter when the N3 is above 10 % on ground, or 30 % in flight.
