Limitations Flashcards
Runway Slope Limits
+/-2%
Maximum Tailwind
15kts
Maximum demonstrated Crosswind
36kts without winglets
33 with winglets
Maximum Speed (Vmo / Mmo)
320kts / 0.82M
Turbulent air penetration speed
280kts / 0.76M
250kts when bellow 15,000ft and bellow MLW
Maximum altitude
41,000ft
Maximum Takeoff and Landing altitude
8,400ft
or
12,000ft with high altitude option
Maximum ramp weight
156,000lbs
or
174,700 lbs with IGW Option
Maximum Takeoff weight
155,500 lbs
or
174,200 with IGW option
Maximum Landing weight
144,000 lbs
Maximum Zero fuel weight
136,000 lbs
Maximum cabin differential pressure
9.1 psi
Maximum Altitude for APU Bleed and Electrical use
10,000ft
*Under Captain’s emergency authority, APU has demonstrated the capacity to supply both bleed air and electrical power up to 20,000ft
Maximum Altitude for APU bleed only use
17,000ft
Maximum Altitude for APU Bleed and Electrical use on the ground
15,000ft
Maximum Altitude for APU Electrical use only
41,000ft
Minimum Altitude for Autopilot use after Takeoff
400ft AGL
Minimum altitude for Autopilot “ON” during Non-precision Approach
50ft below minimums
Maximum engine limits
Redline
Minimum engine limits
Redline
Engine Caution limits
Amber
Engine ignition must be on for
Takeoff
Landing
Heavy rain
Anti-ice
Maximum FLAPS Extention Altitude
20,000ft
Minimum altitude for speed brake use
1000ft
Alternate FLAP Duty cycle (down and back up)
0 - 15 - 0 = 5 min
> 15 = 25 min
Fuel system minimum Temperatures
- 43°C or 3°C above fuel freezing
wichever is warmer
Fuel system Maximum Temperatures
49°C
Random fuel imbalance
1000 lbs for Taxi, Takeoff and Landing
Icing condition Temperature
10°C / 50°F or below
Flight deck door operational check must be checked
Once a day
Escape slide retention bar
Must be installed for Taxi, Takeoff and Landing
Standby altimeter for RVSM Accuracy
Does not meet accuracy requirements for RVSM
Maximum altitude difference between Captain’s and FO’s altimeters for RVSM use while in flight
200 ft
Maximum altitude difference between Captain’s and FO’s altimeters for RVSM use while on the ground
Airport elevation Sea level to 5000ft = 50 ft
5001 ft to 10,000 ft = 60 ft
Maximum altitude difference between Captain’s and FO’s altimeters to airport field elevation while on the ground
75 ft
With engine bleed ON do not run A/C Packs in _____ for Takeoff, Approach and Landing.
High
Note:
Except for NNP (cargo fire, smoke removal) Checklist has priority.
Autopilot Single channel Approach minimum disengagement altitude
50 ft
RA 100 ft for aiports above 8,400 ft on airplanes with HIGH altitude option
Maximum allowable wind components for Autoland Operations
Headwind:
Crosswind:
Tailwind:
25 kts
20 kts
15 kts
Maximum allowable wind components for Autoland Operations (CAT IIIB)
Crosswind:
Tailwind:
25 kts
10 kts
Maximum and Minimum Glideslop angles for Autoland
3.25° and 2.5°
Single engine CAT IIIB Autoland Operations
FLAPS 30 and only for DH at or above 50 ft AGL
Maximum pressure altitude for use of Autoland
8,400 ft
APU Bleed valve must be closed when
Ground air is connected and Isolation Valve is open
Eng 1 Bleed valve is open
Isolation valve and Eng 2 bleed valve are open
APU bleed valve may be open during engine start BUT….
Avoid power settings above idle
Maximum speed for use of Speed Brakes
300 kts
Weather radar limitations
Do not operate in a hangar, 50ft from Personnel and fuel spills.
(Doesn’t apply for TEST mode)
