Limitations Flashcards

(46 cards)

1
Q

Runway Slope Limits

A

+/-2%

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2
Q

Maximum Tailwind

A

15kts

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3
Q

Maximum demonstrated Crosswind

A

36kts without winglets

33 with winglets

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4
Q

Maximum Speed (Vmo / Mmo)

A

320kts / 0.82M

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5
Q

Turbulent air penetration speed

A

280kts / 0.76M

250kts when bellow 15,000ft and bellow MLW

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6
Q

Maximum altitude

A

41,000ft

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7
Q

Maximum Takeoff and Landing altitude

A

8,400ft
or
12,000ft with high altitude option

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8
Q

Maximum ramp weight

A

156,000lbs
or
174,700 lbs with IGW Option

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9
Q

Maximum Takeoff weight

A

155,500 lbs
or
174,200 with IGW option

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10
Q

Maximum Landing weight

A

144,000 lbs

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11
Q

Maximum Zero fuel weight

A

136,000 lbs

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12
Q

Maximum cabin differential pressure

A

9.1 psi

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13
Q

Maximum Altitude for APU Bleed and Electrical use

A

10,000ft
*Under Captain’s emergency authority, APU has demonstrated the capacity to supply both bleed air and electrical power up to 20,000ft

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14
Q

Maximum Altitude for APU bleed only use

A

17,000ft

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15
Q

Maximum Altitude for APU Bleed and Electrical use on the ground

A

15,000ft

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16
Q

Maximum Altitude for APU Electrical use only

A

41,000ft

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17
Q

Minimum Altitude for Autopilot use after Takeoff

A

400ft AGL

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18
Q

Minimum altitude for Autopilot “ON” during Non-precision Approach

A

50ft below minimums

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19
Q

Maximum engine limits

20
Q

Minimum engine limits

21
Q

Engine Caution limits

22
Q

Engine ignition must be on for

A

Takeoff
Landing
Heavy rain
Anti-ice

23
Q

Maximum FLAPS Extention Altitude

24
Q

Minimum altitude for speed brake use

25
Alternate FLAP Duty cycle (down and back up)
0 - 15 - 0 = 5 min | > 15 = 25 min
26
Fuel system minimum Temperatures
- 43°C or 3°C above fuel freezing | wichever is warmer
27
Fuel system Maximum Temperatures
49°C
28
Random fuel imbalance
1000 lbs for Taxi, Takeoff and Landing
29
Icing condition Temperature
10°C / 50°F or below
30
Flight deck door operational check must be checked
Once a day
31
Escape slide retention bar
Must be installed for Taxi, Takeoff and Landing
32
Standby altimeter for RVSM Accuracy
Does not meet accuracy requirements for RVSM
33
Maximum altitude difference between Captain's and FO's altimeters for RVSM use while in flight
200 ft
34
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
35
Maximum altitude difference between Captain's and FO's altimeters to airport field elevation while on the ground
75 ft
36
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.
37
Autopilot Single channel Approach minimum disengagement altitude
50 ft | RA 100 ft for aiports above 8,400 ft on airplanes with HIGH altitude option
38
Maximum allowable wind components for Autoland Operations Headwind: Crosswind: Tailwind:
25 kts 20 kts 15 kts
39
Maximum allowable wind components for Autoland Operations (CAT IIIB) Crosswind: Tailwind:
25 kts | 10 kts
40
Maximum and Minimum Glideslop angles for Autoland
3.25° and 2.5°
41
Single engine CAT IIIB Autoland Operations
FLAPS 30 and only for DH at or above 50 ft AGL
42
Maximum pressure altitude for use of Autoland
8,400 ft
43
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
44
APU bleed valve may be open during engine start BUT....
Avoid power settings above idle
45
Maximum speed for use of Speed Brakes
300 kts
46
Weather radar limitations
Do not operate in a hangar, 50ft from Personnel and fuel spills. (Doesn't apply for TEST mode)