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777 Atlas Air > Limitations > Flashcards

Limitations Flashcards

1
Q

Flaps will not extend under following conditions

A
  1. 20,000ft or higher
  2. 275Kts or higher
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2
Q

Flap1 speed

A

265kts

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3
Q

Flap5 speed

A

245kts

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4
Q

Flap15 speed

A

230kts

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5
Q

Flap20

A

225kts

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6
Q

Flap25

A

200kts

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7
Q

Flap30

A

180kts

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8
Q

APU max altitude electrical and bleed air output

A

Electrical - 43,100ft (Priority)
Bleed Air - 22,000ft

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9
Q

Cabin ALT at max service altitude

A

8,000ft cabin @ 43,100ft altitude

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10
Q

Max Taxi Weight

A

N714SA, N777SA, N707GT-N710GT (+363kg)
= 348,721kg

N702GT-N704GT, N760GT, N774SA-N775SA
= 348,358kg

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11
Q

Max Takeoff Weight

A

N714SA, N777SA, N707GT-N710GT (+363kg)
= 347,814kg

N702GT-N704GT, N760GT, N774SA-N775SA
= 347,451kg

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12
Q

Max Operating Altitude

A

43,100ft

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13
Q

Runway slope

A

+/- 2%

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14
Q

Max Landing Weight (all)

A

260,815kg

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15
Q

Max Zero Fuel Weight (all)

A

248,115kg

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16
Q

External door wind limitations

A
  1. Do not operate in winds greater than 40kts
  2. Do not leave open in winds greater than 65kts

*Strong winds can cause structural damage.

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17
Q

ADIRU alignment time

A

Average 10 minutes.
6 minutes at the equator and 15minutes and furthest latitudes.

Shorter time closer to the equator.

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18
Q

Taxi and power setting limitations with high winds

A
  1. TW/XW 30-45kts max 70% N1
  2. TW/XW >45kts no more than normal N1 for taxi
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19
Q

Auto Land XW for CATII/CATIII

A

15kts

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20
Q

Auto Land XW CATI

21
Q

Auto Land wind limitations ALL (HW,XW, XW CATII+,TW)

A

25kts
25kts
15kts
10kts

22
Q

Max altitude with flaps extended

23
Q

Unauthorized approaches

A

FAA - RNP
ICAO - AR

24
Q

Max takeoff and landing tailwind

25
Max Turbulence penetration speed <25,000ft
270kts
26
Max Turbulence penetration speed >25,000ft
280kts or 0.82m which ever is lower. *when operating <.82m maintain 15kts above min maneuver speed
27
wx Radar limitations
1. Avoid use in hanger 2. Avoid use with persons inside the area normally contained by the radome
28
HF radio limitation
Do not use during fueling operations
29
If center tank contains fuel, main tanks must be loaded to____________
Full main tanks. *If center tank is 1360kg, less than full mains provided 1. Center tank plus actual ZFW is less than MZFW 2. CoG limits are observed
30
Minimum autopilot engagement height
200ft
31
LAND 2 or LAND 3 allowable flaps
Flaps20 or Flaps30
32
Max fuel temperature
49 degrees
33
Minimum fuel temperature for takeoff
1. 40 degrees 2. 3 degrees above the freezing point of the fuel used
34
Minimum fuel temperature for fuel in flight
3 degrees above the freezing point of the fuel used
35
Reverse thrust limitations
1. Intentional selection in flight is prohibited 2. Backing of the airplane is prohibited
36
Auto Land maximum and minimum glide slope angle
Max - 3.25 degrees Min - 2.5 degrees
37
__________ and __________ control inputs are to be avoided inflight. Especially in combination of pitch, roll or yaw even at speed below Va.
Large, Alternating.
38
Maximum cabin differential
9.1dpsi
39
ADIRU latitudes of operation
North 82 degrees South 82 degrees
40
APU starter cycle limits electric and air turbine
1. 3x starts in 60 minutes 2. 60 second wait between starts 1-3
41
Wingspan
212'7"
42
Overall length
209'1"
43
Height
62'4"
44
Minimum pavement for 180 degree turn
157'4"
45
Minimum altitude for FLCH use
1000ft Above field elevation
46
RVSM altimeter tolerance on ground and in flight
Ground - 75ft In flight - 200ft
47
Max demo crosswind
38kts
48
Maximum takeoff and landing altitudes all tails
N704GT 8400ft pressure height Remainder of fleet 9800ft pressure height or field elevation 9650ft

777 Atlas Air (16 decks)

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