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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

A

25kts

21
Q

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

A

25kts
25kts
15kts
10kts

22
Q

Max altitude with flaps extended

A

20,000ft

23
Q

Unauthorized approaches

A

FAA - RNP
ICAO - AR

24
Q

Max takeoff and landing tailwind

A

10kts

25
Q

Max Turbulence penetration speed <25,000ft

A

270kts

26
Q

Max Turbulence penetration speed >25,000ft

A

280kts or 0.82m which ever is lower.

*when operating <.82m maintain 15kts above min maneuver speed

27
Q

wx Radar limitations

A
  1. Avoid use in hanger
  2. Avoid use with persons inside the area normally contained by the radome
28
Q

HF radio limitation

A

Do not use during fueling operations

29
Q

If center tank contains fuel, main tanks must be loaded to____________

A

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
Q

Minimum autopilot engagement height

A

200ft

31
Q

LAND 2 or LAND 3 allowable flaps

A

Flaps20 or Flaps30

32
Q

Max fuel temperature

A

49 degrees

33
Q

Minimum fuel temperature for takeoff

A
  1. 40 degrees
  2. 3 degrees above the freezing point of the fuel used
34
Q

Minimum fuel temperature for fuel in flight

A

3 degrees above the freezing point of the fuel used

35
Q

Reverse thrust limitations

A
  1. Intentional selection in flight is prohibited
  2. Backing of the airplane is prohibited
36
Q

Auto Land maximum and minimum glide slope angle

A

Max - 3.25 degrees
Min - 2.5 degrees

37
Q

__________ and __________ control inputs are to be avoided inflight. Especially in combination of pitch, roll or yaw even at speed below Va.

A

Large, Alternating.

38
Q

Maximum cabin differential

A

9.1dpsi

39
Q

ADIRU latitudes of operation

A

North 82 degrees
South 82 degrees

40
Q

APU starter cycle limits electric and air turbine

A
  1. 3x starts in 60 minutes
  2. 60 second wait between starts 1-3
41
Q

Wingspan

A

212’7”

42
Q

Overall length

A

209’1”

43
Q

Height

A

62’4”

44
Q

Minimum pavement for 180 degree turn

A

157’4”

45
Q

Minimum altitude for FLCH use

A

1000ft Above field elevation

46
Q

RVSM altimeter tolerance on ground and in flight

A

Ground - 75ft

In flight - 200ft

47
Q

Max demo crosswind

A

38kts

48
Q

Maximum takeoff and landing altitudes all tails

A

N704GT
8400ft pressure height

Remainder of fleet
9800ft pressure height or
field elevation 9650ft

777 Atlas Air (16 decks)

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