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84 Cards in this Set

  • Front
  • Back

Max Ramp Weight

85,870

Max T/O Weight

85,517

Max Landing Weight

74,957

Max Zero Fuel Weight

69,886

Minimum Runway Width

100 ft.

Wing Span

93 ft. 11 in.

Aircraft Length

103 ft. 11 in.

Tail Height

32 ft. 4 in.

Max Ops. Alt.

41,000 ft

Max T/O & Land Altitude

8,000 ft.

Max Temp. T/O & Land

ISA + 35°C (52°C)

Min Temp. T/O & Land

-40°C

RWY Slope

+/- 2%

Max Tailwind

15 kt

Max Single Pack Operations Altitude

31,000 ft

VMO


SL - 8,000’

300

VMO


10,000 - Mach Transition

320

MMO

0.82

VA

240

VLO EXT

250

VLE EXT

250

VFE 1

230

VFE 2

215

VFE 3

200

VFE 4

180

VFE 5

180

VFE FULL

165

Max X-Wind


Dry Runway

38 kt

Max X-Wind


Wet Runway

31 kt

Max X-Wind


Runway w/compacted snow

20 kt

Max X-Wind


Runway w/standing water, slush, wet snow, or dry snow

18 kt

VLE RET

250

Max X-Wind


Runway w/ice

12 kt

Static takeoff is not recommended with x-wind component greater than _____.


Why?

30 kt


Due to compressor stall.

Max Alt. Flaps/Slats Extended

20,000 ft

Use of Flaps/Slats for Enroute Ops is ________.

Prohibited

Min. Spoiler Speed

180 kt

Flaps setting for CAT II approach

Mandatory Flaps 5

Go around flaps setting when landing flaps full

Flaps 4

Go around flaps setting when landing Flaps 5

Flaps 2

Minimum battery voltage

22.5 V

Max engine temp for start

815° C

VLE

250

Minimum oil temp. for start

-40°C

Minimum oil pressure for start

25 psi

Engine start cranking limits on ground.


1&2:


3-5:

1&2: 90 sec ON, 10 sec OFF


3-5: 90 sec ON, 5 min OFF

Engine start cranking limits in flight.


1&2:


3-5:

1&2: 120 sec ON, 10 sec OFF


3-5: 120 sec ON, 5 min OFF

Dry motoring duty cycle limits.


1:


2-5:

1: 90 sec ON, 5 min OFF


2-5: 30 sec ON, 5 min OFF

Max fuel capacity

20,935 lb

Max fuel imbalance

794 lbs

Minimum fuel tank temp.

-40°C

Fuel crossfeed must be selected _____ during takeoff & landing.

OFF

Wait _______ after the _______ is energized to start the APU.

30 seconds


EICAS

VTIRE

195

Do not leave the aircraft unattended more than _______ with the APU running. (SW)

Five minutes

Simultaneous use of the ____ and the HP cart is ______.

APU bleed


Prohibited

APU starter duty cycle limits


1&2:


3rd:

1&2: 60 sec OFF


3rd: 5 min OFF

APU start temp. limits

MIN: -54°C


MAX: ISA +35

APU max Start Altitude

30,000 ft.

APU max operating altitude

33,000 ft.

APU max Altitude for generator use

33,000 ft

APU max Altitude for bleed air use

15,000 ft

APU max Altitude to start engine

21,000 ft

Max differential pressure up to 37,000 ft

7.8 psi

VRAT DEPLOY MAX

VMO/MMO

Max differential pressure above 37,000 ft.

8.34 psi

Max differential over pressure

8.77 psi

Max differential negative pressure

-0.5 psi

Max differential pressure for takeoff and Landing

0.2 psi

Minimum hydraulic reservoir temperature for engine start

-18°C

Brake temperature indication must be in the ________ for takeoff.

Green range

Do not attempt a _____________ after deployment of the thrust reversers.

Go-around maneuver

The use of thrust reversers during normal taxi operations is ________.

Prohibited

The use of thrust reversers for power back operations is ________.

Prohibited

Autopilot minimum engagement height

400 ft

VMIN (to provide electrical power)

130

Minimum autopilot use height

50 ft

Minimum autopilot use height (non-precision approach)

MDA

TAS, TAT, and SAT information are only valid above _______.

60 kt

Barometric altimeter minimums must be used for all ________ approaches.

CAT I

VB (below 10,000 ft)

250

VB (10,000 ft & above)

270/.76M (whichever is lower)

Vwiper ops max

250 (SW)

Vwindow

160