Limitations

Question 1

Max Ramp Wt.

Answer 1

85,870 lb

Question 2

Max T/O Wt.

Answer 2

85,517 lb

Question 3

Max Lnd. Wt.

Answer 3

74,957 lb

Question 4

Max ZFW

Answer 4

69,886 lb

Question 5

Min Rwy. Width

Answer 5

100 ft (SKW)

Question 6

Min Txy. Width

Answer 6

50 ft. (SKW)

Question 7

Wing Span

Answer 7

93 ft 11 in

Question 8

Aircraft length

Answer 8

103 ft 11 in

Question 9

Tail height

Answer 9

32 ft 4 in

Question 10

Max Ops. Alt

Answer 10

41,000 ft

Question 11

Max T/O & Lnd. (ft. in MSL)

Answer 11

10,000 ft

Question 12

Max temp. T/O & Lnd.

Answer 12

ISA + 35C (not to exceed 52C)

Question 13

Min. Temp T/O & Lnd.

Answer 13

-40*C

Question 14

Rwy slope

Answer 14

+/- 2%

Question 15

Max tailwind T/O & Lnd

Answer 15

15 kt

Question 16

Max Single Pack Operations (ft. in MSL)

Answer 16

31,000 ft

Question 17

Vmo- [SL-8000]

Answer 17

300 kts

Question 18

Vmo - [10,000-Mach transition]

Answer 18

320 kts

Question 19

Mmo

Answer 19

0.82 Mach

Question 20

Va (maneuvering speed)

Answer 20

240 kts

Question 21

V lo ext

Answer 21

250 kts

Question 22

V le ext

Answer 22

250 kts

Question 23

V le

Answer 23

250 kts

Question 24

V tire

Answer 24

195 kts

Question 25

V rat deploy MAX

Answer 25

Vmo/Mmo

Question 26

V rat deployed (to provide electric power)

Answer 26

130 kts

Question 27

Vb ( < 10,000 ft) (turb air pen. speed)

Answer 27

250 kts

Question 28

Vb ( > 10,000 ft) (turb air pen. spd)

Answer 28

270 / 0.76M (whichever speed is slower)

Question 29

V wiper ops max

Answer 29

250 kts (SKW)

Question 30

V window

Answer 30

160 kts

Question 31

Max flap operating speeds

Answer 31

Vfe 1 = 230 kts
Vfe 2 = 215 kts
Vfe 3 = 200 kts
Vfe 4 = 180 kts
Vfe 5 = 180 kts
Vfe F = 165 kts

Question 32

Max altitude Flaps/Slats extended

Answer 32

20,000’

Question 33

Flap setting - CAT II approach

Answer 33

Mandatory Flap 5 (SKYW)

Question 34

Flap setting on go-around

Answer 34

Landing F = Go-Around Flaps 4

Landing 5 = Go-Around Flaps 2

Question 35

Battery minimum voltage

Answer 35

22.5 V

if voltage between [21.0V and 22.4V], then recharge may be accomplished

if voltage 21.0 or less, then MX write-up

Question 36

ITT maximum operational limits

Answer 36

815*C

Question 37

Starter cranking limits (engine)

Answer 37

Engine start (ground)
Start attempts 1 & 2 = 90s ON, 10s OFF
Start attempts 3 & 4 & 5 = 90s ON, 5m OFF

Engine start (air)
Start attempts 1 & 2 = 120s ON, 10s OFF
Start attempt 3 & 4 & 5 = 120s ON, 5m OFF

times are MAX cumulative per attempt

Question 38

Dry motoring duty cycle limits

Answer 38

#1 - 90s ON , 5m OFF
#2-5  30s ON , 5m OFF
(after 5 sequential attempts, wait 15 min)

Question 39

Max fuel capacity

Answer 39

20,935 lbs

Question 40

Max fuel imbalance

Answer 40

794 lbs
(It’s OK to land/TO with FUEL IMBALANCE)

(Fuel cross feed must be OFF on LAND/TO)

Question 41

Min. fuel tank temp

Answer 41

-37*C

Question 42

APU starter duty cycle

Answer 42

#1,2 - 60s OFF
#3,4,5 - 5m OFF

(Wait 30s after EICAS energized to start)

(If APU ON don’t leave unattended for 5m)

(No simultaneous use of HP & APU bleed)

Question 43

APU operational limits (start limit - OAT)

Answer 43

min -54C to (ISA + 35C)

Question 44

APU operational limits (start altitude)

Answer 44

30,000 ft

Question 45

APU continuous operation limits (OAT)

Answer 45

-54C to [ISA + 35C] (not to exceed 52*C)

Question 46

APU continuous operation limits (altitude)

Answer 46

33,000 ft

Question 47

APU continuous operation limit (altitude for electrical use)

Answer 47

33,000 ft

Question 48

APU continuous operation limit (engine start)

Answer 48

21,000 ft

Question 49

APU continuous operation limit (bleed use)

Answer 49

15,000 ft

Question 50

MAX differential cabin pressure

Answer 50

8.4 psi

Question 51

MAX differential cabin overpressure

Answer 51

8.8 psi

Question 52

MAX differential cabin negative pressure

Answer 52

-0.5 psi

Question 53

MAX differential cabin pressure for T/O, LAND

Answer 53

0.2 psi

Question 54

Minimum hydraulic reservoir temp for engine start

Answer 54

-18*C

Question 55

MAX/Minimum brake temp for T/O

Answer 55

Green range

Question 56

Thrust reverser operations

Answer 56

Don’t attempt go-around after deployed

REV icon must be green before stowing, after deployed

Use of thrust reverse in taxi PROHIBITED

Use of thrust reverse for power back PROHIBITED

Question 57

Operating in icing conditions (on-ground)

Answer 57

TO DATASET MENU on MCDU must be set to ENG when OAT is between 5C and 10C and:

(1) possibilitity of visible moisture up to 1700’ AGL
(2) operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested

TO DATASET MENU on MCDU must be set to ALL when OAT is below 5*C and:

(1) possibilitity of visible moisture up to 1700’ AGL
(2) operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested

Question 58

Operating in icing conditions (in-flight)

Answer 58

• Ice protection mode selector always set to AUTO
• If either ice detector fail, then crew must set mode selector to ON when icing conditions exist or are anticipated below 10*C TAT with visible moisture

Question 59

Autopilot FCS operations

Answer 59

Minimum engagement height = 400’ AGL

Minimum use height on approach = 50’ HAT

Question 60

Instrument, navigation, comms

Answer 60

TAS, TAT, and SAT info valid above 60 kts

Mag compass not valid while on VHF1

BARO ALT mins must be used on CAT I

RNAV (GPS) LP minima not authorized

Predictive EGPWS manually inhibited at non-database airports and during QFE operations to avoid unwanted alerts…..press GND PROX TERR INHIB.