LIMITATIONS

Question 1

MRW, MTOW, MLW, MZFW?

Answer 1

MRW 38222 KG
MTOW 37995 KG
MLW 34065 KG
MZFW 32092 KG

Question 2

Maximum airport pressure altitude for TO & Landings?

Answer 2

10.000 FT

Question 3

Maximum Operating Altitude?

Answer 3

41.000 FT

Question 4

Max. weight in compartment 6 before one FD member has to stay in the cockpit before offload, due to tail tipping?

Answer 4

780 KG

Question 5

Maximum Ambient air temperature approved for TO & Landing is?

Answer 5

ISA + 35 Degrees

Question 6

Minimum Ambient air temperature approved for TO is?

Answer 6

Minus 40 Degrees

Question 7

When shall Cowl Anti-ICE be selected on during ground ops?

Answer 7

OAT is 10 Degrees or below and visible moisture in any form is present such as fog with vis of 1500M or less, rain, snow, sleet & ice crystals.

And when operating on contaminated RWY’s & Taxiways.

Question 8

When shall Cowl Anti-ICE be selected on during flight operations?

Answer 8

When in icing conditions which is:
TAT below 10 degrees and visible moisture is encountered such as clouds, rain, snow etc.

EXCEPT when SAT is -40Degrees or below.

Question 9

When shall wing Anti-ICE be selected on during ground ops?

Answer 9

OAT is 5 Degrees or below and visible moisture in any form is present such as fog with vis of 1500M or less, rain, snow, sleet & ice crystals.

And when operating on contaminated RWY’s.

NOTE: When type II, III or IV anti-icing fluids has been applied, the wing anti-ice system must first be selected on prior to thrust increase for TO.

Question 10

When shall wing Anti-ICE be selected on during flight operations?

Answer 10

When ICE is annunciated on EICAS or when in icing conditions and airspeed is less than 230 KIAS.

Question 11

What is the maximum runway slopes? Up and downhill?

Answer 11

+2% Uphill
-2% Downhill

Question 12

Max tailwind component for take-off & landings?

Answer 12

10 knots.

Question 13

How many minutes must the flight be within a suitable airport, if cargo is carried in either cargo compartment?

Answer 13

60 minutes.

Question 14

Green range for N1?

Answer 14

0 - 99.4% RPM

Question 15

Green range for N2?

Answer 15

0 - 99.3% RPM

Question 16

Green range for oil temp?

Answer 16

-40 - 155 Degrees

Question 17

How many percent must the N1 setting on ED1 be within compared to the N1 setting on the perfo app?

Answer 17

-+1%.

Question 18

How many minutes after engine start does the N1 need to stay below 75%?

Answer 18

2 minutes.

Question 19

Normal take off power and maximum power (two engines) is limited to how many minutes?

Answer 19

5 minutes.

Question 20

APR power for one engine is limited to how many minutes?

Answer 20

10 minutes.

Question 21

ITT must be below how many degrees, before attempting to ground start engine?

Answer 21

120 Degrees.

Question 22

What is the minimum oil level for flight?

Answer 22

40%. = 1 flight.

Question 23

What is a cold soaked airplane?

Answer 23

When the airplane has been parked in more than -30 degrees for more than 8 hours.

Question 24

When shall continuous ignition be used?

Answer 24

Take off and landings on contaminated runways.

Flights through moderate or heavy rainfall

Flights through moderate or severe turbulence.

Flight in the vicinity of thunderstorms.

Question 25

Starter cranking limits on ground during engine start?

Answer 25

The starter must not be used when indicated n2 RPM exceeds 45%. The starter must only be used for 90 seconds during start 1 & 2 followed by a 10 seconds cooldown.

Question 26

Max altitude for engine relight windmilling?

Answer 26

25.000FT

Question 27

Max altitude for engine relight starter assisted?

Answer 27

21.000FT

Question 28

Max altitude for engine relight all-engine-out rapid relight?

Answer 28

10.000FT

Question 29

Max fuel imbalance on ground?

Answer 29

136KG

Question 30

Max fuel imbalance in flight?

Answer 30

363KG

Question 31

Max usable fuel load for left main tank (pressure refueling)?

Answer 31

3398 KG

Question 32

Max usable fuel load for right main tank (pressure refueling)?

Answer 32

3398 KG

Question 33

Max usable fuel load for centre tank (pressure refueling)?

Answer 33

2091KG

Question 34

Max total usable fuel load (pressure refueling)?

Answer 34

8887KG

Question 35

The minimum fuel quantity for go-around is?

Answer 35

272 KG Per wing. (With airplane level and maximum airplane clim attitude of 10 degrees nose up).

Question 36

Minimum fuel temperature for take-off?

Answer 36

5 degrees.

Question 37

Maximum oil consumption on each engine pr. hour?

Answer 37

0.05 us Gallons.

Question 38

Max RPM for the APU?

Answer 38

106% RPM

Question 39

Minimum ambient temperature for starting a cold soaked APU on the ground is?

Answer 39

-40 Degrees

Question 40

Max APU starts per hour?

Answer 40

3 starts / start attempts. ( Two minute delay between cranking attempt to allow for cooling of starter and for APU drainage).

Question 41

Max. EGT, APU on speed on ground?

Answer 41

682 - 789 degrees

Question 42

Max. altitude for APU bleed air extraction?

Answer 42

25.000 FT

Question 43

Max. permissible load on the APU generator?

Answer 43

40 KvA.

Question 44

Max. EGT, APU on speed In flight?

Answer 44

807 degrees. (Green range 0-806)

Question 45

Max mach number during cruise in RVSM airspace?

Answer 45

M 0.82

Question 46

Max speeds for flaps?

Answer 46

FLAPS 1: 230 FLAPS 8: 230 FLAPS 20: 220 FLAPS 30: 185 FLAPS 45: 170

Question 47

Maximum airspeed at which it is safe to extend the landing gear?

Answer 47

220 KIAS

Question 48

Maximum airspeed at which it is safe to retract the landing gear?

Answer 48

200 KIAS

Question 49

Max airspeed at which the airplane may be flown with the landing gear extended and locked?

Answer 49

200 KIAS

Question 50

Tire limit speed?

Answer 50

195 KIAS

Question 51

Max airspeed for ADG operations?

Answer 51

VMO/MMO.

Question 52

Turbulence penetration speed?

Answer 52

280 KIAS / MACH .75

Question 53

Max speed for windshield wiper operation?

Answer 53

250 KIAS

Question 54

Maneuvering limit load factors for flaps up and flaps down?

Answer 54

Flaps up: -1.0G - 2,5G Flaps down: 0.0G - 2.0G

Question 55

Maximum positive differential pressure is?

Answer 55

8.7 PSI

Question 56

Maximum negative differential pressure is?

Answer 56

-0,5 PSI

Question 57

Max altitude for single pack operation?

Answer 57

25.000FT

Question 58

AP minimum use height for TO?

Answer 58

600 ft. AGL

Question 59

AP minimum use height for NPA?

Answer 59

400 ft. AGL

Question 60

AP minimum use height for one engine operating?

Answer 60

110 ft. AGL

Question 61

AP minimum use height for PA?

Answer 61

60 ft. AGL.

Question 62

Maximum permissible time for ground operation with DC power only?

Answer 62

5 minutes to protect the flight compartment CRT displays.

Question 63

Max permissible continuous load on each TRU in-flight?

Answer 63

120 amp.