Limitations

Question 0

Vlo retraction
Vlo extension
Vle

Answer 0

Vlo-R: 200kt
Vlo-E: 250kt
Vle: 250kt

Question 1

VA

Answer 1

200kt

Question 2

Flaps maximum speed

Answer 2

9°- 250kias
18°- 200kias
22°- 200kias
45°- 145kias

Question 3

Pitch trim maximum speed after T/O without retrimming

Answer 3

160 kias

Question 4

Maximum recommended speed to remove direct vision windows

Answer 4

140 kias

Question 5

Turbulent air penetration speed

Answer 5

Above FL100: 250kias/M.63

Below: 200kias

Question 6

Maximum recommended wind speed

Answer 6

Tail: 10kt
Crosswind:
Dry / wet - 30kt
Snow - 25kt
Standing water/slush - 20kt
Ice - 10kt

Question 7

Manouver load factors

Answer 7

Flaps up: +2.5g / -1.0g

Flaps down: 2.0g / no negative g

Question 8

Runway

Answer 8

Paved

Slope +2% / -2%

Question 9

EGPWS

Answer 9

• Do not acount man-made obstacles;
• TERRAIN SYS OVRD must be pressed 15NM before T/O or approach:
• –if there is no ifr procedure;
• –if the RWY is not included in database; or
• –if longest RWY is shorter than 1070m.

Question 10

Electrical

Answer 10

Max load:

Main generator - 400A

APU:
Below FL300 - 400A
Above - 300A

Max batt temp - 70°c
Batt - 28V / 19~24 - charge / >19 change
GPU - 28V (-2/+1)

Question 11

Fuel QTY

Answer 11

Max usbl qty per tank - 2573 L
Unsbl - 27 L (Any pump inop - 149 L)
Max imbalance - 363 kg

Question 12

Fuel tank temperature

Answer 12

52°C / -40°C

Question 13

Hydraulic

Answer 13

2.900 PSI (+/- 200 PSI)

Question 14

IRS knob

Answer 14

Should never be moved to ATT on the ground

Question 15

APU General

Answer 15

Min start temp: -54°c
Max start alt C11: FL250/FL300
                     C14: FL300
Max Alt: FL370
Rotor speed: 108% (C14 auto shut at 104%)

Question 16

APU Temperatures

Answer 16

EGT start: 884°c (C11 may reach 924° above FL250 for 10”)

continuos: 680°c / 717°f for 5’ (C14 may reach 734°c for 3” for APU assisted in-flight start)

Question 17

APU Starter

Answer 17

Between 3 starts - 1’ off

Between 2 series of 3 starts - 30’ off

Question 18

Engine N1 / N2 / ITT

Answer 18

N1: 100%
N2: 102.4% (pos SB 102.5%)
ITT: start 800°c
      T/O 948°c - 5'
       Continuos 901°c

Question 19

Engine Oil Pressure / Temp / Vibration

Answer 19

Oil Press: MIN - below 88% - 34 PSI
                          Above - 50 PSI
MAX - 95 PSI (115 PSI for 5', 155 PSI for 2')
OIL TEMP: MIN . 21°c (-40°c for start)
                  MAX - 126°c
Vibration: LP 1.8 IPS
                HP 1.1 IPS 
                ***Or 2.5 IPS for 5' during t/o or go around and 10" during the reminder flight fase.

Question 20

Engine Starter

Answer 20

On ground:
5’ on - 5’ off or,
first to fourth cycles 1’ on - 1’ off and following cycles 5’ off

In flight:
5’ with no cool down time required.

Question 21

Automatic Take off thrust control system (ATTCS)

Answer 21

ATTCS must be operative to select ALT T/O-1 mode.
For acft eqp with FADEC previous than 8.0 must to perform a check once a week at max take off and checking engine parameters.

Question 22

Thruster reverser

Answer 22

Do not attempt a go around after deployment of the reversers. Select of thrust reverser before touchdown is prohibited.

Question 23

Engine Warm-up / cool down

Answer 23

Warm up : 4’ for cold (shutdown for more than 90’) or 2’ for warm engines.
To increase N2 above 83% eng oil temp must be at 40°c min

Cooldown: 1’ at idle or taxi thrust.

Question 24

Pressurization

Answer 24

Max differential press: 7.8 PSI Max differential overpress: 8.1 PSI Max differential negarive press: -0.3 PSI

Question 25

Icing conditions

Answer 25

Max temp for anti-icing ops: 10°c Min temp for manual a/i ops: -40°c Single engine or single bleed ops max altitude in icing conditions: FL150.

Question 26

Maximum windshield speed operation

Answer 26

170 KIAS

Question 27

ILS

Answer 27

For airplanes with single glide slope receiver the approach may be flown usung normal procedures no lower than localizer MDA. To perform an ILS, the acft must have 2 operating g/s receivers and use independent data and displays.

Question 28

Autopilot

Answer 28

-For acft pre SB 145-31-0016 use of AP below 1500ft is permitted only when coupled to the P1 FD; -minimum DA during an ILS: 200ft AGL; -minimum engagement after t/o:500ft AGL; -malfunction: cruise 80ft maneuver 40ft ILS 15ft -single engine go-around is prohibited; -descent below mda with AP is prohibited; -APP mode during localizer only when inbound; Go-around in basic mode is allowed only with wings level. -go-around height loss: 75ft

Question 29

FMS

Answer 29

-Instrument app procedures prohibited with DGR/DR annunciated on PFD;

Question 30

SDU

Answer 30

``` Flaps: Takeoff - 22° Landing - 45° RWY: no standing water, when wet both reversers must be operational. No t/o or landing during thunderstorm or heavy rain. Max. Tail wind: 10kt Crosswind: 15kt RVR: 1500m ```