Limitations and Immediate Action Items Test

Question 1

Maximum Taxi and Ramp Weight

Answer 1

53,250 lbs

Question 2

Maximum Takeoff Weight

Answer 2

53,000 lbs

Question 3

Maximum Landing Weight

Answer 3

47,000 lbs

Question 4

Maximum Zero Fuel Weight

Answer 4

44,000 lbs

Question 5

Minimum Operating Weight Empty

Answer 5

25,480 lbs

Question 6

Maximum Pressure Altitude for takeoff and landing

Answer 6

8,000 ft

Question 7

Maximum Operating Altitude

Answer 7

36,000 ft

Question 8

Minimum Ambient Temperature for Takeoff

Answer 8

-40°C

Question 9

Definition of Icing Conditions COWL

Answer 9

Icing Conditions exist when the OAT (on the ground and for takeoff) or TAT (inflight) is 10°C or
below, and:
• Visible moisture in any form (such as clouds, fog, mist, rain, snow, sleet, or ice crystals), is present in flight, or below
400 feet AGL for ground operations, or
• When operating on surfaces that are wet or contaminated.

Question 10

When must COWL anti-ice be on

Answer 10

Cowl Anti-Ice must be ON for all ground and flight operations when icing conditions exist except when the inflight SAT
is -40°C or below, or ICE is annunciated by the ice detection system.

Question 11

Definition of Icing Conditions WING

Answer 11

Icing conditions exist when the OAT (takeoff) is 5°C or TAT (inflight) is 10°C or below, and:
• Visible moisture in any form (such as clouds, fog, mist, rain, snow, sleet or ice crystals) is present in flight, or below
400 feet AGL for takeoff, or
• The runway is wet or contaminated.

Question 12

When must WING anti-ice be on

Answer 12

Wing Anti-Ice must be ON for takeoff and flight operations when ICE is annunciated by the ice detection system, or
when icing conditions exist and the airspeed is less than 230 KIAS except when the inflight SAT is -40°C or below. In addition, Wing Anti-Ice must be ON for the final two minutes prior to takeoff during all ground operations 5°C
OAT or below unless Type III or IV anti-icing fluid has been applied.

Question 13

Tactile Check - When-Why-How

Answer 13

OAT is 5°C or less or wing fuel temperature is 0°C or less or the atmospheric conditions have been conducive to frost formation.
Ice and frost may continue to adhere to wing surfaces for some time at OAT above 5°C
Tactile check wing leading edge, wing forward upper surface, wing rear upper surface

Question 14

Do not hold in icing conditions with ____ and/or _____ extended

Answer 14

Slats / Flaps

Question 15

Continued operation in areas where SLD icing conditions exist is__________

Answer 15

Prohibited

Question 16

All contaminated performance data will be for _______ takeoffs

Answer 16

Static

Question 17

Maximum Tailwind for takeoff and landing

Answer 17

10 kts

Question 18

Maximum Crosswind for takeoff and landing

Answer 18

27 kts

Question 19

Maximum 90 degree Crosswind for landing from a Category II approach

Answer 19

15 kts

Question 20

Maximum headwind for landing from a Category II Approach

Answer 20

17 kts

Question 21

Maximum weight in the cargo compartment

Answer 21

3,500 lbs

Question 22

Flights must be within _______ minutes of a suitable airport with cargo in the cargo compartment

Answer 22

45

Question 23

EICAS Limit Markings Red/Amber/Green

Answer 23

Maximum and Minimum Limitations/Caution Range/Normal Operating Range

Question 24

Maximum ITT for start

Answer 24

900°C

Question 25

Maximum N2 split at idle

Answer 25

2%N2

Question 26

Maximum ITT for all air starts

Answer 26

90°C

Question 27

Maximum ITT allowed to advance the thrust levers to idle for all ground starts

Answer 27

120°C

Question 28

Oil pressure Steady-state idle

Answer 28

25 PSI minimum

Question 29

Oil pressure Takeoff Power

Answer 29

45 PSI minimum

Question 30

Minimum oil temperature for engine starting

Answer 30

-40°C

Question 31

During ALL starts, do not exceed ________N1 for _______ minutes after start, or until all operating indications are in the normal range, whichever is _________

Answer 31

75%/2/longer

Question 32

Operate engines at or near idle for ______ minutes prior to shutdown

Answer 32

2

Question 33

Airplane Cold Soak Define:

Answer 33

Before the first flight of the day, when the airplane is cold soaked at an ambient temperature of -30°C or below for more than 8 hours

Question 34

Airplane Cold Soak Operational

Answer 34

The engines must be dry motored for 60 seconds and fan rotation must be verified before an engine start is initiated. Thrust revers must be actuated until deploy and stow cycles are less than 5 seconds

Question 35

Continues ignition must be used during:

Answer 35

Takeoff and landing on contaminated runways Takeoffs with high crosswinds (15 kts or greater) Flight through moderate or heavier precipitation Flight through moderate or heavier turbulence Flight in the vicinity of thunderstorms

Question 36

Starter cranking limits

Answer 36

1 min/10 sec, 1 min/10 sec, 1 min/5 min

Question 37

Dry Motor Cycle for engines

Answer 37

90 sec/5 min, 30 sec/5 min

Question 38

Maximum fuel imbalance between the left and right wing tank

Answer 38

800 lbs

Question 39

Maximum total fuel for pressure refueling

Answer 39

14,518 lbs

Question 40

Takeoff with a fuel load in excess of ______ in the center tank is not permitted unless each wing tank is above ________

Answer 40

500 lbs / 4,400 lbs

Question 41

Powered Crossflow and gravity crossflow must be ______ for takeoff

Answer 41

Off

Question 42

Takeoff with engine fuel temperature indications below ______ is prohibited

Answer 42

5°C

Question 43

Minimum Fuel Quantity for a go-around per wing tank, assuming 10 degrees pitch up _________

Answer 43

450 lbs

Question 44

APU start (on battery)

Answer 44

30 sec/2 min, 30 sec/20 min, 30 sec/2 min, 30 sec/40 min

Question 45

APU start (on DC ground power)

Answer 45

15 sec/2min, 15 sec/20 min, 15 sec/2 min, 15 sec/40 min

Question 46

APU maximum starting altitude

Answer 46

30,000 ft

Question 47

APU maximum operating altitude

Answer 47

36,000 ft

Question 48

Maximum APU RPM

Answer 48

107%

Question 49

With the APU door not closed, or the door position is unknown: The airplane must be limited to _____, or _________

Answer 49

300 KIAS/The APU must remain in operation

Question 50

Maximum bleed air extraction for air conditioning from the APU is______

Answer 50

15,000 ft

Question 51

Maximum engine start altitude with APU bleed air______

Answer 51

13,000 ft

Question 52

Minimum Engine Oil Pressure for takeoff ________

Answer 52

45 psi

Question 53

Flap position 8 Vfe / Vfo

Answer 53

230 KIAS / 200 KIAS

Question 54

Flap position 20 Vfe / Vfo

Answer 54

220 KIAS / 200 KIAS

Question 55

Flap position 30 Vfe / Vfo

Answer 55

185 KIAS

Question 56

Flap position 45 Vfe / Vfo

Answer 56

170 KIAS

Question 57

Gear extension maximum operating airspeed

Answer 57

220 KIAS

Question 58

Gear down and locked maximum operating airspeed

Answer 58

220 KIAS

Question 59

Gear retraction maximum operating airspeed

Answer 59

200 KIAS

Question 60

Maximum Tire Speed ________

Answer 60

182 kts

Question 61

Maximum airspeed for windshield wiper operation failed in the non-parked position__________

Answer 61

220 KIAS

Question 62

Maximum Turbulence Penetration Speed______

Answer 62

280 KIAS or .75M whichever is lower

Question 63

Maximum cruise mach in RVSM airspace

Answer 63

.82 M

Question 64

RVSM Required Equipment List

Answer 64

Autopilot (1) / Must be operational Altitude Alerting System (1) / Must be operational Altitude Reporting Transponder (2) / (1) Must be operaitonal ADC (2) / (2) Must be operational

Question 65

Minimum Auto Pilot engagement altitude ______ except when performing Non-precision approach_________, Precision approach________

Answer 65

600 ft AGL / 400 ft AGL / 80 ft AGL

Question 66

Maximum slats/flaps extension altitude

Answer 66

15,000 ft

Question 67

Maximum permissible time on the ground with only DC power

Answer 67

5 min

Question 68

Minimum altitude for light spoiler deployment

Answer 68

1000 ft AGL

Question 69

Minimum airspeed for flight spoiler use

Answer 69

Vref + 17 KIAS

Question 70

Minimum brake cooling time

Answer 70

15 minutes and all BTMS indicators are green and not increasing

Question 71

During ladning application of thrust reverse above ______ is not permitted at air speeds below _____. Below _____, reverse thrust must be reduced to idle, not above _______

Answer 71

60%N1 / 75 KIAS / 60 KIAS / 30%N1

Question 72

Use of the EMER DEPRESS switch above ______ is prohibited

Answer 72

15,000 ft

Question 73

Max altitude for single pack operations

Answer 73

25,000 ft

Question 74

Max differential pressure for taxi, takeoff, and landing

Answer 74

0.1 psi

Question 75

Maximum relief differential pressure

Answer 75

8.7 psi

Question 76

Braking Loss / Asymmetry

Answer 76

Wheel Brakes...Release Momentarily PM will select ANTI-SKID to OFF Wheel Brakes...Re-apply as required Reverse Thrust...Apply maximum until stopping assured

Question 77

Cabin Alt

Answer 77

Oxygen Masks....Don and 100% Crew Communication....Establish Captain assumes PF duties

Question 78

Double Engine Failure

Answer 78

CONT IGNITION....On | Airpspeed...240 KIAS minimum

Question 79

Smoke/Fumes

Answer 79

Oxygen Masks....Don and 100% | Crew Communication....Establish

Question 80

Stab Trim Runaway

Answer 80

Control Wheel.... Assume manual control and override runaway Both STAB TRIM DISCs....Push, hold, release Captain assumes PF duties STAB CH1 cb (2f5)....open STAB CH2 cb (4a1)....open