Limitations

Question 1

Maximum crosswind for T/O and Landing

Answer 1

27 kts

Question 2

Maximum crosswind for landing from a CAT II

Answer 2

15 kts

Question 3

Maximum headwind for landing from a CAT II

Answer 3

16 kts

Question 4

Maximum tailwind component

Answer 4

10 kts

Question 5

Minimum approved runway width

Answer 5

100ft.

Question 6

Maximum pressure altitude for T/O and landing

Answer 6

8,000ft.

Question 7

Maximum Operating Altitude

Answer 7

41,000 ft.

Question 8

Except in an emergency, takeoff or landing will not be attempted whenever peak wind value exceeds
________. Crosswind components, not including gust factor, are limited to AFM maximum
demonstrated as listed above. Crosswind and tailwind components may be further limited by runway
conditions or Operations Specifications

Answer 8

50 kts

Question 9

Maximum positive pressure differential

Answer 9

8.7 psi

Question 10

Maximum altitude for single pack operation

Answer 10

31,000 ft.

Question 11

Low pressure air must be ____ prior to the main cabin door being closed and secure

Answer 11

OFF

Question 12

EMER DEPRESS switch is prohibited above ________

Answer 12

15,000ft

Question 13

Max Severe Turbulence penetration speed

Answer 13

280 KIAS/ .75 Mach whichever is slower

Question 14

Max Gear Extension speed

Answer 14

220 KIAS

Question 15

Max Gear Extended Speed

Answer 15

220 KIAS

Question 16

Max Gear Retraction Speed

Answer 16

200 KIAS

Question 17

Max Airspeed for windshield operation

Answer 17

250 KIAS

Question 18

Max Cruise Mach in RVSM airspace

Answer 18

.82 M

Question 19

Tire ground limit speed (700)

Answer 19

182 kts

Question 20

Tire ground limit speed (900)

Answer 20

195 kts

Question 21

Flap speeds

Answer 21

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

Question 22

APU Starting limitation

Answer 22

The APU starter motor duty cycle is limited to not more than three (3) starts/start attempts in one (1) hour with a
two (2) minute delay between cranking attempts

Question 23

Max Bleed Air extraction from APU altitude

Answer 23

25,000ft.

Question 24

Max APU starting Altitude

Answer 24

37,000ft.

Question 25

Can the APU be used for bleed air for engine start?

Answer 25

yes

Question 26

APU door limitation

Answer 26

With the APU door not closed or the door position is unknown: * The airplane must be limited to: 220 KIAS * Or the APU must remain in operation

Question 27

To protect the flight compartment CRT displays, the maximum permissible time for ground operations with DC power only is ________.

Answer 27

5 minutes

Question 28

During all starts, do not exceed _____ for 2 minutes after start, or until all operating indications are in the normal range, whichever is longer

Answer 28

75% N1

Question 29

Engines must be at idle for ____ prior to shut down

Answer 29

2 minutes (Taxi time with engines stabilized at 80% N2 or below count towards the cool down period)

Question 30

Normal T/O power and max power on 2 engines is limited to______

Answer 30

5 minutes

Question 31

APR power (1 engine) is limited to

Answer 31

10 minutes

Question 32

ITT must below ____ before start on the ground

Answer 32

120 C

Question 33

ITT must below ____ before start in the air

Answer 33

90 C

Question 34

Before the first flight of the day, when the airplane is cold-soaked at an ambient temperature of -30°C (-22°F) or below for more than 8 hours: (Cold Soak)

Answer 34

* The engines must be motored for 60 seconds and fan rotation must be verified before an engine start is initiated * Thrust reversers must be actuated until the deploy and stow cycles are 2 seconds or less

Question 35

Oil Pressure Steady State idl

Answer 35

25 psi

Question 36

Max Oil pressure for T/O

Answer 36

45 psi

Question 37

After cold start, engine must remain at _____ until oil pressure returns to normal range

Answer 37

idle

Question 38

Continuous Engine Must be on:

Answer 38

* Takeoff and landing on contaminated runways * Takeoff with high crosswind components (15 knots or greater) * Flight through moderate or heavier intensity rain * Flight through moderate or heavier intensity turbulence * Flight in the vicinity of thunderstorms

Question 39

Starter Cranking Limits (on ground)

Answer 39

1: 90 Seconds 10 Seconds OFF 2: 90 Seconds 10 Seconds OFF 3: and Subsequent 90 Seconds 5 Minutes OFF

Question 40

During landing, maximum reverse thrust is prohibited below ______, and reverse idle should be achieved by _____

Answer 40

75 KIAS, 60KIAS

Question 41

Reduced Thrust (FLEX) Takeoff

Answer 41

The following limitations apply to reduced thrust takeoff: 1. Anti-skid must be operative 2. PROHIBITED on contaminated runways 3. PROHIBITED if the airplane has been de-iced 4. PROHIBITED if wing and/or cowl anti-icing bleeds are in use 5. PROHIBITED if warnings of windshear or downdrafts have been forecast 6. PROHIBITED with an engine that cannot achieve full-rated thrust 7. PROHIBITED when a special departure procedure specifies full thrust for takeoff

Question 42

En Route use of Slats/ Flaps

Answer 42

PROHIBITED

Question 43

Max slats and or/ flaps extended

Answer 43

15,00ft.

Question 44

Minimum flight spoiler deployment

Answer 44

1,000 ft. AGL

Question 45

To ensure adequate maneuver margins, flight spoilers must not be extended inflight at airspeeds below the recommended ________

Answer 45

Vref +10

Question 46

Max fuel imbalance for T/O

Answer 46

300 lbs

Question 47

Max Fuel imbalance all other phases of flight

Answer 47

800lbs

Question 48

Gravity Refueling (700)

Answer 48

14,580

Question 49

Gravity Refueling (900)

Answer 49

14,810

Question 50

Pressure Refueling

Answer 50

19,594

Question 51

Engine fuel temperature cannot be below

Answer 51

5C

Question 52

Ground contamination definition

Answer 52

Runways, ramps or taxiways with surface snow, ice, slush or standing water

Question 53

Visual moisture definition

Answer 53

Visible moisture or precipitation in any form (such as fog with visibility of one mile or less, mist, rain, snow, sleet, and ice crystals or clouds inflight)

Question 54

Taxi: Anti Ice

Answer 54

10 C or below: Cowl

Question 55

Take off: Anti-ice

Answer 55

10 C or below :cowl 5 C or below: wing and cowl

Question 56

InFLight: Anti Ice

Answer 56

OAT 10C to SAT -39C greater than or equal to 230: cowl Less than 230: wing and cowl

Question 57

When is Single engine Taxi Prohibited?

Answer 57

when ramps or taxiways are contaminated with snow, slush, or ice, or when snow or other freezing/frozen precipitation is present

Question 58

When is a Tactile Check required?

Answer 58

* The OAT is 10°C or less, or * The bulk 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 even at outside air temperatures above 10°C.

Question 59

Taxi light limitation

Answer 59

The taxi lights must be switched OFF whenever the airplane is stationary in excess of 10 minutes

Question 60

Minimum brake cooling time

Answer 60

15 minutes, and all BTMS indicators must be green and not increasing

Question 61

Category II approaches are prohibited when the braking action is reported as less than

Answer 61

Medium

Question 62

Where can live animals not be transported?

Answer 62

Fwd Cargo

Question 63

Autopilot limitations

Answer 63

Prohibited below: -600 ft. AGL except: +non- precision approach 400 AGL +precision and APV 80 ft. AGL +precision app single engine 110 ft. AGL

Question 64

Max Taxi & Ramp Weight

Answer 64

700: 75,250 900: 85,000

Question 65

Max T/O weight

Answer 65

700: 75,000 900: 84,500

Question 66

Max Landing weight

Answer 66

700: 67,000 900: 75,100

Question 67

Max zero fuel weight

Answer 67

700: 62,300 900: 70,750