SOP Ch 3 Operational Limits

Question 1

Operational Limits

Max Takeoff and Landing Tailwind Component

Answer 1

10 knots

Question 2

Operational Limits

Max Operating Altitude

Answer 2

41,000 feet

Question 3

Operational Limits

Max Flap Extension Altitude

Answer 3

20,000 feet

Question 4

Airspeed Limitations

Max Operation Airspeed

Answer 4

V MO (320 KIAS)

Question 5

Airspeed Limits

Max Operating Mach Number

Answer 5

M MO (.82M)

Question 6

Airspeed Limits
Turbulent Airspeed
Below 10,000 feet

Answer 6

250 KIAS

Question 7

Airspeed Limits
Turbulent Airspeed
At or Above 10,000 feet

Answer 7

270 KIAS/.76M

Whichever is lower

Question 8

Airspeed Limits

Maximum Tire Limit Ground Speed

Answer 8

195 Knots

Question 9

Airspeed Limits

Maximum Windshield Wiper Operation Speed

Answer 9

250 KIAS

Question 10

Airspeed Limits
Maximum Gear Speed
Extension (V LOE)
Extended (V LE)
Retraction (V LOR)

Answer 10

250 KIAS

Question 11

Flap Operating Limits

Flaps 1

Answer 11

230 KIAS

Question 12

Flap Operating Limits

Flaps 2

Answer 12

215 KIAS

Question 13

Flap Operating Limits

Flaps 3

Answer 13

200 KIAS

Question 14

Flap Operating Limits

Flaps 4

Answer 14

180 KIAS

Question 15

Flap Operating Limits

Flaps 5

Answer 15

180 KIAS

Question 16

Flap Operating Limits

Flaps FULL

Answer 16

165 KIAS

Question 17

Flap Operating Limits

The use of Flaps 4 is prohibited during…

Answer 17

Approach and landing

Question 18

Flap Operating Limits

Flaps should never be extended below…

Answer 18

Green dot

Question 19

Flap Operating Limits

When flaps are extended…

Answer 19

Do not hold in ICING conditions

Question 20

Design Maneuvering Speed (V A)

Answer 20

below 240 KIAS

Question 21

Definition of Icing Conditions (3)

When SAT on the ground/takeoff or Total Air Temperature (TAT) in flight is:

Answer 21

1. 10*C or below; AND
2. Visible moisture is present (including Vis 1SM or less)
3. When operating on ground where surface snow, ice, standing water, or slush may be ingested by the engines

Question 22

Engine and Wing Anti-Ice System Operations

During taxi out and takeoff, the MCDU TO DATASET MENU musts be set to…

Answer 22

ALL when SAT is 10*C or below and icing conditions exist or are anticipated

Question 23

Minimum Fuel Tank Temperature

Answer 23

-37*C

Question 24

Maximum Fuel Imbalance

Answer 24

790 lbs

Question 25

Pressurization | Max altitude for single pack operation

Answer 25

31,000 feet

Question 26

EICAS Engine Limit Display Markings | Red

Answer 26

Maximum and Minimum Limitations

Question 27

EICAS Engine Limit Display Markings | Amber

Answer 27

Caution Range

Question 28

EICAS Engine Limit Display Markings | Green

Answer 28

Normal Operating Range

Question 29

Engine Thrust | Use of reduced thrust takeoff procedure is NOT allowed on...

Answer 29

Runways contaminated with standing water, slush, snow or ice

Question 30

APU Operational Limits | Start

Answer 30

30,000 feet

Question 31

APU Operational Limits | Electrical

Answer 31

33,000 feet

Question 32

APU Operational Limits | Bleed

Answer 32

15,000 feet

Question 33

APU Operation Limits | To Assist Engine Start

Answer 33

21,000 feet

Question 34

Single Engine Taxi | Single engine taxi is NOT authorized when (5):

Answer 34

1. Ice accretion in the form of freezing rain, freezing drizzle, freezing fog, or heavy snow is anticipated 2. Braking action is less than good 3. RVR is reported less than 1200 4. Power out is required (no pushback) 5. A two minute warm up cannot be accomplished

Question 35

Single Engine Taxi After Landing If starting the APU...

Answer 35

Do not shut down an engine until the APU has stabilized at 95% or greater for a minimum of 3 seconds

Question 36

Single Engine Taxi After Landing A ___ minute cool down must be observed prior to _________.

Answer 36

2; shutting down an engine

Question 37

Single Engine Taxi After Landing When performing a single engine taxi with engine 2....

Answer 37

The Electric Hydraulic Pump 1 Selector knob must be set to ON to ensure that the hydraulic system 1 is pressurized

Question 38

FMS Speeds | FMS speeds may only be used during

Answer 38

Normal flight operations

Question 39

FMS Speeds | Whenever a QRH procedure requires an airspeed correction...

Answer 39

The use of FMS speed is PROHIBITED

Question 40

Stabilized Approach Criteria | From 1,000 feet above the TDZE, the aircraft will be (3):

Answer 40

1. With the final landing configuration selected 2. On correct vertical path with a descent rate of 1,000 FPM or less 3. Correct lateral track (appropriate for type of approach being flown)

Question 41

Stabilized Approach Criteria | From 500 feet above TDZE, the aircraft will be (2):

Answer 41

1. At calculated approach speed (-5 to +10kts) 2. With engines spooled* * The engines are stabilized at the thrust setting required to maintain the desired airspeed and rate of descent