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B's Republic E170/175 > SOP Ch 3 Operational Limits > Flashcards

SOP Ch 3 Operational Limits Flashcards

1
Q

Operational Limits

Max Takeoff and Landing Tailwind Component

A

10 knots

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2
Q

Operational Limits

Max Operating Altitude

A

41,000 feet

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3
Q

Operational Limits

Max Flap Extension Altitude

A

20,000 feet

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4
Q

Airspeed Limitations

Max Operation Airspeed

A

V MO (320 KIAS)

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5
Q

Airspeed Limits

Max Operating Mach Number

A

M MO (.82M)

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6
Q

Airspeed Limits
Turbulent Airspeed
Below 10,000 feet

A

250 KIAS

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7
Q

Airspeed Limits
Turbulent Airspeed
At or Above 10,000 feet

A

270 KIAS/.76M

Whichever is lower

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8
Q

Airspeed Limits

Maximum Tire Limit Ground Speed

A

195 Knots

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9
Q

Airspeed Limits

Maximum Windshield Wiper Operation Speed

A

250 KIAS

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10
Q 
Airspeed Limits
Maximum Gear Speed
Extension (V LOE)
Extended (V LE)
Retraction (V LOR)
A

250 KIAS

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11
Q

Flap Operating Limits

Flaps 1

A

230 KIAS

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12
Q

Flap Operating Limits

Flaps 2

A

215 KIAS

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13
Q

Flap Operating Limits

Flaps 3

A

200 KIAS

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14
Q

Flap Operating Limits

Flaps 4

A

180 KIAS

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15
Q

Flap Operating Limits

Flaps 5

A

180 KIAS

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16
Q

Flap Operating Limits

Flaps FULL

A

165 KIAS

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17
Q

Flap Operating Limits

The use of Flaps 4 is prohibited during…

A

Approach and landing

18
Q

Flap Operating Limits

Flaps should never be extended below…

A

Green dot

19
Q

Flap Operating Limits

When flaps are extended…

A

Do not hold in ICING conditions

20
Q

Design Maneuvering Speed (V A)

A

below 240 KIAS

21
Q

Definition of Icing Conditions (3)

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

A
  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
22
Q

Engine and Wing Anti-Ice System Operations

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

A

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

23
Q

Minimum Fuel Tank Temperature

A

-37*C

24
Q

Maximum Fuel Imbalance

A

790 lbs

25
Q

Pressurization

Max altitude for single pack operation

A

31,000 feet

26
Q

EICAS Engine Limit Display Markings

Red

A

Maximum and Minimum Limitations

27
Q

EICAS Engine Limit Display Markings

Amber

A

Caution Range

28
Q

EICAS Engine Limit Display Markings

Green

A

Normal Operating Range

29
Q

Engine Thrust

Use of reduced thrust takeoff procedure is NOT allowed on…

A

Runways contaminated with standing water, slush, snow or ice

30
Q

APU Operational Limits

Start

A

30,000 feet

31
Q

APU Operational Limits

Electrical

A

33,000 feet

32
Q

APU Operational Limits

Bleed

A

15,000 feet

33
Q

APU Operation Limits

To Assist Engine Start

A

21,000 feet

34
Q

Single Engine Taxi

Single engine taxi is NOT authorized when (5):

A
  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
35
Q

Single Engine Taxi
After Landing
If starting the APU…

A

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

36
Q

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

A

2; shutting down an engine

37
Q

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

A

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

38
Q

FMS Speeds

FMS speeds may only be used during

A

Normal flight operations

39
Q

FMS Speeds

Whenever a QRH procedure requires an airspeed correction…

A

The use of FMS speed is PROHIBITED

40
Q

Stabilized Approach Criteria

From 1,000 feet above the TDZE, the aircraft will be (3):

A
  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)
41
Q

Stabilized Approach Criteria

From 500 feet above TDZE, the aircraft will be (2):

A
  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

B's Republic E170/175 (3 decks)

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