Day 2 Flashcards

1
Q

TORA / Stopway / clearway

A
  • TORA: take-off run available: runway length available for the ground roll
  • stopway: area beyond runway used for rejected take-offs
  • Clearway: area beyond runway which can be used for the initial climb to screen height. It is free of obstructions.
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2
Q

Screenheights

A

Screen height dry: 35’

Screen height wet: 15’

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3
Q

TODA / ASDA

A
  • TODA: take-off distance available
  • ASDA: accelerated-stop distance available

TODA: TORA+clearway
ASDA: TORA+stopway

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4
Q

Balanced V1/field

A

Balanced V1: TODR = ASDR

Balanced field: TODA = ASDA

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5
Q

V1

A
-  Decision speed: max speed during t/o that the pilot can stop within ASDA, min speed during t/o that pilot can continue T/o with N-1 and achieve the screen height
                            V1 must be:
- greater than Vmcg
- less than Vmbe
- less or equal to Vrotate
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6
Q

Vr

A

The speed at which the rotation of the a/c should be initiated

            Vr can not be less than:
  • V1
  • 1,05 Vmu SE / 1,1 Vmu AE (Minimum unstick speed +5% (SE) +10% (All Engines))
  • 1,05 x Vmca (Minimum control speed airborne) +5%
        Vr can not be greater than
  • Max tyre speed
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7
Q

EPST rotation

A

TO Pitch: 15 degrees
N-1 TO Pitch: 12/13 degrees
Rotation rate: 3 degrees/second
N-1 Rotation rate 2 degrees/second

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8
Q

V2

A

The take-off speed which must be attained at the screen height at the end of the TODR. (Best N-1 ANgle of climb speed, and is a minimum speed for flight until at least 400’ AGL)

        V2 must be greater than:
  • 1G stall speed
  • 1,1 Vmca
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9
Q

Take off Segments

A

First segment:

  • 35’ screen height > gear fully retraced
  • Min req: Positive climb

second segment;

  • gear fully retracted > N-1 Level off Height
  • Min req: 2.4% climb

Third segment:

  • level acceleration > flaps retracted
  • min req: positive climb

Final(fourth) segment:

  • flaps retracted > at N-1 final climb speed = Flaps up manouevring speed
  • min req: 1.2% climb
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10
Q

Runway conditions

A

DRY runway: runway whose surface is free of visible moisture and not contaminated within the area intended to be used

WET Runway: runway whose surface is covered by any visible dampness or water up to and including 3mm deep within the area to be used

CONTAMINATED Runway: A runway of which a significant portion (>25%) of it’s surface within the length and width being used is covered by one or more of the substances listed under the runway surface condition descriptors: compacted, dry and wet snow, frost, ice, slush, standing water, wet ice

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11
Q

Landing distance dry/wet

A

Dry scheduled LDR: demonstrated distance + 67%

Wet scheduled LDR: dry scheduled LDR + 15%

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12
Q

Missed APP climb gradients

A

Approach climb (2.1%)

  • approach configuration (Gear up/Flaps 15)
  • One engine inoperative

Landing climb (3.2%)

  • landing configuration (Gear down, Flaps 40)
  • Both engines at max thrust
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13
Q

Formula’s

A
Crosswind = wind angle, e.g.
60 Deg = Full
45 Deg = 3 quarters
30 Deg = Half
15 Deg = Quarter
Vref = 0,5 x HWC + full gust increment
Vref = (min +5 / max +15)

Calculation table 100% TWC/HWC

ROUND OFF: V1 down VR up V2 up

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14
Q

RVSM Reduced Vertical Seperation Minima

A

RVSM Airspace 28.500’ - 41.500’
- ( FL290 - FL410)

Required equipment:

  • two independent altitude measurement systems
  • an altitude alerting system
  • AP with ALT HOLD function
  • A transponder with altitude raporting system
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15
Q

TCAS

A
  • open (white) diamond: other traffic
  • closed (white) diamond: proximate traffic
  • yellow round: Traffic advisory (TA) (40seconds)
  • red square: Resolution advisory (RA) (25 seconds)
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16
Q

Situational awareness

A

Definition: Continuous extraction of information, the integrarion of this information and using that information to create a mutual mental picture.

  • Notice: extracting information via sensory inputs
  • Understand: processing this information with the use of precious knowledge
  • Think ahead: decision and reactions are the outcome of this process (ANC)
17
Q

MEA / MOCA / every situation

A
  • MEA: minimum enroute altitude: ensures terrain clearance and radio perception 5 nm each side of the airway
  • MOCA: minimum obstacle clearance altitude: ensures terrain clearance

IN EVERY SITUATION 1000’ clearance and in MOUNTAINOUS AREAS 2000’ clearance

18
Q

MORA / MGA / altitude

A
  • MORA: minimum off-route altitude: 10nm from each side of airway
  • MGA: minimum grid altitude: ensures terrain clearance within specified LAT/LONG

1000’ clearance up to 6000’, than 2000’ clearance

19
Q

MSA

A

Minimum sector altitude

  • 25 NM radius around Aerodrome or Navaid
  • provides 1000’ clearance above terrain
  • man made obstacles up to 300’ are not included
20
Q

Cold temperature correction

A

In cold air TRUE ALT is LOWER than INDICATED ALT

  • Only correct when temperature is below 0 degrees
  • to correct: 4% height increase for every 10 degrees below ISA
21
Q

GPWS Warning

A

+2000 feet and above = RED 🔴

  • 500 > +2000 feet = YELLOW 🟡
  • 2000 > -500 feet = GREEN 🟢
  • 2000 and below = BLACK ⚫️ NOT shown
22
Q

Calculate NM REQ for descent

A

(DELTA FL x 3) + 4 + 2

\+4 = speed 300 to 250
\+2 = speed 250 to final config
23
Q

All Engines pitch/ power table

A
CLEAN - 250     
-    2.6 Pitch / 62% Power
Clean - 220 (FUMS)
-    5 Pitch / 58% Power
Flaps 1, speed 1, 190
-    5.5 Pitch / 60% Power
Flaps 5, speed 5, 170
-    6 Pitch / 60% Power
Gear down, flaps 15, speed 15-160
-    6 Pitch / 70% Power
Gear down, flaps 30, FAS - 140 on ILS
-    1 Pitch / 56% Power
24
Q

N-1 Pitch Power table

A
CLEAN - 250     
-    2.6 Pitch / 72% Power
Clean - 220 (FUMS)
-    5 Pitch / 68% Power
Flaps 1, speed 1, 190
-    5 Pitch / 70% Power
Flaps 5, speed 5, 170
-    6 Pitch / 70% Power
Gear down, flaps 15, speed 15-160
-    7 Pitch / 82% Power
Gear down, flaps 30, FAS - 150 on ILS
-    3 Pitch / 70% Power
25
Q

Noise abatement procedures

A

Thrust Reducti / Acceleration
NADP1 1500’ 3000’
NADP2 1500’ 1500’

26
Q

Stabilized APP

A

Sop-33

27
Q

Standard emergency briefing

A

Sop-15