Performance Noter [NUR's Noter] Flashcards

Huske huske huske

1
Q

Landing Distance (CLASS A), from 50 ft screen height.

A

𝐿𝐷 · 0.6 OR 𝐿𝐷 / 1.67

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2
Q

Landing Distance available for WET
CLASS A

A

92%

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3
Q

ACN can exceed flexible PCN by __ %

A

10%

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4
Q

ACN can exceed rigid PCN by __ %

A

5%

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5
Q

Min available climb gradient 1st segment (OEI) 2 engine

A

Positive ROC

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6
Q

Min available climb gradient 1st segment (OEI) 3 engine

A

0.3%

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7
Q

Min available climb gradient 1st segment (OEI) 4 engine

A

0.5%

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8
Q

Min available climb gradient 2nd segment (OEI) 2 engine

A

2.4%

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9
Q

Min available climb gradient 2nd segment (OEI) 3 engine

A

2.7%

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10
Q

Min available climb gradient 2nd segment (OEI) 4 engine

A

3.0%

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11
Q

Min available climb gradient 3rd+4th segment (OEI) 2 engine

A

1.2%

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12
Q

Min available climb gradient 3rd+4th segment (OEI) 3 engine

A

1.5%

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13
Q

Min available climb gradient 3rd+4th segment (OEI) 4 engine

A

1.7%

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14
Q

Minimum speed to reach during 3rd segment, and maintain during 4th segment

A

1.25 Β· 𝑉𝑆

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15
Q

Max bank below 50 ft or Β½ wingspan (greater)

A

0Β°

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16
Q

Max bank below 400 ft

A

15Β°(with approval 20Β°)

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17
Q

Max bank above 400 ft

A

25Β°(with approval 30Β°)

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18
Q

Min. V1 speeds (VMCG and VR/VMBE)

A

No less than VMCG,
No more than VR or VMBE

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19
Q

VR for multi engine

A

VR for multi engine:
no less than V1,
1.05 VMC
1.10 VS1

20
Q

VR for Sinlge engine

A

No less than VS1

21
Q

V2 speeds

A

V2:
no less than 1.1 VMCA,
1.08VSR for 4 engine turbo props (and jets with provision)
1.13
VSR for 2&3 engine turbo props and jets

22
Q

Final takeoff speed (VFTO)?

A

Final takeoff speed (VFTO):
no less than 1.18 VSR

23
Q

VREF (Class A and B)

A

Class A:
1.23 Β· VS0 or V_MCL

Class B:
1.3 Β· VS0 or V_MCL

24
Q

Best range speed jets (tangent of drag/thrust required curve)

A

1.32 Β· 𝑉𝑀𝐷

25
Q

Best prop endurance

A

𝑉𝑀𝑃
(V_X for props)

26
Q

Best prop range

A

𝑉𝑀𝐷

27
Q

Best jet endurance

A

𝑉𝑀𝐷
(V_X for Jets)

28
Q

Best jet range

A

1.32 Β· 𝑉𝑀𝐷

29
Q

Gross to Net climb gradient reduction (2 eng)

30
Q

Gross to Net climb gradient reduction (3 eng)

31
Q

Gross to Net climb gradient reduction (4 eng)

32
Q

Min AEO landing climb gradient (CLASS A)

33
Q

Min OEI approach climb gradients (CLASS A) 2 engine

34
Q

Min OEI approach climb gradients (CLASS A) 3 engine

35
Q

Min OEI approach climb gradients (CLASS A) 4 engine

36
Q

Speed at 50 ft must _____? (twin engine)

A

not be less than greater of

1.20 Β· 𝑉𝑆1 or 1.10 Β· 𝑉𝑀𝐢

37
Q

Speed at 50 ft must _____? (single engine)

A

must not be less than greater of:

1.20 Β· 𝑉𝑆1

AND NOT ANY VMC LIMIT (Due to single engine)

38
Q

Speed for dynamic hydroplaning (takeoff)

A

9 Β· sqrt(psi)

39
Q

Speed for viscous hydroplaning (landing)

A

7.7 Β· sqrt(psi)

40
Q

Min. All Engine Operating climb gradient (Class B)

A

4%

(See CAP)

41
Q

Min. One Engine Inop. climb gradient (CLASS B) at 1500 ft AGL

A

0.75%

(See CAP)

42
Q

Minimum gross climb gradient after balked landing (CLASS B)

A

2.5%

(See CAP)

43
Q

Minimum gross climb gradient for missed approach (Class B)

A

0.75%

(See CAP)

44
Q

Maximum reduction of takeoff thrust allowed.

A

25%

(See CAP)

45
Q

Normal Driftdown obstacle clearance

46
Q

STABILIZED Driftdown obstacle clearance

47
Q

Driftdown obstacle clearance above airport: