Performance Noter [NUR's Noter] Flashcards
Huske huske huske
Landing Distance (CLASS A), from 50 ft screen height.
πΏπ· Β· 0.6 OR πΏπ· / 1.67
Landing Distance available for WET
CLASS A
92%
ACN can exceed flexible PCN by __ %
10%
ACN can exceed rigid PCN by __ %
5%
Min available climb gradient 1st segment (OEI) 2 engine
Positive ROC
Min available climb gradient 1st segment (OEI) 3 engine
0.3%
Min available climb gradient 1st segment (OEI) 4 engine
0.5%
Min available climb gradient 2nd segment (OEI) 2 engine
2.4%
Min available climb gradient 2nd segment (OEI) 3 engine
2.7%
Min available climb gradient 2nd segment (OEI) 4 engine
3.0%
Min available climb gradient 3rd+4th segment (OEI) 2 engine
1.2%
Min available climb gradient 3rd+4th segment (OEI) 3 engine
1.5%
Min available climb gradient 3rd+4th segment (OEI) 4 engine
1.7%
Minimum speed to reach during 3rd segment, and maintain during 4th segment
1.25 Β· ππ
Max bank below 50 ft or Β½ wingspan (greater)
0Β°
Max bank below 400 ft
15Β°(with approval 20Β°)
Max bank above 400 ft
25Β°(with approval 30Β°)
Min. V1 speeds (VMCG and VR/VMBE)
No less than VMCG,
No more than VR or VMBE
VR for multi engine
VR for multi engine:
no less than V1,
1.05 VMC
1.10 VS1
VR for Sinlge engine
No less than VS1
V2 speeds
V2:
no less than 1.1 VMCA,
1.08VSR for 4 engine turbo props (and jets with provision)
1.13VSR for 2&3 engine turbo props and jets
Final takeoff speed (VFTO)?
Final takeoff speed (VFTO):
no less than 1.18 VSR
VREF (Class A and B)
Class A:
1.23 Β· VS0 or V_MCL
Class B:
1.3 Β· VS0 or V_MCL
Best range speed jets (tangent of drag/thrust required curve)
1.32 Β· πππ·
Best prop endurance
πππ
(V_X for props)
Best prop range
πππ·
Best jet endurance
πππ·
(V_X for Jets)
Best jet range
1.32 Β· πππ·
Gross to Net climb gradient reduction (2 eng)
0.8%
Gross to Net climb gradient reduction (3 eng)
0.9%
Gross to Net climb gradient reduction (4 eng)
1.0%
Min AEO landing climb gradient (CLASS A)
3.2%
Min OEI approach climb gradients (CLASS A) 2 engine
2.1%
Min OEI approach climb gradients (CLASS A) 3 engine
2.4%
Min OEI approach climb gradients (CLASS A) 4 engine
2.7%
Speed at 50 ft must _____? (twin engine)
not be less than greater of
1.20 Β· ππ1 or 1.10 Β· πππΆ
Speed at 50 ft must _____? (single engine)
must not be less than greater of:
1.20 Β· ππ1
AND NOT ANY VMC LIMIT (Due to single engine)
Speed for dynamic hydroplaning (takeoff)
9 Β· sqrt(psi)
Speed for viscous hydroplaning (landing)
7.7 Β· sqrt(psi)
Min. All Engine Operating climb gradient (Class B)
4%
(See CAP)
Min. One Engine Inop. climb gradient (CLASS B) at 1500 ft AGL
0.75%
(See CAP)
Minimum gross climb gradient after balked landing (CLASS B)
2.5%
(See CAP)
Minimum gross climb gradient for missed approach (Class B)
0.75%
(See CAP)
Maximum reduction of takeoff thrust allowed.
25%
(See CAP)
Normal Driftdown obstacle clearance
2000ft
STABILIZED Driftdown obstacle clearance
1000ft
Driftdown obstacle clearance above airport:
1500ft