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Cartes-fiches
TODR = TOD × 1.25
TORR = TOD × 1.0
TODR = TOD × 1.15
ASDR = TOD × 1.3
× 1.2
× 1.3
+5% for each 1% upslope (×1.05 per %)
× 1.15
+5% for each 1% downslope (×1.05 per %)
LDR = LD × 1.43
LDR = LD × 1.43 (LD = LDA × 0.7)
LDR = LD × 1.67 (LD = LDA × 0.6)
× 1.15
Compare AEO distance × 1.15 with OEI distance and use the greater value.
2 engines: Gross − 0.8%; 3 engines: Gross − 0.9%; 4 engines: Gross − 1.0%.
2 engines: ≥0%; 3 engines: ≥0.3%; 4 engines: ≥0.5%.
2 engines: ≥2.4%; 3 engines: ≥2.7%; 4 engines: ≥3.0%.
2 engines: ≥1.2%; 3 engines: ≥1.5%; 4 engines: ≥1.7%.
2 engines: ≥2.1%; 3 engines: ≥2.4%; 4 engines: ≥2.7%.
Net gradient = Gross gradient + 0.5%.
2000 ft.
VMCG: 1.05 VMC; V1: ≥1.1 VMC and ≥1.13 VS1G (or ≥1.2 VS without provision); VR: ≥V1 and ≥1.05 VMCA; V2: ≥1.18 VS1G.
V2 = 1.2 VS.
VR ≥ 1.1 VS1 or 1.05 VMC; V2 ≥ 1.2 VS1 or 1.1 VMC.
AEO TOD × 1.15. Compare this with the OEI distance and use the greater value.
TODA: maximum TODR × 1.5. ASDA: reverse thrust only when wet.
What factors are used for an unbalanced take-off?
TORR = TOD × 1.00; TODR = TOD × 1.15; ASDR = TOD × 1.3.
TOD × 1.25 = required.
Dry grass ×1.2; wet grass ×1.3.
2 engines: 0%; 3 engines: 0.3%; 4 engines: 0.5%.
2 engines: 2.4%; 3 engines: 2.7%; 4 engines: 3.0%.
2 engines: 1.2%; 3 engines: 1.5%; 4 engines: 1.7%.
Subtract the safety margin: 2 engines −0.8%; 3 engines −0.9%; 4 engines −1.0%.
0.75% OEI.
4% AEO.
OEI gross gradient + 0.5% margin.
What screen heights are shown for Class B take-off?
Dry: 50 ft;
½ wingspan + 60 m + 0.125 D.
What lateral obstacle clearance is required for a wingspan of 60 m or more?
90 m + 0.125 D.
Up to 600 m + 0.125 D.