Page 179 - Demo

2.40/65
REV 17
A330
CHINA AIRLINES
REV 17
PAGE 65
1 ENGINE INOP APPROACH CLIMB GRADIENT % (After Miss Approach)
Gross Weight (1000 lb)
Per 1K ft correct
Airport OAT (°C)
CONF 3
CONF 2
CONF 1+F
up to 30
35
40
up to 30
35
40
up to 30
35
40
300
-0.65
9.9
9.3
8.6
10.4
9.7
9.1
10.8
10.2
9.7
320
-0.63
8.6
7.9
7.4
9.1
8.5
8.0
9.8
9.2
8.6
340
-0.60
7.4
6.8
6.3
8.2
7.7
7.2
8.9
8.2
7.6
360
-0.56
6.6
6.1
5.6
7.4
6.9
6.3
7.9
7.3
6.8
380
-0.53
5.9
5.4
4.9
6.6
6.1
5.5
7.1
6.5
6.0
400
-0.51
5.2
4.7
4.2
5.9
5.4
4.9
6.3
5.8
5.3
410
-0.50
4.9
4.3
3.9
5.5
5.0
4.5
6.0
5.5
5.0
420
-0.48
4.5
4.0
3.5
5.2
4.7
4.2
5.6
5.2
4.7
430
-0.46
4.2
3.7
3.3
4.9
4.4
3.9
5.3
4.9
4.4
440
-0.45
3.9
3.4
3.0
4.6
4.1
3.7
5.0
4.6
4.1
450
-0.44
3.6
3.2
2.7
4.3
3.8
3.4
4.7
4.3
3.9
460
-0.43
3.3
2.9
2.5
4.0
3.6
3.1
4.5
4.0
3.6
470
-0.43
3.1
2.6
2.2
3.8
3.3
2.9
4.2
3.8
3.4
480
-0.41
2.8
2.4
2.0
3.5
3.1
2.7
4.0
3.5
3.1
490
-0.40
2.6
2.2
1.8
3.3
2.8
2.4
3.7
3.3
2.9
500
-0.39
2.4
2.0
1.6
3.0
2.6
2.2
3.5
3.1
2.7
507
-0.39
2.2
1.8
1.4
2.9
2.5
2.1
3.4
3.0
2.6
Note:
1. All gradient calculation are based on airport pressure altitude 0 ft and AC Packs ON, Anti-Ice Off.
2. The gradient correction per 1,000 ft only applicable until pressure altitude is up to 8,000 ft.
3. Shadow means the Approach Climb Gradient is less than Limit Gross Gradient 2.1%.
4. The CONF shown in the table is the CONF after miss approach.