Page 180 - Demo

REV 20
Page 66
A330
CHINA AIRLINES
2.40/66
REV 20
AOM Procedure
Table 1_ALL ENGINE TAKEOFF CLIMB GRADIENT (%)_AOMP*
CONF 2
TOGA & Climb Thrust 0 Wind/Sea Level
QNH = 1013.25 Air Condition ON Anti-Ice OFF
TOW (1,000 lbs)
Average Climb gradient**(%)
O A T / T F L E X * * * ( °C ) Correction
(∆ ISA per+10°C)
Airport pressure Altitude correction (per +1,000 ft) Up to 8,000 ft
400
8.8
- 0.2
- 0.3
420
8.1
- 0.2
- 0.3
440
7.5
- 0.2
- 0.3
460
6.9
- 0.2
- 0.2
- 0.3
480
6.4
- 0.3
500
5.9
- 0.1
- 0.2
507
5.7
- 0.2
*AOMP: Set Climb power and Acceleration at 1,000 ft AGL **Average Climb gradient: From lift-off until reaching climb speed. (250 kt or green dot speed, whichever is greater)After climb speed, the gradient will increase 3 %. ***Use OAT for full thrust takeoff; use TFLEX for reduced thrust takeoff.
Table 2_If Acceleration > 1,000 ft AGL (1,000 ft < Acc ≤ 4,000 ft )
- 0.1
Average Climb gradient* (%)
OA T/TFLEX(°C) Correction
(∆ ISA per+10°C)
Airport pressure Altitude correction (per +1,000 ft) Up to 8,000 ft
TOW (1,000 lbs)
Acceleration Altitude (AGL)
Up to 2,000'
Up to 3,000'
Up to 4,000'
400
15.1
13.4
12.5
- 0.2
- 0.3
420
13.8
12.3
11.6
- 0.2
- 0.3
440
12.7
11.4
10.7
- 0.2
- 0.3
460
11.7
10.5
9.9
- 0.2
- 0.3
480
10.7
9.6
9.1
- 0.2
- 0.3
500
9.8
8.8
8.3
- 0.1
- 0.2
507
9.5
8.5
8.1
- 0.1
- 0.2
*Average Climb gradient: From lift-off until reaching Acceleration Altitude. After climb speed, the climb gradient increase is negligible.
NADP1
Table 3_NADP 1 (1,500AGL Climb Power/ 3,000AGL Acceleration)
TOW (1,000 lbs)
Average Climb gradient* (%)
OA T/TFLEX(°C) Correction
(∆ ISA per+10°C)
Airport pressure Altitude correction (per +1,000 ft) Up to 8,000 ft
400
14.7
- 0.2
- 0.3
420
13.5
- 0.2
- 0.3
440
12.5
- 0.2
- 0.3
460
11.5
- 0.2
- 0.3
480
10.6
- 0.2
- 0.3
500
9.7
- 0.1
- 0.2
507
9.5
- 0.1
- 0.2
*Average Climb gradient: From lift-off until reaching 3,000 ft AGL. After climb speed, the climb gradient increase is negligible.
Note: Climb gradient (%) = rate of Climb ÷ Ground Speed ÷1.012