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Approved oils See SB CFMI 79-001 or GE specification D50TF1 Class B
Engine Limitations
A330-321
PW 4164
FAA Data Sheet
E36NE
A330-322
PW 4168
FAA Data Sheet
E36NE
A330-323
PW 4168A
FAA Data Sheet
E36NE
Static Thrust at Sea Level
• Take-off (5 mn)1 (flat rated 30º )
• maximum continuous
(flat rated 25º C)
64,500 lbs
55,800 lbs
68,600 lbs
59,357 lbs
68,600 lbs
59,357 lbs
Maximum Engine Speed
• N1 rpm (%)
• N2 rpm (%)
3,600 (101%)
10,450 (103%)
3,600 (101%)
10,450 (103%)
3,600 (101%)
10,450 (103%)
Maximum Gas Temperature
• Take-off (5mn)1
• Maximum Continuous
• Starting2
1,157º F (625º C)
1,112º F (600º C)
1,148º F (620º C)
1,157º F (625º C)
1,112º F (600º C)
1,148º F (620º C)
1,157º F (625º C)
1,112º F (600º C)
1,148º F (620º C)
Maximum Oil Temperature
(Supply Pump Outlet) ºC
• Continuous Operation
• Transient (15 mn max.)
• Minimum Oil Pressure (PSI)
325º F (163º C)
350º F (177º C)
70.0 psid (482.6
KPa )
325º F (163º C)
350º F (177º C)
70.0 psid (482.6
KPa )
325º F (163º C)
350º F (177º C)
70.0 psid (482.6 KPa )
Approved oils See P&W Service Bulletin 238, latest revision.
A46NM Revision 10 8 March 19, 2007
Engine Limitations
A330-341
Trent 768-60
FAA Data Sheet
E39NE
A330-342
Trent 772-60
FAA Data Sheet
E39NE
A330-343
Trent 772B-60
FAA Data Sheet
E39NE
Static Thrust at Sea Level
• Take-off (5 mn)1 (flat rated 30º )
• maximum continuous
(flat rated 25º C)
67,500 lbs
60,410 lbs
71,100 lbs
63,560 lbs
71,100 lbs
63,560 lbs
Maximum Engine Speed
• N1 rpm (%)
• N2 rpm (%)
3,861 (99%)
10,611 (100%)
3,861 (99%)
10,611 (100%)
3,861 (99%)
10,611 (100%)
Maximum Gas Temperature
• Take-off (5mn)1
• Maximum Continuous
• Starting2
1,652º F (900º C)
1,562º F (850º C)
1,562º F (850º C)
1,652º F (900º C)
1,562º F (850º C)
1,562º F (850º C)
1,652º F (900º C)
1,562º F (850º C)
1,562º F (850º C)
Maximum Oil Temperature
(Supply Pump Outlet) ºC
• Continuous Operation
• Transient (15 mn max.)
• Minimum Oil Pressure (PSI)
374º F (160º C)
374º F (175º C)
24.0 psid
374º F (160º C)
374º F (175º C)
24.0 psid
374º F (160º C)
374º F (175º C)
24.0 psid
Approved oils -Aeroshell Turbine Oil (Royco) 500, 555, 560, Mobil Jet Oil II 254,
291,Exxon Turbo Oil 2197
Table references:
(1) 10 minutes at take-off thrust allowed only in case of engine failure (at take-off or during go-around).
(2) 4 consecutive cycles of 2 minutes each.
Center of Gravity Limits: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
Datum: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
Leveling Means: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
Maximum Weight:
Model A330 Airplane A330-301/-321/-322/-341/-342 A330-301
Weight Variant 000
(Basic)
kg / lb
002
(MOD 42600)
kg / lb
001
(MOD 42200)
kg / lb
Maximum Take-off Weight, MTOW 212,000 / 467,460 212,000 / 467,460 184,000 / 405,720
Maximum Landing Weight, MLW 174,000 / 383,670 177,000 / 390,285 174,000 / 383,670
Maximum Zero Fuel Weight, MZFW 164,000 / 361,620 167,000 / 368,235 164,000 / 361,620
Model A330 Airplane A330-323/-343 A330-323
Weight Variant 020
(Basic)
kg / lb
022
(MOD 47785)
kg / lb
050
(MOD 51805)
kg / lb
052
(MOD 51807)
kg / lb
Maximum Take-off Weight, MTOW 230,000 / 507,150 233,000 / 513,765 230,000 / 507,150 233,000 /513,765
Maximum Landing Weight, MLW 185,000 / 407,925 187,000 / 412,335 185,000 / 407,925 187,000 /412,335
Maximum Zero Fuel Weight, MZFW 173,000 / 381,465 175,000 / 385,875 173,000 / 381,465 175,000 /385,875
Minimum Crew: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
　
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