曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

Specification: See
GE specification
D50TF1,
Class B
Oils conforming to
P&W Turbojet
engine Service
Bulletin 238, latest
revision.
-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.
Airspeed Limits
See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
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.
A46NM Revision 10 3 March 19, 2007
Maximum Weight:
Model A330-200 Airplane A330-201/-202/-203/-223/-243 A330-223
Weight Variant 020
(Basic)
kg / lb
050
(MOD 51802)
kg / lb
052
(MOD 51804)
kg / lb
Maximum Take-off Weight,
MTOW
230,000 / 507,150 230,000 / 507,150 233,000 / 513,765
Maximum Landing Weight,
MLW
180,000 / 396,900 180,000 / 396,900 182,000 / 401,300
Maximum Zero Fuel Weight,
MZFW
168,000 / 370,440 168,000 / 370,440 170,000 / 374,850
Minimum Crew: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
Number of Seats: The maximum number of passengers approved for emergency evacuation is:
375 passengers with a 3 pairs of Type A and 1 pair Type 1 exits configuration, and
379 passengers with a 4 pairs of Type A exits configuration.
Maximum Baggage:
Cargo Compartment Maximum Load
(kg / lb)
Forward 18,869 / 41,606
Aft 15,241 / 33,606
Rear 3,468 / 7,646
For the positions and the loading conditions authorized in each position (references of containers, pallets and associated weight) see
weight and Balance Manual: Airbus Document 00G080A0006/C2S for A330-200 airplanes.
Fuel Capacity:
3 Tank Airplane
Usable Fuel Unusable Fuel
Tank
liters gallons liters gallons
Wing 91,300 24,121 348 70
Center 41,560 10,980 83 21.9
Trim Tank 6,230 1,646 6 1.6
Total 139,090 36,746 437 115.5
Maximum Operating Altitude:
See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
Control Surface Movements:
See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
Manufacturer’s Serial Numbers:
See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
Import Requirements:
See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
Certification Basis (A330-200):
a. Part 25 of the FAR effective February 1, 1965, including the following:
• Amendments 25-1 through 25-63, amendments 25-65, 25-66, 25-68, 25-69, 25-73,
25-75, 25-77, 25-78, 25-81, 25-82, 25-84 and 25-85
• § 25.851 as amended by amendment 25-74
• The following sections of Part 25 of the FAR as amended through amendment 25-72:
A46NM Revision 10 4 March 19, 2007
FAR 25.21
FAR 25.29
FAR 25.111
FAR 25.147
FAR 25.177
FAR 25.181
FAR 25.205
FAR 25.307
FAR 25.331
FAR 25.341
FAR 25.343
FAR 25.345
FAR 25.351
FAR 25.361
FAR 25.373
FAR 25.395
FAR 25.397
FAR 25.415
FAR 25.459
FAR 25.571 (b)
FAR 25.613 (Vertical stabilizer only)
FAR 25.615 (Vertical stabilizer only)
FAR 25.693
FAR 25.723
FAR 25.729
FAR 25.731
FAR 25.733
FAR 25.735
FAR 25.772
FAR 25.779
FAR 25.783
FAR 25.933
FAR25.979
FAR 25.1093
FAR 25.1381
FAR 25.1419
FAR 25.1522
FAR 25.1533
FAR 25.1543
FAR 25.1551
FAR 25.1581
FAR 25.1583
FAR 25.1587
b. Part 25 of the FAR amendment 25-64 with the following exceptions:
• Cockpit seats will not meet FAR 25.562 amendment 25-64 but will meet FAR 25.561
• Compliance with 25.785(a), (b), and (c) at amendment 25-64 for front row seats in front of a bulkhead will be based on
ensuring a 35 inch free head strike envelope.
c. Special conditions in accordance with § 21.16 of the FAR.
1. Special conditions originally written for the A330-300 certification basis that are also included in the A330-200 certification
basis: (published in the Federal Register April 15, 1993, Docket No. NM-75, Special Conditions No. 25-ANM-69)
(1) Operation without Normal Electrical Power
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：航空資料2(136)