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• Cabin furnishings, equipment and arrangement shall conform to the following specification:
• 00F252K0005/C01 for cabin seats,
• 00F252K0006/C01 for galley,
A46NM Revision 10 6 March 19, 2007
• 00F252K0020/C01 for cabin attendant seats.
Hydraulic Fluids:
See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
Auxiliary Power Unit (APU):
See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
Tires:
See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
Service Information:
See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
Airplane Flight Manual:
Airplane operation must be in accordance with the EASA Approved Airplane Flight Manual (AFM), US version, listed below, or later
EASA approved revision applicable to the specific airplane model, modification status and serial number.
All placards required by either the AFM, the applicable operating rules, or the certification basis must be installed in the airplane.
Model A330 Aircraft Airbus Document Reference Revision No. Date
-201 STL 33000 1 March 10, 2003
-202 AI/ST-F 33000 2 January 6, 1999
-203 AI/ST-F 33000 1 October 24, 2002
-223 AI/ST-F 33000 2 January 6, 1999
-243 AI/ST-F 33000 2 March 15, 2000
Environmental requirements for noise:
See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
II. Airbus A330-300 Series Transport Category Airplanes:
Airbus A330-301 - approved October 21, 1993
Airbus A330-321 - approved June 21, 1999
Airbus A330-322 - approved June 21, 1999
Airbus A330-323 - approved October 8, 1999:
Airbus A330-341 – approved December 21, 2000
Airbus A330-342 - approved December 21, 2000
Airbus A330-343 - approved December 21, 2000
Model: Definition of Reference Airplane by Airbus Documents:
A330-301 FAA A330-301 Type Design, ref. AI/EA-N 415.1181/96 Issue 3, dated July 16, 1997 for type definition
and Type Certification Standard Equipment list, ref. 00G000A0101/C0S.
A330-321 FAA A330-321 Type Design, ref. AI/EA-N 415.1184/96 Issue 3, dated June 25, 1998 for type definition
and Type Certification Standard Equipment list, ref. 00G000A0121/C0S.
A330-322 FAA A330-322 Type Design, ref. AI/EA-N 415.1183/99 Issue 3, dated June 25, 1998 for type definition
and Type Certification Standard Equipment list, ref. 00G000A0121/C0S.
A330-323 FAA A330-323 Type Design, ref. AI/EA-N 415.1630/99 Issue 1, dated July 20, 1999 for type definition
and Type Certification Standard Equipment list, ref. 00G000A0123/C3S.
A330-341 FAA A330-341 Type Design, ref. AI/EA-N 415.1187/96 Issue 2, dated December 11, 1998 for type
definition and Type Certification Standard Equipment list, ref. 00G000A0141/C0S.
A330-342 FAA A330-341 Type Design, ref. AI/EA-N 415.1182/96 Issue 2, dated December 11, 1998 for type
definition and Type Certification Standard Equipment list, ref. 00G000A0141/C0S.
A330-343 FAA A330-343 Type Design, ref. AI/EA-N 415.2027/99 Issue 1, dated October 22, 1999 for type
definition and Type Certification Standard Equipment list, ref. 00G000A0143/C3S.
A46NM Revision 10 7 March 19, 2007
Engines:
Airplane Model: Engine Model: Engine Type Certificate:
A330-301 Two GE-CF6-80E1A2 turbojet engines FAA-Type Certificate E41NE
A330-321 Two PW 4164 turbojet engines FAA-Type Certificate E36NE
A330-322 Two PW 4168 turbojet engines FAA-Type Certificate E36NE
A330-323 Two PW 4168A turbojet engines FAA-Type Certificate E36NE
A330-341 Two RR Trent 768-60 turbojet engines FAA-Type Certificate E39NE
A330-342 Two RR Trent 772-60 turbojet engines FAA-Type Certificate E39NE
A330-343 Two RR Trent 772B-60 turbojet engines FAA-Type Certificate E39NE
Fuel: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
Engine Limits:
Engine Limitations
A330-301
CF6-80E1A2
FAA Data Sheet
E41NE
Static Thrust at Sea Level
• Take-off (5 mn)1 (flat rated 30º)
• maximum continuous
(flat rated 25º C)
64,530 lbs
60,400 lbs
Maximum Engine Speed
• N1 rpm (%)
• N2 rpm (%)
3,835 (115.5%)
11,105 (113%)
Maximum Gas Temperature
• Take-off (5mn)1
• Maximum Continuous
• Starting2
1,787º F (975º C)
1,724º F (940º C)
1,598º F (870º C)
Maximum Oil Temperature
(Supply Pump Outlet) ºC
• Continuous Operation
• Transient (15 mn max.)
• Minimum Oil Pressure (PSI)
320º F (160º C)
347º F (175º C)
10.0 psid (69 KPa )
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