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A330-202
A330-203
A330-301
Kerosene (conform to GE specification D50TF2
with current exception of JP4 and JET B)
ASTM D
1655 (JET A)
(JET A1)
AIR 3405C DERD
2494/2453
A330-223
A330-321
A330-322
A330-323
Fuel and fuel additives conforming to the latest applicable issue of FAA approved Pratt & Whitney Turbojet
Engine Service Bulletin 2016 may be used separately or mixed in any proportions without adversely affecting the
engine operation or power output.
A330-243
A330-341
A330-342
A330-343
Approved fuel and additives are identified in the relevant Operating instructions defined in the Rolls Royce
Manual F-Trent – A330
(a) Additives: According to GE "Specific Operating Instructions", installation manual. The above mentioned fuels are also suitable for
the APU.
Airspeed Limits (Indicated Airspeed, IAS, unless otherwise stated):
• Maximum Operating Limit Speed/Mach, VMO/MMO 330 KIAS / .86
• Design Diving Speed, VD 365 KIAS / .93
• Design Maneuvering Speed, VA Refer to AFM Performance Section
• Maximum Flaps/Slats Extended Speed or Operating Speed, VFE
Configuration Slats/Flaps/Ailerons º VFE (kt)
1
1 + F
16/0/0
16/8/0
16/8/5
240
215
205
Intermediate Approach
Take-off
Take-off
2 20/14/10 196 Take-off and Approach
3 23/22/10 186 Take-off, Approach, and
Landing
FULL 23/32 180 Landing
• Minimum Control Speed, VMC Refer to AFM performance Section.
(Performance Engineering Program/OCTOPUS)
Landing Gear Speeds:
• Maximum Speed with Landing Gear Operating (Extension and Retraction) VLO 250 KIAS / .55M
• Maximum Speed with Landing Gear Locked Down, VLE 250 KIAS / .55M
• Tire Limit Speed (Ground Speed) 203 KIAS (235mph)
Center of Gravity Limits: Refer to EASA-Approved Airplane Flight Manual, US Version, Limitations Section for
center of gravity envelope. Note: 0% MAC is located 1359.59 in. (34.532m) from the datum line
Datum: The aircraft reference zero datum point is located 251.29 in. (6.3825 m) forward of the nose
section, 275.6 in. (7m) under the fuselage centerline (datum line).
Leveling Means: Inclinometer on cabin seat track rails (refer to WBM chapter 1.80).
Minimum Crew: 2 - Pilots
Maximum Operating Altitude Basic: 41,100 feet (12,527 m) slats and flaps retracted (clean)
Option: 41,450 feet (12,634 m) slats and flaps retracted (clean) with modification 52536
20,000 feet (6,096 m) slats or slats/flaps extended.
A46NM Revision 10 13 March 19, 2007
Control Surface Movements: (Total one-way travel in each direction of each movable control surface on the aircraft.)
Control Surface Maximum Travel
Aileron +25 /- 25º
#1 Spoilers Speed Brake 23º
Lift Dumper 35º
#2,3 Spoilers Roll 35º
Speed Brake 30º
Lift Dumper 50º
#4,5,6 Spoilers Roll 35º
Speed Brake 30º
Lift Dumper 50º
Aileron Droop 10º
Flaps 32º
Slats 23º
Stabilizers +2º/-14º
Elevator +15º/-30º
Rudder +30º/-30º
Environmental requirements for noise:
ICAO Annex 16 Volume 1 – Chapter 3, or Chapter 4 with Modification 55005.
Manufacturer’s Serial Numbers/Production Basis:
A330 aircraft, all series and models, are produced in France under production approval FR.21G.0035 (formerly FG 035) issued by the
DGAC (on behalf of EASA) to Airbus.
Import Requirements:
The FAA can issue a U.S. airworthiness certificate based on an French Export Certificate of Airworthiness (Export C of A) signed by a
representative of the Direction Generale de 'Aviation Civile (DGAC) of France on behalf of the European Community. The Export C of
A should contain the following statement (in the English language): “The aircraft covered by this certificate has been examined, tested,
and found to conform to the Type Design approved under FAA Type Certificate No. A46NM as defined in TCDS A46NM revision 4 (or
later revision) and to be in condition for safe operation."
The U.S. airworthiness certification basis for aircraft type certificated under FAR Section 21.29 and exported by the country of
manufacture is FAR Section 21.183(c) or 21.185(c). The U.S. airworthiness certification basis for aircraft type certificated under FAR
Section 21.29 exported from countries other than the country manufacture (e.g., third party country) is FAR Sections 21.183(d) or
21.185(b). These sections provide that U.S. airworthiness certificates are issued only if the Administrator finds “that the aircraft
conforms to the type design and is in a condition for safe operation.” Notwithstanding that FAR sections 21.183(d) and 21.185(b) do not
　
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