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(2) Electronic Flight Control System (EFCS) failures and Mode Annunciation
(3) Command Signal Integrity
(4) Protection From Lightning and Unwanted Effects of High Intensity Radiated Fields (HIRF)
(5) Interaction of Systems and Structures
(6) Design Dive Speed
(7) Design Maneuver Requirements
(8) Limit Pilot Forces
(9) Tail plane Tank Emergency Landing Loads
(10) Limit Engine Torque
(11) Flight Characteristics
(12) Flight Envelope Protection
(13) Side Stick Controllers
(14) Computerized Airplane Flight Manual (AFM) Performance Information
2. Special condition for the optional installation of the Lower Deck Mobile Crew Rest Compartment:
(published in the Federal Register on January 6, 2005, Docket No. NM287, Special Condition No. 25-281-SC)
Lower Deck Mobile Crew Rest (LD-MCR) Compartment (optional installation)
d. Part 34 of the FAR, effective September 10, 1990, including Amendment 34-1.
e. Part 36 of the FAR, effective December 1, 1969, including Amendments 36-1 through 36-21.
A46NM Revision 10 5 March 19, 2007
f. The technical requirements are complemented by the following guidance material:
For precision approach and landing,
1. AC 120-29
2. AC 120-28C
and for the automatic flight control system
1. AC 20-57A for automatic landing
2. AC 25.1329-1A for cruise
g. Equivalent safety findings have been made in accordance with FAR 21.21(b)(1) for the following paragraphs of the FAR:
(1) 25.335(d) for design airspeeds
(2) 25.345 for high lift devices
(3) 25.349 for control surface loads
(4) 25.351(b) for unsymmetrical loads
(5) 25.371 for gyroscopic loads
(6) 25.373 for speed control devices
(7) 25.101(I); 25.105(c)(1); 25.109(a)(b)(c)(d)(e)(f); 25.113(a)(b)(c); 25.115(a); 25.735(f)(g)(h)(b) for rejected
takeoff and landing performance
(8) 25.933(a)(1)(ii), 25.1309(b)(1) for flight critical thrust reverser
(9) 25.1203(d) for turbine overheat detection (RR Trent 700 powered A330-243 only)
(10) 25.1305(c)(6) Warning means for engine fuel filter contamination (RR Trent 700 powered A330-243 only)
(11) 25.1305; 25.1501(b) for APU system flight deck instrumentation
h. Optional requirements elected:
• 25.801 for ditching.
• 25.1419 for icing.
Note 1: Compliance with the FAA Required Modification List for Airbus Model A330 Aircraft as included under the Import
Requirements section of TCDS Revision 4, dated March 21, 2000 or later TCDS revision, is necessary for an A330 aircraft to be found
in a condition for safe operation.
• The FAA has accepted Model A330-223 aircraft in the Airbus as-delivered configuration for msn 609 and on as compliant with
the applicable modifications of the A330 RML. FAA acceptance is based on the Airbus statement to the FAA (ref. Airbus
letter EAL G03D0415493, dated July 9, 2004) that the RML modifications applicable to model A330-223 aircraft are either
part of the FAA approved type design (ref. AI/EA-N 415.1223/98 Issue 2, dated August 20, 1998), required to be installed at
aircraft delivery by DGAC/EASA AD, or required to be installed by Airbus on all A330-223 aircraft at time of delivery.
The Direction Generale de 'Aviation Civile (DGAC) of France originally type certificated the Airbus Model A330-200 series airplanes
under its type certificate number DGAC-F TC 184. The FAA validated this product under U.S. Type Certificate Number A46NM.
Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of DGAC.
Production Basis:
See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
Equipment:
• The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in
the aircraft for certification.
• The following Airbus Documents defines the set of modifications which comprise the FAA certificated type design. These
documents contain certain modifications determined necessary for FAA certification, including installation of ozone converters,
fuel system improvements and thrust reverser modifications.
• EAL 415.1338/02 Issue 1, dated November 6, 2002 for the A330-201
• AI/EA-N 415.0531/98 Issue 3, dated May 25, 1998 for the A330-202
• AI/EAL 415.1988/01 Issue 2, dated August 5, 2001 for the A330-203
• AI/EA-N 415.1223/98 Issue 2, dated August 20, 1998 for the A330-223
• AI/EA-N 415.2406/98 Issue 1, dated December 11, 1998 for the A330-243
• Equipment approved for installation is listed in the Certification Standard Equipment List
• 00G000A0102/C0S for the A330-202.
• 00G000A0123/C0S for the A330-223.
• 00G000A0143/C0S for the A330-243.
　
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