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FAA Compliance findings to the A330 RML:
The FAA has accepted:
(1) Model A330-323 aircraft in the Airbus as-delivered configuration for msn 524 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 G01M03003568 issue 2, dated
June 24, 2003) that the RML modifications applicable to model A330-323 aircraft are either part of the FAA approved type design (ref.
AI/EA-N 415.1630/99 Issue 1, dated July 20, 1999), required to be installed at aircraft delivery by DGAC/EASA AD, or required to be
installed by Airbus on all A330-323 aircraft at time of delivery.
(2) 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.
FAA Required Modification List(RML) for the Airbus Model A330 Aircraft:
The RML for the A330 is composed of items 1A through 40B as listed on the following pages.
A46NM Revision 4 15 March 21, 2000
A330 Required Modification List (RML)
RML
#
DGAC CN # Mod # Mandatory Action Applicable To: S/B # S/B REV(s) Compliance Time
1A 1996-006-
024(B)R1
42409 FUSELAGE -
REINFORCE JOINT
AT FRAMES 48 - 53.2
Airplanes without
mod 43475 or
without SB A330-
21-3027
53-3015 1 or higher Frames 53/53.1/53.2: Prior to
5800 total flight cycles. For
frames 48 to 52: Prior to
15600 total flight cycles.
1B 1996-006-
024(B)R1
42409 FUSELAGE -
REINFORCE JOINT
AT FRAMES 48 - 53.2
Airplanes with
mod 43475 or
with SB A330-21-
3027
53-3015 1 or higher Frames 53/53.1/53.2 prior to
5300 total flight cycles. For
frames 48 to 52 prior to
14100 total flight cycles.
2 1997-265-
056(B)R1
N/A REVISE AMM
AIRWORTHINESS
LIMITS.
ALL Model A330
Airplanes
AMM
CHAPTER
5
8 or higher Prior to C of A Issuance
3 1998-539-
088(B)
N/A REPLACE
FRANKENJURA
EYE-END ON
ELEVATOR
SERVOCONTRLS
ALL Model A330
Airplanes
AOT 27-24 1 or higher Prior to 7/09/99 or C of A
Issuance; whichever occurs
later
4 1999-111-
093(B)
45870 AND
46231 AND
46891
INSTALL WIRING
FOR E-BRAKE
SHUTOFF VALVE
ALL Model A330
Airplanes
29-3054
AND 32-
3083R2
3054: 0 or
higher
3083: 2 or
higher
Prior to 7/31/01 or C of A
Issuance; whichever occurs
later
5 1999-123-
092(B)
43724, OR
44661, OR
44662
FLIGHT
MANAGEMENT
COMPUTER
REPLACEMENT
ALL Model A330
Airplanes
22-3011,
OR 22-
3009, OR
22-3010
All SB’s
revision 1
or higher
Prior to 6/30/99 or C of A
Issuance; whichever occurs
later
6 1999-142-
097(B)
46170,
OR
46596
FLIGHT CONTROL
UNIT CHANGE
Airplanes with
Mod. 44887 OR
with SB 22-3012
22-3021,
OR 22-3020
1 or higher Prior to 6/30/99 or C of A
Issuance; whichever occurs
later
7 1999-144-
094(B)R1
45977 REPLACE RAT
ACTUATOR
Airplanes with
Sundstrand RAT
29-3057 1 or higher Prior to 12/31/00 or C of A
Issuance; whichever occurs
later
8 1999-331-
098(B)
42447 REPLACE NLG
HINGE FITTING
BRACKETS
ALL Model A330
Airplanes
52-3046 1 or higher Prior to 01/21/01 or C of A
Issuance; whichever occurs
later
9A 1999-350-
100(B)R1
46904,
AND
46905
REPLACE PIVOT
PINS & BELLCRANK
ASSEMBLIES
-202, -223,-243, -
323, -343
32-3095 1 or higher The Later of (a) and (b):
(a) Prior to 4800 total flight
cycles or within 5 years since
new; which ever occurs first;
and
(b) Prior to 06/08/01
9B 1999-350-
100(B)R1
46902,
AND
46903
REPLACE PIVOT
PINS & BELLCRANK
ASSEMBLIES
ALL Model A330
Airplanes
32-3096 1 or higher Prior to 10 years since new or
C of A Issuance; whichever
occurs later
9C 1999-350-
100(B)R1
46904,
　
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