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AMM 12-14-32 revised by TR No 12-001. Adjust/correct as applicable.
Note: the instructions for the NLG pressure check are also given in SB
A320-32-1310 at original issue.
2.2. Perform a boroscopic inspection of the NLG upper support antirotation
lugs and the cylinder lugs, in accordance with AIRBUS
Technical Note 957.1901/05, dated October 18, 2005.
If any upper support anti-rotation lugs are found broken or cracked or if
the cylinder lugs are found to be missing: before next flight, apply all
necessary actions to get a serviceable NLG (contact AIRBUS Fax: 33 5
61 93 32 73).
All inspection results should be reported to AIRBUS.
Note: the instructions for the boroscopic inspection are also given in
SB A320-32-1310 at original issue.
3. For aircraft listed in the applicability paragraph that are equipped
with EMM BSCU standard L4.1 or L4.5:
3.1. At the latest of these two dates:
- Prior to the accumulation of 20 months, or 6000 flight hours, or 4500
flight cycles, since the aircraft first flight, whichever occurs first,
or
- Within the 6 months, or 1800 flight hours, or 1350 flight cycles,
following the effective date of this AD, whichever occurs first,
Perform a boroscopic inspection of the NLG upper support lugs and
4/5
cylinder lugs and apply corrective actions, if necessary, in accordance
with SB A320-32-1310 at original issue.
3.2. Repeat the inspection defined in above paragraph compliance 3.1
at intervals not exceeding 6 months or 1800 flight hours or 1350 flight
cycles, whichever occurs first and apply corrective actions, if
necessary, in accordance with SB A320-32-1310 at original issue.
- Installation of a NLG with new upper support anti-rotation lugs and new
cylinders lugs
Or
- Installation of a NLG for which it can be demonstrated that it was never
driven by a EMM BSCU L4.1 or L4.5
together with the installation of a EMM BSCU standard L4.8 or a non EMM
BSCU render void the requirements of this AD. No further action is
required by this AD.
4. For aircraft listed in the applicability paragraph that are equipped
with EMM BSCU standard L4.8 or a non EMM BSCU:
4.1. At the latest of these two dates:
- Prior to the accumulation of 20 months, or 6000 flight hours, or 4500
flight cycles, since the aircraft first flight, whichever occurs first,
or
- Within the 6 months, or 1800 flight hours, or 1350 flight cycles,
following the effective date of this AD, whichever occurs first,
Perform a boroscopic inspection of the NLG upper support lugs and
cylinder lugs and apply corrective actions, if necessary, in accordance
with SB A320-32-1310 at original issue.
4.2. Repeat the inspection defined in above paragraph compliance 4.1 at
intervals not exceeding 20 months or 6000 flight hours or 4500 flight
cycles, whichever occurs first and apply corrective actions, if
necessary, in accordance with SB A320-32-1310 at original issue.
- Installation of a NLG with new upper support anti-rotation lugs and new
cylinders lugs
Or
- Installation of a NLG for which it can be demonstrated that it was never
driven by EMM BSCU L4.1 or L4.5
renders void the requirements of this AD. No further action is required by
this AD.
Ref. Publications: AIRBUS Aircraft Maintenance Manual TR No 12-001 based on the Nov
01/05 revision
AIRBUS Aircraft Maintenance Manual 12-14-32
AIRBUS Technical Note reference 957.1901/05 dated October 18, 2005
AIRBUS AFM TR 4.02.00/33
AIRBUS AFM TR 4.02.00/34
5/5
AIRBUS Service Bulletin A320-32-1310 at original issue
or later approved revisions.
Remarks : 1. If requested and appropriately substantiated the responsible EASA
manager for the related product has the authority to accept Alternative
Method of Compliance (AMOCs) for this AD.
2. This AD was posted as PAD 06-071 for consultation on 22 March with a
comment period until 05 April 2006. The Comment Response Document
can be found at http://ad.easa.eu.int/ .
3. Enquiries regarding this AD should be addressed to Mr. M. Capaccio, AD
Focal Point, Certification Directorate, EASA.
E-mail: ADs@easa.europa.eu
4. For any question concerning the technical content of the requirements in
this AD, please contact AIRBUS - Fax 33 5 61 93 44 51
1/2
EASA AIRWORTHINESS DIRECTIVE
AD No : 2007-0213
Date: 07 August 2007
No person may operate an aircraft to which an Airworthiness Directive applies, except in accordance with the
requirements of that Airworthiness Directive unless otherwise agreed with the Authority of the State of Registry.
Type Approval Holder’s Name :
AIRBUS
Type/Model designation(s) :
　
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