GOODRICH carbon brake - Reduction of performances
<P>GOODRICH carbon brake - Reduction of performances</P><P>**** Hidden Message *****</P> AIRWORTHINESS DIRECTIVE<BR>No F-2001-499 R4<BR>Distribution:<BR>B<BR>Issue date:<BR>August 31, 2005<BR>Page :<BR>1/2<BR>This Airworthiness Directive is published by the DGAC on behalf of<BR>EASA, Airworthiness Authority of the State of Design for the affected<BR>product, part or appliance.<BR>Translation of « Consigne de Navigabilité » of same<BR>number.<BR>In case of difficulty, reference should be made to<BR>the French issue.<BR>Direction<BR>générale<BR>de<BR>l’aviation<BR>civile<BR>France<BR>GSAC<BR>publication<BR>No person may operate an aircraft to which an Airworthiness Directive applies,<BR>except in accordance with the requirements of that Airworthiness Directive,<BR>unless otherwise agreed with the Authority of the State of Registry.<BR>Corresponding foreign Airworthiness Directive(s):<BR>Not applicable<BR>Airworthiness Directive(s) replaced:<BR>2001-499 R3<BR>Person in charge of airworthiness:<BR>AIRBUS SAS<BR>Type certificate(s) No. 180<BR>TCDS No 180<BR>Type(s):<BR>A319 and A320 aircraft<BR>ATA chapter:<BR>32<BR>Subject:<BR>GOODRICH carbon brake - Reduction of performances<BR>1. EFFECTIVITY:<BR>AIRBUS A319 and A320 aircraft, all certified models and serial numbers which are equipped with<BR>GOODRICH carbon brakes (reference PN 2-1526-4 or 2-1526-5 or 2-1572 or PN 2-1598-1 or PN 2-1600-1<BR>or 2-1600-2 or 2-1600-3) in accordance with:<BR>- AIRBUS modification 24007 or 24260 or 25810 or 30075 or 31146 or 31803 in production,<BR>or<BR>- AIRBUS Service Bulletin (SB) A320-32-1090 or A320-32-1114 or A320-32-1180 or A320-32-1221<BR>(modification 30485) or A320-32-1228 or A320-32-1238 in service.<BR>The aircraft that have received AIRBUS modification 32311 in production are not affected by the<BR>requirements of this Airworthiness Directive (AD).<BR>The aircraft fitted with 4 GOODRICH carbon SEPCARB III brakes PN 2-1600-3 on which brakes mixability<BR>has been forbidden as per application of SB A320-32-1247 in service, are not affected by the<BR>requirements of this AD.<BR>2. REASONS:<BR>One aircraft has experienced a runway excursion during landing.<BR>Investigations revealed a reduction of braking performances during the first application was a contributing<BR>factor.<BR>[…]<BR>The Revision 1 of this AD mentions GOODRICH carbon brake SEPCARB III (PN 2-1598-1) and<BR>introduces limitations to cover brakes mixability for aircraft equipped with GOODRICH carbon SEPCARB III<BR>PN 2-1600-3.<BR>The Revision 2 of this AD rectifies the reference of SB A320-32-1233, which must be read A320-32-1238.<BR>The Revision 3 of this AD aims at deleting the limitations to SA3D brakes once they have accumulated<BR>240 flight cycles, in accordance with AFM Temporary Revision (AFM TR) N° 5.03.00/24 issue 2.<BR>Revision 4 of this AD reduces the applicability field.<BR>n/GH<BR>AIRWORTHINESS DIRECTIVE<BR>No F-2001-499 R4<BR>Distribution:<BR>B<BR>Issue date:<BR>August 31, 2005<BR>Page:<BR>2/2<BR>3. COMPLIANCE TIME AND MANDATORY ACTIONS:<BR>Within 10 days following June 26, 2002 , the flight crew must follow<BR>the procedures/limitations of the following AFM TR:<BR>Concerned aircraft Applicable procedure<BR>1. A320 fitted with GOODRICH SA3D brakes AFM TR 5.03.00/24 issue 2<BR>2. A320 fitted with GOODRICH carbon SEPCARB III<BR>except PN 2-1600-3 AFM TR 5.03.00/21 issue 4<BR>3. A320 fitted with at least one GOODRICH carbon<BR>SEPCARB III PN 2-1600-3 in accordance with<BR>AIRBUS modification 31803 (SB A320-32-1238)<BR>AFM TR 5.03.00/23 issue 2<BR>(in replacement of AFM TR 5.03.00/21<BR>issue 4 or any previous issues)<BR>4. A319 fitted with at least one GOODRICH carbon<BR>SEPCARB III except 2-1600-3 AFM TR 5.02.00/60 issue 4<BR>5. A319 fitted with at least one GOODRICH carbon<BR>SEPCARB III PN 2-1600-3 in accordance with<BR>AIRBUS modification 31803 (SB A320-32-1238)<BR>AFM TR 5.02.00/61 issue 2<BR>(in replacement of AFM TR 5.02.00/60<BR>issue 4 or any previous issues)<BR>Incorporation of the applicable procedure in the aircraft operation manual and accomplishment by the<BR>flight crews will ensure compliance with this AD.<BR>Application of BS A320-32-1247 Revision 2 on an aircraft fitted with 4 GOODRICH carbon SEPCARB III<BR>brakes PN 2-1600-3, cancels the requirements of this AD.<BR>4. REFERENCE PUBLICATION:<BR>AIRBUS AFM TR 5.02.00/60 issue 4<BR>AIRBUS AFM TR 5.03.00/21 issue 4<BR>AIRBUS AFM TR 5.02.00/61 issue 2<BR>AIRBUS AFM TR 5.03.00/23 issue 2<BR>AIRBUS AFM TR 5.03.00/24 issue 2<BR>AIRBUS Service Bulletin A320-32-1247 Revision 2<BR>(Any further approved revision of these documents is acceptable).<BR>5. EFFECTIVE DATES:<BR>Original AD : Upon receipt from October 17, 2001<BR>Revisions 1 and 2 : Upon receipt from April 17, 2002<BR>Revision 3 : Upon receipt from June 26, 2002<BR>Revision 4 : Upon receipt from August 31, 2005.<BR>6. REMARK:<BR>For questions concerning the technical contents of this AD’s requirements, contact:<BR>AIRBUS SAS - Office of Airworthiness - EAS - Fax: 33 5 61 93 44 51.<BR>7. APPROVAL:<BR>This AD Revision is approved under EASA reference No 2005-6191 dated August 22, 2005.
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