AIRPLANE FLIGHT MANUAL - A330

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REFERENCE: TR811 Issue 1 AFM ISSUE DATE: 25 AUG 22 A330 TEMPORARY REVISION TR811 issue 1 A330NEO - HPV CLIP FAILURE MITIGATION AIRPLANE FLIGHT MANUAL This Manual has been reviewed under European Export Control Regulations (EU) 2021/821 and was determined as EU_Not in Export Control List. As this Manual does not contain any US data, US Export control Regulations (15 CFR Part 774) are not applicable. This Manual does not contain any Military Data, pursuant all Regulations as stated above. This Export Control Assessment does not include additional restrictions pursuant to EU, UK, or US Regulations regarding the Destination or the Final User. This Manual must not be re-exported without the clearance of Airbus SAS, to any third party (legal or natural persons). When re-exported, it has to be covered by appropriate authorization and export control licenses when applicable. The content of this document is the property of Airbus. It is supplied in confidence and commercial security on its contents must be maintained. It must not be used for any purpose other than that for which it is supplied, nor may information contained in it be disclosed to unauthorized persons. It must not be reproduced in whole or in part without permission in writing from the owners of the copyright. © AIRBUS 2005. All rights reserved. Intentionally left blank PRELIMINARY PAGES Intentionally left blank A330 AIRPLANE FLIGHT MANUAL PRELIMINARY PAGES TABLE OF CONTENTS TR811 Issue 1 PLP-TOC P 1/2 AFM 25 AUG 22 APPRO APPROVAL DATA APPRO-TR TEMPORARY REVISIONS HPV Clip Failure Mitigation..................................................................................................................................... A LIM LIMITATIONS LIM-36 PNEUMATIC Bleed System...........................................................................................................................................................A ABN ABNORMAL PROCEDURES ABN-36 PNEUMATIC AIR - ENG BLEED NOT CLSD ............................................................................................................................. A AIR - ENG BLEED FAULT......................................................................................................................................B NORM NORMAL PROCEDURES NORM-PFLT PREFLIGHT CHECKS Bleed System...........................................................................................................................................................A NORM-ALDG AFTER LANDING Bleed System...........................................................................................................................................................A A330 AIRPLANE FLIGHT MANUAL PRELIMINARY PAGES TABLE OF CONTENTS Intentionally left blank TR811 Issue 1 PLP-TOC P 2/2 AFM 25 AUG 22 A330 AIRPLANE FLIGHT MANUAL APPROVAL DATA TEMPORARY REVISIONS TR811 Issue 1 APPRO-TR P 1/2 AFM A 25 AUG 22 TR811 Issue 1 HPV CLIP FAILURE MITIGATION Ident.: TDU / APPRO-TR-00025892.0001001 / 25 AUG 22 EASA APPROVED Criteria: (330-800 or 330-900) Impacted DU: NONE APPROVAL REFERENCE APPROVED BY: EASA Approval date: 25 AUG 22 Approval reference: 10079993 Do not remove this Temporary Revision until instructed to do so. Reason for issue: This Temporary Revision (TR) provides the limitation and procedures to mitigate the risk of a non isolated overpressure or overtemperature in the case of an excessive internal leak of the engine bleed High Pressure (HP) valve. Applicable to: All A330neo aircraft. This Temporary Revision is made up of the following Temporary Documentary Units: APPRO-TR-00025892.0001001/25 AUG 22 ABN-36-00016652.0002001/25 AUG 22 LIM-36-00025899.0001001/25 AUG 22 NORM-PFLT-00025894.0001001/25 AUG 22 ABN-36-00025893.0001001/25 AUG 22 NORM-ALDG-00025895.0001001/25 AUG 22 A330 AIRPLANE FLIGHT MANUAL APPROVAL DATA TEMPORARY REVISIONS Intentionally left blank TR811 Issue 1 APPRO-TR P 2/2 AFM 25 AUG 22 A330 AIRPLANE FLIGHT MANUAL LIMITATIONS PNEUMATIC TR811 Issue 1 LIM-36 P 1/2 AFM A 25 AUG 22 BLEED SYSTEM Ident.: TDU / LIM-36-00025899.0001001 / 25 AUG 22 EASA APPROVED Criteria: (330-800 or 330-900) Impacted DU: NONE Belongs to TR811 Issue 1 If a takeoff or go-around is performed with packs OFF or engine bleed OFF or APU bleed ON, a maintenance check of the conditions of the engine bleed HP valve seals after the flight is required in accordance with AOT Ref. A36L009-22. For the following flight, takeoff is prohibited if the maintenance check is not performed. This limitation does not apply in the case of dispatch under MMEL with pack(s) OFF or engine bleed OFF for the affected side(s). Refer to the associated MMEL item for the appropriate dispatch conditions. A330 AIRPLANE FLIGHT MANUAL LIMITATIONS PNEUMATIC Intentionally left blank TR811 Issue 1 LIM-36 P 2/2 AFM 25 AUG 22 A330 AIRPLANE FLIGHT MANUAL ABNORMAL PROCEDURES PNEUMATIC TR811 Issue 1 ABN-36 P 1/2 AFM A 25 AUG 22 AIR - ENG BLEED NOT CLSD Ident.: TDU / ABN-36-00025893.0001001 / 25 AUG 22 EASA APPROVED Criteria: (330-800 or 330-900) Impacted DU: NONE Belongs to TR811 Issue 1  On ground: Return to the gate and request appropriate maintenance actions. A330 AIRPLANE FLIGHT MANUAL ABNORMAL PROCEDURES PNEUMATIC TR811 Issue 1 ABN-36 P 2/2 AFM B 25 AUG 22 AIR - ENG BLEED FAULT Ident.: TDU / ABN-36-00016652.0002001 / 25 AUG 22 EASA APPROVED Criteria: (330-800 or 330-900) Impacted DU: 00005117 Belongs to TR811 Issue 1  In the case of engine bleed overtemperature and the associated engine bleed valve failed open:  On ground: Return to the gate and request appropriate maintenance actions.  In Flight: Turn off affected side engine bleed.  If engine 1 bleed affected: Turn off APU bleed Close crossbleed valve. Turn off affected side pack. Turn off wing anti-ice. Note: Wing anti-ice is inoperative. Refer to ABN-30 A.ICE - WAI SYS FAULT or OFF.  In all other cases:  On ground: Return to the gate and request appropriate maintenance actions.  In Flight: