CTHIn ForceLegislation
AD/B767/232 - Fuel Pump Housing to Wing Structure Electrical Bonding
//
© 2026 Zoe. All rights reserved.
Zoe is a legal information platform. Always consult the Federal Register of Legislation for authoritative text.
AD/B767/232 - Fuel Pump Housing to Wing Structure Electrical Bonding
Start here
Turn the raw legal text into a practical explanation grounded in AD/B767/232 - Fuel Pump Housing to Wing Structure Electrical Bonding.
| AD/B767/232 | Fuel Pump Housing to WingStructure Electrical Bonding | 13/2007 |
|---|
| Applicability: | Model 767-200, -300, -300F, and -400ER series aircraft. |
|---|---|
| Requirement: | Action in accordance with the technical requirements of FAA AD 2007-21-13 Amdt 39-15231.Note: Boeing Service Bulletins 767-57-0092 original issue and Revision 1, and767-57-0093 original issue and Revision 1, or later FAA approved revisions, refer. |
| Compliance: | As specified in the Requirement document, with a revised effective date of20 December 2007. |
| This Airworthiness Directive becomes effective on 20 December 2007. | |
| Background: | The FAA requires reworking the electrical bonding between the aircraft structure and the pump housing of certain fuel boost pumps, and also requires related investigative actions and corrective actions if necessary. Insufficient electrical bonding could result in potential ignition sources inside the fuel tanks, which, in combination with flammable fuel vapours, could result in a fuel tank explosion and consequent loss of the aircraft. |
Image unavailable in extracted text
David Villiers
Delegate of the Civil Aviation Safety Authority
8 November 2007