What it covers
The electric motor/engine driven pumps providing fuel under pressure to the engine fuel control/carburetor for starting and emergency use. Includes parts of the pump, associated motor, and electrical circuitry/switch. Does not include pressure switch indicating system. Typical parts are housing, seal, motor, brush, bearing, connector, and fuel transfer pump, etc.
Service difficulty reports · 2,745
Reports filed under 2822, newest first.
| 1995 | 45 |
|---|---|
| 1996 | 144 |
| 1997 | 89 |
| 1998 | 127 |
| 1999 | 106 |
| 2000 | 84 |
| 2001 | 80 |
| 2002 | 88 |
| 2003 | 81 |
| 2004 | 44 |
| 2005 | 36 |
| 2006 | 45 |
| 2007 | 44 |
| 2008 | 55 |
| 2009 | 52 |
| 2010 | 63 |
| 2011 | 71 |
| 2012 | 57 |
| 2013 | 72 |
| 2014 | 60 |
| 2015 | 71 |
| 2016 | 78 |
| 2017 | 128 |
| 2018 | 138 |
| 2019 | 165 |
| 2020 | 123 |
| 2021 | 138 |
| 2022 | 78 |
| 2023 | 75 |
| 2024 | 102 |
| 2025 | 141 |
| 2026 | 65 |
SDR UIEA2026101300984Pump · failedLEFT CENTER FUEL PUMP CB POPPED IN FLIGHT WITH FUEL IN CENTER TANK. R & R FUEL OVRD/JETT BOOST PUMP HARNESS (LH) PER WDM 28-22-12 SB 767-28A0104; OPS CHECKS GOOD. PERFORMED INSULATION RESISTANCE TEST IAW AMM 20-80-24 AND B767 WDM 28-22-12. TESTED FROM DISCONSDR DXTA2026092509853Actuator · defectiveWHILE CLIMBING THROUGH FL350 WE CROSSFED FUEL FROM THE LEFT TANK TO THE RIGHT ENGINE. AFTER TURNING THE CROSSFEED OFF, THE AMBER FUEL BST PUMP ON L-R CAS MESSAGE APPEARED. FOLLOWED THE PROCEDURE IN THE QRH AND SELECTED BOTH BOOST PUMPS ON. THE CAS MESSAGE REMASDR AALA202609229885Pump · fault messageAIRCRAFT WAS NOT GROUNDED: FUEL LEFT TANK PUMP 2 LOW PRESSURE ON ECAM DURING DESCENT. (OPEN)
See all 2,745 reportsOther codes in chapter 28 · 13
2800Aircraft Fuel System2810Fuel Storage2820Aircraft Fuel Distribution System2821Aircraft Fuel Filter/Strainer2823Fuel Selector/Shut-Off Valve2824Fuel Transfer Valve2830Fuel Dump System2840Fuel Indicating System2841Fuel Quantity Indicator2842Fuel Quantity Sensor2843Fuel Temperature Indicator2844Fuel Pressure Indicator2897Fuel System Wiring