568127202002

BOOST PUMP

Specifications

Part Number: 568127202002
Manufacturer: —
ATA ChapterMaintenance system chapter: 28 — FuelField reports: 28 (100%) — 6 reports
CapabilitySystem area (hydraulics, avionics, landing gear…): Fuel Systems
Inventory ClassRotable, expendable, or consumable: Rotable
Certification: —
Aircraft Category: Unknown
Criticality: Critical
Life & ShelfTypical service/shelf life — verify against OEM data: —

Service Reliabilityfrom FAA SDR (Service Difficulty Reports)

Component-change rate (FAA K-code)

low confidence

SDR reports: 6
Replace events: 2
Repair events: 0
K-code events: 0

Reporting window 1995-12-08 – 2001-11-16Dominant chapter ATA 28

Directional indicator only. Reflects what operators reported to the FAA when a difficulty was logged — not a fleet-normalized failure rate or a cost-based BER. Use alongside operator-specific data.

Airworthiness Directive coverage

FAA / EASA public regulatory data

3directives reference this part number — recurring compliance demand wherever it flies

Most recent

EASAAD 2023-0106effective Jul 25, 2023Prohibition
No summary available - see the EASA publication.
FAAAD 2023-13-01effective Jul 12, 2023ProhibitionNamed as replacement part
The FAA is superseding Airworthiness Directive (AD) 2008-23- 01, which applies to certain Airbus SAS Model A318, A319, A320, and A321 series airplanes. AD 2008-23-01 required inspecting to determine the part number and serial number of the fuel tank boost pumps and, for airplanes with affected pumps, revising the operator's airplane flight manual (AFM) and FAA-approved maintenance program. AD 2008-23-01 also required modifying or replacing certain fuel tank boost pumps, which terminated the AFM limitations and the maintenance program revisions. Since the FAA issued AD 2008-23-01, it has been determined that airplanes fitted with a different fuel pump can be subject to cavitation erosion on the wiring conduit. This AD requires inspecting affected fuel pumps for discrepancies and replacement if necessary, as specified in a European Union Aviation Safety Agency (EASA). This AD also requires replacing certain other fuel pumps. This AD also limits the installation of affected fuel pumps under certain conditions. The FAA is issuing this AD to address the unsafe condition on these products.
EASAAD 2007-0218-R2effective Oct 10, 2014ProhibitionNamed as replacement part
No summary available - see the EASA publication.

Directives citing this part number in the FAA / EASA regulatory corpus we have processed — not a complete historical AD list. An AD is a compliance requirement that drives scheduled work (inspections, replacements, modifications) on the fleets that carry the part; a directive naming this PN as the replacement part is install demand, not an action against it — and none of this is a prediction that the part will fail.