D53480062297

STOP FITTING

OEM

Specifications

Part Number
D53480062297
Manufacturer
Airbus
ATA ChapterMaintenance system chapter
53 — FuselageField reports: 53 (100%) — 5 reports
CapabilitySystem area (hydraulics, avionics, landing gear…)
Structures
Inventory ClassRotable, expendable, or consumable
Expendable
Certification
OEM
Aircraft Category
Wide-Body
Criticality
Standard
Life & ShelfTypical service/shelf life — verify against OEM data

Service Reliabilityfrom FAA SDR (Service Difficulty Reports)

100%
Component-change rate (FAA K-code)*
low confidence

* Structural ATA chapter (53). Verb-based propensity is suppressed because "REPAIRED" in the SDR text typically refers to the airframe being repaired around the part, not the part itself. FAA K-code component-change rate is the honest signal.

SDR reports
5
Replace events
0
Repair events
5
K-code events
5
Reporting window 2013-01-312022-09-10Dominant chapter ATA 53

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

1directive references this part number — recurring compliance demand wherever it flies
Most recent
  • EASAAD 2020-0222effective Oct 28, 2020Mixed actions

    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.

Airframe Applicability(6)

Data Sources(1)

Quick Facts

Airframes6 applicable
AlternatesNone recorded
ClassExpendable
CriticalityStandard
CategoryWide-Body

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