D3215600500600

PINTLE PIN

OEM

Specifications

Part Number
D3215600500600
Manufacturer
Airbus
ATA ChapterMaintenance system chapter
57 — Wings
CapabilitySystem area (hydraulics, avionics, landing gear…)
Landing Gear
Inventory ClassRotable, expendable, or consumable
Consumable
Certification
OEM
Aircraft Category
Wide-Body
Criticality
Standard

Service Reliabilityfrom FAA SDR (Service Difficulty Reports)

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

* Structural ATA chapter (57). 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
19
Replace events
19
Repair events
0
K-code events
19
Reporting window 2010-03-122024-06-11Dominant chapter ATA 57

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

2directives reference this part number — recurring compliance demand wherever it flies
Most recent
  • FAAAD 2025-17-17effective Sep 17, 2025Prohibition

    The FAA is adopting a new airworthiness directive (AD) for all Airbus SAS Model A318, A319, A320, and A321 series airplanes. This AD was prompted by a determination that a batch of main landing gear (MLG) aft pintle pins did not have nickel plating applied to the inner bore during manufacturing. This AD requires replacing affected parts with serviceable parts and also prohibits the installation of affected parts. The FAA is issuing this AD to address the unsafe condition on these products.

  • EASAAD 2025-0167effective Sep 9, 2025Prohibition

    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(4)

Data Sources(1)

Quick Facts

Airframes4 applicable
AlternatesNone recorded
ClassConsumable
CriticalityStandard
CategoryWide-Body

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