BLC1881M52G05
Second Stage High Pressure Turbine Blade
Specifications
- Part Number
- BLC1881M52G05
- ATA ChapterMaintenance system chapter
- 72 — Engine - Turbine / Turboprop
- CapabilitySystem area (hydraulics, avionics, landing gear…)
- Engine Accessories
- Inventory ClassRotable, expendable, or consumable
- Rotable
- Certification
- PMA
- Aircraft Category
- Multi-Category
- Criticality
- Critical & Life-Limited
Airframe Applicability
No airframe data available for this part.
Data Sources(1)
- 2026-03-07
Quick Facts
AirframesUnknown
AlternatesNone recorded
ClassRotable
CriticalityCritical & Life-Limited
CategoryMulti-Category
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