CF680C2

THRUST REVERSER

Specifications

Part Number: CF680C2
Manufacturer: GE
ATA ChapterMaintenance system chapter: 72 — Engine - Turbine / TurbopropField reports: 72 (71%) · 78 (29%) — 7 reports
CapabilitySystem area (hydraulics, avionics, landing gear…): Engine Accessories
Inventory ClassRotable, expendable, or consumable: —
Certification: —
Aircraft Category: Wide-Body
Criticality: Critical

Service Reliabilityfrom FAA SDR (Service Difficulty Reports)

100%

Scrap Propensity (SDR-derived)

low confidence

SDR reports: 7
Replace events: 5
Repair events: 0
K-code events: 1

Reporting window 2003-12-01 – 2020-05-11Dominant chapter ATA 72

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

FAAAD 2021-14-11effective Aug 27, 2021Prohibition
The FAA is adopting a new airworthiness directive (AD) for certain General Electric Company (GE) CF6-80A and CF6-80C2 model turbofan engines. This AD was prompted by an inspection by the manufacturer that revealed cracking of the high-pressure turbine (HPT) rotor stage 1 disk. This AD requires visual inspection and fluorescent penetrant inspection (FPI) of the HPT thermal shield and, if cracking is detected, removal from service of the HPT thermal shield, HPT rotor stage 1 disk and HPT rotor stage 2 disk. The FAA is issuing this AD to address the unsafe condition on these products.

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.