AD 90-20-13

final rule
Data completeness: 70%

CFM INTERNATIONAL Models CFM56-3B-2 and CFM56-3C-1 Series Engines

AD Number
90-20-13
Status
final_rule
Effective Date
Product Category
engine
Docket
90-ANE-16
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine CFM International, S.A. CFM56-3B CFM INTERNATIONAL Models CFM56-3B-2 and CFM56-3C-1 Series Engines
engine CFM International, S.A. CFM56-3C CFM INTERNATIONAL Models CFM56-3B-2 and CFM56-3C-1 Series Engines

Unsafe Condition

Fan blade failure, inflight shutdown, and severe engine damage.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Install fan blade dampers P/N 335-105-305-0, axial stops P/N 335-105-201-0, and bolts P/N J815PO56A in accordance with CFM56 Service Bulletin 72-494, Revision 2. Ferrying is allowed under FAR 21.197 and 21.199.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

within 60 days from the effective date of this AD

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

CFM International models CFM56-3B-2 and CFM56-3C-1 series engines with fan blade P/Ns 9527N99P08, 9527M99P09, 9527M99P10, 9527M99P11, and 1285M39P01, installed in Boeing 737-300/400/500 series aircraft.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.