AD 2013-14-06

final rule
Data completeness: 80%

Airworthiness Directives; CFM International, S. A. Turbofan Engines

AD Number
2013-14-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2012-1114
FR Citation
78 FR 45842

Applicability

TypeManufacturerModelDetails
engine CFM International Airworthiness Directives; CFM International, S. A. Turbofan Engines

Unsafe Condition

Corrosion of the delta-P valve in the hydro-mechanical unit (HMU) fuel control caused by exposure to type TS-1 fuel, leading to seizure of the HMU and potential failure of one or more engines and damage to the airplane.

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

Required Actions

Clean, inspect, and repair affected HMUs. Use paragraph 3.A(2) of CFM SB CFM56-5 S/B 73-0182, Revision 6, or CFM SB CFM56-5B S/B 73-0122, Revision 8, for the inspection. Overhaul is defined as HMU maintenance, including inspection, cleaning, or replacement of the HMU delta-P valve.

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

Compliance Time

Within 4,000 hours from the effective date of the AD.

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

Affected Aircraft

CFM International, S.A. model CFM56-5 and CFM56-5B series turbofan engines.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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