AD 2017-03-03

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Rolls-Royce plc Turbofan Engines

AD Number
2017-03-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2012-0004
FR Citation
82 FR 12289

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce plc Airworthiness Directives; Rolls-Royce plc Turbofan Engines

Unsafe Condition

Wear found between the securing clips and the low-pressure (LP) fuel tube outer surface, which reduces the fuel tube wall thickness, leading to fracture of the fuel tube and consequent fuel leakage.

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

Required Actions

Repetitive inspections of the LP fuel tubes, fuel tube clips, and fuel/oil heat exchanger (FOHE) mounts for evidence of damage, wear, and fuel leakage.

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

Compliance Time

Within the specified inspection intervals as outlined in the AD.

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

Affected Aircraft

Rolls-Royce plc RB211 Trent 500 series turbofan engines, including models RB211 Trent 553-61, RB211 Trent 553A2-61, RB211 Trent 556-61, RB211 Trent 556A2-61, and RB211 Trent 556B-61.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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