AD 2000-03-07

final rule
Data completeness: 70%

Airworthiness Directives; Rolls-Royce plc RB211-524H-36 Series Turbofan Engines

AD Number
2000-03-07
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2000-NE-01-AD
FR Citation
65 FR 7720

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce plc RB211-524H-36 Series Airworthiness Directives; Rolls-Royce plc RB211-524H-36 Series Turbofan Engines

Unsafe Condition

Burn through of the combustor case due to combustion liner cracking, which can result in an engine fire and damage to the aircraft.

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

Required Actions

Install an improved combustion liner with a strengthened head and improved heat shields prior to further flight.

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

Compliance Time

Before further flight

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

Affected Aircraft

Rolls-Royce plc RB211-524H-36 series turbofan engines.

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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