AD 2011-24-11

final rule
Data completeness: 70%

Airworthiness Directives; Honeywell International Inc. Turbofan Engines

AD Number
2011-24-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2011-1261
FR Citation
76 FR 73489

Applicability

TypeManufacturerModelDetails
engine Honeywell International Inc Airworthiness Directives; Honeywell International Inc. Turbofan Engines

Unsafe Condition

Cracks found in second stage high pressure compressor (HPC2) discs, part number 2-101-332-12, during routine inspection. These cracks could lead to disc fracturing before reaching the published life limit, resulting in an uncontained failure and damage to the airplane.

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

Required Actions

Remove from service HPC2 discs, part number 2-101-332-12, with serial numbers listed in Table 2 of Honeywell International Inc. Service Bulletin ALF/LF-72-1113, dated September 16, 2011.

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

Compliance Time

Before accumulating 4,500 cycles-since-new on the affected HPC2 disc, or before exceeding 7 years after the effective date of this AD, whichever occurs first.

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

Affected Aircraft

Honeywell International Inc. ALF502L-2C, ALF502R-3, ALF502R-3A, ALF502R-5, LF507-1F, and LF507-IH turbofan engines with HPC2 discs, part number 2-101-332-12, and serial numbers listed in Table 2 of Honeywell International Inc. Service Bulletin ALF/LF-72-1113.

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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