AD 2003-14-23

final rule
Data completeness: 70%

Airworthiness Directives; Rolls-Royce plc RB211-524G2, -524G2-T, -524G3, -524G3-T, -524H, -524H-T, -524H2, and “524H2-T Series, and Models RB211 Trent 768-60, 772-60, and 772B-60 Turbofan Engines; Correction

AD Number
2003-14-23
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2003-NE-20-AD
FR Citation
68 FR 55811

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce plc RB211-524G2 Airworthiness Directives; Rolls-Royce plc RB211-524G2, -524G2-T, -524G3, -524G3-T, -524H, -524H-T, -524H2, and “524H2-T Series, and Models RB211 Trent 768-60, 772-60, and 772B-60 Turbofan Engines; Correction

Unsafe Condition

This document makes a correction to Airworthiness Directive (AD) 2003-14-23 applicable to Rolls-Royce plc RB211-524G2, -524G2-T, - 524G3, -524G3-T, -524H, -524H-T, -524H2, and "524H2-T Series, and Models RB211 Trent 768-60, 772-60, and 772B-60 turbofan engines that was published in the Federal Register on July 17, 2003. RB211 Trent 768-60, 772-60, and 772B-60 turbofan engine models were included in this AD in error. This document deletes these models from the AD. In all other respects, the or...

Affected Aircraft

Rolls-Royce plc RB211-524G2, -524G2-T, -524G3, -524G3-T, -524H, -524H-T, -524H2, and -524H2-T series turbofan engines with high pressure compressor (HPC) rotor stage 1 through stage 6 drums, part numbers (P/Ns) FK25502 and FW20195 installed.

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

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