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Airworthiness Directive 01-25053

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AD 01-25053 · 2001-10-15 · turbine engine

Airworthiness Directives; Rolls-Royce plc. RB211 535 Turbofan Engines, Correction

What this AD requires

This document makes a correction to Airworthiness Directive (AD) 2001-19-05 applicable to Rolls-Royce plc (RR) models RB211-535C- 37, RB211-535E4-37, RB211-535E4-B-37, and RB211-535E4-B-75 turbofan engines, with radial drive steady bearing, part number (P/N) LK76084, that was published in the Federal Register on September 26, 2001 (66 FR 49099). A part number referenced in items (3) and (4) of Table 1 in the regulatory information is incorrect. This document corrects that part number. In all other respects, the original document remains the same.

Which aircraft AD 01-25053 applies to

MakesRolls-Royce Plc. Rb211 535 Turbofan

Whether AD 01-25053 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

How AD compliance is recorded

A valid compliance record (14 CFR 43.9) states:

Method of compliance — The specific action taken (inspected, replaced, modified) and to what revision.
Date — When the work was done.
Aircraft time — Total time in service / tach at compliance — how recurring next-due is computed.
Signature & certificate — The A&P/IA who returned it to service, with certificate number.
Is AD 01-25053 complied with on your aircraft?

Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.

Look up a tail number →Read the full directive (Federal Register)

Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.