Is AD E7-7032 a recurring Airworthiness Directive?

No — AD E7-7032 is a one-time directive. Verify it was complied with in the aircraft's records.

Airworthiness Directive E7-7032

Q: Which aircraft does AD E7-7032 apply to?

AD E7-7032 applies to Rolls-Royce Plc — models RB211-524B, RB211-524C2, RB211-524D4, RB211-524G2, RB211-524G3, RB211-524H, RB211-535C, RB211-535E. Serial/part conditions may narrow it to specific aircraft.

one-time

AD E7-7032 · 2007-04-16 · turbine engine

Airworthiness Directives; Rolls-Royce plc RB211 Series Turbofan Engines

What this AD requires

The FAA is revising an existing airworthiness directive (AD) for Rolls-Royce plc (RR) RB211-22B series, RB211-524B, -524C2, -524D4, -524G2, -524G3, and -524H series, and RB211-535C and -535E series turbofan engines with high pressure compressor (HPC) stage 3 disc assemblies, part numbers (P/Ns) LK46210, LK58278, LK67634, LK76036, UL11706, UL15358, UL22577, UL22578, and UL24738 installed. That AD currently requires removing from service certain disc assemblies before they reach their full published life if not modified with anticorrosion protection. This AD requires the same actions but relaxes the removal compliance time for certain disc assemblies that have a record of detailed inspection. This AD results from the FAA allowing certain affected disc assemblies that entered into service before 1990 that have a record of detailed inspections, to remain in service for a longer period than the previous AD allowed. We are issuing this AD to relax the compliance time for certain disc assemblies and track the disc life based on a detailed inspection rather than by its entry into service date, while continuing to prevent corrosion-induced uncontained disc assembly failure, resulting in damage to the airplane.

Which aircraft AD E7-7032 applies to

MakesRolls-Royce Plc

ModelsRB211-524B, RB211-524C2, RB211-524D4, RB211-524G2, RB211-524G3, RB211-524H, RB211-535C, RB211-535E, RB211-22B, RB211-524, RB211-535

Part-conditional — LK46210, LK58278, LK67634, LK76036, UL11706, UL15358, UL22577, UL22578.

Applies only to engines with a high pressure compressor (HPC) stage 3 disc assembly bearing one of the listed part numbers installed. Installed on, but not limited to, Boeing 747, 757, 767, Lockheed L-1011, and Tupolev Tu204 series airplanes.

Whether AD E7-7032 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 E7-7032 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.