TailplateTailplate
Run a report

Airworthiness Directive 2024-19-07

one-time
Official AD 2024-19-07 · FR doc 2024-21408 · 2024-09-20 · turbine engine

Airworthiness Directives; CFM International, S.A. Engines

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for certain CFM International, S.A. (CFM) Model LEAP-1A32 engines. This AD was prompted by a report of multiple events of loss of thrust control during go-around. This AD requires replacement of the full set of fuel nozzles. The FAA is issuing this AD to address the unsafe condition on these products.

Which aircraft AD 2024-19-07 applies to

MakesCfm International, S.A.
ModelsLEAP-1A32, LEAP-1A
Serial-conditional — narrows to serials 11200–11200, 11420–11420, 11473–11473, 11609–11609, 11698–11698, 11791–11791, 11815–11815, 12136–12136, 12314–12314, 12370–12370.

Applies only to LEAP-1A32 engines installed on Airbus A321-251NX airplanes bearing one of the ten listed airplane serial numbers, not all LEAP-1A32 engines.

Whether AD 2024-19-07 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 2024-19-07 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.