2026-18019RuleWallet

FAA Orders Jet Engine Teardowns Before They Blow

Published Date: 9/3/2026

Rule

Summary

The FAA is making new rules for certain Pratt & Whitney jet engines because some parts didn’t get the right treatment during manufacturing. Engine owners must check specific compressor parts for issues and replace them if needed before they wear out. These changes start October 8, 2026, and help keep flights safe without causing big costs or delays.

Analyzed Economic Effects

5 provisions identified: 1 benefits, 4 costs, 0 mixed.

Replace parts if incorrect shot peening found

If the inspection finds evidence of incorrect shot peening on the HPC drum rotor disk assembly, you must replace that assembly before further flight with a part eligible for installation. The FAA estimates replacement labor is 10 work-hours (10 x $85/hr = $850) and parts cost $1,622,040, for a per-product replacement cost of $1,622,890.

Mandatory early removal for two serial numbers

Two specific HPC drum rotor disk assemblies must be removed and replaced before reaching reduced life limits: P/N 50S634 S/N CENCD30975 must be removed before accumulating 9,800 total life cycles since new, and P/N 50S634 S/N CENCD42978 must be removed before accumulating 11,000 total life cycles since new.

Estimated U.S. operator compliance cost

The FAA estimates this AD affects four engines on U.S. registry and estimates one of those four engines will require replacement at the reduced life limit. The FAA estimates inspection cost per engine is $850 and replacement cost per product is $1,622,890, with total costs to U.S. operators up to $6,491,560.

Safety goal: prevent engine and airplane damage

The FAA issued this AD to address incorrect shot peening that reduces part life and could cause failure of the HPC drum rotor disk assembly. If not fixed, the unsafe condition could result in uncontained debris release, damage to the engine, and damage to the airplane.

Required visual inspections for specific HPC parts

If you operate Pratt & Whitney PW4074D, PW4077D, PW4084D, PW4090, or PW4090-3 engines, you must perform a visual inspection of certain high-pressure compressor (HPC) drum rotor disk assemblies per PW Alert Service Bulletin PW4G-112-A72-373. The inspection requirement for assemblies with P/N 50S634 and S/Ns CENCD26931, CENCD29577, CENCD29597, CENCD41851, or CENCD43536 must be done before accumulating the total life cycles since new listed in Table 1 of the Accomplishment Instructions of that service bulletin.

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Key Dates

Published Date
Rule Effective
9/3/2026
10/8/2026

Department and Agencies

Department
Independent Agency
Agency
Transportation Department
Federal Aviation Administration
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