2026-08106RuleWallet

FAA Orders Inspections for Pratt & Whitney Engine Cracks

Published Date: 4/24/2026

Rule

Summary

The FAA is rolling out new safety checks for certain Pratt & Whitney engines to catch cracks early and keep flights safe. Starting May 29, 2026, operators must perform regular ultrasonic inspections and replace parts if needed, preventing engine shutdowns like a recent scary incident. This means some extra work and costs but way better than an emergency in the sky!

Analyzed Economic Effects

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

Very Expensive On-Condition Part Replacements

If inspections find cracks, operators must remove and replace affected parts. The AD lists on-condition replacement costs of $730,850 for an HPT 1st-stage disk and $500,850 for a turbine hub (these totals include parts and labor).

Immediate Removal of Specific Seal Assemblies; 14 U.S. Replacements

The AD requires removal from service at the next piece-part exposure of HPT lenticular seal assemblies with the part number 1B8575 and the serial numbers listed in the rule; 14 affected assemblies are estimated to require replacement on U.S.-registered airplanes. The FAA estimates replacement cost per affected seal assembly at $512,345 and a total cost to U.S. operators of $7,172,830; one serial number (DKLBG48292) must be removed at next piece-part exposure or before 2,750 cycles since new, whichever occurs first.

Mandatory Ultrasonic Inspections from May 29, 2026

Starting May 29, 2026, operators of specified Pratt & Whitney engines (F117-PW-100, PW2037, PW2037D, PW2037M, PW2040, and PW2040D) must perform angled ultrasonic inspections (AUSIs) of HPT 1st-stage disks and turbine hubs at the next piece-part exposure and at every subsequent piece-part exposure. Each AUSI is estimated at 5 work-hours (5 x $85/hr = $425) per part.

Installation Limits and Documentation Requirements

As of May 29, 2026, persons may not install specified HPT 1st-stage disks (P/N 1B7801, 1B3601, 1B3601-001) or turbine hubs (P/N 1B4902, 1B6602, 1B8002) unless they are "parts eligible for installation." Eligible parts must have passed the AUSI, have a certificate of conformance showing compliance with NDIP-1282/1283, or be new with an FAA Form 8130-3 dated March 1, 2025, or later.

Optional Termination by Updating Maintenance Limits

Operators may choose optional terminating action: revise the airworthiness limitations section (ALS) of the engine manual and the operator's approved maintenance/inspection program to include the additional inspections in figure 2 of the AD. Incorporating those ALS inspections constitutes terminating action for the repetitive AUSIs required by paragraphs (g)(1) through (3).

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Key Dates

Published Date
Rule Effective
4/24/2026
5/29/2026

Department and Agencies

Department
Independent Agency
Agency
Transportation Department
Federal Aviation Administration
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