Technology · In the factory and the shop
Engine durability engineering
Turbine blade coatings, cooling geometry, time on wing
Two independent sources on every claim.
Why it is here
Time on wing is the number that decides engine economics, and both CFM and Rolls-Royce are rebuilding it.
At a glance
- Rolls-Royce reports a 100 percent improvement in time on wing across the Trent fleet since its durability programme began, and lifted its own target in February 2026.
- CFM's LEAP-1B high pressure turbine durability kit was certified in July 2026 and doubles time on wing in hot and harsh environments.
- Both fixes are the same engineering problem solved twice: keeping cooling air where it belongs in the hottest part of the engine.
- Full LEAP production cutover is targeted for early 2027, so the fleet will carry mixed build standards through next year.
What it is
Time on wing is how long an engine stays installed before it must come off for a shop visit. It is the single number that decides engine operating economics, because a shop visit is expensive, slow, and consumes a spare engine while it happens.
In plain terms
The high pressure turbine sits immediately behind the combustor, in the hottest gas in the engine. Its blades survive because cooling air is bled through tiny holes in the blade surface, forming a film of cooler air over the metal. Almost every durability problem in a modern engine is a variation on that film failing.
Why it matters on the line
The two current programmes are instructive because they failed differently and were fixed differently.
On the LEAP, fine sand ingested in the Middle East, India and parts of Africa clogged the film cooling holes. The redesigned stage 1 blade uses revised internal cooling geometry so particulates pass through rather than accumulating, with reinforced nozzle structures to stop thermal warping. CFM reports the new blades held structural integrity twice as long as the original.
On the Trent 1000, the failures were in the intermediate pressure turbine and compressor, and the fix was a staged durability enhancement package: reduced weight high pressure turbine blade shrouds and new advanced coatings, approved in June, followed by a second phase adding roughly another 30 percent. Together they should deliver up to triple the original time on wing.
On the line
Both fixes reach the installed fleet gradually, at scheduled refurbishment rather than through a mandated campaign, so your fleet will carry a mix of build standards for a year or more. Track time on wing by build standard rather than averaging across the fleet, or the improvement will be invisible in your own data. When an engine is inducted, confirm which standard it will come out with, because that changes the interval you plan the next removal against. The LEAP gain is also concentrated in hot and harsh operations, so do not apply one expected interval across a mixed network.
Where to read more
The two programmes are on the CFM LEAP and Trent 1000 pages. The Trent 7000 was where Rolls-Royce proved its upgrades first.
Sources
- Aviation Pros, "CFM International Announces FAA and EASA Certification for LEAP-1B Durability Kit Upgrades", July 2026. https://www.aviationpros.com/aircraft-maintenance-technology/engines-parts/press-release/55392040/cfm-international-announces-faa-and-easa-certification-for-leap-1b-durability-kit-upgrades
- FlightGlobal, "Rolls-Royce readies roll-out of next Trent 1000 durability upgrade step", January 2026. https://www.flightglobal.com/engines/2026/01/rolls-royce-readies-roll-out-of-next-trent-1000-durability-upgrade-step/
- FlightGlobal, "Rolls-Royce lifts Trent engine durability-improvement target", February 2026. https://www.flightglobal.com/engines/2026/02/rolls-royce-lifts-trent-engine-durability-improvement-target/
- Safran, "FAA and EASA certify more durable CFM LEAP HPT hardware", 9 December 2024. https://www.safran-group.com/pressroom/faa-and-easa-certify-more-durable-cfm-leap-hpt-hardware-2024-12-09