E-Props propellers have always been designed, manufactured and tested to meet the requirements of aeronautical standards. Quality and safety are ongoing concerns for E-PROPS throughout the design, procurement, manufacturing, testing and marketing of all its products.
This page brings together the five parts of that process, to expand below: the progress of EASA certifications (POA, DOA, Type Certificate, STC, Part-145); compliance with the ASTM F2506-26 standard for Light Sport Aircraft; Service Bulletins, which flag any corrective action needed on a propeller already delivered; Service Letters, for less urgent information; and finally the additional approvals obtained in Germany from the DULV and the DAeC, with the details of each validated aircraft/engine configuration.

E-PROPS is engaged in a European certification process (EASA) covering propeller design, production, product certification and maintenance. These approvals and certificates complement each other, in the following sequence:
1) POA – Part 21 Subpart G (Production Organisation Approval) – Production
The POA is the Production Organisation Approval: it certifies that the manufacturer has full control of its industrial processes (quality, traceability, conformity) to produce aeronautical products in accordance with an approved design definition. At E-PROPS, the Part-21G POA is currently in progress (under instruction in France via OSAC within the EASA system). See also: our workshops and production equipment.
2) DOA – Part 21 Subpart J (Design Organisation Approval) – Design
The DOA is the Design Organisation Approval: it recognises an organisation's capability to design and substantiate compliance (airworthiness) of a product, as well as its evolutions (changes/repairs), in accordance with Part-21. The Part-21J DOA of E-PROPS is currently under instruction with EASA.
3) TC – Type Certificate – Product certification
A Type Certificate (TC) is an EASA certificate confirming that a propeller model or range complies with its certification basis (technical requirements + demonstration of compliance with a reference standard). Obtaining a TC requires a complete test campaign, including structural testing and extensive vibration testing.
E-PROPS already holds an EASA Type Certificate P.512. The range of three-blade propellers for geared engines DURANDAL - EPGU3 was certified by EASA in March 2023 under the CS-22 Subpart J standard.
=> EASA P.512 (EPGU3), dated 2 March 2023
=> Available on the EASA website: EASA.P.512 – E-Props EPGU3 series propeller
=> EPGU3 installation and maintenance manual
The TC for the ASCALON range (2- and 3-blade, for direct-drive engines) is currently under instruction by EASA. Further TC applications, for other E-PROPS propeller ranges, will follow.
4) STC – Supplemental Type Certificate – Installation (aircraft + engine + propeller)
An STC is an EASA approval for a major modification to an already certified product. A propeller STC is specific to each combination (airframe + engine + propeller) and requires a dedicated test campaign to demonstrate compliance in that configuration. Prerequisite: holding the TC (or an equivalent certification basis) for the propeller range concerned.
5) Part-145 – Maintenance Organisation Approval – Maintenance
Part-145 is the Maintenance Organisation Approval (repair/maintenance) to ensure the continuing airworthiness of aeronautical products and components. E-PROPS plans to apply for a Part-145 approval for propeller maintenance.
Certification is at the heart of E-Props' approach: it is a mark of seriousness, industrial reliability and quality-system maturity, directly benefiting customers, integrators and certification authorities. In 2026, seven engineers are dedicated to these activities, reflecting the company's human and technical commitment to these demanding processes.
E-PROPS propellers (DURANDAL, EXCALIBUR, GLORIEUSE ranges) meet the ASTM F2506-26 standard for Light Sport Aircraft (LSA).
The ASTM F2506-26 standard sets minimum requirements for the design, testing and quality assurance of fixed-pitch, ground-adjustable and in-flight variable-pitch propellers for LSA-regulated light aircraft. Traction testing, mechanical strength measurement, fatigue testing, endurance testing and teardown inspections were carried out to meet the prescribed requirements.
Service Bulletins are issued by manufacturers of aeronautical products. They are established to warn users of a technical issue, a novelty or an improvement to an aeronautical product, and to convey technical information about the use of that product. E-PROPS Service Bulletins are listed below.
Subject: corrective action for certain three-blade DURANDAL propellers manufactured in late 2019, fitted with titanium leading-edge protections.
Affected propellers: 27 DURANDAL propellers for tractor ultralights fitted with Rotax 912 / 912S engines.
Reason: risk of progressive debonding of the blade leading-edge protections.
Action: return the blades, or preferably the complete propeller, to E-Props within 30 days for replacement and re-bonding of the titanium leading-edge protections. No immediate grounding required.
Concerns exclusively the Excalibur-5 (5-blade propeller) when mounted on the Super Petrel XP with Rotax 915iS & 916iS engines.
Reminder of assembly, tightening and verification instructions for hub screws on V12 EXCALIBUR-6 propellers [1/2].
Reminder of assembly, tightening and verification instructions for hub screws on V12 EXCALIBUR-6 propellers [2/2].
Download the bulletin (French) — DGAC information bulletin ref. BI 2020-ULM-01, revision 1 (French)
The LAA — Light Aircraft Association, United Kingdom — has published Mandatory Technical Directive MTD-02-2026, applicable to aircraft operated in the United Kingdom under an LAA Permit to Fly and fitted with a three-blade E-Props DURANDAL propeller with a HexMc® hub. This directive requires identification of the affected hubs, either by the serial numbers listed in the document or by visual inspection, followed by an inspection of the hub to detect any cracks, with particular attention to the periphery of the hub and to the area around the blade clamping bolts. If a crack is found, the LAA requires the hub to be replaced before any further flight.
E-Props acknowledges the publication of this directive, but does not share the LAA's analysis regarding the level of risk associated with the observed phenomenon. Based on the technical evidence available, E-Props considers that the observed marks correspond to resin pockets located on the periphery of the hub, with no demonstrated impact on mechanical integrity, blade retention, or flight safety. E-Props points out that these areas are not located in the main load path, and that no mechanical, structural or safety incident related to the integrity of these hubs has been reported to date.
Here is the E-Props analysis: HEP-2026-0474.pdf.
This directive falls under the LAA's own authority for aircraft operating under its Permit to Fly regime in the United Kingdom. E-Props remains available to assist owners, inspectors and authorities with hub identification, technical analysis of reported cases, and the supply of replacement parts if required.
A Service Letter is issued to draw attention to a piece of information.
Is your E-Props propeller not yet listed on a DULV or DAeC sheet (see below) for your specific aircraft/engine combination? This means an additional approval (EMZ) must be requested in Germany, including a mandatory on-site noise test. As a French company, E-Props is not authorised to carry out this German acoustic test itself.
To support flying clubs and pilots through this process, E-Props offers an attractive commercial arrangement: the propeller is purchased at full price, and part of its cost is refunded once the German approval has been obtained. This is E-Props' standard procedure for this type of request in Germany — please get in touch with us if you are in this situation, at helices@e-props.fr.
The DULV (Deutscher Ultraleichtflugverband), mandated by the German Federal Ministry of Transport, issues the "Gerätekennblätter": the type data sheets that define, for each ultralight aircraft approved in Germany, its approved engine/propeller configuration. This German approval is an important reference in Germany and in many Central and Eastern European countries. Below is the list of configurations approved by the DULV with an E-Props propeller, with a link to each official data sheet:
| Manufacturer | Model | Engine | E-Props propeller | Noise (dB) | Kennblatt no. |
|---|---|---|---|---|---|
| Aeroprakt Ltd. | A32 | Rotax 912 S, ULS, FR | E-Props GLOR-3-175-C8-T | 69,81 dB | 978-21 3 |
| Aeroprakt Ltd. | A32 | Rotax 912 iS / iSc Sport | E-Props GLOR-3-175-C8-T | 69,81 dB | 986-21 2 |
| Altus Aero KFT - Krisztian Dolhai | Altus ST | Rotax 912 S, ULS, FR | E-Props DUR-2-170-C8-T | 62,5 dB | 1015-25 1 |
| SIA "SMART AERO" - Juris Libmanis | Belmont DW200 | Rotax 912 S, ULS, FR | E-Props DUR-3-175-C4-T | 66,6 dB | 999-23 1 |
| SIA "SMART AERO" - Juris Libmanis | Belmont DW200 | Rotax 912 iS 2 Sport / iSC 2 Sport | E-Props DUR-3-175-C4-T | 66,6 dB | 999-23 5 |
| SIA "SMART AERO" - Juris Libmanis | Belmont DW210 RG | Rotax 912 S, ULS, FR | E-Props DUR-3-175-C4-T | 66,6 dB | 1005-23 1 |
| SIA "SMART AERO" - Juris Libmanis | Belmont DW210 RG | Rotax 914 UL | E-Props GLOR-3-170-C8-T | 58,01 dB | 1005-23 5 |
| BLACKWING Sweden AB - Niklas Anderberg | BLACKWING | Rotax 915 iS / iSC | E-Props Glorieuse 3 | 60,7 dB | 960-18 11 |
| BLACKWING Sweden AB - Niklas Anderberg | BLACKWING | Rotax 915 iS / iSC | E-Props Glorieuse 3 | 60,7 dB | 960-18 12 |
| BLACKWING Sweden AB - Niklas Anderberg | BLACKWING | Rotax 916 iS | E-Props Glorieuse 3 | 62,5 dB | 960-18 13 |
| BLACKWING Sweden AB - Niklas Anderberg | BW650SW | Rotax 916 iS | E-Props Glorieuse 3 | 62,5 dB | 1018-25 1 |
| ellipse aero s.r.o. | Ellipse Spirit | Rotax 912 S, ULS, FR | E-Props DUR-3-170-C4-T | 60,3 dB | 972-20 2 |
| Ing. Nando Groppo S.r.l. | G70 | Rotax 912 S, ULS, FR | E-Props 3-Blade Rotax912 S | 69,7 dB | 957-18 3 |
| Ing. Nando Groppo S.r.l. | G70 | Rotax 912 iS / iSc Sport | E-Props 3-Blade Rotax912 S | 69,7 dB | 957-18 9 |
| Ing. Nando Groppo S.r.l. | G70 | Rotax 912 iS / iSc Sport | E-Props Glorieuse | 64,2 dB | 957-18 12 |
| Ing. Nando Groppo S.r.l. | G70 | Rotax 912 S, ULS, FR | E-Props Glorieuse | 64,2 dB | 957-18 13 |
| Ing. Nando Groppo S.r.l. | G70 | Rotax 914 UL | E-Props GLOR-3-175-C8-T | 69,2 dB | 957-18 14 |
| Ing. Nando Groppo S.r.l. | G70 TD | Rotax 912 iS / iSc Sport | E-Props Glorieuse | 64,2 dB | 1014-25 1 |
| Ing. Nando Groppo S.r.l. | G70 TD | Rotax 912 S, ULS, FR | E-Props Glorieuse | 64,2 dB | 1014-25 2 |
| Kitplanes for Africa (Pty) Ltd. - Stefan Coetzee | KFA Explorer UL 600 Bugrad | Rotax 912 iS / iSc Sport | E-Props GLOR-3-170-C8-T | 67,1 dB | 1009-24 6 |
| Kitplanes for Africa (Pty) Ltd. - Stefan Coetzee | KFA Explorer UL 600 Spornrad | Rotax 912 iS / iSc Sport | E-Props GLOR-3-170-C8-T | 67,1 dB | 968-19 6 |
| Orličan s.r.o. | M8 Eagle | Rotax 914 UL | E-Props GLOR-3-175-C8-T | 63,7 dB | 1007-23 2 |
| Costruzioni Aeronautiche Tecnam S.p.A. | P 92 Echo MKII | Rotax 912 iS 2 Sport / iSC 2 Sport | E-Props DUR-3-170-C4-T | 69,3 dB | 974-20 4 |
| Blackshape S.p.A. | Prime BS100 | Rotax 915 iS / iSC | E-Props Glorieuse | 64,5 dB | 883-12 4 |
| SHARK.AERO s.r.o. | SHARK 600 T | EP914Ti_Gen2 | E-Props Glorieuse 3 | 68,1 dB | 1028-26 1 |
| Air Lony - Petr Lonský | Skylane | Rotax 914 UL | E-Props DUR-3-190-C4-T | 59,1 dB | 788-10 6 |
| Aerospool, spol. s.r.o. | WT 9 600 NG FG | Rotax 916 iS | E-Props GLOR-3-175-C9-T | 61,3 dB | 993-22 3 |
| Aerospool, spol. s.r.o. | WT 9 600 NG RG | Rotax 916 iS | E-Props GLOR-3-175-C9-T | 61,3 dB | 994-22 3 |
| Niki Rotor Aviation - Miglena Nikolova | Kallithea | Rotax 914 UL | E-Props Excalibur-6 | 65,3 dB | 964-18 1 |
| Niki Rotor Aviation - Miglena Nikolova | Kallithea | Rotax 912 S, ULS, FR | E-Props Excalibur-6 | 67,5 dB | 964-18 2 |
| TL Ultralight | TL96 Sting | Rotax 912 S, ULS, FR | E-Props GLOR-3-180-C8-T | 59,6 dB | EMZ 47 |
The DAeC (Deutscher Aero Club), through its Air Sports Equipment Office (Luftsportgeräte-Büro), remains fully entitled to issue approvals and "Gerätekennblätter" for ultralight aircraft in Germany, just like the DULV. In practice, most new applications are nowadays filed with the DULV, which is more service-oriented. Here are the configurations approved by the DAeC with an E-Props propeller:
| Manufacturer | Model | Engine | E-Props propeller | Noise (dB) | Kennblatt no. |
|---|---|---|---|---|---|
| Czech Aircraft Works s.r.o. | Zenair Zodiac CH-601XL | Rotax 912 S/ULS/ULSFR | E-Props Durandal 100 L | 59.6 dB | 61196 |
| ZENAIR Ltd. | Zenair Zodiac CH-601XL (from 2007) | Rotax 912 S/ULS/ULSFR | E-Props Durandal 100 L | 59.6 dB | 61196.1 |
| ZENAIR Ltd. | Zenair Zodiac CH 650 E | Rotax 912 S/ULS/ULSFR | E-Props Durandal 100 L | 59.6 dB | 61196.2 |
| I.C.P. srl | Zenair Zodiac CH 650 Ei | Rotax 912 S/ULS/ULSFR | E-Props Durandal 100 L | 59.6 dB | 61196.3 |
| ZALL JIHLAVAN airplanes s.r.o. | JA-400 Skyleader | Rotax 912/UL | E-Props Durandal 80-M | 59.6 dB | 61249 |
| Comco Ikarus GmbH | Ikarus C42 C / CS | Rotax 912 S/ULS | E-Props DUR-3-170-C4-T | 66.6 dB | 66141.7 |
| I.C.P. Srl | Savannah SR | Rotax 912 S/ULS | E-Props V20-DUR-3-175-C4-T | 68.9 dB | 66170 |
| I.C.P. Srl | Savannah SR | Rotax 912 S/ULS | E-Props Glorieuse GLOR-3-175-C8-T | 68.5 dB | 66170 |
| Alpi Aviation S.R.L. | Pioneer 300 | Rotax 912 iS/iSC | E-Props Glorieuse-3-175-C8-T | 68.9 dB | 66187 |
| Alpi Aviation S.R.L. | Pioneer 300 | Rotax 915 iS3A | E-Props Glorieuse-3-175-C8-T | 59.5 dB | 66187 |
| Tomark spol s.r.o. | SD4 Viper (600 kg) | Rotax 912 S2/ULS2 | E-Props Durandal DUR-3-170-C4-T | 63.4 dB | 66220 |
| Breezer Aircraft GmbH & Co. KG | Breezer Sport (600 kg) | Rotax 915 iS/iSC | E-Props Glorieuse GLR-3-175-C9-T | 59.3 dB | 66250 |
| Breezer Aircraft GmbH & Co. KG | Breezer Sport (600 kg) | Rotax 916 iS/iSC | E-Props Glorieuse GLR-3-175-C9-T | 61.6 dB | 66250 |
| BRM AERO s.r.o. | Bristell LSA / LSA-K | Rotax 915 iS | E-Props GLOR-3-175-C8-T / C9-T | 58.3 dB | 66253 |
| BRM AERO s.r.o. | Bristell LSA / LSA-K | Rotax 916 iS | E-Props GLOR-3-175-C8-T / C9-T | 61.3 dB | 66253 |
| ZALL JIHLAVAN airplanes s.r.o. | JA-400 Skyleader 400 (600 kg) | Rotax 912 S/ULS/ULSFR | E-Props DUR-3-170-C4-T | 65.9 dB | 66255 |
| ZALL JIHLAVAN airplanes s.r.o. | JA-600 Skyleader 600 (600 kg) | Rotax 912 S/ULS | E-Props DUR-3-170-C4 | 66.6 dB | 66256 |
| Carbon Design s.r.o. | FM250 Vampire 600 | Rotax 912 S/ULS | E-Props DUR-3-175-C4-T | 62.7 dB | 66262 |
| Innovaviation s.r.l. | FX1 | Rotax 912 ULS | E-Props DUR-3-175-C4-T | 58.4 dB | 66268 |
| GRYPHEN Aircraft Industries S.r.l. | Gryphen Storch GI 10 / GI 20 | Rotax 912 S2/ULS2 | E-Props Durandal DUR-3-170-C4-T | 66.1 dB | 66269 |