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Last Updated: Apr 25, 2025 | Study Period: 2023-2030
Aircraft Landing Gear actuators are manufactured from complete hog outs or finish machined from forgings to a one piece body. Housings are commonly made out of stainless steel for strength and anti-corrosive properties.
High strength and wear resistant materials are utilized for the piston, end gland, and bearings to ensure longevity and reliable service without the need for overhauls or scheduled maintenance.
Additional features can be incorporated, such as snubbing effects in the extend/retract directions and regeneraton circuits to minimize the load on aircraft hydraulic systems.
The rising number of passenger transport and increased aircraft deliveries due to upgrades in the aircraft. Advances in existing aircraft types and new technological developments to improve aircraft performance and efficiency are the factor driving the market growth of the Aircraft Landing Gear Market.
The Global Aircraft Landing Gear Market report provides a holistic evaluation of the market.
The primary factors driving the market growth are increasing the adoption of modern aircraft due to their improved properties and fuel efficiency.
In addition, with the growing demand for fleet expansion and the development of low-cost and ultra-low-cost airlines, the market is witnessing a surge in orders for commercial aircraft, which is expected to drive this market.
In addition, increased government spending on military aircraft to strengthen defense capabilities could also contribute to market growth.
Also, increasing the adoption of UAVs for military operations increases the market growth of the Aircraft Landing Gear Market. Suspension components such as brakes, wheels, and actuation systems can wear out later and need to be serviced regularly.
The Global Aircraft Landing Gear Actuator market accounted for $XX Billion in 2022 and is anticipated to reach $XX Billion by 2030, registering a CAGR of XX% from 2023 to 2030.
Tactair's - Tactair's Main Landing Gear Retraction Actuators are designed to provide retraction and extension forces while maintaining light weight and reliability.
Tactair designed and manufactures retraction actuators for regional jet, business jet as well as smaller aircraft and rotorcraft markets.
Universal Test Rig for conducting Performance Acceptance Tests (PAT) for all the actuators of a passenger aircraft landing gear.
The tests include Proof pressure and Static Test, Static load compression test, Static load tensile test, Dynamic leakage test, Antagonistic Test - Extension, Antagonistic Test - Retraction, Leakage Tests(including long duration testing), Dampening measurement for Aircraft Landing gear actuators
Sl no | Topic |
1 | Market Segmentation |
2 | Scope of the report |
3 | Abbreviations |
4 | Research Methodology |
5 | Executive Summary |
6 | Introduction |
7 | Insights from Industry stakeholders |
8 | Cost breakdown of Product by sub-components and average profit margin |
9 | Disruptive innovation in the Industry |
10 | Technology trends in the Industry |
11 | Consumer trends in the industry |
12 | Recent Production Milestones |
13 | Component Manufacturing in US, EU and China |
14 | COVID-19 impact on overall market |
15 | COVID-19 impact on Production of components |
16 | COVID-19 impact on Point of sale |
17 | Market Segmentation, Dynamics and Forecast by Geography, 2023-2030 |
18 | Market Segmentation, Dynamics and Forecast by Product Type, 2023-2030 |
19 | Market Segmentation, Dynamics and Forecast by Application, 2023-2030 |
20 | Market Segmentation, Dynamics and Forecast by End use, 2023-2030 |
21 | Product installation rate by OEM, 2023 |
22 | Incline/Decline in Average B-2-B selling price in past 5 years |
23 | Competition from substitute products |
24 | Gross margin and average profitability of suppliers |
25 | New product development in past 12 months |
26 | M&A in past 12 months |
27 | Growth strategy of leading players |
28 | Market share of vendors, 2023 |
29 | Company Profiles |
30 | Unmet needs and opportunity for new suppliers |
31 | Conclusion |
32 | Appendix |