EUROLAB Laboratory provides accredited testing and conformity assessment service under the MIL DTL 27422 F standard, This specification meets the requirements and validation tests of crash-proof, ballistic-tolerant fuel cells for use on fixed-wing and rotary-wing aircraft (including pitch rotor). covers. Exact design criteria such as fuel cell dimensions, overall weight and interface requirements will depend on the intended aircraft specified in the contract or purchase order.
Aircraft systems covered by this standard are to be designed to minimize practically all aircraft damage while minimizing the number and severity of injuries and preventing passenger deaths during collision effects. This will be achieved by selecting the most effective mix of crash resistance factors and applying their requirements. For example, the individual energy attenuation provided by the landing gear, structure and seats can be adjusted to achieve the desired system crash response using a systems analysis approach.
EUROLAB Laboratory provides accredited testing services within the scope of the Test Standard for MIL DTL 27422 F Tank, Fuel, Impact Resistant, Ballistic Tolerant Aircraft.
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