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CS 25.625 Fitting factors

Large Aeroplanes (CS-25) · CS-25 · EAR revision 26 Jan 2023

IRImplementing rule

CS 25.625Fitting factors

For each fitting (a part or terminal used to join one structural member to another), the following apply:

(a)For each fitting whose strength is not proven by limit and ultimate load tests in which actual stress conditions are simulated in the fitting and surrounding structures, a fitting factor of at least 1·15 must be applied to each part of –

(1)The fitting;

(2)The means of attachment; and

(3)The bearing on the joined members.

(b)No fitting factor need be used –

(1)For joints made under approved practices and based on comprehensive test data (such as continuous joints in metal plating, welded joints, and scarf joints in wood); or

(2)With respect to any bearing surface for which a larger special factor is used.

(c)For each integral fitting, the part must be treated as a fitting up to the point at which the section properties become typical of the member.

(d)For each seat, berth, safety belt, and harness, the fitting factor specified in CS 25.785(f)(3) applies.

IR · CS 25.625 — CS-25 · ED Decision 2003/2/RM · CS-25 Easy Access Rules · EAR revision 26 Jan 2023

All rules in SUBPART D – DESIGN AND CONSTRUCTION

Consolidated from the EASA Easy Access Rules (revision 26 Jan 2023, extracted 17 Aug 2026) for convenience. Not the official publication — verify against the Official Journal of the European Union and the EASA publications before operational use.

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