Holders of and applicants for type certificates—Repairs.

CFR · 2024-01-01 · US · Title 14

(a) (1) A maximum type certificated passenger seating capacity of 30 or more; or (2) A maximum payload capacity of 7,500 pounds or more. (b) (1) Identify fatigue critical baseline structure for all airplane model variations and derivatives approved under the type certificate; and (2) Develop and submit to the responsible Aircraft Certification Service office for review and approval, a list of the structure identified under paragraph (b)(1) of this section and, upon approval, make the list available to persons required to comply with § 26.47 and §§ 121.1109 and 129.109 of this chapter. (c) (1) Review the repair data and identify each repair specified in the data that affects fatigue critical baseline structure identified under paragraph (b)(1) of this section; (2) Perform a DTE and develop the DTI for each repair identified under paragraph (c)(1) of this section, unless previously accomplished; (3) Submit the DT data to the responsible Aircraft Certification Service office or its properly authorized designees for review and approval; and (4) Upon approval, make the DTI available to persons required to comply (d) (1) Perform a DTE and develop the DTI. (2) Submit the DT data required in paragraph (d)(1) of this section for review and approval by the responsible Aircraft Certification Service office or its properly authorized designees. (3) Upon approval, make the approved DTI available to persons required to comply with §§ 121.1109 and 129.109 of this chapter. (e) (1) Develop re

official document · source cfr-2024 · id 14:§ 26.43