Application for Repair Design Approval (RDA)

Description

This service allows the beneficiaries to apply for a GACA Repair Design Approval (RDA) to be installed on Saudi registered aircraft under the provisions of GACAR Part 21 Subpart E “Repair Design Approvals”, other than repair design issued under Subpart C.

Audience
GACA certificated air carrier, air operator or repair station certificated under GACA/FAR Parts 121, 125, 135 or 145, or a GACA/FAR Part 91 Aircraft Owner/Operator who has engineering resources or can obtain engineering services under contract.
Pre-Requisites
1. GACA acceptance to support the project via response to the letter of intent.
2. Familiarity with the RDA Certification process.
Procedure
GACA AC 021-07 Alterations and Repairs.
Required Documents
1.GACA response to the Letter of Intent
2.Letter of application addressed to Airworthiness Manager.
3.GACA Form 8110-12 Application for Supplemental Type Certificate (STC) and Repair Design Approval (RDA).
4.Preliminary Certification plan including basis of certification.
5.Preliminary Compliance Checklist.
6.Master Data List - Draft.
7.Preliminary Certification Data (as applicable).
8.Preliminary Required Operating Data such as Aircraft Flight Manual Supplement (AFMS).
9.Preliminary Continued Airworthiness Data, includes, but is not limited to: (a) Instructions for Continued Airworthiness. (b) Airworthiness Limitations. (c) Electrical Wiring Interconnection System.
10.Proof of fee payment
Delivery Time
140 Business Days
Terms and Conditions
1. Refer to GACA AC 021-07 Alterations and Repairs. 2. The application for RDA may be subject to a sequencing process due to workload, which may impact the initiation of the project. 3. A GACA RDA project coordination meeting should take place AEAP.
Additional Help
Refer to GACA AC 021-07

Help Documents



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