Generation Global hold the following certificates and approvals:

• EASA Part 21G Production Organization Approval
• NZCAA Part 148 Manufacture Organization Certificate
• NZCAA Part 145 Maintenance Organization Certificate
  

The following certification method is acceptable for aircraft registered in EASA approved countries:

• Design Approval: EASA Part 21J minor design change approval in accordance with EASA Part 21A.91
• Release Documentation: EASA Form 1 Authorized Release Certificate (ARC).

NOTE: Option to supply the parts with a Certificate of Conformity and Burn Certificates is available for installers who wish to arrange their own installation approval.

The following certification method is acceptable for FAA registered aircraft:

• Design Approval: EASA Part 21J minor design change approval in accordance with EASA Part 21A.91. Under paragraph 3.2 of the FAA-EASA Bilateral agreement, FAA automatically accept EASA Part 21J design changes classified as a ‘minor change’ in accordance with EASA Part 21A.91 (equivalent to a FAA 8110-3) as acceptable data and require no further investigation or application for validation.
• Release Documentation: EASA Form 1 Authorized Release Certificate (ARC). Under paragraph 3.5.1 of the
  FAA-EASA Bilateral agreement, FAA automatically accept an EASA form 1 Authorized Release Certificate (ARC) as the equivalent to a FAA Form 8130-3 Authorized Release Certificate (ARC) and require no further investigation.
  

NOTE: Option to supply the parts with a Certificate of Conformity and Burn Certificates is available for installers who wish to arrange their own installation approval.

The following certification method is acceptable for TCAA registered aircraft:

• Design Approval: EASA Part 21J minor design change approval in accordance with EASA Part 21A.91. Under paragraph 3.3.5.3 of the TCAA-EASA Bilateral agreement, TCAA automatically accept EASA Part 21J design changes as acceptable data and require no further investigation or application for validation.
• Release Documentation: EASA Form 1 Authorized Release Certificate (ARC). Under paragraph 5.3.2.1 of the TCCA-EASA Bilateral agreement, TCAA automatically accept an EASA form 1 Authorized Release Certificate (ARC) as the equivalent to a TCAA Form 1 Authorized Release Certificate (ARC) and require no further investigation.

NOTE: Option to supply the parts with a Certificate of Conformity and Burn Certificates is available for installers who wish to arrange their own installation approval.

The following certification method is acceptable for CASA registered aircraft:

• Design Approval: CASA Engineering Order in accordance with CASR Part 21.437.
• Release Documentation: NZCAA Form 1 Authorized Release Certificate (ARC).

NOTE: Option to supply the parts with a Certificate of Conformity and Burn Certificates is available for installers who wish to arrange their own installation approval.

The following certification method is acceptable for NZCAA registered aircraft:

• Design Approval: NZCAA Form CAA 337 Design Change Approval in accordance with NZCAA Part 21.81.
• Release Documentation: NZCAA Form 1 Authorized Release Certificate (ARC).

NOTE: Option to supply the parts with a Certificate of Conformity and Burn Certificates is available for installers who wish to arrange their own installation approval.

The following certification method is acceptable for JCAB registered aircraft:

Design Approval: EASA and the Civil Aviation Bureau, Ministry of Land, Infrastructure, Transport and Tourism Japan (JCAB) have signed a Working Arrangement which states that an EASA approval of a minor change will be automatically accepted by JCAB without the need for further showing of compliance. (Ref Article 13. 3)

Release Documentation: EASA Form 1 Authorized Release Certificate (ARC) are accepted by JCAB.

NOTE: Option to supply the parts with a Certificate of Conformity and Burn Certificates is available for installers who wish to arrange their own installation approval.

Generation Global maintains in-house test facilities as well as using external approved test facilities to accomplish all required testing and certification.

Flammability

• 14CFR25.853(a) Bunsen Burner test for all cushion/cover individual materials
• 14CFR25.853(c) Oil Burner test for cushion assembly-foam, fireblocking, dress cover

Flotation

• TSO C72(c) Flotation Cushion testing

Crash Test

• TSO C127(a) Dynamic Seat Crash Testing