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SE145.0045 - EASA.21J.339 - SE.21G.0016 - LFS2007:47
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European Aviation Safety Agency

APPROVAL CERTIFICATE

EASA.21J.339

Pursuant to Regulations (EC) 216/2008 and (EU) 748/2012 and
subject to the conditions specified below, the Agency hereby
certifies

Bromma Air Maintenance AB
Hangar 4, Bromma Airport
5-168 67 Bromma
Sweden

as a DESIGN ORGANISATION

approved according to Part 21, Section A, Subpart J.

  1. The approval is limited to that specified in the enclosed Terms of Approval, and
  2. This approval requires compliance with the procedures specified in the Design Organisation Handbook, reference BAM Design Organisation Handbook, in the latest revision, and
  3. This approval is valid whilst the approved Design Organisation remains in compliance with Part21., Section A, Subpart J.
  4. Subject to compliance with the foregoing conditions, this approval shall remain valid until surrendered or revoked.
For the European Aviation Safety Agency,
Date of issue: 12 March 2015

Dominique ROLAND
Head of Design Organisations Department

 

Terms of Approval

Design Organisation Approval Certificate

EASA.21J.339

  1. Scope of work

    The holder of the Design Organisation Approval is entitled to design in accordance with the applicable type-certification basis, operational suitability data certification basis and environmental protection
    requirements as defined in Annex A.

  2. Privileges

    1. The holder of this design organisation approval shall be entitled to perform design activities under
      Part 21 and within its scope of approval.

    2. Subject to 21.A.257(b), the Agency shall accept without further verification compliance documents submitted by the holder of this design organisation approval for the purpose of obtaining, as per 21.A.263(b):
      1. [Not applicable]
      2. [Not applicable]
      3. a supplemental type-certificate
      4. [Not applicable]
      5. [Not applicable]

    3. The holder of this design organisation approval shall be entitled, within its terms of approval and under the relevant procedures of the design assurance system, as per 21.A.263(c):
      1. to classify changes to type-certificate and repairs as "major" or "minor"
      2. to approve minor changes to type-certificate and minor repairs
      3. to issue information or instructions containing the following statement: "The technical content of this document is approved under the authority of DOA ref. E4S4.21J.339"
      4. to approve minor revisions to the aircraft flight manual and supplements, and issue such
        revisions containing the following statement: "Revision No [YY] to AFM (or supplement) ref. [ZZ] is approved under the authority of DOA ref. E4S4.21J.339."
      5. [Not applicable]
      6. [Not applicable]
      7. [Not applicable]

  3. Obligations

    The holder of the Design Organisation Approval shall, as per 21..4.265:
    1. maintain the handbook in conformity with the design assurance system;
    2. ensure that this handbook is used as a basic working document within the organization;
    3. determine that the design of products, or changes or repairs thereof, as applicable, comply with
      applicable requirements and have no unsafe feature;
    4. except for minor changes or repairs approved under the privilege of paragraph 2(c), provide to the Agency statements and associated documentation confirming compliance with paragraph 3(c);
    5. provide to the Agency information or instructions related to required actions under Part 21 point 27.4.3B;
    6. [Not applicable];
    7. [Not applicable];

 

Date of issue: 22/06/2018
lain HIGGINS
Senior DOA Team Leader

 

Annex A

Scope of work

TC
STC
major changes
minor changes
major repairs
minor repairs
flight conditions
permit to fly
Large and small aeroplanes
Avionics
Autoflight systems
Communication systems
Diagnostic and Maintenance systems
lndicating, Alerting systems
Navigation systems
Recording systems
Surveillance systems
Cabin
Cabin interiors
Cargo compartments
Electrical cabin systems
External schemes, placards and markings
Flight deck interiors
Electrical Systems
Electrical generation / distribution systems
External lighting systems
Wireless transmission systems
Structures
Control surfaces / Moveables
Empennage
Engine mounts
Fuselage
Landing gears
Support for external equipment
Wings
Large and small rotorcraft
Avionics
Autoflight systems
Communication systems
Diagnostic and Maintenance systems
lndicating, Alerting systems
Navigation systems
Recording systems
Surveillance systems
Cabin
Cabin interiors
Cargo compartments
Electrical cabin systems
External schemes, placards and markings
Flight deck interiors
Electrical Systems
Electrical generation / distribution systems
External lighting systems
Wireless transmission systems
Powerplant and Fuel Systems
Fuelsystems
Structures
Control surfaces / Moveables
Engine mounts
Fuselage
Landing gears
Support for external equipment

 

List of products

[Not applicable]

 

Limitations

Limitations common to all products and activities

  1. Changes and repairs impacting products' noise and emissions characteristics are excluded.
  2. The technical field of Fuel Systems is limited to auxiliary fuel systems.
  3. Development of Operational Suitability Data excludes the OSD constituents CCD, FCD, MCSD and SIMD.