Under certain circumstances, special conditions are required to operate the aircraft, for example for maintenance reposition fligth or a check flight. A non EASA aircraft manufacturer may issue No techical objection or similar statement that requires a coverage by a EASA DOA organisation.
This may need to be processed by a DOA organisation before it can be presented to EASA or local office for the application for a Permit to Fly.
Interior configuration modification to be completed per Bombardier Completion Center Master Drawing List ML100628, Rev D, dtd 9/7/01. Approved for serial number 9040 ONLY. Aircraft may not be offered for common carriage or used in revenue passenger service unless aft divans are placarded 'DIVAN MAY NOT BE OCCUPIED DURING TAXI, TAKEOFF OR LANDING.'
Reduced Max Take-off Weight to 75,000 LB, Reduced Max Landing Weight to 68,000 LB
EASA validation of Transport Canada STC SA16-110 at issue 1for:Installation, Conductive Antenna Gaskets. TCCA STC SA16-110
Installation of a Honeywell DU-875 or DU-875AF Liquid Crystal Display(LCD) including two Cursor Control Devices (CCDs),in accordance withLearjet, Inc. Learjet, Inc. Master Document List (MDL), Document NumberBAS67010045, Revision F, dated2 November 2017, or later approvedrevision. FAA STC ST00299BOAS AMENDED BY
Installation of a Crane Aerospace & Electronics Tire Sensor Assembly
Increasing efficiency of your aircraft maintenance by monitoring performance of the organization, identifying waste factors and eliminating these waste factors Something companies spend a lot of money on by hiring Lean consultants. Avilytics is able to do this in just a few seconds once it is connected to the systems you use in the organisation.
Installation of Crane Aerospace & Electronics Tire PressureSensor inplace of the existing tire fill valve. FAA STC NO. ST02293SE
Installation of BACN Mission Payload Integration in accordance with FAA Approved Master Drawing List 10-BD700-100, Revision āJā dated August 15, 2011, or later FAA approved revisions.