Under specific circumstances, such as maintenance repositioning flights or check flights—special flight conditions must be defined to operate the aircraft safely and in compliance with regulations.
When a non-EASA aircraft manufacturer issues a No Technical Objection (NTO) or similar statement, EASA requires these be assessed and formalized by a DOA-approved organization before a Permit to Fly application can be submitted.
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 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 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.