Client: VAZAR

Client Request: The DHC-3 Otter had a history of failures in the elevator servo-tab bellcrank.  VAZAR agreed to address this issue on their turbine conversion to increase safety of the aircraft and meet the newer 23.629 requirement of flutter free after a single failure.  Volant Technica was asked to develop the fix for the servo tab.

Project Summary:  Volant Technica, (a precursor company to Fliegen Works,) worked with the FAA to address this service difficulty and produced the design data, developed loads and a structural test proposal, then DER witnessed the structural test.  We also wrote the flight test plan and helped with the issuance of the TIA.  The STC is a method of compliance to AD 2004-05-01.  Fliegen Works currently holds PMA for fabrication of the redundant servo tab. that includes a 2^nd control rod and other modification to fix in-service failure problem.

Results: STC SA01059SE was granted to VAZAR (as American Aeromotives) and is licensed to Fliegen Works for manufacture under PMA PQ2380NM.

 Client: Wilson Construction Company

 Client Request: The linemen working from a rotorcraft needed a handle with an anchor point for their safety harness.

Project Summary: We provided design, detail drawings, structural substantiation, as well as a rotorcraft flight manual supplement –(RFMS).  This included enough data for a coordinated field approval with the assistance of Dave Swan.

Results: Multiple 337 approvals to install handle on helicopters owned by the client.

 Project Name: Rudder Tab On A-1 Series Blimps

 Client: American Blimp Company

 Client Request:  The client requested a fix to balance the aerodynamic torque created by an installed Lightsign on the left side of the blimp’s envelope. 

 Project Summary: We did the preliminary sizing and worked with ABC on the detail design.  Fliegen Works developed the aerodynamic loads, produced a structural test proposal and then DER witnessed the tests.  The design of a fixed tab on a Rudder of  ABC A-1 series airship was a challenge since a number of engineering estimations were made.  From minimal available blimp flight and aerodynamic data and old NACA data an analysis was performed to design a fixed rudder tab that biased the rudder to compensate for the unsymmetrical drag on  the airship due to the Lightsign on one side of the airship.  This was a major change to the type design by the type certificate holder. 

Results: Successful flight testing, installation and approval of rudder tab on A-1 series blimp.  Pilot force required to maintain straight flight reduced acceptable levels. Rather than complex CFD a simple method combined with a little guesswork was applied.  Minimal time and cost was required to produce the required results in this manner.