AIRCRAFT PARTS THEREOF

Brand Owner (click to sort) Address Description
A TOUGH BIRD NORTH AMERICAN ROCKWELL CORPORATION Pittsburgh PA AIRCRAFT AND PARTS THEREOF;
AIRBUS DEUTSCHE AIRBUS GMBH ARABELLASTRASSE 30 8000 MUENCHEN 81 Germany AIRCRAFT AND PARTS THEREOF;
CITATION STALLION CESSNA AIRCRAFT COMPANY, THE 5800 East Pawnee Wichita KS 67218 AIRCRAFT AND PARTS THEREOF;
DRAGON DE HAVILLAND AIRCRAFT COMPANY LIMITED THE HATFIELD AERODROME HATFIELD AIRCRAFT AND PARTS THEREOF;
MOONEY MOONEY AIRCRAFT CORPORATION Louis Schreiner Field Kerrville TX 78028 AIRCRAFT AND PARTS THEREOF;
MOONEY MOONEY INTERNATIONAL CORP. 165 Al Mooney Rd Kerrville TX 78028 AIRCRAFT AND PARTS THEREOF;
MOONEY SOARING AMERICA AVIATION CORPORATION 1641 W. MAIN STREET, SUITE 220 ALHAMBRA CA 91801 AIRCRAFT AND PARTS THEREOF;
MOONEY MOONEY AVIATION COMPANY, INC. 165 AL MOONEY ROAD NORTH KERRVILLE TX 78028 AIRCRAFT AND PARTS THEREOF;
MOONEY MOONEY AIRPLANE COMPANY, INC. LOUIS SCHREINER FIELD KERRVILLE TX 780290072 AIRCRAFT AND PARTS THEREOF;
MOONEY AEROSTAR AIRCRAFT CORPORATION OF TEXAS P.O. BOX 72 KERRVILLE TX 7808 AIRCRAFT AND PARTS THEREOF;
MUSTANG TEXTRON INNOVATIONS INC. 40 Westminster Street Providence RI 02903 AIRCRAFT AND PARTS THEREOF;
PARADIGM SAFEAIR AEROSPACE CORPORATION 1140 Centre Rd. Auburn Hills MI 48326 Aircraft and parts thereof, namely, propeller ducting, airplane wings and fuselages;
SABRE NORTH AMERICAN ROCKWELL CORPORATION Pittsburgh PA AIRCRAFT AND PARTS THEREOF;SABER;
TBM TBM NORTH AMERICA, INC. 8901 WETMORE ROAD SAN ANTONIO TX 78216 AIRCRAFT AND PARTS THEREOF;
TRIDENT DE HAVILLAND AIRCRAFT COMPANY, LIMITED THE HATFIELD AIRCRAFT AND PARTS THEREOF;
 

Where the owner name is not linked, that owner no longer owns the brand

    
Technical Examples
  1. The door comprises a panel (14) formed from two rigid parts (14a, 14b) hinged to each other edge to edge. A first part (14a) of these two parts is connected to the aircraft structure through a pivot pin (20) and a control means (22) is inserted between this first part (14a) and the structure. A kinematic control mechanism (16) connects the two parts (14a, 14b) to the aircraft structure, so as to enable progressive and controlled folding of these parts when opening the door. Thus the landing gear door can be opened and closed without any risk of it coming into contact with the wheels when the landing gear is extended.