MILITARY AIRCRAFT F-35. Photo courtesy U.S. Air Force/Airman 1st Class Caleb Worpel. Lockheed Martin photo/phaedra Loftis F-35 SUSTAINMENT SERVICES

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MILITARY AIRCRAFT F- Photo courtesy U.S. Air Force/Airman st Class Caleb Worpel Lockheed Martin photo/phaedra Loftis F- SUSTAINMENT SERVICES

Photo courtesy U.S. Air Force/Staff Sgt. Madelyn Brown MOOG F- GLOBAL SUSTAINMENT SERVICES Moog has an outstanding record for providing global sustain ment support on the world s current fleet of military aircraft including F-, F-, F/A-8, F-, Typhoon, Gripen, IDF and AMX. Through our expanding Global Sustainment operations we ensure the needs of domestic and international operators are met through a network of support facilities and regional experts. We offer a wide range of services from complete turnkey solutions to discrete services with flexible commercial options. We believe our most valuable offering is customer support, and we are committed to delivering a superior level of sustainment services for all of our customers. Moog is continuing this tradition, supplying the following services for the new th generation F- aircraft equipped with Moog s advanced systems. Turnkey Sustainment Services Technical Support and Training Forward Stocking of Assets Dedicated Engineering, Manufacturing, Repair and Overhaul Support Agile Responsive Global Logistics Support Public-Private Partnerships including Joint Depot Operations

FLIGHT CONTROLS INTEGRATOR & SUPPLIER Moog has a rich history in the F- Joint Strike Fighter as an OEM supplier and system integrator / prime contract holder for system design and development of the Primary Flight Control Actuation System (PFCAS). In addition to the PFCAS, which is comprised of the Electrohydrostatic Actuation System (EHAS) and Leading Edge Flap Actuation System (LEFAS) component systems, Moog also developed and is the OEM supplier for the F-C CV Wing Fold Actuation System (WFAS) and F-B STOVL Lift System Actuation Controls. ELECTROHYDROSTATIC ACTUATION SYSTEM (EHAS) OVERVIEW Eliminating the traditional tie to aircraft generated hydraulic power, the electronically controlled and driven Electrohydrostatic Actuators (EHA) provide fully integrated precision motion control of the primary flight control surfaces (flaperon, horizontal tail & rudder). Actuation system software and Electronic Control Units (EU s) provide the system interface to the aircraft electrical drive power and command/control functions of the aircraft Vehicle Management Computer (VMC). Integration of these components provides complete system control. LEADING EDGE FLAP ACTUATION SYSTEM (LEFAS) OVERVIEW Utilizing similar Electronic Control Units (EU s) from the EHAS system, the Leading Edge Flap Actuation System (LEFAS) provides fully integrated precision motion control of the leading edge flap flight surfaces. System components include electronically controlled and driven rotary Power Drive Units (PDU), Asymmetry Brakes, and Outboard Position Sensors (OPS). F-C CV aircraft also include a Foldbox Assembly to act in conjunction with the Wingfold Actuation System. WINGFOLD ACTUATION SYSTEM (WFAS) OVERVIEW This fully integrated, electronically controlled and driven rotary transmission system acts as powered hinge to either fold or spread the outer wing tips on the F-C CV aircraft. Courtesy U.S. Air Force Courtesy USAF/ SSGT Joely M Santiago U.S. Navy photo courtesy of Lockheed Martin by Andy Wolfe Courtesy U.S. Air Force Photographer/Alex R Lloyd LIFT SYSTEM ACTUATION CONTROLS The hovering ability of the F-B STOVL aircraft is provided by the lift system, which combines a thrust vectoring nozzle that directs main engine exhaust downward to generate aft vertical lift and a centrally mounted lift fan to counterbalance forward vertical lift. Moog is the OEM supplier of several key system components which include the Three-Bearing Swivel Module (BSM) and the Lift Fan Variable Area Vane Box Nozzle (VAVBN) & Variable Inlet Guide Vane (VIGV) actuation controls. These complex electronically controlled hydraulic and fueldraulic servoactuators are specially designed for operation in extreme temperature and vibration environments.

F-A/B PRIMARY FLIGHT CONTROL AND LEADING EDGE FLAP SYSTEM *Part location is approximate Leading Edge Flap Control Unit Outboard Position Sensor Leading Edge Power Drive Unit Flaperon EHA Asymmetry Brake Horizontal Tail Electronic Control Unit

F-B LIFT SYSTEM 7 8 *Part location is approximate Variable Inlet Guide Vane Linear Actuator Variable Area Vane Box Nozzle Control Valve Block Variable Area Vane Box Nozzle Linear Actuator Nozzle Cooling Valve Actuator Variable Area Vane Box Nozzle Rotary Actuator 7 Bearing Swivel Module Variable Inlet Guide Vane Control Valve Block 8 Transfer Gearbox

F-C PRIMARY FLIGHT CONTROL, LEADING EDGE FLAP AND WINGFOLD SYSTEM 7 8 9 0 *Part location is approximate Leading Edge Flap and Rudder Electronic Control Unit Wingfold Transmission Leading Edge Flap Power Drive Unit 7 Flaperon EHA Fold Box 8 Flaperon Electronic Control Uit Asymmetry Brake 9 Rudder EHA Outboard Position Sensor 0 Horizontal Tail Electronic Control Unit

HARDWARE FOR F- VARIANT SYSTEMS A Variant B Variant C Variant Nomenclature Qty Per S/S Moog P/N Moog P/N Moog P/N Primary Flight Control System Leading Edge Flap Electronic Control Unit CB80-00 CB80-00 CB80-00 Horizontal Tail Electronic Control Unit CB800-00 CB800-00 CB800-00 Flaperon Electronic Control Unit (C Variant Only) N/A N/A CB800-00 Rudder Electronic Control Unit (C Variant Only) N/A N/A CB80-00 Flaperon EHA C89-00 CA77-00 CA88-00 Rudder EHA (Left Hand) (C Variant Only) N/A N/A CA89-0 Rudder EHA (Right Hand) (C Variant Only) N/A N/A CA080-0 Leading Edge Flap Drive System Electronic Power Drive Unit C-00 C-00 C87-00 Asymmetry Brake C99-00 C8-00 C-00 Outboard Position Sensor C-00 C-00 C90-00 Fold Box (C Variant Only) N/A N/A C89-00 Lift System (B Variant Only) Variable Inlet Guide Vane Linear Actuator N/A P0A000-0 N/A Variable Inlet Guide Vane Control Valve Block N/A P0A000-0 N/A Variable Area Vane Box Nozzle Linear Actuator N/A PA000-0 N/A Variable Area Vane Box Nozzle Rotary Actuator N/A P0A000-0 PA000-0 N/A Variable Area Vane Box Nozzle Control Valve Block N/A PA000-0 PA000-0 PA000-0 N/A Transfer Gearbox N/A P8A000-0 N/A Nozzle Cooling Valve Actuator N/A P9A000-0 N/A Bearing Swivel Module N/A PA000-0 P7A000-0 N/A Wingfold Actuation System (C Variant Only) Wingfold Transmission N/A N/A C8-00

Moog Inc. East Aurora, New York 7.-000 www.moog.com/aircraft 08 Moog, Inc. All rights reserved. Product and company names listed are trademarks or trade names of their respective companies. Form 00-8 08