Manuals Combined Uh 60 Black Hawk Pilot Flight Training Engine Electrical Fuel System Instrument Crew Functions Visual Training Materials

Over 900 pages ... Just a sample of the contents: LANDING GEAR TERMINAL LEARNING OBJECTIVE ACTION: Determine the major components and operational characteristics of the UH-60 landing gear system. CONDITIONS: Given multiple choices, visual representations of the UH-60 landing gear system components, and applicable references. STANDARDS : Select from multiple choices, the major components and operating characteristics of the UH-60 landing gear system. SAFETY REQUIREMENTS- Use care when operating training aids and/or devices. RISK ASSESSMENT- Low. ENVIRONMENTAL CONSIDERATIONS- None. EVALUATION: This block of instruction will be tested on the UH-60 aviation subjects written examination I (011-1374). A minimum score of 70% is required for passing. LEARNING STEP / ACTIVITY 1 Identify the primary components and operational characteristics of the UH-60 main landing gear system. Crash Worthiness UH-60 Main Landing Gear System Description: conventional, non-retractable, reverse tricycle arrangement. Components: Drag beam. Axle assembly. Main shock strut. Main wheel assembly. Wheel brake. Drag Beam Drag Beam Switches Drag Beam Strut at Rest Strut Under High Impact Load Strut Airborne Kneeling Valves Main Wheel Tire Details Master Cylinders Slave Cylinders/Parking Brake Valve Parking Brake Schematic Brake Wear Check Check On Learning Question: The lower stage of the main landing gear struts is designed to absorb landing loads up to ____ feet per second. Answer: 10 LEARNING STEP / ACTIVITY 2 Identify the primary components and operational characteristics of the UH-60 tail landing gear system. UH-60 Tail Landing Gear System Tail landing gear. Operation. Tail wheel assembly. Swivels 360 degrees. Upper end of strut. Yoke of tail gear. Fork assembly. Split aluminum rim. Tail wheel lock system. Tail Landing Gear Assembly Tail Strut Tail Yoke and Fork Tailwheel Lock System Tail Wheel Lock Check On Learning Question: Power to operate the tail wheel lock system is provided through the ____ bus. Answer: DC essential. SUMMARY Identified the primary components and operational characteristics of the UH-60 main landing gear system. Identified the primary components and operational characteristics of the UH-60 tail landing gear system. BREAK TIME! POWERTRAIN AND ROTOR SYSTEM TERMINAL LEARNING OBJECTIVE ACTION: Determine the major components and operational characteristics of the UH-60 powertrain system. CONDITIONS: Given multiple choices, visual representations of the UH-60 powertrain system components, and applicable references. STANDARDS : Select from multiple choices, the major components and operating characteristics of the UH-60 powertrain system. SAFETY REQUIREMENTS- Use care when operating training aids and/or devices. RISK ASSESSMENT- Low. ENVIRONMENTAL CONSIDERATIONS- None. EVALUATION: This block of instruction will be tested on the UH-60 aviation subjects written examination I (011-1374). A minimum score of 70% is required for passing. ENABLING LEARNING OBJECTIVE A ACTION: Identify the operational characteristics and modules of the UH-60 main transmission system. CONDITIONS: Given multiple choices, visual representations of the UH-60 main transmission system, and applicable references. STANDARDS: Select from multiple choices, the characteristics of the UH-60 main transmission system. Main Transmission Location Main Transmission Components Input and Accessory Modules Freewheeling Unit Accessory Module Main Module Details Check On Learning Question: The UH-60 main transmission system consists of how many modules? Answer: 5 (five). ENABLING LEARNING OBJECTIVE B ACTION: Identify the characteristics of the UH-60 main transmission lubrication system components. CONDITIONS: Given multiple choices, visual representations of the UH-60 transmission lubrication system, and

Developed to replace the UH-1 Iroquis, Sikorsky s UH-60 Black Hawk first entered service in 1979. A four-blade, twin-engine, medium-lift utility helicopter, the UH-60 serves as the U.S. Army s primary tactical transport helicopter. Modified versions include models for the U.S. Navy and Air Force, and specialized versions including the UH-60C (modified for Command and Control missions), EH-60A (electronic systems operations and electronic warfare), and the UH-60Q (medical transport). Two major variants of the Black Hawk currently exist: the UH-60L and UH-60M. The UH-60L incorporates improvements to the basic design that provide more power and lifting capability, as well as automatic flight control. The newer UH-60M features upgraded engines, improved rotor blades, and state-of-the-art flight controls that will allow the helicopter s service life to extend to 2020 and beyond. Over 2500 Black Hawks have been built, and nearly 1000 more are currently on order. Black Hawks have seen combat service for the U.S. Military in Grenada, Panama, Somalia, Afghanistan and Iraq. Other nations also employ the UH-60 including Brazil, Colombia, Israel, Mexico, Taiwan, Australia, Japan, and Turkey. Created by Sikorsky and the U.S. Army, this pilot s flight operating manual profiles the UH-60Q Black Hawk. Over 500 pages long, this unclassified document is reprinted here in its entirety."

BOTH MANUALS: Approved for public release; distribution unlimited. DESCRIPTION. This manual contains the complete operating instructions and procedures for UH-60A, UH-60Q, UH-60L, and EH-60A helicopters. The primary mission of this helicopter is that of tactical transport of troops, medical evacuation, cargo, and reconnaissance within the capabilities of the helicopter. The observance of limitations, performance, and weight and balance data provided is mandatory. The observance of procedures is mandatory except when modification is required because of multiple emergencies, adverse weather, terrain, etc. Your flying experience is recognized and therefore, basic flight principles are not included. IT IS REQUIRED THAT THIS MANUAL BE CARRIED IN THE HELICOPTER AT ALL TIMES.

Designed without horizontal stabilizers, the X-4 Bantam had a semi-tailless design that bore some resemblance to Germany¿s Me-163 rocket plane. The small, twin-jet craft relied on combined elevator and aileron surfaces ¿ known as elevons ¿ for pitch and roll control. The role of the X-4 was to explore the transonic speed zone, and to determine whether the design would lessen the stability and control problems affiliated with compressibility. Although two Bantams were built, only one proved mechanically sound. The second was flown over eighty times by Northrop, Air Force and NACA pilots. They learned that the X-4 was sensitive in pitch, and showed a tendency to ¿hunt¿ about all three axes as it approached Mach 1.0. Thus, the X-4¿s design proved a failure. Originally printed by Northrop, NACA and the USAF, this handbook provides a fascinating glimpse inside the cockpit of this experimental plane. The manual was recently declassified and is here reprinted in book form.