UH-72 Lakota Helicopter Flight Manual PDF Download
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Author: Publisher: Jeffrey Frank Jones ISBN: Category : Languages : en Pages : 1386
Book Description
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.
Author: United States Government US Army Publisher: CreateSpace ISBN: 9781514383971 Category : Languages : en Pages : 198
Book Description
This manual, Training Circular TC 3-04.21 (TC 1-272) Aircrew Training Manual, Light Utility Helicopter, UH-72A November 2013, standardizes aircrew training programs (ATPs) and flight evaluation procedures. It provides specific guidelines for executing light utility helicopter UH-72A aircrew training and establishes crewmember qualification, refresher, mission, and continuation, training, and evaluation requirements. This manual applies to all UH-72A crewmembers and their commanders in the active Army, the Army National Guard Bureau (NGB), the United States (U.S) Army National Guard (ARNG), the U.S Army Reserve (USAR) and Department of the Army Civilians (DACs) unless otherwise stated. This manual applies to the Active Army, the Army National Guard (ARNG), the Army National Guard of the United States (ARNGUS), and the United States Army Reserve (USAR) unless otherwise stated. The operator's manual is the governing authority for operation of the aircraft. If differences exist between the maneuver descriptions in the rotorcraft flight manual (RFM) and this manual, then this manual is the governing authority for training and flight evaluation purposes only. The manufacturer RFM and any applicable supplements are the governing authority for operation of the aircraft. Implementation of this manual conforms to AR 95-1 (flight regulations) and TC 3-04.11. If a conflict exists between this manual, and TC 3-04.11, the ATP commander determines the method of accomplishment based upon the requirement and the unit's mission as to which manual takes precedence. This manual, in conjunction with the ARs and TC 3-04.11, will help aviation commanders, at all levels; develop a comprehensive ATP. By using this ATM, commanders ensures, that individual crewmembers and aircrew proficiency is commensurate with the units' mission that aircrews routinely employ standard techniques and procedures. Crewmembers will use this manual as a "how to" source for performing crewmember duties. It provides performance standards and evaluation guidelines so that crewmembers know the level of performance expected. Each task provides a description of how the task should be perform to meet the standards.. ATP commanders of active Army, National Guard, and Army Reserve units operating the UH-72A helicopter will use this ATM and TC 3-04.11 to develop individual commander's task lists for assigned aviators.
Author: Chinese Aeronautical Society Publisher: Springer Nature ISBN: 9819988616 Category : Technology & Engineering Languages : en Pages : 711
Book Description
This book contains the original peer-reviewed research papers presented at the 6th China Aeronautical Science and Technology Conference held in Wuzhen, Zhejiang Province, China, in September 2023. Topics covered include but are not limited to Navigation/Guidance and Control Technology, Aircraft Design and Overall Optimisation of Key Technologies, Aviation Testing Technology, Airborne Systems/Electromechanical Technology, Structural Design, Aerodynamics and Flight Mechanics, Advanced Aviation Materials and Manufacturing Technology, Advanced Aviation Propulsion Technology, and Civil Aviation Transportation. The papers presented here share the latest findings in aviation science and technology, making the book a valuable resource for researchers, engineers and students in related fields.
Author: Publisher: Jeffrey Frank Jones ISBN: Category : Languages : en Pages : 962
Book Description
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