2009 UH-60A UH-60L EH-60A Helicopter Operator’s Manual TM 1-1520-237-10 PDF
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Department of the Army Operator’s Manual TM 1-1520-237-10 dated 25 September 2009 for UH-60A, UH-60L, and EH-60A helicopters. This extensive operator reference covers aircraft systems, T700 engine configurations, avionics, mission equipment, operating limits, weight and balance, performance data, normal procedures, emergency procedures, and servicing information.
Description
UH-60A, UH-60L and EH-60A Operator Reference
The 2009 UH-60A UH-60L EH-60A Helicopter Operator’s Manual TM 1-1520-237-10 PDF is the Department of the Army technical manual issued 25 September 2009 for operators of the UH-60A, UH-60L, and EH-60A helicopters. The manual states that it contains the complete operating instructions and procedures for these helicopter series, with mandatory limitations, performance information, and weight-and-balance data. Its coverage extends from basic aircraft and system descriptions through avionics, mission equipment, operating restrictions, loading, extensive performance charts, normal operating procedures, and emergency procedures.
Model and configuration effectivity is identified throughout the manual. The UH-60A coverage includes helicopters equipped with T700-GE-700 engines as well as modified UH-60A configurations using T700-GE-701D/CC engines. UH-60L information covers T700-GE-701C and T700-GE-701D/CC engine installations. The document also separates performance material for T700-GE-700-equipped helicopters from the 701C and 701D/CC configurations, making the performance sections easier to match to the applicable aircraft.
Aircraft Systems and Operating Information
TM 1-1520-237-10 gives operators a broad system-level understanding of the helicopter before moving into limits and procedures. Aircraft coverage includes cockpit and cabin arrangements, landing gear, emergency equipment, engines and associated systems, fuel, flight controls, hydraulic and pneumatic systems, powertrain, main and tail rotor groups, utility systems, environmental systems, electrical power, auxiliary power, lighting, flight instruments, and servicing. Illustrated pages throughout the manual identify controls, components, system arrangements, and operating relationships.
The engine section explains the T700 installation and its major modules and associated fuel, oil, ignition, bleed-air, anti-icing, starting, and control systems. Separate effectivity markings distinguish information for the T700-GE-700 and later 701C or 701D/CC configurations. Flight-control material covers cyclic, collective and directional controls together with servo systems, stability augmentation, flight-path stabilization, trim, and stabilator operation. Hydraulic coverage addresses the No. 1, No. 2, and backup systems and the leak detection and isolation logic used to maintain flight-control capability.
Electrical and auxiliary-power sections describe the helicopter’s AC and DC power architecture, generators, converters, battery arrangements, buses, circuit protection, external power, and APU functions. The manual also includes detailed cockpit illustrations, control-panel layouts, system diagrams, hydraulic logic diagrams, electrical schematics, engine illustrations, rotor-system drawings, and performance charts.
Complete Bookmarks
The complete bookmarks in the “2009 UH-60A UH-60L EH-60A Helicopter Operator's Manual TM 1-1520-237-10 PDF” are as follows:
+CHAPTERS
+CHAPTER 2p. 15
+CHAPTER 3p. 133
+CHAPTER 4p. 285
+CHAPTER 5p. 373
+CHAPTER 7p. 427
+CHAPTER 7Ap. 593
+CHAPTER 8p. 787
+CHAPTER 9p. 815
+FIGURES
+TABLES
+APPENDICES
+PAGES
File Details
- Manual type: Operator’s Manual / Technical Manual
- Models: UH-60A, UH-60L, EH-60A helicopters
- Document number: TM 1-1520-237-10
- Issue date: 25 September 2009
- Supersedes: TM 1-1520-237-10 dated 17 April 2006, including all changes
- Language: English
- PDF file: 902 pages
- Format: PDF
Chapters Covered
- Chapter 1 – Introduction
- Chapter 2 – Aircraft and Systems Description and Operation
- Aircraft
- Emergency Equipment
- Engines and Related Systems
- Fuel System
- Flight Controls
- Hydraulic and Pneumatic System
- Powertrain System
- Main and Tail Rotor Groups
- Utility Systems
- Heating, Ventilating, Cooling, and Environmental Control Unit
- Electrical Power Supply and Distribution Systems
- Auxiliary Power Unit
- Lighting
- Flight Instruments
- Servicing, Parking, and Mooring
- Chapter 3 – Avionics
- General
- Communications
- Navigation
- Transponder and Radar
- Chapter 4 – Mission Equipment
- Mission Avionics
- Armament
- Cargo Handling Systems
- Mission Flexible Systems
- Air Warrior
- Chapter 5 – Operating Limits and Restrictions
- General
- System Limits
- Power Limits
- Loading Limits
- Airspeed Limits
- Maneuvering Limits
- Environmental Restrictions
- Other Limitations
- Chapter 6 – Weight/Balance and Loading
- General
- Weight and Balance
- Fuel/Oil
- Personnel
- Mission Equipment
- Cargo Loading
- Center of Gravity
- Chapter 7 – Performance Data 700
- Introduction
- Maximum Torque Available
- Hover
- Cruise
- Optimum Cruise
- Drag
- Climb – Descent
- Fuel Flow
- Airspeed System Description
- Special Mission Performance
- Chapter 7A – Performance Data 701C 701D/CC
- Introduction
- Maximum Torque Available
- Hover
- Cruise
- Optimum Cruise
- Drag
- Climb – Descent
- Fuel Flow
- Airspeed System Characteristics
- Special Mission Performance
- Chapter 8 – Normal Procedures
- Mission Planning
- Operating Procedures and Maneuvers
- Instrument Flight
- Flight Characteristics
- Adverse Environmental Conditions
- Chapter 9 – Emergency Procedures
- Aircraft Systems
- Mission Equipment
- Appendix A – References
- Appendix B – Abbreviations and Terms
- Index
Taken as a whole, the 2009 UH-60A UH-60L EH-60A Helicopter Operator’s Manual TM 1-1520-237-10 PDF combines system familiarization with the data an operator needs for planning and operating the applicable helicopter configuration. The two large performance chapters provide dedicated data sets for the T700-GE-700 and T700-GE-701C/T700-GE-701D/CC configurations, including torque-available, hover, cruise, climb/descent, fuel-flow, airspeed, and special-mission performance information. Weight-and-balance material supports loading calculations and center-of-gravity checks, while the limits chapter consolidates system, power, loading, airspeed, maneuvering, and environmental restrictions.
IMAGES PREVIEW
Illustrated Technical Reference
Numerous drawings and diagrams make this manual useful for locating and understanding cockpit controls and major aircraft systems. Examples include general-arrangement drawings of the helicopter, principal-dimension illustrations, cockpit and instrument-panel diagrams, T700 engine drawings, flight-control illustrations, hydraulic-system logic diagrams, rotor and deice-system diagrams, and electrical-system layouts. These illustrations complement the operating text and help connect procedures and indications to the associated controls and equipment.
Distribution and Export-Control Notice
This manual carries an export-control warning and Distribution Statement D. The document states that its technical data is subject to export restrictions and that distribution is authorized to the U.S. Department of Defense and DoD contractors only, with other requests referred to the designated U.S. Army authority. Access, purchase, use, and dissemination must therefore comply with all applicable authorization and export-control requirements.
Operational Scope
The value of this UH-60A, UH-60L and EH-60A operator manual lies in the way its information is tied together. Aircraft-system descriptions provide context for indications and controls; operating limits define the boundaries that must be observed; weight-and-balance and performance sections support mission planning; and the normal and emergency procedure chapters provide the procedural reference for operating the helicopter. The result is a single, extensive reference covering the principal information identified by TM 1-1520-237-10 for these helicopter configurations.
PDF Delivery and Operator Reference
The 2009 UH-60A UH-60L EH-60A Helicopter Operator’s Manual TM 1-1520-237-10 PDF supports authorized operators and technical users who need the applicable system descriptions, operating procedures, limits, performance data, loading information, and emergency-reference material in one document. Using the correct model and engine-effectivity information is essential because limits, procedures, and performance data can differ by aircraft configuration. For recipients legally authorized to possess this restricted technical data, the manual is supplied as an instant PDF download with no physical shipping required and can be viewed on compatible computers, tablets, and phones or printed for reference.
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