TM 1-1520-240-102-1-1CHAPTER 2AIRCRAFT AND SYSTEMS DESCRIPTION AND OPERATIONSECTION I. HELICOPTER2-1-1. General.The CH-47D (fig. FO-1, 2-1-1 and 2-1-2) is a twin-turbineengine, tandem rotor helicopter designed for transportationof cargo, troops, and weapons during day, night, visual, andinstrument conditions. (Unless otherwise noted, numbersrefer to fig. FO-1.) The helicopter is powered by twoT55-L-712 or T55-GA-714A shaft-turbine engines (18) onthe aft fuselage. The engines simultaneously drive two tan-dem three-bladed counterrotating rotors (13 and 19) throughengine transmissions (25), a combining transmission (16),drive shafting (14), and reduction transmissions (12 and 23).The forward transmission is on the forward pylon above thecockpit (1). The aft transmission, the combining transmis-sion, and drive shafting are in the aft cabin section and aftpylon sections (3 and 4). Drive shafting from the combiningtransmission to the forward transmission is housed in atunnel along top of the fuselage. When rotors are stationary,a gas-turbine auxiliary power unit (22) drives a generatorand hydraulic pump to furnish hydraulic and electrical power.Fuel is carried in pods on each side of the fuselage. Thehelicopter is equipped with four non-retractable landing gear.An entrance door (15) is at the forward right side of the cargocompartment (2). At the rear of the cargo compartment is ahydraulically powered loading ramp (26). The pilots seat (9)and controls are at the right side of the cockpit; the copilot’sseat (40) and controls are on the left side. See figure 2-1-3for typical cockpit and controls.2-1-2. Gross Weight.The maximum gross weight of the CH-47D is 50,000pounds. Chapters 5 and 6 provide additional weight informa-tion.2-1-3. Landing Gear System.The landing gear system consists of four non-retractablelanding gears mounted on the fuselage pods. The forwardlanding gears are a fixed-cantilever type and have twinwheels. The aft landing gears are of the single–wheel, full-swivel (360_) type which can be power centered and lockedin trailed position. In addition, the aft right landing gear canbe steered from the cockpit by using the steering controlknob on the console. Each landing gear has an individualair-oil shock strut and is equipped with tube-type tires.2-1-4. Landing Gear Proximity Switches.a.Two proximity switches are installed, one on each aftlanding gear. Each switch is activated when its associatedshock strut is compressed during touchdown. The switchesimprove ground handling by reducing pitch axis gain of theAFCS, by canceling the longitudinal Control Position Trans-ducer (CPT), therefore longitudinal stick input, to the Differ-ential Airspeed Hold (DASH) actuators, and by driving bothlongitudinal cyclic trim (LCT) actuators to the ground posi-tion. In addition to the above functions, the switch on the rightaft landing gear, when activated, disables the flare dispenserto prevent accidental flare release, and enables the holdfunction of mode 4 transponder codes.b.On helicopters equipped with GROUND CONTACTindicating lights, activation of the proximity switches whenthe associated shock strut is compressed will cause theassociated GROUND CONTACT indicating light on theMAINTENANCE PANEL to illuminate. CAUTIONShould either or both GROUND CONTACTindicating lights remain illuminated afterlift-off to hover, the illuminated system(s)DASH will not function properly in forwardflight. If both GROUND CONTACT indicat-ing lights remain illuminated after lift-off,the AUTO function of both cyclic trim sys-tems will be inoperative and both LCT ac-tuators will remain in the GND position.c.Aft landing gear proximity switches are not actuatedin a water landing. As a result, DASH actuators will respondto longitudinal stick motion, producing an apparent increasein control sensitivity. Cyclic motion of +3/4 inch from neutral,if held, will drive DASH actuators hard over. If longitudi-nal cyclic movement is required for taxing, set the AFCSSYSTEM SEL switch to OFF.2-1-5. Steering and Swivel Lock System. The steering and swivel lock system consists of the powersteering control box with the STEERING CONTROL panelon the center console, utility system pressure controlmodule, power steering actuator, power steering module,swivel lock actuating cylinder, and the PWR STEER mastercaution capsule. The STEERING CONTROL panel consistsof a three position SWIVEL switch and a steering controlknob. The SWIVEL switch controls operation of powersteering and swivel locks.
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