Руководство по летной эксплуатации robinson

• Page 3
  CLASS Q SUBSCRIPTION SERVICE If you wish to receive future changes to R44 Pilot’s Operating Handbook and copies of future Safety Notices, send a check or money order for $15 USD to: ROBINSON HELICOPTER COMPANY 2901 Airport Drive Torrance, CA 90505 You will receive all future changes to the Handbook and future Safety Notices for a period of one year.
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  ROBINSON MODEL R44 LOG OF PAGES LOG OF PAGES APPROVED BY FAA TYPE CERTIFICATE NO. H11NM Page Approval Page Approval Date Date Cover 10 Dec 92 Log of Pages 10 Mar 15 Section 2 16 Apr 03 16 Apr 03…
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  ROBINSON MODEL R44 LOG OF PAGES LOG OF PAGES NOT REQUIRING FAA APPROVAL Page Revision Page Revision Date Date Section 1 10 Jul 12 16 Apr 03 General 10 Jul 12 16 Apr 03 10 Jul 12 5 Oct 11…
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  This helicopter is approved as a normal category rotorcraft under FAA Type Certificate No. H11NM as Model R44. COLOR CODE FOR INSTRUMENT MARKINGS Operating limit. Edge of red line indicates limit.
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  ROBINSON SECTION 2 MODEL R44 LIMITATIONS WEIGHT LIMITS Maximum gross weight 2400 lb (1089 kg) Minimum gross weight 1550 lb (703 kg) Maximum per seat including baggage compartment 300 lb (136 kg) Maximum in any baggage compartment 50 lb (23 kg) CENTER OF GRAVITY (CG) LIMITS See figure on page 2-4.
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  ROBINSON SECTION 2 MODEL R44 LIMITATIONS CENTER OF GRAVITY LIMITS FAA APPROVED: 21 FEB 2014…
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  ROBINSON SECTION 2 MODEL R44 LIMITATIONS FLIGHT AND MANEUVER LIMITATIONS Aerobatic flight prohibited. CAUTION Abrupt control inputs may produce high fatigue stresses and cause catastrophic failure of a critical component. Low-G cyclic pushovers prohibited. CAUTION pushover (forward cyclic maneuver) performed from level flight or following a…
• Page 24
  Tanks without bladders: Main tank 31.6 (120) 30.6 (116) Auxiliary tank 18.5 (70) 18.3 (69) Combined capacity 50.1 (190) 48.9 (185) Note: Per R44 Service Bulletin SB-78B, fuel tanks without bladders should no longer be in service. FAA APPROVED: 21 FEB 2014…
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  ROBINSON SECTION 2 MODEL R44 LIMITATIONS PLACARDS (cont’d) Near aux tank fuel gage: For bladder-style tank AUX: 17.0 US GAL For aluminum (non-bladder) tank AUX: 18.3 US GAL In clear view of pilot: MINIMUM SOLO PILOT WEIGHT 150 LB (SEE PILOT’S HANDBOOK)
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  ROBINSON SECTION 2 MODEL R44 LIMITATIONS PLACARDS (cont’d) Inside each baggage compartment: CAUTION DO NOT EXCEED ANY OF THE FOLLOWING: • COMPARTMENT CAPACITY: 50 LB MAX • COMBINED SEAT PLUS COMPARTMENT: 300 LB MAX • ROTORCRAFT GROSS WEIGHT LIMIT SEE ROTORCRAFT FLIGHT MANUAL FOR ADDITIONAL LOADING INSTRUCTIONS.

• Page 31: Table Of Contents

  ROBINSON SECTION 3 MODEL R44 EMERGENCY PROCEDURES SECTION 3 EMERGENCY PROCEDURES CONTENTS Page Definitions ……..

• Page 33: Definitions

  ROBINSON SECTION 3 MODEL R44 EMERGENCY PROCEDURES SECTION 3 EMERGENCY PROCEDURES DEFINITIONS Land Immediately — Land on the nearest clear area where a safe normal landing can be performed. Be prepared to enter autorotation during approach, if required. Land as soon as practical — Landing site is at pilot’s discretion based on nature of problem and available landing areas.

• Page 34: Power Failure Above 500 Feet Agl

  ROBINSON SECTION 3 MODEL R44 EMERGENCY PROCEDURES POWER FAILURE ABOVE 500 FEET AGL 1. Lower collective immediately to maintain rotor RPM. 2. Establish a steady glide at approximately 70 KIAS. (For maximum glide distance or minimum rate of descent, see page 3-3.) 3.

• Page 35: Power Failure Below 8 Feet Agl

  ROBINSON SECTION 3 MODEL R44 EMERGENCY PROCEDURES POWER FAILURE BELOW 8 FEET AGL 1. Apply right pedal as required to prevent yawing. 2. Allow rotorcraft to settle. 3. Raise collective just before touchdown to cushion landing. MAXIMUM GLIDE DISTANCE CONFIGURATION 1.

• Page 36: Emergency Water Landing — Power Off

  ROBINSON SECTION 3 MODEL R44 EMERGENCY PROCEDURES EMERGENCY WATER LANDING – POWER OFF 1. Follow same procedures as for power failure over land until contacting water. If time permits, unlatch doors prior to water contact. 2. Apply lateral cyclic when aircraft contacts water to stop rotors.

• Page 39: Tachometer Failure

  ROBINSON SECTION 3 MODEL R44 EMERGENCY PROCEDURES TACHOMETER FAILURE If rotor or engine tach malfunctions in flight, use remaining tach to monitor RPM. If it is not clear which tach is malfunctioning or if both tachs malfunction, allow governor to control RPM and land as soon as practical.

• Page 42: Warning/Caution Lights

  ROBINSON SECTION 3 MODEL R44 EMERGENCY PROCEDURES WARNING/CAUTION LIGHTS (cont’d) BRAKE Indicates rotor brake is engaged. Release immediately in flight or before starting engine. STARTER-ON Indicates starter motor is engaged. If light does not go out when ignition switch is…

• Page 43
  ROBINSON SECTION 4 MODEL R44 NORMAL PROCEDURES SECTION 4 NORMAL PROCEDURES CONTENTS Page Recommended Airspeeds ….. . . 4-1 Daily or Preflight Checks ……

• Page 45: Recommended Airspeeds

  ROBINSON SECTION 4 MODEL R44 NORMAL PROCEDURES SECTION 4 NORMAL PROCEDURES RECOMMENDED AIRSPEEDS Takeoff and Climb 60 KIAS Maximum Rate of Climb (V 55 KIAS Maximum Range 100 KIAS* Landing Approach 60 KIAS Autorotation 70 KIAS* * Certain conditions may require lower airspeeds.

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  ROBINSON SECTION 4 MODEL R44 NORMAL PROCEDURES DAILY OR PREFLIGHT CHECKS (cont’d) 1. Upper Forward Cowl Doors — Right Side Battery switch ……ON Oil pressure and alternator lights .
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  ROBINSON SECTION 4 MODEL R44 NORMAL PROCEDURES DAILY OR PREFLIGHT CHECKS (cont’d) 11. Fuselage Left Side Baggage compartments ….Check Removable controls … . . Secure if installed Collective control .

• Page 50: Before Starting Engine

  ROBINSON SECTION 4 MODEL R44 NORMAL PROCEDURES DAILY OR PREFLIGHT CHECKS (cont’d) CAUTION Fill baggage compartments under unoccupied seats to capacity before using baggage compartments under occupied seats. Avoid placing objects in compartment which could injure occupant if seat collapses during a hard landing.

• Page 51: Starting Engine And Run-Up

  ROBINSON SECTION 4 MODEL R44 NORMAL PROCEDURES STARTING ENGINE AND RUN-UP Throttle twists for priming ….As required Throttle ……..Closed Battery, strobe switches .

• Page 53: Cruise

  ROBINSON SECTION 4 MODEL R44 NORMAL PROCEDURES CRUISE 1. Adjust carb heat if required. (See page 4-12.) 2. Verify RPM in green arc. 3. Set manifold pressure with collective for desired power. 4. For aircraft with manual controls, adjust cyclic trim to zero forces.

• Page 54: Practice Autorotation — Power Recovery

  ROBINSON SECTION 4 MODEL R44 NORMAL PROCEDURES PRACTICE AUTOROTATION — POWER RECOVERY 1. Adjust carb heat if required. (See page 4-12.) 2. Lower collective to down stop and adjust throttle as required for small tachometer needle separation. CAUTION To avoid inadvertent engine stoppage, do not chop throttle to simulate a power failure.

• Page 57: Approach And Landing

  ROBINSON SECTION 4 MODEL R44 NORMAL PROCEDURES APPROACH AND LANDING 1. Make final approach into wind at lowest practical rate of descent with initial airspeed of 60 knots. Adjust carb heat as required. 2. Reduce airspeed and altitude smoothly to hover. (Be sure rate of descent is less than 300 FPM before airspeed is reduced below 30 KIAS.)

• Page 58: Shutdown Procedure

  ROBINSON SECTION 4 MODEL R44 NORMAL PROCEDURES SHUTDOWN PROCEDURE Collective down, RPM 60-70% … . . Friction ON Cyclic and pedals neutral ….Friction ON Trim switch (if installed) .

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  ROBINSON SECTION 6 MODEL R44 WEIGHT AND BALANCE SECTION 6 WEIGHT AND BALANCE CONTENTS Page General ……..
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  ROBINSON SECTION 6 MODEL R44 WEIGHT AND BALANCE SECTION 6 WEIGHT AND BALANCE GENERAL The helicopter must be flown only within weight and balance limits specified in Section 2. Loadings outside these limits can result in insufficient control travel for safe operation.
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  Weight and Balance Record form. NOTE Calculated CG with full fuel and 150 lb pilot must be within CG limits. Following modification, ad- justment to fixed nose ballast may be required. See R44 Maintenance Manual. REVISED: 21 FEB 2014…
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  ROBINSON SECTION 6 MODEL R44 WEIGHT AND BALANCE WEIGHT AND BALANCE RECORD (cont’d) REVISED: 21 FEB 2014…
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  ROBINSON SECTION 6 MODEL R44 WEIGHT AND BALANCE LOADING INSTRUCTIONS The following table may be used when calculating loaded helicopter weight and CG position. COMMON ITEM WEIGHT & CG Weight Longitudinal Lateral arm (in.) Item (lb) arm (in.) (+ = right side) Pilot (right 49.5*…
• Page 77
  ROBINSON SECTION 6 MODEL R44 WEIGHT AND BALANCE LOADING INSTRUCTIONS (cont’d) The following sample calculation demonstrates how to determine loaded helicopter weight and center of gravity. A worksheet is provided on the page following the sample calculation for a weight and balance calculation for your helicopter.
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  ROBINSON SECTION 6 MODEL R44 WEIGHT AND BALANCE LOADING INSTRUCTIONS (cont’d) SAMPLE LOADING CALCULATION Location Moment Lat. Arm Weight Long. Item (in.) Long. Lat. (lb) += Right (in.-lb) (in.-lb) (in.) Side Basic empty weight 1460 106.2 0.2 155,052 Remove forward right door —7.5…
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  ROBINSON SECTION 6 MODEL R44 WEIGHT AND BALANCE LOADING INSTRUCTIONS (cont’d) LOADING CALCULATION WORKSHEET Location Moment Lat. Arm Weight Long. Item (in.) Long. Lat. (lb) += Right (in.-lb) (in.-lb) (in.) Side Basic empty weight Remove forward right door 49.4 24.0 Remove forward left door 49.4…
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  ROBINSON SECTION 6 MODEL R44 WEIGHT AND BALANCE THIS PAGE INTENTIONALLY BLANK ISSUED: 21 FEB 2014…
• Page 81
  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION SECTION 7 SYSTEMS DESCRIPTION CONTENTS Page General ……..

• Page 83: General

  SYSTEMS DESCRIPTION SECTION 7 SYSTEMS DESCRIPTION GENERAL The R44 is a four-place, single main rotor, single engine helicopter constructed primarily of metal and equipped with skid-type landing gear. The primary fuselage structure is welded steel tubing and riveted aluminum sheet.

• Page 84: Rotor Systems

  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION ROTOR SYSTEMS The main rotor has two all-metal blades mounted to the hub by coning hinges. The hub is mounted to the shaft by a teeter hinge. The coning and teeter hinges use self-lubricated bearings.

• Page 86: Flight Controls

  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION FLIGHT CONTROLS Dual controls are standard equipment and all primary controls are actuated through push-pull tubes and bellcranks. Bearings used throughout the control system are either sealed ball bearings which do not require lubrication or have self-lubricated liners.

• Page 87: Removable Flight Controls

  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION REMOVABLE FLIGHT CONTROLS Left seat pilot controls may be removed and installed by maintenance personnel or pilots as follows: 1. To remove cyclic grip, remove quick-release pin by depressing button and pulling, then pull outward on left grip while supporting cyclic center post.

• Page 88: Rpm Governor

  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION RPM GOVERNOR The governor maintains engine RPM by sensing changes and applying corrective throttle inputs through a friction clutch which can be easily overridden by the pilot. The governor is active only above 80% engine RPM and can be switched on or off using the toggle switch on the end of the right seat collective.

• Page 90: Control Friction Adjustment

  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION CONTROL FRICTION ADJUSTMENT Cyclic and collective controls are equipped with adjustable friction devices. The collective friction lever is located near the aft end of the pilot’s collective. It is actuated aft to increase friction and forward to release it.

• Page 91: Clutch Actuator

  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION ENGINE CONTROLS (cont’d) Correct throttle linkage adjustment may be verified during preflight by rolling the twist-grip through the overtravel spring and holding against the hard idle stop. carburetor throttle arm should just barely start to move when the collective is raised full up.

• Page 92: Fuel System

  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION FUEL SYSTEM The fuel system is gravity-flow (no fuel pumps) and includes main and auxiliary tanks, a shutoff valve control located between the front seats, and a strainer (gascolator). The fuel tanks have flexible bladders in aluminum enclosures.

• Page 93: Electrical System

  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION ELECTRICAL SYSTEM A 14-volt DC electrical system which includes an alternator and a sealed lead-acid battery is standard. A 28-volt electrical system is optional. The battery is located either in the engine compartment, under the left front seat, or beneath the instrument console.

• Page 94
  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION ELECTRICAL SYSTEM (cont’d) ELECTRICAL SYSTEM (EARLIER AIRCRAFT) REVISED: 21 FEB 2014 7-12…
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  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION ELECTRICAL SYSTEM (cont’d) ELECTRICAL SYSTEM (LATER AIRCRAFT) REVISED: 21 FEB 2014 7-13…
• Page 96
  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION ELECTRICAL SYSTEM (cont’d) CIRCUIT BREAKER PANEL – TYPICAL (EARLIER AIRCRAFT) REVISED: 21 FEB 2014 7-14…
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  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION ELECTRICAL SYSTEM (cont’d) CIRCUIT BREAKER PANEL – TYPICAL (LATER AIRCRAFT) REVISED: 21 FEB 2014 7-15…

• Page 98: Lighting System

  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION LIGHTING SYSTEM A red anti-collision light is installed on the tailcone and is controlled by the strobe switch. Position lights are installed on each side of the cabin and in the tail and are controlled by the nav lights switch.

• Page 99: Instrument Panel

  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION INSTRUMENT PANEL Standard primary instruments include airspeed indicator, engine and rotor dual tachometer, altimeter, manifold pressure gage, and magnetic compass. Engine gages include an ammeter, oil pressure, oil temperature, cylinder head temperature, and fuel quantity for main and aux tanks.

• Page 100
  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION 1. VERTICAL SPEED INDICATOR 21. CLOCK 2. OPTIONAL INSTRUMENT 22. ENGINE INSTRUMENTS 3. AIRSPEED INDICATOR 23. PANEL LIGHTS DIMMER 4. ENGINE AND ROTOR TACHS 24. ROTOR BRAKE LIGHT 5. ALTIMETER 25. NAVIGATION LIGHTS SWITCH 6.
• Page 101
  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION 1. ENGINE AND ROTOR TACHS 23. OIL PRESSURE LIGHT 2. AIRSPEED INDICATOR 24. ROTOR BRAKE LIGHT 3. ARTIFICIAL HORIZON 25. CARBURETOR AIR TEMP 4. ALTIMETER 26. CLOCK 5. MANIFOLD PRESSURE GAGE 27. ENGINE INSTRUMENTS 6.
• Page 102
  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION 1. VERTICAL SPEED INDICATOR 22. IGNITION SWITCH 2. AIRSPEED INDICATOR 23. PILOT’S SIDE CONSOLE (OPT’L) 3. ENGINE AND ROTOR TACHS 24. ENGINE INSTRUMENTS 4. OPTIONAL INSTRUMENT 25. CARBURETOR AIR TEMP 5. ALTIMETER 26. CLOCK 6.

• Page 103: Audio System

  OPTIONAL AVIONICS A wide range of optional avionics are available for the R44. It is not practical to provide a description of all equipment in this manual. All aircraft are delivered with the manufacturers’ operating manuals for each piece of installed equipment.

• Page 104: Pitot-Static System

  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION PITOT-STATIC SYSTEM The pitot-static system supplies air pressure to operate the airspeed indicator, altimeter, and vertical speed indicator. The pitot tube is located on the front edge of the mast fairing. The static sources are located on each side of the cabin aft of the rear doors.

• Page 105: Warning And Caution Lights

  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION WARNING AND CAUTION LIGHTS Warning and caution lights include clutch, main gearbox over-temperature, main and tail gearbox chip, engine fire, starter on, low fuel, low RPM, alternator, low oil pressure, rotor brake, carbon monoxide, and full throttle (later aircraft).

• Page 106: Cabin Heating And Ventilation

  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION CABIN HEATING AND VENTILATION Fresh air vents are located in each door and in the nose. Door vents are opened and closed using the knob near the vent door hinge. A rotating knob is provided to lock vents closed.

• Page 107: Landing Gear

  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION SEATS, BELTS, AND BAGGAGE (cont’d) Four- or five-point harnesses are optional for the front seats. The lap belts on these harnesses should be adjusted to eliminate slack. On five-point harnesses, the lower strap should be adjusted as necessary to ensure that the buckle does not interfere with the cyclic grip in the full aft position.

• Page 108: Rotor Brake

  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION ROTOR BRAKE The rotor brake is mounted on the aft end of the main gearbox and is actuated by a cable connected to a pull handle located on the cabin ceiling. To stop the rotor, use the following procedure: 1.

• Page 109: Carbon Monoxide Detector

  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION CARBON MONOXIDE DETECTOR The carbon monoxide (CO) detector indicates elevated cabin CO levels. CO is an odorless, toxic gas present in engine exhaust which causes headaches, drowsiness, and possible loss of consciousness. CO levels may become elevated due to an exhaust leak or exhaust recirculation during prolonged hovering.

• Page 110: Emergency Locator Transmitter (Optional)

  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION EMERGENCY LOCATOR TRANSMITTER (OPTIONAL) The Emergency Locator Transmitter (ELT) installation consists of a transmitter with internal battery pack, an external antenna, and a remote switch/annunciator. The transmitter is mounted to the upper steel tube frame and is accessible through the aft, upper cowl door.

• Page 111: Optional Accessory Mounts

  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION OPTIONAL ACCESSORY MOUNTS Provisions for mounting small, portable items are an option. The provisions use mounting bars located forward of the pilot’s seat, the copilot’s seat, or both. The bars are fitted with one or more clamp assemblies which are compatible with a variety of commercially available accessory mounts.

• Page 112
  ROBINSON SECTION 7 MODEL R44 SYSTEMS DESCRIPTION THIS PAGE INTENTIONALLY BLANK ISSUED: 10 MAR 2015 7-30…
• Page 113
  ROBINSON SECTION 8 MODEL R44 HANDLING AND MAINTENANCE SECTION 8 HANDLING AND MAINTENANCE CONTENTS Page General ……..

• Page 115: General

  HANDLING AND MAINTENANCE GENERAL This section outlines procedures recommended handling, servicing, and maintaining the R44 helicopter. Every owner should stay in close contact with a Robinson Service Center to obtain the latest service and maintenance information. Owners should also be registered with…

• Page 116: Required Inspections

  This annual inspection must be signed off by a mechanic with Inspection Authorization (lA). In addition to the annual inspection, the R44 Maintenance Manual requires a complete inspection after every 100 hours of operation.

• Page 120: Parking

  ROBINSON SECTION 8 MODEL R44 HANDLING AND MAINTENANCE PARKING 1. Place cyclic control in neutral and apply friction. 2. Put collective full down and apply friction. 3. Align rotor blades approximately fore and aft. Apply rotor brake. Use blade tie-downs in windy conditions.

• Page 121: Engine Oil

  8. Install new filter per instructions printed on filter. Use only Champion CH48108, CH48108-1, Tempest AA48112, or Robinson B123-1 or -2 filter with Robinson filter adapter or use Champion CH48103 or CH48103-1 filter with early-style filter installation. Safety wire is not required on filter. If no filter is installed, re-install pressure screen and housing.

• Page 122
  ROBINSON SECTION 8 MODEL R44 HANDLING AND MAINTENANCE ENGINE OIL (cont’d) 9. Close quick drain and fill sump with 9 quarts of appropriate grade oil as recommended below. 10. Start helicopter. Verify oil pressure within 30 seconds. Ground run for a few minutes, shut down, and verify no leaks.

• Page 123: Tail Rotor Gearbox Oil

  1. Cut safety wire (if installed) and remove filler/vent cap located on top of gearbox. 2. Use only Robinson part number A257-2 oil. 3. Fill very slowly to center of sight gage. DO NOT overfill. (Less than a tablespoon of oil is usually required.)

• Page 124: Battery

  ROBINSON SECTION 8 MODEL R44 HANDLING AND MAINTENANCE BATTERY The battery is located in the engine compartment, under the left front seat, or beneath the instrument console. The battery is sealed and does not require fluid level checks. A discharged battery is NOT AIRWORTHY because it will not have the reserve capacity to operate the electrical system should the charging system fail in flight.

• Page 125: Cleaning Helicopter

  ROBINSON SECTION 8 MODEL R44 HANDLING AND MAINTENANCE CLEANING HELICOPTER CLEANING EXTERIOR SURFACES The helicopter should be washed with mild soap and water. Harsh abrasives, alkaline soaps, or detergents could scratch painted or plastic surfaces or could cause corrosion of metal. Cover areas where cleaning solution could cause damage.

• Page 126
  ROBINSON SECTION 8 MODEL R44 HANDLING AND MAINTENANCE CLEANING HELICOPTER (cont’d) CLEANING WINDSHIELD AND WINDOWS (cont’d) CAUTION Do not use gasoline, other alco- hols, benzene, carbon tetrachlo- ride, thinner, acetone, or window (glass) cleaning sprays. 4. After cleaning plastic surfaces, apply a thin coat of hard polishing wax.
• Page 127
  ROBINSON SECTION 9 MODEL R44 SUPPLEMENTS SECTION 9 SUPPLEMENTS OPTIONAL EQUIPMENT SUPPLEMENTS Information contained in the following supplements applies only when the related equipment is installed. CONTENTS Page Peak Beam Searchlight ….9-4.1 Fixed Floats .
• Page 183
  ROBINSON SECTION 9 MODEL R44 ADS-B EQUIPMENT SUPPLEMENT FAA APPROVED R44 PILOT’S OPERATING HANDBOOK ADS-B EQUIPMENT SUPPLEMENT This supplement must be included in the FAA-approved Pilot’s Operating Handbook when ADS-B equipment is installed. The information contained herein supplements or supersedes…
• Page 184
  The supplemental information allows optimization of flight plan routes and aircraft spacing. ADS-B Out equipment may be required for operation in certain airspace. The R44 ADS-B Out installation has been shown to meet the requirements of 14 CFR § 91.227.
• Page 185
  Other aircraft which have been equipped with ADS-B Out systems can broadcast their position directly to the receiver. The R44 may be equipped with only ADS-B Out or with both ADS-B Out and ADS-B In. ISSUED: 21 FEB 2014 9-11.3…
• Page 186
  ADS-B receiver (if installed) must all be powered and in normal operating modes for proper system function. ADS-B OUT The R44 ADS-B Out system is a single point of entry system. Mode 3/A codes, IDENT commands, and emergency codes are set on the transponder and are automatically incorporated in ADS-B Out broadcasts.
• Page 187
  ROBINSON SECTION 9 MODEL R44 ADS-B EQUIPMENT SUPPLEMENT SECTION 4: NORMAL PROCEDURES (cont’d) ADS-B SYSTEM OPERATION (cont’d) ADS-B IN The ADS-B In receiver is mounted underneath the left, front seat and has no direct pilot interface. The receiver is powered by the Transponder/ADS-B circuit breaker.
• Page 188
  ROBINSON SECTION 9 MODEL R44 ADS-B EQUIPMENT SUPPLEMENT SECTION 6: WEIGHT AND BALANCE No change. SECTION 7: SYSTEM DESCRIPTION ADS-B SYSTEM The ADS-B Out system consists of a GPS receiver connected to the transponder which broadcasts the aircraft’s position, identification, and certain other parameters to air traffic control.
• Page 194
  MODEL R44 SAFETY TIPS SAFETY NOTICES The following Safety Notices have been issued by Robinson Helicopter Company as a result of various accidents and incidents. Studying the mistakes made by other pilots will help you avoid making the same errors. Safety Notices are available on the RHC website: www.robinsonheli.com.
• Page 212
  Safety Notice SN-32 Issued: March 1998 Revised: May 2013 HIGH WINDS OR TURBULENCE A pilot’s improper application of control inputs in response to high winds or turbulence can increase the likelihood of a mast bumping accident. The following procedures are recommended: 1.
• Page 213
  Issued: March 1998 Revised: July 2013 DRIVE BELT SLACK R22 and R44 drive belts must have the proper slack prior to engine start. Belts which are too loose may jump out of their sheave grooves during engine start while clutch is engaging.
• Page 214
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• Page 220
  Some pilots mistakenly attribute this yaw to loss of tail rotor effectiveness (LTE), implying that the tail rotor stalled or was unable to provide adequate thrust. Tail rotors on Robinson helicopters are designed to have more authority than many other helicopters and are unlikely to experience LTE.
• Page 221
  Safety Notice SN-43 Issued: January 2015 USE EXTRA CAUTION DURING POST-MAINTENANCE FLIGHTS A number of fatal accidents have occurred during flights immediately following maintenance. In several cases, the cause was incorrect or incomplete reassembly of the helicopter, and the error would have been detectable during a careful preflight inspection.
• Page 222
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