Skip to main content

DAILY OR PREFLIGHT CHECKS

Robinson R44 Raven II · Checklist

Free account — keep the POHs & checklists you reference in one place.

Overview

This document is a preflight checklist specifically for the Robinson R44 helicopter. It outlines the daily or preflight checks that pilots and maintenance personnel should perform to ensure the aircraft is airworthy and safe for flight. The checklist includes various inspections of the helicopter's components, including the fuselage, cabin, engine, and rotor systems. It emphasizes the importance of verifying the condition of critical parts and systems, as well as ensuring that safety measures are in place before flight. This document serves as a vital reference for pilots and ground crew to maintain operational safety and compliance with aviation standards.

  • Ensure all doors are unlocked before flight for emergency access.
  • Check engine oil level (7-9 quarts) before flight.
  • Verify that no frost, ice, or snow is present on rotor blades.
  • Inspect for visible damage and fluid leaks during preflight checks.
  • Ensure that torque stripes on critical fasteners are intact.

Document

Source

Originally published by robinsonstrapistorprod.blob.core.windows.net. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

Report a problem or request removal

Document details

Type
Checklist
Year
2021
Pages
2
File size
67 KB
Publisher
robinsonstrapistorprod.blob.core.windows.net
How rare is it?
1,002Robinson R44 Raven II registered worldwide · 0 active

Common. One of the most common aircraft types we track.

Documentation completeness
5/7

Most owners only have the POH. Here's the essential set for the Robinson R44 Raven II.

More Robinson R44 Raven IImanuals & documents

See all 45
Similar aircraft

If you fly the Robinson R44 Raven II, you may also be researching these.

In this document

General Procedures

The checklist begins with general procedures that must be followed before conducting a preflight inspection. This includes removing ground handling wheels and covers, checking for frost or ice on rotor blades, and verifying that the aircraft is airworthy through maintenance records. It also advises using an 8-foot ladder for inspecting the main rotor and checking for visible damage or fluid leaks.

Fuselage Checks

Specific checks for the fuselage include inspecting baggage compartments, seat belts, and ensuring that doors are unlocked and latched. The condition of the landing gear and position lights must also be verified, along with ensuring that static ports are clear.

Cabin Interior Checks

Inside the cabin, pilots should remove loose articles and check the condition of instruments, switches, and controls. The checklist emphasizes the importance of ensuring that all doors are unlocked before flight for emergency access.

Engine and Fuel Checks

The checklist includes detailed checks for the engine, such as verifying oil levels (7-9 quarts), ensuring that the throttle linkage is operable, and checking for leaks in fuel and oil lines. Fuel quantity and leakage must also be assessed.

Tail Rotor and Gearbox Checks

Checks for the tail rotor include verifying the condition of the gearbox, ensuring that oil is visible and there are no leaks. The blades must be clean and free from damage, and the pitch links should show no looseness.

Safety notes

  • Remove left seat controls if the person in that seat is not a rated helicopter pilot.
  • Fill baggage compartments under unoccupied seats to capacity before using those under occupied seats to prevent injury during a hard landing.
  • Shorter pilots may require a cushion to ensure full control travel.

Full document text

ROBINSON HELICOPTER COMPANY MODEL R44 DAILY OR PREFLIGHT CHECKS Visit www.robinsonheli.com to verify this checklist is current. GENERAL PROCEDURES • Remove ground handling wheels and all covers and tie-downs. • Remove even small accumulations of frost, ice, or snow, especially from rotor blades. • Check maintenance records to verify aircraft is airworthy. An 8-foot step ladder is recommended for preflight inspection of the main rotor; however, main rotor hub may be reached by first opening right rear seat and stepping on seat support and then stepping on deck below the aux fuel tank. • Check general condition of aircraft and verify no visible damage, fluid leakage, or abnormal wear. • Verify no fretting at rivets and seams where parts are joined together. Fretting of aluminum parts produces a fine black powder while fretting of steel parts produces a reddish-brown or black residue. • Verify Telatemps show no temperature increase that cannot be attributed to a change in operating conditions (mechanics draw a reference line to the right of the highest temperature square which has darkened in operation). • Verify torque stripes on critical fasteners are not broken or missing. REV: 17 NOV 2021 Page 1 of 6 Page 6 of 6 13. Fuselage Right Side Baggage compartments. . . . . . . . . . . . . . . . . Check Seat belts . . . . . . . . Check condition and fastened Aft door . . . . . . . . . . . . . . . . Unlocked and latched Door hinge safety pins . . . . . . . . . . . . . . . . . Installed Landing gear . . . . . . . . . . . . . . . . . . . . . . . . . Check Position light . . . . . . . . . . . . . . . . . . . . . . . . . Check Static port . . . . . . . . . . . . . . . . . . . . . . . . . . . . Clear 14. Cabin Interior Loose articles . . . . . . . . . . . . . . . Removed or stowed Instruments, switches, and controls . . Check condition Clock . . . . . . . . . . . . . . . . . . . . . . . . . . Functioning Adjustable pedals (if installed) . . . . . . Pins secure CAUTION Remove left seat controls if person in that seat is not a rated helicopter pilot. 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. CAUTION Ensure all doors are unlocked before flight to allow rescue or exit in an emergency. CAUTION Shorter pilots may require cushion to obtain full travel of all controls. Verify aft cyclic travel is not restricted. NOTE Aircraft with optional equipment may have modified or additional checklist items. Refer to appropriate Pilot’s Operating Handbook Supplement. Page 5 of 6 Additional Items Preflight items for optional equipment installed on aircraft: ROBINSON MODEL R44 ROBINSON MODEL R44 8. Tailcone Skins . . . . . . . . . . . . . . . . . . . . . . . . . No cracks or dents Strobe light condition . . . . . . . . . . . . . . . . . . . . . . Check Antenna . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check 9. Cowl Door - Left Side Engine oil . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-9 qt Oil filter (if installed) . . . . . . . . . . . . . . . Secure, no leaks Throttle linkage . . . . . . . . . . . . . . . . . . . . . . . . Operable Battery and relay (if located here) . . . . . . . . . . . . Secure Steel tube frame . . . . . . . . . . . . . . . . . . . . . . . No cracks Engine sheet metal . . . . . . . . . . . . . . . . . . . . . No cracks Exhaust system . . . . . . . . . . . . . . . . . . . . . . . No cracks Cowl door . . . . . . . . . . . . . . . . . . . . . . . . . . . . Latched 10. Main Fuel Tank Quantity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check Filler cap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Tight Leakage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . None 11. Fuselage Left Side Baggage compartments . . . . . . . . . . . . . . . . . . Check Removable controls . . . . . . . . . . . . Secure if installed Collective control . . . . . . . . . . . . . . . . . . . . . . Clear Seat belts . . . . . . . . . . . Check condition and fastened Doors . . . . . . . . . . . . . . . . . . . . Unlocked and latched Door hinge safety pins . . . . . . . . . . . . . . . . . Installed Landing gear . . . . . . . . . . . . . . . . . . . . . . . . . Check Position light . . . . . . . . . . . . . . . . . . . . . . . . . Check Static port . . . . . . . . . . . . . . . . . . . . . . . . . Clear 12. Nose Section Pitot tube . . . . . . . . . . . . . . . . . . . . . . . . . . . . Clear Windshield condition and cleanliness . . . . . . . . Check Landing lights . . . . . . . . . . . . . . . . . . . . . . . . Check Yaw string . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check Page 2 of 6 Page 3 of 6 Page 4 of 6 3. Lower Cowl Door - Right Side Cabin air ducts . . . . . . . . . . . . . . . . . . . . . . . . . . Secure Carb heat scoop . . . . . . . . . . . . . . . . . . . . . . Secure Engine sheet metal . . . . . . . . . . . . . No cracks Fuel lines . . . . . . . . . . . . . . . . . . . . . . . No leaks Oil lines . . . . . . . . . . . . . . . . No leaks or chafing Exhaust system . . . . . . . . . . . . . . . . . . . . . No cracks Primer (if installed). . . . . . . . . . . . . Prime as required/ Locked/No leaks Cowl door . . . . . . . . . . . . . . . . . . . . . . . . . . Latched 4. Aft Cowl Door - Right Side Oil cooler door. . . . . . . . . . . . . . . . . . . . . . . . . . . Check V-belt condition . . . . . . . . . . . . . . . . . . . . . . Check V-belt slack . . . . . . . . 1.5 inches (4 cm) maximum Sprag clutch . . . . . . . . . . . . . . . . . . . . . . . No leaks Upper bearing . . . . . . . . . . . . . . . . . . . . . No leaks Telatemp - upper bearing . . . . . . . . . . . . . . . Normal Sheave condition. . . . . . . . . . . . . . . . . . . . . Check Flex coupling . . . . . . . . . . . No cracks, nuts secure

Show full text

Yoke flanges . . . . . . . . . . . . . . . . . . . . . . . . . . No cracks Steel tube frame . . . . . . . . . . . . . . . No cracks Tail rotor control . . . . . . . . . . . . . . No interference Tailcone attachment bolts . . . . . . . . . . . . . . . Check Cowl door . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Latched 5. Engine Rear Cooling fan nut . . . . . . . . . . . . . . . Pin in line with marks Cooling fan . . . . . . . . . . . . . . . . . . . . . . . . . . . No cracks Fan scroll . . . . . . . . . . . . . . . . . . . . . . . . . . . . No cracks Tailpipe hanger . . . . . . . . . . . . . . . . . . . . . . . . No cracks 6. Empennage Tail surfaces . . . . . . . . . . . . . . . . . . . . . . . . . . No cracks Fasteners . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Secure Position light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check Tail rotor guard . . . . . . . . . . . . . . . . . . . . . . . No cracks 7. Tail Rotor Gearbox Telatemp . . . . . . . . . . . . . . . . . . . . . . . . Normal Gearbox . . . . . . . . . . . . . . . . . . . . . . Oil visible, no leaks Blades . . . . . . . . . . . . . . . . Clean and no damage/cracks Pitch links . . . . . . . . . . . . . . . . . . . . . . . . . No looseness Teeter bearings . . . . . . . . . . . . . . . . . . . Check condition Teeter bearing bolt . . . . . . . . . . . . . . . . . Does not rotate Control bellcrank . . . . . . . . . . Free without looseness 1. Upper Forward Cowl Doors - Right Side Battery switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON Oil pressure and alternator lights . . . . . . . . . . . . . . . . ON Warning light test switches . . . . . . . . . . . . . Push to test Fuel quantity . . . . . . . . . . . . . . . . . . . . . . . Check gages Battery switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF Aux fuel tank quantity . . . . . . . . . . . . . . . . . . . . . Check Fuel filler cap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Tight Aux fuel tank . . . . . . . . . . . . . . . . . . . . . . . . . . No leaks Fuel lines . . . . . . . . . . . . . . . . . . . . . . . . . . . . . No leaks Fuel tank sump, gascolator drains . . . . . . . . . Sample Gearbox oil . . . . . . . . . . . . . . . . . . . . . . . . Full, no leaks Hydraulic system . . . . . . . . . . . . . . Fluid full, no leaks Rotor brake . . . . . . . . . . . . . . . . . . . . Actuation normal Flex coupling . . . . . . . . . . . . . . . No cracks, nuts secure Yoke flanges . . . . . . . . . . . . . . . . . . . . . . . . . No cracks Gearbox, hydraulic pump Telatemps . . . . . Normal Control rod ends . . . . . . . . . . . . Free without looseness Steel tube frame . . . . . . . . . . . . . . . . . . . . . . No cracks All fasteners . . . . . . . . . . . . . . . . . . . . . . . . . . . . Secure Tail rotor control . . . . . . . . . . . . . . . . . . No interference 2. Main Rotor CAUTION Do not pull down on blades to teeter rotor. To lower a blade, push up on opposite blade. Blades . . . . . . . . . . . . . . . . Clean and no damage/cracks CAUTION Verify erosion on lower surface of blades has not exposed skin-to-spar bond line. Reference Rotor Systems description in Section 7 of the Pilot’s Operating Handbook. Pitch change boots . . . . . . . . . . . . . . . . . . . . . No leaks Main hinge bolts . . . . . . . . . . . . . . . Cotter pins installed All rod ends . . . . . . . . . . . . . . . . Free without looseness All fasteners . . . . . . . . . . . . . . . . . . . . . . . . . . . . Secure Swashplate scissors . . . . . . . . No excessive looseness Upper forward cowl doors. . . . . . . . . . . . . . . Latched ROBINSON MODEL R44 ROBINSON MODEL R44 ROBINSON MODEL R44

775 Robinson R44 Raven II parts for sale

See all →

Parts listed for sale by vetted eBay sellers — confirmed on eBay at checkout.