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BELLL 47G 3B1.

TCs Tips to make your Daily/Pre-flight Inspection safer.

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The following hints can be incorporated with the daily and pre flight inspections required by BELL and the aircraft log book maintenance statement.


   Start at the left (pilots) side of the helicopter and work your way around the machine in an anti-clockwise direction.  Duplicate the left side inspection on the right hand side where required. 

   Standing outside the helicopter, lean in and check that the cyclic and collective control frictions are off. Read the next 5 tips carefully before moving the cyclic, collective and pedals through their full range

   Take care anytime that you are tightening the collective friction. Over tightening can easily strip the thread in the friction control rod attach nut under the cabin. If the nut is stripped, it is possible for the collective to suddenly rise if you take your hand off it while the rotors are turning. This could be a disaster if it happened on the ground at flight RPM. 

   Hold the throttle fully closed, while checking the collective lever for full up and down freedom of travel. This action stops the carburetor accelerator fuel pump from over priming and flooding the engine 

   Yes - its OK to move the cyclic in a circle to check its full range of movement on the cyclic control rigging stops.  It's better to then move the cyclic fore and aft and then laterally, feeling for any resistance between the full fore/aft and lateral rigging stops. This because  it is important to realise that each cyclic control servo cylinder acts in two directions and therefore a positive check of the feel in BOTH directions of each power cylinder is required. 

   Lean back and observe all control systems on the engine side of the firewall while moving the cyclic through its full range with your left hand to see they are not hitting or binding on anything. Particularly eyeball each rod end to see that it is tight. Worn rod ends cause delay with control inputs to the rotor disc and make hovering harder.  

    lean inside and push the left and right Tail Rotor pitch control pedals fully back and forward. Listen for the banging noise from under the cabin floor as the pedals hit their max rigging stops. Have your mechanic check the tail rotor rigging at the tail rotor gearbox if no noise is heard. You may not be getting full tail rotor pitch travel. This could turn into a really serious in flight control problem if the tail rotor cannot obtain either full high or full low pitch angles. 

   If a door is fitted, check that both retainer pins are through their hinges when the door is closed and latched. If a part of the system is damaged or out of alignment causing a pin to not protrude through the hinge, the door may come off in flight and hit your main or tail rotor. 

    Starting with the left front, check the skid uprights for weld cracks. 

    Check the rear skid cross tube attach saddle clamps for security and grip (is the cork or rubber gasket loose?) 

   Look through both the front and rear cross tubes. You should be able to see daylight at the other end. If you cannot see through a tube, it may have too much permanent set due age or a hard landing. Usually your mechanic can roll the tube 180 degrees as a fix. 

   Check the condition of both fan belts about 3/8 inch bow in when pushed hard in with one finger.  Tighten loose belts they may fling off if loose and under high power circumstances and the engine may seize within one minute due to lack of forced cooling air. Make sure any excess grease from the engine/transmission adaptor plate or fan bearings does not fall onto the belts. 

       Use a torch and check the edges of both fan belts for fraying and also inside the belt cogs for cracks which may go into the belt ply  

   NOTE:  If any oil is leaking from the transmission side of the Top Fan Drive Pulley or if the pulley can be made to move or rock in/out or in a horizontal or vertical plane, DO NOT FLY THE AIRCRAFT UNTIL THE CAUSE HAS BEEN DETERMINED.  I REPEAT Do not fly the aircraft! It may be that the fan drive gear or its support bearings are stuffed.  CHECK THE ENGINE OIL PRESSURE FILTER FOR MAGNETIC METAL CONTAMINATION.  

   At the bottom of each hydraulic servo is a pin with a round head passing through the clevis on the servo rod. On the other side of the clevis, it has a castellated nut with a safety split pin through it. You must be able to freely turn the pin. If hydraulic fluid is leaking from the lower seal on the servo onto the pin, clean it off as it can attract dust and grit which in turn can cause wear on the pin. 

   Place both hands in the middle of the left side of the fuel tank. Push on/off against the fuel tank, checking for security. Sometimes the tank works loose on the main frame/basket attach bolt or one of the small rear attach brackets may be broken. 

    Before any flight, condensation or small water droplets clinging to the inside of the tank may be dislodged if the tank is slapped with palm of your hands. 

   Flight Tip: Plan fuel consumption at 70 litres per hour.  Dip the tank after 2 hours.  On level ground, fuel 1 inch (approx) deep in front of forward tank baffle gives you 8 10 minutes until dry tanks.  If you have fuel quantity this low dont fly!!!  Take the temporary embarrassment in exchange for no accident under pressure and no insurance claim with your name FOREVER attached to it.  You are still employable anywhere, only if your accident record is clean.  Think about it!  

    Make sure that both fuel filler caps are latched in a down position.  If latched up, water can seep thru centre pin if the O ring is worn.  By keeping the latch down, water will not accumulate around centre pin and will drain overboard.  

   Look for cracks in the horizontal airframe tube near where the fuel tank attaches (between the basket/airframe attach bolt and the rear of the tank). These can be caused by internal corrosion. If the frame cracks completely through, there is potential for the tail rotor drive front short shaft to become disconnected in flight. 

   Look for loose or missing engine cylinder rocker cover screws. These tend to vibrate loose when cork gaskets are used under the rocker cover. It is preferable to use the new red neoprene gaskets for long life, no oil leaks and retention of the rocker cover screws. 

   On turbo machines check that no exhaust manifold pipe to cylinder holding studs have shaken loose and gone overboard. Often you can hear this in flight or at ground idle as a loud ticking noise as the hot exhaust gas exits the hole. When a stud comes loose or comes out, the white hot exhaust gas can erode the alloy cylinder flange, distort the exhaust pipe flange, damage/burn a spark plug and make for sluggish turbo response.  

   Observe that no green or blue Avgas fuel stains are coming from the intake manifold pipe/cylinder attach area gaskets. A blown gasket in this area can lead to sluggish performance. Erratic fuel air mixtures can cause a cylinder to run lean and damage the piston or exhaust valves.  Check for any suspected leaks by gently spraying a garden hose in the area while the engine is idling. If a gasket is faulty, water will be sucked in and cause the spark plugs to short out on the cylinder with the faulty intake gasket  

   If this is the first time that you will have flown the machine or some one else has recently been flying it in a dusty environment remove the filter cover and remove and inspect the air filter. Look inside the housing for signs of dust bypassing the air filter or passing through any cracks in the flexible tube connecting between the housing and turbo.  

   Check that a non thinking mechanic has not drilled a hole inside the filter housing to get his screwdriver in to adjust the density controller!  If there is a hole and it isnt sealed hot engine air and damaging dust will be able to flow through/bypassing the filter. 

   While the air filter is out shine your torch in on the turbo impeller and inspect for damage on the blades such as nicks, scratches or where the blades might have been rubbing on the turbo casing. Grip the centre of the impeller and try to move it up/down, or in/out, it should only have a minimal amount of movement; excessive play may indicate a stuffed turbo.  

   Note: There are two types of turbocharger heavy and lightweight. The heavyweight identified by having four studs or bolts securing the large diameter exhaust pipe to the turbo itself - should have no free play; the lightweight has a small amount. 

   When refitting the air filter, smear some rubber grease on both the ends to ensure a good seal between the filter and the filter seals.  

   Turbo flight tips:


     Continuous high manifold pressure requires much higher turbo rpm. Higher rpm causes extra loading on the turbo and may cause premature bearing wear thus reducing turbo time before overhaul.



If you need to hover above 26 inches MAP, get into wind and, if possible, use ground effect.



Try to always keep above transition to keep your power requirements down therefore   prolonging the turbo life and reducing the chance of turbo failure.



Remember - that extra inch of boost you dont really need to be using is causing the turbo to spin another 5,000 rpm. 



If you are safely able to do it 30 inches MAP and 42 knots are good figures to try and keep at for a climb. You will use a lot less fuel, the engine and main transmission will have reduced wear and run cooler while the turbo life will be increased dramatically



     Engine Oil tank Quantity: Check the dip stick reading is 10 US Qts of oil. This allows for any oil burn during a 3 hour flight.   Max oil consumption is 1 litre per 2 hours.  In the warm ambient conditions in Australia, normal power usage consumes about 1 litre of oil per 4 hours.  Through fitment of an external oil cooler to maintain the oil temperature at 75 o C, I have flown machines with an oil consumption as low as 1 litre in 15 hours which equates to 1 litre used over the 25 hour oil change period as it does not need topping up again before the scheduled oil change. Contact  TC if you want information on his extra oil cooler installation.



Use the correct viscosity oil for the average ambient temp. If in doubt regarding which grade or type of oil to use or you cannot positively identify the type in a container do not put it in the engine!



Check the Engine Driven Fuel Pump for three items

1        The screw that adjusts the fuel pressure regulator is loc wired correctly to stop it coming loose in flight.

2        The bottom of the mounting flange on the pump has a threaded hole to allow the fitment of a tube to drain any   fuel/oil leakage that main accumulate in the enclosure between the pump and the engine. Check that no person has fitted a solid blank to block this hole - True I have seen this!

3    Before every flight, check that fuel is not dripping from this area. Do Not Fly if there is any sign of a constant drips, as it may be an indication that the pump is about to fail. This could lead to complete engine failure in certain circumstances.


Before proceeding further down the left side of the machine to the tail rotor, clamber up on the left rear side of the transmission to inspect Up Top. Do not grab a hand hold on the front tail rotor drive short shaft to help yourself up as you may damage it


    Inspect the leading edge of the blades for erosion.  It is soft, easily damaged stainless steel, and, in an erosive environment, requires 18 inches of 3M M/R blade tape fitted outboard at all times.  Failure to operate without tape in a dusty environment shortens blade life considerably!  Keep out of the dust by defensive flying (an understanding of performance, wind and the power required curve.)  AVOID these DUSTY situations.  If the tape is holed or damaged, remove BOTH tapes and install new tape on return to base.


     Grease ALL the M/R hub bearings.  Always purge the M/R grip bearings (starting with gentle pressure on the outboard nipple concealed near the M/Rotor blade root). Apply the grease slowly so that it has a chance to work through the bearings and force the old grease before it. Use only Aeroshell grease 14 throughout the aircraft.


    With a torch, inspect the inboard area of the M/R grips for cracks emanating from the internal threads machined for the Grip retainer nut.


     With a torch, inspect the steel inner gimbal trunnion for cracks.


     With a torch, inspect the outside surface of the alloy gimbal ring for cracks radiating from the inner Gimbal trunnion bearing machined recess.


     With a torch, inspect the damper frame clamps for security and cracks. Check the damper frame is tight on the mast,  otherwise if loose more control inputs required especially for steady hover.


     With a torch, inspect the damper levers for cracks.


      Check all control bolts/rod ends for fretting due lack of shimming.


      Check both loc wired bolts in the swash plate scissors for security.


      Check/identify any oil leaks from the main transmission, especially from the top seal area.


      Check the inlet induction hose isnt collapsing so it that it doesnt suck closed when the engine is running.


     Check that there is a small gap between the collective yoke and the collective stops. The stops are the 2 loc wired bolts in the slot underneath the swashplate, 180 degrees apart. This is critical on a machine with a hydraulic boosted collective.


Now complete the remainder of your inspection down the tail boom to the tail rotor:



     Tail rotor drive shaft: very little play is permitted in the first and last bearings on the T/Rotor drive shaft. Look especially for cracks in the weld of the bearing mount/tail boom attach brackets.


     Rear T/Rotor drive short shaft: with the M/Rotor untied, turn the main rotor slowly and check that the rear short shaft is not bent, indicating a tail Rotor Blade strike on Grass or water. A bent shaft requires inspection of the Tail rotor drive system.


     Check/clean all the tail rotor and sync elevator stainless steel flexible control cables with a rag.  Use the rag  for the following reasons:

1.      To snag any slivers indicating breaks or frays in the weave of the cable

2.      To wipe them clean to look for shiny wear flats where they pass thru pulleys. (Grease on cables attracts dust dust works into the cables the cables wear)

3.      The rag also stops pain and blood caused by your fingers being ripped open by any cable frays.


         Rear Strobe/rotating beacon: Check that beacon, including the plastic lens cover, is secure and therefore cannot fall off  and damage tail rotor blades.


     Check that no fretting marks are coming from the front of the T/Rotor drive extension tube, where it is clamped to the rear frame yoke.  It may need tightening. Check that none of the back end is loose by pushing and pulling (gently) the T/R guard tube, just behind the TRGBox.


     Check that the tail rotor slider boot hasnt been over greased, popping the boot.


     Check all round the turbo exhaust transition for exhaust leaks or missing attach bolts. Inspect for cracks around the weld area on the transition assy.


    Oil change and check the engine pressure filter as per Lycoming requirements every 25 engine running hours.


    Remove and inspect or replace any external full flow oil filter every 50 engine running hours.


COCKPIT: Start up Checks and Tips: (see B47 Pilot Notes Page)


Check: Nothing to jam the T/R pedals in the chin bubble.


Check: Turn the master switch on and check that all temp gauges reading ambient at the first start of day if not how do you really know if you are under or over temping?.


Check: Oil Temp switch: Oil temp priority = transmission.


Check: If the Door(s) off secure the seats etc with the seat belts so they are not sucked out the opening in flight and hit the T/Rotor.


Check: Nothing to jam the dual collective, if fitted. Make sure that the dual collective is not restricting full down collective otherwise auto rotation could be embarrassing besides extremely dangerous.


Remember:   Hot start Nil or no more than one throttle prime.

                    Cold start 3 - 4 throttle primes.

Below Zero Ambient cold start:  Lift the collective full up prime with the throttle 4 times holding the throttle in the full open position for about 3 seconds on each stroke then collective down, throttle closed and start with full carb heat on.

Flooded engine procedure (smoking exhaust pipe or fuel running from carb filter drain):  mixture lean, mags off, full throttle, clear engine, close throttle, mags on try start again.

Note: Every time you lift the collective or work the throttle you are making the carb accelerator pump push raw fuel into the system.  Great if the engine needs it cold. When its hot - all you are doing is keeping the Arabs rich and stuffing your battery as you try to get a flooded engine started.





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