CorporateCare Enhanced. Complete engine management, from line maintenance parts to full engine overhauls. Relax, we've got you covered. CorporateCare Enhanced is the most comprehensive aftermarket program providing full transfer of maintenance risk at a predictable, fixed price. CorporateCare Enhanced is a total risk transfer program that increases asset value and liquidity. For a fixed hourly cost CorporateCare Enhanced covers all Engine parts and labour when the time comes for the engine to be sent to an authorised Rolls-Royce overhaul facility.
It covers all parts and labour for mandatory and recommended service bulletins, as well as unscheduled shop visit costs. The Rolls-Royce global network of repair and overhaul operations ensures convenient access to the required facilities.
Our CAA part - approved training courses are designed against a backdrop of in-service operational data, latest maintenance practices, and troubleshooting procedures.
As experts in our field, we can help you identify your training requirements and create a training package that perfectly fits. Our practical approach to learning can be delivered at any one of our training centres around the world, or on-site at your own facility.
Our app provides owners and operators of Rolls-Royce powered business jets with contact information to assist in the operational availability of their aircraft by providing contact information for key customer contacts, locations of the nearest Authorized Service Centres and spares ordering information.
Vulnerability Reporting. Throughout our history, we have set out to achieve extraordinary goals. Investor Relations Keep up to date with the latest announcements, reports and publications from Rolls-Royce. Supermarine Spitfire Mk. Chance Vought F4U Corsair [gen]. F4U Corsair. Thanks for the quick response. I love these blueprints. I have a game room with an av Read More Crankcase fonvard end. Volute drain pipe union each end.
Retaining screws for carburetter chokes two. Supercharger securing nuts four wires , eight nuts. Plug for fuel pump r elief valve. Two oil filter covers two screws and one cap nut for each. Lock Wires. It should also be confirmed that the two earthing wires have been fitted, one connecting the short extension pipe with supercharger, and the other connecting the coolant pump with short coolant pipe to carburetter.
It is important that the cut-out hole, 0 , Fig. Therefore, except where an assembly has been extensively altered or is additional e. This applies also to "Fits and Clearances". PAGE Fig. Fig: Fig. Revised and Reprinted June, i Leading Particulars of Engines. Page x. Weight of engine as a. Din1ensions, new. Permissible worn dimensions. I Ins.
I lns. Bore of rocker arm J iamcter of floating bush! Page Dimensio11s, new. IPermissible worn clearance. I Bore of rear wheelca.
I to page 75 for remaining dimensions. Diameter of upper planet cage shank Backlash between any pair of gears in epicyclic train See Foundation Diagram B. II E. Arrangement of Dual Drive Unit. Arrangement of Manual Control to Oil Cock. F'i tt. Gl2AM Nf 5. Double Banjo Connection on Relief Valve Pf'YCM 6. See Arrgt. Change bottom Plug J r to small Banjo Fitting. Sec Arrgt. Of:' 8 Et. Replace :. Ope n Cock by moving Lever to the Rearward position.
Replace Plate to lock Lever in the new position, lock with wire and seal. See Foundation Diagram C. See Atrgt. Cits" Oil Seal. Inset the Inner Tube T2 down the bore of Shaft, and carefully screw down to. Follow up with the outer tube T3 also pressed down to a sho.
Fit Piston and Cylinder. Care must be ta. Pl:scx No. Pipe Cra11kcaae. Inner Tube-. Page a Prepare the engine for short-term storage as follows: Remove the bottom magnetic plug to drain the oil from the power-and-accessory gearbox REF. Move the engine mounting bracket adapters 14 inboard to engage the side engine mounting brackets 1.
Page d Tighten the screws to in-lb 3. Page 2 Remove the shipping covers and caps on the right side of the engine. Page 4 Remove the shipping covers and caps on the front and the rear of the engine. Page Exciter Terminal Stud Cover. Page c Operate the engine at groud idle for 15 minutes.
Page b Do the preservation of the engine oil system each 90 days if the aircraft is stored outdoors and each days if the aircraft is stored indoors. Page MIL-D at intervals based on local humidity conditions and replace as necessary.
Page Examine the desiccant at regular intervals based on local humidity conditions , and rejuvenate as necessary. Keep the engines indoors if not installed in an aircraft or engine shipping container. Page b Remove the dust caps from the tubes, fittings, hoses, and electrical connectors, if applicable. Page 5 Make sure that the fuel flow and the oil pressure are satisfactory.
Page 2 Remove the engine and the engine components. Page b Put up the applicable warning signs. Page a Remove the power-turbine fuel governor REF. Page d Remove the washer 16 and spacer 17 from the turbine bearing scavenge-oil fitting 14 and the washer 18 from the turbine bearing pressure oil fitting Page b Install the main oil temperature sensor REF.
Page - The system is safe - Access is available - The applicable circuit breakers are open - The applicable warning signs are in position. Page a Install the igniter lead REF. Page Examine the area around the orifice at the end of the next flight for a minimum of five minutes.
Page Decrease the speed to ground idle. Do a check of the operation of the anti-icing valve REF. Operate for two minutes. Stop the engine REF. Section Page FAA approved flight manuals can be used in lieu of the procedure given in this manual if they are Rolls-Royce approved. Go to step 1.
Page Engine performance does not come back to the initial baseline power available when the engine was new or overhauled. Page The torque indication position necessary will be from the torque correction chart when you record the chosen base line torque and pressure altitude to be flown. Page b Fly the aircraft at a pressure altitude convenient to usual flight and in increments of feet from sea level. The maximum altitude for the check is 10, ft. Page This plot will be almost the same as shown in FIG.
Page The data can be used to get an indication of the engine area where corrective action is necessary. Page - Dynamic Solutions Systems, Inc. Page Record the vibration data that applies to ground operation.
Record as many test points as possible before you fly the aircraft. Page k Manufacturer aid If suspected airframe and engine components have been inspected, repaired, or replaced, refer to the applicable manufacturers instructions as indicated by the vibration test data. If the vibration symptoms continue, speak with Rolls-Royce. Page - Examine the gas producer turbine case for damage. Page - Attaching hardware that has damage, or is missing or loose.
If necessary, do the maintenance action to correct the unsatisfactory condition. Page b Do the inspection of the turbine REF. Page e Do steps I. Page If necessary, you can also steam clean the external surfaces of the engine.
Page If the engine was operating when the extinguishing agent the agent was applied it is not necessary to clean the internal surfaces. Page 10 seconds. Make sure that the water spray flows as close to the bullet nose of the compressor inlet as possible. Page 1 Clean the exterior of the engine. Page Torquemeter support shaft nuts at interface splitlines after nut installation. Turbine assembly mounting pads on gearbox cover. Gearbox cover mounting face for the turbine. Paint the depressed fireshield area.
Page This applies to all areas not previously protected or to areas on which a layer was previously applied. Page 1 Blend repair the compressor impeller. Page Clean the oil pressure reducer 3 REF.
Examine the oil pressure reducer 3 REF. Page b Remove the applicable warning signs. Page a Remove the oil pressure reducer REF.
Page a Remove the internal retaining ring 1. Page b Remove the right hand adapter 2 from the compressor scroll 5. Page b Remove the left hand adapter 4 from the compressor scroll 5. Page a Examine all of the replacement parts and their interfaces to make sure that they are serviceable.
Page 2 from the compressor scroll adapter flange 6. Page a Remove the piston split ring 3 , rope packing 4 , and piston split ring 5 from the left and right hand compressor-discharge air tubes 1 and 2. Page a Examine all of the replacement parts and their interfaces to make sure they are serviceable.
Page Repair the air tube REF. Page Replace the split seal piston no effect on sealing. Not repairable. Replace the split seal piston ring. Page NOTE: It is not necessary to remove the burner drain valve or plug from the outer combustion case before removal of the outer combustion case from the engine.
Page 3. Remove the case assembly 8 from the engine. Page a Do the visual inspection of the case assembly to the limits that follow.
Page b Remove the valve assembly 3 from the outer combustion case 1. Discard the O-ring. Page a Pull the combustion liner 2 away from the 1st-stage turbine nozzle shield 1. Page 1 Do the visual inspection of the combustion liner assembly combustion liner.
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