Easa part 66 module 15 Gas Turbine Engine CH 24/25.
The Jet Engine by Rolls Royce
Chapter 1/25 : Basic mechanics (page 1 to 10)
Chapter 2/25 : Working cycle and airflow (page 11 to 18)
Chapter 3/25 : Compressors (page 19 to 34)
Chapter 4/25 : Combustion chambers (page 35 to 44)
Chapter 5/25 : Turbines (page 45 to 58)
Chapter 6/25: Exhaust system (page 59 to 64)
Chapter 7/25 : Accessory drives (page 65 to 73)
Chapter 8/25 : Basic mechanics (page 73 to 85)
Chapter 9/25 : Lubrication (page 85 to 94)
Chapter 10/25 : Internal air system (page 95 to 120)
Chapter 11/25 : Fuel system (page 121 to 132)
Chapter 12/25 : Starting and ignition (page 133 to 146)
Chapter 13/25 : Ice protection (page 147 to 152)
Chapter 14/25 : Fire protection (page 153 to 158)
Chapter 15/25 : Thrust reversal (page 159 to 168)
Chapter 16/25 : Afterburning (page 169 to 180)
Chapter 17/25 : Water injection (page 181 to 186)
Chapter 18/25 : Vertical/short take-off and landing (page 187 to 198)
Chapter 19/25 : Noise suppression (page 199 to 206)
Chapter 20 & 21 /25 : Thrust distribution & Performance (page 207 to 214)
Chapter 22/25 : Manufacture (page 215 to 228)
Chapter 23/25 : Power Plant Installation (page 229 to 242)
Chapter 24/25 : Maintenance (page 243 to 262)
Chapter 25/25 : Overhaul (page 251 to 264)
Download Full Document from Amazon Last edition (2015-07-20).
Maintenance ( Chapter 19/25) PDF.
Maintenance Rolls Royce the jet.
Aircraft Maintenance Engineering
2. as a result of several aspects of maintenance are subject to the approval of a recognized authority, it ought to be absolutely understood that the data given during this half is of a general nature and isn’t meant as a substitute for any official directions.
3. the excellent directions covering the particular work to be done to support maintenance (para. 8) and unexpected maintenance (para. 10) are contained within the craft maintenance manual. each this publication, and also the craft maintenance schedule mentioned in para. 8, are supported manufacturers’ recommendations and are approved by the acceptable soundness authority aircraft maintenance engineering.
4. the most time associate engine will stay put in in an craft (engine life) is restricted to a hard and fast amount in agreement between the engine manufacturer and soundness authority. On some engines this era is brought up because the time between overhaul (T.B.O.) and on reaching it the engine is removed for complete overhaul aircraft maintenance engineering.
5. as a result of the T.B.O. is truly determined by the lifetime of one or 2 assemblies among the engine, throughout overhaul, it’s typically found that the opposite assemblies are automatically sound and fit continue in commission for a way longer amount. Therefore, with the introduction of standard engines and also the improved scrutiny and observation
techniques offered, the T.B.O. methodology on limiting the engine’s life on-wing has been replaced by the ’on-condition’ method. aircraft maintenance engineering.
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Module 15: Gas Turbine Engine
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