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时间:2011-08-26 01:03来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

1 EGT Margin: the difference between actual EGT and the maximum EGT that can be tolerated by the engine.  Once this maximum temperature is reached the engine must be removed for maintenance and consequent restoration of EGT margin.

3.2.5.2.1.  Routine Engine Maintenance 
The following maintenance initiatives should be  Data - Mission A 
considered for all operations.  Annual cycles:  1800 
Annual Flight Hours:  2700 
Engine wash  Average sector length (Hours):  1.5 
With time, dirt will accumulate on the engine’s fan and compressor airfoils and consequently reduce engine efficiency. Water washes of the engine fan and core are recommended to  Data - Mission B Data - Mission C Annual cycles: Annual Flight Hours: Average sector length (Hours):  1500 3000 2 
remove this and can often reduce fuel flow by  Annual cycles:  1100 
0.5% and up to 1% - representing an annual  Annual Flight Hours:  3300 
fuel  cost  saving  per  aircraft  typically  from  Average sector length (Hours):  3 
US$24,100 and up to US$51,700 (with fuel at 

US$2.00 per US gallon and depending on the mission). Periodic engine water washes also have a positive effect on the exhaust gas temperature margin and consequently on engine overhaul intervals.
Contamination levels depend on the aircraft’s operation and environment, so each operator must optimize their wash frequency. As a starting point, operators are advised to carry out engine washes once a year. Operators wishing to optimize wash frequency may do so by monitoring the effects against and appropriate control data set (e.g. previously accumulated data or a partial fleet at the previous wash frequency). 
Engine wash Potential fuel economy per sector (Kilograms)
 Mission A  (1.5 Hours)  Mission B (2 Hours)  Mission C (3 Hours) 
20 to 35 KGs  25 to 50 KGs  35 to 70 KGs 

Figure 3-15
Potential benefits of Engine wash on fuel consumption

Reference document
AMM procedure: 72.00.00 PB701

Check of thrust reverser seal condition
The clean passage air through the engine nacelles (known as the by-pass air) is essential to overall engine efficiency. Seals around the thrust reversers play a crucial role in ensuring that this occurs and that overboard leakage is avoided.
Reference documents
AMM procedure: 
CFM:   78-11-11 PB601          78-32-41 PB601
IAE:  78-11-11 PB601          78-32-79 PB601


3.2.5.3. AIRFRAME MAINTENANCE
The airframe is a complex shape and includes many panels, doors and flight control surfaces. In order for the aircraft to perform at its optimum efficiency (i.e. to create the lowest amount of drag), the airframe must be as free from irregularities as possible. This means that surfaces should be as smooth as possible, panels and doors should be flush with surrounding structure and all control surfaces should be rigged to their specified positions.
 
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