Light
Dark
System
Log In
Loading...
Compare / EASA/
Incorporated Amendments
/
Compare & Highlight Differences
AMC E 690 Engine bleed
Available versions for ERULES-1963177438-8953
ED Decision 2007/015/R
found in: CS-E Amdt 5 - Engines (Dec 2018)
Version
...18)
Text
Removed: 0
Added: 0
Unchanged: 0
Share
AMC E 690 Engine bleed ED Decision 2007/015/R For reducing test complexity, and for improved flexibility needed to attain the key parameters (speed, temperature and torque) during the 2-hour test of [CS-E 740(c)(3)(iii)](#_DxCrossRefBm1371447586), maximum air bleed for Engine and aircraft services need not be used if the applicant can show by test or analysis based on test that the Engine's ability to meet the strip examination specifications of [CS-E 740(h)(2)](#_DxCrossRefBm1371447586) is not enhanced. The analysis should include — The effect of the bleed air extraction to the Engine secondary air system which provides cooling air to various Engine components, — The thermodynamic cycle effects of bleed (e.g., gas generator speed to output shaft speed changes). [Amdt. No.: E/1]
Instantly search and compare regulation versions
Cite and compare ruling versions
Build personal collections of key clauses
Generate compliance documentation effortlessly
Let the AI focus on specific regulation versions
Create Free Account (limited time offer)
Don't show this again