Applications/Uses
- Aviation hydraulic systems
 
LD-4 Overview
Skydrol LD-4 was introduced in 1977 and also it is well known around the world. At the time of its introduction, it was a breakthrough product, solving problems of valve erosion and thermal stability common in earlier fluids. Because of its excellent thermal stability under real world conditions has given it a reputation as the gold standard among Type IV fluids. Skydrol LD-4 features low density, excellent thermal stability, valve erosion prevention, and also deposit control.
Approvals
Meets or Exceeds these Airframe Specifications
- Airbus Industrie NSA307110
 - Boeing Commercial Airplane Co. BMS3-11
 - McDonnell Douglas Corp. DMS2014
 - Lockheed Aircraft Corp. LAC C-34-1224
 - Society of Automotive Engineers AS1241
 - British Aerospace BAC M.333.B
 - Fokker
 - Embraer
 - Lastly, Bombardier BAMS 564-003
 
SKYDROL LD-4 Specifications
- Appearance: Clear, purple liquid
 - Neutralization number: 0.10 max
 - Moisture content (wt.%): 0.20 max
 - Finally, Specific gravity, 77°F/77°F: 1.003-1.013
 
Viscosity in cSt
- at 210°F/99°C: 3.66-4.00
 - at -65°F/-54°C: 2000 max.
 - Flashpoint, COC, min.: 320°F/160°C
 - Refractive Index @ 25°C: 1.443 to 1.451
 - at 100°F/38°C: 10.65-11.65
 - Lastly, Cleanliness Level: NAS 1638 Class 7 or better
 
			




				
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