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Normas SAE

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SAE

SAE AMS4001H

En Vigor
2002-08-21
Aluminum Sheet and Plate 0.12Cu (1100-0) Annealed
 
SAE

SAE AIR13A

En Vigor
1951-10-01
FINAL REPORT ON COLD STARTING OF RECIPROCATING AIRCRAFT ENGINES
 
SAE

SAE AMS5671F

En Vigor
1996-09-01
Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings 72Ni - 15.5Cr - 0.95Cb - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode or Vacuum Induction Melted 1800 °F (982 °C) Solution Heat Treated, Precipitation Hardenable
 
SAE

SAE ARP699B

En Vigor
1963-12-01
LOW PRESSURE HIGH TEMPERATURE PNEUMATIC DUCTING SYSTEMS (300 PSI AND 1000 F MAXIMUM)
 
SAE

SAE AMS3267/1

En Vigor
1992-04-01
SEALING COMPOUND, LOW ADHESION, CORROSION INHIBITING 200 - 600 Poises (20 - 60 Pa·s), 1/2 Hour Application Time (A-1/2)
 
SAE

SAE ARP488G

En Vigor
2024-12-04
Cabin Emergency Exits Design and Operation - Transport Category Aircraft
 
SAE

SAE AMS5010B

En Vigor
1946-01-01
STEEL Screw Stock
 
SAE

SAE AMS4764G

En Vigor
2019-06-17
Copper Alloy, Brazing Filler Metal 52.5Cu - 38Mn - 9.5Ni 1615 to 1700 °F (879 to 927 °C) Solidus-Liquidus Range