MIL L 87100 : 0

Superseded

Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, POLYPHENYL ETHER BASE

Available format(s): PDF

Superseded date: 28-11-1997

Language(s): English

Published date:

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Outlines one grade of aircraft gas turbine engine lubricating oil.

Committee	FSC 9150
Document Type	Standard
ISBN
Pages
Published
Publisher	US Military Specs/Standards/Handbooks
Status	Superseded
Superseded By	MIL-PRF-87100 Revision A:1997

PPP-C-1337 Revision B:1976	CONTAINERS, COMPOSITE (STEEL DRUM WITH POLYETHYLENE INSERT)
MIL-STD-147 Revision E:2008	PALLETIZED UNIT LOADS
MIL-STD-290 Revision H:2013	PACKAGING AND MARKING OF PETROLEUM AND RELATED PRODUCTS
MIL-L-27502 Base Document:1972	LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, ESTER BASE
SAE AMS 5544 : 2014	NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 57NI - 19.5CR - 13.5CO - 4.2MO - 3.0TI - 1.4AL - 0.05ZR - 0.006B, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, ANNEALED
MIL-S-13282 Revision B:1973	SILVER AND SILVER ALLOYS
SAE AMS 6260S : 2016	STEEL, BARS, FORGINGS, AND TUBING, 1.2CR - 3.2NI - 0.12MO (0.07 - 0.13C) (9310)
SAE AMS 6490 : 2014	STEEL BARS, FORGINGS, AND TUBING 4.0CR - 4.2MO - 1.0V (0.77 - 0.85C) (M-50) PREMIUM AIRCRAFT-QUALITY FOR BEARING APPLICATIONS CONSUMABLE ELECTRODE VACUUM MELTED
SAE AMS 4908 : 1988	TITANIUM ALLOY, SHEET AND STRIP 8MN ANNEALED, 110 KSI (758 MPA) YIELD STRENGTH
SAE AMS 6475 : 2013	STEEL, NITRIDING, BARS, FORGINGS, AND TUBING, 1.1CR - 3.5NI - 0.25MO - 1.2AL (0.21 - 0.26C)
FED-STD-791 Revision D:2007	TESTING METHOD OF LUBRICANTS, LIQUID FUELS, AND RELATED PRODUCTS
MIL-STD-105 Revision E:1989	SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES

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Outlines one grade of aircraft gas turbine engine lubricating oil.

Committee	FSC 9150
Document Type	Standard
ISBN
Pages
Published
Publisher	US Military Specs/Standards/Handbooks
Status	Superseded
Superseded By	MIL-PRF-87100 Revision A:1997

PPP-C-1337 Revision B:1976	CONTAINERS, COMPOSITE (STEEL DRUM WITH POLYETHYLENE INSERT)
MIL-STD-147 Revision E:2008	PALLETIZED UNIT LOADS
MIL-STD-290 Revision H:2013	PACKAGING AND MARKING OF PETROLEUM AND RELATED PRODUCTS
MIL-L-27502 Base Document:1972	LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, ESTER BASE
SAE AMS 5544 : 2014	NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 57NI - 19.5CR - 13.5CO - 4.2MO - 3.0TI - 1.4AL - 0.05ZR - 0.006B, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, ANNEALED
MIL-S-13282 Revision B:1973	SILVER AND SILVER ALLOYS
SAE AMS 6260S : 2016	STEEL, BARS, FORGINGS, AND TUBING, 1.2CR - 3.2NI - 0.12MO (0.07 - 0.13C) (9310)
SAE AMS 6490 : 2014	STEEL BARS, FORGINGS, AND TUBING 4.0CR - 4.2MO - 1.0V (0.77 - 0.85C) (M-50) PREMIUM AIRCRAFT-QUALITY FOR BEARING APPLICATIONS CONSUMABLE ELECTRODE VACUUM MELTED
SAE AMS 4908 : 1988	TITANIUM ALLOY, SHEET AND STRIP 8MN ANNEALED, 110 KSI (758 MPA) YIELD STRENGTH
SAE AMS 6475 : 2013	STEEL, NITRIDING, BARS, FORGINGS, AND TUBING, 1.1CR - 3.5NI - 0.25MO - 1.2AL (0.21 - 0.26C)
FED-STD-791 Revision D:2007	TESTING METHOD OF LUBRICANTS, LIQUID FUELS, AND RELATED PRODUCTS
MIL-STD-105 Revision E:1989	SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES