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SAE AS8181A

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

Detector, Ice, Air Intake Duct, Aircraft Engines and Airframe Systems, General Specification For

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

08-07-2002

Withdrawn date

08-07-2002

US$145.14
Excluding Tax where applicable

Foreword
1 Scope
2 Applicable documents
3 Quality assurance provisions
4 Preparation for delivery
6 Notes

Defines requirements for ice detectors.

DevelopmentNote
Supersedes MIL D 8181 (B). (09/2004)
DocumentType
Standard
Pages
19
PublisherName
SAE International
Status
Withdrawn
Supersedes

This specification establishes requirements for ice detectors.

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DEFSTAN 00-970(PT0)/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/14(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/11(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/13(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/12(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/8(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS

MS33540 Revision J:1986 SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR (S/S BY NASM33540)
MIL L 7808 : K (1) LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE
MIL-STD-129 Revision R:2014 Military Marking for Shipment and Storage
MIL-STD-704 Revision F:2004 Aircraft Electric Power Characteristics
MIL-STD-130 Revision N:2007 Identification Marking of U.S. Military Property
MIL P 8585 : LATEST PRIMER COATING, ZINC CHROMATE, LOW-MOISTURE SENSITIVITY
MIL-D-6055 Revision D:1987 Drum, Metal Reusable, Shipping and Storage (Cap. from 88 to 510 Cubic Inches)
MIL-D-70327 Base Document:1959 DRAWINGS, ENGINEERING AND ASSOCIATED LISTS
MS33678 Revision A:2004 Connector, Receptacle, Electric, Integral Mounting
MIL E 5400 : T ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR
MIL-STD-831 Base Document:1963 TEST REPORTS, PREPARATION OF
MS33588 Revision E:1984 Nuts, Self-Locking, Aircraft, Reliability and Maintainability Usage Requirements for (S/Sby NASM33588)
MS20995 Revision E:1974 WIRE, SAFETY OR LOCK (S/S BY NASM20995)
MIL P 7936 : LATEST PARTS AND EQUIPMENT, AERONAUTICAL, PREPARATION FOR DELIVERY
MIL-STD-143 Revision B:1969 STANDARDS & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970)
MIL E 5557 : LATEST
MIL A 8625 : F ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS
MIL-P-116 Revision J:1988 PRESERVATION, METHODS OF (S/S BY MIL-STD-2073-1)
MIL C 5015 : G CONNECTOR, ELECTRICAL, CIRCULAR THREADED AN TYPE, GENERAL SPECIFICATION FOR
MIL-STD-202 Revision H:2015 Electronic and Electrical Component Parts
QQ-P-416 Revision F:1991 Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416)
MIL S 6743 : LATEST SWITCHES, PUSHBUTTON AND LIMIT
MIL-B-5087 Revision B:1964 Bonding, Electrical, and Lightning Protection, for Aerospace Systems (S/S by MIL-STD-464)
MIL-S-7742 Revision D:1991 Screw Threads, Standard, Optimum Selected Series: General Specification for
MIL N 25027 : G NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F

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US$145.14
Excluding Tax where applicable