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SAE AS 8181 : 1997

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

View Superseded by

DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS, GENERAL SPECIFICATION FOR

Available format(s)

Hardcopy , PDF

Withdrawn date

01-06-2002

Superseded by

SAE AS 5498 : 2001

Language(s)

English

Published date

01-01-1997

€121.68
Excluding VAT

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

Defines requirements for ice detectors.

Committee
G-12
DevelopmentNote
Supersedes MIL D 8181 (B). (09/2004)
DocumentType
Standard
Pages
19
PublisherName
SAE International
Status
Withdrawn
SupersededBy
Supersedes

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DEFSTAN 00-970(PT0)/11(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
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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

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MIL L 7808 : K (1) LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE
MIL-STD-129 Revision R:2014 Military Marking for Shipment and Storage
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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
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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
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MIL P 7936 : LATEST PARTS AND EQUIPMENT, AERONAUTICAL, PREPARATION FOR DELIVERY
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MIL-P-116 Revision J:1988 PRESERVATION, METHODS OF
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)
MIL S 6743 : LATEST SWITCHES, PUSHBUTTON AND LIMIT
MIL-B-5087 Revision B:1964 BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
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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