MIL-T-18607(Aer)
31 March 1955
Superseding
SR-105b
10 December 1948
MILITARY SPECIFICATION
THERMAL ANTI-ICING EQUIPMENT, WING AND EMPENNAGE
This specification has been approved by the
Bureau of Aeronautics, Department of the Navy
1.
SCOPE
1.1 Scope.-This specification covers the general requirements for the
design, installation, and performance of thermal anti-icing equipment for the wings
and empennage surfaces in aircraft.
1.2 Classification. -There shall be no restriction as to the type of thermal
anti-icing equipment used. It is considered that either a system using the exhaust
heat of the engine, or combustion heaters will be acceptable for use as the prime
source of heat. For clarity, thermal anti-icing systems shall be designated-as:
Exhaust Heat Exchanger Anti-Icing System
Combustion Heater Anti-Icing System
Compressor Bleed Air Anti-Icing System
2.
APPLICABLE DOCUMENTS
2.1 The following specifications, standards,and publications of the issue
in effect on date of invitation for bids, form a part of this specification.
SPECIFICATIONS
FEDERAL
L-T-101
Tape, Shielding and Identification; Pressure
Sensitive
QQ-P-416
Plating, Cadmium (Electrodeposited]
WW-T-787
Tubing, Aluminum Alloy 52S, Round Seamless,
Drawn
MILITARY
JAN-A-669
Compound; Anti-seize; White' Lead Base, General
Purpose (for Threaded Fittings)
MIL-C-5015
Connectors; Electrical, "AN" Type
MIL-B-5087
Bonding; Electrical (for Aircraft)
MIL-W-5088
Wiring, Aircraft, Installation
MIL-E-5272
Environmental Testing, Aeronautical Equipment,
General Specification
MIL-H-5484
Heaters; Aircraft, Combustion Type
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