Browse Standards AIR4367
Historical ISSUED 1995-04-01

AIRCRAFT ICE DETECTORS AND ICING RATE MEASURING INSTRUMENTS AIR4367

This document provides information regarding ice detector technology, and design and operating requirements. Icing rate information is included where applicable. The primary application is associated with ice forming on the leading edges of airfoils and inlets with significant forward velocities. Information related to detection of ice at static conditions, ice over cold fuel tanks, and icing at low velocity operation is also included. The material is primarily applicable to transport and light aircraft. Special consideration for rotorcraft is appended separately.
AIR4367B
2022-05-24
Latest
Revised
AIR4367A
2012-10-11
Historical
Reaffirmed
AIR4367
1995-04-01
Historical
Issued

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 10% off list price.
Login to see discount.
Special Offer: AeroPaks offers a customized subscription plan that is cost-effective and allows you to choose the number of downloads and Aerospace and Aerospace Material documents you need. Find more information here.
We also recommend:
STANDARD

Design and Verification of Aircraft Nose Wheel Steering Systems

ARP1595B

View Details

STANDARD

Wheels and Brakes, Supplementary Criteria for Design Endurance Civil Transport Aircraft

ARP597E

View Details

STANDARD

Aircraft Nosewheel Steering/Centering Systems

AIR1752A

View Details

Get Involved

Want to participate in updating this standard?

X