A-82-055

NTSB Safety Recommendation — Aviation

Recommendation text

IN VIEW OF THE POTENTIALLY CATASTROPHIC RESULTS OF A PROPELLER BLADE FAILURE, THE NTSB RECOMMENDS THAT THE FEDERAL AVIATION ADMINSTRATION: REVIEW THE DESIGN OF THE RATIER-FIGEAC MODEL 146 PROPELLERS FOR COMPATIBLE COMPOSITION OF THE DEICING BOOT, ITS ADHESIVE MATERIAL, AND THE PROPELLER BLADE MATERIAL IN THE EVENT IT IS EXPOSED TO EXCESSIVE HEAT. IF CORROSIVE BYPRODUCTS ARE PRODUCED BY EXCESSIVE HEAT, REQUIRE MODIFICATION OF THE BOOT TO ELIMINATE CORROSIVE BYPRODUCTS WHEN THE BOOT IS OVERHEATED.

In plain language (FlightFinder summary)

The Federal Aviation Administration is asked to review the design of Ratier-Figeac Model 146 propellers for compatible composition of the deicing boot, its adhesive material, and the propeller blade material when exposed to excessive heat. If corrosive byproducts are produced by excessive heat, the FAA must require modification of the boot to eliminate those byproducts.

This plain-language summary is written by FlightFinder to explain the recommendation above. It is not the official wording — the verbatim NTSB text is quoted above.

Details

StatusClosed - Acceptable Action
ModeAviation
ClosedApr 23, 1985
NTSB numberNYC82IA051
AddresseesFAA

External links

NTSB safety recommendations are advisory; addressees are not legally required to adopt them. Source: NTSB CAROL (public domain).