A-99-038

NTSB Safety Recommendation — Aviation

Recommendation text

THE NTSB RECOMMENDS THAT THE FAA: ISSUE AN AIRWORTHINESS DIRECTIVE REQUIRING, IN ACCORDANCE WITH PROCEDURES DEVELOPED BY CESSNA AIRCRAFT COMPANY, (1) REPETITIVE INSPECTION FOR CRACKING IN THE CORNER BETWEEN THE TWO INNER DIAMETER PORTIONS OF THE MAIN LANDING GEAR ACTUATOR HOUSINGS (P/N 1281001-3) USED IN THE MAIN LANDING GEAR SYSTEMS OF CESSNA MODELS 172RG AND 182RG AIRPLANES UNTIL ANY GRINDING OR FILING MARKS HAVE BEEN REMOVED AND THE COMPONENT HAS BEEN FOUND TO BE CRACK-FREE; AND (2) THE REMOVAL OF GRINDING OR FILING MARKS FROM THIS SAME AREA.

In plain language (FlightFinder summary)

The FAA is asked to issue an airworthiness directive requiring repetitive inspections for cracks in the main landing gear actuator housings (part number 1281001-3) on Cessna Models 172RG and 182RG until any grinding or filing marks are removed and the part is found crack-free, and to require removal of those marks.

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 Alternate Action
ModeAviation
ClosedJul 16, 2002
NTSB numberMIA98SA252
AddresseesFAA

External links

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