Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 170, 172, F172, FR172 and 175 Series Aeroplanes
AD/CESSNA 170/44 Limited Elevator Movement - Placard 9/81
Applicability: All model 172 RG with S/Nos 172 RG 0001 to 172 RG 0769.
Requirement: 1. Install a locally manufactured placard in clear view of the pilot, using letters at least 2.4 mm (3/32 inch) high, which reads:
"ELEVATOR MOVEMENT MAY BE LIMITED WHEN RIGHT RUDDER IS APPLIED IF THIS CONDITION IS ENCOUNTERED, CENTER THE RUDDER PEDALS, LAND AS SOON AS PRACTICAL AND COMPLY WITH AD/CESSNA 170/45 PRIOR TO FURTHER FLIGHT."
2. Remove placard after compliance with AD/CESSNA 170/45.
Note: FAA AD 81-14-06 Amdt 39-4158 and Cessna Single Engine Service Letter SE80-99 Rev 1 refer to this subject.
Compliance: Before further flight.
Background: In-service failure of the jack screw shaft of the rudder trim/nose gear steering bungee could limit elevator control system movement and for safety, the aircraft should land as soon as practicable after the pilot experiences elevator control limited movement.
We try to embed the page this law was scraped from. If the site blocks framing, you still get the link and a local excerpt.
Last checked with source on —
Checking whether the official page can be embedded…
Plain-English simplify of this law: a short summary, key points, and both sides of the argument. Generated on first view via Replicate, then cached. Vote on what helps your study.
No study brief is cached for this law yet. Sign up to generate a plain-English brief.
Sign up to generate