AD/PA-38/12 - Additional Flow Strip Installation
1AD/PA-38/12 - Additional Flow Strip Installation
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Piper PA-38 (Tomahawk) Series Aeroplanes
AD/PA-38/12 Additional Flow Strip Installation 8/79
Applicability: Model PA-38-112 aircraft with S/Nos. 38-78A0001 through 38-79A0582.
Requirement: 1. Install additional flow strips and modify or replace the airspeed indicator in accordance with Piper SL No. 876.
- An approved amendment must be introduced to the aircraft flight manual before further flight following incorporation of SL No. 876, to reflect the increased stall speeds, take-off and landing safety speeds and distances which result from the modification.
Compliance: Within 100 hours time in service after 30 September 1979.
Background: The flow strip installation is to improve the handling character- istics of the aircraft during stall manoeuvres.