AD 80-02-08

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AD Number:
80-02-08
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; VARGA AIRCRAFT CORPORATION Model 2150 and 2150A Series Airplanes
Subject:
Rudder Balance Attach Bolts
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/21/1980
Make:
Augustair, Inc.
Model:
2150 | 2150A
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 80-02-08
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3664

AD NUMBER:   80-02-08

SUBJECT HEADING:   Airworthiness Directives; VARGA AIRCRAFT CORPORATION Model 2150 and 2150A Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective January 21, 1980.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
80-02-08 VARGA AIRCRAFT CORPORATION (Morrisey): Amendment 39-3664. Applies to Varga Model 2150 and 2150A series airplanes certificated in all categories. Compliance required within the next ten (10) hours' time in service from the effective date of this AD, unless already accomplished. To prevent jamming of the rudder cables on the rudder balance weight attach bolts, accomplish the following:

(a) Remove the two bolts attaching the rudder balance weight to the static balance arm and reinstall these bolts head downward, as shown in Figure 1 of this AD.



(b) Alternative inspections, modifications or other actions which provide an equivalent level of safety may be used when approved by the Chief, Aircraft Engineering Division, FAA Western Region.


This amendment becomes effective January 21, 1980.

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