- Effective
- January 21, 1980
- Models
- 2150, 2150A
- Data sheet
- TCDS4A19
- Registered aircraft
- 109 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-3664
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
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|---|---|---|---|
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On this page
The airworthiness directive
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.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 109
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1958 | 1 |
|---|---|
| 1959 | 2 |
| 1961 | 11 |
| 1962 | 5 |
| 1974 | 1 |
| 1975 | 3 |
| 1976 | 6 |
| 1977 | 13 |
| 1978 | 15 |
| 1979 | 20 |
| 1980 | 4 |
| 1982 | 1 |
| 1985 | 1 |
26 with no year recorded