| AD Number | 79-06-04 | Status | Active |
| Effective Date | March 26, 1979 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-3438 |
| Product Type | ["Aircraft"] | Product Subtype | ["Small Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Mooney Aviation Company Inc |
| Model(s) | M20F M20J |
79-06-04 MOONEY: Amendment 39-3438. Applies to models M20F and M20J, registration numbers:
N3207F
N201A
N9545M
N201WX
N201EU
N201MF
N201TN
N201MR
N201NW
N201WT
N201TS
N201KJ
HB-DWK
N201YD
N201YB
N201WE
N201JF
OE-DHM
N201TW
N201ND
N201MS
N201GJ
N201WM
N201MW
N201SE
Compliance is required within the next 25 hours of flight time after the effective date of this Airworthiness Directive (unless already accomplished).
To prevent elevator control lock, accomplish the following:
1. Inspect the pitch servo installation in accordance with Edo-Aire Mitchell Service Bulletin MB-14 dated 3/30/78 and assure servo stop bracket part number 7B1320 is installed and adjusted in accordance with SB MB-14, paragraph 5.
2. If servo stop bracket is not installed, accomplish the installation in accordance with Service Bulletin MB-14.
This amendment becomes effective March 26, 1979.