| AD Number | 46-21-01 | Status | Active |
| Effective Date | Not specified | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | N/A |
| Product Type | ["Aircraft"] | Product Subtype | ["Small Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Fairchild Industries, Inc. |
| Model(s) | 24 C8 24 C8A 24 C8B 24 C8D 24 C8DS 24 C8E 24 C8ES 24 C8F (Army UC-61J) 24 C8FS 24G (Army UC-61H) 24GS 24H 24HS 24J (Army UC-61B) 24JS 24K (Army UC-61E) 24KS |
46-21-01 FAIRCHILD: (Was Mandatory Note 6 of AD-702-2: 2 of AD-706-1; 4 of AD- 517-2; 5 of AD-535-2; 4 of AD-564-2; 5 of AD-633-2; 5 of AD-600-2; 4 of AD-667-2.) Applies to Model 24 Series Aircraft.
Compliance required at next periodic inspection.
To correct the freezing of the upper and lower universal joints on the landing gear oleo shock struts, install new universal joints, Fairchild P/N 3330 and 3328.
(Fairchild Service Bulletin 46-24-1-A, revised December 23, 1946, covers this same subject.)