| AD Number | 46-40-02 | 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) | 22 C7 22 C7A 22 C7AM 22 C7AS 22 C7B 22 C7D 22 C7E 22 C7F 22 C7G 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 |
46-40-02 FAIRCHILD: (Was Mandatory Note 2 of AD-667-2; 3 of AD-633-2; 3 of AD- 535-2; 3 of AD-564-2; 3 of AD-600-2.) Applicable to Models 22 and 24 Series Aircraft Serial Numbers 3300 to 3319, Inclusive, and 3350 to 3358, Inclusive, Except Seaplanes.
Compliance required at next 100-hour inspection.
Unless previously accomplished, reinforce the oleo tubes at the piston end by installing sleeve. Fairchild part SK-1636. Sleeve may be attached by using two AN 435-5-4 rivets or by welding through four 5/16-inch holes drilled in the piston tube. All damaged parts should be replaced. Fairchild Service Bulletin 40-5, revised July 3, 1945, and 44-6-C dated May 8, 1944, cover this same subject.)