| AD Number | 50-47-02 | 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) | Superior Aircraft Company |
| Model(s) | V V-2 |
50-47-02 CULVER: Applies to All Models V and V2 Aircraft Equipped With Sensenich Models C2FB3 or C2FB1 Propeller With C276A2, PC276A6, PC276A7 and C276A6 Blades.
Compliance required as indicated.
(1) Replacement required prior to January 31, 1951.
In order to eliminate the continued occurrence of broken blade lag screws and/or cracked blade shanks and ferrules, all C276A2 blades must be retired from service and replaced with blade Model PC276A6, PC276A7 or C276A6.
(2) Inspection required every 500 hours of operation after installation of blade Models PC276A6, PC276A7 and C276A6.
The propeller blades should be removed from the hub, and the wood blade shank and the split retaining ring groove in the blade ferrule should be carefully inspected for cracks. The lag screws should be check-tightened to 160 inch-pounds torque. Blade with broken lag screws or cracked wood shank or ferrule must be removed from service. The ferrule and all ferrous metallic parts of the hubshould be magnetically inspected.
The blades are subjected to excessive vibratory stresses when operation beyond the allowable engine r.p.m. ratings inadvertently occurs. It is recommended, therefore, that the accuracy of the tachometer be checked in order to preclude such operation. Operation between 1,800-2,000 r.p.m. is to be avoided when the nose landing gear is extended.
(Sensenich Service Bulletins Nos. 133, 134 and 135 cover these same subjects.)
This supersedes AD 47-47-09.