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05/19/2008 07:10 8708862489 AMERICAN AGVIATION PAGE 02/02
ERUMMAN AMERICAN AVIATION SERVICE
CORPORATION FO BOX 2206 SAVANNAN GEORGIA 31402 (8121864 - 3000 TELEX NO. 54-6470 AG-CAT SERVICE BULLETIN #61 DATE: JUNE 6, 1977 SUBJECT: RUDDER TUBE CORROSION APPLICABILITY: G-164 - S/N 1 through 400 G-164A - S/N 401 through 1674 G-164B - S/N 1B through 79B Field reports indicate that excessive corrosion may occur on the main tubular spar (P/N A1203-11) of the rudder assembly. It is therefore recommended that, upon receipt of this Bulletin, the following be accomplished.
(1) Remove the rudder assembly from the aircraft.
(2) Remove the bellcrank assembly from the A1203-33 rudder fitting.
(3) Drill a .50 dia (¿") hole through the bottom of the A1203-33 fitting and inspect the interior and exterior of the main tube for corrosion.
(4) If no signs of corrosion are noted, fill the tube with linseed oil and drain. Plug the .50 dia (¿") hole with Scotch caulking compound and reinstall the rudder bellcrank to the 1203-33 fitting.
(5) If corrosion is noted, determine the extent of the corrosion and repair accordingly.
(6) If a repair is required, repairy with Step #4 above after completion of the Drill. 50 dia (¿") hole 25 A1203-33 A1203-33 © GRUMMAN AMERICAN AVIATION CORPORATION 1977