CTHRepealedLegislation
AD/MU-2/65 - Engine Torque Indication System
For MU-2B-25, -26, -35 and -36 aeroplaneFor MU-2B-25, -26, -35 and -36 aeroplanes:
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For MU-2B-25, -26, -35 and -36 aeroplanes:
Inspect the torquemeter in accordance with MHI SB No 233 dated 7 October 1998.
2. If, during the Requirement 1 inspection, the errors in the torque indication system are found to exceed the allowable limit specified in the SB, repair or replace the torquemeter in accordance with the SB.
3. Inspect the torque transducer in accordance with the SB.
4. If, during the Requirement 3 inspection, the torque transducer output voltage is found to exceed the allowable limit specified in the SB, adjust the torque transducer output voltage in accordance with the SB.
5. Accomplish a ground check of the engines in accordance with the SB.
Note: JCAB AD TCD-4889-98 refers.