AD/R22/29 - Main Rotor Pitch Link

1. Prior to next flight after 16 June 1987, and each flight thereafter until Part B is accomplished.

Note 1. If cracks are found, perform Part B of RHC S.B. No. 57 prior to any further flight.

Note 2. This inspection may be accomplished by the pilot in command in which case he shall enter and certify for this A.D. in col. 2 part 3 of the Maintenance Release on each occasion.

2. Within the next 10 flight hours or by 15 July 1987 whichever occurs first.