AD/SD3-60/22 Amdt 1 - Horizontal Stabilizer Spar Webs

Aircraft referenced in Part A which have only used a 15 degree take-off flap configuration during their first 5000 flights may utilize the Part B compliance.

Part B: For aircraft with S/Nos SH 3680 through SH 3691 and SH 3694; at the next scheduled inspection for Maintenance Release issue after 31 December 1987, and thereafter at intervals not exceeding 1500 flights, until modified in accordance with Shorts SB SD360-55-12 Rev 2.