2. The control arm must be connected between the stabilator trim tab horns and the trim I. adjustment mechanism. PIPER COMA~CHE SERVICE MA~L-\L ~. Add \\eight links P 'R 1262 and or 21564 as necessary or decrease weight bydrilling balance weight in designated arca. IRefer to Figure 4- ia. I -t Check the stabilator throughout its complete travel urailing edge up. down. center. ctc.r: II should not move from any position it is placed in when properly balanced. d. IPA-::!~-~O()I After complying with steps (altb) and both the ~OTE and CAl'TIO' proceed a, fo II (\\\ s: I. Disconnect the tab control arm from the tab horn . ., Align the tab and stabilator trailing edges.
l 'se a small piece of tape to hold tab in place. 'OTE vlaximurn acceptable tab trailing edge misalignment is .129 of an inch. ~. Place a master check weight. P '\ ]~541 (] Ibs. 13.2507.) on top of the stabila ror balance weight with the check weight tab facing aft. (Refer to Figure 4-7a.) 4. Balance the -tabilaror by installing balance "eight plates. P '\ 2~179 until it i, completely balanced. The stabilator should not move from any position (trailing edge up. down. center. crc.i it j, placed in \\ hen properly balanced. 5. E\ enIy distribute weights on both sides of the arm: remove master check weight and connect controls. e. (P .-\-24-::!50 and 260 \\ ith sta bilator tip \\ eights I I.
I ('\1:1 the aircraft and set the trim tab in neutral position. .., The control arm must he connected between the stabilator trim tab horns and the trim tuh adjustment mechanism. ~. Add weight links, P , HI262 and or 215M as necessary or decrease weight by drilling t balance weight in the designated area. (Refer to Figure 4-7a.) 4. Check the stabilator throughout its complete travel (trailing edge up. down. center. ctc.): it should not move from any po, ition it is placed in when properly balanced. - ITAal&.ATOlt ~ IU,""ltT ITA"O ~~ ~ DIAL. .MDICATelt - FIGl'RE 4-7b. CHECKI'\G STABILATOR FREE PLAY RE\'ISED: ... /10/81 IF2