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CHECK  CONTROLS  CLEARANCE
CHECK  CONTROLS  CLEARANCE (Continued)

TM-55-1520-240-23-9 CH-47D Heilcopter Manual
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TM  55-1520-240-23-9 11-5 CHECK CONTROLS  CLEARANCE (Continued) 11-5 SUBMINIMUM  CLEARANCE CHECK 2. Check  flight  control  system  for  subminimum clearances  as  follows: LOCATION PARTS  INVOLVED SUBMINIMUM ALLOWABLE CLEARANCE (INCH) STA 565.00 0.06 WL +100.00 Between MS27576-4-19 bolt  inboard end  and  114S4118 beam.  (Bolt in  aft clevis  of  145C2514 bellcrank.) BL 8.00LH STA 534.00 0.120 WL +63.00 Without   38    -  Between  145S3308  frame  doubler  clearance  hole and 145C2010-11 link  assembly. BL 7.00RH STA 534.00 0.120 WL +63.00 With   38   -  Between 145S3308 frame doubler clearance hole and 145CS340-3 link  assembly. BL 7.00RH STA 552.00 Between 114S4113-113 deck  angle and 145C2513-1 or  -3 bellcrank. 0.120 WL +71.00 BL 12.00RH STA 554.00 0.120 WL +90.00 Without  38  - Between 145S4112-6 & 114S4115-103 angles and 145C2010-12 link  assembly. BL 10.00LH STA 554.00 0.120 WL +90.00 With   38   -  Between 145S4112-6 &  114S4115-103 angles and 145CS340-5 link  assembly. BL 10.00LH STA 78.00 Between 114C1103-157 angle and 114C1168 or 414C1168 roll  bellcrank. 0.120 WL -20.00 BL 12.00LH STA 41.00 Between 114C1103-119 web and 114C1014-1 yaw links. 0.08 WL -22.00 BL 15  & 26RH BL 15  & 26LH STA 92.44 0.10 WL +59.28 Between bolt/nut  in fwd end of 145C3230 bellcrank and 145C1813-1 fitting. (Bolt head outboard.) BL 15.00LH STA 95.35 0.18 WL +55.25 Between  145C3231  bellcrank  and cylinder  barrel  of pivoting actuator 145H6600. BL 14.00RH STA 53.0 0.12 WL +25.0 Between 114C1160-1 thrust bellcrank and 114C1012-2 pitch rod assy. BL 13.5 STA 70.62 Between 114C1102-26 bracket and 114C1130-4 pitch horn. 0.120 WL -26.15 BL 20.00LH Cockpit Between 145C1306 cyclic  stick  and 114C1124 pedal adjustment lever. 0.06 (See Note 2) STA 61.38 0.06 WL -27.97 Between the 114C1014-2 roll  link  and 114C1103-77 angle of copilot control box  assembly. BL 18.25LH 11-13







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