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
