Garmin G3X - Page 189

190-01115-01 G3X™/G3X Touch™ Avionics Installation Manual
Rev. AV Page 16-29
Figure 16-10.1 GSA 28 RV-4/8 Pitch Mounting Kit 011-02952-11 (page 1 of 4)
4-VRNOITPIRCSEDYTQN/P NIMRAGMETI & PRE-SEPT 2006 RV-8 POST-SEPT 2006 RV-8
XXTUN KCOL A2301-563NA430-71100-0121
XXREHSAW 01-069NA0101-53000-212
2
XXTLOB A7-3NA150-09000-1123
XXTFEL ,TEKCARB HCTIP 8/4-VR130-45810-5114
XXTLOB A11-3NA170-09000-1125
6
XGNL 57.x573.x291. ,RECAPS130-39000-312
XGNL 578.X573.X291. ,RECAPS140-39000-312
7
XTLOB
A5-3NA110-09000-1
12
XTLOB A6-3NA160-09000-112
X
XREHSAW 3-07
9NA230-08000-2128
XXTHGIR ,TEKCARB HCTIP 8/4-VR140-45810-5119
10
X
A41-3NA18
0-09000-112
XTLOB A51-3NA190-09000-112
X5 ETON EESA51-4NA131-09000-11211
XXGNIRAEB DNE DOR ELAM220-91000-28321 XXTUJ MAJ R3-513NA230-61100-01231
XXDEPPAT ,G
NL "52.2 ,AID 8/3 ,DOR HSUP100-24500-71141
XXREHSAW )NIHT( L01-069NA101-34000-21251
2
SEE NOTE 6
8.
SEE NOTE 4
2
SEE DETAIL A
3
11
8
2
5
2
4
6
7
2
9
2
1
10
1
SEE NOTE 3
ALUMINUM PUSH ROD (ITEM 14) MUST NOT BE LESS THAN 0.375". THREAD ENGAGEMENT BETWEEN ROD END BEARINGS (ITEM 12) AND
9.
2
2
NOTES:
DIMENSIONS: INCHES.1. DIMENSIONS ARE NOMINAL AND TOLERANCES ARE NOT IMPLIED UNLESS 2. SPECIFICALLY STATED. HOLE MUST BE DRILLED THROUGH BELL CRANK TO ATTACH PUSH ROD. 3. SEE SHEET 2 FOR HOLE SIZE AND LOCATION.
SINGLE AN960-10 WASHER (ITEM 2) MUST BE PLACED IN-BETWEEN BELL 4.
CRANK HALVES CONCENTRIC WITH DRILLED HOLES. AN4-15A BOLT PROVIDED IS TO BE USED WITH POST-SEPT 2006 RV-8 5. ONLY. FOR RV-4 AND PRE-SEPT 2006 RV-8, USE BOLT PROVIDED WITH
AIRFRAME KIT. NUT AND WASHERS FOR AN4 BOLT ARE NOT PROVIDED IN GSA28 MOUNTING 6.
KIT. USE PARTS PROVIDED WITH AIRFRAME KIT. TIGHTEN PER AIRFRAME MANUFACTURER'S SPECIFICATION. NOTE HAS BEEN REMOVED.
7.
NOTE HAS BEEN REMOVED.
SEE NOTE 6
15
3.69
SEE SHEET 2, NOTE 1
(.530)
SEE NOTE 9
(.530)
SEE NOTE 9
14 12
13
12
13
DETAIL A