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1. FUJI HEAVY INDUSTR ES LTD HEAD OFFICE SUBARU BLDG SHINJUKU TOKYO JAPAN NO 200 007 DATE September 30 1987 SUPERSEDES NO REV DATE SUPERSEDES NO The Partial Revision for FA 200 Service Manual and Paris Catalogue Part 2 Since FA 200 MAIN WHEEL ASSY was added FA 200 Service Manual and Parts Catalogue has been modified so we will inform you of the modified contents We attached Service Manual and Parts Catalogue separately Please use them according to the following attached documents l Service Manual No Attached Service Manual Page 1 200 O10003A ee PAGE 3 6 2 200 0100153 vr tr ret PAGE 7 10 2 Parts Catalogue No Attached Parts Catalogue Page 200 0000 Pero wra PAGE 11 12 4 19 4 20 A E ea PAGE 13 14 4 19 4 20 AEROSPACE COMPANY SERVICE NEWS 200 007 1 11 YOUNAN 1 CHOME UTSUNOMIYA TOCHIGI JAPAN PAGE 1 OF 14 320 8564 TEL 028 684 7283 FAX 028 684 7260 BLANK SERVICE NEWS 200 007 PAGE 2 OF 14 FUJI FA 200 SERVICE MANUAL account 5 Install and tighten the wheel attaching bolts as follows a 9532522 wheel Position countersunk washer under bolt with countersink toward bolt head Then insert the bolt with bolt head inboard Install nut and one plain washer on the bolt First tighten three nuts to 30 in Ibs torque Next tighten them to 60 in lbs torque and then tighten them to 83 in lbs torque b 9532522 1 wheel After applying antiseize compound MIL T 55442. The wheel landing gear struct cover and fairing to be removed per applicable instructions 1 With the air valve cap 11 removed discharge air completely from the core 12 2 Remove the air valve body 13 from the plug 16 3 With the snap ring 15 removed remove the stopper 19 plug and 0 ring 17 4 Pull out the orifice tube 18 5 Drain oil 6 Remove the torque knee 28 7 With the bolt 32 removed disconnect the piston 25 from the socket 26 8 Pull out the piston from the upper end of the cylinder 9 With the snap ring 24 of the cylinder skirt section removed remove the adapter 23 and scraper ring 22 10 Remove the O ring 20 and oil pad 33 from inside the cylinder 9 3 11 ASSEMBLING OF MAIN GEAR SHOCK STRUT 1 After cleaning all parts properly check them for wear and damage Replace defective parts Replace 0 rings with new ones 2 Install O ring and oil pad inside the cylinder 3 Install the scraper ring and adapter on the cylinder skirt with the snap ring 4 Insert the piston from the upper side of the cylinder 5 Install the piston and socket with bolts Tighten bolts to 30 to 40 in lbs 6 Install the torque knee 7 Install the orifice tube 8 Lubricate the strut in accordance with para 3 2 2 9 Install the O ring stopper and plug with the snap ring 10 Install the 0 ring and valve body on the plug 11 Charge
3. GEAR USABLE ON CODE 1 W gt W gt W gt N WD m Y ISSUED SEPTEMBER 1987 FIGURE 14 WHEEL ASSEMBLY MAIN LADING GEAR USE WITH TUBE TYPE TIRE 4 19 SERVICE NEWS 200 007 PAGE 13 OF 14 FIG 8 INDEX NO 14 1 i Q NG gt t DOR 4 20 SERVICE NEWS 9532522 9532522 1 9524218 13889 22FH 428 42F LLW 428 MS20002 4 NAS144 23 MS20002C4 9525391 5008252 9525392 5008253 9524201 13830 MS20426DD6 6 9525059 9524318 13830 x AN504 8R8 9524491 9524877 9524876 9524875 9524858 AN520 10 10 NAS679A3W PAGE 14 OF 14 200 007 DESCRIPTION 1234567 WHEEL ASSY MAIN LANDING GEAR U S G Y WHEEL ASSY MAIN LANDING GEAR nennen SEAL BEARING EEE NER E CONE BEARING sevsesnvavvansanernnnsasnnnnanssnranssneansvnnvennens NUT SELF LOCKING see AT NUT SELF LOCKING see ee ewa aneen sanane ooo 0000 MASA au pana EE WASHER COUNTERSUNK ccrcecsaresevsensevcnsrssenes NR PLATE DATA ADHESIVE INBOARD eroine PLATE DATA ADHESIVE INBOARD rennen PLATE DATA ADHESIVE OUTBOARD esenzioni PLATE DATA ADHESIVE OUTBOARD ceo WHEEL SUBASSEMBLY INBOARD 10a00nennnnerneseeen a BEARING vw lilla aaa ao DE RIVET 0a00ererrv0erneenner EP nenne pyernavnaranennnennnnnnes CLIP DISC PATTY G mme ee WHEEL SUBASSEMBLY OUTBOARD OZ CUP BEARING serer enea ra aan aaa no won aaa owa areo SCREW e 0r0000
4. 0 10 10 NAS679A3W 4 20 SERVICE NEWS PAGE 12 OF 14 200 007 AP dr eg S gt E E E EL DESCRIPTION 1234567 WHEEL ASSY MAIN LANDING GEAR sia U S G Y WHEEL ASSY MAIN LANDING GEAR renne SEAL BEARING eresie aaa CONE BEARING serer ea aaa aaa nana NUT SELF LOCKING see TAT NUT SELF LOCKING seenen ri reina cere reeee size nio nizero WASHER ENE YTEW WASHER COUNTERSUNE ant PLATE DATA ADHESIVE INBOARD crono PLATE DATA ADHESIVE INBOARD ernennen PLATE DATA ADHESIVE OUTBOARD e PLATE DATA ADHESIVE OUTBOARD e WHEEL SUBASSEMBLY INBOARD nennen versene CUP BEARING ervsneenvevaserennrenneannannenenerensvesersvnsesee RIVET s0srersrsvnesnssnnnasseres ail ii erre CLIP DISC eee cea Gad WHEEL SUBASSEMBLY OUTBOARD rm CUP BEARING eee eee eee ea a a ana aaa aaa aa a wsio laine CLIP VALVE sseenvsarenannanenesaversavesnvernvanenennesneasnseensne VAL gt KIT WHEEL BALANCE WEIGHT erre ORDER SEPARATELY CLIP BALANCE WEIGHT DISG 0rrererrsereassaneereraree DISC BALANCE WEIGHT rveserrersannensennnanssere RED WEIGHT LEAD BALANCE erereesensareannnssanvesnrnnvenres SCREW BALANCE WEIGHT seresververse ea NUT BALANCE WEIGHT cere ie ei eo en izonionneoeo NOT ILLUSTRATED emi FOR 9532522 WHEEL ASSY Bossarrorsznenas FOR 9532522 1 WHEEL ASSY M MM I A pnt pe pe k M Y W W WW NI NI tri a WHEEL ASSEMBLY MAIN LANDING
5. air in accordance with para 3 2 12 and install the valve cap 9 4 NOSE LANDING GEAR SEE FIG 9 6 9 4 1 REMOVAL AND INSTALLATION OF NOSE LANDING GEAR 1 Remove the upper engine cowling 2 Lift the nose gear off the ground either by a lifting the forward fuselage using the engine hoist ring or b jacking up the airplane per para 2 2 ISSUED SEPTEMBER 1987 9 7 SERVICE NEWS 200 007 PAGE 9 OF 14 FUJI FA 200 SERVICE MANUAL p A Cap Valve core Body a ring Snap ring Plug 0 ring Stopper Orifice tude 0 ring Oil pad Cylindef Adapter Scraper ring Snap ring Piston Torque link Torque link Pin pin Cotter pin Bolt Spacer Washer Nut Bushing Socket Bolt Spacer el e i OANA OD 28 29 FIG 9 5 MAIN GEAR SHOCK STRUT AND TORQUE LINK 9 8 SERVICE NEWS 200 007 PAGE 10 OF 14 ISSUED NOVEMBER 1970 FIGURE 14 WHEEL ASSEMBLY MAIN LADING GEAR USE WITH TUBE TYPE TIRE SERVICE NEWS PAGE 11 OF 14 200 007 SECTION Y LANDING GEAR GROUP FIG amp INDEX NO 14 9532522 9532522 1 9524218 13889 22FH 428 I 42FLW 428 MS20002 4 NAS144 23 MS20002C4 9525391 5008252 9525392 5008253 7 9524201 8 13830 9 MS20426DD6 6 10 9525059 11 9524318 12 13830 AN504 8R8 9524491 sk 9524877 W NN l O Oi a 9524876 9024870 9524858 AN52
6. enesrnsnevansereradsersvennvnannevnnnenunnsudsenneereneree CL P VALVE eevoennvavsanrenanssasessavenesnreensenersursnaresasners KR KIT WHEEL BALANCE WEIGHT een ORDER SEPARATELY CLIP BALANCE WEIGHT DISC runs DISC BALANCE WEIGHT cecororocensnncensancannoneonnccnecanos WEIGHT LEAD BALANCE nun SCREW BALANCE WEIGHT rennen era nenn NUT BALANCE WEIGHT r rerrevsersevssvevnnsvnvsnsrenerarne NOT ILLUSTRATED deck FOR 9532522 WHEEL ASSY Bresrearaseserns FOR 9532522 1 WHEEL ASSY USABLE ON CODE 1 A 1 B 3 2 3 A 3 B 3 3 3 1 A 1 B 1 A 1 B 1 1 3 3 1 I 1 1 o 3 1 2 2 2 ISSUED SEPTEMBER 1987
7. lt Spacer Washer Nut Bushing Socket Bolt Spacer ww SARNPapPr FIG 9 5 MAIN GEAR SHOCK STRUT AND TORQUE LINK 9 8 SERVICE NEWS 200 007 PAGE 6 OF 14 ISSUED APRIL 1972 FUJI FA 200 SERVICE MANUAL account 5 Install and tighten the wheel attaching bolts as follows a 9532522 wheel Position countersunk washer under bolt with countersink toward bolt head Then insert the bolt with bolt head inboard Install nut and one plain washer on the bolt First tighten three nuts to 30 in lbs torque Next tighten them to 60 in lbs torque and then tighten them to 83 in lbs torque b 9532522 1 wheel After applying antiseize compound MIL T 5544 to thread part of bolt contact area of bolt head and washer self locking nut countersunk washer and plain washer install and tighten the nut by the same procedures as 9532522 wheel CAUTION When installing 42FLW 428 nut on 9532522 wheel refer to proper bolt tightening procedure for 9532522 1 wheel ISSUED SEPTEMBER 1987 9 6A SERVICE NEWS 200 007 PAGE 7 OF 14 BLANK SERVICE NEWS 200 007 PAGE 8 OF 14 FUJI FA 200 SERVICE MANUAL 6 Eliminate the wrinkles of the tube by inflating and deflating it After setting it to the tire rim inflate the tire to the specified air pressure 9 3 10 DISASSEMBLING OF MAIN GEAR SHOCK STRUT SEE FIG 9 5 The following procedures are applicable to the shock struts removed from the airplane
8. ng 20 and oil pad 33 from inside the cylinder 9 3 11 ASSEMBLING OF MAIN GEAR SHOCK STRUT 1 After cleaning all parts properly check them for wear and damage Replace defective parts Replace O rings with new ones 2 Install O ring and oil pad inside the cylinder 3 Install the scraper ring and adapter on the cylinder skirt with the snap ring 4 Insert the piston from the upper side of the cylinder 5 Install the piston and socket with bolts Tighten the bolts to 270 300 in lb 6 Install the torque knee 7 Install the orifice tube 8 Lubricate the strut in accordance with para 3 2 2 9 Install the 0 ring stopper and plug with the snap ring 10 Install the O ring and valve body on the plug 11 Charge air in accordance with para 3 2 12 and install the valve cap 9 4 NOSE LANDING GEAR SEE FIG 9 6 9 4 1 REMOVAL AND INSTALLATION OF NOSE LANDING GEAR 1 Remove the upper engine cowling 2 Lift the nose gear off the ground either by a lifting the forward fuselage using the engine hoist ring or b jacking up the airplane per para 2 2 ISSUED SEPTEMBER 1987 9 1 SERVICE NEWS 200 007 PAGE 5 OF 14 FUJI FA 200 SERVICE MANUAL Cap Valve core Body O ring Snap ring Plug O ring Stopper Orifice tude O ring Oil pad Cylinder Adapter Scraper ring Snap ring Piston Torque link Torgue link Pin pin Cotter pin Bo
9. to thread part of bolt contact area of bolt head and washer self locking nut countersunk washer and plain washer install and tighten the nut by the same procedures as 9532522 wheel CAUTION When installing 42FLW 428 nut on 9532522 wheel refer to proper bolt tightening procedure for 9532522 1 wheel ISSUED SEPTEMBER 1987 9 6A SERVICE NEWS 200 007 PAGE 3 OF 14 BLANK SERVICE NEWS 200 007 PAGE 4 OF 14 FUJI FA 200 SERVICE MANUAL 6 Eliminate the wrinkles of the tube by inflating and deflating 1t After setting it to the tire rim inflate the tire to the specified air pressure 9 3 10 DISASSEMBLING OF MAIN GEAR SHOCK STRUT SEE FIG 9 5 The following procedures are applicable to the shock struts removed from the airplane The wheel landing gear struct cover and fairing to be removed per applicable instructions 1 With the air valve cap 11 removed discharge air completely from the core 12 2 Remove the air valve body 13 from the plug 16 3 With the snap ring 15 removed remove the stopper 19 plug and 0 ring 17 4 Pull out the orifice tube 18 5 Drain oil 6 Remove the torque knee 28 7 With the bolt 32 removed disconnect the piston 25 from the socket 26 8 Pull out the piston from the upper end of the cylinder 9 With the snap ring 24 of the cylinder skirt section removed remove the adapter 23 and scraper ring 22 10 Remove the O ri
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