HBOOK - ARTE - rev0

05-25-00 LIGHTING SYSTEM 33/45/03/000/000/030 Sea rchl i ght SPECTROLAB SX16. - Peri odi c 100FH AMM 33-45-03, 6-1 2 OP N REPETI D O05-22-01 Ch e ck . 33-45-03, 5-1 1 OP V 33/45/03/000/000/02005-22-01 LIGHTING SYSTEM 33/45/03/000/000/040 Sea rchl i ght GVI - Peri odi c 600FH AMM 1 OP V05-22-01 33-45-96 1 OP V REPETI D O05-22-00 LIGHTING SYSTEM 33/45/03/000/000/050 Sea rchl i ght - Fa n/Brus hes SPECTROLAB SX16. - Peri odi c 600FH CMM 33-45-96 4X V 47/50/10/000/000/00005-22-00 Equi pment tes t. 34-00-00, 6-1 0,5 X V05-21-02 LIGHTING SYSTEM 33/45/03/000/000/060 Sea rchl i ght - Juncti on box - Peri odi c 600FH CMM 34-20-00, 5-1 4X V NAVI GATI ON FT 24-33-00, 5-205-25-00 NAVI GATI ON 34/00/00/000/000/000 Na vi ga ti on s ys tem SPECTROLAB SX16. - Peri odi c 600FH//24M AMM 47-50-10, 3-2 NAVI GATI ON Ch e ck . 47-50-10, 3-1 DI SPECTROLAB SX16. Ch e ck . DI Ch e ck . DI Pi l ot's a nd copi l ot's Tes t. - Peri odi c 600FH//24M AMM 34/21/00/000/000/000 gyros copi c a nd di recti ona l FT hori zon 34/25/00/000/000/010 Sta nd-by hori zon - Sta nd-by Check a nd cha rge the EE0033 704A46140000 - Peri odi c 12M AMM ba ttery ba ttery. EE0033A 704A46140000 - Peri odi c 2M AMM FT - Peri odi c 1M AMM WEAPONS ELECTRONICS 47/50/10/000/000/000 Flir 1,5 OP V Sta r SAFIRE II.05-25-00 WEAPONS ELECTRONICS 47/50/10/000/000/020 Flir Bl eedi ng a nd ni trogen 1 OP N fi l l i ng of the turret. SVC Sta r SAFIRE II. Turret des i cca nt ca rtri dge ch e ck . VC 040-10504 704A41512003 Vi s ua l check of the 040-10505 704A41512004 sliding window.04-20-00 DOORS 52/10/00/000/000/000 Sta nda rd door GVI 040-11099-990 704A41512025 CHK Peri odi c 100FH AMM 56-11-00, 6-1 0,5 X V05-22-00 355A25-2030-00 -05-22-0005-22-00 M468AS100-25 704A4151200505-22-0005-22-00 M468AS100-26 704A4151200604-20-00 DOORS 52/10/00/501/000/000 Crew door Functi ona l tes t - Jetti s on. - Peri odi c 600FH//24M AMM 52-11-00, 5-1 1,5 X V DOORS FT 52-11-00, 6-1 1X V DOORS 52-31-00, 5-1 1X V DOORS Vi s ua l check wi thout 52-31-00, 6-1 1X V DOORS 52-12-00, 6-1 3,5 X V DOORS 52/10/00/601/000/000 Crew door remova l . - Peri odi c 600FH//24M AMM 56-11-00, 6-1 0,5 XA N GVI Functi ona l tes t - 52/30/00/000/000/010 La tera l ca rgo door Indi ca ti ng s ys tem. - Peri odi c 600FH//24M AMM FT Vi s ua l check wi thout 52/30/00/000/000/020 La tera l ca rgo door remova l . - Peri odi c 600FH//24M AMM 52/90/00/000/000/000 Sliding door 52/90/00/000/000/010 Sliding door GVI Deta i l ed check. - Peri odi c 600FH//24M AMM DI Vi s ua l check of the 35-0101L 704A41512010 CHK Peri odi c 100FH AMM REPETI D O sliding window. 35-0101R 704A41512011 52/90/00/000/000/000 GVI PRE MOD 073287 (LH door), PRE MOD 073290 (RH door).04-20-00 DOORS 52/90/00/000/000/015 Sliding door Checki ng the rol l er CHK Peri odi c 100FH AMM 52-12-00, 6-3 1X V di a meter a nd the front end opening dimension of the mi ddl e ra i l . DI Repl a cement of the05-22-00 DOORS 52/90/00/000/000/020 Sliding door rubber wa s her of the - Peri odi c 600FH//24M AMM 52-12-00, 4-3 3,5 X V05-25-00 FUSELAGE front upper rol l er. 12-30-00, 3-4 1 ATM V05-25-0005-25-00 DI05-25-00 53/00/00/000/000/000 Corros i on preventi ve bea d Tropi ca l a nd da mp Ch e ck . - Peri odi c 150FH//6M AMM a tmos phere SVC Ch e ck . After hoveri ng or l ow- FUSELAGE 53/00/00/000/000/010 Corros i on preventi ve bea d Sa l t-l a den a l ti tude fl i ght, thi s - Peri odi c 150FH//6M AMM 12-30-00, 3-4 1 ATM N REPETI D O AS350B2 / H125 a tmos phere opera ti on s houl d be 53/00/00/000/000/000 ca rri ed out duri ng the P Hbook 2016 – rev0 ch e ck . SVC FUSELAGE 53/00/00/000/000/020 Protecti on by s pra yi ng Tropi ca l a nd da mp SVC - Peri odi c 7D AMM 12-30-00, 3-4 0,5 ATM V FUSELAGE 53/00/00/000/000/030 Protecti on by s pra yi ng a tmos phere 12-30-00, 3-4 After hoveri ng or l ow- a l ti tude fl i ght, thi s Sa l t-l a den opera ti on s houl d be - Peri odi c 7D AMM 0,5 ATM N REPETI D O a tmos phere ca rri ed out duri ng the P 53/00/00/000/000/030 ch e ck . SVC Wa s hi ng the s tructure wi th fres h wa ter. After hoveri ng or l ow-05-25-00 FUSELAGE 53/00/00/000/000/040 Structure Sa l t-l a den a l ti tude fl i ght, thi s - Peri odi c 7D AMM 12-30-00, 3-1 2 ATM N REPETI D O a tmos phere opera ti on s houl d be 53/00/00/000/000/060 ca rri ed out duri ng the P ch e ck . CLN Tropi ca l a nd da mp a tmos phere05-25-00 FUSELAGE 53/00/00/000/000/050 Structure - Doors , fa i ri ngs , Sa l t-l a den Cl ea ni ng a nd grea s i ng. - Peri odi c 7D AMM 12-30-00, 3-4 0,5 ATM N panels a tmos phere CLN|LUB Sand-laden and/or









































Chapter Section ATA Title Task number Task Title MOD Climatic Condition Description MPN PN Maintenance Frequency Limit Ref Manual Documentation H/H CONDIÇÃO ROTEIRO OBS Subject Mode BFF AMM 05-40-00, 6-9 05-20-00 PRE MOD 075580 Sand-laden and/or dust- Note: Operations can be carried TA AMM TIME 05/21/00/604/000/ Check before the first flight of the PRE MOD 073453 laden atmosphere out by a crew member. - Periodic ALF AMM 0,5 X V 05-20-00 LIMITS/MAINTENANCE 000 day (BFF) - Optional equipments VC ALF AMM Sand-laden and/or dust- ALF AMM 05-20-00 CHECKS laden atmosphere Note: Operations can be carried 05-20-00 out by a crew member. 05-20-00 TIME 05/21/00/606/000/ Turnaround check (TA) - Optional VC - Periodic 05-40-00, 6-5 0,5 X V LIMITS/MAINTENANCE 000 equipments Note: Operations can be carried CHECKS out by a crew member. VC TIME 05/21/00/607/000/ Check after the last flight of the Visual check. - Periodic 05-40-00, 6-10 0,5 X V LIMITS/MAINTENANCE 000 day (ALF) - Optional equipments VC - Periodic 05-40-00, 6-6 0,25 AMS V Visual check of the - Periodic 05-40-00, 6-6 0,25 AMS V CHECKS attachments. VC TAIL ROTOR 64/10/00/000/000/ Tail rotor blade (ALF) Check for erosion. 070 In the event of intensive POWER PLANT 71/00/00/000/000/ Power plant air intake (ALF) operation in heavily sand-laden 010 areas, all the necessary05-20-01 ROTOR (S) 62/10/20/601/000/ Main rotor blade measures should be taken to - Periodic 10FH AMM 62-11-00, 6-3 0,7 ATM V 020 ensure optimum operation of the aircraft, if necessary, by05-20-01 TAIL ROTOR 64/10/00/000/000/ Tail rotor blade - Periodic 10FH AMM 64-10-00, 6-1 0,3 ATM V 220 shortening the suggested intervals. - Periodic05-20-02 TIME 05/21/00/000/000/ P-Check GVI - Periodic 10FH//7D AMM 05-40-00, 6-7 0,7 X V05-20-02 LIMITS/MAINTENANCE 000 P-check - Optional equipments Check for erosion. 10FH//7D AMM 05-40-00, 6-8 0,3 X V CHECKS In the event of intensive operation in heavily sand-laden 150FH//12M AMM 21-51-10, 6-1 1 OP V TIME 05/21/00/000/000/ areas, all the necessary 150FH//12M AMM 63-11-00, 6-18 1X V LIMITS/MAINTENANCE 010 measures should be taken to 150FH//12M AMM 63-11-00, 6-2 1X V ensure optimum operation of 150FH//12M AMM 63-11-00, 6-15 3 AMS V CHECKS the aircraft, if necessary, by 150FH//12M AMM 63-11-00, 6-3 0,5 AMS V shortening the suggested 150FH//12M AMM 63-11-00, 3-1 1 AMS V 150FH//12M AMM 65-11-00, 6-13 1 OP V intervals. AMM 73-20-00, 6-1 1,5 OP GVI 150FH AMM 25-21-00, 6-1 1,5 AMS 150FH AMM 29-10-00, 5-1 Note: Operations can be carried 1 AMS out by a crew member. 150FH AMM 53-10-00, 6-1 1 AMS GVI 150FH AMM 53-10-00, 6-2 1X 150FH AMM 53-31-00, 6-4 0,5 X Note: Operations can be carried 150FH AMM 55-20-00, 6-1 out by a crew member. 3X GVI 150FH AMM 62-11-00, 6-3 1X05-21-00 AIR CONDITIONING 21/51/20/000/000/ Freon air conditioning system Visual inspection of the system. - Periodic 150FH AMM 62-21-00, 6-1 2,5 X 025 GVI 150FH AMM 62-21-00, 6-2 1X 150FH AMM 62-32-00, 3-1 3 ATM05-21-00 ROTOR DRIVE (S) 63/10/00/000/000/ Flexible coupling Visual check. - Periodic 150FH AMM 62-33-00, 3-105-21-00 ROTOR DRIVE (S) 060 VC - Periodic05-21-00 ROTOR DRIVE (S) - Periodic 150FH AMM05-21-00 ROTOR DRIVE (S) 63/10/00/000/000/ Hydraulic pump Drive-belt and bearing check. - Periodic05-21-00 TAIL ROTOR DRIVE 065 VC - Periodic05-21-00 - Periodic05-21-01 63/10/00/000/000/ Hydraulic pump splines belt drive PRE MOD 079561 & PRE Greasing. - Periodic05-21-01 200 MOD 079566 LUB - Periodic05-21-01 63/10/00/000/000/ Hydraulic pump drive bearing POST MOD 079566 & PRE Greasing. - Periodic05-21-01 270 MOD 079568 LUB - Periodic05-21-01 - Periodic05-21-01 65/10/00/000/000/ Rubber sleeve POST MOD 079059 Visual check. - Periodic 200 VC05-21-01 - Periodic ENGINE INDICATING 77/00/00/601/000/ FADEC unit FADEC self-test.05-21-01 000 Engine ARRIEL 2B/2B1. - Periodic05-21-01 - Periodic05-21-01 EQUIPMENTS AND 25/10/11/000/000/ Pilot and copilot seats - Seat FT 350A77-0068- - - Periodic05-21-01 FURNISHINGS 000 buckets and attachments Visual check. 01 - Periodic05-21-01 HYDRAULIC POWER 29/10/10/501/000/ Single hydraulic generation POST MOD 073263 GVI - Periodic 000 system - Servocontrol Check of the electrical system part. DI FUSELAGE 53/10/00/000/000/ Transmission deck [PRE MOD 073362 // PRE Check. AS350B2 / H125 FUSELAGE 080 Longitudinal bulkheads MOD 073342] & POST CLN|GVI AMM 53-10-00, 8-14 Hbook 2016 – rev0 53/10/00/000/000/ Visual check. 120 PRE MOD 074349 GVI FUSELAGE 53/10/01/000/000/ Tail rotor drive shaft bearing Visual check of the bearing 000 bracket mounts bracket mounts. GVI STABILIZER 55/20/00/000/000/ Upper and lower fin Check of skin. 030 GVI ROTOR (S) 62/10/00/000/000/ Skin Check the skin in the area 005 between 900 mm and the blade ROTOR (S) 62/20/00/000/000/ Starflex star tip. ROTOR (S) 190 GVI ROTOR (S) Checking the central area. ROTOR (S) 62/20/00/000/000/ Starflex star - Bush and swivel GVI 195 bearing Visual check and radial play check. 62/30/00/000/000/ Swashplates DI 163 Greasing the bearing. LUB 62/30/00/000/000/ Scissors bushings and attachment Sand-laden and/or dust- Greasing. laden atmosphere LUB 320 bolts The sample must be taken during the inspection nearest to ROTOR DRIVE (S) 63/20/00/000/000/ Spectrometric Oil Analysis each due time. 60-00-00, 6-1 0,25 X 065 Program (SOAP) Oil monitoring using SOAP is optional.