TIME 00 LFS Compass Swing Stand By iaw LFS 1980:5 8 (BCL-M 4.3) 496, : , :5 LFS 1980:5 4-7 (BCL-M 4.3) , ,00 02

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1 AS350B3e (H125) MAINTENANCE PROGRAM AIRFRAME INSPECTION PROGRAM AC Serial number 8242 AC Total time 1, HRS at date SE-JRU TASK TASK LAST INSPECTION ATA REF REQUIREMENT DESCRIPTION TYPE INTERVAL TIME DATE TIME DATE TIME DYS LFS Compass Swing Stand By iaw LFS 1980:5 8 (BCL-M 4.3) CHK 730 DYS HRS 16-mar mar , :5 8 DUE AT REMAINING LFS Pitot Static System - Check - Altimeter and Airspeed Indicator check iaw CHK 730 DYS HRS 16-mar mar , :5 LFS 1980:5 4-7 (BCL-M 4.3) /CAME/ Airworthiness Review - Perform Annual Airworthiness Review Extension CHK 365 DYS HRS 31-maj maj , /CAME/ Airworthiness Review - Renewal CHK 1095 DYS 16. HRS 31-maj maj , /05/0 1FH /150FH Inspection (MSM / /05-25-) CHK 1 HRS HRS 04-okt-18 /0/ 1 648,60 19, 05 05/06/0 12M Inspection (MSM ) CHK 365 DYS HRS 10-maj maj , 186 /0/

2 05 05/08/0 6FH / 24M INSPECTION (MSM /-01 /-02) CHK 6 HRS HRS 15-jul-18 /0/ 1 862, 233, 05 05/08/0 6FH / 24M INSPECTION (MSM /-01 /-02) CHK 730 DYS HRS 15-jul jul , 617 /0/ 05 05/09/0 12FH / 48M Inspection (MSM / -01 / -02) CHK 12 HRS HRS 15-jul-18 /0/ 2 462, 833, 05 05/09/0 12FH / 48M Inspection (MSM / -01 / -02) CHK 1460 DYS HRS 15-jul jul , 1347 /0/ 05 05/10/0 MAJOR INSPECTION 144 M (MSM ) CHK 4380 DYS 0. HRS 16-maj maj , 3477 /0/ 08 08/EU Aircraft Weighing CHK 1460 DYS 11-maj , 553 OPS-CAT 25 AS350 Emergency floatation gear - Check of the front and rear attachment CHK 390 DYS HRS 10-maj jun , 211 SB- brackets - Comply with paragraph 3. (except paragraph 3.B.2.a.) /10/11/ MSM : Front seats with shock absorbers - Rails. SICMA 159. CHK 18 HRS 1 8, 171, 0/0/0 Check. DI. (Ref AMM , 6-2) 30

3 25 25/10/11/ MSM : Front seats with shock absorbers. SICMA 159. Detailed CHK 18 HRS 0/0/0 check. DI. (Ref AMM , 6-7) , 171, 25 25/10/12/ MSM : Pilot and copilot seats - Rails. CHK 18 HRS 0/0/0 FISCHER H140. Check. DI. (Ref AMM , 6-8) , 171, 29 29/// MSM : Hydraulic system - Drain and fill. Servicing of the stainer CHK 1460 DYS 0. HRS 16-maj maj , 557 0/0/0 and the filter. DRN. (Ref AMM 29--, 3-3 / 3-6) 29 29/10/10/ MSM : Single hydraulic generation system - Hose. PRE MOD CHK 2190 DYS 0. HRS 16-maj maj , 404/0/ Replacement. DS. (Ref AMM , 8-1) 29 29/// MSM : Hydraulic system - Drain and fill. Servicing of the stainer CHK 30 HRS 0. HRS 16-maj-16 0/0/0 and the filter. DRN. (Ref AMM 29--, 3-3 / 3-6) 3 0, 1 371, 29 29/10/10/ MSM : Single hydraulic generation system - Hose. PRE MOD CHK 50 HRS 0. HRS 16-maj /0/ Replacement. DS. (Ref AMM , 8-1) 5 0, 3 371, 32 32/13// MSM : Skid landing gear. Detailed check. DI FT. (Ref AMM 32- CHK 54 HRS 601/0/0 11-, 6-1 / 6-3 / 6-4) , 3 771, 32 32/// MSM : Landing gear shock absorber - Detailed check. DI FT. CHK 54 HRS 0/0/0 (Ref AMM , 5-1 / 6-2) 1 5 4, 3 771,

4 53 53/10/02/ ALS : Rear frame. PRE MOD and not equipped with the CHK 5 HRS 0/0/0 2 reinforcement angles on the RH side (task , 8-5 AMM). Visual check. Operation to be done from 3250 FH. - If there is/are cracks of length less than or equal to 30 mm, this check must be carried out every 110 FH. - If there is at least one crack of length more than 30 mm, comply with task , 8-5 (AMM). DI (Ref AMM , 6-6) 53 53/10/02/ ALS : Rear frame. Visual check to be carried out from 3250 FH CHK 5 HRS 0/0/0 on aircraft: - PRE MOD , - equipped with the 2 reinforcement 05 angles on the RH side (task , 8-5 AMM), - not equipped with the 4 reinforcement angles (task , 8-5 AMM). DI (Ref AMM , 6-7) 3 750, 3 750, 2 121, 2 121, 53 53/10// MSM : Tail boom-to-fuselage junction. Check. TCK. (Ref AMM CHK 2190 DYS 0. HRS 16-maj maj , 0/0/ , 6-1) /10// MSM : Tail boom-to-fuselage junction. Check. TCK. (Ref AMM CHK 25 HRS 0. HRS 16-maj-16 0/0/ , 6-1) , 871, 55 55/// MSM : Fins. Detailed check. DI TCK FT. (Ref AMM , 6- CHK 54 HRS 0/0/0 2) , 3 771, 62 ASB Check the sealant bead on the main rotor mast P/N: 350A CHK 165 HRS 1 7, 71, 3.B.2.a.( 04(M/R SHAFT ASSY) S/N: FR2507 2) repetetiv / EASA AD /10// MSM : Main Rotor Blade pin greasing - LUB. (Ref AMM CHK 182 DYS HRS 15-jul jan-19 69, /0/0, 3-3) 62 62/30// MSM : Swashplate. Visual check of the guide and swivel CHK 3 HRS HRS 04-okt-18 0/0/2 bearing. Detailed check of the swashplate. VC DI. (Re AMM , / 6-2 / 6-3) 1 848,60 219,

5 62 62/10// MSM : Main Rotor Blade pin greasing - LUB. (Ref AMM CHK 6 HRS HRS 15-jul /0/0, 3-3) 1 862, 233, 62 ASB Check of the two bearing retaining rings P/N: 350A (M/R CHK 660 HRS 3.B.2.b / SHAFT ASSY) S/N: FR2507 EASA AD , 233, 62 ASB Check of the two bearing retaining rings P/N: 350A (M/R CHK 730 DYS 14-jul , B.2.b / SHAFT ASSY) S/N: FR2507 EASA AD /20// MGB Oil Filter element - CH48108/FA01315A - replacement CHK 6 HRS HRS 15-jul-18 0/0/ , 233, 63 63/20// MGB Oil Filter element - CH48108/FA01315A - replacement CHK 730 DYS HRS 15-jul jul , 617 0/0/ /40// MSM : Oil temperature warning system. Check. DRN DI FT. (Ref CHK 2190 DYS 0. HRS 16-maj maj , 0/0/0 AMM , 5-1 / 5-2) 63 63/30// MSM : MGB suspension cross bar. Check with removal. DI. (Ref CHK 2190 DYS 0. HRS 16-maj maj , 0/0/0 AMM , 6-1 / 6-3) /40// MSM : Oil temperature warning system. Check. DRN DI FT. (Ref CHK 24 HRS 0. HRS 16-maj-16 0/0/0 AMM , 5-1 / 5-2) 2 4, 771,

6 63 63/30// MSM : MGB suspension cross bar. Check with removal. DI. (Ref CHK 30 HRS 0. HRS 16-maj-16 0/0/0 AMM , 6-1 / 6-3) , 1 371, 65 65/20// MSM : Hinge Bearing. Check. GVI. (Ref AMM , 6-10) CHK 730 DYS HRS 16-mar mar , /0/ /20// MSM : Hinge Bearing. Check. GVI. (Ref AMM , 6-10) CHK 12 HRS HRS 16-mar /0/ ,90 494, 67 67/30// MSM : Tail servocontrol - Hose. Replacement. DS. PRE MOD CHK 2190 DYS 0. HRS 16-maj maj , 406/0/ (Ref AMM , 8-1) 67 67/30// MSM : Tail servocontrol - Hose. Replacement. DS. PRE MOD CHK 50 HRS 0. HRS 16-maj /0/ (Ref AMM , 8-1) 5 0, 3 371, 71 STC AFS-AS350B-IBF-ICA. 1FH/1Y CHK 1 HRS HRS 04-okt-18 EASA.IM. R.S ,20 15, 71 STC AFS-AS350B-IBF-ICA. 1FH. CHK 1 HRS HRS 04-okt-18 EASA.IM. Function check of IBF Bypass Cockpit Switch as defined in Iaw R.S.0150 AFS-AS350B-IBF-ICA table 1 note ,60 19, 71 STC AFS-AS350B-IBF-ICA. 1Y CHK 365 DYS HRS 04-jul jul , 241 EASA.IM. R.S.0150

7 76 EASA AD Engine Controls Switches 53Ka, 53Kb and 65K Inspection / CHK 365 DYS HRS 04-okt okt , Modification (EASB / ) EASA AD Engine Controls Switches 53Ka, 53Kb and 65K Inspection / CHK 660 HRS HRS 04-okt Modification (EASB / ) ,60 579, 76 76/30/12/ Twist grip - Load spring CHK 12 HRS HRS 15-jul-18 0/0/0 Engine ARRIEL 2D. 10 Replacement of the load spring acc to AMM , 4-2 DS 2 462, 833, Due at date is calculated based on average values defined for this aircraft and remaining dys is calculated from this. Page 1/