AS350B3e (H125) MAINTENANCE PROGRAM AIRFRAME INSPECTION PROGRAM AC Serial number 8242 AC Total time 1,629.30 HRS at date 02.11.2018 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 922.90 HRS 16-mar-18 15-mar-20 496, 496 1980:5 8 DUE AT REMAINING LFS Pitot Static System - Check - Altimeter and Airspeed Indicator check iaw CHK 730 DYS 922.90 HRS 16-mar-18 15-mar-20 496, 496 1980:5 LFS 1980:5 4-7 (BCL-M 4.3) 4-7 04 04/CAME/ Airworthiness Review - Perform Annual Airworthiness Review Extension CHK 365 DYS 1091.70 HRS 31-maj-18 30-maj-19 206, 206 01 04 04/CAME/ Airworthiness Review - Renewal CHK 1095 DYS 16. HRS 31-maj-16 31-maj-19 207, 207 02 05 05/05/0 1FH /150FH Inspection (MSM 05-21-/05-21-01/05-25-) CHK 1 HRS 1548.60 HRS 04-okt-18 /0/ 1 648,60 19, 05 05/06/0 12M Inspection (MSM 05-21-02) CHK 365 DYS 1014.20 HRS 10-maj-18 10-maj-19 186, 186 /0/
05 05/08/0 6FH / 24M INSPECTION (MSM 05-22- /-01 /-02) CHK 6 HRS 1262. HRS 15-jul-18 /0/ 1 862, 233, 05 05/08/0 6FH / 24M INSPECTION (MSM 05-22- /-01 /-02) CHK 730 DYS 1262. HRS 15-jul-18 14-jul-20 617, 617 /0/ 05 05/09/0 12FH / 48M Inspection (MSM 05-23- / -01 / -02) CHK 12 HRS 1262. HRS 15-jul-18 /0/ 2 462, 833, 05 05/09/0 12FH / 48M Inspection (MSM 05-23- / -01 / -02) CHK 1460 DYS 1262. HRS 15-jul-18 14-jul-22 1 347, 1347 /0/ 05 05/10/0 MAJOR INSPECTION 144 M (MSM 05-24-02) CHK 4380 DYS 0. HRS 16-maj-16 13-maj-28 3 477, 3477 /0/ 08 08/EU Aircraft Weighing CHK 1460 DYS 11-maj-20 553, 553 OPS-CAT 25 AS350 Emergency floatation gear - Check of the front and rear attachment CHK 390 DYS 1014.20 HRS 10-maj-18 04-jun-19 211, 211 SB- brackets - Comply with paragraph 3. (except paragraph 3.B.2.a.) 05..63 25 25/10/11/ MSM 05-25-: Front seats with shock absorbers - Rails. SICMA 159. CHK 18 HRS 1 8, 171, 0/0/0 Check. DI. (Ref AMM 25-21-, 6-2) 30
25 25/10/11/ MSM 05-25-: Front seats with shock absorbers. SICMA 159. Detailed CHK 18 HRS 0/0/0 check. DI. (Ref AMM 25-21-, 6-7) 10 1 8, 171, 25 25/10/12/ MSM 05-25-: Pilot and copilot seats - Rails. CHK 18 HRS 0/0/0 FISCHER H140. Check. DI. (Ref AMM 25-21-, 6-8) 70 1 8, 171, 29 29/// MSM 05-25-: Hydraulic system - Drain and fill. Servicing of the stainer CHK 1460 DYS 0. HRS 16-maj-16 15-maj-20 557, 557 0/0/0 and the filter. DRN. (Ref AMM 29--, 3-3 / 3-6) 29 29/10/10/ MSM 05-25-: Single hydraulic generation system - Hose. PRE MOD CHK 2190 DYS 0. HRS 16-maj-16 15-maj-22 1 287, 404/0/0 074239. Replacement. DS. (Ref AMM 29-10-, 8-1) 29 29/// MSM 05-25-: 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 05-25-: Single hydraulic generation system - Hose. PRE MOD CHK 50 HRS 0. HRS 16-maj-16 404/0/0 074239. Replacement. DS. (Ref AMM 29-10-, 8-1) 5 0, 3 371, 32 32/13// MSM 05-25-: Skid landing gear. Detailed check. DI FT. (Ref AMM 32- CHK 54 HRS 601/0/0 11-, 6-1 / 6-3 / 6-4) 10 5 4, 3 771, 32 32/// MSM 05-25-: Landing gear shock absorber - Detailed check. DI FT. CHK 54 HRS 0/0/0 (Ref AMM 32-11-, 5-1 / 6-2) 1 5 4, 3 771,
53 53/10/02/ ALS 04-20-: Rear frame. PRE MOD 073215 and not equipped with the CHK 5 HRS 0/0/0 2 reinforcement angles on the RH side (task 53-31-, 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 53-31-, 8-5 (AMM). DI (Ref AMM 53-31-, 6-6) 53 53/10/02/ ALS 04-20-: Rear frame. Visual check to be carried out from 3250 FH CHK 5 HRS 0/0/0 on aircraft: - PRE MOD 073215, - equipped with the 2 reinforcement 05 angles on the RH side (task 53-31-, 8-5 AMM), - not equipped with the 4 reinforcement angles (task 53-31-, 8-5 AMM). DI (Ref AMM 53-31-, 6-7) 3 750, 3 750, 2 121, 2 121, 53 53/10// MSM 05-25-: Tail boom-to-fuselage junction. Check. TCK. (Ref AMM CHK 2190 DYS 0. HRS 16-maj-16 15-maj-22 1 287, 0/0/0 53-31-, 6-1) 30 53 53/10// MSM 05-25-: Tail boom-to-fuselage junction. Check. TCK. (Ref AMM CHK 25 HRS 0. HRS 16-maj-16 0/0/0 53-31-, 6-1) 30 2 5, 871, 55 55/// MSM 05-25-: Fins. Detailed check. DI TCK FT. (Ref AMM 55-20-, 6- CHK 54 HRS 0/0/0 2) 50 5 4, 3 771, 62 ASB Check the sealant bead on the main rotor mast P/N: 350A37-1290- CHK 165 HRS 1 7, 71, 3.B.2.a.( 04(M/R SHAFT ASSY) S/N: FR2507 2) repetetiv / EASA AD 2018-0206 62 62/10// MSM 05-25-: Main Rotor Blade pin greasing - LUB. (Ref AMM 62-11- CHK 182 DYS 1262. HRS 15-jul-18 13-jan-19 69, 69 401/0/0, 3-3) 62 62/30// MSM 05-25-: Swashplate. Visual check of the guide and swivel CHK 3 HRS 1548.60 HRS 04-okt-18 0/0/2 bearing. Detailed check of the swashplate. VC DI. (Re AMM 62-32-, 6-10 1 / 6-2 / 6-3) 1 848,60 219,
62 62/10// MSM 05-25-: Main Rotor Blade pin greasing - LUB. (Ref AMM 62-11- CHK 6 HRS 1262. HRS 15-jul-18 401/0/0, 3-3) 1 862, 233, 62 ASB Check of the two bearing retaining rings P/N: 350A37-1290-04(M/R CHK 660 HRS 3.B.2.b / SHAFT ASSY) S/N: FR2507 EASA AD 2018-0206 1 862, 233, 62 ASB Check of the two bearing retaining rings P/N: 350A37-1290-04(M/R CHK 730 DYS 14-jul-20 617, 617 3.B.2.b / SHAFT ASSY) S/N: FR2507 EASA AD 2018-0206 63 63/20// MGB Oil Filter element - CH48108/FA01315A - replacement CHK 6 HRS 1262. HRS 15-jul-18 0/0/0 45 1 862, 233, 63 63/20// MGB Oil Filter element - CH48108/FA01315A - replacement CHK 730 DYS 1262. HRS 15-jul-18 14-jul-20 617, 617 0/0/0 45 63 63/40// MSM 05-25-: Oil temperature warning system. Check. DRN DI FT. (Ref CHK 2190 DYS 0. HRS 16-maj-16 15-maj-22 1 287, 0/0/0 AMM 63-42-, 5-1 / 5-2) 63 63/30// MSM 05-25-: MGB suspension cross bar. Check with removal. DI. (Ref CHK 2190 DYS 0. HRS 16-maj-16 15-maj-22 1 287, 0/0/0 AMM 63-31-, 6-1 / 6-3) 60 63 63/40// MSM 05-25-: Oil temperature warning system. Check. DRN DI FT. (Ref CHK 24 HRS 0. HRS 16-maj-16 0/0/0 AMM 63-42-, 5-1 / 5-2) 2 4, 771,
63 63/30// MSM 05-25-: MGB suspension cross bar. Check with removal. DI. (Ref CHK 30 HRS 0. HRS 16-maj-16 0/0/0 AMM 63-31-, 6-1 / 6-3) 60 3 0, 1 371, 65 65/20// MSM 05-25-: Hinge Bearing. Check. GVI. (Ref AMM 65-21-, 6-10) CHK 730 DYS 922.90 HRS 16-mar-18 15-mar-20 496, 496 601/0/0 65 65/20// MSM 05-25-: Hinge Bearing. Check. GVI. (Ref AMM 65-21-, 6-10) CHK 12 HRS 922.90 HRS 16-mar-18 601/0/0 2 122,90 494, 67 67/30// MSM 05-25-: Tail servocontrol - Hose. Replacement. DS. PRE MOD CHK 2190 DYS 0. HRS 16-maj-16 15-maj-22 1 287, 406/0/0 074239. (Ref AMM 67-33-, 8-1) 67 67/30// MSM 05-25-: Tail servocontrol - Hose. Replacement. DS. PRE MOD CHK 50 HRS 0. HRS 16-maj-16 406/0/0 074239. (Ref AMM 67-33-, 8-1) 5 0, 3 371, 71 STC AFS-AS350B-IBF-ICA. 1FH/1Y CHK 1 HRS 1548.60 HRS 04-okt-18 EASA.IM. R.S.0150 1 644,20 15, 71 STC AFS-AS350B-IBF-ICA. 1FH. CHK 1 HRS 1548.60 HRS 04-okt-18 EASA.IM. Function check of IBF Bypass Cockpit Switch as defined in 3.1.5. Iaw R.S.0150 AFS-AS350B-IBF-ICA table 1 note 8. 1 648,60 19, 71 STC AFS-AS350B-IBF-ICA. 1Y CHK 365 DYS 1229. HRS 04-jul-18 04-jul-19 241, 241 EASA.IM. R.S.0150
76 EASA AD Engine Controls Switches 53Ka, 53Kb and 65K Inspection / CHK 365 DYS 1548.60 HRS 04-okt-18 04-okt-19 333, 333 2017- Modification (EASB 05..61 / 05..77) 59 76 EASA AD Engine Controls Switches 53Ka, 53Kb and 65K Inspection / CHK 660 HRS 1548.60 HRS 04-okt-18 2017- Modification (EASB 05..61 / 05..77) 59 2 208,60 579, 76 76/30/12/ Twist grip - Load spring CHK 12 HRS 1262. HRS 15-jul-18 0/0/0 Engine ARRIEL 2D. 10 Replacement of the load spring acc to AMM 76-12-04, 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 1/1 05.11.2018