Ng CY. ENL.FLIGHT LOG: AC/TT: 425,3 DATE:
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1 OPERATOR: Barken timmer Ng CY. ENL.FLIGHT LOG: AC/TT: 425,3 DATE: AIRCRAFT TYPE: AS 350 B2 Nf CY. ENL.FLIGHT LOG: LANDINGS: AIRCRAFT S/N: 4474 ENG./TT: 425,3 REGISTRATION: SE-HJL ENG.Ng/CY: ENG.Nf/CY: A=Airframe hrs, E= Engine hrs, L=Landings, C=Cycles INSTALLATION TBO TBO REM REM HRS/ M. TO HRS / C INSPECTION P/N S/N POS. DATE. HRS / TSO HRS / M HRS / DATE C/M IN SERV TO CODE VARN CYCLE CYCLE CYCLE SERV. SERV. 150 Hours/12 Month inspection MSM , M 458, h 3,3 m 33 h A 150 Hours inspection MSM , ,2 67 h 33 h A 600 Hours inspection MSM , ,0 425 h 175 h A 600 Hours/24 Month inspection MSM , M 769, h 0,7 m 344 h A VARN 1200 Hours inspection MSM , M 1200,0 425 h 775 h A 1200 Hour / 48 Month airframe inspection MSM , M 1369, h 22,7 m 944 h A 12 Month airframe inspection MSM ,2 0 12M ,3 m A 24 Month airframe MSM ,5 0 26M ,7 m A VARN 48 Months inspection MSM ,5 0 48M ,7 m A 144 Month airframe inspection MSM , M h 69,3 m A ENGINE 15 HRS/7DAYS ,2 15 0M 426, h -2,1 m 1 h A ENGINE 30 HRS , ,2 14 h 16 h A ENGINE 50 HRS , ,2 14 h 36 h A ENGINE 100 HRS , ,2 67 h 33 h A ENGINE 400 HRS , ,2 67 h 333 h A ENGINE 300 HRS/1YEAR , M 658, h 3,3 m 233 h A ENGINE 500 HRS , ,0 425 h 75 h A ENGINE 600 HRS , ,0 425 h 175 h A ENGINE 750 HRS , ,5 256 h 494 h A ENGINE 1000 HRS , M 1000,0 425 h 575 h A ENGINE 1200 HRS , M 1200,0 425 h 775 h A ENGINE 1500 HRS , M 1500,0 425 h 1075 h A ENGINE 3000 HRS , M 3000,0 425 h 2575 h A ENGINE 3600 HRS , M 3600,0 425 h 3175 h A COMPONENT Task Ref TAIL ROTOR BLADE INSP SB R ,2 0,0 30 h 441,2 14 h 16 h A VARN AD , TR PITCH LINK SB ,2 0,0 30 h 441,2 14 h 16 h A VARN AD R1, SWASHPLATE INSPECTION SB ,2 A Blade skin AMM , 6-3 MSM ,2 100 h 458,2 67 h 33 h A VARN Chip detector AMM , 6-2 MSM ,2 100 h 458,2 67 h 33 h A VARN Rod end-fitting AMM , 6-1 MSM ,2 100 h 458,2 67 h 33 h A VARN Hydraulic pump - drive shaft splines AMM MSM ,2 0,0 100 h 6M 511 h ,1 h 3,9 m 86 h A TAIL ROTOR PITCH HORN AD SB R ,6 165 h 495,6 95 h 70 h A
2 OPERATOR: Barken timmer Ng CY. ENL.FLIGHT LOG: AC/TT: 425,3 DATE: AIRCRAFT TYPE: AS 350 B2 Nf CY. ENL.FLIGHT LOG: LANDINGS: AIRCRAFT S/N: 4474 ENG./TT: 425,3 REGISTRATION: SE-HJL ENG.Ng/CY: ENG.Nf/CY: A=Airframe hrs, E= Engine hrs, L=Landings, C=Cycles INSTALLATION TBO TBO REM REM HRS/ M. TO HRS / C INSPECTION P/N S/N POS. DATE. HRS / TSO HRS / M HRS / DATE C/M IN SERV TO CODE VARN TAIL ROTOR BLADE SB R5. BEARING REMOVED ,0 0,0 500 h 500,0 425 h 75 h A Swashplate 62/30/00/000/000/210 MSM ,1 0,0 300 h 0M 567,1 158 h 142 h A Starter generator 80/00/00/402/000/080 MSM , h 0M 567,1 158 h 142 h A FUEL TANK DRAIN CONTROL CABLE SB ,1 600 h 24M 983, ,5 m 558 h A #REFERENS! REAR FRAME REINFORCEMENT ANGLES SB ,0 0,0 165 h 650,0-60 h 225 h A MGB, MOBIL JET OIL 2 63/20/00/000/000/025 MSM ,5 0,0 500 h 26M 669, h 0,7 m 244 h A #REFERENS! Check of the start gen. Elec. Harness SB ,0 600 h 739,0 286 h 314 h A #REFERENS! AD , Comp. Gas. Gen. SB ,0 750 h 750,0 425 h 325 h A F R ,2 400 h 758,2 67 h 333 h A #REFERENS! TGB, MOBIL JET OIL 2 65/20/00/000/000/030 MSM ,2 0,0 500 h 24M 858, h 15,3 m 433 h A Blade pin AMM , 3-3 MSM ,2 0,0 600 h 6M 1011, h 3,9 m 586 h A Gas generator 2nd turbine blade A ,0 150 h 1200,0 775 h A AD ND STAGE TURBINE BLADES ,0 0, h 1200,0 425 h 775 h A Casing 65/20/00/000/000/140 MSM ,5 0, h 26M 1369, h 0,7 m 944 h A Pitch control lever 65/20/00/601/000/020 MSM ,5 0, h 26M 1370 h ,8 h 0,7 m 944 h A Pilot & copilot seats AMM , 6-2 MSM , h 1800,0 425 L 1375 h A Pilot & copilot seat rails CMM SICMA , h 1800,0 425 L 1375 h A Oil temp warning system 63/40/00/000/000/000 MSM ,0 0, h 78M 2400, h 3,2 m 1975 h A FUEL PUMP-Brush check 28/20/00/000/000/065 MSM ,0 0, h 2400,0 425 h 1975 h A Tail boom-to-fuselage junction 53/10/00/000/000/030 MSM ,0 0, h 78M 2500, h 3,2 m 2075 h A #REFERENS! Hydraulic system - drain & fill 29/00/00/000/000/000 MSM ,5 0, h 48M 2670 h ,8 h 22,7 m 2244 h A Vibration damper, spring type 62/20/00/604/000/000 MSM ,0 0, h 78M 3000, h 3,2 m 2575 h A MGB suspension cross bar 63/30/00/000/000/060 MSM , h 78M h 3,2 m 2574,7 A Hydraulic system - Hose replacement 29/10/10/404/000/000 MSM , h 78M 5000 h ,3 h 3,2 m 4575 h A Landing gear shock absorber 32/00/00/000/000/010 MSM ,0 0, h 0M 5400 h 425,3 h 4975 h A Skid landing gear 32/13/00/601/000/010 MSM ,0 0, h 0M 5400 h 425,3 h 4975 h A Fins 55/00/00/000/000/050 MSM ,0 0, h 0M 5400,0 425 h 4975 h A Cabin fire extinguisher 26/22/00/000/000/020 MSM ,2 0,0 0 h 6M ,9 m A Transmission components 60/00/00/000/000/120 MSM ,0 0,0 0 h 144M ,3 m A #REFERENS! Main rotor shaft 62/30/00/000/000/085 MSM ,0 0,0 0 h 78M ,2 m A #REFERENS! Engine intake seal insp. SB ,0 24M ,3 m A #REFERENS! TRH pitch change unit- labyrint seal - bearing AMM , 6-15 MSM ,5 0,0 A AD , 41/23 bevel gear check SB Ver B M ,4 m A AD ALS Section 4 P/N S/N GAS GENERATOR ROTATING ASSY AND REAR BEARING - CHK/
3 OPERATOR: Barken timmer Ng CY. ENL.FLIGHT LOG: AC/TT: 425,3 DATE: AIRCRAFT TYPE: AS 350 B2 Nf CY. ENL.FLIGHT LOG: LANDINGS: AIRCRAFT S/N: 4474 ENG./TT: 425,3 REGISTRATION: SE-HJL ENG.Ng/CY: ENG.Nf/CY: A=Airframe hrs, E= Engine hrs, L=Landings, C=Cycles INSTALLATION TBO TBO REM REM HRS/ M. TO HRS / C INSPECTION P/N S/N POS. DATE. HRS / TSO HRS / M HRS / DATE C/M IN SERV TO CODE VARN Starflex star 350A M , h 2400,0 425 L 1975 h A Spherical thrust bearing bolts 350A , h 3000,0 425 h 2575 h A Spherical thrust bearing bolts 350A , h 3000,0 425 h 2575 h A Spherical thrust bearing bolts 350A , h 3000,0 425 h 2575 h A Spherical thrust bearing bolts 350A , h 3000,0 425 h 2575 h A Spherical thrust bearing bolts 350A , h 3000,0 425 h 2575 h A Spherical thrust bearing bolts 350A , h 3000,0 425 h 2575 h A MRH attachment bolts 350A ,0 0, h 3000,0 425 h 2575 h A MRH attachment bolts 350A ,0 0, h 3000,0 425 h 2575 h A MRH attachment bolts 350A ,0 0, h 3000,0 425 h 2575 h A MRH attachment bolts 350A ,0 0, h 3000,0 425 h 2575 h A MRH attachment bolts 350A ,0 0, h 3000,0 425 h 2575 h A MRH attachment bolts 350A ,0 0, h 3000,0 425 h 2575 h A MRH attachment bolts 350A ,0 0, h 3000,0 425 h 2575 h A MRH attachment bolts 350A ,0 0, h 3000,0 425 h 2575 h A MRH attachment bolts 350A ,0 0, h 3000,0 425 h 2575 h A MRH attachment bolts 350A ,0 0, h 3000,0 425 h 2575 h A MRH attachment bolts 350A ,0 0, h 3000,0 425 h 2575 h A MRH attachment bolts 350A ,0 0, h 3000,0 425 h 2575 h A TRH pitch change unit - Bearing 704A ,0 0, h 3000,0 425 h 2575 h A MGB Oil pump 350A M ,0 0, h 3500,0 425 h 3075 h A EPICYCLIC REDUCTION GEAR 350A M ,0 0, h 288M 3500, h 3075 h A BEVEL REDUCTION GEAR 350A M ,0 0, h 288M 4200, h 3775 h A TAIL GEAR BOX 350A MA , h 288M 3000, h 2575 h A Tail rotor blade 355A , h 4000,0 425 h 3575 h A Tail rotor blade horn 350A ML , h 20000,0 425 h h A Tail rotor blade horn 350A ML , h 20000,0 425 h h A TR Pitch rod LB , h 20000,0 425 h h A lower sleeve flange (Flat) 350A M , h 4400,0 425 L 3975 h A lower sleeve flange (Flat) 350A M , h 4400,0 425 L 3975 h A lower sleeve flange (Flat) 350A M , h 4400,0 425 L 3975 h A Upper sleeve flange (Flat) 350A M , h 4400,0 425 L 3975 h A Upper sleeve flange (Flat) 350A M , h 4400,0 425 L 3975 h A Upper sleeve flange (Flat) 350A M , h 4400,0 425 L 3975 h A Bevel gear 350A L , h 4700,0 425 h 4275 h A
4 OPERATOR: Barken timmer Ng CY. ENL.FLIGHT LOG: AC/TT: 425,3 DATE: AIRCRAFT TYPE: AS 350 B2 Nf CY. ENL.FLIGHT LOG: LANDINGS: AIRCRAFT S/N: 4474 ENG./TT: 425,3 REGISTRATION: SE-HJL ENG.Ng/CY: ENG.Nf/CY: A=Airframe hrs, E= Engine hrs, L=Landings, C=Cycles INSTALLATION TBO TBO REM REM HRS/ M. TO HRS / C INSPECTION P/N S/N POS. DATE. HRS / TSO HRS / M HRS / DATE C/M IN SERV TO CODE VARN Spherical thrust bearing 704A , h 6400,0 425 L 5975 h A Spherical thrust bearing 704A , h 6400,0 425 L 5975 h A Spherical thrust bearing 704A , h 6400,0 425 L 5975 h A Aft shaft 350A M ,0 0, h 10500,0 425 h h A Bevel wheel 350A L ,0 0, h 14000,0 425 h h A Main rotor blade 355A , h 0M 20000,0 425 L h A #REFERENS! Main rotor blade 355A , h 0M 20000,0 425 L h A Main rotor blade 355A , h 20000,0 425 L h A Planet gear 350A L ,0 0, h 20000,0 425 h h A Planet gear 350A L ,0 0, h 20000,0 425 h h A Planet gear 350A L ,0 0, h 20000,0 425 h h A Planet gear 350A L ,0 0, h 20000,0 425 h h A Planet gear 350A L ,0 0, h 20000,0 425 h h A MGB bottom casing 350A MAP , h 20000,0 425 h h A #REFERENS! Bevel gear 350A M ,0 0, h 20000,0 425 L h A Bevel wheel 350A L ,0 0, h 20000,0 425 h h A Fixed ring gear 350A M ,0 0, h 20000,0 425 h h A Casing 350A MA ,0 0, h 20000,0 425 h h A Tail rotor shaft 350A MA ,0 0, h 20000,0 425 h h A Planet gear holder 350A CUR ,0 0, h 68700,0 425 h h C Blade horn 350A MAP , h 80000,0 425 L h A Blade horn 350A MAP , h 80000,0 425 L h A Blade horn 350A MAP , h 80000,0 425 L h A Main rotor shaft 350A FR ,0 0, c ,0 425 h c A Main casing 350A MAP ,0 0,0 INF INF Control lever 350A MA ,0 0,0 INF INF COMPONENT AC/TT, ENGINE ARRIEL 1D1S/N: M05 Magnetic plug check N/A , h 441,2 14 h 16 h A #REFERENS! M01 Magnetic plug check N/A , h 441,2 14,1 c 16 h C SOAP (OPTIONAL) N/A N/A , h 408,2 67,1 c -17 h C ÖVER Electric magnetic plug - Inspection and cleaning N/A , h 12M 711, ,1 c 9,9 m 286 h C Engine oil change MOBIL JET OIL 2 N/A , h 12M 683, h 7,4 m 257,8 A FUEL FILTER CLOG TEST AMM , ,0 500 h 24M h 1,1 m 74,7 A Fuel filter N/A , h 48M ,3 c 1,1 m 575 h GAS GEN 2ND STAGE BLADES A1J0 RS , h h 774,7
5 OPERATOR: Barken timmer Ng CY. ENL.FLIGHT LOG: AC/TT: 425,3 DATE: AIRCRAFT TYPE: AS 350 B2 Nf CY. ENL.FLIGHT LOG: LANDINGS: AIRCRAFT S/N: 4474 ENG./TT: 425,3 REGISTRATION: SE-HJL ENG.Ng/CY: ENG.Nf/CY: A=Airframe hrs, E= Engine hrs, L=Landings, C=Cycles INSTALLATION TBO TBO REM REM HRS/ M. TO HRS / C INSPECTION P/N S/N POS. DATE. HRS / TSO HRS / M HRS / DATE C/M IN SERV TO CODE VARN ENGINE ARRIEL 1D , h 180M h 99,9 m 3074,7 A Module 3-Gas generator 70BM , h 180M h 99,9 m 3074,7 RED GB NUT , h h 3174,7 A FREE TURBINE REDUCTION GEAR 70BM , h 180M h 99,9 m 3174,7 2ND ST NGV HUB (FRONT) PR , c h 3174,7 2ND ST NGV HUB (REAR) PR , h h 3174,7 GAS GEN REAR BEARING , h h 3174,7 FREE TURBINE FRONT BEARING , h h 3174,7 RED. EQUIPPED SLEEVE SET , h h 3174,7 GAS GEN 1ST STAGE BLADES A1K0 JR , h h 5574,7 Module 2-Axial compressor 70BM , h 180M h 99,9 m 6774,7 A Bearing , c h 6774,7 Bearing , c h 6774,7 Bearing , c h 6774,7 FREE TURBINE MODULE 70BM , h 180M h 99,9 m 6774,7 FREE TURBINE REAR BEARING , h h 6774,7 FREE TURBINE REAR BEARING , h h 6774,7 FREE TURBINE BLADES A1N0 HB , h h 6774,7 RED. DRIVE GEAR FRON BEARING , h h 6774,7 RED. DRIVE GEAR REAR BEARING , h h 6774,7 RED. OUTPUT GEAR FRONT BEARING , h h 6774,7 RED. OUTPUT GEAR REAR BEARING , h h 6774,7 RED. INTERMEDIATE GEAR FRONT BEARING , h h 6774,7 RED. INTERMEDIATE GEAR REAR BEARING , h h 6774,7 RED. TRIPLEX BEARING , h h 6774,7 Injection wheel AD , c h 9574,7 Turbine disc HP F620AD , c h 9574,7 TURBINE DISC 1ST STAGE E728AD , c h 9574,7 TURBINE DISC 2ND STAGE F006AD , c h 9574,7 GAS GEN 2ND STAGE BLADES A1J0 RS , c h 9574,7 GAS GEN 1ST STAGE BLADES A1K0 JR , c h 11574,7 FREE TURBINE BLADES A1N0 HB , c h 11574,7 Axial comp. Wheel TT , c c 13574,7 Centrifugal impeller CAR , c h 13574,7 O/SPEED BLEEDING VALVE , M ,8 m A
6 OPERATOR: Barken timmer Ng CY. ENL.FLIGHT LOG: AC/TT: 425,3 DATE: AIRCRAFT TYPE: AS 350 B2 Nf CY. ENL.FLIGHT LOG: LANDINGS: AIRCRAFT S/N: 4474 ENG./TT: 425,3 REGISTRATION: SE-HJL ENG.Ng/CY: ENG.Nf/CY: A=Airframe hrs, E= Engine hrs, L=Landings, C=Cycles INSTALLATION TBO TBO REM REM HRS/ M. TO HRS / C INSPECTION P/N S/N POS. DATE. HRS / TSO HRS / M HRS / DATE C/M IN SERV TO CODE VARN Module 1-Acessories gearbox 70BM , M ,9 m A FUEL CONTROL UNIT , h h 3174,7 A FREEWHEEL SHAFT ASSY , h FREE WHEEL , h FREEWHEEL BEARING , h FREEWHEEL SHAFT , h COMPLETE VALVE , M ,8 m COMPONENT, CALENDER TIME ELT, FUNCTIONAL CHECK S ,2 1M m -1,1 m ÖVER ARC AS M m 11,1 m BATTERY, CMM CH1 V M m -1,2 m ÖVER BATTERY, CMM CH1 V ,1 0 6M m 1,5 m BATTERY, CMM CH1 V M m 10,8 m FIRE EXTINGUISHER H1-10AIR ,2 6M m 3,9 m COMPASS SWING U8429 BC M m -1,4 m ÖVER AIRSPEED IND M m -1,4 m ÖVER ALTIMETER M m -1,4 m ÖVER FIRST AID KIT ,1 12M m 7,5 m ELT, ME406HM, BATTERY S M m 51,3 m FIRE EXTINGUISHER H1-10AIR M m 45,2 m #REFERENS! HOSE 5110 DIA12X18,5 ATA M m 45,2 m #REFERENS! HOSE 350A ATA M m 45,2 m HOSE 350A ATA M m 45,2 m
7 REMARKS N/A TO P/N INST. WO 1563
8 REMARKS DI, LUB INSPECTION INSP LUB LUB LUB MM , 6-13 MM , 6-12 AMM , 6-2 CMM MM , 5-1 & 5-2 MM , 6-1 MM , 6-11 MM , 6-1, 6-2, 6-3 MM , 8-1 DI DI DI, INIT 144M REP 72M MM , 6-5 N/A. DUE T MOD P DUE AT MODULE 1 REMO DUE AT MODULE 3 REMO
9 REMARKS
10 REMARKS TC TC INSP INSP INSP INSP
11 REMARKS OVERHAUL
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