Aircraft Status List & Maintenance Forecast Component

Transcription

1 Owner: Segi Gemilang LH RH Eurocopter EC 135 P2 Date: 21-Jun-11 Eng. Hrs CRS-SMI issue from A/C S/N: 0289 Latest Tech Log Date 18-Jun-11 NG / N1 / CT Cyc Airframe AD = Germany Installed/Last C/W Time at install Current Eurocopter EC 135 P2 EC 135 P Nov-10 1 Y Renew Certificate of Airworthiness 9-Nov D Eurocopter EC 135 P2 EC 135 P Jan-11 1 Y Renew Aircraft Radio Licence 6-Jan D Eurocopter EC 135 P2 EC 135 P Jun-11 CMR368 4 M Renew Cert. of Maintenance Review 9-Oct D Eurocopter EC 135 P2 EC 135 P Dec H 400 Hrs Intermediate Inspection, H Eurocopter EC 135 P2 EC 135 P Dec M 12 Mth Inspection, Dec D Eurocopter EC 135 P2 EC 135 P Dec H 800 Hrs / 3 Year Periodical Inspection, H Eurocopter EC 135 P2 EC 135 P Dec Y 800 Hrs / 3 Year Periodical Inspection, Dec D Eurocopter EC 135 P2 EC 135 P n/a n/a 50 H 50 Hrs Supplementary Inspection N/A N/A Eurocopter EC 135 P2 EC 135 P Jul M Annual Radio Inspection 19-Jul D Eurocopter EC 135 P2 EC 135 P Jul H In-Situ Calibration of Engine Instruments AMM , 6-1 N/A N/A H Eurocopter EC 135 P2 EC 135 P Jul M In-Situ Calibration of Engine Instruments AMM , 6-1 N/A N/A D Eurocopter EC 135 P2 EC 135 P Jun H In-Situ Calibration of Flight Instruments AMM , Eurocopter EC 135 P2 EC 135 P Jun Y In-Situ Calibration of Flight Instruments AMM , Eurocopter EC 135 P2 EC 135 P Nov M Compensate standy Compass, , Nov D Eurocopter EC 135 P2 EC 135 P Mar H 100H/3M - AN 19A, Para 5: Check of battery H Eurocopter EC 135 P2 EC 135 P Mar M 100H/3M - AN 19A, Para 5: Check of battery 21-Jun-11 0 D ASB / AD ASB / AD ASB / AD Eurocopter EC 135 P2 EC 135 P Jun-11 6 M AD (SB 02/2011) Para 3 - ELT Antenna modification / replacement 2-Dec D Eurocopter EC 135 P2 EC 135 P May-11 M ASB 26A-003R1 Engine Fire Extinguishing System - Retrofit of heat-resistant injection tubes 31-Mar D Eurocopter EC 135 P2 EC 135 P May o/c(after adjustment, install/removal) 100 H ASB 67A-022 Tail rotor controls- Para. 1.E. Check of the ball bearing control c/o c/o H ASB A-045 EC 135 P Mar H 100 H/60 D ASB A Insp. & Mod. Of Eng. Control Switches on switch unit 20 c/o c/o H ASB A-045 EC 135 P Mar D 100 H/ 60 D ASB A Insp. & Mod. Of Eng. Control Switches on switch unit 2 c/o c/o D ASB A-045 R1 EC 135 P H ASB A-045 R1 - Insp. Of Eng. Control (Eng I and II) H ASB A-045 EC 135 P Oct M ASB A Insp. & Mod. Of Eng. Control Switches on switch unit 20VE. c/o c/o D Eurocopter EC 135 P2 EC 135 P Oct D AD E (ASB 31A-053) N/A N/A D Eurocopter EC 135 P2 EC 135 P Nov D ASB 31A-053 R1 N/A N/A D AD H1-10 AIR Ha EC 135 P Jan one time only.-c/o in W/O # D AD H1-10 AIR Halon 1211-Fire Ext.-Inspect for applicability IAW Annex in AD. c/o c/o D AD E-Fire Protection Portable Fire Extinguishers Identification / Replacement EC 135 P /8/ one time only.-c/o in W/O # Portable Fire Ext.,Identification/Replacement c/o c/o D SIN 2131-I-34 EC 135 P Jan one time only.-c/o in W/O # To check for interference of pitot-static lines with vibration dampers IAW SIN c/o c/o D SIN 2118-S-25 EC 135 P Jan one time only.-c/o in W/O # D To check for proper belt inlet plate installation IAW SIN c/o c/o D SIN 2118-S-25 EC 135 P Jan one time only.-c/o in W/O # H To check for proper belt inlet plate installation IAW SIN c/o c/o H AD R.1[Portable FEC 135 P Jan one time only.-c/o in W/O # D Halon 1211 Fire Ext. - Identification/Replacement. c/o c/o D AD (ASB EC 135EC 135 P /29/ Effective date for, before next flight-repetitive, pre-flight. AD (ASB EC A-021) c/o c/o D AD EU EC 135 P Feb Y AD EU : Mode S & C transponder cx n/a n/a D complied with in ASB A-007 EC 135 P Mar-10 one time only 100 H Insp. of hydraulic lines-fenestrom. c/o c/o H ASB A-007 EC 135 P Mar-10 one time only Insp. of hydraulic lines-fenestrom. c/o c/o D ASB A-049 EC 135 P Aug H Fuel S/O Valve - Check of Switches EMERG OFF 1 & 2. c/o c/o H ASB A-049 EC 135 P Aug M Fuel S/O Valve - Check of Switches EMERG OFF 1 & 2. c/o c/o D ASB A-049 R1 EC 135 P Nov M Fuel S/O Valve - Check of Switches EMERG OFF 1 & 2. c/o c/o D ASB A-012 EC 135 P Jan one time 50 H L/G Aft Cross-Tube - Inspection c/o c/o H ASB A-012 EC 135 P Jan C L/G Aft Cross-Tube - Inspection (TO CHECK P/N AND NOTE IF AFFECTED OR NOT) C ASB A-012 EC 135 P Jan Y L/G Aft Cross-Tube - Replacement (WOULD DEPEND ON INSPECTION) 31-Dec D AD E (ASB 33A-00EC 135 P Dec D AD E (ASB 33A-009) c/o c/o D ASB 52A-003 R0 EC 135 P Dec H ASB 52A-003 R0, Para. 3 MSM MSM ASB 53A-015 R0 EC 135 P Dec H ASB 53A-015 R0, Para H ASB 53A-015 R0 EC 135 P Jun ASB 53A Check water drainage holes c/o c/o ASB 63A-003 R0 EC 135 P Dec H ASB 63A-003 R0, Para. 3 MSM MSM ASB 53A-018 R0 EC 135 P Feb once only ASB 53A-018 R1 c/o c/o D EASA AD R1 & A EC 135 P Jan R0 c/o 100 H ASB 53A-022 R1:(replaced by ASB 53A-022 R2) Rear Structure Accomplish visual N/A N/A H Eurocopter EC 135 P2 EC 135 P Nov H ASB 53A-022 R2 N/A N/A Eurocopter EC 135 P2 EC 135 P Dec SB c/o c/o ASB 63A-012 R4 / EASA AD EC 135 P Feb st C/O at H 100 H 100H/12M ASB 63A-012 R4: Intro of oil analysis [DGAC AD E] After oil chg.take see oil drain H ASB 63A-012 R4 EC 135 P Feb st C/O at H 12 M 100H/12M ASB 63A-012 R4: Intro of oil analysis [DGAC AD E] After oil chg.take see oil drain D Stage II SB63A-012R4 EC 135 P Feb in cases of Stage II and above 25 H ASB 63A-012r4 para3.a.(5)(b)-mgb teeth inspection required by Stage II determined at the o c/o c/o H Eurocopter Malaysia SDN BHD Page 1 of 7

2 Installed/Last C/W Time at install Current ASB 63A-012 R4 EC 135 P Mar Limiting Fh for analysis of oil sample res 25 H ASB 63A-012R4 -the analysis of the oil sample H ASB 63A-013 R0 EC 135 P Oct once ASB 63A-013 R2: Cx attachment hardware [EASA AD E] c/o c/o H ASB 63A-016 EC 135 P Dec M SB R1- rec. c/o c/o D EASA (ASB 67A R3) EC 135 P Nov H (T/R Insp. of Control Rod & Ball Pivot) MET (6),(7) H [ASB 67A-019 R3] EC 135 P Jan Insp. c/o in W/O# & H /ASB 67A-019 R3 c/o c/o H [ASB 67A-019 R3] EC 135 P Jan H 800H/12M Inspection EASA (ASB 67A-019 R3) Para 3.C Tail Rotor and Collectiv N/A N/A H Retrofit found c/ [ASB 67A-019 R3] EC 135 P Jan M 800H/12M Inspection EASA (ASB 67A-019 R3) Para 3.C Tail Rotor and Collectiv N/A N/A D Retrofit found c/ [ASB 67A-019 R3] EC 135 P Oct of effective date of EASA AD M MOD. - 12M ASB 67A-019 R3 c/o c/o D [ASB 67A-019 R3] EC 135 P Sep H 800 H/ 36 M (EASA ) ASB 67A-019R3 Para 3.B Tail Rotor and Collective controls H [ASB 67A-019 R3] EC 135 P Sep M 800 H/ 36 M (EASA ) ASB 67A-019R3 Para 3.B Tail Rotor and Collective controls 28-Sep D ASB 04A-006 R1 EC 135 P Jan ONCE ASB 04A-006 R1, Para. 3B. (3) c/o c/o ASB 24A-013 R1 EC 135 P Nov ONCE ASB 24A-013 R1, Para. 3 c/o c/o ASB 24A-016 R0 EC 135 P Feb ONCE H ASB 24A-016 R0 c/o c/o ASB 21A-007 R2 EC 135 P Nov ONCE H ASB 21A-007 R2 - Ventialtion wire harnesses (next 800H) c/o c/o ASB 22A-014 R0 EC 135 P Mar ONCE H ASB 22A-014 R0-Chk H/ware for correct Installation. c/o c/o ASB 22A-015 EC 135 P Jul ONCE H ASB 22A-015. Chk. SEMA/control rod for correct attachment hardware. c/o c/o ASB 67A-009 EC 135 P Jul H ASB 67A-009 (Inspection & Repair of Pedal Bearings) H SB R0 EC 135 P Dec ONCE SB R0 (Coloured marking) c/o c/o ASB 67A-015 EC 135 P Jul ONCE ASB 67A-015 (Mod.of Cyc.Stick Locking Device/Ctr.Device) c/o c/o ASB 88A-001 R0 EC 135 P Jul ONCE ASB 88A-001 R0 wiring c/o c/o 05,50,00 SB EC 135 P Nov ONCE SB Connecting Flange to Fuel Supply line-check for leaks. c/o c/o 05,50,00 SB EC 135 P Nov ONCE SB Connecting Flange to Fuel Supply line-check for leaks. c/o c/o EC 135 P Mar once SIN-2158-S-67[Collective Lever Fixation] c/o c/o D Eurocopter EC 135 P2 EC 135 P Jul Y Weight & balance, (2Y TSN, 5Y TSI) 18-Jul D Flexible Hoses All All 30-Jun Check Condition o/c o/c D Metro Aviation Aircon Sys. EC135AC UNK 8-Nov Installed Metro Aviation Aircon Sys. EC135AC UNK 22-Mar H 50Hrs Complementary Check, Metro Aviation MM , para H Metro Aviation Aircon Sys. EC135AC UNK 12-Nov H 100 Hrs/12 Mth Insp, Metro Aviation MM , H Metro Aviation Aircon Sys. EC135AC UNK 12-Nov M 100 Hrs / 12 Mth Inspection, Metro Aviation MM , Nov D Metro Aviation Aircon Sys. EC135AC UNK 26-Mar H 400 Hrs Intermediate Inspection, Metro Aviation MM , H Air-conditioning Drive 90 O Ge510286D Aug H 90 O Gearbox, TBO (component must be returned to STC holder for overhaul) H Flex Drive Shaft 625-SMP-56-00BB-1C72 26-Mar H 400H Lubrication Flex Drive Shaft, Metro Aviation MM , H Flex Drive Shaft 625-SMP-56-00BB-1C Jul H Flex Drive Shaft, TBO (Fwd & Aft Coupl.) (component must be returned to STC holder for ov H Blower JBS K Mar H Supp insp: Blower, TBO (See MSM , 6-1) n/a n/a Blower JBS K Jul H Supp insp: Blower, Check Brushes for Wear, , 6-1 n/a n/a Ni-Cad Battery 40 Ah (Varta) Mar Installed Ni-Cad Battery 40 Ah (Varta) Jun H 100H/1M Battery, Visual Chk. (Hawker MM Ch.5.2) H Ni-Cad Battery 40 Ah (Varta) Jun M 100H/1M Battery, Visual Chk. (Hawker MM Ch.5.2) 6-Jul D Ni-Cad Battery 40 Ah (Varta) Jun H 300H/3M Battery, Elec. Chk (Hawker MM Ch.5.3) H Eurocopter Malaysia SDN BHD Page 2 of 7

3 Installed/Last C/W Time at install Current Ni-Cad Battery 40 Ah (Varta) Jun M 300H/3M Battery, Elec. Chk (Hawker MM Ch.5.3) 5-Sep D Ni-Cad Battery 40 Ah (Varta) Jun M Battery, TBO (Hawker MM Ch.6) 7-Jun D Ni-Cad Battery 40 Ah (Varta) May Y Temperature switch test (Hawker MM Ch.6.10) in cap cx in cap cx Over Head Panel UNK UNK 2400 H Inspection (i.a.w MET ,6-1) H Pilot Seat Belt System N/A 30-Jun Y Seat Belt System, SLL ** 31-Jan D Copilot Seat Belt System N/A 30-Jun Y Seat Belt System, SLL ** 31-Jan D ELT Artex 406 C406-2HM Jun OC OC OC ELT Artex 406 C406-2HM Mar M ELT serviceability cx, DCA LTO 35, Artex MM Para 3.7 (Transmitter self test) 21-Jul D ELT Artex 406 C406-2HM Nov M Supp insp: Annual ELT inspection, Artex Maint Manual Para Nov D ELT Battery UNK 22-Mar M ELT battery full voltage cx, DCA LTO 35, Artex MM 20-Sep D ELT Battery UNK 29-Sep Y ELT battery, OTL, Artex 406 MM Para Aug D First Aid Kit UNK UNK 19-Jul M Annual First aid kit insp 18-Jul D Expl. Cartridge Fwd UNK 30-Jun Y Expl. Cartridge Fwd, TBO 1-May D Expl. Cartridge Fwd UNK 30-Jun Y Expl. Cartridge Fwd, TBO 1-May D Engine Fire Extinguisher Nov Y Fire Extinguisher, TBO 7-Nov D Engine Fire Extinguisher Sep M Eng. Fire. Ext., Weight Chk AMM , Sep D Hand Fire Extinguisher (TOT HAL Jun Y Portable Fire Ext., OTL 22-Oct D Hand Fire Extinguisher (TOT HAL Jun Y Supp insp: container hydrostatic pressure test 22-Oct D Hand Fire Extinguisher (TOT HAL Sep M Supp insp: Fire Ext., weighing AMM , 5-1 & Sep D Fuel Pump Rhd D Jun OC OC OC Carttridge Dec H Cartrigde, TBO H Fuel Pump D Jun OC OC OC Carttridge Jul H Cartrigde, TBO H Fuel Pump Aft D Jan OC OC OC Carttridge Jul H Cartrigde, TBO H Fuel Pump D Jun OC OC OC Carttridge Jun H Cartrigde, TBO H Hydraulic Pump L290 M20A1 014 ALL 14-Sep H 800H/12M Lubrication drive shaft teething hydraulic pump, , 4-1 & , H Hydraulic Pump L290 M20A1 014 ALL 14-Sep M 800H/12M Lubrication drive shaft teething hydraulic pump, , 4-1 & , Sep D Valveblock/Reservoir L290M20A Mar ,500 H TBO H Valveblock/Reservoir L290M20A Mar ,500 H TBO H Variable Displacement PumpL290M20A Mar ,500 H TBO H Variable Displacement PumpL290M20A Mar ,500 H TBO H Pressure Supply L290M20A Mar ,500 H TBO H Pressure Supply L290M20A Mar ,500 H TBO H Hydraulic Fluid FLUID 41 N/A 14-Sep H 800H/12M Chg Hyd.Fluid, MM , H Hydraulic Fluid FLUID 41 N/A 14-Sep M 800H/12M Chg Hyd.Fluid, MM , Sep D Indicating and recording system N/A N/A 24 M Supp insp: functional test of immersion probe for H/C with FCDS, AMM , 5-3 N/A N/A Indicating and recording system 17-Dec H Supp insp: functional test fans in PELICAN rack, AMM , H Indicating and recording system 17-Dec H Supp insp: functional test fans for H/C with CPDS, AMM , H Search and Landing light 17-Dec H SIN 2313-S-33 Check routing electrical connecting Wire H HEEL system 12 M Supp insp; Chk state of charge of NC Battery, AMM ,6-2 n/a n/a HEEL system 18 M Supp. Insp: Chk power supply, recharge battery and perform cap. Chk,AMM n/a n/a HEEL system 18 M Supp. Insp: Perform functional test of immersion switch,amm ,5-1 and 5-2 n/a n/a Emergency Power Supply (S May M Supp insp: Emer. Batt Insp - JET Model PS-835 (Goodrich MM Pg 205) 21-Nov D Emergency Power Supply (S Nov M Supp insp: Emer. Batt Insp - JET Model PS-835 (Goodrich MM Pg 206) 29-Nov D Avionicx equipment N/A N/A 12-Nov M Supp insp: Insp avionics equipment 11-Nov D Pitot Static System N/A N/A 11-Nov M Supp insp: Leak Test of pitot static system, , Nov D Pitot Static System N/A N/A 11-Nov M Supp insp: Test display accuracy of pitot static system, , Nov D Pitot static system-ifr 12 M Supp insp: Drain pitot-static system, AMM , Nov D Pitot static system-ifr 12 M Supp insp: Clean pitot-static system, AMM , Nov D Air data system ADS 3000 N/A N/A 11-Nov M Supp insp: Functional Test air data system ADS 3000, , Nov D AHRS Attitude and Heading Reference System 12 M Supp insp: Compensate Attitude and Heading Reference System AHRS 10-Nov D Doors and service covers N/A N/A 17-Dec H Supp insp: Visual inspect upper arm of sliding door for cracks, , H XY fitting 11-Nov H Inspect main transmission fittings, , 6-2 (7) H Eurocopter Malaysia SDN BHD Page 3 of 7

4 Installed/Last C/W Time at install Current Engine mount fittings 3500 H Supp insp:inspect engine mount fittings, AMM ,6-2(when eng overhauled) H Engine mount fittings 4000 H Supp insp:inspect engine mount fittings, AMM , H Rear Assy L535A EVL288 1-Mar H Life Limit N/A By P/N. O/C O/C 53,50,00 ASB A-008(Fwd. RingL535A N/A 7700 H Ring Frame X 5730, SLL H 53,50,00 ASB A-008(Aft Ring F L535H FR Jun H Ring Frame X 9227, SLL H ASB A-025 once Check water drainage holes 30-Jun Stator Blades This insp. deleted.(27/02/09) This insp. deleted 50 H Inspect Root of Stator Blades for cracks MSM N/A N/A Ejectable side panes( at rear N/A N/A N/A N/A 2 Y Supp insp: Remove & install ejectable side panes(at rear of Sliding Doos), , 4-3 N/A N/A D Sliding/Fixed side panes on N/A N/A 5-Nov Y Supp insp: Remove & install, , Nov D Main rotor hub shaft L623M FRMA Dec H Supp insp: Inspect rotor hub shaft for cracks, , 6-3 N/A N/A Main rotor hub shaft L623M FRMA Dec H Supp insp: Remove & insp rotor hub shaft (with main transmission overhaul), , H Main rotor hub shaft L623M FRMA Dec H Supp insp: Remove, disassemble & insp swashplate (with main transmission overhaul), H Main rotor hub shaft L623M FRMA Dec H Supp insp: Insp swashplate bearing for rolling friction (with main transmission overhaul), H Main rotor hub shaft L623M FRMA Dec H Supp insp: Remove, disassemble & insp driving link unit, , 4-1, 4-3, H Main rotor hub shaft L623M FRMA H Condional insp ,6-8 Pg. 601 (After installation of Main Rotor Hub Shaft) H Adapter of static discharger L623M FRMA Dec H Supp insp: Visual Inspect adapter of static discharger for cracks, , H Main rotor blades (Ops witho L623M FRMA Dec H Supp insp: Remove & inspect MRB when without mast moment system, ,4-2, H Main Rotor Blade L621 M ALL 50 H Inspect PU protective film for roughness SB rev1 n/a n/a Main Rotor Blade 1 L621 M Sep H Main Rotor Blade, SLL ** H Damper L621 M LK Oct Y Damper, SLL ** 31-Aug D Damper L621 M LK Oct H Damper, SLL ** H Damper L621 M LK Oct Y Damper, SLL ** 31-Aug D Damper L621 M LK Oct H Damper, SLL ** H Main Rotor Blade 2 L621 M Jun H Main Rotor Blade, SLL ** H Damper L621 M LK Sep Y Damper, SLL ** 31-Mar D Damper L621 M LK Sep H Damper, SLL ** H Damper L621 M LK Sep Y Damper, SLL ** 31-Mar D Damper L621 M LK Sep H Damper, SLL ** H Main Rotor Blade 3 L621 M Dec H Main Rotor Blade, SLL ** H Damper L621 M LK Jul Y Damper, SLL ** 31-Mar D Damper L621 M LK Dec H Damper, SLL ** H Damper L621 M LK Jul Y Damper, SLL ** 31-Mar D Damper L621 M LK Dec H Damper, SLL ** H Main Rotor Blade 4 L621 M Dec H Main Rotor Blade, SLL ** H Damper L621 M10T Oct Y Damper, SLL ** 30-Jun D Damper L621 M10T Dec H Damper, SLL ** H Damper L621 M10T Oct Y Damper, SLL ** 30-Jun D Damper L621 M10T Dec H Damper, SLL ** H Blade bolt L621 M May H Blade bolt, SLL ** H Blade bolt L621 M May H Blade bolt, SLL ** H Blade bolt L621 M May H Blade bolt, SLL ** H Blade bolt L621 M May H Blade bolt, SLL ** H Blade bolt L621 M May H Blade bolt, SLL ** H Blade bolt L621 M May H Blade bolt, SLL ** H Blade bolt L621 M May H Blade bolt, SLL ** H Blade bolt L621 M May H Blade bolt, SLL ** H Swashplate L623 M A027Z 18-Sep OC OC OC Cardan Ring L623 M A027ZN 18-Sep H Cardan Ring, SLL H Bearing Ring L623 M Sep OC OC OC Swashplate Bearing L623 M UNK 14-Sep H 400H/12M Lubricate Swashplate Bearing, AMM , H Swashplate Bearing L623 M UNK 14-Sep M 400H/12M Lubricate Swashplate Bearing, AMM , Sep D Ring (on control ring) L623 M A027ZN 18-Sep H Ring, SLL H Ring (on bearing ring) L623 M A027ZN 18-Sep H Ring, SLL H Bolt (on control ring) L671 M A027ZN1 18-Sep H Ring, SLL H Bolt (on control ring) L671 M A027ZN2 18-Sep H Ring, SLL H Bolt (on sliding sleeve) L623 M A027ZN1 18-Sep H Ring, SLL H Bolt (on sliding sleeve) L623 M A027ZN2 18-Sep H Ring, SLL H Main Transmission Dec H Supp insp: Interim Inspection by manufacturer H Main transmission mounts After each MGB removal Supp insp: Insp fittings of main transmissions mounts, , 6-2 c/o c/o Torque strut preassy 13-Dec H Supp insp: Remove & inspect torque strut preassy, , 4-1 & H Drive shafts 13-Dec H Supp insp: Remove & inspect drive shafts, , 4-1 & H Eurocopter Malaysia SDN BHD Page 4 of 7

5 Installed/Last C/W Time at install Current Drive shafts 13-Dec Y Supp insp: Remove & inspect drive shafts, , 4-1 & Dec D Drive shafts 13-Dec H Supp insp: Remove & Inspect spacer tube, , 4-3, 4-5, H Gearbox cover with Y-strut Dec H Cover, SLL ** H Main Transmission Dec H Main Gear Box, TBO H Main Transmission Mar H 600H/12M MGB, Oil Change, AMM , H Insert oil type if Main Transmission ZFN L3001 OIL Mar M 600H/12M MGB, Oil Change, AMM , Mar D Main Transmission ZFL L3001 OIL Aug H MGB Oil Change, AMM , 3-1 c/o c/o H Main Transmission Aug H MGB Oil Change and SOAP only after TBO/TSN/TSR, AMM , 3-1 c/o c/o H ASB 63A-012 R Mar H SOAP between 90fh and 100fh i.a.w SB63A-012 Analysis must be performed within 25 fh H Main Transmission ZFL L3001 OIL Aug H A toothing inspection on the freewheel unit and MGB iaw section 3C of the ASB 63A-012 is required c/o c/o H Main Transmission Oct once only 150 H Insp. Of Driving Unit iaw AMM , 6-1, para 3 c/o c/o Main Transmission Dec once only 400 H Insp. Of Driving Unit iaw AMM , 6-1, para 3 c/o c/o H AD EU Oct H AD EU (ASB 63A-017 Para 3.B.2(b)) H AD EU Nov M AD EU (ASB 63A-017 Para 3.B.2(a)) c/o c/o D to be c/o with M Upper Housing Dec H Upper Housing, SLL ** H Lower Housing Dec H Lower Housing, SLL ** H Support Tube Dec H Support Tube, SLL ** H Intermediate Shaft LH Sep H Intermediate Shaft, SLL ** H Intermediate Shaft RH Dec H Intermediate Shaft, SLL ** H Bevel Gear LH Sep H Bevel Gear, SLL ** H Bevel Gear RH Dec H Bevel Gear, SLL ** H Pinion Shaft Dec H Pinion Shaft, SLL ** H Pinion Dec H Pinion, SLL ** H Input Pinion LH Sep H Input Pinion, SLL ** H Input Pinion RH Sep H Input Pinion, SLL ** H Collector Wheel Dec H Collector Gear, SLL ** H Collector Shaft Dec H Collector Shaft, SLL ** H Rotor Brake Fluid UNK N/A 8-Dec H 800H/3Y Change Brake Fluid, MM , H Rotor Brake Fluid UNK N/A 8-Dec Y 800H/3Y Change Brake Fluid, MM , Dec D Rotor Brake System UNK N/A 8-Dec H Supp insp: Insp rotor brake system, , H Tail Rotor Head L642 A M May OC OC OC Tail Rotor Head L642 A M 1299 N/A, cargo hook not fitted 800 H Supp insp: Insp laminated tension-torsion bar, , 4-1, 4-3, 6-3, 6-10 N/A N/A Tail Rotor Head L642 A M Aug H Supp insp: Insp tail rotor, ,4-1, 4-3,6-1,6-2,6-4 to H Tail Rotor Head L642 A M Aug Y Supp insp: Insp tail rotor, ,4-1, 4-3,6-1,6-2,6-4 to Aug D Tail Rotor Blade L642 A M Aug H Blade, SLL ** H Tail Rotor Blade L642 A M Jun H Blade, SLL ** H Tail Rotor Blade L642 A M Aug H Blade, SLL ** H Tail Rotor Blade L642 A M Jun H Blade, SLL ** H Tail Rotor Blade L642 A M Jun H Blade, SLL ** H Tail Rotor Blade L642 A M Jun H Blade, SLL ** H Tail Rotor Blade L642 A M Jun H Blade, SLL ** H Tail Rotor Blade L642 A M Jun H Blade, SLL ** H Tail Rotor Blade L642 A M Jun H Blade, SLL ** H Tail Rotor Blade L642 A M Jun H Blade, SLL ** H Splined flange L642A PRD Mar H Splined flange, SLL H Shaft Long Assy L651 M Jun OC OC OC T/R Drive - Long Drive Shaft 30-Sep once or every 25H 100 H ASB 65A-004 R0 - check of sealing washers c/o c/o H Tail Rotor Drive Shaft only after initial 800 H insp. 100 H Cx radial deflection (800TSN then 100 TSI) Supp Insp Pg H Tail Rotor Drive Shaft 3-Sep H Cx radial deflection (800TSN then 100 TSI) Supp Insp Pg H Tail Rotor Drive Shaft 30-Jun H Supp insp: remove & insp TRDS, AMM , 4-1, 4-2, 4-3, 4-5, H Tube L651 M Jun H Tube, SLL H Coupling part L651 M Jun H Coupling flange, SLL H Coupling part L651 M Jun H Coupling flange, SLL H Shaft (Aft) L651 M Jun OC OC OC Adapter L651 M CN 05/ Jun OC OC OC Eurocopter Malaysia SDN BHD Page 5 of 7

6 Installed/Last C/W Time at install Current Adapter L651 M CN 05/ Jun OC OC OC Tube L651 M Jun OC OC OC Shaft (Fwd) L651 M Jun OC OC OC Adapter L651 M CN 05/ Jun OC OC OC Adapter L651 M CN 05/ Jun OC OC OC Tube L651 M Jun OC OC OC Tail Rotor Transmission L652 A M May H Tail Rotor Transmission, TBO H Tail Rotor Transmission L652 A M May H Supp insp 1200H/3Y: remove & insp TRTM, , 4-1,4-3, H Tail Rotor Transmission L652 A M May Y Supp insp 1200H/3Y: remove & insp TRTM, , 4-1,4-3, May D Tail Rotor Transmission L652 A M 1029 N/A, input drive flange P/N L652A not installed 1200 H Supp insp 1200H/3Y: insp TRTM, , 6-1 N/A N/A Tail Rotor Transmission L652 A M Jun H 400H/12M TRTM, Oil Change , H Tail Rotor Transmission NYCOLUBE 3525 M Jun M 400H/12M TRTM, Oil Change , Jun-11 1 D input Gear Wheel L652 A M 46 1-May H Pinion, SLL ** H output Gear Wheel L652 A M May H Wheel, SLL ** H Equiped gear box housing L652 A ML May OC OC OC OC Wheel bearing 7050 A May OC OC OC OC Gear bearing 7050 A May OC OC OC OC Control rod bearing 7050 A May OC OC OC OC Main Rotor Actuator L673M20A May H TR Actuator - TBO H Main Rotor Actuator(LongitudL673M20A May H TR Actuator - TBO H Main Rotor Actuator(Lateral AL673M20A May H TR Actuator - TBO H Main Rotor Actuator(CollectivL673M20A May H TR Actuator - TBO H T/R Actuator(Fenestron Serv L673M40A Dec H TR Actuator - TBO H Tail Rotor Control 30-Jun H Supp insp:adjust boosted sect, , H Rotor Flight Control 14-Sep M Insp. control rods for cracks(as far as they are accessable without being removed) 13-Sep D Mixing lever gear unit L671 M UNK Installed n/a n/a Mixing lever gear unit L671 M UNK 30-Jun H Supp insp: remove & inspect mixing lever gear unit, AMM , 4-1, H Forked Lever L671 M Jun H Forked Lever, SLL ** H Hinged Support L671 M CN 05/ Jun H Hinge Support, SLL ** H Bolt L671 M CN 05/ Jun H Bolt, SLL ** H Control rod L671 M CN 05/ Jun H Control rod, SLL ** H Control Rod - Ball pivot N/K 28-Mar H Insp. Iaw EC135-67A-017/AD c/o every 100H H Housing E / 91 UNK 30-Jun H Housing, SLL ** H Starter Generator RH Aug H Starter Generator, TBO H This component Starter Generator LH Jan H Starter Generator, TBO H INLET BARRIER FILTER N/I N/I N/I N/I N/I N/I N/I N/I N/I N/I N/I 72L LH ENGINE 72L Engine PW206B2 PCE-BJ May Installed n/a n/a 72L Engine mounts PW206B2 PCE-BJ 0268 After each engine removal Supp insp: Insp fittings of engine mounts, , 6-2 c/o c/o 72L Engine PW206B2 PCE-BJ Dec H Power Ass. Cx. (Interval iaw Flight Manual) H Engine PW206B2 PCE-BJ Mar H 200H insp - Insp.P3 Fitting i.a.w. P&WC MM H 72L Engine PW206B2 PCE-BJ Dec H 800 Hrs Engine Inspection H 72L Engine PW206B2 PCE-BJ Dec M 12 Mth Engine Inspection 16-Dec D 72L Engine PW206B2 PCE-BJ Dec H P&WC SB R3: Replacement of Fuel Nozzle H 72L Engine SB A28280 R3 PCE-BJ 0113 one time P&WC SB A28280 R4 [CF R1] : Compressor turbine disc insp. & retaining nut replac c/o c/o 72L Engine SB R1 PCE-BJ Dec one time P&WC SB R1: Inspection of Gas-Generator Fire Detector ( c/o c/o Engine PW206B2 PCE-BJ Mar one time P&WC SB A28293R1 Insp. Of P3 Fitting c/o c/o 72L Engine PW206B2 PCE-BJ 0113 n/a, no oil change for PW206B2 Engine oil change n/a n/a 72L Reduction Gearbox Module RGB-BJ Jun H Reduction Gearbox Module, TBO H 72L Reduction Gearbox Module RGB-BJ Jun H Reduction Gearbox Module, TBO SB R H 72L Turbomachinery Module TM-BJ Jun H Turbomachinery Module, TBO H 72L Turbomachinery Module TM-BJ Jun H PW R H 72L Turbomachinery Module TM-BJ Jun H PW PW H 72L Compressor Turbine Disc A 001 AC3K 30-Jun ,641 10,000 C C.T. Disc, Life Limit 10,000 8,359 C 72L Power Turbine Disc A 001 BD80 30-Jun ,597 15,000 C P.T. Disc, Life Limit 15,000 13,403 C 72L Impeller A 001 AOCW 30-Jun ,037 15,000 C Impeller, Life Limit 15,000 13,963 C 72.73L.21.10Fuel Management Module Jun H Fuel Management Module, TBO H 72R RH ENGINE 72R Engine PW206B2 PCE-BJ May Installed n/a n/a 72R Engine mounts PW206B2 PCE-BJ 0268 After each engine removal Supp insp: Insp fittings of engine mounts, , 6-2 c/o c/o Eurocopter Malaysia SDN BHD Page 6 of 7

7 Installed/Last C/W Time at install Current 72R Engine PW206B2 PCE-BJ Dec H Power Ass. Cx. (Interval iaw Flight Manual) H Engine PW206B2 PCE-BJ Mar H 200H insp - Insp.P3 Fitting i.a.w. P&WC MM H 72R Engine PW206B2 PCE-BJ Dec H 800 Hrs Engine Inspection H 72R Engine PW206B2 PCE-BJ Dec M 12 Mth Engine Inspection 16-Dec D 72R Engine PW206B2 PCE-BJ Dec H P&WC SB R3: Replacement of Fuel Nozzle H 72R Engine SB A28280 R3 PCE-BJ 0114 one time P&WC SB A28280 R4 [CF R1] : Compressor turbine disc insp. & retaining nut replac c/o c/o 72R Engine SB R1 PCE-BJ Dec one time P&WC SB R1: Inspection of Gas-Generator Fire Detector ( c/o c/o Engine PW206B2 PCE-BJ Mar one time H P&WC SB A28293R1 Insp. Of P3 Fitting c/o c/o 72R Engine PW206B2 PCE-BJ 0114 n/a, no oil change for PW206B2 Engine oil change n/a n/a 72R Reduction Gearbox Module RGB-BJ Jun H Reduction Gearbox Module, TBO H 72R Reduction Gearbox Module RGB-BJ Jun H Reduction Gearbox Module, TBO SB R H 72R Turbomachinery Module TM-BJ Jun H Turbomachinery Module, TBO H 72R Turbomachinery Module TM-BJ Jun H PW R H 72L Turbomachinery Module TM-BJ Jun H PW PW H 72R Compressor Turbine Disc A 001 AC3T 30-Jun ,614 10,000 C C.T. Disc, Life Limit 10,000 8,386 C 72R Power Turbine Disc A 001 BE9H 30-Jun ,603 15,000 C P.T. Disc, Life Limit 15,000 13,397 C 72R Impeller A 001 AK07 30-Jun ,024 15,000 C Impeller, Life Limit 15,000 13,976 C 72.73R.21.10Fuel Management Module Jun H Fuel Management Module, TBO H Engine fuzz burner system N/A N/A 12 M Supp insp: Inspect engine fuzz burner system, , 6-1 N/A N/A Eurocopter Malaysia SDN BHD Page 7 of 7