DS9 Document EFTA01084848

Bell 430 Single Pilot IFR Equipment • Retractable Undercarriage • Pilot and Co-pilot Brakes • Dual Controls • Air Conditioning • VIP Step R/H passenger side • Particle Separator • Bleed Air Environmental Control System • Cockpit Boost Fan for ECS • Dual Flight Controls • Retractable Wheel Gear • Co-Pilot Wheel Brakes • Shadin Fuel Flow Indicators on IIDS • 48 Gal. Auxiliary Fuel Tank • Heated Glass Windshield • Ice/Refreshment Drawers • Wool Carpet • Custom cockpit storage • Quiet Zone Interior • Engine Plugs and Covers • Forward recognition lights with pulse • Whelen Strobe Light System with end lights on horizontal stabilizer • LED Lower Anti-Collision light • Devore tail rotor floodlight system • Dual Pane Windows • Thermal/Acoustic Insulation System for soundproofing cabin. • Cabin door activated overhead dome lights Pil PremiAir Aircraft Details Serial Number: Registration: Manufacturer Date: Total Time Airframe: Location: 49078 N901RL 2001 1,660 hrs @ Jan 2010 UK Exterior / Interior Flag blue exterior with Gold accent stripes. Cream leather upholstery in a 5 seat configuration with cabinet bar (Edwards & Associates interior). No known damage history Avionics • Avionics Master Switch • Gold Crown Wiring Harness • Dual AFCS w/Flight Director • Four Tube EFIS • Dual King Gold Crown KTR-908 • Dual Nav KNR-634 • DME KDM-706 • Garmin GNS 500 • ADF KDF 806 • Transponder MST-67A • PS Engineering PAC 24 Audio Panel • RDR 2000 Weather Radar • Radar Altimeter • ELT- 406 mhz • Standby Attitude Ind. 3" • Honeywell KTA870 TAS System • Bose Headsets Engines Two Allison 250-C408 engines The otter for safe of this aircraft is sullect to contract and the aircraft may at any time be vothdrmyn from the mother without prior notice Specification is subject to verification by the purchaser For further information. please contact PremiAir Global on or email PrenuAu Global Business Aviation Centre Farnborough Airport Farnborou h Ham shim Gum 6XA Onded Kingdom. Tel: Far I MEmail: err ininviorermairciobal corn Registered Address PremiAir Aircraft Sales Ltd Sixth Floor 90 Fetter Lane London EC4A 1PT No: 6637055 EFTA01084848 NPremiAir Globat Bell 430 S/N 49078 Major Component / Engine Status COMPONENT SLUTS° (hrs) I Time Remaining Time Remaining (hrs) j (%) Main Rotor Blade x .1 On Condition Main Rotor Yoke SO Cs° I 3.340 Main Rotor Mast Assembly 5.000 3.340 Main Rotor Swash Plate 5,000 i 3.340 Main Drive Shaft Left & A t'7 5 Finn 5IS t yr 3r-nt is Transmission 5,000 I 3.340 Tail Gearbox 5.000 3.340 Tad Rotor Hub 2,500 I 2,197 87", Tail Rotor Blade 5.000 4.320 86"0 Rotor Ellade t.. , • 5,000 5,000 100% Tail Rotor Yoke 5.000 3.340 66nx ENGINES L Engine #1 1 Engine #2 SLL/TBO Remaining Remaining Remaining (hrs) (hrs) (%) (hrs) 15* Stage Turbine Wheel I 1,775 1 1,726 97% 1.726 2.- Stage Turbine Wheel 1,775 1.726 97% 1.726 3rd Stage Turbine Wheel I 2,890 64% I 2,890 Li Stage Turbine Wheei Engine Gearbox Compressor Bleed Valve Starter Generator :4;3:.11/ 0 rn. On Condition 1.50c 1.000 5,857 78% 340 17% 747 320 24% 32% 5.840 345 I la 930 66 25- x 66% Remaining (%) 97% 1 97', 64% 93% The offer for sale of this aircraft is setyea to contract and the aircraft may at any time be withdrawn (torn rho MA Ihout prior notice Specification ,s sublect to ventication by the perches& Premihr Global Business Aviation Centre Farnborough AirpOrt Farnborough Hampshire G014 6XA United Kingdom. Tel Fax = mail Web. hiwittoreceiairglobaloom Registered Address: PremiAir Airerah Sales Ltd Sixth Floor 90 Feller Lane London EC4A IPT No: 6637055 EFTA01084849 PremiAir Aircraft Engineering Ltd Aircraft Compliance Report Aircraft: N901RL Make/Model: BELL 430 Serial No: 49078 11$1,7010 hat 13:41:35 Page MCN 2430-0000 PN TSP-283 SN 10801683 Desc BATTERY ATA 24-30.00 DC GENERATION Position N/A Condition SERVICEABLE NOTE: Calendar based on Overhaul. MCN 2620-1000 PN 222.369-911-001 SN A37870A1 Desc CONTAINER, ENG. FIRE ATA 26-20-00 FIRE EXTINGUISHING Position LEFT Condition SERVICEABLE NOTE: Calendar based on Overhaul. MCN 2620-2000 PN 222.369-911.001 SN 38013A1 Desc CONTAINER, ENG. FIRE ATA 26-20-00 FIRE EXTINGUISHING Position RIGHT Condition SERVICEABLE NOTE: Calendar based on Overhaul. MCN 6200-1050 PN SN Desc ATA Position BLUE Condition NEW 430.010.411-105 TY0350 LINK, MR PITCH 62-00-00 MAIN ROTORS MCN 6200.2050 PN 430.010-411-105 SN TY0351 Dose LINK. MR PITCH ATA 62-00-00 MAIN ROTORS Position ORANGE Condition NEW Hours Current Airframe as of 28/09/2009 1660:00 Customer. BOVALE DEVELOPMENTS Cycles Landings 0 0 Component Times Curren Battery CAP check Since O H 01/10/2039 Calendar Overhaul Wa Hours Cycles Landings rya 4'a Airframe - Intervals Tolerance Last Done Next Due Remaining 4M Na Na Na fire Extinguisher Cor tamer - Left. Hydro check. Data reference: BHT-430-MM-3. Since OM 01/03/2C Calendar Overhaul 1660 l Hours r a Cycles I-7a Landings by ‘i 06/10/2009 1660:00 Na Na 01/03/2005 Na Na Na Fire ExtIngUISher Container - Right. Hydro check. Data reference: BHT-430-MM-3. Since OH 01/03/2055 Calendar Overhaul 5Y 1660:00 Hours Na ; ha Cycles Na Landings Na Main Rotor Pitch Link Since New ria 1660± Main Rotor Pitch Link. Since New n'a 1660:00 rva Calendar Hours Cycles Landings Retirement Na 10000:00 Na Na Calendar Retirement Hours Cycles Landings Na 10000:00 Na n/a 01/03/2005 Na Na Na 02/04/2001 Na Na Na 02/04/2001 Na Na n/a 01/02/2010 Na Na Na 01/03/2010 Na Na Na 01/03/2010 Na Na Na Na 10000:00 Na Na n/a 10000:00 Na Na 21d n/a Na Na 1m 21d Na Na Na 1m 21d Na Na Na Na 8340:00 Na Na Na 8340:00 Na Na AvaSt SYSIEYS tr.0 EFTA01084850 PremiAir Aircraft Engineering Ltd Aircraft Compliance Report Current Airframe as of 28/09/2009 1660:00 Hours Cycles Landings 0 0 Aircraft: f4901RL Customer. IOVALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component 77ntes Airframe ammo: II/DI/2010 Tin*: 134145 Par" 2 Current; Intervals Tolerance Last Done Next Due Remaining MCN 6200-3050 PN 430-010-411-107 SN TY0344 Dose LINK, MR PITCH ATA 62-0000 MAIN ROTORS Position RED Condition NEW MCN 6200-4050 PN 430-010-411-107 SN TYD343 Desc LINK, MR PITCH ATA 62-00-00 MAIN ROTORS Position GREEN Condition NEW Main Rotor Pitch Link.: Since New Ka Calendar Retirement Na 02104/2001 Na nra 1660:0) Hours 10000:00 Na 10000:00 8340:00 NA Cycles Na Na Na Na nta Landings rile ilia nta iva Mein Rotor Pitch Link. Since New n a Calendar Retirement Na 02/04/2001 Na n/a 1660:03 Hours 10000:00 Na 10000:00 8340:00 ma Cyclos Na Na n/a Na rya Landings Na Na Na Na MCN 6210-1000 Main Rotor Blade. PN 430-015.001.123 SN A-1265 Desc BLADE, MAIN ROTOR ATA 62-10.00 MAIN BLADES Position BLUE Condition NEW MCN 6210-2000 PN 430-015.001.123 SN A-I248 Dose BLADE. MAIN ROTOR ATA 62-10-00 MAIN BLADES Position ORANGE Condition NEW MCN 6210-3000 PN 430.015.001-123 SN A-1229 Dose BLADE. MAIN ROTOR ATA 62-10.00 MAIN BLADES Position RED Condition NEW On Condition 02/04/2001 Calendar Na 02/04/2001 n/a Na 166010 Hours n/a Na ilia Na Cycles Na Landings Na LN Na n/a Na Na Na Na Main Rotor Blade. On Condition 02,04/2001 Calendar Na 02/04/2001 Na Na 1660:C0 Hours Na Na Na Na 3 Cycles Na Na Na Na 0 Landings n/a Na n/a Na Main Rotor Blade, On Condition 02/04/20,61 Calendar Na 02/04/2001 Na Na 166040 Hours Na Na Na Na ,0 Cycles Na n/a Na Na 0 Landings Na Na Na Na Av•13ASE STSIEmS Inc • 13 EFTA01084851 PremiAir Aircraft Engineering Ltd Aircraft Compliance Report Hours Cycles Landings Current Airframe as of 28/09/2009 1660:00 0 0 Aircraft: N901RL Customer )VALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component Times Airframe Pr/Med:114)MM Tkne: 13.41:35 Page: 3 Curren. Intervals Tolerance Last Done Next Due Remaining MCN 6210-4000 MaIn Rotor Blade. PN 430-015-001-123 On Condition 02/04/2(01 Calendar Na 02/04/2001 n/a Na SN A-1249 Den BLADE, MAIN ROTOR 1660:00 Hours Na Na n/a Na ATA 62-10-00 MAIN BLADES 0 Cycles Na Na Na Na Position GREEN 0 Landings n/a Na Na Na Condition NEW MCN 6220-0450 Main Rotor Drive Plat). PN 430-010-126-105 Since Thep tia Calendar inspection Na 3010612009 Na Na SN A-000181 Dose PLATE, MR DRIVE 4910 Hours 10000:00 1611:00 11611:00 9951:00 ATA 62-20-00 MAIN HEADS r io Cycles Na Na Na n/a Position ONLY 612 Landings Na Na Na Na Condition NEW MCN 6220-1050 Main Rotor Blade Pin PN 430.010-127-101 Since New la Calendar Retirement Na 02/04/2001 Na Na SN A-0834 Dose PIN, MR BLADE 1660. iC Hours 10000:00 Na 10000:00 8340:00 ATA 62-20-00 MAIN HEADS Position #1 r'i, r ',7, Cycles Landings Na Na n/a Na Na Na n/a Na Condition NEW MCN 6220-1060 Main Rotor Blade Pin. PN 430-010-127.101 Since New iv a Calendar Retirement Na 02/04/2001 Na Na SN A-0871 Dew PIN, MR BLADE 1660 :/0 Hours 1000000 Na 10000:00 13340:00 ATA 62-20-00 MAIN HEADS Ca Cycles Na Na Na n/a Position II r:a Landings Na Na Na Na Condition NEW MCN 6220-1100 Main Rotor Adapter. PN 430.010.109.101 Since New Calendar Retirement Na 02/04/2001 n/a Na SN A-378 Desc ADAPTER, MR BLADE 1660:40 Hours 10000:00 Na 10000:00 8340:00 ATA 62-20.00 MAIN HEADS a Cycles Na n/a Na Na Position #1 a Landings Na Na Na Na Condition NEW AV-SASE SVSTOrS - 13 EFTA01084852 PremiAir Aircraft Engineering Ltd Hours Cycles Landings Aircraft Compliance Report Current Airframe as of 28/09/2009 1660:00 0 0 Aircraft: N901RL Customer: LOVALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component Times Airframe Previa): I T0V2010 Time: O:41:35 Page: a Current Intervals Tolerance Last Done Next Due Remaining MCN 6220-1150 Main Rotor Pitch Horn. PN 430-010-115.101 Since New Na Calendar Retirement rveri 02/04/2001 Na n/a SN A-381 Dose HORN, MR PITCH 1660:C.0 Hours 10000.00 n/a 10000:00 8340:00 ATA 62-20-03 MAIN HEADS Na Cycles n/a Na n/a Position #1 rt a Landings Na Na Na Na Condition NEW MCN 6220-1200 PN 430-310-104-105 SN LK0487 Desc DAMPER BLADE SET ATA 62-20-00 MAIN HEADS Position #1 Condition NEW MCN 6220-1250 PN 430310.101.107 SN LK1360 Desc RESTRAINT. MR SHEAR ATA 62-20-00 MAIN HEADS Position #1 Condition NEW MCN 6220-1300 PN 430-010-105-105 SN A-556 Desc PLATE SET. CLAMP ATA 62-20-00 MAIN HEADS Position #1 Condition NEW MCN 6220-1350 PN 430-010-124-103 SN A-304 Dose BUSHING. MR DRIVE ATA 62.20.00 MAIN HEADS Position #1 Condition NEW Main Rotor Damper Blode Set. Since New r a Calendar Retirement n/a 02/04/2001 n/a ilia 1660 1 5 Hours 10000:0D Na 10000:00 8340:00 n a Cycles Na Na n/a Na n a Landings Na Na n/a Na Main Rotor Shear Res;raint. Since New r /a Calendar Retirement n/a 25110/2005 Na Na 750:c:8 Hours 10000:00 909:12 10909:12 9249:12 n a Cycles Na Na Na Na n 'a Landings Na n/a Na nia Main Rotor Clamp Pie a Set. Since New r !a Calendar Retirement Na 02/04/2001 Na Na 166010 Hours 10000:00 Na 10000:00 8340:00 n'a Cycles Na n/a n/a Na n'a Landings n/a Na ilia Na Main Rotor Drive Ousbina. Since New r /a Calendar Ftetiretnent Na 02/04/2001 Na n/a 1660:00 Hours 5000:00 Na 5000:00 3340:00 rasa Cycles Na Na n/a Na nia Landings Na Na n/a Na Av•BASE SYSTEMS PC 13 EFTA01084853 PremiAir Aircraft Engineering Ltd Aircraft Compliance Report Hours Cycles Landings Current Airframe as of 28/09/2009 1660:00 0 0 Aircraft: N901RL Customer: BOVALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 4. Component Times Airframe Primed: N/01/20W TIM: 13W:3S Page. 5 Curreri Intervals Tolerance Last Done Next Due Remaining MCN 6220-1360 Main Rotor Drive Buthinat PN 430-010-124-103 Since Now. rva Calendar Retirement Na 02/04/2001 Na Na SN A-308 Desc BUSHING, MR DRIVE 1660 00 Hours 5000:00 Na 5000:00 3340:00 ATA 62.20-00 MAIN HEADS t/a Cyclos Na Na Na Na Position #1 .Va Landings n/a Na Na Na Condition NEW MCN 6229-1500 PN 430-010-101.101 SN A-173 Desc YOKE. MAIN ROTOR ATA 62-20-00 MAIN HEADS Position UPPER Condition SERVICEABLE MCN 6220-2050 PN 430-010.127-101 SN A-0823 Desc PIN. MR BLADE ATA 62.20-00 MAIN HEADS Position #2 Condition NEW MCN 6220-2060 PN 430-010-127.101 SN A-0839 Desc PIN. MR BLADE ATA 62.20-00 MAIN HEADS Position #2 Condition NEW MCN 6220-2100 PN 430-010.109-101 SN A-373 Desc ADAPTER. MR BLADE AM 62.20-00 MAIN HEADS Position #2 Condition NEW Main Rotor Yoke - Dam On Condition Calendar Na 02/04/2001 Na Na 1660 00 Hours Na Na Na Na 0 Cycles Na Na Na Na 0 Landings Na Na Na Na Main Rotor Blade Pin Since New va Calendar Retirement Na 02/04/2001 Na Na 1660:10 Hours 10000:00 Na 10000:00 8340:00 i /a Cycles Na Na Na Na r ta Landings Na Na Na Na Main Rotor Blade Pin Since New Calendar Retirement Na 02/04/2001 Na n/a us;)(: >1 Hours 10000:00 Na 10000:00 8340:00 i , Cycles Na Na Na Na r s Landings Na n/a Na Na Main Rotor Adaoter Since New Na Calendar Retirement Na 02/04/2001 Na Na 1660:00 Hours 10000:00 Na 10000:00 8340:00 Na Cycles Na Na Na Na a Landings Na n/a Na Na EFTA01084854 PremiAir Aircraft Engineering Ltd Aircraft Compliance Report Aircraft: N901 RL Make/Model: BELL 430 Serial No: 49078 Printed: 11 er 2010 17nm:13:41:36 MCN 6220-2150 PN 430.010-115-101 SN A-393 Desc HORN. MR PITCH ATA 62-20-00 MAIN HEADS Position 62 Condition NEW MCN 6220.2200 PN 430-310.104-105 SN LK0462 Dose DAMPER BLADE SET ATA 62-20-00 MAIN HEADS Position 02 Condition NEW Page: 6 MCN 6220.2250 PN 430-310-101.107 SN LK1312 Desc RESTRAINT. MR SHEAR ATA 62-20-00 MAIN HEADS Position e2 Condition NEW MCN PN SN Desc ATA 62-20-00 MAIN HEADS Position ft2 Condition NEW 6220-2300 430-010.105-105 A-550 PLATE SET. CLAMP MCN PN SN Dose ATA Position Condition NEW 6220-2350 430-010-124-103 A-271 BUSHING. MR DRIVE 62-20-00 MAIN HEADS #2 Hours Cycles Landings Current Airframe as of 28/09/2009 1660:00 3OVALE DEVELOPMENTS 0 0 Current Main Rotor Pitch Horn, Since New nMa 1660:00 n.•a Component Times Intervals Calendar Retirement Hours Cycles Landings Main Rotor Damper BI ide Set. Since New Calendar Retirement I 660 ' Flours Cycles Landings Main Rotor Shear Res mint. Since New Calendar Hours Cyc'es Landings 750:48 a Main Rotor Clamp Pla e Set. Since New Retirement Calendar Retirement 1660 ( ( Hours Cycles Landings nx Main Rotor Drive Buslast, Since New r✓a 1660:$0 a 18 Calendar Retirement Hours Cycles Landings Na 10000:00 Na Na Na 10000:00 Na Na Na 10000:00 Na Na Na 10000:00 Na Na Na 5000:00 Na Na Tolerance Airframe Last Done Next Due 02/04/2001 Na Na Na 02/04/2001 Na Na Na 25/10/2005 909:12 Na Na 02/04/2001 Na Na Na 02/04/2001 Na Na Na n/a 10000:00 Na Na Na 10000:00 Na Na Na 10909:12 Na Na Na 10000:00 Na n/a Na 5000:00 Na Na Remaining Na 8340:00 Na Na Na 8340:00 Na Na Na 9249:12 Na Na n/a 8340:00 Na Na Na 334000 Na Na ♦VBSSE StS7E450.0 EFTA01084855 PremiAir Aircraft Engineering Ltd Aircraft Compliance Report Hours Cycles Landings Current Airframe as of 28/09/2009 1660:00 0 0 Aircraft: N901RL Customer: I3OVALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component Times Airframe Printed: II/MOW Tane:13.41:38 Page: 7 Currer t Intervals Tolerance Last Done Next Due Remaining MCN 6220-2360 Main Rotor Drive Bus Nine. PN 430-010.124-103 SN A-3O1 Desc BUSHING. MR DRIVE ATA 62-20-00 MAIN HEADS Position 02 Condition NEW MCN 6220-2500 PN 430-010.101.101 SN A-168 Den YOKE. MAIN ROTOR ATA 62-20-00 MAIN HEADS Position LOWER Condition SERVICEABLE MCN 6220-3050 PN 430-010-127-101 SN A-O882 Desc PIN. MR BLADE ATA 62.20-00 MAIN HEADS Position #3 Condition NEW MCN 6220-3060 PN 430-010.127-101 SN A-O869 Desc PIN, MR BLADE ATA 62-20-00 MAIN HEADS Position 113 Condition NEW MCN 6220-3100 PN 430-010-109-101 SN A-535 Dosc ADAPTER. MR BLADE ATA 62-20-00 MAIN HEADS Position #3 Condition NEW Since New 1660 00 Calendar Retirement Hours Cycles Landings Na 02/04/2001 Na Na 5000:130 n/a 5000:00 3340:00 Na n/a Na Na Na Na Na Na Main Rotor Yoke • Lover. On Condition Calendar Na 02/04/2001 n/a n/a 1660 )0 Hours Na Na Na Na 0 Cycles Na n/a Na Na 0 Landings Na Na n/a Na Main Rotor Blade Pin Since New va Calendar Retirement Na 02/042001 n/a n/a 1660: Xi Hours 10000:00 Na 10000:00 8340:00 Cycles Na Na Na Na I is Landings Na Na Na Na Main Rotor Blade Pin Since New t).1 a Calendar Retirement Na 02/04/2001 Na Na 1660- X Hours 10000:00 Na 10000:00 8340:00 i ,i. Cycles Na Na Na Na I PZ. Landings Na Na Na Na Main Rotor Adapter. Since New Calendar Retirement Na 02/04/2001 Na Na i 66O:CC Hours 1000000 Na 10000:00 8340:00 Cycles Na n/a Na Na r 'a Landings Na Na Na Na Ai &St.( 'AVA AA: I". EFTA01084856 PremiAir Aircraft Engineering Ltd Aircraft Compliance Report Aircraft: N901RL Make/Model: BELL 430 Serial No: 49078 Printed: 111972070 time: 73:41:36 Page: MCN 6220-3150 PN 430-010-115-101 Customer: SOVALE DEVELOPMENTS Component 8 Main Rotor Pitch Horn. Times Intervals Tolerance Retirement Na — Last Done 02/04/2001 Akfrturre Next Due Remaining Na Na Since New rVa Calendar SN A-363 Desc HORN, MR PITCH 1660:C0 Hours 10000:00 Na 1000090 834090 ATA 62-20-00 MAIN HEADS Na Cycles rea Na Na Na Position 03 n a Landings Na Na Na Na Condition NEW MCN 6220-3200 Main Rotor Damper BlaSbi a PN 430-310-104-105 Since New tiro Calendar Retirement Na 02/04/2001 Na Na SN LK0471 Desc DAMPER BLADE SET 1660-.0 0 Hours 10000:00 n/a 10000:00 8340:00 ATA 62-20.00 MAIN HEADS n a Cycles Na Na Na Na Position 03 n a Landings Na Na Na Na Condition NEW MCN 6220-3250 Main Rotor Shear Res raint. PN 430.310-101.107 Since New Calendar Retirement Na 25✓10/2005 Na n/a SN 11(1322 Desc RESTRAINT, MR SHEAR 750.'8 Hours 10000:00 909:12 10909:12 9249:12 ATA 62-20-00 MAIN HEADS n'a Cycles Na Na Na Na Position 03 n'a Landings Na n/a Na Na Condition NEW MCN 6220-3300 Main Rotor Clamp Plate Set. PN 430-010.105.105 Since New r/a Calendar Retirement Na 02/04/2001 Na Na SN A-529 Dew PLATE SET. CLAMP 1660:00 Hours 10000:00 Na 10000:00 8340:00 ATA 62-20-00 MAIN HEADS ra Cycles Na n/a Na Na Position 03 ra Landings Na Na n/a n/a Condition NEW MCN 6220-3350 Main Rotor Drive Bus PN 430-010-124-103 Since New Na Calendar Retirement Na 02/04/2001 Na Na SN A-299 Desc BUSHING, MR DRIVE 1660:00 Hours 500090 Na 5000:00 334090 ATA 62-20-00 MAIN HEADS n'a Cycles Na Na Na Na Position 03 Ca Landings n/a Na Na Na Hours Cycles landings Current Airframe as of 28/09/2009 1660:00 0 0 Condition NEW ♦v4ASE SYSTEWS INC EFTA01084857 PremiAir Aircraft Engineering Ltd Aircraft Compliance Report Aircraft: N901RL Make/Model: BELL 430 Serial No: 49078 prised: I IV1/2010 Tlintx t3tIt:36 Pane MCN 6220-3360 PN 430-010-124-103 Customer '0VALE DEVELOPMENTS Component 9 0' Main Rotor Drive Bur hinq. Times Intervals Retirement Tolerance Last Done Alrftame Next Due Na Remaining n/a n/a 02/04/2001 Since New a'a Calendar SN A-267 Desc BUSHING, MR DRIVE 1660 00 Hours 5000:00 n/a 5000:00 3340:00 ATA 62-20-00 MAIN HEADS va Cycles Na n/a n/a Na Position #3 Landings Na Na Na Na Condition NEW MCN 6220-4050 Main Rotor Blade Pin. PN 430-010-127-101 Since New v a Calendar Retirement Na 02/04/2001 Na Na SN A-0879 Dose PIN, MR BLADE 1660:x) Hours 10000:00 Na 10000:00 8340:00 ATA 62-20-00 MAIN HEADS Iva Cycles Na Na Na Na Position #4 ivri Landings Na Na n/a n/a Condition NEW MCN 6220-4060 Main Rotor Blade Pin PN 430.010.127-101 Since New Va Calendar Retirement Na 02/04/2001 Na n/a SN A-0841 Oesc PIN. MR BLADE 1660:00 Hours 10000:00 Na 10000:00 8340:00 ATA 62-2D00 MAIN HEADS r la Cycles Na Na n/a Na Position 04 r /a Landings Na n/a n/a ilia Condition NEW MCN 6220-4100 Main Rotor Adapter. PN 430.010.109-101 Since New Va Calendar Retirement Na 02/04/2001 Na Na SN A-199 Dose ADAPTER, MR BLADE 1660:t0 Hours 10000:00 Na 10000:00 8340:00 ATA 62.2000 MAIN HEADS r 'a Cycles Na Na Na n/a Position 04 r fa Landings Na Na Na Na Condition NEW MCN 6220-4150 Main Rotor Pitch Horn. PN 430.010-115-101 Since New Ca Calendar Retirement Na 02/04/2001 Na Na SN A-376 1660.00 Hours 10000:00 n/a 10000:00 8340:00 Desc HORN, MR PITCH ATA 62-20.00 MAIN HEADS rra Cycles Na Na Na Na Position e4 Na Landings Na Na Na Na Hours Cycles Landings Current Airframe as of 28/09/2009 1660:00 0 0 Condition NEW AV•8ASE SYSTEMS INC. • *3 EFTA01084858 PremiAir Aircraft Engineering Ltd Aircraft Compliance Report Hours Cycles Landings Current Airframe as of 28/09/2009 1660:00 0 0 Aircraft: N901RL Customer: 30VALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component Times Airframe Printed: n/91/LOW rune: 13.+1:37 Pepe: 70 Current Intervals Tolerance Last Done Next Due Remaining MCN 6220-4200 Main Rotor Damper Slide Set. PN 430-310-104-105 Since New n'a Calendar Retirement Na 02/04/2001 Na Na SN LK0478 Dose DAMPER BLADE SET 1660 CO Hours 10000:00 We 10000:00 8340:00 ATA 62-20-00 MAIN HEADS n,a Cycles Ilia Na Na Na Position 04 n, a Landings Na Na Na Na Condition NEW MCN 6220-4250 PN 430.310.101-107 SN 0(1323 Dose RESTRAINT. MR SHEAR ATA 62-20-00 MAIN HEADS Position 04 Condition NEW MCN 6220-4300 PN 430-Ot0.105.105 SN A-534 Dose PLATE SET. CLAMP ATA 62-20-00 MAIN HEADS Position 04 Condition NEW MCN 6220.4350 PN 430-010-124-103 SN A-276 Dose BUSHING, MR DRIVE ATA 62-20-00 MAIN HEADS Position 04 Condition NEW MCN 6220-4360 PN 430-010.124.103 SN A-307 Dose BUSHING. MR DRIVE ATA 62-20-00 MAIN HEADS Position 04 Condition NEW Main Rotor Shear Res mint. Since New r a Calendar Retirement Na 25/10/2005 Na Na 750 / 9 Hours 10000:00 909:12 10909:12 9249:12 n a Cycles Na Na ilia Na n a Landings nee Na Na Na Main Rotor Clamp Pla e Set. Since New r 'a Calendar Retirement Na 02/04/2001 Na Na 1660 ( 0 Hours 11X/00M rile 10000:00 8340:00 n a Cycles Na Na ilia Na n a Landings Na Na Na Na Main Rotor Drive Bushing. Since New r Calendar Retirement Na 02/04/2001 n/a Na 1660(10 Hours 5000:00 Na 5000:00 3340:00 na Cycles Na n/a Na Na i a Landings Na Na Na Na Main Rotor Drive Bus ling, Since New Calendar Retirement Na 02/04/2001 Na Na 1660: IC Flows 5000:00 Na 5000:00 3340:00 r la Cycles Na Na Na Na Landings n/a Na Na Na 4134A5( SYSTEMS IOC • 13 EFTA01084859 PremiAir Aircraft Engineering Ltd Hours Cycles Landings Aircraft Compliance Report Current Airframe as of 28/09/2009 1660:00 0 0 Aircraft: Make/Model: Serial No: Primed: trOl/20to MCN PN N901RL Customer BOVALE DEVELOPMENTS BELL 430 49078 Component Times now 12:47:37 Peet I / Currer 6230-0000 Main Rotor Mast Ass :rnbly. Airframe Intervals Tolerance Last Done Next Due Remaining 430-110-400-105 SN Since OH A-82 Na Calendar Overhaul Na 10/07/2009 n/a Na Desc MAST ASSEMBLY 1660 00 Hours 5000:00 1611:00 5000:00 3340:00 ATA Position 62.30-00 MAIN MAST/SWASHPLATE ONLY Va tlfa Cycles Landings Na Na Na Na n/a n/a n/a n/a Condition REPAIRED MCN 6230-0100 Main Rotor Mast. PN SN 430-040-130-115S Since New DN190 La Calendar Retirement Na 10,07/2009 n/a n/a Desc MAST, MAIN ROTOR 49:00 Hours 10000:00 1611:00 11611:00 9951:00 ATA 62.30-00 MAIN MAST/SWASHPLATE Cycles Na Na Na Na Position ONLY rVa Landings Na Na Na n/a Condition NEW MCN 6230-0150 Main Rotor Swasholsie Drive Hub. PN SN 430-010-410-101 Since New RE91 Va Calendar Retirement Na 02/04/2001 Na Na Dose HUB. SP DRIVE 1660:J0 Hours 10000:00 Na 10000:00 8340:00 ATA Position 62-30-00 MAIN MAST/SWASHPLATE ONLY Na Na Cycles Landings Na Na Na n/a Na Na Na Na Condition NEW 1. MCN 6230-0160 Main Rotor Swasholap Drive Idler Link. PN SN 430-010-409-105 Since New Na Calendar Retirement RE109 Na 02t04/2001 Na Na Dose LINK. SP IDLER 166010 Hours 10000:00 Na 10000:00 8340:00 ATA 62.30-00 MAIN MAST/SWASHPLATE ela Cycles Na Na Na n/a Position ONLY ra Landings Na Na Na Na Condition NEW MCN 6230-0170 Main Rotor Swasholale Drive Link. PN 430-010-408-101 Since New //a Calendar Retirement n/a 02/04/2001 Na Na SN RE91 Dose LINK. SP DRIVE 1660:60 Hours 10000:00 n/a 10000:00 8340:00 ATA Position 62-30-00 MAIN MAST/SWASHPLATE ONLY 4a Cycles Landings Na Na Na n/a Na Na Na Na Condition NEW AY-USE SYSIEPOSOC • V& EFTA01084860 PremiAir Aircraft Enqineerinq Ltd Aircraft Compliance Report Hours Cycles Landings Current Airframe as of 28/09/2009 1660:00 0 0 Aircraft: N901RL Customer: 3OVALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component Times Airframe Printed: 11O120W Time: 73:41:37 Page: 72 Current Intervals Tolerance Last Done Next Due Remaining MCN 6230-0200 Main Rotor Swasnoiati) and Su000rt. PN 430-010-400-105 Since 0 H NB Calendar Overhaul Na 02/04/2001 Na Na SN 49076 Desc SWASHPLATE, MR 1660:03 Hours 5000:00 Na 5000:00 3340:00 ATA 62-30-00 MAIN MAST/SWASHPLATE 717.71 Cycles Na Na Na n/a Position ONLY roe Landings Na Na Na Na Condition SERVICEABLE MCN 6230-0250 Main Rotor Swash plat SUWON. PN 430-010.404-101 Since New na Calendar Retirement Na 02/04/2001 n/a Na SN A-114 Desc SUPPORT. SWASHPLATE 1660 ( .) Hours 1000010 Na 10000:00 8340:00 ATA 62.30-00 MAIN MAST/SWASHPLATE 11 1 Cycles Na Na Na Na Position ONLY Landings ilia Na Na Na Condition NEW MCN 6230-0300 PN 430-010.403-105 SN A-139 Desc SLEEVE. BALL ATA 62-30-00 MAIN MAST/SWASHPLATE Position ONLY Condition NEW Main Rotor Swashplat ) Ball and Sleeve. Since New rfa Calendar Retirement Na 02/04/2001 Na Na 1660:60 Hours 10000:00 Na 10000:00 8340:00 n`a Cycles Na Na Na Na n'a Landings Na n/a Na Na MCN 6230-0350 Main Rotor Swashplai a Non-Rotating Ring. PN 430-010-402-101 SN RE97 Desc RING, SP NONROTATING ATA 62-30-00 MAIN MAST/SWASHPLATE Position ONLY Condition NEW MCN 6230-0400 Main Rotor Swasholale Rotating Ring. PN 430-010-401-105 Since New Na Calendar Retirement Na 02/04/2001 Na Na SN RE90 1660:00 Hours 10000:00 n/a 10000:00 8340:00 Dose RING. SP ROTATING ATA 62.30-00 MAIN MAST/SWASHPLATE rya Cycles Na Na Na n/a Position ONLY a Landings Na Na Na Na Condition NEW Since New r . Calendar Retirement Na 02104/2001 Na Na 660 i 0 Hours 1000010 nia 10000:00 8340:00 rva Cycles Na n/a Na Na r a Landings Na Na Na n/a AV-BASE SYSTEMS PC 13 EFTA01084861 PremiAir Aircraft Aircraft: Make/Model: Aircraft Engineering Ltd Compliance Report Current Airframe as of 28/09/2009 N90IRL Customer4 BOVALE DEVELOPMENTS BELL 430 Hours 1660:00 Cycles Landings Serial No: 49078 Component Tenn Airframe Printed: 11 O12010 nriw: t3:41:37 Pay.: 13 Currerf Intervals Tolerance Last Done Next Due Remaining MCN 6230.0450 Collective Lever. PN SN 430-010-405-105 Since New A-108 Na Calendar Retirement Na 02/04/2001 Na Na Desc LEVER, COLLECTIVE 1660110 Hours 10000:00 Na 10000:00 8340:00 ATA 62-30-00 MAIN MAST/SWASHPLATE 'Ye Cycles Na Na Na Na Position ONLY oia Landings Na Na Na Na Condition NEW • - MCN 6230-0500 Collective Idler Link. PN 430-010-407-101 Since New ua Calendar Retirement Na 02/04/2001 Na Na SN RE91 Desc LINK. IDLER 1660:10 Hours 10000:00 Na 10000:00 8340:00 ATA 62-30-00 MAIN MAST/SWASHPLATE r la Cycles Na Na Na Na Position ONLY r a Landings Na Na Na Na Condition NEW MCN 6230-1460 Main Rotor Swashpla a Ball Sleeve to Collective Lever Pin - Left. PN 430-010442.101 Since New Calendar Retirement Eva 02/04/2001 Na Na SN A-229 Desc PIN Hours 5000:00 Na 5000:00 3340:00 ATA 62-30.00 MAIN MAST/SWASHPLATE Cycles Na n/a Na n/a Position LEFT Landings n/a Na n/a Na Condition NEW MCN 6230-1550 Cyclic Lever - Lett. PN 430-010-406-101 Since New era Calendar Retirement Na 02/04/2001 Na Na SN RE186 Dose LEVER, CYCLIC 1660:00 Hours 10000:00 n/a 10000:00 8340:00 ATA 62-30.00 MAIN MAST/SWASHPLATE rte Cycles n/a Na Na Na Position LEFT r /a Landings Na Na Na Na Condition NEW MCN 6230-1560 Main Rotor Swasholal e Collective Lever to Cyclic Lever Pin - Lett. PN 430.310-055-101 Since New 're.' Calendar Retirement Na 02/04/2001 Na Na SN ST-71 Desc PIN, CYCLIC 1660.00 Hours 5000:00 Na 5000:00 3340:00 ATA 62.30-00 MAIN MAST/SWASHPLATE n-a Cycles Na rile Na Na Position LEFT n a Landings n/a Na n/a Na Condition NEW AV4ASE SYSTEUS PC. -13 EFTA01084862 PremiAir Aircraft Engineering Ltd Aircraft Compliance Report Aircraft: N901RL Make/Model: BELL 430 Serial No: 49078 Printed: 11912010 Time: 13:41:38 Page: (4 MCN 6230-1600 PN 430-010412-105 SN RE258 Desc LINK, CYCLIC ATA 62-30-00 MAIN MAST/SWASHPLATE Position LEFT Condition NEW MCN 6230-2460 PN 430-010-442-101 SN A-236 Desc PIN ATA 62-30-00 MAIN MAST/SWASHPLATE Position RIGHT Condition NEW MCN 6230-2550 PN 430-010-406-101 SN RE184 Desc LEVER. CYCLIC ATA 62-30-00 MAIN MAST/SWASHPLATE Position RIGHT Condition NEW Current Airframe as of 28/09/2009 1660:00 Customer: 3OVALE DEVELOPMENTS Hours .,[1:anqs 0 Current Cyclic Link - Left. Since New Component Times Intervals Tolerance Na Calendar Retirement 1660:00 Hours na Cycles n a Landings n/a 10000:00 Na Na Main Rotor Swash plat .t Ball Sleeve to Collective Lever Pin - Right. Since New MCN 6230-2560 PN 430-310-455-101 SN ST-101 Desc PIN, CYCLIC ATA 62-30-00 MAIN MAST/SWASHPLATE Position RIGHT Condition NEW a Calendar Retirement 1660.(0 Hours n a Cycles na Landings Cyclic Lever - Right. Since New r 1660.(0 na Calendar Retirement Hours Cycles r a Landings n'a 5000:00 Na Na Na 1000060 Na Na Main Rotor Swasnolal a Collective Lever to Cvellc Lever Pin - Right. Since New MCN 8230-2600 PN 430-010-412.106 SN RE277 Dose LINK. CYCLIC ATA 62-30.00 MAIN MAST/SWASHPLATE Position RIGHT Condition NEW /a Calendar 1660x0 Hours ,a Cycles rt 'a Landings Cyclic Link - Rlaht, Since New Retirement n/a 5000:00 Na Na Na Calendar Retirement 1660:p0 Hours Na Cycles l a Landings Na 10000:00 Na Na Last Done 02/04/2001 n/a Na Na 02./04/2001 Na nta Na 02104'2001 Na Na 02/04/2001 Na n'a Na 02/04/2001 Na Na Na Air hank, Next DUO Na 10000:00 Na Na Na 5000:00 Na n/a Na 10000:00 Na Na n/a 5000:00 Na Na Na 10000:00 Na Na Remaining n/a 8340:00 Na Na 3340:00 Na Na Na 8340:00 Na Na Na 3340:00 Na Na Na 8340:00 Na Na AY43ASE SYSTEVS Pic • Is EFTA01084863 PremiAir Aircraft Engineering Ltd Aircraft Compliance Report Aircraft: N9O1RL Customers BOVALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Printed: I miaow Tint I3:41:all Page T.5 Currer: MCN 6310-1050 Main Drive Shaft - Lag, Component Calendar Thies Intervals Airframe Next Due Remaining 4, 3m 3d Tolerance Last Done Overhaul 5Y 14/04/2006 14/04/2011 PN 222-044.885105 Since 0/H 14/04/2006 SN A-1109 Desc SHAFT. MAIN DRIVE 6796 Hours 5000:00 980:54 5980:54 4320:54 ATA 63-10-00 ENGINE/TRANSMISSION DRIVE n/a Cycles Na Ilia Na Na Position LEFT Na Landings Na Na Na rya Condition SERVICEABLE NOTE: Calendar based an Ovetha I. MCN 6310-2050 Main Drive Shaft - Ric ht. PN 222-044-685-105 Since OH 14:04:2(06 Calendar Overhaul 5Y 14/04/2006 14/04/2011 1y 3m 3d SN A-1087 Desc SHAFT, MAIN DRIVE 6794)6 Hours 5000:00 980:54 5980:54 4320:54 ATA 63-10-00 ENGINE/TRANSMISSION DRIVE r/e Cycles Na Na Na Na Position RIGHT r Landings Na Na Na Na Condition SERVICEABLE NOTE: Calendar based on Overhaul. MCN 6320-0000 Main Transmission. PN 430.040-003-109 ria Since Map Calendar Inspection Na 02/04/2001 Na lira SN A 85 1660 IC Desc TRANSMISSION. MAIN Hours 3000:00 n/a 3000:00 134000 ATA 63-2000 Aiffi GEARBOX r 'a Cycles Na Na Na Na Position ONLY r/a Landings Na n/a Na Na Condition SERVICEABLE Since 0 H tin Calendar Overhaul Na 02/04/2001 Na 'Ira 1660.00 Hours 5000:00 n/a 5000:00 3340:00 ma Cycles Na rva ilia Na rin Landings Na Na Na Na MCN 6330-0050 actuator Support. PN 222-040-125-001 Since New Calendar Retirement Na 02/04/2001 Na Na SN A-303 1660:(0 Desc SUPPORT. ACTUATOR Hours 5000:00 n/a 5000:00 3340:00 ATA 63-30.00 M'R GEARBOX MOUNTS n a Cycles Na n/a Na Na Position ONLY 0 a Landings Na Na Na Na Hours Cycles Landings Current Airframe as of 28/09/2009 1660:00 0 0 Condition NEW ALSALSE SYMMS INC EFTA01084864 PremiAir Aircraft Engineering Ltd Aircraft Compliance Report Current Airframe as of Aircraft: N901RL Customer: 30VALE DEVELOPMENTS Make/Model: BELL 430 28/09/2009 Hours 1660:00 Cycles Landings 0 0 Serial No: 49078 Component Times Airframe Praire& II/O1/2010 1Ims: 73:41:38 Page: I6 Current Intervals Tolerance Last Done Next Due Remaining MCN 6330-1100 Main Rotor Pylon Elul( Mount - Left. PN 430-310-200-107 Since New n'a Calendar Retirement Na 02/04/2003 Na Na SN LK0255 Desc MOUNT. PYLON 1210.00 Hours 10000:00 450:00 10450:00 8790:00 ATA 63-30-00 M/R GEARBOX MOUNTS Na Cycles Na n/a Na Na Position LEFT na Landings Na n/a Na Na Condition NEW MCN 6330-2100 Main Rotor Pylon Fluid Mount - Right. PN 430.310.200.107 Na Since New wa Calendar Retirement 02/04/2003 n/a Na SN LK0306 1210:C0 Hours 10000:00 Dose MOUNT. PYLON 450:00 10450:00 8790:00 ATA 63-30-03 WA GEARBOX MOUNTS na Cycles n/a Na n/a Na Position RIGHT nia Landings n/a n/a Na Na Condition NEW ---- MCN 6410-1000 Tail Rotor Blade. PN 222.016-001-t39M Since New i-7a Calendar Retirement Na 08/03/2008 Na Na SN A-2171 679:(6 Desc BLADE. TAIL ROTOR Hours 5000:00 135701 5980:54 4320:54 ATA 64-10-00 T/R BLADES na Cycles Na Na rtia n/a Position Al na Landings Na Na n/a n/a Condition REPAIRED MCN 6420-0000 Tail Rotor Hub. PN 222-012.701.135FM Since 0 H a Calendar Overhaul Na 07/03/2008 n/a n/a SN A-473 302: Hours 250000 Desc T/R HUB 1357:01 3857:01 2197:01 ATA 64-20-00 T/R HEADS a Cycles Na Na Na Na Position ONLY Landings n/a Na Na Na d'a Condition REPAIRED MCN 6420-0050 Tall Rotor Trunnion. 5 PN 222.012-703-107 Since New Afa Calendar Retirement Na 07/03/2008 Na Na SN A•105 166010 Hours 5000:00 Desc TRUNNION. TAIL ROTOR 1357:01 5000:00 3340:00 ATA 64-20-00 T/R HEADS n'a Cycles Na Na Na Na Position ONLY r .ta Landings n/a Na Na Na Condition OVERHAULED AYSASE SYMMS INC • 13 EFTA01084865 PremiAir Aircraft Engineering Ltd Hours Cycles Landings Aircraft Compliance Report Current Airframe as of 28/09/2009 1660:00 0 0 Aircraft: N901RL Customeri BOVALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component Times Airframe Printed: 119120,0 Tem l3:41 all Pepe 17 Currer I Intervals Tolerance Last Done Next Due Remaining MCN 6420-0100 Tail Rotor Yoke. PN 222-012-702-109 Since New ra Calendar Retirement Na 07/03/2008 ilia n/a SN A-470 Dose YOKE. TAIL ROTOR 1660 DO Hours 5000:00 1357:01 5000:00 3340:00 ATA 64-20-00 T/R HEADS Cycles Na Na Na Na Position ONLY Landings Na n/a Na Na Condition SERVICEABLE MCN 6510-1200 PN 222-044-003-Wr t SN 5MAY07-04 Disc HANGER, TAIL ORVSHFT ATA 65-10-00 T/R DRIVE SHAFT Position FORWARD Condition SERVICEABLE MCN 6510-1250 PN 222.344-606.103 SN MB629 Dose BEARING. TRDS ATA 65-10-00 T/R DRIVE SHAFT Position FORWARD Condition NEW MCN 6510-2200 PN 222-044003404 • c"., SN 15MAY07-05 Dose HANGER. TAIL ORVSHFT ATA 65-10-00 T/R DRIVE SHAFT Position CENTER Condition SERVICEABLE MCN 6510-2250 PN 222.344.606.103 SN MB952 Dose BEARING. TRDS ATA 65-10-00 T/R DRIVE SHAFT Position CENTER Condition NEW Tall Drive Shaft Hangar - Forward. On Condition Calendar Na 25/01)2007 Na n/a 523 36 Hours Na 1136:24 Na Na • . 0 Cycles Na Na n/a Na 0 Landings n/a Na Na n/a Tail Drive Shah Hangar Bearing - Forward. Since New 25/01,2(0? Calendar Retirement 3Y 25/01/2007 25/01/2010 14d 523:36 Hours 3000:00 1136:24 4136:24 2476:24 n/2. Cycles Na n/a Na Na rd:. Landings Na Na Na n/a Tall Drive Shaft Hang it - Center. On Condition Calendar Na 25101/2007 Na Na ), 52&16 Hours MI 113624 Na Na 0 Cycles Na n/a Na Na 0 Landings n/a Na Na Na Tall Drive Shaft Hangar Bearing - Center. Since New 25101/20)7 Calendar Retirement 3Y 25/01/2007 25/01/2010 14d 52326 Hours 3000:00 1136:24 4136:24 2476:24 n'a Cycles Na Na Na Na ri?a, Landings Na ilia Na Na AY BASE SYSTEMS PC 13 EFTA01084866 PremiAir Aircraft Endineerinq Ltd Aircraft Compliance Report Current Airframe as of 28/09/2009 1660:00 Aircraft: k49O1RL Customer 3OVALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component Times Airframe Primed: 118:114010 Time: 1341:38 Page: :8 Current Intervals Tolerance Last Done Next Due Remaining Hours Cycles Landings 0 0 MCN 6510-3200 Tall Drive Shaft Hanoa r - Alt. PN 222-044-003-1011 i 'S On Condition Calendar Na 25/01/2007 Na Na SN 19.4AY07-06 -'1,i.--E ru 1 ,( mi.-, 52333 Hours Na 1136:24 Na Na Desc HANGER. TAIL DRVSHFT ATA 65-10-00 T/R DRIVE SHAFT p Cycles ' n/a Na Na Na Position AFT 3 Landings Na Na Na Na Condition SERVICEABLE MCN 6510-3250 PN 222-344.606.103 SN MB955 Dose BEARING. TRDS ATA 65-10-00 T/R DRIVE SHAFT Position AFT Condition NEW MCN 6520-0000 PN 222.042.001-103 SN A-747 Desc GEARBOX. TAIL ATA 65-20-00 T/R GEARBOXES Position ONLY Condition SERVICEABLE MCN 6520-0050 PIN! 222.042402.005 SN A.410 Dose SHAFT. TR OUTPUT ATA 65.20.00 T/R GEARBOXES Position ONLY Condition NEW Tall Drive Shaft Hangar Bearing - Aft. Since New 25 01,20( 7 Calendar Retirement 3Y 25/01/2007 25/01/2010 14d 523':5 Hours 300000 1136:24 4136:24 2476:24 n i Cycles Na Na Na Na ft a Landings Na Na Na Na Tail Rotor Gearbox. Since Map Since 0 H Calendar Inspection Na 02/04/2901 n/a n/a 1660 :( 0 Hours 300090 n/a 3000:00 134090 n a Cycles Na Na Na N8 n a Landings Na n/a Na n/a r ra Calendar Overhaul Na 02/04/2001 Na Na 1660 ( 0 Hours 5000:00 n/a 5000:00 3340:00 n'a Cycles Na Na Na Na n'a Landings Na Na Na Na Tail Rotor Gearbox Or tout Shaft. Since New r 'rr Calendar Retirement Na 02/04/2001 n/a Na I E%60.( (3 Hours 5000:00 Na 5000:00 334090 r a Cycles Na Na Na n/a r a Landings n/a Na Ilia Na Ay -EASE SYSTEMS h`C EFTA01084867 PremiAir Aircraft Engineering Ltd Aircraft Compliance Report Current Airframe as of 28/09/2009 Aircraft: N901RL Make/Model: BELL 430 Serial No: 49078 Printod: 1 V0L2010 Tem 13:4I:39 Page: 19 MCN 7200-1000 PN 250-C40B SN CAE-844167 Dose ENGINE ATA 72-00-00 TURBINE ENGINE Position PI Condition REPAIRED MCN 7200-2900 PN 250-C4OB SN CAE-844169 Dose ENGINE ATA 72-00.00 TURBINE ENGINE Position 42 Condition REPAIRED MCN 7230-1000 PN 23065593 SN CAC-44957 Desc COMPRESSOR ATA 72.30-00 ENG COMPRESSOR Position 41 Condition SERVICEABLE MCN PN SN Desc ATA Position 91 Condition INSPECTED MCN PN SN Desc ATA Position Condition SERVICEABLE 7230.2000 23065593 CAC-45034 COMPRESSOR 72-30-00 ENG COMPRESSOR #2 SECTION 7230-1100 23065591 JY100665 IMPELLER: COMPRESSOR 72-30.00 ENG COMPRESSOR SECTION Customer?, BOVALE DEVELOPMENTS Hours Cycles Landings 1660:00 0 0 Engine - 01. On Condition Currer t Component Times Intervals 19/03/2401 Calendar 1660 00 Hours O Cycles O Landings Eng #1 Engine - #2. On Condition 1 Calendar Hours Cycles Landings 2020.00 Eng 92 Na Na n/a Na Na Na n/a n/a n/a Na Tolerance Last Done 30/06/2009 1611:00 n/a n/a 1965.00 30/06/2009 1611:00 Na Na 1965.00 Airframe Next Due Compressor #1. An time the compressor Is removed from the engine. visually Inspect the aft end of On Condition 1642 )6 SECTION Calendar Hours Cycles Landings Compressor impeller hes Since New a Calendar 1642. Hours a Cycles a Landings 1985.00 Eng #1 Compressor • 02. Anylime the compressor is removed from the engine visually inspect the aft end of On Condition 12/02/20)1 Calendar 1124:f:4 Hours O Cycles O Landings n/a n/a n/a n/a 30/06/2009 1611.00 n/a n/a Retirement Na 7500:00 Na Na 15000.00 Na Na n/a n/a 30/06/2009 1611:00 Na Na 1965.00 30/062009 161100 nia Na Remaining n/a Na Na n/a Na n/a Na Na Na Na Na n/a Na Na Na Na Na Ne Na Na n/a Na Na Na Na Na Ne n/a Na 7517:54 Na Na 15035.00 Na Na Na n/a n/a 5857:54 Na n/a 13015.00 n/a Na Na Na AY4LASC SYSTEMS %1 EFTA01084868 PremiAir Aircraft Engineering Ltd Aircraft Compliance Report Aircraft: N901 RL Make/Model: BELL 430 Serial No: 49078 Printed:11/0MM Time 1341:39 Page: 20 MCN 7230-2100 Compressor Customer: i3OVALE DEVELOPMENTS Component 71rnes Airframe Due Na 7500:00 Na Na 15000.00 Remaining Na 5840:00 Na Na 12980.00 Curren: Intervals Tolerance Last Done Next Impeller - #2. 30/06/2009 1611:00 Na Na 1965.00 the splines on the fo PN 23065591 Since New ria Calendar Retirement n/a SN JY102124 Dose IMPELLER, COMPRESSOR 1660:0) Hours 7500:00 ATA 72-30.00 ENG COMPRESSOR SECTION rill Cycles n/a Position W2 Na Landings Na Condition SERVICEABLE 2020.03 Eng #2 15000.00 MCN 7250-1000 Turbine - #1. Anytime the turbine is removed from the engine. visually Inspect PN 23063354 Since OM Na Calendar Overhaul Na 30/06/2009 Na n/a SN CAT-44746 Desc TURBINE 49:C0 Hours 1750:00 1611:00 3361:00 1701:00 ATA 72-50.00 ENG TURBINE SECTION na Cycles na Na Na Na Position #1 na Landings Na Na Na Na Condition OVERHAULED MCN 7250-1050 Turbine Wheel, First Stage - #1. PN 23053299 Since New Na Calendar Retirement Na 30106'2009 Na Na SN X583182 Desc WHEEL. TURBINE 1ST 49:63 Hours 1775:00 1611:00 3386:00 1726.00 ATA 72-50-00 ENG TURBINE SECTION nie Cycles Na n'a Na Na Position 1$1 alb Landings Na Na Na Na Condition NEW 55.00 Eng #1 3000.00 1965.00 4965.00 2945.00 - • • MCN 7250-1100 Turbine Wheel, Second Stage - #1. PN 23032280 Since Now 'la Calendar Retirement Na 30/06/2009 Na Na SN X569531 Desc WHEEL, TURBINE 2ND 49:00 Hours 1775:00 1611:00 3386:00 1726:00 ATA 72-50-00 ENG TURBINE SECTION Cycles Na Na rite Na Position #1 n'a landings n/a Na Na Na Condition NEW 55.00 Eng ill 3000.00 1965.00 4965.00 2945.00 MCN 7250-1150 Turbine Wheel, Third 5taae - #1. PN 6898663 Since New r /a Calendar Retirement Na 30/06/2009 Na Na SN HX93537 One WHEEL, TURBINE 3RD 1660110 Hours 4550:00 1611:00 4550:00 2890:00 ATA 72-50-00 ENG TURBINE SECTION rid Cycles Na Na Na Na Position #1 Ca Landings Na Na Na na Condition SERVICEABLE 2020.00 Eng #1 6000.00 1965.00 6000.00 3980.00 Hours Cycles Landings Current Airframe as of 28/09/2009 1660:00 0 0 AV-BASE 5'1511%51NC 0 EFTA01084869 PremiAir Aircraft Engineering Ltd Aircraft Compliance Report Aircraft: N901 RL Make/Model: BELL 430 Serial No: 49078 Printed: ilt0112010 Thin: tag, le Pager 1r MCN 7250-1200 PN 23066744 SN HX76889 Desc WHEEL. TURBINE 4TH ATA 72-50-00 ENG TURBINE SECTION Position Ai Condition SERVICEABLE MCN 7250-2000 PN 23063354 SN CAT-44750 Desc TURBINE ATA 72-50-00 ENG TURBINE SECTION Position 82 Condition OVERHAULED Hours Cycles Landings Current Airframe as of 28/09/2009 1660:00 0 0 Customer:. BOVALE DEVELOPMENTS Currer t - Component 77mes Intervals Tolerance Turbine Wheel Four(i Stage-fi t Since New 1660 va 2020..10 Calendar Retirement Hours Cycles Landings Eng #1 Airborne Last Done Next Due Remaining Na 4550:00 Na Na 6000.00 30/06/2009 1611:00 Na rile 1965.00 Turbine - 12. Anytime the turbine is removed from the enable. visually Inspect the sullnes on the to Since O H MCN 7250-2050 PN 23053299 SN X5513151 Desc WHEEL. TURBINE 1ST ATA 72.50-00 ENG TURBINE SECTION Position #2 Condition NEW MCN 7250-2100 PN 23032280 SN X569825 Dose WHEEL. TURBINE 2ND ATA 72-50-00 ENG TURBINE SECTION Position 02 Condition NEW MCN 7250-2150 PN 6898663 SN HX93598 Desc WHEEL. TURBINE 3RD ATA 72.50-00 ENG TURBINE SECTION Position 82 Condition SERVICEABLE vi Calendar Overhaul 49: XI Hours I /a Cycles r ia Landings Turbine Wheel, First !.tade - 82. Since New a Calendar Retirement 49:X. Hours r Cycles ria Landings 55.qC Eng #2 Turbine Wheel. Second Stacie - #2. Since New Na Calendar Retirement 49.(0 Hours Cycles Landings 55.0 Eng 82 Turbine Wheel. Third 3laae - #2. Since New r la Calendar Retirement 1660.00 Hours n a Cycles n a Landings 2020.(0 Eng 82 nia 1750:00 Na Na Na 1775:00 Na Na 3000.00 Na 1775:00 n/a Na 3000.00 Na 4550:00 n/a Na 6000.00 30'06/2009 1611:00 n'a Na 30,06•:2009 1611:00 Na n/a 1965.00 30106/2009 1611:00 Na rite 1965.00 30/06/2009 1611:00 n/a nla 1965.00 Na Na 4550:00 2890:00 Na Na Na no 6000.00 3980.00 rea Na 3361:00 1701:00 Na n/a Na Na Na Na 3386:00 1726:00 Na rila Na Na 4965.00 2945.00 Na rile 3386:00 1726:00 Na Na Na n/a 4965.00 2945.00 Na Na 4550:00 2890:00 Na Na Na Na 6000.00 3980.00 •Y.SSSE SYSTEMS WC • Ii EFTA01084870 PremiAir Aircraft Engineering Ltd Aircraft Compliance Report Aircraft: N90IRL Custo !ALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component Printed: I 1O12010 Time:1341:39 Page: 22 Curren; MCN 7250-2200 Turbine Wheel. Fourth .51age - #2. Times Intervals Retirement Airframe Next Due Na Remaining Na Tolerance rya Last Done 30/06/2009 PN 23066744 Since New n a Calendar SN HX76810 1660:00 Hours Dose WHEEL, TURBINE 4TH 455000 1611:00 4550:00 2890:00 ATA 72.50.00 ENG TURBINE SECTION Na Cycles nra nra Na Na Position 92 iva Landings Na Na Na n/a Condition SERVICEABLE 2020.00 Eng 82 6000.00 1965.00 6000.00 3980.00 MCN 7260-1000 Gearbox - 81. PN 23063380 19/0312001 Calendar On Condition Na 30/06/2009 Na n/a SN CAG-44167 49:CO Hours Desc GEARBOX. ENGINE ATA 72-60.00 ENG ACCESSORY DRIVES 0 Cycles Na Na 1611:00 Na n/a Na Na Na Position #1 0 Landings Na n/a Na Na Condition SERVICEABLE MCN 7260-2000 Gearbox - 82. PN 23063380 12/02/2001 Calendar On Condition Na 30/06/2009 Na n/a SN GAG-MISS 49:C0 Hours Desc GEARBOX. ENGINE ATA 72-60-00 ENG ACCESSORY DRIVES 0 Cycles n/a n/a 1611:00 Na n/a n/a Na Na Position e2 0 Landings Na Na n/a Na Condition SERVICEABLE MCN 7300-1000 Hvdromechanical Unit (HMU) - #1. PN 23078033A rta Calendar Since OM Overhaul Na 30/06/2009 Na Na SN JGALM0158 69:2 Hours Desc HMU ATA 73-00-00 ENGINE FUEL n'a Cycles 2500:00 n/a 1611:00 Na 4090:38 n/a 2430:38 Na Position 81 Landings Na n/a n/a Na Condition SERVICEABLE MCN 7300-2000 Hydromechanical Unli (HMU) -112. PN 23078034 Since 0.11 its Calendar Overhaul Na 30/06/2009 Na Na SN JGAMT0603 1660X0 Hours Desc HMU 2500:00 1611:00 2500:00 840:00 ATA 73-00-00 ENGINE FUEL r (a Cycles Position 42 r Landings n/a Na Na Na Na n/a Na Na Current Airframe as of 28/09/2009 1660:00 Hours Cycles Landings 0 0 Condition SERVICEABLE AviASESYSTEMSOC.I3 EFTA01084871 PremiAir Aircraft Engineering Ltd Aircraft Compliance Report Aircraft Make/Model: Serial No: Pa:ISO:11VMM MCN PN N901RL Customer BELL 430 BOVALE DEVELOPMENTS 49078 Time: Page Component Times Intervals Last Done Airframe Next Due Rem...Jiro° Tolerance I341:39 23 Currer$ 7310.1100 Fuel Nozzle - #1, 23077067 SN Since Ortl 1XR05440 11/9 Calendar Overhaul Na 30/06/2009 Na Na Desc NOZZLE, FUEL 166010 Hours 2000:00 1611:00 2000:00 340:00 ATA 73.10-00 ENGINE FUEL DISTRIBUTION eia Cycles Na Na Na Na Position 01 ii/a Landings Na Na Na Na Condition SERVICEABLE MCN 7310-2100 Fuel Nozzle - 02. PN 23077067 Since 0 H Calendar Overhaul n/a 30/06/2009 Na ilia SN 1ZR04765 Desc NOZZLE. FUEL 1654:34 Hours 2000:00 1611:00 2005:06 345:06 ATA 73-10-00 ENGINE FUEL DISTRIBUTION Ida Cycles Na Na Na Na Position 12 tra Landings Na Na n/a nia Condition SERVICEABLE MCN 7530-1000 Compressor Blurt Vr lye - #1. PN 23073353 Since 0/H a Calendar Overhaul Na 30/06/2009 nia Na SN FF58672 Desc BLEED VALVE 1136: IC Hours 1500:00 1611:00 2024:00 364:00 ATA 75.30-00 ENG COMPRESSOR BLEED CON. r Cycles Na n/a Na n/a Position 01 , a Landings Na n/a n/a Na Condition SERVICEABLE MCN 7530-2000 Compressor Bleed Valve - #2. PN SN 23073353 Since 0 H FF36207 Ya Calendar Overhaul Na 30/06/2009 Na Na Desc BLEED VALVE 201 Hours 1500:00 1611:00 2958:38 1298:38 ATA 7530.00 ENG COMPRESSOR BLEED CON a Cycles ilia Na n/a Na Position N2 r4 Landings Na Na n/a Na Condition OVERHAULED MCN 7920-1000 011 Cooler Blower - til PN 230-365-001-101 Since ON Ala Calendar Overhaul Na 12/10/2001 n/a Na SN 0115 Desc BLOWER, OIL COOLER 2252: Hours 3000:00 36:18 2407:18 747:18 ATA 79-20-00 ENG OIL DISTRIBUTION rt. Cycles Na n/a Na Na Position II Landings Na Na Na Na Hours Cycles Landings Current Airframe as of 28/09/2009 1660:00 0 0 Condition SERVICEABLE AV4ASE $YSTEVS ITC 1) EFTA01084872 PremiAir Aircraft Engineering Ltd Aircraft Compliance Report Aircraft: N901RL Make;Model: BELL 430 Serial No: 49078 Printed: 11,01/2010 Tans: 13.41.40 Page: MCN 7920-2000 PN 230-365-001-101 24 OIl Cooler Custert: 3OVALE DEVELOPMENTS Component Times Current Blower - to2. Intervals Tolerance n/a Last Done 02/04/2001 Airframe Next Due Na Remaining Na Since OH n:a Calendar Overhaul SN 1109 Desc BLOWER, OIL COOLER 1660:00 Hours 3000:00 n/a 3000:00 1340:00 ATA 79.20.00 ENG OIL DISTRIBUTION IV3 Cycles Na Na Na ela Position #2 rva Landings n/a Na Na Na Condition SERVICEABLE MCN 8010-1000 Starter-Generator -111. PN 206.062.200.129 Since OH Na Calendar Overhaul Na 24/08/2007 n/a Na SN Y10348 Dese STARTER-GENERATOR 679:66 Hours 1000:00 1294:47 1980:54 320:54 ATA 80-10.00 ENGINE CRANKING Na Cycles Na Na Na Na Position NI na Landings Na Na Na Na Condition REPAIRED MCN 8010-2000 Starter-Generator - #2. PN 206.062.200-129 Since O/H Na Calendar Overhaul Na 01/10/2008 ilia Na SN Y0402 Desc STARTER-GENERATOR 69:212 Hours 100000 1590:38 2590:38 930:38 ATA 80.10-00 ENGINE CRANKING Na Cycles Na Na Na Na Position It2 Condition OVERHAULED nla Landings f Na Na Na Na 4-- check aryl CAP check MRS Clock Batten', MCN 9500-0000 PN BP9 Electric leak 01/10/2009 24/12/2009 -18d Since O H 24:99t 9 Calendar Overhaul 3M SN 25262 Desc BATTERY PACK n'a Hours Na 1660:00 Na Na ATA 95.00-00 Added in Conversion n'a Cycles Na Na Na n/a Position N/A n'a Landings Na Na Na n/a Hours Cycles Landings Current Airframe as of 28/09/2009 1660:00 0 Condition TESTED NOTE: Calendar based on Overhaul. Ref: 95-00.00.97 AV BASE SYSTEMS INC EFTA01084873 PremiAir Aircraft Engineering Ltd Aircraft Compliance Report Aircraft: N901RL Make/Model: BELL 430 Serial No: 49078 Printed: 11/01/2010 hint 19:4140 Page: 25 MCN 9900-0000 PN Z2-13430 SN NSOIRL Desc AD/SB LOG km 05-00-00 MAINTENANCE CHECKS Position N/A Condition SERVICEABLE Hours Cycles Landings Current Airframe as of 28/09/2009 1660:00 0 0 Customer XWALE DEVELOPMENTS AD:SB Loq On Condition 1660 00 0 0 Component Times Calondar Hours Cyclos Landings intervals Tolerance Airframe Last Done Next Due Remaining Na Na Na Na Component MCNs Only. Does not Include: Superseded, Not Pequired, Applied Only. No Status. Disabled MCNs. 02/04/2001 Na Na n/a Na Na Na Na Na Ilia Na Na "'End of Report— AMEASC SYSTEMS INC 13 EFTA01084874 EFTA01084875 Bell 430 Reg' n : N901RL Current Engine Hours : #1 Engine s/n : CAE 844167 TSN : 1660 Hrs #2 Engine s/n : CAE 844169 TSN : 1660 Firs Engine Gearbox is on condition i.a.w. Maintenance Manual Chap 72-00-00 Table 6 #1 Engine Component Status ( Eng TSN ) Fuel Nozzle due O/H @ 2000 Hr Bleed valve due O/H @ 2024 Hr Oil Cooler Blower due O/H @ 2407 Hr Starter-Generator due O/H @ 1981 Hr Note : Main Driveshaft due overhaul now #2 Engine Component Status ( Eng TSN ) Fuel Nozzle Bleed valve Oil Cooler Blower Starter-Generator due O/H @ 2000 Hr due O/H @ 2959 Hr due O/H @ 3000 Hr due O/H @ 2590 Hr Significant Scheduled Maint Inspection items due : 50/150/600 Hr Airframe Radio Annual Auto Fiji:A Compurieni iiispeciion Compass Calibration Altimeter & Altimeter Encoder per Appendix E Part 43 Chap 1 Test and Insp Altimeter system/Attitude reporting equipment i.a.w FAR 91.411 Fire bottle(s) Hydrostatic Test ASB 430-10-44 Hydraulic Servo Piston Insp All the above as of 2 August 2011 EFTA01084876 Service Bulletin - Available Cor Content Revision 18/0712011 File ID: NEW Aircraft Registration rg et I 4,— SB Number Effective Date Doscrlp :Ion Complied Date Time Amendment Number Method of Compliance/Applicability Once or Recur Nest Duo Data Time 1. Facility 3. Cert. Num. 2. Cort. Type 4. Author. By Manufacturer Category Model Part #: Allison Engine Company Engine f'. 250-C40B SerialIII CAE-844.67 4. 24+m 1317-A-1166 1511011982 ENGINE FUEL ANOCONTROL, BENDIX FUEL CONTROL ASSEMBLIES AND POWER TURBINE GOVERNOR ASSYS- INSPECT BUSING ASSYS I pi 640".4e nittpx4._ r•furnevirse. ffl-t ral-1-6 9 Once „ NI itt 1. Pf-Entiotta Atear-r 2. IE-Cortnraigeirtic ctj) 3. L ..Thgaret sA'ei..--i 4. 0 I AuG Zor t OUP (ATP OATP Signature C30•A•73-3103 R3 05/06/2003 ag, -A-73- 6ot) rGoodricbengine, foal and controtinspectIon of MU drive splines and power lever angle (KA) signal . CM AT 9394 6 4[6, rots Sone Sant Et.W.T.t-saS c4 fr.( AT- so-o-P OS or moPtAisp nie..-1 N/A- 0.4 9/4 1.4 Ogni..r.Cap - 2 SCrirn.34. Ceig& 5o2t ea./ Real( ' 1Jfmt ale_ fated:et 2. a r ra, wiroge.472. Up 3. 1.- -11:10.-b. -4 4. FA IN Cs Zed 1 oATP CAW 0...k 104 - A-73 - 4- re.R.....$) OATP lima rdait i. C40-A-72-5009 21/05/1997 ENGINE, GEARBOX ASSEMBLY- REPLACEMENT OF CERTAIN POWER TAKE-OFF GEARS, PIN 23056617 NIA frai-i aresee.6er7t Sean.- rsfinf-atr inf5,014....4;4> bisIn 64-fate- ES Once • Peon-late flees, - 2. G...Cdri-50110,4G 3. L . -flavrirefo.....1 4. 01 ich.)6 2-01 I MOP OATF OATP C6) Wr------ C40-A-72-5048 R2 27/06/2006 Engine, turbine assembly-new threshold event recording and new steady-state operation avoidance range limit CIIAI ,, 2. Cane. _ , ner4Als it i oriG(sw+.•>7) ci.-4 AT i I 36.4- µ4S 32Ar69 2.5awriZtiol 4 z 6,46. csa*K09 611,4 AT II 36 -sl- 1165 9A-tiop 2.5a-...-12.c.c.7 Once NI /A l • Peam.Afe mecat CE-Iglaaa.C.mif,- tip 3. 1.....-rita-nes-D-1 4. e-t Fist,- '1_'01l CcATP OAT'? refereCoq OATP Signature: C40,4-73-5029 04/0912003 Engine, fuel delivery-release of new fuel nozzle N IA Se17.t.A01,-4 4:.rCon-fientrot. acko-as Once r-ilA I- m 'AC AreCeetr-r- 2. lenter.4.14W-,,.&- t..-W3 a L.. ropene.se—s 4. en aritsGe OeM i OA T P OAT; Caw Signature: c r----4*.---- -- C40-A-73-5029 Rt 30/08/2004 Engine, fuel delivertwelease of new fuel nozzle I ; I pec,,Aeogx Gip.) i 5M FAA "P fc04- g4.. e9 4i &w isti4ifs0 rfoZZLeciSiratmeep ar 529. 0 des rnagp IS ocr 2003 42 CI-C.: C6440.9 rcotzLe.. arritac-€4> AT 53o-o PCS ..TAnS.j> 29 OCR' 2a:35 Once N/A ''ream. rate2 oh Caner 2. EaThat& (-74D 3. L.-raw-rec...I 4. ta4 A-...3-G- 2c2.1/ OATP m lore: ice.t FAAREpAir r...)n fr oirtoott,00 A4DATTP„Soigna. ea -Aina-Pi °I ASS eon IZaiirria OATP Printed 01/08Q011 13:37:66 O CCC Page of 5 EFTA01084877 Service - Content Revision: 18/07/2011 File ID: *NEW' Aircraft Registration hi of t..- S13 Number Effective Date . .. . . Descrit ti on . ... Complied Date • Time Amendment NuMber Method of Compliance/Applicability Once or Recur Next Due Date Time 1. Facility 3, Cert. Num. 2. Cert. Type 4. Author. By _ Manufacturer Category Model Bell Helicopter Airframe 430 Part IS: Sorial U: 42O78 430.985 12/06/1998 OATP Vertical fin assembly., installation Inspection and modiication OATP Civ.I A-i gurn-co Corna.i6P tni or* Ar e,..n to Recur ©ATP NO 1 igiamaie. AtAcei4F-i- 2. 644-...reisci..rc- t-aD 3. i- . nterne5.O.4 4. etre Zee i Signature: _....) ------- 430-98.6 12/0611998 OATP Replacement of latedst control tube assembly P/N 430001-018-101and rework of forward talking P/N,contd OATP C i iiNt Ac p4 iLp Cornier,. lap 1.41114 AT ree4) Once OATP "(IA 1VerseniatZ AlieCCAC-r- 2. 64-4,...ase24.4 -1P c r- 3. L. ntorrieSa..-4 4. rei ad Gr .7-0 4 I Signature: ......,...-- - LAICKan,tele r4/A irti....r.„....---- AleCAtzr 2. E....rerwasaieuec. t..., 3. L. .11Th,rveinsm--1 4. At Auc Col I 430-98-8 31/12/1998 ©ATP Damper blade sot P44 430310-104.105, ineoeuctIonof ©ATP; Cli.".1 A-D akst IA? Cern9g465,2 u'SIN- AT get tC) Once OATP Signature; ----lt 430-99-10 16/12/1999 ®ATP Electrical power distdbution system, Improvements ; OATP CI w Al- Ikrit.9 Cowin-16p F-rimi iti - guild) Once saw r4 A -ftsgmlfrie etteCentg- a V-9-6fraSseast. 40 3. L. natenia,tera 4. on Atfrii toll Signature: 0.------ 1•PrZgarnutte Aistetri- 430-99-11 07105/1999 OATP Autopilot resolver installation Improvement of i ©ATP i el r l4 A 0e.M4'.) • eatriLlep .11114 AT' emilL.N> Once OATP r4 IA 2. arecni-regeN4C tap 3. r.....-n-karnreec.-4 4. erl Ad G ZAW I Signature: 430-99-13 13/12/1999 ©ATP F uel quantity Indicating system calibration ©ATP Cp.4 Ar 6vi Lp eArrIA-41, la illi An— Sudep Once OATP r 4 0 • e- i -e-i-0.4 6 .- rieCe•-•vricr 2. rE,...iCemcbea.4., Ln, 3. I- • Theereacrl 4. en AI5(, Cat Signature as:I/Algae& te-rai i Page c 2 '4..,--------- OATP Printed (Tc-Ninncl L44) AV' liztabO• iMetip et AS& REPAIR STATION IFAA MUM. 01/08/2011 13:37:58 ( .7 .--A....A------ 4 of 5 EFTA01084878 Service Bulletin - Avail Content Revision: 18/07/2011 File ID: *NEW* Aircraft Registration: NI 90 I /Ct.- SB'Number Effective Date Descript on Complied Date Tyne Amendment Number Method of CompllancidApplIcabllity I ., , .. . .. , Once or Recur Next Due ' Date .. Time 1. Facility 3. Cert. Num 2. Cert. Type 4. Author. By Manufacturer Category Model Part N: Bell Helicopter Airframe 430 Serial ft: -490 7 53 430-07-41 RA 1310912007 'RBI-Tail rotor blade rissembly. inspection of r‘i /A siu,_ As6 44-30-67- +I 4 0 AZ C.c>rnet-ill-e4Ca Once r-4/A 1. Pea.", anZ 44-ie-cgAr-r 2, C.-...-rrin-riiCiel-rE, i-r1> 3. L . T74ornoSra•-•I 4. CI Ali 6 Zob-11 ©ATP OATP ©ATP Signature: • ,„,---- 430-07.41 RC 20109/2007 'RBI-Tallrotor blade i issembly, Inspection of NO 5a- As& 14-30 -o7-- Al RP f t w coryeuen4o-E Once r4A -7.:- e low_ Aler-emer 2. G,461,4aiii-).45 LIP 3. I- .Th....-netr.-ra.--1 4, of Aro-G ?all ©ATP OATP ©ATP Signature: .---e .,&..1.4,--, --------- 430-07-41 RD 29111/2010 'RBI-TAIL ROTOR BLADE ASSEMBLY, INSPECTION OF cl AT i i.4 l-96-$ eiV HeS -64, SIr4 TA-ii- Caere'e ..C.L.-r-S. A- 2 (7 i keg- rzt-oeur cat:1%Z ANA-1114d. t gr..7 -le_ s‘m•ra Once s--1Crerarnin-ge_ r‘i )o; Fr‘Cce.4.9- 2. et•Kalo4eatels-1‘ uj 3. i,_. nst-^0.10,--1 4, cal AlsEr 2.041 ©ATP ©ATP .PA, ieystsreq OATP Signature: 430-10-44 18/08/2010 *WOODWARD *WOODWARD HRT-NYDFtAULIC SERVOACTUATOR P/N 222-382- 001.107 MANUFACTURED BY WOODWARD HRT, INSPECTION OF Once 1. 2. 3. 4. ©ATP OATP ©ATP Signature: 430.97.2 11107/1997 Model 430 temporary airspeed restriction NIA Ai 4c-Cei•tr nrtapir,C-p AS ed.hz Ase. 4-3c-97- 4 Once r4/ 4 1. PACrnIpric2 i11ae 2- a.14/t•tri-6 124., e ,--Ti3 3. L. awn(' in.--, 4. of "SG, 'Zerri ©ATP ©ATP' ©ATP Signature: 430-974 19/12/1997 Temporary airspeed iestriction removal of, following limper yoke set P/N 430-310-100101 and,contd. CI t' Al- bort-S) Cennnfturr-4, “irti AT ..‘ii L-5> Recur Ni/4 ccrr,Tht------- . ,ek,rz Ma:ten- 2. a.....r&-....rage...../G Grp 3. 2...../acamP.Sc-J 4, 4,1 f1-4 & Seri i ©ATP CAD, . ©ATP Signature: Corn Pii...64., Ai- athe • to Al PA-IroP of it-or..; ?or t FAA REPAIR STATi NUUY650L les OATP Printed 01/08/2011 13:37:56 ( ----, acte 3 of 5 EFTA01084879 Service Bulletin - Available ComDli Content Revision. 18/07/2011 File ID. NEW Aircraft Registration ni 901 gt_ SB Number Effective Date Deacrir non Compiled Date Time Amendment Number Method of Compliance/Applicability Once or Recur Next Due Date Time 1. Facility 3. Cert. Num 2. Cart. Type 4. Author. By Manufacturer Category Model Part 0: Bell Helicopter Airframe 430 Serial 0: 496.72., 430.04.30 RC 16/0212006 4DATP Tall rotor counterweight bc4Icrank P/N 222-012-727-00a, Removal from service @ATP ~1A plc( e hi la i t._ eare•42.. C3-"-n-trSe it-if-Wait faiscesT-44 t 1-451-14•4_ "0 Once @ATP t4 IA 1. co:a.m.-4.e_ thect.n.c..- 2. 0.46-1.466se4-6- .so 3. L .7-°.--,osc...a 4. el AO& 2Ce4 i Signature: 430.0441 RA 29/11/2004 @ATP Tali rotor blade PIN 222-016-001.123 anc -131, inspection of CIATP, a I u4 (sea- cleknots & I" ..' ",.. re tante./ ilg. .6..vritzr‘ 12/4 in- cit.-04-W '61 A - all i cow AT $76 • err * ires (Ts....0 . Ai...earns*, hiEL,t rig. Palace l'isGwe• P.E..u--roScren..1 Recur NI @ATP I-4 /A • PesSer i n-re ace-cw‘r- 2 ra.-ral...reacc..n.rer urf, 3. i.. • Thc..-nrr ./...•—) 4, of frag ', flit Signature: 430-04-31 RC 31/03/2008 Tail rotor blade P/N i 222-016-001-123, -123M, -131and -139M, inspection arch rework of CAW Clibi (12.zsr- . 4447" 4" to_ rearcencrr) Tie Sowe 9/..-12n- c.0 - cat -Byrn ti-J A - 201 c4,4 Al- 5-71.•01 Akzucs (Testi) Alan prGi H&J tie. acerC- frierv-, ertat..-re.ecte-oa Once SNIP NIA 6.nmnie. Aier-ear 2. rf,d6."..nsee.i...4.- Lilci, 4. coi ad& .q.sra I. CATP Signature: -- 430-04-32 RB 15/03/2006 @ATP ail rotor counterweight bellcrank P/N 222-012-727-10f, Inspection and recall of CAW 1. NM ev-/ fir.1 TA i L Cow& C 11-Gt`r all+414. Recur OATP N/A Pe-amione A-rec - 2. /.....tari.404.C.s....C... 3. L riarneSin-.1 4. of awes 2011 antrffeCtrt65-1Grwr 1.-64-mt.A..firs Signature: 430-05.33 16/020005 CATP introduction of retirement life for the servo actuator to achiator support bolts P/N 50-047C8-31 CATP ' ci t, j AT 7525 • tS kW ergs 02.4-4-17 '2, ryinCler .rAv4 /ells 43O - cis - $i Once ©ATP N A fRatniftle thecears 2' 0.-*P-41C.fsg-nriG 1.4) 3. L..n+..+,..-.PS.tora 4. car ay es 'Zorl Signature: rer 2. 3. 4. 430.07-39 09/01/2007 @ATP Tali rotor pitch change mechanism, Revised rigging procedures CAW ; Once ©ATP Signature: COnnPmetc) Pry !bee. co eilqg f 2,(...... .7010C.- 7-O•I ( *ATP Printed 01/08/2011 13:37:56 ---. Page 1 FM PEPAMSTATION licaptesa 10 '45. 2 of 5 EFTA01084880 Service Bulletin - Available Comalia Content Revision: 18/07/2011 File 1O 'NEW' Aircraft Registration: r-.I 9O1 CI- SE Number Effective On Deecripl! on Complied • .. Dita .rips Amendment Number . Mithod of CoMpilaincalAptilloabillty Once . 'Pi Nil* Due DIM ti Facility :.. ..3; Cert., Num '2; OCart:ifiAgef.**4ti*.iir Manufacturer Category Model Part 0: Bell Helicopter Airframe 430 serial N: 49o79 230-00.18 19/05/2000 Hydraulic actuator apport P/N 222-040-125-001, Inspection of Once 1. 2. 3. 4. CATP CATP OATP Signature: 230-01-20 07/02/2001 Upper fuel enclosure Right side, Addition of drain provision Once 1. 2. 3. 4. ®ATP CAT? *ATP Signature: 430-00-17 19/0512000 Hydraulic actuator st pport P/N 222-040-125-001, Inspection of C. I in/ AT emnit 2 Cannel-16P V41-n-i AT tai ii--3C:. Once hi i A 1. taan.,,,c n-tr2c.ese 2. (EnCriag.atli-rb cSP 3. L. . -roarnosolan-t 4. an Ahffs. ?All CATP CATP CAT? Signature: 430-01-19 22/0212001 Electrical system, improvements CI it,l AT 2X) 1 1-43. C-omet_.14.9 v-lirr-V AT Au, kis> SAO- ASiS v4-5C..-- 9 9 - t o Once NI I A miol.trz. ione..cren- 2. pErfaii-malesm-2. txt> 3. L. -1- Sorennciar.1 4. oi in-JC., gait -Rs,- come lic•-rica-- "IL -. CATP CATP CATP Signature: 430-01.21 07/02/2001 Upper fuel enclosure, tight side, addition of drain protislon ej,,, Arr An p Co enp,A6.O v-ri-n1 A-r- 5;_m-j.) Once (44 - Pe-eFrni sane. 'net -A* 2. 6..44,4644-em-c, tsp 3. L. .TharrteSce-J 4. 01 PVC- 2041 CATP *ATP OAT? Signature: 430-03-33 1110612003 Fuel valve switch. Rewiring of Once c2:5-$ 2. 3. 4. OAT? *DATE CATP Signature: FM REPAIR Mg algemplu6.9 ,ti - 166O. co F- this MIMI. 2orrep at a.r e.c>t I °ATP Printed Ol/08/2017 13:37:56 7..„-------xyk„......--- Pap of 5 ON EFTA01084881 EASA Airworthiness Directive Compliance Record Content Revision 18/07/2011 File ID: NEW Aircraft Registration! NI 9ot Rt_ : EASA AD Number Effective Date • , Desert Aim Compiled . . . ',Date Amendment Number Method of Compliance/Applicability. , Once , or' . Recur. Next Due Date . . ;Time • . 1. Facility 3. Cert. Num 2. Cart Type 4. Author. By Manufacturer Category Model Part St Allison Engine Company Engine 250-C40B Serial #: CAE-5426 67 4. S . tto 2004-0009R2 15112/2004 MAT P Engine control system' pipes- Inspection CATP Once iDATP 1. 2. 3. 4. Signature: E. t i ©ATP ( Printed 29/07/2011 15:50:14 Page 1 of 1 EFTA01084882 FAA Airworthiness Directive Compliance Record Content Revision: 18107/2011 ' File ID: NEW Aircraft Registration: NI 9o1 Rt_ FAA AD Number Effective Date Description Complied Date Time Amendment Number Method of Compliance/Applicability Once or 'Recur Next Due Date Time 1. Facility 3. Cert. Num. 2. Cert. Type 4. Author. By Manufacturer Category Model Part : Allison Engine Company Engine 250-C4OB serial : CAE -$44 0.7 d 044 I 97-25-09 23/12/1997 CATP TO PREVENT FATIGUE FAILURE OF THE HELICAL POWER TAKEOFF GEARSHIFT ASSY, WHICH COULD RESULT IN A LOSS OF,CONTD. . ilsiATP & LT ef(e- , e4< Sr•-..eich-. r-.1,./rriaae ir4Spcii-L-Cto u-4 -eer/4 iS - CEntaLS 026.13 -A -12 -Soca) Once ®ATP NI A 1. ee‘rn,A, Al ece-rWr 2. a-tau.resteLwar.- 4-1-5> 3. L. .-nicunc•Ster-i 4. 29 ..w-1 2,c-i I Signature: 2004-24-09 05/0112005 OATP Superseded by 2008.1644 ©ATP NI /Pc Ste (--RA A9 2ocae -Ho- 04 Once OATP I' VA 1- tanucniz fre.e.C4r-r 2. d:4Q1.-tge.at..tra- Loy 3. L ,11.k..-nrAlma 4. 2-9 7t-n-9 2o11 Signature: 2006-16-04 07/09/2006 ©ATP To minimize the risk of sudden loss of engine power andunoommanded shutdown of the engine due to fuel.conld. ©ATP g ai t,/ (..:AA AD .200.444 it i sac. rs,p4.00) raez..4. cr./Lace° Al 6.,,, 5 .z9:-0 nes isitra., is ec_i _ 20es tf 2 C.L.A. (g44a....9 •44.7.2..a actRaap Per 530 . casts PA-' tep 294x-2°03. (c.i26 - A - 13 - 502., el-) Once ©ATP Ni /A '•liicedenalia. AuZcilith- 2. IF.4.' 16..460-2...-‘6 ,--ZO 3. L _lova, . a4N--t 4. 2-9 nl-p--1 Zott Signature: ( relit+ f ----- w2 2006-20-07 0211112 006 ©ATP To prevent loss of ix wer. possible engine shutdown, or uncontained failure ©ATP L.I tt4 / (ee- ret a...‘ cl2-4-cao) ,. S 4 I F:1-4 Clui-lb7)4 .4 AT 1 l 36-4 IV s >me. as -.)-A.4200i .1t a E.4Ci- (3.441V1) dr.! Ar- tin . ti. t-tez.S .DA-riS.t> 25n-ilia 2ocr7 ea e. -A - -72- So+8) Once @ATP AT Amty 0.16459669 CZ:4%11'MP' Atecerr6- 2' r.Se-f&Ir4a 9-4,44- L.TIO 3. I._ . TscriAPIa-1 4 .2 9 annm 2.4z.i I Signature: .„...._ ,.....,....,--- _ Cornett -6P A-1- learie • ‘-:° nes rEIFR;Jiiknom ,.4.-ret.p. z,.3tiu.-/ tut i tfr4 i ialltY6301 OATP ?,o Fn. Printed 29/07/2011 15:48:32 Pape 5 of 5 EFTA01084883 FAA Airworthiness Directive Content Revision. 18/07/2011 File ID, 'NEW' Aircraft Registration: r•LCIO1 el — FAA AD Number Effective Date Dose' iption Complied Date Time Amendment Number Method of Compliance/Applicability Once I or 'Recur Next Due Date Time. 1. Facility 3. Cert. Num. 2. Cert. Type 4. Author. By Manufacturer Category Model Bell I lelicopter Airframe 430 Part N: Serial #: 49o7E3 2009-08.03 24/04/2009 ©ATP Superseded by 20 i 0.2G-51 CAW Set- FA-4- 49 2010 - 2-‘ -•-ct Once ©MP 1. re.6_,,,,(4•02. ArC.cgol-e- 2. firiGinifft-ei...C. op 3. i.....-n.b.-nraS.-1 4. :9 3,...k.m 2.1.4 t Signature: 2 6''-------- 2. 3. 4. 2010-10-12 16/07/2010 eWrh To detect a crack in the blade. and to prevent loss of the blade and subsequent loss of control of the helicopter SAW Recur ©ATP Signature: 2010-19-51 09/12/2010 SAW To detect corrosion' or a nonconforming grinl relief on the output piston rod atiembly (piston rod),to preventconti ®AT' Once ©ATP 1. 2. 3. 4. Signature: 2010.26.51 25/03/2011 ©ATP To prevent loss of a.blade tip weight loss of a blade, and subsequent loss of control of the helicopter CF-Zed?- - Zed? - Zt RI AafS 4+$0. -7 " 44 elav9 OATIl O4 eftvi a.r...f r-4/A 0'1 St ---1 yir2_ eKA-Apa. lennquxis> ..... ni...1 22.2.- ea 6 - col -I -.3.9m =ii•-.1 A - 2 i-7I iti.-in.iro-46I, z"°7-/e. gtap( fr:Oravn-i 0.-aa.,_ -rawre.-O-4 Once ©ATP NI jA 1. Prailen.rase. Atiecenes- 2. E.444.46c,e+.4c_ u3C3 3. L . Tar-v-rio.-4 4. 2.9 ataft-t 2:04 I Signature: --- -- 6;PrviPt 147 An 166O. oo Alp YM6P 29 -7t.44-1 2OI t tics tti% TalatTiniTiiiON lama wir ©ATP Printed 29/07/2011 15:48:32 Pape 4 of 5 ( EFTA01084884 FAA Airworthiness Directive Compliance Record Content Revision. 18/07/2011 File ID 'NEW Aircraft Registration r-4 90, /2 L FAA AD Number Effective Date Descrip ton Complied Date 'Time . Amendment Number Method of Compliance/Applicability . Once or Recur Next Due Date Time . 1. Facility 3. Cert. Num. 2. Cert. Type 4. Author. By Manufacturer Category Model Part a: Bell Helicopter Airframe 430 Serial #: 49o78 2006-13.14 11/07/2006 CAW To prevent bellcrank failure, loss of a weighted portion of the balk:rank, and subsequent lostd, of control of the,00ntd. CCF- 2tx;:s - 27Ci.) OATU c i tsj ht 798 -8 A/F trey .-PAt1.59 Ot4 ea.ji thy' 14/Pc 64-1 Pin! -rna._ Itc7Prr< Ccts-lreetkiateitic err_LaCarK r r-Larret449 . (As6 a 50 -Pe-33443x awe ) Recur CATP r•VA 1. PaerniPrie. AleCgAll- 2. ariairwirte-s..x, LAp 3. L ..rilrriPa.'-e--.1 4. 2 S 71.-4^1 2.011 Signature: s-7745 Tn4a-i nisis-i m.: sg:Ra il iir 200749-52 05/12/2007 OATP To prevent foss of a blade tip weight, loss of a blade, and subsequent loss of control of the helicopter CATS. 4 1,3 AT lz94,rg trioc de-1 * Pal*, icr5.6.4,107 -rig 6.capg shi ite.- trt ici u4serscreo pe-€O 26.4.64-s6p acy f4.6).- PArdo 19 3Ctil- t.0o7 (92.7. :4 -r-......0 1-/C $4.4spa 57rj A-20 i r4Or A00,-IcaStAS fiLf -tom .4-n-npfia. Once OATP SIgNnatik ure: r1 /A ri.- 23494 t Crie 64=4- 2. Ci.-40-4-tOgreir-rg, 0 -0 3. L . rnornitra.e.- 4. Z• 33.0‘"-1 Zo4 l 2007-26-10 06/02/2008 CATP To prevent fatigue failure of the bolt and subsequent lost. of control of the helicopter dDATP c../Ld AP 751 • la A-/F re acr e /44 ralv-1 AS& 430- OS- 33 CCP-2005-09 ctittc. warre..-5) Once COMP Signature: --- _...,.--.-- 2008-14-01 14/08/2008 OATP To prevent interruption of the fuel supply caused by fa lure of the switch, which could I esuit in loss of ,contd. @ATI' Once eATP 1. 2. 3. 4. Signature: 2008-15-04 03/0912008 SATP To prevent the misatgnment of the tail rotor counterweight bellcrank • CATO Once OATP 1. 2 3 4. Signature: 2008.19.02 16/10/2008 CATP To prevent failure ofthe support and subsequent losS of control of the helicopter war,. Nf CovvIt..t64) 1,4 1114 Ar • J3•4 ti.p AAS 430 - Go- I-7 (CF -Zcoo- Z9 cklx- rect.'s) Recur OATP 4/A 1 AU"-, -,mc inne.e.ati- 2. efiermazdea-11,- ts 3. i...r4:4.--nPlear4 4. ?....133..s...4 Wat i Signature: con,Pri..6.p pm-ap CATP Printed 29/07/2011 15:48:32 AT Ibbo. zsa.-/ C...---e tr oo AIF r.,oil r FMI IrPAITI STAT:ON e INUIZOL i.tc 3 of 5 CfP4 1----- Page EFTA01084885 FAA Airworthiness Directive Compliance Record Content Revision: 18/07/2011 File IO: •NEVV* Aircraft Registration r4 9oi IZ l•-• FAA AD Number 1 Effeativetate • DeloriptIon Complied .Date .-aline r Amendment Number Method of Compllence/Applicability Once • or Recur NextDue Date Time 1. Facility 3. Con. Num 2. Cen. Typo 4. Author. By Manufacturer Category Model Part : Bell Helicopter Airframe 430 Serial : 49o78 2001-01.51 02/03/2001 ©ATP To prevent failure of the supped and subsequent Io.!s of control of the helicopter IDAjtil NIA XAW ASS 4-30- oo - q CCP-. Z000- Z9 °A so f-e-(I-A) SuOisearese) OM FM A9 2008-19-02 lrl attend/4.i e (DeoRes/izenn.s Recur ®ATP a A 1. PearrnAle. AI eck'srr 2. aagrver.6.22.4G- L1-0 3. L...1-No-nrsc-..._, 4, 2.9 dt.n....t zoo Signature. 2001-05-09 24/0412001 4OATP To To prevent loss of electrical power and subsequent kits of control of the helicopter tan' 0 A 11/2 Aige.,244-r-t- Cra.ISTIC.ca-lor..l rJorru3642. (A56/.4.30-99- to 81, CF- Zo-co.-c(4) Once fOATP ni/A .-rraignThi-ra. 4ii2c2442r a Gr4eladdlei.-46 LIT) 3. L. • Tncterarsa...i 4. 29 awl 2.011 Signature: 2002-01-07 21/02/2002 @ATP To prevent failure df both generators, loss of kimary electrical power, & subsequent loss of control of theecorld ®ATP 1•1/A /2 .11 (204511Zocotc>.—i Once man, kVA i0E;i .lr------------ • Mien! 414Z itiergserr 2. I.... ra .aece....r-- 1-rl> a • rannersessJ 4. 2,9 aNAA-1 2c4 I A-ICC-44 Wmtes./C (Mc. 14- 30 - Oi - 9 4 ef-Zzot-3214) Signature: 2002.20-02 Om 112002 OATP To prevent accumulation of fuel In the right-hand upper fuel enclosu re area, a fire, & a sutt.equent forced,contd. ®Are Fot.n...4, L., I ekheiod3u.r C/v4 /sr rt.9Adie tla5 ‘are Ansc.i 17(t4....tto.15-o-i Ciartiti> t,4111-I eistS44,30-et-21 4 ce-20.1-z2 Once @ATP N/A • tokrat r uisiC ecg4A- a fr.r.(4-9Kniatost tap 3. t...-f4orenco--1 4. 2.9 ativ•-f 2011 Signature: 2004-28.11 1870112005 ©ATP Superseded by 200304 -09 CATO hi /A- eta_ FAA 4$) 26:05-04-0, Recur @ATP Kr A • pao..,.„,c,„c. taitte.g - ar-r 2, 6.420 woddratrr 1-re, 3. L. .11amerorSa.-.1 4. Z9 jten..7 Lott Signature: 2005-04-09 04/03/2005 SAW Superseded by 201,?-10-12 CAT; fi_tR._ czAh hp 20)0- to -i2. Recur @ATP PIA • ~Ale insectale-- 2. if..i4-n-hte.,..cd. kin> 3. ‘,./.40.-nr.S.a.-..i 4. 2,1 o......)-r 24pt 1 Signature: CarriPtvap AT iistuo • oc. tariC ' fa offal STATION i, 7~09 2 9 vt-.0-; @ATP Printed 29/07/2011 15:49:32 20I I Page 2 of 5 tiltlYMOL I EFTA01084886 FAA Airworthiness Directive Comoli Content Revision: 18/07/2011 File ID: NEW ' ' Aircraft Registration NI 90 I et_. .f,-.-.FA.*014. - •;,...': ,•,:Et ft* 't - - r Down tionK --. ' .... 1.Complled,.: •-•::...iPil s• 4 1: ; :'. :•;•,;::11nie,:: :, ArnondMerst.Number • Method of ConipNanceiApplIcability - ' PIS*. • _ .,or . Recut Next Due -Date • • : • :Ttrni . '1,:,telkttyl- 3.Cert,Aurft:. lakikeriittlYp,' 4::sicilarr% By ; .-" - - • • ' • _ ., __ Manufacturer Category Model Part 9: Bell Helicopter Airframe 430 Serial ft 4-9o18 97-15.16 24/10/1997 4MTP Superseded by 200D-16-04 @ATP 14 /A .. , 8 -P-e... FAA Ap 1000 .-I 6- 04- Once 1. &OP , hit ituc PPS..,, 412 Al &earl- 2-1-liaarro - is° 3. , ri.krienesio-1 i... 4. 29 ant-I 20..1 t Signature; ......... eir•--•------- - . 7112.6ewiairt_Araci-er-r- 2-614G,- a... taw? 3. L .11kw-riti4w4 4. 29 3vv-i 2..st1 98-24-31 03/0211999 ®ATP To prevent binding a the lateral control tube (control tube) assembly with the inside surface of the forward,contd. OAT? tq A 6 ,-/ Ai ecgia-Pr Cs>sigge-hJertor-1 Nuhriffesa . (Ass tao-93-4. 3 CF - ,i3 - 2,) Once ©ATP NI/A Signature: 1•Sit -'--------- CH • 47124nlIrrie 2. 5.-ictinfactodc. 3. t_..-rikirrie50,..3 4. 29 al.n.4 AitzeRne-i- 99-23.03 19/11/1999 CATP To prevent loss of lc rque of the vertical fin attachment bolts (bolls), which could lead to "racture,conld ©ATI' rliA &. PrieC4A-r—r - cal Recur @ATP r•I/A ,...-c, 200 ta.yrn Sag, 015614-20 - 96-6 4 e.. - 9 e - 21) Signature: 2000-16.04 19/09/2000 ©ATP To prevent lip path plane separation. increased vibrations, damage to the main rotor system. and,contd, ©ATM' cite./ AT 930 .9 A,f tic/ "Arra .° su-.. .,94 id. \Mang 6P Co.•••-•atri,D or 1 ,r1-1 pg,o g it , p6Lvalzy a,...1 A$6'4.3O- 93- IS (As.& /.4.$,..97...z 4 CF- 97- 23q Once !ATP NA • tCe-n 'Alt stiecf-Ae- 2. ry..-r 3. t_ .5,irl6"..A., g-11> 40,-,-.0Sa.-J 4. 29 3,-ils•-i 2011 Signature: -1' W 2000.16-06 20/09/2000 ©ATP To prevent a jammed flight control & subsequent loss of control of the helicopter ©ATP NVA . OW Ai Cc-esiri- (.2o-t5reue.no4 Ni,len &GS CAI'S 'ISO' 991 1 4 cr - 99- 26) Once CATP 'NI/`c e1/4 ,r—1 • Pre.deninii2 An2c.ftwor 2. 644-...,acie•-e.. L-3D 3. j._, inarheSca.-J 4. 2 9 .7t-h-•-r 2ow / Signature: .,..- 2000-22-13 12/12/2000 ©ATP To prevent an inaccirate fuel quantity indicating sistern reading, engine flameout 4w' to fuel slarvation,contd. CATI' is( iA RN Priecemr-s- Cail- re-4C.41or-i rii..)-r-rienva (1564•So - 99-IS il. c.4-2occ.--e-ot) Once ©ATP C--tr- r4 / A 41m14,42 2. IZ_rerndesea-rtw 3. i_. TI.k..,.-wP50...-1 4. 2.9 Toi..--t ..-- c...:O4—.--.----- cheer-4cl- LTP 2011 Signature: qtr.& .4 ' Cov-i.nOndeAP Aft- li:161:1 • ob A-jr #70,1r6.9 2, you,/ Zot I *ATP Printed 29/07/2011 15:48:32 /".. FAA REPAIR STATION MJUY650L Page 1 of 5 EFTA01084887