by date← Jun 10, 2009·Jun 10, 2009 →

EFTA01084848

Dataset 9

June 10, 200940 pages11,960 words

https://www.justice.gov/epstein/files/DataSet%209/EFTA01084848.pdf

Extracted Text

EFTA01084848 Bell 430 Single Pilot IFR PilPremiAir Aircraft Details Serial Number: 49078 Registration: N901RL Manufacturer Date: 2001 Total Time Airframe: 1,660 hrs @ Jan 2010 Location: UK Exterior / Interior Flag blue exterior with Gold accent stripes. Cream leather upholstery in a 5 seat configuration with Equipment cabinet bar (Edwards & Associates interior). • Retractable Undercarriage No known damage history • Pilot and Co-pilot Brakes • Dual Controls Avionics • Air Conditioning • Avionics Master Switch • VIP Step R/H passenger side • Gold Crown Wiring Harness • Particle Separator • Dual AFCS w/Flight Director • Bleed Air Environmental Control System • Four Tube EFIS • Cockpit Boost Fan for ECS • Dual King Gold Crown KTR-908 • Dual Flight Controls • Dual Nav KNR-634 • Retractable Wheel Gear • DME KDM-706 • Co-Pilot Wheel Brakes • Garmin GNS 500 • Shadin Fuel Flow Indicators on IIDS • ADF KDF 806 • 48 Gal. Auxiliary Fuel Tank • Transponder MST-67A • Heated Glass Windshield • PS Engineering PAC 24 Audio Panel • Ice/Refreshment Drawers • RDR 2000 Weather Radar • Wool Carpet • Radar Altimeter • Custom cockpit storage • ELT- 406 mhz • Quiet Zone Interior • Standby Attitude Ind. 3" • Engine Plugs and Covers • Honeywell KTA870 TAS System • Forward recognition lights with pulse • Bose Headsets • Whelen Strobe Light System with end lights on horizontal stabilizer Engines • LED Lower Anti-Collision light Two Allison 250-C408 engines • Devore tail rotor floodlight system • Dual Pane Windows 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 • Thermal/Acoustic Insulation System for Specification is subject to verification by the purchaser soundproofing cabin. • Cabin door activated overhead dome lights 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 EFTA01084849 Bell 430 S/N 49078 NPremiAir Globat Major Component / Engine Status Time Remaining COMPONENT Main Rotor Blade x .1 SLUTS° (hrs) On Condition I Time Remaining (hrs) j (%) Main Rotor Yoke 3.340 SO Cs° I Main Rotor Mast Assembly 5.000 3.340 Main Rotor Swash Plate 5,000 3.340 66 i Main Drive Shaft Left & A t'7 5 Finn 5IS t yr 3r-nt is 25- x Transmission 5,000 3.340 66% I Tail Gearbox 5.000 3.340 2,500 I 2,197 87", Tad Rotor Hub 5.000 4.320 86"0 Tail Rotor Blade Rotor Ellade t.. , • 5,000 5,000 100% Tail Rotor Yoke 5.000 3.340 66nx Engine #2 ENGINES L SLL/TBO Remaining Engine #1 Remaining 1 Remaining Remaining (hrs) (hrs) (%) (hrs) (%) 1,775 1 1,726 97% 1.726 97% 1 15* Stage Turbine Wheel I 1,775 1 .726 97% 1.726 97', 2.- Stage Turbine Wheel 2,890 64% I 2,890 64% 3rd Stage Turbine Wheel I Li Stage Turbine Wheei :4;3:.11/ 0 rn. 5,857 78% 5.840 Engine Gearbox On Condition 340 17% 345 Compressor Bleed Valve 1.50c 747 24% la I Starter Generator 1.000 320 32% 930 93% (torn rho MA Ihout prior notice The offer for sale of this aircraft is setyea to contract and the aircraft may at any time be withdrawn 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 PremiAir Aircraft Engineering Ltd Hours Cycles Landings Aircraft Compliance Report Current Airframe as of 28/09/2009 1660:00 0 0 Aircraft: N901RL Customer. BOVALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component Times 11$1,7010 hat 13:41:35 Page Airframe - Curren Intervals Tolerance Last Done Next Due Remaining MCN 2430-0000 Battery CAP check PN TSP-283 SN Since OH 01/10/2039 Calendar Overhaul 4M 10801683 06/10/2009 01/02/2010 21d Desc BATTERY Wa Hours Na 1660:00 Na n/a ATA 24-30.00 DC GENERATION rya Cycles Na Na Na Na Position N/A 4'a Landings Na Na Na Na Condition SERVICEABLE NOTE: Calendar based on Overhaul. MCN 2620-1000 fire Extinguisher Cor tamer - Left. Hydro check. Data reference: BHT-430-MM-3. PN 222.369-911-001 SN A37870A1 Since OM 01/03/2C Calendar Overhaul by 01/03/2005 01/03/2010 1m 21d Desc CONTAINER, ENG. FIRE 1660 l Hours Na Na Na ATA 26-20-00 FIRE EXTINGUISHING r a Cycles Na Na Na Position LEFT I-7a Landings ‘i Na Na Na Condition SERVICEABLE NOTE: Calendar based on Overhaul. MCN 2620-2000 Fire ExtIngUISher Container - Right. Hydro check. Data reference: BHT-430-MM-3. PN 222.369-911.001 Since OH 01/03/2055 Calendar Overhaul 5Y 01/03/2005 SN 38013A1 01/03/2010 1m 21d Desc CONTAINER, ENG. FIRE 1660:00 Hours Na Na Na Na ATA 26-20-00 FIRE EXTINGUISHING ha Cycles ; Na Na Na Na Position RIGHT Landings Na Na Na Na Condition SERVICEABLE NOTE: Calendar based on Overhaul. MCN 6200-1050 Main Rotor Pitch Link PN 430.010.411-105 Since New ria Calendar Retirement Na 02/04/2001 SN TY0350 Na Na Desc LINK, MR PITCH 1660± Hours 10000:00 Na 10000:00 8340:00 ATA 62-00-00 MAIN ROTORS Cycles Na Na Na Na Position BLUE Landings Na Na Na Na Condition NEW MCN 6200.2050 Main Rotor Pitch Link. PN 430.010-411-105 Since New n'a Calendar Retirement Na 02/04/2001 SN TY0351 n/a Na Dose LINK. MR PITCH 1660:00 Hours 10000:00 Na 10000:00 8340:00 ATA 62-00-00 MAIN ROTORS rva Cycles Na Na Na Na Position ORANGE Landings n/a n/a Na Na Condition NEW AvaSt SYSIEYS tr.0 EFTA01084850 PremiAir Aircraft Engineering Ltd Current Airframe as of 28/09/2009 Hours 1660:00 Cycles 0 Landings 0 Aircraft Compliance Report 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 Main Rotor Pitch Link.: PN 430-010-411-107 Na 02104/2001 Na nra Since New Ka Calendar Retirement SN TY0344 1660:0) Hours 10000:00 Na 10000:00 8340:00 Dose LINK, MR PITCH NA Cycles Na Na Na Na ATA 62-0000 MAIN ROTORS Position RED nta Landings rile ilia nta iva Condition NEW MCN 6200-4050 Mein Rotor Pitch Link. PN 430-010-411-107 na 02/04/2001 Na n/a Since New Calendar Retirement Na SN TYD343 8340:00 1660:03 Hours 10000:00 Na 10000:00 Desc LINK, MR PITCH ma Cyclos Na Na n/a Na ATA 62-00-00 MAIN ROTORS Position GREEN rya Landings Na Na Na Na Condition NEW MCN 6210-1000 Main Rotor Blade. PN 430-015.001.123 Na 02/04/2001 n/a Na On Condition 02/04/2001 Calendar SN A-1265 ilia Na 166010 Hours n/a Na Desc BLADE, MAIN ROTOR Cycles Na Na Na Na ATA 62-10.00 MAIN BLADES Position BLUE L N Landings Na n/a Na Na Condition NEW MCN 6210-2000 Main Rotor Blade. PN 430-015.001.123 Calendar Na 02/04/2001 Na Na On Condition 02,04/2001 SN A-I248 Na 1660:C0 Hours Na Na Na Dose BLADE. MAIN ROTOR 3 Cycles Na Na Na Na ATA 62-10-00 MAIN BLADES Position ORANGE 0 Landings n/a Na n/a Na Condition NEW MCN 6210-3000 Main Rotor Blade, PN 430.015.001-123 02/04/20,61 Calendar Na 02/04/2001 Na Na On Condition SN A-1229 Na 166040 Hours Na Na Na Dose BLADE. MAIN ROTOR ,0 Cycles Na n/a Na Na ATA 62-10.00 MAIN BLADES Position RED 0 Landings Na Na Na Na Condition NEW Av•13ASE STSIEmS Inc • 13 EFTA01084851 PremiAir Aircraft Engineering Ltd Hours Cycles Landings Aircraft Compliance Report 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 Pr/Med:114)MM Tkne: 13.41:35 Page: 3 Airframe Curren. Intervals Tolerance Last Done Next Due Remaining MCN 6210-4000 MaIn Rotor Blade. PN 430-015-001-123 SN On Condition 02/04/2(01 Calendar Na 02/04/2001 A-1249 n/a Na 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 SN A-000181 Na Na 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 SN A-0834 Na Na Dose PIN, MR BLADE 1660. iC Hours 10000:00 Na 10000:00 8340:00 ATA 62-20-00 MAIN HEADS r'i, Cycles Na n/a Na n/a Position #1 r ',7, Landings Na Na Na Na Condition NEW MCN 6220-1060 Main Rotor Blade Pin. PN 430-010-127.101 Since New iva Calendar Retirement Na 02/04/2001 SN A-0871 Na Na 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 Na Calendar rveri 02/04/2001 Na n/a Since New Retirement 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 Main Rotor Damper Blode Set. PN 430-310-104-105 r a Calendar 02/04/2001 ilia Since New Retirement n/a n/a SN LK0487 Desc 16601 5 Hours 10000:0D Na 10000:00 8340:00 DAMPER BLADE SET ATA 62-20-00 MAIN HEADS n a Cycles Na Na n/a Na Position #1 na Landings Na Na n/a Na Condition NEW MCN 6220-1250 Main Rotor Shear Res;raint. PN 430310.101.107 Na Na Since New r /a Calendar Retirement n/a 25110/2005 SN LK1360 Desc 750:c:8 Hours 10000:00 909:12 10909:12 9249:12 RESTRAINT. MR SHEAR ATA 62-20-00 MAIN HEADS n a Cycles Na Na Na Na Position #1 n 'a Landings Na n/a Na nia Condition NEW MCN 6220-1300 Main Rotor Clamp Pie a Set. PN 430-010-105-105 Since New r !a Calendar Retirement Na 02/04/2001 Na Na SN A-556 Desc PLATE SET. CLAMP 166010 Hours 10000:00 Na 10000:00 8340:00 ATA 62-20-00 MAIN HEADS n'a Cycles Na n/a n/a Na Position #1 n'a Landings n/a Na ilia Na Condition NEW MCN 6220-1350 Main Rotor Drive Ousbina. PN 430-010-124-103 r /a Calendar Since New Ftetiretnent Na 02/04/2001 Na n/a SN A-304 Dose BUSHING. MR DRIVE 1660:00 Hours 5000:00 Na 5000:00 3340:00 ATA 62.20.00 MAIN HEADS rasa Cycles Na Na n/a Na Position #1 nia Landings Na Na n/a Na Condition NEW Av•BASE SYSTEMS PC 13 EFTA01084853 PremiAir Aircraft Engineering Ltd Hours Cycles Landings Aircraft Compliance Report 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 SN A-308 Na Na 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 Main Rotor Yoke - Dam PN 430-010-101.101 On Condition Calendar Na 02/04/2001 Na SN A-173 Na Desc YOKE. MAIN ROTOR 1660 00 Hours Na Na Na Na ATA 62-20-00 MAIN HEADS 0 Cycles Na Na Na Na Position UPPER 0 Landings Na Na Na Na Condition SERVICEABLE MCN 6220-2050 Main Rotor Blade Pin PN 430-010.127-101 Since New va Calendar Retirement Na 02/04/2001 SN A-0823 Na Na Desc PIN. MR BLADE 1660:10 Hours 10000:00 Na 10000:00 8340:00 ATA 62.20-00 MAIN HEADS i /a Cycles Na Na Na Na Position #2 r ta Landings Na Na Na Na Condition NEW MCN 6220-2060 Main Rotor Blade Pin PN 430-010-127.101 Since New Calendar Retirement Na 02/04/2001 SN A-0839 Na n/a Desc PIN. MR BLADE us;)(: >1 Hours 10000:00 Na 10000:00 8340:00 ATA 62.20-00 MAIN HEADS i , Cycles Na Na Na Na Position #2 r s Landings Na n/a Na Na Condition NEW MCN 6220-2100 Main Rotor Adaoter PN 430-010.109-101 Since New Na Calendar Retirement Na 02/04/2001 Na SN A-373 Na Desc ADAPTER. MR BLADE 1660:00 Hours 10000:00 Na 10000:00 8340:00 AM 62.20-00 MAIN HEADS Na Cycles Na Na Na Na Position #2 a Landings Na n/a Na Na Condition NEW EFTA01084854 PremiAir Aircraft Engineering Ltd Hours Cycles 0 Landings 0 Aircraft Compliance Report Current Airframe as of 28/09/2009 1660:00 Aircraft: N901RL 3OVALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component Times Airframe Printed: 11 er 2010 17nm:13:41:36 Page: 6 Current Intervals Tolerance Last Done Next Due Remaining MCN 6220-2150 Main Rotor Pitch Horn, PN 430.010-115-101 Since New nMa Calendar Retirement Na 02/04/2001 n/a Na SN A-393 1660:00 Hours 10000:00 Na 10000:00 8340:00 Desc HORN. MR PITCH ATA 62-20-00 MAIN HEADS Cycles Na Na Na Na Position 62 n.•a Landings Na Na Na Na Condition NEW MCN 6220.2200 Main Rotor Damper BI ide Set. PN 430-310.104-105 Calendar 02/04/2001 Na Na Since New Retirement Na SN LK0462 8340:00 I 660 ' Flours 10000:00 Na 10000:00 Dose DAMPER BLADE SET Cycles Na Na Na Na ATA 62-20-00 MAIN HEADS Position 02 Landings Na Na Na Na Condition NEW MCN 6220.2250 Main Rotor Shear Res mint. PN 430-310-101.107 Na 25/10/2005 Na Na Since New Calendar Retirement SN LK1312 9249:12 750:48 Hours 10000:00 909:12 10909:12 Desc RESTRAINT. MR SHEAR a Cyc'es Na Na Na Na ATA 62-20-00 MAIN HEADS Position e2 Landings Na Na Na Na Condition NEW MCN 6220-2300 Main Rotor Clamp Pla e Set. PN 430-010.105-105 Since New Calendar Retirement Na 02/04/2001 Na n/a SN A-550 8340:00 1660 ( ( Hours 10000:00 Na 10000:00 Desc PLATE SET. CLAMP nx Cycles Na Na Na Na ATA 62-20-00 MAIN HEADS Position ft2 Landings Na Na n/a Na Condition NEW MCN 6220-2350 Main Rotor Drive Buslast, PN 430-010-124-103 Retirement Na 02/04/2001 Na Na Since New r✓a Calendar SN A-271 334000 1660:$0 Hours 5000:00 Na 5000:00 Dose BUSHING. MR DRIVE a Cycles Na Na Na Na ATA 62-20-00 MAIN HEADS Position #2 18 Landings Na Na Na Na Condition NEW ♦VBSSE StS7E450.0 EFTA01084855 PremiAir Aircraft Engineering Ltd Hours Cycles Landings Aircraft Compliance Report 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 Printed: II/MOW Tane:13.41:38 Page: 7 Airframe Currer t Intervals Tolerance Last Done Next Due Remaining MCN 6220-2360 Main Rotor Drive Bus Nine. PN 430-010.124-103 A-3O1 Since New Calendar Retirement Na 02/04/2001 SN Na Na Desc BUSHING. MR DRIVE 1660 00 Hours 5000:130 n/a 5000:00 3340:00 ATA 62-20-00 MAIN HEADS Cycles Na n/a Na Na Position 02 Landings Na Na Na Na Condition NEW MCN 6220-2500 Main Rotor Yoke • Lover. PN 430-010.101.101 SN On Condition Calendar Na 02/04/2001 n/a A-168 n/a Den YOKE. MAIN ROTOR 1660 )0 Hours Na Na Na Na ATA 62-20-00 MAIN HEADS 0 Cycles Na n/a Na Na Position LOWER 0 Landings Na Na n/a Na Condition SERVICEABLE MCN 6220-3050 Main Rotor Blade Pin PN 430-010-127-101 Since New va Calendar Retirement Na 02/042001 SN A -O882 n/a n/a Desc PIN. MR BLADE 1660: Xi Hours 10000:00 Na 10000:00 8340:00 ATA 62.20-00 MAIN HEADS Cycles Na Na Na Na Position #3 I is Landings Na Na Na Na Condition NEW MCN 6220-3060 Main Rotor Blade Pin PN 430-010.127-101 Since New t).1a Calendar Retirement Na 02/04/2001 SN A-O869 Na Na Desc PIN, MR BLADE 1660- X Hours 10000:00 Na 10000:00 8340:00 ATA 62-20-00 MAIN HEADS i ,i. Cycles Na Na Na Na Position 113 I PZ. Landings Na Na Na Na Condition NEW MCN 6220-3100 Main Rotor Adapter. PN 430-010-109-101 Since New Calendar Retirement Na 02/04/2001 Na SN A-535 Na Dosc ADAPTER. MR BLADE i 66O:CC Hours 1000000 Na 10000:00 8340:00 ATA 62-20-00 MAIN HEADS Cycles Na n/a Na Na Position #3 r 'a Landings Na Na Na Na Condition NEW Ai &St.( 'AVA AA: I". EFTA01084856 PremiAir Aircraft Engineering Ltd Hours Cycles landings Aircraft Compliance Report Current Airframe as of 28/09/2009 1660:00 0 0 Aircraft: N901RL Customer: SOVALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component Times — Akfrturre Printed: 111972070 time: 73:41:36 Page: 8 Intervals Tolerance Last Done Next Due Remaining MCN 6220-3150 Main Rotor Pitch Horn. PN 430-010-115-101 02/04/2001 Na Since New rVa Calendar Retirement Na Na SN A-363 1660:C0 Hours 10000:00 Na 1000090 834090 Desc HORN, MR PITCH ATA 62-20-00 MAIN HEADS Na Cycles rea Na Na Na Position 03 na Landings Na Na Na Na Condition NEW MCN 6220-3200 Main Rotor Damper BlaSbi a PN 430-310-104-105 Na Na Since New tiro Calendar Retirement Na 02/04/2001 SN LK0471 1660-.0 0 Hours 10000:00 n/a 10000:00 8340:00 Desc DAMPER BLADE SET ATA 62-20.00 MAIN HEADS na Cycles Na Na Na Na Position 03 na Landings Na Na Na Na Condition NEW MCN 6220-3250 Main Rotor Shear Res raint. PN 430.310-101.107 Na n/a Since New Calendar Retirement Na 25✓10/2005 SN 11(1322 750.'8 Hours 10000:00 909:12 10909:12 9249:12 Desc RESTRAINT, MR SHEAR 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 Na Na Since New r/a Calendar Retirement Na 02/04/2001 SN A-529 1660:00 Hours 10000:00 Na 10000:00 8340:00 Dew PLATE SET. CLAMP 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 02/04/2001 Na Na Since New Na Calendar Retirement Na SN A-299 1660:00 Hours 500090 Na 5000:00 334090 Desc BUSHING, MR DRIVE ATA 62-20-00 MAIN HEADS n'a Cycles Na Na Na Na Position 03 Ca Landings n/a Na Na Na Condition NEW ♦v4ASE SYSTEWS INC EFTA01084857 PremiAir Aircraft Engineering Ltd Hours Cycles Landings Aircraft Compliance Report Current Airframe as of 28/09/2009 1660:00 0 0 Aircraft: N901RL Customer '0VALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component Times prised: I IV1/2010 Tlintx t3tIt:36 Pane 9 Alrftame 0' Intervals Tolerance Last Done Next Due Remaining MCN 6220-3360 Main Rotor Drive Bur hinq. PN 430-010-124-103 Since New a'a Calendar Retirement n/a 02/04/2001 SN A-267 Na n/a 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 va Calendar Retirement Na 02/04/2001 SN A-0879 Na Na 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 SN A-0841 Na n/a 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 SN A-199 Na Na 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 SN A-376 Na Desc HORN, MR PITCH 1660.00 Hours 10000:00 n/a 10000:00 8340:00 ATA 62-20.00 MAIN HEADS rra Cycles Na Na Na Na Position e4 Na Landings Na Na Na Na Condition NEW AV•8ASE SYSTEMS INC. • *3 EFTA01084858 PremiAir Aircraft Engineering Ltd Current Airframe as of 28/09/2009 Hours 1660:00 Cycles 0 Landings 0 Aircraft Compliance Report 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 1660 CO Hours 10000:00 We 10000:00 8340:00 Dose DAMPER BLADE SET n,a Cycles Ilia Na Na Na ATA 62-20-00 MAIN HEADS Position 04 n, a Landings Na Na Na Na Condition NEW MCN 6220-4250 Main Rotor Shear Res mint. PN 430.310.101-107 Na 25/10/2005 Na Na Since New ra Calendar Retirement SN 0(1323 750 / 9 Hours 10000:00 909:12 10909:12 9249:12 Dose RESTRAINT. MR SHEAR na Cycles Na Na ilia Na ATA 62-20-00 MAIN HEADS Position 04 na Landings nee Na Na Na Condition NEW MCN 6220-4300 Main Rotor Clamp Pla e Set. PN 430-Ot0.105.105 Na 02/04/2001 Na Na Since New r 'a Calendar Retirement SN A-534 8340:00 1660 ( 0 Hours 11X/00M rile 10000:00 Dose PLATE SET. CLAMP na Cycles Na Na ilia Na ATA 62-20-00 MAIN HEADS Position 04 na Landings Na Na Na Na Condition NEW MCN 6220.4350 Main Rotor Drive Bushing. PN 430-010-124-103 Since New r Calendar Retirement Na 02/04/2001 n/a Na SN A-276 3340:00 1660(10 Hours 5000:00 Na 5000:00 Dose BUSHING, MR DRIVE in a Cycles Na n/a Na Na ATA 62-20-00 MAIN HEADS Position 04 Landings Na Na Na Na Condition NEW MCN 6220-4360 Main Rotor Drive Bus ling, PN 430-010.124.103 02/04/2001 Na Na Since New Calendar Retirement Na SN A-307 1660: IC Flows 5000:00 Na 5000:00 3340:00 Dose BUSHING. MR DRIVE r la Cycles Na Na Na Na ATA 62-20-00 MAIN HEADS Position 04 Landings n/a Na Na Na Condition NEW 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: N901RL Customer BOVALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component Times Primed: trOl/20to now 12:47:37 Peet I / Airframe Currer Intervals Tolerance Last Done Next Due Remaining MCN 6230-0000 Main Rotor Mast Ass :rnbly. PN 430-110-400-105 SN Since OH Na Calendar Overhaul Na A-82 10/07/2009 n/a Na Desc MAST ASSEMBLY 1660 00 Hours 5000:00 1611:00 5000:00 3340:00 ATA 62.30-00 MAIN MAST/SWASHPLATE Va Cycles Na Na n/a n/a Position ONLY tlfa Landings Na Na n/a n/a Condition REPAIRED MCN 6230-0100 Main Rotor Mast. PN 430-040-130-115S SN Since New La Calendar Retirement Na DN190 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 430-010-410-101 Since New Va Calendar Retirement Na 02/04/2001 SN RE91 Na Na Dose HUB. SP DRIVE 1660:J0 Hours 10000:00 Na 10000:00 8340:00 ATA 62-30-00 MAIN MAST/SWASHPLATE Na Cycles Na Na Na Na Position ONLY Na Landings Na n/a Na Na Condition NEW MCN 6230-0160 1. Main Rotor Swasholap Drive Idler Link. PN 430-010-409-105 SN Since New Na Calendar Retirement Na 02t04/2001 RE109 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 SN RE91 Na Na Dose LINK. SP DRIVE 1660:60 Hours 10000:00 n/a 10000:00 8340:00 ATA 62-30-00 MAIN MAST/SWASHPLATE 4a Cycles Na Na Na Na Position ONLY Landings Na n/a Na Na Condition NEW AY -USE SYSIEPOSOC • V& EFTA01084860 PremiAir Aircraft Enqineerinq Ltd Hours 1660:00 Cycles 0 Landings 0 Current Airframe as of 28/09/2009 Aircraft Compliance Report 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 1660:03 Hours 5000:00 Na 5000:00 3340:00 Desc SWASHPLATE, MR 717.71 Cycles Na Na Na n/a ATA 62-30-00 MAIN MAST/SWASHPLATE ro e Landings Na Na Na Na Position ONLY Condition SERVICEABLE MCN 6230-0250 Main Rotor Swash plat SUWON. PN 430-010.404-101 na Calendar Retirement Na 02/04/2001 n/a Na Since New SN A-114 1660 ( .) Hours 1000010 Na 10000:00 8340:00 Desc SUPPORT. SWASHPLATE 11 1 Cycles Na Na Na Na ATA 62.30-00 MAIN MAST/SWASHPLATE Landings ilia Na Na Na Position ONLY Condition NEW MCN 6230-0300 Main Rotor Swashplat ) Ball and Sleeve. PN 430-010.403-105 rfa Calendar Retirement Na 02/04/2001 Na Na Since New SN A-139 Na 10000:00 8340:00 1660:60 Hours 10000:00 Desc SLEEVE. BALL n`a Cycles Na Na Na Na ATA 62-30-00 MAIN MAST/SWASHPLATE n'a Landings Na n/a Na Na Position ONLY Condition NEW MCN 6230-0350 Main Rotor Swashplai a Non-Rotating Ring. PN 430-010-402-101 Since New r . Calendar Retirement Na 02104/2001 Na Na SN RE97 nia 10000:00 8340:00 660 i 0 Hours 1000010 Desc RING, SP NONROTATING rva Cycles Na n/a Na Na ATA 62-30-00 MAIN MAST/SWASHPLATE r a Landings Na Na Na n/a Position ONLY Condition NEW MCN 6230-0400 Main Rotor Swasholale Rotating Ring. PN 430-010-401-105 Na Calendar Retirement Na 02/04/2001 Na Na Since New SN RE90 n/a 10000:00 8340:00 1660:00 Hours 10000:00 Dose RING. SP ROTATING n/a rya Cycles Na Na Na ATA 62.30-00 MAIN MAST/SWASHPLATE a Landings Na Na Na Na Position ONLY Condition NEW AV-BASE SYSTEMS PC 13 EFTA01084861 PremiAir Aircraft Engineering Ltd Hours Cycles Landings Aircraft Compliance Report Current Airframe as of 28/09/2009 1660:00 Aircraft: N90IRL Customer4 BOVALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component Tenn Airframe Printed: 11O12010 nriw: t3:41:37 Pay.: 13 Currerf Intervals Tolerance Last Done Next Due Remaining MCN 6230.0450 Collective Lever. PN 430-010-405-105 SN Since New Na Calendar Retirement Na A-108 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 SN RE91 Na Na 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 SN A-229 Na Na 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 SN RE186 Na Na 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 SN ST-71 Na Na 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 Hours 1660:00 .,[1:anqs 0 Aircraft Compliance Report Current Airframe as of 28/09/2009 Aircraft: N901RL Customer: 3OVALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component Times Air hank, Printed: 11912010 Time: 13:41:38 Page: (4 Current Intervals Tolerance Last Done Next DUO Remaining MCN 6230-1600 Cyclic Link - Left. PN 430-010412-105 Na n/a Since New Na Calendar Retirement n/a 02/04/2001 SN RE258 1660:00 Hours 10000:00 n/a 10000:00 8340:00 Desc LINK, CYCLIC na Cycles Na Na Na Na ATA 62-30-00 MAIN MAST/SWASHPLATE Position LEFT na Landings Na Na Na Condition NEW MCN 6230-2460 Main Rotor Swash plat .t Ball Sleeve to Collective Lever Pin - Right. PN 430-010-442-101 a Calendar Retirement n'a 02./04/2001 Na Na Since New SN A-236 3340:00 1660.(0 Hours 5000:00 Na 5000:00 Desc PIN n a Cycles Na nta Na Na ATA 62-30-00 MAIN MAST/SWASHPLATE Position RIGHT na Landings Na Na n/a Na Condition NEW MCN 6230-2550 Cyclic Lever - Right. PN 430-010-406-101 r 02104'2001 Na Na Since New Calendar Retirement Na SN RE184 10000:00 8340:00 1660.(0 Hours 1000060 Na Desc LEVER. CYCLIC na Cycles Na Na Na Na ATA 62-30-00 MAIN MAST/SWASHPLATE Position RIGHT r a Landings Na Na Na Condition NEW MCN 6230-2560 Main Rotor Swasnolal a Collective Lever to Cvellc Lever Pin - Right. PN 430-310-455-101 /a Calendar Retirement 02/04/2001 n/a Na Since New n/a SN ST-101 Na 5000:00 3340:00 1660x0 Hours 5000:00 Desc PIN, CYCLIC ,a Cycles Na n'a Na Na ATA 62-30-00 MAIN MAST/SWASHPLATE Position RIGHT rt 'a Landings Na Na Na Na Condition NEW MCN 8230-2600 Cyclic Link - Rlaht, PN 430-010-412.106 Since New Na Calendar Retirement Na 02/04/2001 Na Na SN RE277 1660:p0 Hours 10000:00 Na 10000:00 8340:00 Dose LINK. CYCLIC Na Cycles Na Na Na Na ATA 62-30.00 MAIN MAST/SWASHPLATE a Landings Na Na Na Na Position RIGHT Condition NEW l AY43ASE SYSTEVS Pic • Is EFTA01084863 PremiAir Aircraft Engineering Ltd Hours Cycles Landings Aircraft Compliance Report Current Airframe as of 28/09/2009 1660:00 0 0 Aircraft: N9O1RL Customers BOVALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component Thies Printed: I miaow Tint I3:41:all Page T.5 Airframe Currer: Intervals Tolerance Last Done Next Due Remaining MCN 6310-1050 Main Drive Shaft - Lag, PN 222-044.885105 SN A-1109 Since 0/H 14/04/2006 Calendar Overhaul 5Y 14/04/2006 14/04/2011 4, 3m 3d 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 SN Since OH 14:04:2(06 Calendar Overhaul 5Y 14/04/2006 A-1087 14/04/2011 1y 3m 3d 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 Since Map ria Calendar Inspection Na 02/04/2001 SN A 85 Na lira Desc TRANSMISSION. MAIN 1660 IC 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 SN A-303 Na Na Desc SUPPORT. ACTUATOR 1660:(0 Hours 5000:00 5000:00 n/a 3340:00 ATA 63-30.00 M'R GEARBOX MOUNTS n a Cycles Na n/a Na Na Position ONLY 0a Landings Na Na Na Na Condition NEW ALSALSE SYMMS INC EFTA01084864 PremiAir Aircraft Engineering Ltd Hours Cycles 0 Landings 0 Aircraft Compliance Report Current Airframe as of 28/09/2009 1660:00 Aircraft: N901RL Customer: 30VALE DEVELOPMENTS Make/Model: BELL 430 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 n'a Calendar Retirement Na 02/04/2003 Na Na Since New SN LK0255 1210.00 Hours 10000:00 450:00 10450:00 8790:00 Desc MOUNT. PYLON Na Cycles Na n/a Na Na ATA 63-30-00 M/R GEARBOX MOUNTS 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 02/04/2003 n/a Na Since New wa Calendar Retirement Na SN LK0306 1210:C0 Hours 10000:00 450:00 10450:00 8790:00 Dose MOUNT. PYLON na Cycles n/a Na n/a Na ATA 63-30-03 WA GEARBOX MOUNTS Position RIGHT nia Landings n/a n/a Na Na Condition NEW ---- MCN 6410-1000 Tail Rotor Blade. PN 222.016-001-t39M Na 08/03/2008 Na Na Since New i-7a Calendar Retirement SN A-2171 4320:54 679:(6 Hours 5000:00 135701 5980:54 Desc BLADE. TAIL ROTOR na Cycles Na Na rtia n/a ATA 64-10-00 T/R BLADES Position Al na Landings Na Na n/a n/a Condition REPAIRED MCN 6420-0000 Tail Rotor Hub. PN 222-012.701.135FM Na 07/03/2008 n/a n/a Since 0 H a Calendar Overhaul SN A-473 3857:01 2197:01 302: Hours 250000 1357:01 Desc T/R HUB a Cycles Na Na Na Na ATA 64-20-00 T/R HEADS Position ONLY d'a Landings n/a Na Na Na Condition REPAIRED MCN 6420-0050 Tall Rotor Trunnion. 5 PN 222.012-703-107 Calendar Retirement Na 07/03/2008 Na Na Since New Afa SN A•105 3340:00 166010 Hours 5000:00 1357:01 5000:00 Desc TRUNNION. TAIL ROTOR n'a Cycles Na Na Na Na ATA 64-20-00 T/R HEADS Position ONLY r .ta Landings n/a Na Na Na Condition OVERHAULED AYSASE SYMMS INC • 13 EFTA01084865 PremiAir Aircraft Engineering Ltd Aircraft Compliance Report Hours Cycles Landings Current Airframe as of 28/09/2009 1660:00 0 0 Aircraft: N901RL Customeri BOVALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Printed: 119120,0 Component Times Tem l3:41all Pepe 17 Currer I Airframe Intervals Tolerance Last Done Next Due Remaining MCN 6420-0100 Tail Rotor Yoke. PN 222-012-702-109 SN A-470 Since New ra Calendar Retirement Na 07/03/2008 ilia Dose YOKE. TAIL ROTOR 1660 DO Hours n/a 5000:00 1357:01 5000:00 ATA 64-20-00 T/R HEADS Cycles 3340:00 Na Na Na Position ONLY Landings Na Condition SERVICEABLE Na n/a Na Na MCN 6510-1200 Tall Drive Shaft Hangar - Forward. PN 222-044-003-Wr t SN 5MAY07-04 On Condition Calendar Na 25/01)2007 Na Disc HANGER, TAIL ORVSHFT 523 36 Hours n/a • . Na 1136:24 Na ATA 65-10-00 T/R DRIVE SHAFT 0 Cycles Na Na Na n/a Position FORWARD 0 Landings Na Condition SERVICEABLE n/a Na Na n/a MCN 6510-1250 Tail Drive Shah Hangar Bearing - Forward. PN 222.344-606.103 SN MB629 Since New 25/01,2(0? Calendar Retirement 3Y 25/01/2007 25/01/2010 14d Dose BEARING. TRDS 523:36 Hours 3000:00 1136:24 4136:24 2476:24 ATA 65-10-00 T/R DRIVE SHAFT n/2. Cycles Na Position FORWARD n/a Na Na rd:. Landings Na Condition NEW Na Na n/a MCN 6510-2200 Tall Drive Shaft Hangit - Center. PN 222-044003404 • c"., SN 15MAY07-05 On Condition Calendar Na ), 25101/2007 Na Na Dose HANGER. TAIL ORVSHFT 52&16 Hours MI 113624 Na Na ATA 65-10-00 T/R DRIVE SHAFT 0 Cycles Na n/a Na Position CENTER 0 Landings Na Condition SERVICEABLE n/a Na Na Na MCN 6510-2250 Tall Drive Shaft Hangar Bearing - Center. PN 222.344.606.103 SN MB952 Since New 25101/20)7 Calendar Retirement 3Y 25/01/2007 25/01/2010 14d Dose BEARING. TRDS 52326 Hours 3000:00 1136:24 4136:24 2476:24 ATA 65-10-00 T/R DRIVE SHAFT n'a Cycles Na Na Na Position CENTER ri?a, Landings Na Condition NEW Na ilia Na Na AY BASE SYSTEMS PC 13 EFTA01084866 PremiAir Aircraft Endineerinq Ltd Hours 1660:00 Cycles 0 Landings 0 Current Airframe as of 28/09/2009 Aircraft Compliance Report 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 MCN 6510-3200 Tall Drive Shaft Hanoa r - Alt. PN 222-044-003-1011 i 'S Calendar 25/01/2007 Na Na On Condition Na SN 19.4AY07-06 -'1,i.--E ru 1 ,( mi.-, Na 52333 Hours Na 1136:24 Na Desc HANGER. TAIL DRVSHFT ATA 65-10-00 T/R DRIVE SHAFT p Cycles n/a Na Na Na ' Na Na Na Na Position AFT 3 Landings Condition SERVICEABLE MCN 6510-3250 Tall Drive Shaft Hangar Bearing - Aft. PN 222-344.606.103 3Y 25/01/2007 25/01/2010 14d Since New 25 01,20( 7 Calendar Retirement SN MB955 4136:24 2476:24 523':5 Hours 300000 1136:24 Dose BEARING. TRDS n i Cycles Na Na Na Na ATA 65-10-00 T/R DRIVE SHAFT Position AFT ft a Landings Na Na Na Na Condition NEW MCN 6520-0000 Tail Rotor Gearbox. PN 222.042.001-103 Since Map Calendar Inspection Na 02/04/2901 n/a n/a SN A-747 3000:00 134090 1660:( 0 Hours 300090 n/a Desc GEARBOX. TAIL na Cycles Na Na Na N8 ATA 65-20-00 T/R GEARBOXES Position ONLY na Landings Na n/a Na n/a Condition SERVICEABLE Since 0 H 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 MCN 6520-0050 Tail Rotor Gearbox Or tout Shaft. PIN! 222.042402.005 Since New r 'rr Calendar Retirement Na 02/04/2001 n/a Na SN A.410 5000:00 334090 I E%60.( (3 Hours 5000:00 Na Dose SHAFT. TR OUTPUT r a Cycles Na Na Na n/a ATA 65.20.00 T/R GEARBOXES Position ONLY ra Landings n/a Na Ilia Na Condition NEW Ay -EASE SYSTEMS h`C EFTA01084867 PremiAir Aircraft Engineering Ltd Hours Cycles Landings Aircraft Compliance Report Current Airframe as of 28/09/2009 1660:00 0 0 Aircraft: N901RL Customer?, BOVALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component Times Printod: 1V0L2010 Tem 13:4I:39 Page: 19 Airframe Currer t Intervals Tolerance Last Done Next Due Remaining MCN 7200-1000 Engine - 01. PN 250-C40B SN On Condition 19/03/2401 Calendar Na CAE-844167 30/06/2009 n/a Na Dose ENGINE 1660 00 Hours Na 1611:00 Na n/a ATA 72-00-00 TURBINE ENGINE O Cycles n/a n/a Na n/a Position PI O Landings Na n/a Na Na Condition REPAIRED Eng #1 Na 1965.00 Na Na MCN 7200-2900 Engine - #2. PN 250-C4OB SN On Condition 1 Calendar Na 30/06/2009 CAE -844169 Na n/a Dose ENGINE Hours n/a 1611:00 Na Na ATA 72-00.00 TURBINE ENGINE Cycles n/a Na Na Na Position 42 Landings n/a Na Ne Na Condition REPAIRED 2020.00 Eng 92 Na 1965.00 Na Na MCN 7230-1000 Compressor #1. An time the compressor Is removed from the engine. visually PN 23065593 Inspect the aft end of On Condition Calendar n/a 30/06/2009 SN CAC -44957 n/a Na Desc COMPRESSOR 1642 )6 Hours n/a 1611.00 Na Na ATA 72.30-00 ENG COMPRESSOR SECTION Cycles n/a n/a Na Na Position 41 Landings n/a n/a Ne n/a Condition SERVICEABLE MCN 7230-1100 Compressor impeller hes PN 23065591 SN Since New a Calendar Retirement Na 30/06/2009 JY100665 Na n/a Desc IMPELLER: COMPRESSOR 1642. Hours 7500:00 1611:00 7517:54 5857:54 ATA 72-30.00 ENG COMPRESSOR SECTION a Cycles Na Na Na Na Position 91 a Landings Na Na Na n/a Condition INSPECTED 1985.00 Eng #1 15000.00 1965.00 15035.00 13015.00 MCN 7230.2000 Compressor • 02. Anylime the compressor is removed from the engine visually inspect the PN 23065593 aft end of On Condition 12/02/20)1 Calendar Na 30/062009 SN CAC -45034 Na n/a Desc COMPRESSOR 1124:f:4 Hours Na 161100 Na Na ATA 72-30-00 ENG COMPRESSOR SECTION O Cycles n/a nia Na Na Position #2 O Landings n/a Na n/a Na Condition SERVICEABLE AY4LASC SYSTEMS %1 EFTA01084868 PremiAir Aircraft Engineering Ltd Current Airframe as of 28/09/2009 Hours 1660:00 Cycles 0 Landings 0 Aircraft Compliance Report Aircraft: N901RL Customer: i3OVALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component 71rnes Airframe Printed:11/0MM Time 1341:39 Page: 20 Curren: Intervals Tolerance Last Done Next Due Remaining MCN 7230-2100 Compressor Impeller - #2. PN 23065591 ria Calendar Retirement n/a 30/06/2009 Na Na Since New SN JY102124 1660:0) Hours 7500:00 1611:00 7500:00 5840:00 Dose IMPELLER, COMPRESSOR rill Cycles n/a Na Na Na ATA 72-30.00 ENG COMPRESSOR SECTION Na Landings Na Na Na Na Position W2 Condition SERVICEABLE 2020.03 Eng #2 15000.00 1965.00 15000.00 12980.00 MCN 7250-1000 Turbine - #1. Anytime the turbine is removed from the engine. visually Inspect the splines on the fo PN 23063354 Since OM Na Calendar Overhaul Na 30/06/2009 Na n/a SN CAT-44746 49:C0 Hours 1750:00 1611:00 3361:00 1701:00 Desc TURBINE na Cycles na Na Na Na ATA 72-50.00 ENG TURBINE SECTION 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 1611:00 3386:00 1726.00 1775:00 Desc WHEEL. TURBINE 1ST 49:63 Hours nie Cycles Na n'a Na Na ATA 72-50-00 ENG TURBINE SECTION alb Landings Na Na Na Na Position 1$1 Condition NEW 55.00 Eng #1 3000.00 1965.00 4965.00 2945.00 - • • MCN 7250-1100 Turbine Wheel, Second Stage - #1. PN 23032280 'la Calendar Retirement Na 30/06/2009 Na Na Since Now SN X569531 1611:00 3386:00 1726:00 49:00 Hours 1775:00 Desc WHEEL, TURBINE 2ND Cycles Na Na rite Na ATA 72-50-00 ENG TURBINE SECTION n'a landings n/a Na Na Na Position #1 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 1660110 Hours 4550:00 1611:00 4550:00 2890:00 One WHEEL, TURBINE 3RD Na rid Cycles Na Na Na ATA 72-50-00 ENG TURBINE SECTION Ca Landings Na Na Na na Position #1 Condition SERVICEABLE 2020.00 Eng #1 6000.00 1965.00 6000.00 3980.00 AV-BASE 5'1511%51NC 0 EFTA01084869 PremiAir Aircraft Engineering Ltd Hours Cycles Landings Aircraft Compliance Report Current Airframe as of 28/09/2009 1660:00 0 0 Aircraft: N901RL Customer:. BOVALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 - Component 77mes Printed: ilt0112010 Thin: tag,le Pager 1r Airborne Currer t Intervals Tolerance Last Done Next Due Remaining MCN 7250-1200 Turbine Wheel Four(i Stage -fi t PN 23066744 Since New Calendar Retirement Na SN HX76889 30/06/2009 Na Na Desc WHEEL. TURBINE 4TH 1660 Hours 4550:00 1611:00 4550:00 2890:00 ATA 72-50-00 ENG TURBINE SECTION Cycles Na Na Na Na Position Ai va Landings Na rile no Na Condition SERVICEABLE 2020..10 Eng #1 6000.00 1965.00 6000.00 3980.00 MCN 7250-2000 Turbine - 12. Anytime the turbine is removed from the enable. visually Inspect the PN 23063354 sullnes on the to SN Since OH vi Calendar Overhaul nia CAT-44750 30'06/2009 rea Na Desc TURBINE 49: XI Hours 1750:00 1611:00 3361:00 1701:00 ATA 72-50-00 ENG TURBINE SECTION I /a Cycles Na n'a Na n/a Position 82 r ia Landings Na Na Na Na Condition OVERHAULED MCN 7250-2050 Turbine Wheel, First !.tade - 82. PN 23053299 Since New a Calendar Retirement Na SN X5513151 30,06•:2009 Na Na Desc WHEEL. TURBINE 1ST 49:X. Hours 1775:00 1611:00 3386:00 1726:00 ATA 72.50-00 ENG TURBINE SECTION r Cycles Na Na Na rila Position #2 ria Landings Na n/a Na Na Condition NEW 55.qC Eng #2 3000.00 1965.00 4965.00 2945.00 MCN 7250-2100 Turbine Wheel. Second Stacie - #2. PN 23032280 Since New Na Calendar Retirement Na SN X569825 30106/2009 Na rile Dose WHEEL. TURBINE 2ND 49.(0 Hours 1775:00 1611:00 3386:00 1726:00 ATA 72-50-00 ENG TURBINE SECTION Cycles n/a Na Na Na Position 02 Landings Na rite Na n/a Condition NEW 55.0 Eng 82 3000.00 1965.00 4965.00 2945.00 MCN 7250-2150 Turbine Wheel. Third 3laae - #2. PN 6898663 Since New r la Calendar Retirement Na 30/06/2009 SN HX93598 Na Na Desc WHEEL. TURBINE 3RD 1660.00 Hours 4550:00 1611:00 4550:00 2890:00 ATA 72.50-00 ENG TURBINE SECTION n a Cycles n/a n/a Na Na Position 82 n a Landings Na nla Na Na Condition SERVICEABLE 2020.(0 Eng 82 6000.00 1965.00 6000.00 3980.00 •Y.SSSE SYSTEMS WC • Ii EFTA01084870 PremiAir Aircraft Engineering Ltd Current Airframe as of 28/09/2009 Hours 1660:00 Cycles 0 Landings 0 Aircraft Compliance Report Aircraft: N90IRL Custo !ALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component Times Airframe Printed: I 1O12010 Time:1341:39 Page: 22 Curren; Intervals Tolerance Last Done Next Due Remaining MCN 7250-2200 Turbine Wheel. Fourth .51age - #2. PN 23066744 rya 30/06/2009 Na Na Since New n a Calendar Retirement SN HX76810 1660:00 Hours 455000 1611:00 4550:00 2890:00 Dose WHEEL, TURBINE 4TH Na Cycles nra nra Na Na ATA 72.50.00 ENG TURBINE SECTION 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 Na 30/06/2009 Na n/a On Condition 19/0312001 Calendar SN CAG-44167 49:CO Hours Na 1611:00 n/a Na Desc GEARBOX. ENGINE 0 Cycles Na Na Na Na ATA 72-60.00 ENG ACCESSORY DRIVES Position #1 0 Landings Na n/a Na Na Condition SERVICEABLE MCN 7260-2000 Gearbox - 82. PN 23063380 30/06/2009 Na n/a On Condition 12/02/2001 Calendar Na SN GAG-MISS n/a Na 49:C0 Hours n/a 1611:00 Desc GEARBOX. ENGINE 0 Cycles n/a Na n/a Na ATA 72-60-00 ENG ACCESSORY DRIVES Position e2 0 Landings Na Na n/a Na Condition SERVICEABLE MCN 7300-1000 Hvdromechanical Unit (HMU) - #1. PN 23078033A Overhaul Na 30/06/2009 Na Na Since OM rta Calendar SN JGALM0158 2430:38 69:2 Hours 2500:00 1611:00 4090:38 Desc HMU n'a Cycles n/a Na n/a Na ATA 73-00-00 ENGINE FUEL Position 81 Landings Na n/a n/a Na Condition SERVICEABLE MCN 7300-2000 Hydromechanical Unli (HMU) -112. PN 23078034 its 30/06/2009 Na Na Since 0.11 Calendar Overhaul Na SN JGAMT0603 2500:00 840:00 1660X0 Hours 2500:00 1611:00 Desc HMU r (a Cycles n/a Na Na Na ATA 73-00-00 ENGINE FUEL Position 42 r Landings Na Na n/a Na Condition SERVICEABLE AviASESYSTEMSOC.I3 EFTA01084871 PremiAir Aircraft Engineering Ltd Hours Cycles Landings Aircraft Compliance Report Current Airframe as of 28/09/2009 1660:00 0 0 Aircraft N901RL Customer BOVALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component Times Airframe Pa:ISO:11VMM Time: I341:39 Page 23 Currer$ Intervals Tolerance Last Done Next Due Rem...Jiro° MCN 7310.1100 Fuel Nozzle - #1, PN 23077067 SN Since Ortl 11/9 Calendar Overhaul Na 30/06/2009 1XR05440 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 SN 1ZR04765 30/06/2009 Na ilia 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 SN FF58672 nia Na 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 23073353 SN Since 0H Ya Calendar Overhaul Na 30/06/2009 FF36207 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 SN 0115 n/a Na 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 Condition SERVICEABLE AV4ASE $YSTEVS ITC 1) EFTA01084872 PremiAir Aircraft Engineering Ltd Current Airframe as of 28/09/2009 Hours 1660:00 Cycles 0 Landings Aircraft Compliance Report Aircraft: N901RL Custert: 3OVALE DEVELOPMENTS Make;Model: BELL 430 Serial No: 49078 Component Times Airframe Printed: 11,01/2010 Tans: 13.41.40 Page: 24 Current Intervals Tolerance Last Done Next Due Remaining MCN 7920-2000 OIl Cooler Blower - to2. PN 230-365-001-101 02/04/2001 Na Na Since OH n:a Calendar Overhaul n/a SN 1109 1660:00 Hours 3000:00 n/a 3000:00 1340:00 Desc BLOWER, OIL COOLER ATA IV3 Cycles Na Na Na ela 79.20.00 ENG OIL DISTRIBUTION Position #2 rva Landings n/a Na Na Na Condition SERVICEABLE MCN 8010-1000 Starter-Generator -111. PN 206.062.200.129 Na 24/08/2007 n/a Na Since OH Na Calendar Overhaul SN Y10348 679:66 Hours 1000:00 1294:47 1980:54 320:54 Dese STARTER-GENERATOR Na Cycles Na Na Na Na ATA 80-10.00 ENGINE CRANKING Position NI na Landings Na Na Na Na Condition REPAIRED MCN 8010-2000 Starter-Generator - #2. PN 206.062.200-129 Na 01/10/2008 ilia Na Since O/H Na Calendar Overhaul SN Y0402 2590:38 930:38 69:212 Hours 100000 1590:38 Desc STARTER-GENERATOR Na Cycles Na Na Na Na ATA 80.10-00 ENGINE CRANKING Position It2 nla Landings Na Na Na Na Condition OVERHAULED f 4-- MCN 9500-0000 Electric leak check aryl CAP check MRS Clock Batten', PN BP9 Since O H 24:99t 9 Calendar Overhaul 3M 01/10/2009 24/12/2009 -18d SN 25262 Na n'a Hours Na 1660:00 Na Desc BATTERY PACK n'a Cycles Na Na Na n/a ATA 95.00-00 Added in Conversion n'a Landings Na Na Na n/a Position N/A Condition TESTED NOTE: Calendar based on Overhaul. Ref: 95-00.00.97 AV BASE SYSTEMS INC EFTA01084873 PremiAir Aircraft Engineering Ltd Hours Cycles Landings Aircraft Compliance Report Current Airframe as of 28/09/2009 1660:00 0 0 Aircraft: N901RL Customer XWALE DEVELOPMENTS Make/Model: BELL 430 Serial No: 49078 Component Times Printed: 11/01/2010 hint 19:4140 Page: 25 Airframe intervals Tolerance Last Done Next Due Remaining MCN 9900-0000 AD:SB Loq PN Z2-13430 SN NSOIRL On Condition Calondar Na 02/04/2001 Na Na Desc AD/SB LOG 1660 00 Hours Na n/a Na Na km 05-00-00 MAINTENANCE CHECKS 0 Cyclos Na Na Na Na Position N/A 0 Landings Na Ilia Na Na Condition SERVICEABLE Component MCNs Only. Does not Include: Superseded, Not Pequired, Applied Only. No Status. Disabled MCNs. "'End of Report— AMEASC SYSTEMS INC 13 EFTA01084874 EFTA01084875 EFTA01084876 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 due O/H @ 2000 Hr Bleed valve due O/H @ 2959 Hr Oil Cooler Blower due O/H @ 3000 Hr Starter-Generator 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 Service Bulletin - Available Cor Content Revision 18/0712011 File ID: NEW Aircraft Registration rg et I 4,— SB Number Complied Amendment Number Once Nest Duo 1. Facility 3. Cert. Num. Effective Date Doscrlp :Ion Date Method of Compliance/Applicability or Data 2. Cort. Type 4. Author. By Time Recur Time Manufacturer Category Model Part #: Allison Engine Company Engine 250-C40B SerialIII CAE-844.67 4. 24+m f'. 1317-A-1166 ENGINE FUEL ANOCONTROL, Once 1. Pf-Entiotta Atear-r ctj) 1511011982 BENDIX FUEL CONTROL pi 640".4e nittpx4._ ASSEMBLIES AND POWER „ 2. IE-Cortnraigeirtic NI itt 3. L ..Thgaret sA'ei..--i TURBINE GOVERNOR ASSYS- r•furnevirse. ffl-t ral-1-6 9 INSPECT BUSING ASSYS I 4. 0 I AuG Zor t OUP (ATP OATP Signature C30•A•73-3103 R3 05/06/2003 r Goodricbengine, foal and controtinspectIon of MU drive CM AT Sant Et.W.T.t-saS c4 fr.( AT- so-o-P Real( ' 1Jfmt ale_ fated:et moPtAisp nie. -1 N/A- 0.4 2. a r ra, wiroge.472. Up splines and power lever angle (KA) 9394 OS or 6 4[6, rots 9/4 1.4 Ogni..r.Cap - 2 SCrirn.34. 3. 1.- -11:10.-b. -4 ag, -A-73- 6ot) signal oATP C40-A-72-5009 CAW . ENGINE, GEARBOX ASSEMBLY- REPLACEMENT OF CERTAIN Sone 0...k 104 Ceig& - A-73 - 5o2t ea./ 4- re.R.....$) OATP Once lima rdait i. 4. FA IN Cs Zed • Peon-late flees, - 1 21/05/1997 frai-i aresee.6er7t Sean.- 2. G...Cdri-50110,4G POWER TAKE-OFF GEARS, PIN 23056617 rsfinf-atr inf5,014....4;4> bisIn 3. L . -flavrirefo.....1 NIA 64-fate- ES 4. 01 ich.)6 2-01I MOP OATF OATP Engine, turbine assembly-new C6) Wr------ C40-A-72-5048 R2 l • Peam.Afe mecat 27/06/2006 threshold event recording and new CIIAI it i oriG(sw+.•>7) ci.-4 AT i I 36.4- Once ,, 2. CE-Iglaaa.C.mif,- tip steady-state operation avoidance Cane. , _ µ4S 32Ar69 2.5awriZtiol range limit ner4Als 4 z 6,46. csa*K09 611,4 AT II 36 -sl- NI /A 3. 1.....-rita -nes-D-1 refereCoq 1165 9A-tiop 2.5a-...-12.c.c.7 4. e-t Fist,- '1_'01l CcATP OAT'? OATP Signature: C40,4-73-5029 Engine, fuel delivery-release of new Once I- m 'AC AreCeetr-r- 04/0912003 fuel nozzle Se17.t.A01,-4 4:.rCon-fientrot. 2. lenter.4.14W-,,.&- t..-W3 N IA acko-as r-ilA a L..ropene.se—s 4. en aritsGe OeM i OA TP OAT; Caw Signature: c r---- 4*.---- -- C40-A-73-5029 Rt Engine, fuel delivertwelease of new pec,,Aeogx 4i &w isti4 meep Once 30/08/2004 fuel nozzle I; ifs0 rfoZZLeciSirat ''ream. rate2 oh Caner Gip.) i ar 529. 0 des rnagp IS ocr 2003 2. EaThat& (-74D I 5M FAA "P 42 CI-C.: C6440.9 rcotzLe.. arritac-€4> N/A 3. L.-raw-rec...I 4. ta4 A-...3-G- 2c2.1/ fc04- g4.. e9 AT 53o-o PCS ..TAnS.j> 29 OCR' 2a:35 OATP oirtoott,00 A4DATTP„Soigna. lore: ice.t FAAREpAir r...)n fr ea m -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' S13 Number Aircraft Registration hi of Effective Date Complied Amendment NuMber t..- Descrit ti on Date • Once Next Due 1. Facility . .. . . . ... Method of Compliance/Applicabilit 3, Cert. Num. Time y or Date 2. Cert. Type 4. Author. By Manufacturer Category _ Recur Model Time Bell Helicopter Airframe 430 Part IS: 430.985 Vertical fin assembly., installation Sorial U: 42O78 12/06/1998 Inspection and modiication Civ.I Recur 1igiamaie. AtAcei4F-i- Corna.i6P tni or* Ar e,..n to A-i 2. 644-...reisci..rc- t-aD gurn-co NO 3. i- . nterne5.O.4 OATP OATP 4. etre Zee i 430-98.6 Replacement of latedst control tube ©ATP Signature: _....) ------- 12/0611998 assembly P/N 430001-018-101and Once rework of forward talking P/N,contd C i iiNt 1VerseniatZ AlieCCAC-r- Ac Cornier,.lap 1.41114 AT ree4) 2. 64-4,...ase24.4c r--1P OATP OATP p4 iLp "(IA 3. L. ntorrieSa..-4 4. rei ad Gr . 7- 0 4 I 430-98-8 Damper blade sot P44 OATP Signature: ......,...-- - irti....r.„....- 31/12/1998 430310-104.105, ineoeuctIonof --- Cli.".1 Once Cern9g465,2 u'SIN- AT get LAICKan,tele AleCAtzr A-D tC) 2. E....rerwasaieuec. t..., akst IA? r4/A 3. L. .11Th,rveinsm--1 ©ATP 4. At Auc Col I ©ATP; 430-99-10 Electrical power distdbution system, OATP Signature; ; ----lt 16/12/1999 Improvements CI w Once Cowin-16p F-rimi iti - guild) - ftsg Al- mlfrie etteCentg- a V-9-6fraSseast. 40 Ikrit.9 r4 A 3. L. natenia,tera ®ATP OATP 4. on Atfrii toll 430-99-11 Autopilot resolver installation saw Signature: 0.------ 07105/1999 Improvement of i el l4 • Once Ar eatriLlep .11114 AT' emil 1•PrZgarnutte Aistetri- L.N> OATP 0e.M4'.) r4 IA2. arecni-regeN4C tap 3. r.....-n-karnreec.-4 ©ATP i 4. erl Ad G ZAW I 430-99-13 F uel quantity Indicating system OATP Signature: 13/12/1999 calibration Once Cp.4 • i e--e-i-0. 64 rieCe .- eArrIA-41 , la illi An— Sudep •-•vricr Ar 2. rE,...iCemcbea.4., Ln, 6vi Lp r40 3. I- • Theereacrl ©ATP ©ATP 4. en AI5(, Cat OATP Signature c 2 '4..,--------- (Tc-Ninncl L44) AV' liztab O• as:I/Algae& iMetip et AS& te-rai i IFAA REPAIR STATION OATP MUM. Printed 01/08/2011 13:37:58 ( .7 .--A....A------ Page 4 of 5 EFTA01084878 Service Bulletin - Avail Content Revision: 18/07/2011 File ID: *NEW* Aircraft Registration: NI 90 I /Ct.- SB'Number Complied Amendment Number Once Next Due ' 1. Facility 3. Cert. Num Effective Date Descript on Date Method of CompllancidApplIcabllity I or Date 2. Cert. Type 4. Author. By Tyne ., , .. . .. , Recur .. Time Manufacturer Category Model Part N: Bell Helicopter Airframe 430 Serial ft: -49 0 7 53 430-07-41 RA 'RBI-Tail rotor blade rissembly. 1310912007 inspection of siu,_ As6 44-30-67- +I 4 0 Once 1. Pea.", anZ 44-ie-cgAr-r 2, C.-...-rrin-riiCiel-rE, i-r1> r‘i /A AZ C.c>rnet-ill-e4Ca r-4/A 3. L . T74ornoSra•-•I 4. CI Ali 6 Zob-11 ©ATP OATP ©ATP Signature: ,„,---- • 430-07.41 RC 'RBI-Tallrotor blade i issembly, 20109/2007 Inspection of 5a- As& 14-30 -o7-- Al RP Once -7.:-e low_ Aler-emer 2. G,461,4aiii-).45 LIP NO f tw coryeuen4o-E r4A 3. I- .Th....-netr.-ra.--1 4, of Aro-G ?all ©ATP OATP ©ATP Signature: .---e .,&..1.4,--, --------- 430-07-41 RD 'RBI-TAIL ROTOR BLADE Once 29111/2010 cli i.4 s--1Crerarnin-ge_ Fr‘Cce.4.9- ASSEMBLY, INSPECTION OF SIr 4 TA-ii- Caere'e ..C.L.-r-S. AT uj 2. et•Kalo4eatels-1‘ l-96-$ A-2 (7 i keg- rzt-oeur cat:1%Z r‘i )o; 3. i,_. nst-^0.10,--1 eiV HeS .PA,-64, ANA-1114d. t gr..7 -le_ s‘m•ra 4, cal AlsEr 2.041 ©ATP ©ATP ieystsreq OATP Signature: 430-10-44 *WOODWARD HRT-NYDFtAULIC Once 1. 18/08/2010 SERVOACTUATOR P/N 222-382- 001.107 MANUFACTURED BY 2. WOODWARD HRT, INSPECTION 3. OF 4. ©ATP OATP ©ATP Signature: 430.97.2 Model 430 temporary airspeed Once 1. PACrnIpric2 i11ae 11107/1997 restriction Ai 4c-Cei•tr nrtapir,C-p AS 2- a.14/t•tri-6 124., e ,--Ti3 NIA ed.hz Ase. 4-3c-97- 4 r 4/ 4 3. L. awn(' in.--, 4. of "SG, 'Zerri ©ATP ©ATP' ©ATP Signature: 430-974 Temporary airspeed iestriction ccrr,Tht------- Recur . 19/12/1997 removal of, following limper yoke CI t' Cennnfturr-4, “irti AT ..‘iiL-5> ,ek,rz Ma:ten- set P/N 430-310-100101 Al- 2. a.....r&-....rage...../G Grp and,contd. Ni/4 3. 2...../acamP.Sc-J bort-S) 4, 4,1 f1-4 & Seri i ©ATP CAD, . ©ATP Signature: FAA REPAIR STATi Corn Pii...64., Ai - athe • to Al NUUY650L PA -IroP of it-or..; ?or t 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 Compiled Effective Date Amendment Number Once Next Due 1. Facility Deacrir non Date 3. Cert. Num Method of Compliance/Applicability or Date Time 2. Cart. Type 4. Author. By Manufacturer Recur Time Category Model Bell Helicopter Airframe Part 0: 430 430.04.30 RC Tall rotor counterweight bc4Icrank Serial 0: 496.72., 16/0212006 P/N 222-012-727-00a, Removal Once 1. co:a.m.-4.e_ thect.n.c..- from service plc( ehi la i t._ eare•42.. ~1A C3-"-n-trSe it-if-Wait faiscesT-44 t4IA 2. 0.46-1.466se4-6- .so 3. L .7-°.--,osc...a 4DATP @ATP t 1-451-14•4_ "0 4. el AO& 2Ce4 i 430.0441 RA Tali rotor blade PIN @ATP Signature: 29/11/2004 222-016-001.123 anc -131, a I u4 ilg. .6..vritzr‘ 12/4 in- Recur cit.-04-W NI • PesSer n-re i ace-cw‘r- inspection of 2 ra.-ral...reacc..n.rer urf, (sea- '61 A - all i cow AT $76 • err cleknots * ires (Ts....0 . Ai...earns*, hiEL,t I-4 /A 3. i.. • Thc..-nrr./...•—) @ATP CIATP, & "I ..' ",.. rig. Palace l'isGwe• P.E..u-- roScren..1 4, of frag ', flit re tante. / @ATP Signature: 430-04-31 RC Tail rotor blade P/N i 222-016-001-123, -123M, -131and Once 31/03/2008 -139M, inspection arch rework of Clibi Tie Sowe 9/..-12n- c.0 - cat -Byrn 6.nmnie. Aier-ear (12.zsr- . ti-J A - 201 c4,4 Al- 5-71.•01 2. rf,d6."..nsee.i...4.- Lilci, Akzucs NIA 4447 t o_" 4" (Testi) Alan prGi H&J tie. acerC- CATP 4. coi ad& .q.sra I. CAW rearcencrr) fr ierv-, ertat..-re.ecte-oa 430-04-32 RB ail rotor counterweight bellcrank SNIP Signature: -- 15/03/2006 P/N 222-012-727-10f, Inspection Recur Pe-amione A-rec and recall of ev-/ fir.1 TAi L Cow& 2. /.....tari.404.C.s....C... - NM CantrffeCtrt65-1Grwr 11-Gt`r all+414. N/A 3. L riarneSin-.1 @ATP 1.-64-mt.A..firs 4. of awes 2011 CAW 1. 430-05.33 introduction of retirement life for the OATP Signature: ci t, j 16/020005 servo actuator to achiator support Once bolts P/N 50-047C8-31 AT .rAv4 /ells 43O - cis - $i fRatniftle thecears 7525 • tS 2' 0.-*P-41C.fsg-nriG 1.4) kW ergs N A 3. L..n+..+,..-.PS.tora CATP 430.07-39 09/01/2007 CATP ' Tali rotor pitch change mechanism, Revised rigging procedures 02.4-4-17 '2,ryinCler ©ATP Once Signature: rer 4. car ay es 'Zorl 2. 3. @ATP CAW ; 4. ©ATP Signature: COnnPmetc) Pry 1 FM PEPAMSTATION !bee. co eilqg f licaptesa (...... 2, .7010C.- 7-O•I ( 10 *ATP Printed 01/08/2011 13:37:56 ---. '45. Page 2 of 5 EFTA01084880 Service Bulletin - Available Comalia Content Revision: 18/07/2011 File 1O 'NEW' Aircraft Registration: r-.I 9O1 CI- SE Number Complied Amendment Number . Once Nil* Due ti Facility :.. ..3; Cert.,Num Effective On Deecripl!on • ..Dita Mithod of CoMpilaincalAptilloabillty . 'Pi DIM '2; OCart :ifiAgef.**4ti*.iir .rips Manufacturer Category Model Part 0: Bell Helicopter Airframe 430 serial N: 49o79 230-00.18 Hydraulic actuator apport P/N Once 1. 19/05/2000 222-040-125-001, Inspection of 2. 3. 4. CATP CATP OATP Signature: 230-01-20 Upper fuel enclosure Right side, Once 1. 07/02/2001 Addition of drain provision 2. 3. 4. ®ATP CAT? *ATP Signature: 430-00-17 Hydraulic actuator st pport P/N Once 1. taan.,,,c n-tr2c.ese 19/0512000 222-040-125-001, Inspection of C.I in/ Cannel-16P V41-n-i AT 2. (EnCriag.atli-rb cSP AT tai ii--3C:. hii A 3. L. . -roarnosolan-t emnit 2 4. an Ahffs. ?All CATP CATP CAT? Signature: 430-01-19 Electrical system, improvements Once miol.trz. ione..cren- 22/0212001 CI it,l C-omet_.14.9 v-lirr-V AT 2. pErfaii-malesm-2. txt> AT Au,kis> NI I A 3. L. -1- Sorennciar.1 2X) 11-43. SAO- ASiS v4-5C..-- 9 9 - t o 4. oi in-JC., gait CATP CATP -Rs,- come lic•-rica-- CATP Signature: "IL -. 430-01.21 07/02/2001 Upper fuel enclosure, tight side, addition of drain protislon ej,,, Co enp,A6.O v-ri-n1 A-r- Once - Pe-eFrni sane. 'net -A* 2. 6..44,4644-em-c,tsp Arr 5;_m-j.) (44 3. L. .TharrteSce-J An p 4. 01 PVC- 2041 CATP *ATP OAT? Signature: c2:5-$ 430-03-33 Fuel valve switch. Rewiring of Once 1110612003 2. 3. 4. OAT? *DATE CATP Signature: FM REPAIR Mg ON algemplu6.9 ,ti - 166O. co F- this MIMI. 2orrep at a.r e.c>t I 7..„-------xyk„......--- °ATP Printed Ol/08/2017 13:37:56 Pap of 5 EFTA01084881 EASA Airworthiness Directive Co Content Revision 18/07/2011 File ID: NEW mpliance Record : EASA AD Number Aircraft Registration! NI9ot Rt_ Effective Date . Com. . piled Amendment Number • , Desert Aim , Once Next Due 1. Facility ',Date Method of Compliance/Applicability. 3. Cert. Num , or' Date 2. Cart Type 4. Author. By Manufacturer Category . Recur. . . ;Time • . Allison Engine Company Model Engine Part St 250-C40B 2004-0009R2 Engine control system' pipes- Serial #: 15112/2004 Inspection CAE-5426 67 4. S . tto Once 1. 2. 3. MAT P CATP 4. iDATP 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 Complied Amendment Number Once Next Due 1. Facility 3. Cert. Num. Effective Date Description Date Method of Compliance/Applicability or Date 2. Cert. Type 4. Author. By Time 'Recur Time Manufacturer Category Model Part : Allison Engine Company Engine 250-C4OB serial : CAE -$44 0.7 d 044 I 97-25-09 TO PREVENT FATIGUE FAILURE Once 1. ee‘rn,A, Al ece-rWr 23/12/1997 OF THE HELICAL POWER & LT ef(e- , e4< Sr•-..eich-. 2. a-tau.resteLwar.- 4-1-5> TAKEOFF GEARSHIFT ASSY, NI A 3. L. .-nicunc•Ster-i WHICH COULD RESULT IN A r-.1,./rriaae ir4Spcii-L-Cto u-4 -eer/4 iS- CEntaLS 4. 29 ..w-1 2,c-iI LOSS OF,CONTD. . CATP ilsiATP 026.13 -A -12 -Soca) ®ATP Signature: 2004-24-09 Superseded by 2008.1644 Once 1- tanucniz fre .e.C4r-r Ste (--RA A9 2ocae -Ho- 04 05/0112005 2. d:4Q1.-tge.at..tra- Loy I'VA 3. L ,11.k..-nrAlma NI /Pc 4. 2-9 7t-n-9 2o11 OATP ©ATP OATP Signature: 2006-16-04 To minimize the risk of sudden loss g ai t,/ it i sac. rs,p4.00) raez..4. cr./Lace° Once '• edenalia. liic AuZcilith- 07/09/2006 of engine power andunoommanded 6.,,, (..:AA 5 .z9:-0 nes isitra., is ec_i _ 20es 2. IF.4.' 16..460-2...-‘6 ,--ZO shutdown of the engine due to Al AD Ni /A 3. L _lova, . a4N--t fuel.conld. .200.444 tf 2 C.L.A. (g44a....9 •44.7.2..a actRaap 4. 2-9 nl-p--1 Zott Per 530 . casts PA-'tep 294x-2°03. ©ATP ©ATP (c.i26 - A - 13 - 502., el-) ©ATP Signature: 2006-20-07 To prevent loss of ix wer. possible L .I tt4 ,. Once AT Amty ( relit+ fw2 ----- Atecerr6- 0211112006 engine shutdown, or uncontained / 4 I F:1-4 Clui-lb7)4 S .4 AT 1l 36-4 (ee- 0.16459669 2' r.Se-f&Ir4a 9-4,44- L.TIO failure IV s >me. as -.)- A.4200i 3. I._ . TscriAPIa-1 ret a...‘ .1t a E.4Ci- (3.441V1) dr.! Ar- tin . ti. CZ:4%11'MP'4 .2 9 annm 2.4z.iI cl2-4-cao) t-tez.S .DA-riS.t> 25n-ilia 2ocr7 Signature: .„...._ ©ATP ©ATP ea e. -A - -72- So+8) @ATP ,.....,....,--- _ Cornett -6P A- 1- learie • ‘-:° nes r EIFR;Jiiknom ,.4.-re t.p. z,.3tiu.-/ tut i tfr4 i ? ,o ialltY6301 Fn. OATP Printed 29/07/2011 15:48:32 Pape 5 of 5 EFTA01084883 FAA Airworthiness Directive Content Revision. 18/07/2011 File ID, 'NEW' FAA AD Number Aircraft Registration: Complied r•LCIO1 el — Effective Date Dose' iption Amendment Number Once I Next Due Date Method of Compliance/Applicabilit 1. Facility 3. Cert. Num. Time y or Date 2. Cert. Type 4. Author. By Manufacturer Category 'Recur Time. Bell I lelicopter Model Airframe 430 Part N: 2009-08.03 Superseded by 20 i 0.2G-51 Serial #: 49o7E3 24/04/2009 Once Set- FA-4- 49 2010 - 2-‘ -•-ct 1. re.6_,,,,(4•02. ArC.cgol-e- 2. firiGinifft-ei...C. op 3. i.....-n.b.-nraS.-1 ©ATP CAW 4. :9 3,...k.m 2.1.4 t 2010-10-12 To detect a crack in the blade. and ©MP Signature: 16/07/2010 to prevent loss of the blade and Recur 2 6''-------- subsequent loss of control of the helicopter 2. eWrh 3. SAW 4. 2010-19-51 To detect corrosion' or a ©ATP Signature: 09/12/2010 nonconforming grinl relief on the Once 1. output piston rod atiembly (piston rod),to preventconti 2. SAW 3. ®AT' 4. 2010.26.51 To prevent loss of a.blade tip ©ATP Signature: 25/03/2011 weight loss of a blade, and O4 eftvi a.r...f r-4/A Once 1.Prailen.rase. Atiecenes subsequent loss of control of the 0'1 St ---1 - helicopter CF-Ze d?- Zt RI yir2_ eKA-Apa. lennquxis> ..... 2. E.444.46c,e+.4c_ u3C3 - Zed AafS 4+$0.-7 " ni...1 22.2.- ea 6 - col -I .-3.9m =ii•-. 1 NI jA 3. L . Tar-v-rio.-4 ©ATP 44 elav9 A - 2 i -7I iti.-in.iro-46I, z"°7-/e. OATIl gta p( 4. 2.9 ataft-t 2:04 I fr:Oravn-i 0.-aa.,_ -rawre.-O-4 ©ATP Signature: --- -- 6;PrviPt 147 An 166O. oo Alp tics TalatTiniTiiiON YM6P 29 -7t.44-1 2OI t tti% 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 Complied Amendment Number Once Next Due 1. Facility 3. Cert. Num. Effective Date Descrip ton Date Method of Compliance/Applicability or Date 2. Cert. Type 4. Author. By 'Time . . Recur Time . Manufacturer Category Model Part a: Bell Helicopter Airframe 430 Serial #: 49o78 2006-13.14 To prevent bellcrank failure, loss of c i tsj Recur 1. PaerniPrie. AleCgAll- Ot4 ea.ji thy' 14/Pc 64-1 Pin! -rna._ 11/07/2006 a weighted portion of the balk:rank, 2. ariairwirte-s..x, LAp and subsequent lostd, of control of ht Itc7Prr< Ccts-lreetkiateitic err_LaCarK r•VA 3. L ..rilrriPa.'-e--.1 the,00ntd. 7 98 -8 r r-Larret449 . CCF- 2tx;:s - 27Ci.) A/F trey .-PAt1.59 (As6a 50 -Pe-33443x awe ) 4. 2 S 71.-4^1 2.011 CAW OATU CATP Signature: 200749-52 To prevent foss of a blade tip 4 1,3 - rig 6.capg shi ite.- trt ici u4serscreo Once 05/12/2007 weight, loss of a blade, and AT pe-€O 26.4.64-s6p acy f4.6).- PArdo 19 subsequent loss of control of the lz94,rg helicopter 3Ctil- t.0o7 (92.7.:4 -r- ......0 1-/C $4.4spa trioc de-1 * 64=4- 57r j A-20 i r4Or A00,-IcaStAS Pal*, OATP CATS. icr5.6.4,107 fiLf -tom .4-n-npfia. OATP SIgNnatikure: t ri.- 23494 s-7T nni 745Crie sm.is-il 4a-i: sg:Rai r 2007-26-10 To prevent fatigue failure of the bolt Once and subsequent lost. of control of c../Ld 06/02/2008 ralv-1 AS& 430- OS- 33 2. Ci.-40-4-tOgreir-rg, 0 -0 the helicopter AP 751• la r1/A 3. L . rnornitra.e.- A-/F re 4. Z• 33.0‘"-1 Zo4 l CATP dDATP acr e /44 CCP-2005-09 ctittc. warre..-5) COMP Signature: --- _...,.--.-- 2008-14-01 To prevent interruption of the fuel Once 1. 14/08/2008 supply caused by fa lure of the 2. switch, which could I esuit in loss 3. of,contd. 4. OATP @ATI' eATP Signature: 2008-15-04 To prevent the misatgnment of the Once 1. 03/0912008 tail rotor counterweight bellcrank 2 3 • 4. SATP CATO OATP Signature: 2008.19.02 To prevent failure ofthe support Recur 1 AU"-, -,mc inne.e.ati- 16/10/2008 and subsequent losS of control of CovvIt..t64) 1,4 1114 Ar • J3•4 ti.p 2. efiermazdea-11,- ts the helicopter 4/A Nf AAS 430 - Go- I-7 3. i...r4:4.--nPlear4 4. ?....133..s...4 Wat i CATP war,. (CF -Zcoo- Z9 cklx- rect.'s) OATP Signature: C...---e tr con,Pri..6.p AT Ibbo. oo AIF r FMI IrPAITI STAT:ON e pm-ap zsa.-/ r.,oil c .t i INUIZOL CATP Printed 29/07/2011 15:48:32 CfP4 1----- Page 3 of 5 EFTA01084885 FAA Airworthiness Directive Compliance Record Content Revision: 18/07/2011 File IO: •NEVV* FAA AD Number Aircraft Registration r4 9oi IZ l•-• 1 Complied Amendment Number Effeativetate • DeloriptIon .Date Once NextDue 1. Facility 3. Con. Num Method of Compllence/Applicability • or Date .-aline r 2. Cen. Typo 4. Author. By Manufacturer Recur Time Category Model Bell Helicopter Airframe Part : 430 2001-01.51 To prevent failure of the supped Serial : 49o78 02/03/2001 and subsequent Io.!s of control of Recur XAW ASS 4-30- oo - q 1. PearrnAle. AI eck'srr the helicopter CCP-. Z000- Z9 °A so f-e-(I-A) a A 2. aagrver.6.22.4G- L1-0 3. L...1-No-nrsc-..._, NIA SuOisearese) OM FM A9 2008-19-02 ©ATP 2001-05-09 IDAjtil To prevent loss of electrical power lrl attend/4.i e (DeoRes/izenn.s ®ATP Signature. 4, 2.9 dt.n....t zoo 24/0412001 and subsequent kits of control of Once .-rraignThi-ra. 4ii2c2442r the helicopter 1/12 Aige.,244-r-t- Cra.ISTIC.ca-lor..l a Gr4eladdlei.-46 LIT) 0 A rJorru3642. ni/A 3. L. • Tncterarsa...i 4OATP 4. 29 awl 2.011 tan' (A56/.4.30-99- to 81, CF- Zo-co.-c(4) 2002-01-07 To prevent failure df both fOATP Signature: i0E;i .lr------------ 21/02/2002 generators, loss of kimary Once • Mien! 414Z itiergserr electrical power, & subsequent loss 2/ .11 A-ICC-44 (204511Zocotc>.—i of control of theecorld 2. I.... .aece....r-- 1-rl> 1•1/ A Wmtes./C kVA a• rarannersessJ @ATP ®ATP (Mc. 14-30- Oi - 9 4 ef-Zzot-3214) man, 4. 2,9 aNAA-1 2c4 I 2002.20-02 To prevent accumulation of fuel In Signature: Fot.n...4, Om112002 the right-hand upper fuel enclosure L., Once • tokrat uisiC recg4A- area, a fire, & a sutt.equent I ekheiod3u.r 17(t4....tto.15-o-i Ciartiti> t,4111-I forced,contd. a fr.r.(4-9Kniatost tap C/v4 /sr N/A 3. t...-f4orenco--1 rt.9Adie OATP tla5 4. 2.9 ativ•-f 2011 ®Are ‘are Ansc. eistS44,30-e i t-21 4 ce-20.1-z2 @ATP Signature: 2004-28.11 Superseded by 200304 -09 1870112005 eta_ FAA 4$) 26:05-04-0, Recur • pao..,.„,c,„c. taitte.gar-r- hi/A- 2, 6.420 woddratrr 1-re, Kr A 3. L. .11amerorSa.-.1 4. Z9 jten..7 ©ATP CATO Lott 2005-04-09 Superseded by 201,?-10-12 @ATP Signature: 04/03/2005 fi_tR._ czAh hp 20)0- to -i2. Recur • ~Ale insectale-- 2. if..i4-n-hte.,..cd. kin> PIA 3. ‘,./.40.-nr.S.a.-..i SAW 4. 2,1 o......)-r 24pt 1 CAT; @ATP Signature: CarriPtvap AT iistuo • oc. tariC ' i, fa offal STATION I 7~09 2 9 vt-.0-; 20I I tiltlYMOL @ATP Printed 29/07/2011 15:49:32 Page 2 of 5 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 Down tionK --. 1.Complled,.: ' •-::. .iPil s• 4 1: ; :'. • ArnondMerst.Number Method ofConipNanceiApplIcability ' PIS*. • Next Due '1,:,telkttyl- 3.Cert,Aurft:. _., or . -Date • • lakikeriittlYp,' 4::sicilarr% By -- r __ .... :•;•,;::11nie,:: :, - Recut : • :Ttrni . ; .-" - - • • ' • _ ., Manufacturer Category Model Part 9: Bell Helicopter Airframe 430 Serial ft 4-9o18 97-15.16 Superseded by 200D-16-04 Once 1. PPS..,, 412 Al&earl- 24/10/1997 8 -P-e... FAA Ap 1000 .-I 6- 04- .. , , 2-1l-iaarro - is° hit ituc 3. i... , ri.krienesio-1 14 /A 4. 29 ant-I 20..1t 4MTP @ATP &OP Signature; ........ eir•--•------- 98-24-31 To prevent binding a the lateral Once . 7112.6ewiairt_Araci-er-r- control tube (control tube) assembly 6 ,-/ Ai ecgia-Pr Cs>sigge-hJertor-1 - 03/0211999 2-614G,- a... taw? with the inside surface of the Nuhriffesa forward,contd. tq A NI/A 3. L .11kw-riti4w4 . 4. 29 3vv-i 2..st1 ®ATP OAT? (Ass tao-93-4. 3 CF - ,i3 - 2,) ©ATP Signature: CH1•Sit - ' --------- 99-23.03 To prevent loss of lc rque of the Recur • 47124nlIr rie AitzeRne-i- vertical fin attachment bolts (bolls), 19/11/1999 which could lead to "racture,conld &. PrieC4A-r —r - cal 2. 5.-ictinfactodc. ,...-c, ta.yrn Sag, r•I/A 3. t_..-rikirrie50,..3 rliA 4. 29 al.n.4 200 CATP ©ATI' 015614-20 - 96-6 4 e.. - 9 e - 21) @ATP Signature: 2000-16.04 To prevent lip path plane Once • tCe-n'Alt stiecf-Ae- cite./ 19/09/2000 separation. increased vibrations, AT \Mang6P Co.•••-•atri,D or 1,r1-1 2. ry..-r.5,irl6"..A., g-11> damage to the main rotor system. .9 pg,o g it , p6Lvalzy a,...1 and,contd, 930 NA 3. t_ 40,-,-.0Sa.-J A,f tic/ A$6'4.3O- 93- IS 4. 29 3,-ils•-i 2011 ©ATP ©ATM' "Arra.° su-..,94 id. (As.& /.4$,..97...z 4 CF- 97- 23q !ATP Signature: ,r —1 e 1/4-1' W 2000.16-06 To prevent a jammed flight control & . Once 20/09/2000 subsequent loss of control of the • Pre.deninii2 An2c.ftwor helicopter OW AiCc-esiri- (.2o-t5reue.no4 2. 644-...,acie•-e.. L-3D Ni,len&GS 3. j._, inarheSca.-J NVA 'NI/`c 4. 2 9 .7t-h-•-r 2ow / ©ATP ©ATP CAI'S 'ISO' 991 1 4 cr - 9 9- 26) CATP Signature: .,..- 2000-22-13 To prevent an inaccirate fuel Once quantity indicating sistern reading, C--tr- 41m14,42 cheer-4cl- 12/12/2000 RN Priecemr-s- Cail- re-4C.41or-i 2. IZ_rerndesea-rtw LTP engine flameout 4w' to fuel slarvation,contd. iA rii..)-r-rienva r4 / A 3. i_. TI.k..,.-wP50...-1 is( 4. 2.9 Toi..--t 2011 ©ATP CATI' (1564•So - 99-IS il. c.4-2occ.--e-ot) ©ATP Signature: c... ..--:O4—.--.----- Cov-i.nOndeAP Aft- li:161:1 • ob A-jr qtr.& FAA REPAIR STATION #70,1r6.9 2, you,/ Zot I MJUY650L .4 ' *ATP Printed 29/07/2011 15:48:32 /".. Page 1 of 5 EFTA01084887

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