ROTORCRAFT INLET BARRIER FILTER SYSTEMS for AIRBUS H125/AS350 SERIES HELICOPTERS (Single Hydraulic)

Transcription

1 ROTORCRAFT INLET BARRIER FILTER SYSTEMS for AIRBUS H125/AS350 SERIES HELICOPTERS (Single Hydraulic)

2 INSTALL BEFORE FLIGHT Helicopters routinely contend with dust, sand and debris that attack turbine engines and impact engine reliability, hampering efficient engine operation. Installing an Inlet Barrier Filter (IBF) system is the most effective way to protect engines from damage ranging from lost efficiency to catastrophic failure while adding significant advantages. Meet established engine time between overhaul requirements More power available than alternate sand filter options Longer engine life due to elimination of erosion Reduced engine maintenance cost Available factory-direct Dry media in certification H125/AS350 PERFORMANCE AT-A-GLANCE Features Design Features Filter Life (Service Cycles) Emergency Bypass Components Performance Certificates (call for latest updates) H125/AS350B/BA/B1/B2/B3/B3e, Soloy SD/SD1/SD2, Heli-Lynx FX1/FX2 Part number /103 Single, rugged, lightweight, flat filter common to many AS350 models, utilizing captive fasteners allowing fast filter exchange; additional self-contained and structurally integrated fairing assembly mounted into the top of the existing engine inlet cowling; simple installation with minimal modifications 4,500 hours (15 cycles every 300 hours) Aft-facing bypass door to protect against dirt & snow; no flight restrictions with bypass open Easily accessible and common to other models; non-intrusive cockpit installation; components easily inspected via bypass door or integral sight glass; filter maintenance aid for on-condition assessment of filter status while aircraft is on the ground. Environmental Cover for all weather non-operating protection included. Certified for use with basic inlet charts, backup Sand Filter charts United States, Canada, Europe, Brazil For more information, contact: Chesterfield Airport Road, Chesterfield, MO North America Europe aerospace.emea@donaldson.com To learn more about the visit Brochure No. F (2/16) 2016 Donaldson Company, Inc. All rights reserved. Donaldson Company, Inc. reserves the right to change or discontinue any model or specification at any time and without notice. Printed in the U.S.A.

3 ROTORCRAFT INLET BARRIER FILTER SYSTEMS for MD HELICOPTERS MD 500 and MD 900/902

4 INSTALL BEFORE FLIGHT Helicopters routinely contend with dust, sand and debris that attack turbine engines and impact engine reliability, hampering efficient engine operation. Installing an Inlet Barrier Filter (IBF) system is the most effective way to protect engines from damage ranging from lost efficiency to catastrophic failure while adding significant advantages. Reduced engine turbine operating temperatures over alternate systems Meet established engine time between overhaul requirements More power available than alternate filtration options Longer engine life due to elimination of erosion Reduced engine maintenance cost Available factory-direct Dry media in certification MD 900 MD 500 PERFORMANCE AT-A-GLANCE Features Design Features MD 500 Series 369H/HE/HM/HS/D/E/F, AH/MH-6 Part number Two flat filters, dual entry air inlets, utilizes new composite cowling, new reduced FOD potential bypass system MD 900/902 Series Part number Two conformal filters, no increased drag penalty, structurally integrated into the existing manufacturer s inlet plenum for simple installation, utilize existing bypass system Filter Life (Service Cycles) 7,500 hours (15 cycles every 500 hours) 4,500 hours (15 cycles every 300 hours) Emergency Bypass Components Performance Certificates (call for latest updates) Inboard-facing flush bypass door protects against dirt & snow; no flight restrictions with bypass open Easily accessible and common to other models; includes a cockpit annunciation and activation switch along with a filter maintenance aid for on-condition monitoring while aircraft is on the ground. Environmental Cover for all weather non-operating protection included. Certified with Rotorcraft Flight Manual charts for Particle Separator Installed, Scavenge Air Off, Without Mist Eliminator United States, Argentina, Brazil, Canada, Europe Utilizes existing MD 900 production aircraft bypass system Cockpit annunciation and activation switch is standard MD 900 production aircraft equipment. IBF messaging is through the IIDS display. Environmental Cover for all weather non-operating protection included. US, Canada and European certified for use with EAPS charts, Category A operations approved United States, Europe, Canada For more information, contact: Chesterfield Airport Road, Chesterfield, MO North America aerospace.americas@donaldson.com Europe aerospace.emea@donaldson.com To learn more about the visit Brochure No. F (2/16) 2016 Donaldson Company, Inc. All rights reserved. Donaldson Company, Inc. reserves the right to change or discontinue any model or specification at any time and without notice. Printed in the U.S.A.

5 ROTORCRAFT INLET BARRIER FILTER SYSTEMS for BELL 206B/206L and 407 HELICOPTERS

6 INSTALL BEFORE FLIGHT Helicopters routinely contend with dust, sand and debris that attack turbine engines and impact engine reliability, hampering efficient engine operation. Installing an Inlet Barrier Filter (IBF) system is the most effective way to protect engines from damage ranging from lost efficiency to catastrophic failure while adding significant advantages. Meet established engine time between overhaul requirements More power available than alternate filtration options Longer engine life due to elimination of erosion Bell 407 & 206L-4 available factory-direct Reduced engine maintenance cost Inducer Vent Filter (IVF) available to supplement IBF for 100% inlet protection Dry media in certification Bell 407 Bell 206B/206L PERFORMANCE AT-A-GLANCE Features Design Features Bell 206B, OH58A/C Part number Two rugged, lightweight, flat filters designed for fast exchange via a unique top access door without removal of the inlet fairing; self-contained and structurally integrated into the existing inlet plenum; simple installation with minimal modifications maintaining firewall integrity and utilizing original particle separator mount provisions; new engine water wash provision that operates without removal of the filters Bell 206L-3/4, 206L-1(C30) Part number Single, rugged, lightweight, flat filter designed for fast exchange via a unique side access door without removal of the inlet fairing; self-contained and structurally integrated into the existing inlet plenum; simple installation with minimal modifications maintaining firewall integrity and utilizing original particle separator mount provisions; new engine water wash provision Bell 407/407 GX Oiled Media part number , Dry Media part number Single, rugged, lightweight, flat filter designed for fast exchange via a unique side access door without removal of the inlet fairing; self-contained and structurally integrated into the existing inlet plenum; simple installation with minimal modifications maintaining firewall integrity and utilizing original particle separator mount provisions; new engine water wash provision Filter Life (Service Cycles) 4,500 hours (15 cycles every 300 hours) 4,500 hours (15 cycles every 300 hours) 4,500 hours (15 cycles every 300 hours) Emergency Bypass Components Performance Certificates (call for latest updates) Unique plenum floor mounted bypass door to protect against dirt & snow; no flight restrictions with bypass open Easily accessible via lower side access doors, common components with other models; non-intrusive cockpit installation; filter maintenance aid for on-condition assessment of filter status while aircraft is on the ground Certified for use with basic inlet charts, backup EAPS charts Unique plenum floor mounted bypass door to protect against dirt & snow; no flight restrictions with bypass open Easily accessible via lower side access doors, common components with other models; non-intrusive cockpit installation; filter maintenance aid for on-condition assessment of filter status while aircraft is on the ground Certified for use with basic inlet charts, backup EAPS charts Unique plenum floor mounted bypass door to protect against dirt & snow; no flight restrictions with bypass open Easily accessible via lower side access doors, common components with other models; non-intrusive cockpit installation; filter maintenance aid for on-condition assessment of filter status while aircraft is on the ground Certified for use with basic inlet charts, backup EAPS charts; improved hover performance with BHT-407- FMS-8 United States, Argentina, Brazil, Canada, Europe United States, Argentina, Brazil, Canada, Europe United States, Argentina, Brazil, Canada, Europe For more information, contact: Chesterfield Airport Road, Chesterfield, MO North America aerospace.americas@donaldson.com Europe aerospace.emea@donaldson.com To learn more about the visit Brochure No. F (2/16) 2016 Donaldson Company, Inc. All rights reserved. Donaldson Company, Inc. reserves the right to change or discontinue any model or specification at any time and without notice. Printed in the U.S.A.

7 ROTORCRAFT INLET BARRIER FILTER SYSTEMS for BELL 205A1, UH-1H, HUEY II, EAGLE SINGLE, and BELL 429, 430/230 HELICOPTERS

8 INSTALL BEFORE FLIGHT Helicopters routinely contend with dust, sand and debris that attack turbine engines and impact engine reliability, hampering efficient engine operation. Installing an Inlet Barrier Filter (IBF) system is the most effective way to protect engines from damage ranging from lost efficiency to catastrophic failure while adding significant advantages. Meet established engine time between overhaul requirements More power available than alternate filtration options Longer engine life due to elimination of erosion Reduced engine maintenance cost Bell 429 available factory-direct Bell 205 Bell 430 PERFORMANCE AT-A-GLANCE Features Design Features Bell 205A1, UH-1H, Huey II, Eagle Single Part number Four rugged, lightweight, flat filters for fast filter exchange; self-contained structural assembly is mounted aft of the main rotor mast and integrated into the existing inlet plenum; new forward firewall interface: improved engine drive shaft and coupling access; minimal aircraft modifications; includes improved engine wash manifold Bell 429 Part number /104 Conformal filters that blend into the aircrafts smooth lines with an integral bypass system. Installed as standard configuration on the production line Bell 430/230 Part number /103 Dual, rugged, lightweight, flat filter design; selfcontained and structurally integrated into the existing inlet cowlings utilizing existing mounting provisions and creating an internal bypass plenum; minimal aircraft modifications Filter Life (Service Cycles) 4,500 hours (15 cycles every 300 hours) 6,000 hours (15 cycles every 400 hours) 4,500 hours (15 cycles every 300 hours) Emergency Bypass Components Performance Certificates (call for latest updates) Unique dual access bypass system with vertical doors to protect against dirt & snow; no flight restrictions with bypass open Easily accessible and common to other models; includes a cockpit annunciation and activation switch along with a filter maintenance aid for on-condition monitoring while the aircraft is on the ground. Environmental Cover for all weather nonoperating protection included. Certified for use with basic inlet performance charts or other approved STC Flight Manual charts United States, Canada, Brazil Inboard-facing flush bypass door protects against dirt & snow; no flight restrictions with bypass open Easily accessible bypass components, integral cockpit indication system with standard avionics package In accordance with Bell flight manuals Bell Type Certificate, United States, Canada, Europe, Brazil Internal inlet plenum bypass doors protects against dirt & snow; no flight restrictions with bypass open Easily accessible and common to other models; includes a cockpit annunciation and activation switch along with a filter maintenance aid for on-condition monitoring while aircraft is on the ground Certified for use with basic inlet charts, backup EAPS charts United States, Brazil For more information, contact: Chesterfield Airport Road, Chesterfield, MO North America aerospace.americas@donaldson.com Europe aerospace.emea@donaldson.com To learn more about the visit Brochure No. F (2/16) 2016 Donaldson Company, Inc. All rights reserved. Donaldson Company, Inc. reserves the right to change or discontinue any model or specification at any time and without notice. Printed in the U.S.A.

9 ROTORCRAFT INLET BARRIER FILTER SYSTEMS for FINMECCANICA AB139 and AW139 HELICOPTERS

10 INSTALL BEFORE FLIGHT Helicopters routinely contend with dust, sand and debris that attack turbine engines and impact engine reliability, hampering efficient engine operation. Installing an Inlet Barrier Filter (IBF) system is the most effective way to protect engines from damage ranging from lost efficiency to catastrophic failure while adding significant advantages. Meet established engine time between overhaul requirements More power available than alternate filtration systems Longer engine life due to elimination of erosion Reduced engine maintenance costs Available factory-direct Dry media in certification AW139 PERFORMANCE AT-A-GLANCE Features Design features Filter Life (Service Cycles) Emergency Bypass Components Performance Certificates (Call for latest updates) AB139, AW139 Part number Two low-drag conformal fairing assemblies with two filters per side designed for fast filter exchange, fairing assembly structural kit mounted on the existing engine door to create a sealed intake plenum, auxiliary air inlet eliminated, straight forward IBF installation 4,500 hours (15 cycles every 300 hours) Flush inward opening side facing bypass door to protect against dirt & snow; no flight restrictions with bypass open Easily accessible and common to other models; includes a cockpit annunciation and activation switch along with a filter maintenance aid for on-condition monitoring while aircraft is on the ground. Environmental Cover for all weather non-operating protection included. US, Canada, Brazil certified for use with basic inlet charts, backup EAPS charts, Category A operations approved STC: United States, Brazil, Canada Finmeccanica TC: Italy For more information, contact: Chesterfield Airport Road, Chesterfield, MO North America aerospace.americas@donaldson.com Europe aerospace.emea@donaldson.com To learn more about the visit Brochure No. F (2/16) 2016 Donaldson Company, Inc. All rights reserved. Donaldson Company, Inc. reserves the right to change or discontinue any model or specification at any time and without notice. Printed in the U.S.A.

11 ROTORCRAFT ENGINE INLET BARRIER FILTER SYSTEMS for MILITARY AIRCRAFT

12 INSTALL BEFORE FLIGHT Helicopters routinely contend with dust, sand and debris that attack turbine engines and impact engine reliability, hampering efficient engine operation. Installing an Inlet Barrier Filter (IBF) system is the most effective way to protect engines from damage ranging from lost efficiency to catastrophic failure while adding significant advantages. Reduced engine turbine operating temperatures over alternate systems More power available than alternate filtration solutions Meets established engine time between overhaul limits Reduced engine maintenance over alternate systems Extends engine life due to elimination of erosion Available factory-direct PERFORMANCE AT-A-GLANCE Features OH-58A/OH-58C Kiowa, TH- 57, TH-67 Part number AH/MH-6 Little Bird Part number UH-1H Huey, TH-1H Part number OH-58D/F Kiowa Warrior Part number H-60 BLACK HAWK Part number , -105 Design Features Structurally integrated kit; two rugged flat filters for fast filter exchange via top access door; simple installation with minimal modifications; maintains firewall integrity; utilizes original mount provisions for particle separator: includes improved water wash manifold Structurally integrated kit; two rugged flat filters with quarter turn fasteners for fast exchange; all new engine inlet fairing engineered to be structurally sound, lighter, and less complex; reduction in parts compared to original OEM design; unique dual entry inlet optimizes airflow in hover and forward flight Structurally integrated kit; four interchangeable rugged, lightweight, flat filters designed for fast filter exchange: selfcontained kit integrated into existing inlet plenum; new forward firewall interface; improved drive shaft and coupling access; minimal aircraft modification: includes improved water wash manifold Structurally integrated kit; two rugged, lightweight, flat engine inlet filters; separate system for protection of the engine inducer bleed system with one small flat filter; designed for fast filter exchange after removal of blast shields; self-contained inside existing inlet plenum; maintains existing engine wash system Structurally integrated Sikorsky A-kit; removable Donaldson B-kit; modular design; transition module mounts to engine inlet; filter & bypass module mount to aircraft; eight interchangeable filters; swings open for maintenance access; cruise flight bypass system; inherent bird strike protection capability Emergency Bypass Internal compartment bypass door to protect against dirt, ice & snow; activation allows flight in all environments Conformal external bypass door with fewer parts than original OEM design; activation allows flight in all environments Dual access bypass system with vertical doors to protect against dirt & snow; activation allows flight in all environments Internal compartment bypass door protects against dirt & snow; activation allows flight in all environments Unique bypass system with forward ram air entry for use as bypass or for power recovery in forward flight Components Easily accessible via lower side access doors; non-intrusive cockpit installation; filter maintenance aid for on-condition filter assessment Easily accessible externally and inside forward inlet fairings; Uses OEM cockpit annunciation system; filter maintenance aid for on-condition filter assessment Easily accessible externally and inside forward cover; nonintrusive cockpit installation; filter maintenance aid for oncondition filter assessment Easily accessible via lower side access doors; Filters protected by blast shields; non-intrusive cockpit installation Easily accessible B-Kit with components mounted for quick change out; modular design for fast combat damage repairs Performance Operate with more power margin than EAPS, uses basic inlet charts with backup EAPS charts; lower pressure drop than other options with superior particle separation efficiency Per TMs, significant performance improvement over EAPS with lower inlet pressure drop and a flat pressure drop characteristic with forward airspeed; fully qualified for weapons fire Operate with more power margin than EAPS, uses basic inlet charts; lower pressure drop than other options with superior particle separation efficiency Per TMs, lower pressure drop than EAPS; superior particle separation efficiency; fully qualified for weapons fire Per TMs, designed to provide lowest possible inlet loss with fully contaminated filters in a hover condition with superior particle separation efficiency Proven The US Army has equipped 100% of its TH-67 fleet and has equipped over 25% of its OH- 58A/C fleet with the IBF. The Iraqi Air Force operates the IBF. Commercial kits used by law enforcement and commercial operators worldwide. Standard configuration on the US Army Special Operations Little Bird; Standard equipment on the MD Helicopters production line. The Royal Jordanian Air Force, Afghan Air Force and Republic of Korea Army OH/AH-6 operate the IBF. Commercial kits used by law enforcement and commercial operators worldwide. Fielded by the US Department of State on its fleet of UH-1H Huey II aircraft. The Iraqi Air Force, Royal Thai Air Force and Georgian Air Force operate the IBF. Commercial kits used by law enforcement and commercial operators worldwide. Standard configuration on the US Army fleet. Engines routinely make published TBO even while operating in Iraq and Afghanistan. The significant advantages of the filter led to it being specified on the US Army Armed Reconnaissance Helicopter (ARH) Program. The US Army has equipped 25% of its UH-60 fleet with the IBF. The United Arab Emirates Air Force, Royal Saudi Air Force and Swedish Armed Forces operate the IBF. For more information, contact: Chesterfield Airport Road, Chesterfield, MO North America aerospace.americas@donaldson.com Europe aerospace.emea@donaldson.com To learn more about the visit Brochure No. F (2/16) 2016 Donaldson Company, Inc. All rights reserved. Donaldson Company, Inc. reserves the right to change or discontinue any model or specification at any time and without notice. Printed in the U.S.A.

13 ROTORCRAFT AUXILIARY POWER UNIT INLET BARRIER FILTER SYSTEMS for MILITARY AIRCRAFT

14 INSTALL BEFORE FLIGHT Helicopters routinely contend with dust, sand and debris that attack turbine engines and impact engine reliability, hampering efficient engine operation. Installing an Inlet Barrier Filter (IBF) system is the most effective way to protect engines from damage ranging from lost efficiency to catastrophic failure while adding significant advantages. Donaldson Military platform APU IBF Systems (U.S. patent #6,824,582) are available for the UH-60 BLACK HAWK, SH-60 SEAHAWK, AH-64 Apache, CH-47 Chinook, UH-1Y Venom, and AH-1Z Viper. Meets established APU time between overhaul limits Extends APU life due to elimination of erosion Provides clean filter air to secondary systems Available factory-direct No operating limitations 99% particle separation efficiency at rated APU airflow AH-64A Apache APU PERFORMANCE AT-A-GLANCE Features UH-60 BLACK HAWK, UH-1Y Venom, AH-1Z Viper Hamilton Sundstrand APU Part number UH-60 BLACK HAWK, Honeywell APU Part number AH-64A Apache Part number AH-64D Apache Part number CH-47 Chinook Part number Design Features Structurally integrated APU kit; two rugged half moon filters designed for fast filter exchange; common APU model firewall provisions Structurally integrated APU kit; two rugged half moon filters designed for fast filter exchange; common APU model firewall provisions; integrated APU lifting lug Structurally integrated APU kit; new inlet plenum with dual entry inlets; two rugged half moon filters for fast filter exchange; improved sealing system Structurally integrated APU kit; new inlet plenum with dual entry inlets; two rugged half moon filters for fast filter exchange; improved sealing system Structurally integrated APU kit; two rugged half moon filters designed for fast filter exchange; can install without removing APU Components Frame assembly secures filters to APU; filter maintenance aid for on-condition filter assessment Frame assembly secures filters to APU; filter maintenance aid for on-condition filter assessment Plenum assembly secures filters to APU; filter maintenance aid for on-condition filter assessment Plenum assembly secures filters to APU; filter maintenance aid for on-condition filter assessment Frame assembly secures filters to APU; filter maintenance aid for on-condition filter assessment Proven The US Army/Navy have equipped over 1,300 of its APUs with the IBF. The Israeli Air Force, Royal Jordanian Air Force, Royal Saudi Air Force, Swedish Armed Forces and United Arab Emirates Air Force operate the APU IBF. The US Army/Navy have equipped over 600 of its APUs with the IBF. The US Army has equipped over 100 of its APUs with the IBF. This kit is completing qualification testing with the US Army. The US Army has over 170 Donaldson APU IBF kits. For more information, contact: Chesterfield Airport Road, Chesterfield, MO North America Europe aerospace.emea@donaldson.com To learn more about the visit Brochure No. F (2/16) 2016 Donaldson Company, Inc. All rights reserved. Donaldson Company, Inc. reserves the right to change or discontinue any model or specification at any time and without notice. Printed in the U.S.A.

15 ROTORCRAFT INLET BARRIER FILTER SYSTEMS for FINMECCANICA AW109E/AW109S/AW109SP, AW119 KOALA, and AW119KE HELICOPTERS

16 INSTALL BEFORE FLIGHT Helicopters routinely contend with dust, sand and debris that attack turbine engines and impact engine reliability, hampering efficient engine operation. Installing an Inlet Barrier Filter (IBF) system is the most effective way to protect engines from damage ranging from lost efficiency to catastrophic failure while adding significant advantages. Meet established engine time between overhaul requirements More power available than alternate filtration systems Longer engine life due to elimination of erosion Reduced engine maintenance cost Available factory-direct AW109 AW119 PERFORMANCE AT-A-GLANCE Features Design features AW109E/AW109S/AW109SP Part number Two conformal filters mounted in the existing engine cowl doors, two bypass filters, no increased drag penalty, internally mounted bypass system with easy access aft cover AW119, AW119Ke Part number Three conformal filters, no increased drag penalty, selfcontained and structurally integrated system into the existing manufacturer s inlet plenum for simple installation Filter Life (Service Cycles) 4,500 hours (15 cycles every 300 hours) 4,500 hours (15 cycles every 300 hours) Emergency Bypass Components Performance Certificates (Call for latest updates) Internally mounted inside the upper sail to protect from environmental conditions Easily accessible and common to other models; includes a cockpit annunciation and activation switch along with a filter maintenance aid for on-condition monitoring while aircraft is on the ground. Environmental Cover for all weather non-operating protection included. US certified for use with basic inlet charts, Category A operations approved United States, Brazil Aft-facing bypass door to protect against dirt & snow; no flight restrictions with bypass open Easily accessible and common to other models; includes a cockpit annunciation and activation switch along with a filter maintenance aid for on-condition monitoring while aircraft is on the ground. Environmental Cover for all weather nonoperating protection included. US certified for use with basic inlet charts, European certified for use with EAPS charts United States, Canada, Brazil, Europe For more information, contact: Chesterfield Airport Road, Chesterfield, MO North America aerospace.americas@donaldson.com Europe aerospace.emea@donaldson.com To learn more about the visit Brochure No. F (2/16) 2016 Donaldson Company, Inc. All rights reserved. Donaldson Company, Inc. reserves the right to change or discontinue any model or specification at any time and without notice. Printed in the U.S.A.

17 ROTORCRAFT INLET BARRIER FILTER SYSTEM/UNIVERSAL FILTER MODULE for HEAVY TWIN HELICOPTERS

18 INSTALL BEFORE FLIGHT Helicopters routinely contend with dust, sand and debris that attack turbine engines and impact engine reliability, hampering efficient engine operation. Installing an Inlet Barrier Filter (IBF) system is the most effective way to protect engines from damage ranging from lost efficiency to catastrophic failure while adding significant advantages. Meet established engine time between overhaul requirements More power available than alternate filtration solutions Longer engine life due to elimination of erosion Reduced engine maintenance cost PERFORMANCE AT-A-GLANCE Features Design features Filter Life (Service Cycles) Emergency Bypass Components Availability Universal Filter Module (UFM) currently available for Sikorsky S-61 and SH-3 Variants, applicability to wide range of heavy twin rotorcraft with other applications in development Low-drag filter module mounted forward of the engine inlets, entire module quickly removable, features three filters easily accessed and removable for service. Improved engine inlet access compared with other configurations. Environmental Cover for all weather non-operating protection included. 4,500 hours (15 cycles every 300 hours) Forward facing dome bypass provides protection from the environment for internal engine components Common filter elements interchangeable among aircraft, service same as other Donaldson IBF s. Contact Coulson Group for S-61 Commercial Aircraft and Donaldson for Military SH-3 or Para-Military S-61 applications. The Coulson Group 4890 Cherry Creek Road, Port Alberni, BC, Canada V9Y 8E9 Phone (250) Fax (250) For more information, contact: Chesterfield Airport Road, Chesterfield, MO North America Europe aerospace.emea@donaldson.com To learn more about the visit Brochure No. F (2/16) 2016 Donaldson Company, Inc. All rights reserved. Donaldson Company, Inc. reserves the right to change or discontinue any model or specification at any time and without notice. Printed in the U.S.A.

19 ROTORCRAFT INLET BARRIER FILTER SYSTEMS for AIRBUS H130/EC130B4/ EC130 T2/AS350B3/AS350B3E HELICOPTERS (Dual Hydraulic)

20 INSTALL BEFORE FLIGHT Helicopters routinely contend with dust, sand and debris that attack turbine engines and impact engine reliability, hampering efficient engine operation. Installing an Inlet Barrier Filter (IBF) system is the most effective way to protect engines from damage ranging from lost efficiency to catastrophic failure while adding significant advantages. Meet established engine time between overhaul requirements More power available than alternate sand filter options Longer engine life due to elimination of erosion Reduced engine maintenance cost Available factory-direct Dry media options in development H130/EC130B4/EC130 T2/AS350B3/AS350B3e PERFORMANCE AT-A-GLANCE Features Design Features Filter Life (Service Cycles) Emergency Bypass Components Performance Certificates (call for latest updates) H130/EC130B4/AS350B3/AS350B3e with dual hydraulics Oiled Media part number , Dry Media part number Single, rugged, lightweight, flat filter utilizing captive fasteners allowing fast filter exchange; selfcontained and integrated inside the existing engine inlet cowling; simple installation with minimal modifications 4,500 hours (15 cycles every 300 hours) Aft-facing bypass door to protect against dirt & snow; no flight restrictions with bypass open Easily accessible and common to other models, non-intrusive cockpit installation, components easily inspected via bypass door, filter maintenance aid for on-condition assessment of filter status while aircraft is on the ground. Environmental Cover for all weather non-operating protection included. Certified for use with basic inlet charts, backup Sand Filter charts United States, Canada, Brazil For more information, contact: Chesterfield Airport Road, Chesterfield, MO North America Europe aerospace.emea@donaldson.com To learn more about the visit Brochure No. F (2/16) 2016 Donaldson Company, Inc. All rights reserved. Donaldson Company, Inc. reserves the right to change or discontinue any model or specification at any time and without notice. Printed in the U.S.A.