Rev. 1, June 2010 2 Bell 407 Product Speci
Rev. 1, June 20102Bell 407 Product Specification
Publishers NoticeThe data presented in this document is general in nature, and has been compiled from Bell HelicopterTextron, Inc. [BHTI] source materials including but not limited to; The Approved Rotorcraft Flight Manual,Maintenance Manual, Illustrated Parts Catalog, and other engineering design specifications.This document is intended for the use of BHTI Sales Personnel and for prospective customers as an aidin determining estimated weight and performance of the helicopter when configured with equipment forspecific missions.Disclosure, reproduction, or use of any material in this document by persons other than BHTI employees,and BHTI independent representatives [International Dealers] is forbidden without written permissionfrom Bell Helicopter Textron.The listings of Optional Equipment [KITS] are subject to revision and change, and also may be different forspecific serial number helicopters or special custom configurations. Please consult the NOTES found inthe right margins of the optional equipment list pages for equipment compatibility. The continuing productimprovement process of BHTI may cause some components, equipment, and compatibility to be changedor replaced.The specifications, weights, dimensions, and performance data shown in this document are subject tochange without notice. 2010 Bell Helicopter Textron Inc.Bell 206B3, 206L-4, 407, 427, 430, 412, 609, JetRanger and LongRanger areregistered trademarks of Bell Helicopter Textron Inc.All rights reserved.Bell 407 Product Specification1Rev. 1, June 2010
Exterior DimensionsStandard Low Skid Gear407Standard GearOptional High Skid Gearwith AAI Flightstep 407High Skid GearRev. 1, June 20102Bell 407 Product Specification
Optional EmergencyFloat Gearwith AAI Floatstep 407Float GearOptional Blade FoldingKit DimensionsMinimum Hanger Size*Rotor Not Folded25.1 ft x 36.6 ft(7.7 m x 11.2 m)Minimum Hanger Size*Rotor Folded7.7 ft x 41.6 ft(2.4 m x 12.7 m)*Allowance should be made for high skid gear, ground wheels,emply fuel condition and door lip when considering hangardoor width and heightBell 407 Product Specification3Rev. 1, June 2010
Internal Dimensions(approximate)Approximate Cargo Space:Aft Cabin2.4 cubic meters(85 cubic feet)Left front0.6 cubic meters(20 cubic feet)Baggage compartment0.45 cubic meters(16 cubic feet)Floor Loading:Cabin3.7 kg/sq. meter(75 lb/ sq. foot)Baggage4.2 kg/sq. meter(86 lb/sq. foot)113 kg(250 pounds)Max Baggage weightSpecifications subject to change without notice.Rev. 1, June 20104Bell 407 Product Specification
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Specification Summary (U.S. Units)WEIGHTSLBSStandard Configuration Weight (Note 1)2676Internal Gross Weight [Normal / Optional] (Note 2)5000 / 5250*External Load Gross Weight6000Useful Load [Gross Wt Standard Configuration Wt] {Normal / Optional} (Note 2)2332 / 2582*Maximum External Load [Cargo Hook Limit}2646Performance Summary (International Standard Day except as noted)Takeoff gross weightIGE Hovering Ceiling(4.5 h Skid Height)OGE Hovering CeilingService Ceiling @ MCP(100 400*ISA 20Cft15,60011,70079003150*ISA 0*ISA 20Cft13,800965057503150*ISA 30Cft11,05065001850(5200lb @ SL)*ISAft20,000 20,000 17,60016,050ISA 20Cft20,000 21nm383375364357kn118120120120Cruise at Long Range Cruise Speed (LRC)Range {standard fuel}LRC SpeedRange {standard fuel}4000 ft, ISALRC SpeedMaximum Cruise SpeedSL,ISAkn136135133132@ Takeoff Gross WeightSL,ISA 20Ckn1301291261254000 ft, ISAkn1401381351334000 h, ISA 20Ckn133130126123SL,ISAhr4.03.93.83.74000 ft, ISAhr4.54.44.24.1Endurance @ Loiter 60 knENGINE RATING:Rolls-Royce 250-C47B with Full Authority Digital Electronic Control:Takeoff Horsepower (Uninstalled Thermodynamic Capability)(Mechanical Limit)Maximum Continuous (Uninstalled Thermodynamic Capability)(Mechanical Limit)SHP813SHP674SHP701SHP630TRANSMISSION RATING (Engine Output):Takeoff Horsepower (5 minutes)SHP674Maximum ContinuousSHP630FUEL CAPACITY (Usable):Standard127.8 US GallonsAuxiliary (Optional)19.0 US Gallons* Refer to demonstrated takeoff and landing and maximum operating altitude notes on the performance chartsNote 1: The Standard Configuration Weight includes 7-place upholstered interior with individual seat belts, carpeting, andsoundproofing material. Ballast is not included since it is a function of installed optional equipment. 13 pounds of oil isincluded.Note 2: Operation at Internal Gross Weight above 5000 pounds / 2381 Kilograms requires the Optional Increased Internal GrossWeight KitThe data set forth on this document are general in nature and may vary with conditions.For performance data and operating limitations for any specific flight mission, reference must be made to the approved Flight ManualRev. 1, June 20106Bell 407 Product Specification
Specification Summary (Metric Units)WEIGHTSKGStandard Configuration Weight (Note 1)1214Internal Gross Weight [Normal / Optional] (Note 2)2268/2381*External Load Gross Weight2722Useful Load [Gross Wt Standard Configuration Wt] {Normal / Optional} (Note 2)1058/1171*Maximum External Load [Cargo Hook Limit}1200Performance Summary (International Standard Day except as noted)Takeoff gross weightKG1814204122682381ISAm5852475537181646*ISA 20Cm475535662408960*IGE Hovering Ceiling(1.4 M Skid Height)ISA 30Cm403926971402625*ISAm5364422131851646*OGE Hovering CeilingISA 20Cm420629411753960*ISA 30Cm33681981564(2358kg @ SL)*ISAm6096 6096 53644892ISA 20Cm6096 541043593856Service Ceiling @ MCP(0.5 m/s)Cruise at Long Range Cruise Speed (LRC)Range {standard fuel}SL,ISALRC SpeedRange {standard fuel}1200m, ISALRC m/h219222222222Maximum Cruise SpeedSL,ISAkm/h250250246244@ Takeoff Gross WeightSL,ISA 20Ckm/h2412392342311200m, ISAkm/h2592562502461200m, ISA 20Ckm/h246241234228SL,ISAhr4.03.93.83.71200m, ISAhr4.54.44.24.1Endurance @ Loiter 111 km/hENGINE RATING:Rolls-Royce 250-C47B with Full Authority Digital Electronic Control:Takeoff Horsepower (Uninstalled Thermodynamic Capability)(Mechanical Limit)Maximum Continuous (Uninstalled Thermodynamic Capability)(Mechanical Limit)kW606kW503kW523kW470TRANSMISSION RATING (Engine Output):Takeoff Horsepower (5 minutes)kW503Maximum ContinuouskW470FUEL CAPACITY (Usable):Standard484 LitersAuxiliary (Optional)72 Liters* Refer to demonstrated takeoff and landing and maximum operating altitude notes on the performance chartsNote 1: The Standard Configuration Weight includes 7-place upholstered interior with individual seat belts, carpeting, andsoundproofing material. Ballast is not included since it is a function of installed optional equipment. 13 pounds of oil isincluded.Note 2: Operation at Internal Gross Weight above 5000 pounds / 2381 Kilograms requires the Optional Increased Internal GrossWeight KitThe data set forth on this document are general in nature and may vary with conditions.For performance data and operating limitations for any specific flight mission, reference must be made to the approved Flight ManualBell 407 Product Specification7Rev. 1, June 2010
407 SeatingCrew Seating - Two individual ergonomically designed seats with adjustable lumbar support, each equippedwith seat belt, double strap shoulder harness and inertia reel, are located in the cockpit. Thecolor and upholstery material for the seats, and interior trim of the cockpit match that whichis selected for the cabin. The seat belts are black.Standard Seating and Interior TrimThe standard cabin seating consists of five ergonomically designed seats with individual seat belts and singlestrap shoulder harness, arranged with three equal width forward facing seats across the rear of the cabin andtwo individual rearward facing seats aft of the cockpit. Available with Grey, Blue, Red, or Tan upholstery fabricwith Black seat belts. All vinyl or vinyl surround / fabric insert upholstery is available as an extra cost option.The standard interior trim consists of full plastic closeouts on all airframe areas, vinyl covered arm rests, andmolded plastic outboard headliners. The floor is covered in low loop blend carpet. The standard seating andinterior trim are included in the basic aircraft weight.Specifications subject to change without notice.Rev. 1, June 20108Bell 407 Product Specification
Corporate Seating and Interior TrimThe corporate cabin seating consists of five ‘Overstuffed Style’ seats with individual seat belts and singlestrap shoulder harness, arranged with two extra wide forward facing outboard seats and a middle seat foroccasional use across the rear of the cabin (with a fold down arm rest between the outboard seats) andtwo individual rearward facing seats aft of the cockpit. Available with Pewter, Mushroom, Dark Blue, Saddle,Burgundy, Smoke Grey, and Forest Green upholstery with color coordinated seat belts (Crew seat belts areblack). Seats can be all fabric (basic ship), optional leather with fabric inserts or all leather. The corporateinterior trim consists of full plastic closeouts on all airframe areas, fabric covered outboard headliner blankets,and armrests covered with color coordinated leather. Carpet is 100% wool cut pile. Selection of the corporateinterior trim also specifies installation of Corporate Soundproofing, which provides a reduced interior noiselevel. The corporate seating and interior trim (and corporate soundproofing) increase the basic aircraft emptyweight 9 lbs. (4.1 kg.).Specifications subject to change without notice.Bell 407 Product Specification9Rev. 1, June 2010
Standard Configuration (Items Included in List Price)AIRFRAMEROTORS AND CONTROLSCabin; bonded aluminum honeycomb, andsemimonocoque structure with composite side panelsand aft fuselage skinsMain rotor, soft in plane flex beam hub with fourfiberglass blades, CHOICE of STANDARD [black topwhite bottom] or HIGH VISIBILITY [orange/white topwhite bottom] painted rotor bladesDoors (five), one hinged double door & copilot door onleft side, pilot & passengers on right side, all doors arecomposite materialTail rotor; two fiberglass blades, semirigidHydraulic boost system for Main & Tail Rotor (separatepump and reservoir)Landing gear, tubular skid type with replaceable kidshoesMechanical flight control linkages throughoutLocks for cabin doors and luggage compartmentLuggage compartment (16 cu ft, 250 lbs capacity), withcomposite doorAirspeed Activated Pedal Stop [AAPS] with built in testfunction, electrical override release switch, and manualoverride releaseProvisions for mooring, jacking and single point liftingTRANSMISSION DRIVE SYSTEMTail boom, monocoque structure with vertical fin andfixed stabilizerSoft mounted pylon isolation systemFreewheeling unit (between engine and maintransmission)Tail skid (tail rotor guard)Kaflex input drive shaftWindows (except windshield), gray tinted plexiglass[sliding panels in doors are available as a no-costoption]Gearbox, tail rotor, 90O reductionMain transmissionThree color exterior paint schemes Standard paintschemes A, B, and C, as shown on paint selector pageat rear of this book. Custom paint schemes are quotedon request.Oil coolerOil filter with replaceable type cartridgeOil pump, constant pressureINTERIORFLIGHT AND ENGINE INSTRUMENTS7-place interior with soundproofing, carpeting, and datacase. Color options available for upholstery and carpetClock, digital w/ OAT & Volt Meter7-place shoulder harnesses, dual straps in cockpit,single strap in cabinDual tachometer (rotor and engine)Compass, magneticInclinometerFire extinguisher, cabinIndicator, airspeedFirst aid kitIndicator, altimeterParcel shelf (behind aft seat)Indicator, IVSIRam air ventilation systemIndicator LCD, engine oil pressure / temperatureStorage area behind pilot & copilot seatsPOWERPLANTIndicator LCD, fuel quantity with forward cell quantityswitchRolls-Royce Model 250-C47B gas turboshaft enginewith FADEC and Direct Reversion to Manual GovernorIndicator LCD, fuel pressure / generator load meterIndicator LCD, NG speedFuel pump, engine drivenw / EXCEEDANCE MONITERINGIndicator LCD, Torque w / EXCEEDANCE MONITERINGFuel pumps (4 canister type) w/ 2 boost pumpssubmerged in main tank, and 2 transfer pumps in theforward fuel tanksIndicator LCD, transmission oil pressure / temperatureIndicator LCD, T. O. T. w / EXCEEDANCE MONITERINGFuel system, 127.8 gal [484 liter] usable capacityHour meter (located in battery compartment)Oil system, 1.5 gal [5.7 liter] capacity, with sight glassMaintenance download ports(FADEC & LCD instruments)Compressor wash provisionsEngine mounted 10-micron oil filterAirframe Fuel Filter [eliminates requirement for PRIST]Specifications subject to change without notice.Rev. 1, June 201010Bell 407 Product Specification
MONITORING SYSTEMELECTRICALCaution indication lights:28 volt DC systemAuto relightBattery, 17 amp-hr nickel cadmiumBaggage doorExternal power and grounding receptacleBattery hotLights:Anticollision strobeCockpit/mapInstrumentAft cabinLanding (two 250 watt)PositionBattery relayCheck instrumentsCyclic CenteringEngine anti-iceEngine chip detectorEngine out and low rotor RPM warning lights and hornwith mute switch. (Low RPM or engine out)Starter-generator (180 ampere)Engine overspeed28 volt outlet in cabinFuel boost pump inoperative, left & rightHeated pitot tube & Static portsFuel transfer pump inoperative, left & rightMISCELLANEOUSFuel filter bypass indicatorCovers, engine inlet and exhaust stackFuel valve in transitCover pitot tubeFuel lowFlight bagFadec faultGround handling wheels with lift tubeFadec failOperating manuals:Aircraft log bookEngine log bookEngine operating & maintenance manualEngine parts manual flight manualSolid state voltage regulatorPedal StopFadec degradedFadec manualGenerator failureHydraulic systemIllustrated parts catalogMaintenance and overhaul manualLitter doorTiedown assemblies, main rotor and tail rotorRestart FaultStartTail rotor gearbox chip detectorTransmission oil pressureTransmission oil temperatureTransmission(& Freewheeling unit) chip detectorSpecifications subject to change without notice.Bell 407 Product Specification11Rev. 1, June 2010
Optional AccessoriesRefer to notes for kit compatibilityAdditional kits and STC items may be available for factory installation.Please consult sales or contract personnel regarding special needs prior to selection of final configuration.Wt(lbs)Wt (Kg)NotesHIGH SKID GEAR with FLIGHTSTEPS32.114.61, 2EMERGENCY POPOUT FLOATS (LANDING GEAR)83.838.01, 3, 18Kit DescriptionBell Manufactured KitsAIRFRAMEEMERGENCY POPOUT FLOATS (FLOTATION KIT)88.940.318EMERGENCY POPOUT FLOATS (RESERVOIR KIT)68.731.218SKID GEAR FAIRINGS for LOW SKID ONLY11.95.4AUX. FUEL TANK PROVISIONS (19 GAL)5.02.3AUX. FUEL TANK EQUIPMENT (19 GAL)29.613.4DUAL CONTROLS11.75.3AFT AUDIO ICS - 3 STATION with 3 HEADSETS & DROP CORDS8.63.9AFT AUDIO ICS - 5 STATION with 5 HEADSETS & DROP CORDS13.56.18.13.7AUDIOAVIONICSVHF EQUIPMENT (KX-155) for OMNI w/KI-208 ONLY4VHF EQUIPMENT (KX-165) for ANY KCS-55A w/HIS KI-525A8.84.04ADF EQUIPMENT (KR-87)6.32.94TRANSPONDER PROVISIONS (KT-76A) MODE C0.90.45TRANSPONDER EQUIPMENT (KT-76A) MODE C2.51.15TRANSPONDER PROVISIONS (DIGITAL) (KT-70)0.70.355TRANSPONDER EQUIPMENT (DIGITAL) (KT-70)3.81.7GPS PROVISIONS (KLN-89B)4.42.0GPS EQUIPMENT (KLN-89B w/KA33 BLOWER)5.32.4OMNI w/CDI KI208 for KX-155 ONLY3.61.6COMM#2 KY196A EQUIPMENT3.41.5AVIONICS MASTER SWITCH (standalone-NO ENC. ALT.)1.40.6COMM#2 KY196A PROVISIONS1.70.8VHF/ADF PROVISIONS w/AUDIO PANEL ( KMA24H-71 )9.14.1COMPASS SYSTEM KCS-55A PROVISIONS w/KI-525A3.91.8COMPASS SYSTEM KCS-55A EQUIPMENT w/KI-525A7.63.4COMPASS SYSTEM KCS-55A PROV w/KI-525A (GPS COMPAT.)4.92.25, 67COMPASS SYSTEM KCS-55A EQIP W/ KI-525A (GPS COMPAT.)8.33.87, 8ENCODING ALTIMETER w/AVIONICS MASTER SWITCH2.31.01, 5TURN & SLIP / ATTITUDE INDICATOR4.52.0DIRECTIONAL GYRO3.71.7ELT POINTER 4000 W/3001 WHIP ANTENNA3.91.8ADF ANTENNA RELOCATION-2.0-0.94VHF ANTENNA RELOCATION3.01.44C. I. S. [Russian] CERTIFICATION PROVISIONS1.20.597Specifications subject to change without notice.Rev. 1, June 201012Bell 407 Product Specification
Kit DescriptionWt(lbs)Wt (Kg)NotesPARTICLE SEPARATOR WITH BLEED AIR NETWORK17.07.71, 10ENGINE FIRE DETECTION2.00.9QUIET CRUISE1.50.75250 POUND GROSS WEIGHT OPTION0.00.05.22.4EXPANDABLE BLADE BOLTS (2 EACH)1.50.7CARGO HOOK EQUIPMENT10.44.7ENGINEEQUIPMENTSNOW BAFFLE1CARGO HOOK PROVISIONS3.51.6ROTOR BRAKE7.33.3CARGO RESTRAINT INTERNAL PROVISIONS1.90.928 AMPS HOUR BATTERY24.911.3COCKPIT STORAGE KIT1.40.6LITTER EQUIPMENT (ONE)22.010.01111SKI PROVISIONS (for Single Litter ONLY)1.50.7LITTER PROVISIONS for Single Litter5.72.6INTERIOR, CORPORATE7.33.31, 12SOUND-PROOFING, CORPORATE8.23.71, 12STANDARD HEADLINER with A/C DUCTS4.72.11ARM RESTS, CORPORATE (pair)0.30.11, 12CORPORATE SEATS7.73.51WINDOWS, SLIDING R OPENERS CREW2.81.3DOOR OPENERS PASSENGER2.81.3DOOR OPENERS BAGGAGE1.00.5INTERIORPAINTMARKINGS FOR HIGH VISIBILITY M/R BLADES (WHITE & ORANGE)CreditsEQUIPMENTGROUND HANDLING WHEELSPAINTNO EXTERIOR PAINTWHITE PAINT ONLYVendor Kits - STC’sAIRFRAMESTEP / HANDLE (ONE STEP)1.00.5MAINTENANCE STEP FOLDING L/H2.00.9MAINTENANCE STEP FOLDING R/H2.00.9MAINTENANCE STEP FIXED L/H2.00.9MAINTENANCE STEP FIXED R/H2.00.9SLIDING DOOR L/H10.64.813Specifications subject to change without notice.Bell 407 Product Specification13Rev. 1, June 2010
Kit DescriptionSLIDING DOOR R/HWt(lbs)Wt (Kg)Notes10.64.813ENVIRONMENTAIR CONDITIONER (SINGLE FORWARD EVAPORATORS)95.443.34, 15AIR CONDITIONER (DUAL FORWARD EVAPORATORS)105.647.94, 15BLEED AIR HEATER W/ CHIN BUBBLE DEFROSTER22.610.310BLEED AIR ARCTICHEATER W/ CHIN BUBBLE DEFROST23.610.710ENGINE BLEED AIR NETWORK3.81.710FORCED AIR VENTILATION28.412.915PARAVION BLADE FOLDING KIT W/2 EXPANDABLE BOLTS1.80.816WIRE STRIKE - HIGH SKID - RECOMMENDED KIT12.45.617WIRE STRIKE - LOW SKID - RECOMMENDED KIT12.95.917FLOOR PROTECTOR (CREW AND PASSENGER)8.33.8FLOOR PROTECTOR tional Accessories Explanatory NotesAll equipment kits require Provision Kits prior to installationNotes: For commonality, notes shown below are identical in Product Specification and Price List.(1)Price and / or Weight includes credit for basic ship hardware removed.(2)Kit includes Flitesteps (STC # 407-326-003) [weight; 28 lbs (12.7 kgs)].(3)Kit includes Floatsteps (STC # 407-303-003) [weight; 29 lbs(13 kgs)].(4)When ANY Airconditioner Kit is installed, and VHF and/or ADF are installed, the antennas must be relocated.(5)Encoding Altimeter or Blind Encoder (customizing) is required to enable Mode C/Mode S altitude reporting and/or GPS altitudeinput. Customer must obtain Aircraft ID code for Mode S.(6)One Geographic Database must be selected and installed concurrently with GPS Equipment KLN-89B.(7)When ANY Compass System KCS-55A is installed the Directional Gyro is NOT required.(8)For GPS compatible KCS-55A to function, GPS Provisions & Equipment must be installed.(9)Requires installation of VHF/ADF Prov. and VHF/eqpt.; Flight Inst.; ELT; and Engine Fire Det.(10) Particle separator and Bleed Air Heaters both include Bleed Air Network. If both kits are installed subtract 3.8 lb(1(11) Requires installation of -159 Litter provisions.(12) Corporate interior requires corporate soundproofing and corporate arm rests.(13) Sliding door(s) require sliding door arm rest(s) 407-705-605-105 which subtracts 1.9 lb (0.9kg) per door.(14) Standard or High Visibility Main Rotor Blade Paint to be specified by Sales Order.(15) Requires Standard Headliner with A/C ducts (407-705-604-105), weight 4.0 lb(1.8kg).(16) Weight is for provisions only.(17) For High Skids or floats, weight is 12.7 lb(5.8kg). The Wire Strike Kit is a RECOMMENDED extra cost option. The customermust specify on
Takeoff gross weight lbs 4000 4500 5000 5250 IGE Hovering Ceiling ISA ft 19,200 15,600 12,200 5400* (4.5 h Skid Height) ISA 20C ft 15,600 11,700 7900 3150* . Service Ceiling @ MCP ISA m 6096 6096 5364 4892 (0.5 m/s) ISA 20C m 6096 5410 4359 3856 Cruise at Long Range Cruise Speed (LRC)
The Rt. Rev. George N. Hunt The Rev. Frederick K. Jellison The Rev. Dn. Ida R. Johnson The Rev. Michaela Johnson The Rev. Paul S. Koumrian The Rev. Canon Harry E. Krauss * The Rev. H. August Kuehl The Rev. Richard T. Laremore * The Rev. Donald A. Lavallee The Rev. Canon John E. Lawrence The Rev. Dr. Gary C. Lemery * The Rev. Dn. Betsy Lesieur *
Conc Diagram- All Failures Cispa Data Avalon Date PCB Lot Number Igarashi TPS date codes. MB Panel Number VIAS Hole Location Failure 9-June'09 11-June'09 923 162 12-June'09 923 163,164 TBD TBD 1 13-June'09 923 164 15-June'09 923 166 16-June'09 923 167 17-June'09 923 168,171 18-June'09 923 171 19-June'09 923 171 20-June'09 923 171 22-June'09 923 173 23-June '09 923 179 24-June '09 923 .
NACE Rev. 1.1 (ISIC Rev. 3) codes are often linked with more than one NACE Rev. 2 (ISIC Rev. 4) code. For example, 323 NACE Rev. 1.1 is linked with 261, 263 and 264 NACE Rev. 2 codes; 261 NACE Rev. 2 is linked with only one part of 311, 312, 313, 321 and 323 NACE Rev. 1.1 codes. Thus, it is not possible to obtain full codes of NACE
June 16 Shelach Lecha June 23 - Korach June 30 Hukath We Remember Sylvia Marans Elberg - June Vera Meyerhoff - June Daniel Rosenberg - June1 Edward Wandrei - June 6 Helen Feinberg-Ginsburg - June 6 Thelma Cohn - June 12 Wilma Sizemore June - 16 Joseph P. Suffel - June 21 Eliot Rivers - June 31 Paul Aaron Kowarsky - Sivan 14 -
Winter Carnival 14 June P&C Disco 8 17 June Board Meeting 18 June 19 June 20 June 21 June Bletchley Vale Cup 9 24 June Swimming Lessons Yr 3 – 6 P&C Meeting 25 June Swimming Lessons Yr 3 – 6 26 June Swimming Lessons Yr 3 – 6 Pre Primary Junior Olympics 27 June Swimming Lessons Yr 3 – 6 Yr2 Start Smart 28 June Swimming Lessons Yr 3 – 6 10
1912-1914 Most Rev. Edward Joseph Hanna 1939-1948 Most Rev. Thomas Arthur Connolly 1947-1962 Most Rev. Hugh Aloysius Donohoe 1948-1950 Most Rev. James Thomas O’Dowd 1950-1969 Most Rev. Merlin Joseph Guilfoyle 1637-1969 Most Rev. Mark Joseph Hurley 1967-1979 Most Rev. William Joseph McDonald 1970-1974 Most Rev. Norman Francis McFarland
Unión Pentecostés de Iglesias Locales Internacional, Incorporadas BOARD OF TRUSTEES Rev. Dr. Santiago "Jimmy" Longoria, Jr. Rev. C. Isaac De Los Santos D.Th Rev. Dr. John V. Carmona Rev. Josué B. Sánchez Rev. Roy Faragoza Rev. Becky Tafolla Rev. Salomon Munoz COMISIÓN DE ARTÍCULOS CONSTITUCIONALES Rev. Josué B. Sánchez
16 Rev. Michael Keller 1983 17 Rev. Cyril McDonnell 2000 19 Rev. Thomas Foudy 2019 21 Msgr. David Bushey 1994 21 Rev. Jose Izquierdo SJ 1997 22 Rev. Julian Bastarrica, OFM 1990 23 Rev. Harry Ringenberger 2016 29 Rev. John Lama 1994 Eternal rest grant unto them O Lord, And may perpetual light shine upon them.
