HueyII_ProductSpecBook

Bell Huey IIProduct SpecificationsAugust 2012

Bell Huey II Product Specification i © 2012 Bell Helicopter Textron Inc. August 2012

Specifications subject to change without notice.

Table of ContentsPublisher’s Notice ............................................................................................................................1

Introduction ......................................................................................................................................3

Specification Summary (U.S. Units) ................................................................................................4

Specification Summary (Metric Units) .............................................................................................5

Exterior Dimensions (Low Gear) .....................................................................................................6

Bell Huey II Seating and Interior ......................................................................................................7

Standard Configuration....................................................................................................................8

Helicopter Performance Charts .......................................................................................................11

Cost of Operations...........................................................................................................................19

Limited Life Components .................................................................................................................22

Bell Huey II Product Specification 1 © 2012 Bell Helicopter Textron Inc. August 2012


Publisher’s NoticeThe data presented in this document are general in nature, and have been compiled from Bell Helicopter Textron 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 employees, and BHTI independent representatives (international dealers), and for prospective customers as an aid in determining estimated weight and performance of the helicopter when configured with equipment for specific missions.

Disclosure, reproduction, or use of any material in this document by persons other than BHTI employees, and BHTI independent representatives, and prospective customers are forbidden without written permission from Bell Helicopter Textron Inc.

The listings of Optional Equipment (“Kits”) are subject to revision and change, and also may be different for specific serial number helicopters or special custom configurations. Please consult the “Notes” column found in the optional equipment list tables for equipment compatibility. The continuing product improvement process of BHTI may cause some components, equipment, and compatibility to be changed or replaced.

The specifications, weights, dimensions, and performance data shown in this document are subject to change without notice.

© 2012 Bell Helicopter Textron Inc. Bell, 206, 407, 407GX, 429, 412, Huey II, LongRanger, and JetRanger are registered trademarks of Textron Innovations Inc.

Export Classification N/A. No Technical Data.


The data set forth in 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 Manual

IntroductionThe Bell Huey II is the ideal platform for the customer that needs heavy lift capability at an affordable price. Using the rugged and proven UH-1H airframe, the aircraft is upgraded with modernized components, giving the aircraft new life as a more robust and capable medium utility helicopter.

Unsurpassed as a law enforcement utility helicopter, the Bell Huey II carries up to 11 fully outfitted SWAT team members, without the need for external platforms, delivering excellent lift capability with single-engine economics. Emergency response teams also appreciate the exceptional cabin volume and ample power of the Bell Huey II, facilitating a wide range of search and rescue, disaster response, special operations and fire fighting missions.

The Bell Huey II is a versatile multirole medium lift aircraft that offers maximum performance at an affordable price. Starting with the venerable UH-1H airframe, the aircraft is upgraded with modern commercial accessories and all components are refurbished or replaced to zero-time condition.

This major upgrade greatly improves performance, decreases direct operating cost and extends the life of your Bell Huey II. Hover ceiling increases 39 percent on a standard day, 275 percent on a hot day. Payload increases to a maximum internal gross weight of 10,500 lb (4,763 kg) and 11,200 lb (5,080 kg) external gross weight. Direct operating cost is lowered by nearly 30 percent. Best of all, it’s the only UH-1H upgrade designed and backed by Bell Helicopter, so conversion is easy and reliability is assured. With over 300,000 flight hours amassed across a fielded fleet of over 225 Bell Huey IIs, it’s also proven to be the smart, cost efficient decision for Huey owners worldwide.

Nothing delivers like a Huey, and the Bell Huey II delivers the biggest return for the smallest investment. It’s a Huey at its best.


© 2012 Bell Helicopter Textron Inc. 4 Bell Huey II Production Specification August 2012



Specification Summary (U.S. Units)Weights lbEmpty Weight (VFR Std Config.) 1 5,627

Max Gross Weight (Internal) 10,500

Max Gross Weight (External) 11,200

Useful Load (Internal, VFR Std Config.) 4,873

Cargo Hook Capacity 5,000

Performance SummaryTakeoff, Gross Weight lb 8,500 9,500 10,500 11,200

IGE Hovering Ceiling (TOP capability)ISA ft 18,673 15,554 12,594 10,631

ISA+20°C ft 16,559 12,979 9,379 6,800

OGE Hovering Ceiling (TOP capability)ISA ft 14,544 11,200 5,333 (11,000 lb @ SL)

ISA+20°C ft 11,824 7,727 3,060 (10,800 lb @ SL)

T/O and Ldg Limit, WATISA ft 13,579 10,088 6,867 -na-

ISA+20°C ft 11,312 7,818 4,595 -na-

Service Ceiling (continuous power) ISA ft 20,000+ 19,073 16,223 -na-

Maximum Cruise Speed (true airspeed) SL, ISA ktas 118 112 106 -na-

Long Range Cruise Speed (average true airspeed) SL, ISA ktas 118 112 106 -na-

Range (no reserve) SL, ISA nmi 271 261 248 -na-

Endurance, at Loiter Speed (62 ktas) (no reserve) SL, ISA hr 2.9 2.8 2.6 -na-

Power Ratings: Honeywell T53-L-703Uninstalled

Thermodynamic PowerMechanical

LimitTakeoff Horsepower SHP 1,800 1,500

Max Continuous Power SHP 1,500 1,350

Transmission RatingsTakeoff (5-minute) SHP 1,290

Max Continuous Power SHP 1,134

FuelType Aviation Turbine

Capacity (Usable) 211 gallons

Note 1 VFR configuration includes all items listed in the Stardard Configuration table of this document as well as 46.5 pounds of engine/transmission oil and trapped fuel. Ballast is not included in standard configuration weight (ballast is a function of installed equipment).

Note 2 Performance shown for weights between 10,500 and 11,200 pounds is for external load operations only.

Specification Summary (Metric Units)Weights kgEmpty Weight (VFR Std Config.) 1 2,552

Max Gross Weight (Internal) 4,763

Max Gross Weight (External) 5,080

Useful Load (Internal, VFR Std Config.) 2,210

Cargo Hook Capacity 2,268

Performance SummaryTakeoff, Gross Weight kg 3,856 4,309 4,763 5,080

IGE Hovering Ceiling (TOP capability)ISA m 5,692 4,741 3,839 3,240

ISA+20°C m 5,047 3,956 2,859 2,073

OGE Hovering Ceiling (TOP capability)ISA m 4,433 3,414 1,625 (4,990 kg @ SL)

ISA+20°C m 3,604 2,355 933 (4,899 kg @ SL)

T/O and Ldg Limit, WATISA m 4,139 3,075 2,093 -na-

ISA+20°C m 3,448 2,383 1,401 -na-

Service Ceiling (continuous power) ISA m 6,096+ 5,813 4,945 -na-

Maximum Cruise Speed (true airspeed) SL, ISA km/h 219 207 196 -na-

Long Range Cruise Speed (average true airspeed) SL, ISA km/h 219 207 196 -na-

Range (no reserve) SL, ISA km 502 483 459 -na-

Endurance, at Loiter Speed (115 km/h) (no reserve) SL, ISA hr 2.9 2.8 2.6 -na-

Power Ratings: Honeywell T53-L-703Uninstalled

Thermodynamic PowerMechanical

LimitTakeoff Horsepower kW 1,342 1,118

Max Continuous Power kW 1,118 1,007

Transmission RatingsTakeoff (5-minute) kW 962

Max Continuous Power kW 846

FuelType Aviation Turbine

Capacity (Usable) 799 liters

Note 1 VFR configuration includes all items listed in the Stardard Configuration table of this document as well as 21.0 kilograms of engine/transmission oil and trapped fuel. Ballast is not included in standard configuration weight (ballast is a function of installed equipment).

Note 2 Performance shown for weights between 4763 and 5080 kilograms is for external load operations only.





Bell Huey II Seating and InteriorDesCrIPTIoN

The seats are of tubular construction with reinforced canvas webbing for support areas. The seats are attached to the floor and transmission support structure. Seats can be installed for rescue missions, then folded and stowed flat; or they can be folded for cargo missions as required.

ArrANGeMeNT

Eleven passengers can be seated in the aft area of the forward fuselage section. Three seats facing forward, and accomodating five passengers, may be placed across the cabin immediately forward of the transmission support structure. A one-passenger seat, without a back rest, is located between 2-place seats which have backs. Two, 2-place seats, without backs, are located aft of the five-passenger seats parallel to the helicopter center line. Passengers in these seats face outboard. Two single passenger folding seats, facing aft, with backs, are located just aft of the crew seats.

SEAT BELTS

Individual lap-type seat belts are provided for all seats. These same belts, with web extensions, are provided for litter patients when helicopter is used for rescue missions.

Exterior Dimensions (Low Gear)





Standard Configuration

GENERALFire Extinguisher (Qty 2)First Aid Kit (Qty 4)Skid Type Landing Gear with Replaceable Wear Shoes Wire Strike Protection SystemCargo Hook Provisions – Standard UH-1HInternal Rescue Hoist Provisions – Standard UH-1H New Windshields, Fuselage Windscreens, Door WindscreensInlet Barrier Filter (IBF)FUEL SYSTEMNew Crashworthy Fuel Cells (5-Cell)Crashworthy Provisions for Auxiliary Fuel SystemHot and Cold refueling receiverPOWERPLANTHoneywell T53-L-703 Turboshaft Engine5,000 Hour Time Between Overhaul (TBO)Honeywell OEM Specification Overhaul/ConversionroTorsMain Rotor, semi-rigid, two bladed212 Main Rotor Hub Assembly (w/ Grease Conversion)212 Stabilizer Bar Assembly212 Main Rotor Blades (Qty 2) High Visibility 212 Scissors & Sleeve Assembly212 Swashplate & Support212 Tail Rotor Hub Assembly212 Tail Rotor Blades (Qty 2)FLIGHT CONTROLSCyclic Stick (Pilot and Copilot)Collective Sticks (Pilot and Copilot)Tail Rotor Control Pedals-Adjustable (Pilot and Copilot)Hydraulic System (Single 1,500 PSI)Tail Rotor Controls Push-Pull Type Throughout212 Synchronized Elevators LIGHTINGCockpit – NVG (Instrument, Control, Map)Exterior

Landing LightStd UH-1H Search LightPosition Lights (Standard and NVG Compatible)Rotating Beacon or Strobe

ELECTRICAL100% RewiringDC Power Distribution System (28 VDC)

Main Generator (28 VDC 300 AMP)Standby Generator (28 VDC 300 AMP)Battery (28 VDC 34 AMP/HR) –NiCad

AC Power Distribution System (115 VAC 400 Hz 1-Phase)Main Inverter (115 VAC) Standby Inverter (115 VAC)

AVIoNICsCommunication

Intercommunication System NAT 301 065 (A 301) - 4 StationVHF / NAV #1 & #2 KX-165A (Honeywell)UHF - KTR-909 (Honeywell)Control Head - KFS-599A (Honeywell)

NavigationADF – KR-87 (Honeywell)Compass – KCS-55A (Honeywell)GPS – KLN-900 (Honeywell)Transponder – KT-76C (Honeywell)

OtherELT - A406 - 2HM (Artex)

INSTRUMENT PANEL AND INDICATORSPilot and Copilot

Airspeed, Altitude, Altimeter, Attitude, VVIRadar Altimeter - KRA-405, KNI-416 (Honeywell)HSI - KI-525 Pilot/ KI-825 Co-Pilot (Honeywell)RMI - KI-229 (Honeywell)Turn and Slip

CenterDual Tachometer (Nr & Nf) Torque Tachometer (Ng) Exhaust Gas Temperature Engine Oil Pressure & Temperature Transmission Oil Pressure & TemperatureFuel PressureFuel Quantity

Standard Configuration (continued)

NSTRUMENT PANEL AND INDICATORS (continued)Other

8 Day ClockMagnetic CompassVoltmeter, DC Voltmeter, AC Load meter, DC Load meter, AC

eXTerIorPrimed and ready for customer Paint SchemePaint Scheme finish includes up to three (3) ColorsINTerIorArmored Crew Seats – Black Fiber Mesh with CushioningPassenger Seats (11 places)

9-place standard black rag and tube seats Two 1-place utility rag and tube seatsBlack Interior Sound Insulation BlanketsoTHerGround Handling Wheels (Set of 2)



Helicopter Performance Charts





Airspeed Operating Limits Maximum Torque Available (5 Minute Operation)UH-1H-II with T53-L-703 Engine

Anti-Ice Off, Bleed Air Heater Off 324 Rotor / 6600 Engine RPM





IGE Hover CeilingUH-1H-II with T53-L-703 Engine

Maximum Torque Available (5 Minute Operation) Partical separator off, Heater off

324 Rotor / 6,600 Engine RPM, 4 Foot Skid Height

IGE Hover CeilingUH-1H-II with T53-L-703 Engine

Maximum Torque Available (Continuous Operation) Partical separator off, Heater off


6500 7500 8500 9500 10500 11500Gross

WeIGHT

- LB

0

2000

4000

6000

8000

10000

12000

14000

16000

18000

20000

Pre s

sUr

e AL T

ITU

De -

FT

IGe HoVer

CeILINGMAXIMUM

CoNTINUoUs

TorQUe

AVAILABLe

(CoNTINUoUs

oPerATIoN)

4 FT

sKID

HeIGHT

MODEL: UH-1H-IIENGINE: T53-L-703324

ROTOR

RPM

/ 6600

ENGINE

RPM

BASIC INLET

HEATER OFF

GENERATOR LOAD

100%

6500 7500 8500 9500 10500 11500Gross

WeIGHT

- LB

0

2000

4000

6000

8000

10000

12000

14000

16000

18000

20000

Pre s

sUr

e AL T

ITU

De -

FT

IGe HoVer

CeILINGMAXIMUM

TorQUe

AVAILABLe

(5

MINUTe

oPerATIoN)

4 FT

sKID

HeIGHT


ROTOR

RPM

/ 6600

ENGINE

RPM

BASIC INLET

HEATER OFF

GENERATOR LOAD

100%





OGE Hover CeilingUH-1H-II with T53-L-703 Engine

Maximum Torque Available (5 Minute Operation) Partical separator off, Heater off


6500 7500 8500 9500 10500 11500Gross

WeIGHT

- LB

0

2000

4000

6000

8000

10000

12000

14000

16000

18000

20000

Pre s

sUr

e AL T

ITU

De -

FT

oGe HoVer

CeILINGMAXIMUM

TorQUe

AVAILABLe

(5

MINUTe

oPerATIoN)

60 FT

sKID

HeIGHT


ROTOR

RPM

/ 6600

ENGINE

RPM

BASIC INLET

HEATER OFF

GENERATOR LOAD

100%

OGE Hover CeilingUH-1H-II with T53-L-703 Engine

Maximum Torque Available (Continuous Operation) Partical separator off, Heater off


6500 7500 8500 9500 10500 11500Gross

WeIGHT

- LB

0

2000

4000

6000

8000

10000

12000

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18000

20000

Pre s

sUr

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ITU

De -

FT

oGe HoVer

CeILINGMAXIMUM

CoNTINUoUs

TorQUe

AVAILABLe

(CoNTINUoUs

oPerATIoN)

60 FT

sKID

HeIGHT


ROTOR

RPM

/ 6600

ENGINE

RPM

BASIC INLET

HEATER OFF

GENERATOR LOAD

100%



Cost of operationsINTRODUCTIONBell Helicopter Textron’s cost of operations data for current production helicopters is based on information from Bell Helicopter operators and service facilities. BHT’s Product Support organization accumulates cost data from a diverse group of operators - large, small; sub-polar, subtropical; inland, coastal; corporate, charter. This information is analyzed to generate sample data for each production model which are averages of the field experience. BHT intends to continue monitoring actual costs to enable annual updates of the data to maintain its currency.

The following discussion is provided to review the variables involved in the helicopter’s direct and indirect cost of operations as well as its cost of ownership.

The total cost of helicopter ownership and operation involves both direct and indirect costs. The direct costs are those which are incurred essentially by the flight hour and include:

• Fuel, Lubricants • Basic Airframe Maintenance • Powerplant Maintenance

The indirect costs are not directly dependent upon the number of hours flown and include: • Insurance • Facilities (hangar, workshop, etc.) • Crew Compensation • Financial Factors (depreciation, investment tax credit, financing costs, etc.)

Sample direct operating cost data is available for each current production model. Detailed estimates for total costs relating to specific operations are available through the BHT regional marketing manager or corporate office using input data supplied by customer/prospect.

DIreCT CosTsFuel, LubricantsA typical average value of fuel and lubricant costs is included in the sample data provided for each model. Fuel consumption depends upon speed, temperature, externally-mounted accessories, sling loads, etc. A band of approximately 10% more or less than sample value will cover these factors for normal operations. Fuel pricing varies considerably based on where the fuel is purchased geographically and whether it is purchased retail or in bulk`. The sample cases use average retail purchase price prevalent at the time of the sample data are prepared.

Basic Airframe MaintenanceAirframe maintenance is divided into four categories:

• Periodic Inspections • Overhauls • Replacement of Retirement Parts • Unscheduled

Periodic inspections include those inspection tasks, with their part requirements, listed in the Maintenance Manual for each model. Man hours for periodic inspections can vary from the sample value provided because of differences in personal experience, tool and parts availability, facilities, environmental effects such as extremes in working temperatures. Man hour costs/hour are also variable among the Authorized Service Centers as a result of differences in local costs, overhead expenses and volume of work. The sample value is an average of costs per hour at Authorized Service Centers at the time of publication.

Overhauls include removal, disassembly, inspection, parts replacement, reassembly and reinstallation of certain components/assemblies at the periods stated in the BHT Maintenance Manual. Overhaul man hour and parts requirements are subject to considerable variation depending upon the helicopter’s operations and environments. The sample data reflect average values.





Cost of Operations (continued)Retirement parts are those which are subject to disposal after an operating time stated in the Maintenance Manual. These are normally components of the rotors/control systems which are subject to oscillatory loads and are designed and tested for use over a finite number of flight hours rather than on their condition. The replacement at the required intervals requires some labor which is included in the man hour data in the sample.

Unscheduled maintenance encompasses labor and parts replacement for major maintenance not covered under the formal Maintenance Manual requirements for inspections and overhauls. It also includes those additional maintenance requirements imposed by the manufacturer through issue of Service Bulletins.

The sample data for periodic inspections provide for some minor unscheduled maintenance tasks resulting from the inspection.

Powerplant MaintenanceThe powerplant (engine [s]) requires periodic inspection and overhauls. The overhaul periods are based on the number of operating hours or on the number of cycles, whichever is the first limit to be attained. Start cycles are a factor because thermal cycles are important in the design of the turbine engine’s rotating components. Overhauls are performed by the engine manufacturer and/or at authorized facilities. Powerplant overhaul can be performed for the engine as a unit, or in some cases for individual modules. (Modules can be gearbox, compressor, turbine, for example.) Each module can have its own overhaul period. Modular overhaul can be cost-effective for some operations and its use should be evaluated. Engine or module exchanges can be made in lieu of overhaul. For details, contact the engine manufacturer or his authorized distributors/service centers. The sample costs are based on an average exchange. The powerplant may also require unscheduled maintenance (unscheduled removals for repair, parts replacement).

INDIreCT CosTsInsuranceInsurance rates are based on a number of factors including claim experience, type of operations, and crew qualifications. Rates can be obtained from insurance agent/broker.

FacilitiesFacilities can include hangar, workshop, parts storage area, tools, ground support equipment and administrative area as appropriate to the specific operation.

Crew CompensationThe number of aircrew personnel depends on the individual operation; i. e., whether the normal crew consists of one or two pilots, hours per day flown, backup requirements for illness, vacation, etc. Bell Helicopter regional marketing managers can advise typical local costs for estimation purposes.

Financial FactorsFunding a helicopter purchase can be accomplished in a variety of ways, including cash, short term note, long term note, partnership, etc. For investment accounting, several depreciation methods also exist; straight line, double declining, sum of the year’s digits, etc. Value of resale is a significant factor.

Miscellaneous FactorsStaff expenses (other than aircrew and direct maintenance personnel), utilities, office expenses, etc.

OWNERSHIP ANALYSIS PROGRAMBell Helicopter Textron uses the most recently published edition of the Life Cycle Cost computer program provided by Conklin & de Decker Associates, Inc. to determine ownership costs for an operators planned period of utilization for the aircraft. Conklin’s Rotorcraft Analysis Office may be contacted at: Phone: (817) 277-6403 or Fax: (817) 277-6402.

Bell Helicopter’s regional marketing managers or corporate office personnel will be able to assist in preparing an ownership analysis which is customized for our customer’s specific individual conditions and needs.

Sample Direct Cost of Operations - US Dollars per Flight HourBell Huey II DMC Plus Fuel Estimate Summary Schedule

Parts Labor (1) TotalAirframe Maintenance

Scheduled Inspections (2) $3.73 $27.57 $31.30Scheduled Retirements (3) $114.98 $1.04 $116.02Scheduled Overhauls (4) $38.74 $7.68 $46.42Provision for Unscheduled Maintenance and Service Bulletins on above Components $13.54 $1.20 $14.74

On-condition Maintenance of Other Airframe Components $65.59 $96.78 $162.37subtotal $236.58 $134.27 $370.85

1.68 Mx Man-Hour / Flt. HrPowerPlant - Honeywell (T53-L-703)

Mfg. Estimate of Engine Cost - TBO 5,000 $120.00BHT Estimate of Additional Line Maintenance $8.90

subtotal $128.90Total DMC $499.75

Fuel and LubricantsFuel (5) $370.80Lubricants $3.71

subtotal $374.51Grand Total w/ Fuel $874.26

Notes: (1) Labor rate figured at $80.00 per hour. (2) Based on average flight hours for Bell 204/205/212 per year, 400 Flight Hours / Year. (3) Based on 100% Life. (4) Based on 100% TBO. (5) Catculated at 93 GPH at $4.00 per gallon.

Other assumptions: Basic VFR helicopter with no optional equipment installed, mature helicopter, no warranty cosiderations.

print production-quality Component TBO (Flt Hr) Component TBO (Flt Hr)

Main rotor Hub Driveshaft Hangar Assy 3,000Interim Inspection 1,200 Intermediate Gearbox 5,000Overhaul 2,400 Tail Rotor Gearbox 5,000

Mast Assembly (1) Tail Rotor Hub 2,500Interim Inspection 3,100 Oil Cooler Turbine Fan 1,000Overhaul 5,000 Starter/Generator 1,000

Transmission (1)

Interim Quill Inspection 1,200Interim Inspection 3,100Overhaul 6,000

Notes: (1) To obtain the total overhaul part cost for the component, add both the part cost for the interim inspection and overhaul categories. Do the same for labor hours.



Limited Life Components

Part Number Componenet Life in Flight Hours Qty per Aircraft

Main rotor Hub204-011-105-001 Trunnion 15,000 1204-011-120-005 Pitch Horn 3,000 2204-011-135-105 Bushing 3,600 4204-011-450-105 Mast 15,000 1204-012-103-005 Outboard Strap Fitting 3,600 2204-012-104-005 Strap Pin 2,400 4204-310-101-101 Tension-Torsion Strap 1,200 2212-010-103-007 Inboard Strap Fitting 2,400 2212-011-102-105 Main Rotor Yoke 10,000 1212-015-501-115 Main Rotor Blade 4,000 2

Main rotor Controls204-010-404-001 Gimbal Ring Assembly 9,000 1204-011-127-003 Pitch Link 9,000 2204-011-307-105 Stabilizer Bar Ctr Frame 10,000 1204-011-403-001 Swashplate Outer Ring 9,000 1204-011-404-127 Swashplate Support 600 1

204-011-405-013 Scissors Hub 9,000 1

204-011-407-001 Swashplate Drive Link 9,000 2204-011-408-107 Collective Sleeve 9,000 1204-076-267-005 Tube Assembly 6,400 1212-010-302-105 Mixing Lever 9,000 2212-010-403-107 Collective Lever 9,000 1212-010-404-005 Scissors Tube 9,000 2

Tail rotor Controls212-010-750-117 Tail Rotor Blade 2,500 2212-011-702-001 Tail Rotor Yoke 5,000 1

other204-040-433-101 Main Drive Shaft 5,000 1212-704-092-105 Control System Bolts 1,000 1

P.O. Box 482, Fort Worth, Texas 76101Phone: 817-280-2800Fax: 817-278-8802www.bellhelicopter.com

Bell Helicopter Textron Canada Limited12,800 rue de l’ AvenirMirabel, Quebec, Canada J7J1R4Phone: 450-437-3400Fax: 450-437-2006

©2012 Bell Helicopter Textron Inc.All Rights Reserved. Printed in USA August 2012

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