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UH-60M BLACK HAWK

AAAA Annual Convent ionLTC(P) Chip Lunn

Product Manager, UH-60M11 May 2007

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Armys Work Horse In OIF

Bot tom Line:

Aircraft is workhorse of OIF and OEF

280 Aircraft in Theater as of 5 Feb 07 Hours flown - 3X greater than peace time

Harsh environment (sand/dust, FOD, heat, wind)

Combat Operations 17 accidental & combat losses in Theater since initiation of

operations

Issues - lack of situational awareness, power, survivability

Fleet is old (bulk of fleet is older than soldiersflying in them!) Army Acquisition Objective (AAO) for UH60A-to-A RECAP

aircraft: 193

Total UH-60A Inductions, to date: 95 of 193

Fully-Funded to RECAP 20 aircraft in FY2007

Adds 10 yrs of service life to the airframe; 20% reduction inmaintenance

RESET 40% of Aircraft in Theater have been RESET at least once 892 aircraft completed to date at AVG Cost of $0.97M

561 a/c RESET once, 164 a/c twice, and 1 a/c three times

A/C returning from OIF are to be RESET within 24 months

No Other Replacement Strategy exists

Current OPTEMPO about 3X more than Peacetime

As of 15 APRIL 2007

Fleet Cumulat ive Totals:

1,481,716 Hour s

Arm y Theater Cumulat ive Totals:461,076 Hou rs

MC: 87%

OPTEMPO: 42.9

Arm y Theater Current Info:

214 of 223 ACFT repo rted

11,724 hou rs

MC: 88%

OPTEMPO: 54.7

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UH-60M Evolu t ion

UH-60A/L

Baseline

Yesterday

UH-60M

Block I

2010 2015

Analog Cockpit STD Transmission 700 Series Engine

Digital Cockpit

Dual Digital Flight Controls Fully-Coupled Flt Director Wide Chord Blades Rotor Brake Provisions Folding Composite Stabilator Improved Durability Gearbox 701D Engine IVHMS ARC-231 CMWS/ICMD Blue Force Tracker

Improved Turbine EngineProgram (ITEP)

Improved Transmission

FLIR/MMR Large Fuel Cell Improved ASE Composite Airframe

Fly-by-Wire (FBW)Advanced Flight Controls

Common Cockpit -Common AvionicsArchitecture Sys (CAAS)

Full-Authority DigitalEngine Control (FADEC)

CompositeTailcone/Driveshaft

JTRS (when available)

External Lift (4500 lbs)Net Ready

External Lift (4500 lbs)Net Ready

External Lift (9000 lbs)Net ready

Block II

FUTUREFORCE

Performance Attributes (4K/95):

UH-60M

Block IUpgrade

READY NOW

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BLACK HAWK Acquis i t ion Strategy

UH-60M(ACAT ID)

UH-60L(ACAT IC)

PROGRAM

UH-60A/A(Recap)

UH-60M

Upgrade

10 9 11 12

LRIP C/A

FY05 FY06 FY07 FY09 FY10 FY11 FY12 FY13 FY14FY08

20 9 10 102922

IPR

Operational Test

PDR

1 2Test A/C Development

Dev Testing

FUE

DT / Flight Test

LUT SIL

Cut-In IPR Contract Award

OT

FRP

MY VII C/A

FUE

LRIP C/A

MS C

MY VIII CA

30 5

CDR

MEDEVAC MEP

5 66/59* 38 57 4717

UH-60AAO1806

ADS-33, E3, CTSF, Log Demo

Full-rate IPR

4 7 18 27

60 63 74

19

MEDEVAC MEP

MEDEVAC MEP 21 23 22

4 15

UH-60A-AAAO193

38 32

43 42 42 42US Navy MH-60S/MH-60R 42

* 7 A/C plus-up possible if supplemental Funds

received; otherwise P-Forms number is 59

1

NOW

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UH-60M Baseline BLACK HAWK

4 Multifunction Displays Improved Data ModemEnhanced GPS / INS SystemARC-231

TACAN

On- Board Diagnostics

(HUMS)

Conditioned Based

Maintenance (CBM)

Performance BasedLogistics

MonolithicMachined PartsTransmission

BeamsCorrosion

Protection

Wide Chord BladesT700-GE-701D EngineRotor Brake

Enhanced Laser Warning System Improved IR SuppressionCrashworthy Fuel System (CEFS)

Common Missile Warning System

Blue Force TrackerDual Digital Flight ControlsDigital Map Integrated Storm Scope

Enhanced Survivabi l i ty

New Cabin Sect ionPropu ls ion

Log is t ics

Init iat ives

Integrated Digital Cockp it

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Fleet Management

Training &Publications/

IETMs

FieldMaintenance

Condition Based Maintenance

UID

Goal:

Increase Airc raf t Avai labi l i ty

Reduce Operat ional Cost

Improve Readiness

Maintenance &Logistics Data

Overhaul & Repair

Performance BasedLogistics

Fleet Visibility

Health & Usage Monitoring

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HH-60M MEDEVACMission Equ ipment Package

Multifunctional Crew Seat

On-board Oxygen Generating System

Navigation Forward Looking Infra-Red (FLIR) Variable Position Litter System

External Electric Rescue Hoist

Environmental Control System

Additional Emergency Medical Equipment

TACAN303 HH-60M's

Same Configuration as Baseline M plus the Mission Equipment Package

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Externally lift 4500 lbs

4,000 feet, 95 degrees F

Radius: 135 km

Armored pilot/copilot seats (7.62mm)

Provisions for armor in cabin (7.62mm)

Key Interface Profiles (KIP) compliance

Net-centric Operational WarfareReference Model (NCOW RM) compliance

Information assurance

Integrated Architecture Products

Key Performance Parameters

External Lif t

Force Protect ion

CriteriaParameter

Net Ready

No increase in IR from UH-60L

Passive and Active CM systems

Active IR warning and countermeasures

Self sealing internal fuel systems (7.62mm)

Survivabi l i ty

Status

All Criteria Demonstrated

Compliance with KIP / NCOW RMhas been demonstrated by Armyand Joint Certification Process

System accredited by DesignatedApproving Authority (31 Oct 06)

IA Products complete in ORD

Demonstrated/Qualified

Provisions included

Component level demonstrated,system level test prior to FRP

Demonstrated

Demonstrated on UH-60L

Demonstrated/Qualified

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ATEC Assessment

The UH-60M is Effective, Suitable, and Survivable:

All KPPs Met:

External lift: 4,500 lb, 135 km range

NET Ready: JITC Certification (assessment of MYVII), IAAccreditation, demonstration of network connectivity in IOT.

Survivability KPPs: CMWS integrated; meets fuel cell and crewprotection requirements.

ORD reliability thresholds: MTBMA, MTBEMA and MTBMAFexceed requirement

All mission types successful during three separate operationallyrealistic and tactically challenging OT events.

Observations:

Improved crew performance

Digital map for navigation reduces workload

Steeper learning curve in cockpit but yields big dividends.

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ATEC AssessmentRecommended Imp rovements

Monitor and ensure AN/ARC-231 Encryption load devicesreceive Upgraded software to enable easier loading of radios.

Enable warm reboot of individual radios and processors and

improve overall reliability of radios and systems.

Improve ergonomics of crew chief seats and redesign harness

system to improve ease of ingress and egress of crews.

Improve NVG lighting to include Red navigation light and IR

searchlight.

Improve Flight Management System to include more waypoints,

routes, Flight plans and provide a one-button target store.

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UH-60M Reliabi l i ty Improvement

Hours

0

50

100

150

MS C DTCombined

DT/IOTIOT

MTBMA 40

MTBMAF 15

MTBEMA 3.7

261.6

MAR 05354.9 Hours

DEC 05

608.9 Hours

DEC 06

925.3 Hours

DEC 06

261.6 Hours

3.38

25.3

59.2

70.6

32.9

48.7

115.6

130.8

32.7

4.3 6.7

MTBMA

MTBMAF

MTBEMA

ORDRequirements

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Techn ical Performance Measures (TPM)UH-60M Baseline

Attribute Spec. Status

Weight Empty (lb) 12,500 12,418

Min. Rate of Climb, OEI (ft./min.) 100 160

External Lift Payload (lb.) KPP 4500 5395

Sustained Cruise Airspeed OEI (KTAS) 100 107

Primary Mission Combat Radius (km.) 225 236

IGE TOGW, OEI (lb.) at Mid. Mission 14771 15010

CSquared Endurance (hr.) 4.0 4.2

Sustained Cruise Airspeed (KTAS) 145 146

Self-Deployment (nm.) 1056 1118

MTBMAF

(Mean Time Between Mission Affecting Failures )15 49

MTBMA

(Mean Time Between Mission Aborts)40 116

MTBEMA

(Mean Time Between Essential Maintenance Actions)3.7 6.7

KEY:Within Spec

as o f: 1/4/2007

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Transpo rtable B lack Hawk OperationsSimu lator (T-BOS) Sys tem

High fidelity flight simulator

Ruggedly containerized fordeployability/transportability

Transportable by ship, rail, road, andmilitary air

Deployable to corps, brigade and

battalion Power and environmental control

systems included

< 8 hours set up with four person team

Capabilities:

Immersive training environment forIndividual/crew tasks

Aircrew integrated mission planning,mission rehearsal, maintenance testpilot operations, emergencyprocedures

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UH-60M Upgrade Black Hawk

Composite Tail Coneand Driveshafts

New Cabin, Upper Deck,Transmission Beams and Servo Rails

Wide Chord Blades

ImprovedPVI

IntegratedJACS and CMWS

Integrated ASEDisplays

FADEC

Dual, Triple Fly-by-Wire FCS

Active Controls w/Tactile Feedback for

Improved Situational Awareness

New MRS/TRS with12.7 mm Ballistic Tolerance

Hydraulic and ElectricalImprovements

T700-GE-701D Enginewith FADEC

Permanent Magnetic GeneratorsTransmission Driven Backup PumpRemoved Quick Disconnect FittingsExtended Emergency DC Electrical PowerImproved Ballistic Tolerance

Common CAAS Cockpit

Improved Stabilator Actuator,triplex position sensor with

Digital Interface to FBW

Airframe Improvements

Embedded Flight ModelImproved Hover, EICAS, WCA DisplaysIntegrated FD PanelIntegrated with FBW FCS

Regime based CLAWS withAlways On Level 1 DVE

Capability Fully Integrated TripleRedundant Fight Director

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Upgrade Status

ostSchedulePerformance

CAASOperation in

IBTF

FADEC Equipped

T701D

Cabin andComposite Tail Cone

Upgrade FlightControl Laws RASCAL

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Overal l Program Summary

Operational Test Training completed Upgrade System CDR completed

Operational Testing completed

IKPT Training started January 2007

MEDEVAC Excursion January 2007

CMWS/ARC-231 DT/OT March 2007

Full Rate Production Decision May 2007

First Unit Equipped Training July 2007

Upgrade Aircraft Roll-out September 2007

Upgrade First Flight late 2007 First Unit Equipped April 2008 (Baseline)

Upgrade LUT May 2008

Upgrade Low Rate Cut-in late 2008