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Transcript of 07_UH60M
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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