UH-60A/L Baseline UH-60A/L Baseline Today UH-60M Block I UH-60M Block I  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 / HUMS  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 / HUMS  Improved Turbine Engine Program (ITEP)  Improved Transmission  FLIR/MMR  Large Fuel Cell  Improved ASE  Composite Airframe  Improved Turbine Engine Program (ITEP)  Improved Transmission  FLIR/MMR  Large Fuel Cell  Improved ASE  Composite Airframe  Fly-by-Wire (FBW) Advanced Flight Controls  Common Cockpit - Common Avionics Architecture Sys (CAAS)  Full-Authority Digital Engine Control (FADEC)  Composite Tailcone/Driveshaft  JTRS – (Alt Comms)  CMWS / ICMD  Fly-by-Wire (FBW) Advanced Flight Controls  Common Cockpit - Common Avionics Architecture Sys (CAAS)  Full-Authority Digital Engine Control (FADEC)  Composite Tailcone/Driveshaft  JTRS – (Alt Comms)  CMWS / ICMD External Lift (4500 lbs) Net Ready External Lift (4500 lbs) Net Ready External Lift (9000 lbs) Net ready UH-60M Block II UH-60M Block II UH-60M Evolution FUTURE FORCE FUTURE FORCE UH-60M Upgrade UH-60M Upgrade Performance Attributes (4K/95):

UNCLASSIFIED UH-60M BLOCK 1 BLACK HAWK  On- Board Diagnostics (HUMS)  Conditioned Based Maintenance (CBM)  Performance Based Logistics  Monolithic Machined Parts  Transmission Beams  Corrosion Protection  Wide Chord Blades  T700-GE-701D Engine  Rotor Brake  Enhanced Laser Warning System  Improved IR Suppression  Crashworthy Fuel System (CEFS)  4 Multifunction Displays  Improved Data Modem  Enhanced GPS / INS System  BFT  Dual Digital Flight Controls  Digital Map  Integrated Storm Scope Enhanced Survivability New Cabin Section Propulsion Logistics Initiatives Integrated Digital Cockpit UNCLASSIFIED

UH-60M Upgrade Black Hawk Composite Tail Cone and Driveshafts New Cabin, Upper Deck, Transmission Beams and Servo Rails Wide Chord Blades Improved PVI Integrated JACS and CMWS Integrated ASE Displays FADEC Dual Channel, Triplex Fly-by-Wire FCS Dual Channel, Triplex Fly-by-Wire FCS Hydraulic and Electrical Improvements T700-GE-701D Engine with FADEC Permanent Magnetic Generators Transmission Driven Backup Pump Removed Quick Disconnect Fittings Extended Emergency DC Electrical Power Improved Ballistic Tolerance Common CAAS Cockpit Improved Stabilator Actuator, triplex position sensor with Digital Interface to FBW Airframe Improvements Regime based CLAWS with “Always On” Level 1 DVE Capability Fully integrated Triple Redundant Flight Director Embedded Flight Model Improved Hover, EICAS, WCA Displays Integrated FD Panel Integrated with FBW FCS Active Controls w/ Tactile Feedback for Improved Situational Awareness New MRS/TRS with 12.7 mm Ballistic Tolerance