S-92 SAR Standard Presentation - Aircraft Sales & Leasing

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SIKORSKY S-92®

SEARCH AND RESCUE CONFIGURATION

This Page Contains No Technical Data Controlled by the ITAR or EARSikorsky Aircraft Corporation Proprietary Information

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S-92® HELICOPTER

Overview FeaturesSafetyMaintenance and Support



SIKORSKY S-92Modern Evolution of Two World-Class Aircraft

UH60 Black Hawk• Rugged, Powerful Propulsion• Crash and Damage Tolerant• All Weather

S61R Sea King• Large Stand Up Cabin• Multi-mission

S-92A• FAR Amendment 29

Requirements


SAFE, RELIABLE MULTI-MISSION SOLUTION

Off Shore

Search And RescueVIP/HOS Transport

Utility


S-92® HELICOPTER209 In-service Aircraft


EXCEPTIONAL UTILLIZATION

Over 706,000 flight hours total

Over 246,000 flight hours January 2012 to January 2013

~1300 flight/hrs per year per aircraft

90%

3%

4% 1% 2%

Flight Hours by Mission Type

Off Shore SAR Utility VIP VVIP


S-92® FLEET HIGH TIME AIRCRAFT


EXCEPTIONAL RELIABILITY

9

More On Time Departures More Aircraft Revenue Opportunity

93% Fleet Wide Unscheduled Availability

* Estimated


EXCEPTIONAL SAFETY

Flight Hours: estimated from various public sources and Sikorsky DataAccident Data: www.AviationSafety.net and Sikorsky Data

0.15 – Fixed Wing Part 121 Scheduled Airline

0.61 – Fixed Wing Part 135 On-Demand Ops

2.39 – Civil Helicopter Twin Turbine Engine


S-92® HELICOPTER

Overview FeaturesSafety and SurvivabilityMaintenance and Support



Large Multi Use Cabin• 6 ft cabin height • 19 passenger seats• High capacity heating and air conditioning

Large Multi Use Cabin• 6 ft cabin height • 19 passenger seats• High capacity heating and air conditioning

S-92® KEY FEATURES

Reliable State of the Art Propulsion System• Composite 3rd Gen main and tail rotor blades • Flaw tolerant rotor system and dynamics • Dual GE CT7-8A engines • HUMS monitoring

Reliable State of the Art Propulsion System• Composite 3rd Gen main and tail rotor blades • Flaw tolerant rotor system and dynamics • Dual GE CT7-8A engines • HUMS monitoring

Modern Navigation And Flight Controls• Large intuitive flat panel displays• Integrated systems for enhanced situation awareness• Fully coupled 4 axis autopilot

Modern Navigation And Flight Controls• Large intuitive flat panel displays• Integrated systems for enhanced situation awareness• Fully coupled 4 axis autopilot

Certified All Weather Operation• Cat A operation, VFR, IFR• Launch into known icing conditions• Rotor start in 55kts Winds

Certified All Weather Operation• Cat A operation, VFR, IFR• Launch into known icing conditions• Rotor start in 55kts Winds


Dimensions• Main rotor diameter (blade tip circle) 56’ 4” 17.17 m• Tail rotor diameter (blade tip circle) 11’ 0” 3.35 m• Fuselage length 56’ 2” 17.10 m• Fuselage width 12’ 9” 3.89 m• Fuselage height (to top of tail pylon) 14’ 2” 4.32 m• Length over-all (including rotors) 68’ 6” 20.88 m• Height over-all 17’11” 5.47 m• Passenger cabin width 6’ 7” 2.01 m• Passenger cabin height 6’ 0” 1.83 m

S-92® DIMENSIONS


S-92® INOVATIONSImproving Safety and Capabilities

Meets FAR Part 29, No Exceptions Flaw Tolerant Design 4 AXIS AFCS with RIG APPROACH™ Certified Ditching in Sea State 6 conditions Certified Main Rotor Start in 55kt windCertified Launch Into Known Icing ConditionsFleet Wide HUMS Data Monitoring and AnalyticsReal Time Bearing Monitor Dynamic Component Life Extension

Meets FAR Part 29, No Exceptions Flaw Tolerant Design 4 AXIS AFCS with RIG APPROACH™ Certified Ditching in Sea State 6 conditions Certified Main Rotor Start in 55kt windCertified Launch Into Known Icing ConditionsFleet Wide HUMS Data Monitoring and AnalyticsReal Time Bearing Monitor Dynamic Component Life Extension

2002 Collier Award"the greatest achievement in aeronautics or astronautics in America."


MODERN INTEGRATED PILOT WORKSTATION

Enhanced safety through intuitive design minimizes workload

Large Field Of View And Intuitive DisplaysFully Integrated To Enhance Situation AwarenessNVG Compatible


FULLY INTEGRATION DISPLAYSEnhanced Situational Awareness

16EAR99-NLR This Page Contains No Technical Data Controlled by the ITAR or EAR

NAV Page

Primary Flight Display Page


ADVANCED AFCS

17EAR99-NLR This Page Contains No Technical Data Controlled by the ITAR or EAR

• Fully Coupled Flight Director with SAR Modes• Approach to hover• Mark on target• Auto climb out


DESIGNED FOR EXTREME ENVIRONMENTS

Sea State 6 Flotation and Life Rafts

Main Engine Inlet Particle Separator

Inlet Barrier Filter

Operation To -40C

Launch into Know Icing Conditions

Main Rotor Start in 55Kt wind


Tail Rotor Gearbox Sight

Glass

APU/ECU Compartment Access Doors

Intermediate Gearbox Sight Glass

Fire Extinguishing Access Door

Work Platform

Step

Handhold

Fuel Cell Access Cover

Handhold Fairing Access Door

Oil Cooler Compartment

Work Platforms

Single Point Engine Wash

(option)Gravity Fuel (Both Sides)

Flush Steps

External Power

Forward Avionics Compartment

Sliding Fairing

Engine Wash(Both Sides)

Hinged Cover

MAINTAINABILITY BY DESIGNRapid Maintenance Access and Inspection

Integrated Ladders, Walk Ways And Work Platforms


S92

EC225

AW101AS332L2

*2013 Data (Scheduled and Unscheduled Maint.)

MAINTAINABILITYBest in Class MMH/FH


S-92® CABIN Best in Class Passenger and Baggage Volume

Top View

Side View


Fold-up inboard facing utility seats

SAR technician operator’s console

Full-height sliding doorwith bubble

window

Triple Litter Kit

SAR Interior

SAR CargoContainer Dual Internal Aux Fuel

Tanks (420 gallons total)FLIR

Search Light

Dual Rescue Hoist

Loudhailer

SAR AFCS

Rescue Hoist Operator Seat

S-92® HELICOPTER Options to Enhance SAR Mission Capability


S-92® Helicopter 10 Passenger and Two Crew Seats


S-92® Helicopter 18-Passenger Seats and one Crew Seat


S-92® HELICOPTER Search and Rescue

Six passengers, two crew, internal aux tanks and triple litter kit


S-92® HELICOPTER Medical Evacuation

Five passenger seats, two crew seats and two three-patient litter kits


S-92® HELICOPTER Cargo layout*

*The attendant seat is not FAA certified.


S-92® CABIN Large Sliding Main Door

50 inch Sliding Door • Stand Up Height• Bubble window (option)

Single or Dual 600Lb Capacity Hoists• Hoist Light• Fuselage Mounted SAR scene lights

Hover Trim Controller


S-92® CABIN Best in Class Volume and Comfort

Best in Class Cabin Space• Stand up height • Rapid Re-configuration

High Comfort Environmental Control • High capacity air conditioning • Dual zone separately controllable heat/vent/AC

APU allows cooling or heating aircraft prior to boarding passengers

Smooth Ride• Main rotor Bifilar vibration absorber• Active vibration control (AVC)

Quiet Cabin• Normal conversation without headsets• 92.0 dBA, 81.5 dBSIL4


MULTIUSE CABIN

Full Cabin Width Ramp Door Facilitates Rapid Loading/Unloading Operations


ADVANCED MISSION SYSTEMSSurveillance

Electro Optical

Multi-Mode Surveillance RADAR

GMTI ISAR

Precision stabilized gimbalIR with high magnification Color Daylight Camera with Zoom LensCMCCD Night Spotter for ID in low-light conditionsCabin Hand ControllerIntegrated functionality of the Nightsun XP searchlight

High Res SAR

Images are for illustrative purposes and do not reflect actual performance


S-92® HELICOPTER




Crew Improvements- Reduced Pilot Workload- Improved Ergonomics- OEI Training- HUMS- Weather Radar

CFIT Improvements- Cockpit Visibility - EGPWS- TCAS- ADSB Out

Maintenance Improvements- Designed for Easy Maintenance - Designed for Easy Visual Inspections- Tolerant to In-Service Damage (Flaws)- Long Inspection Intervals (1,500 hrs)- Reduced Parts Count- HUMS

Material Improvements- Flaw Tolerance- Lessons Learned from 9

Million Flt Hrs (H-60/H-53) - Corrosion Protection- Fatigue-Based Drivetrain- Bearing Monitor- Redundant Airframe Struct.- Redundant Systems- HUMS

Other Improvements- Bird Strike Protection- Lightning Protection- HIRF Protection- Turbine/Fan Burst Protection- Icing Protection

OtherFailure

10%Maint Error10%

MaterialFailure

13% Crew Error,Including CFIT

67%

DESIGNED TO LOWER ACCIDENT OCCURRENCE


ENHANCED PILOT SITUATION AWARENESS

Weather and Ground Map RADAR(Optional XM WX Aviation Weather)Weather and Ground Map RADAR(Optional XM WX Aviation Weather)

Enhanced Ground Proximity Warnings Enhanced Ground Proximity Warnings

TCAS II Display and Warnings TCAS II Display and Warnings

Four Axis AFCS with Rig Approach™Minimizes Pilot WorkloadFour Axis AFCS with Rig Approach™Minimizes Pilot Workload


DESIGNED FOR IMPROVED SURVIVABILITYCertified Protection To The Latest FAA Standards

Lightning Strike

Turbine Burst

High Intensity Radiated Fields

Bird Strike

Crash Loads


DESIGNED FOR IMPROVED SURVIVABILITYS-92 meets latest version of CFR 29.561 for Crash Loads

Amendment 24 crash loadsS92 Crash Loads


S-92 ® Helicopter landing gar absorbs crash energy while the shock absorbing seats and restraints protects crew and cabin Occupants

CREW AND PASSENGER SAFETY

Side Mounted Cabin Utility Seat

Energy Absorbing Crashworthy Seats

Energy Absorbing Landing Gear

Crashworthy Main Fuel Sponsons Isolated from crew and passengersSelf sealing breakaway valvesSuction fuel feed


EMERGENCY EGRESSExceeds FAA/JAA Requirements

Emergency Exit Lighting Large Push Out Windows Sponson Walk Area


OVER-WATER SAFETY EQUIPMENTSea State 6 Enhanced Emergency Flotation System

Deploys Automatically Or Manually

Safe Guarded Against Spontaneous/Inadvertent Deployment

Sea State 6 Demonstrated


EMERGENCY LIFE RAFT SYSTEM

• Externally mounted in forward sponson• Left and right hand (total 2)• 14 person capacity with 50% overload capability• Electrical and mechanical deployment

41This page contains no technical data subject to the EAR or the ITARSikorsky Aircraf t Corporation Proprietary 41

Full scale fatigue testing of intentionally flawed components

confirm strength and life

Composites are tested with built-in voids and

hammer blows

Clearly detectable damage 0.040” deep

gouge

Barely detectable flaw 0.005” deep

gouge

S-92 design prevents mishaps caused by small corrosion pits, dents and damage due to field use!

Critical Structures Absorb Flaws, Damage and Corrosion

FLAW AND DAMAGE TOLERANT


UNSURPASSED CREDENTIALS

S-92

Designed to newer FAA regulations, without exception

FAA certified, flaw-tolerant design throughout

Meets FAA lubrication failure regulation, without exception

Exceeds FAA requirements for crashworthiness

Fuel system meets latest FAA requirements

Lowest accident rate in class*

Highest fleet hours in class*

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*from publically available data cited earlier


S-92® HELICOPTER




Tail Rotor Gearbox Sight

Glass

APU/ECU Compartment Access Doors

Intermediate Gearbox Sight Glass

Fire Extinguishing Access Door

Work Platform

Step

Handhold

Fuel Cell Access Cover

Handhold Fairing Access Door

Oil Cooler Compartment

Work Platforms

Single Point Engine Wash

(option)Gravity Fuel (Both Sides)

Flush Steps

External Power

Forward Avionics Compartment

Sliding Fairing

Engine Wash(Both Sides)

Hinged Cover

MAINTAINABILITY BY DESIGNRapid Maintenance Access and Inspection

Integrated Ladders, Walk Ways And Work Platforms


ANALYTICS AND TECHNOLOGYUsing HUMS data to reduce cost and increase availability

Converting Unscheduled Maintenance to Scheduled Maintenance

Usage Based Component Lives

5

1 0

1 5

2 0

2 5

3 0

2/1 2 /0 8 2/2 2 /0 8 3/3 /0 8 3 /1 3 /0 8 3 /2 3 /0 8 4 /2 /0 8 4 /1 2 /0 8 4 /2 2 /0 8

2400 hour life extension

Post Flight HUMS Data Transfer

Post Flight Processing Data

Part Stock Aligned to Aircraft Usage


HUMS data and component log cards are used to provide usage data

Up to 2400 hour life extension beyond 4900 hour retirement time dependent upon usage

Sikorsky Aircraft is the first to ever fully satisfy the FAA’s criteria & obtain approval for a methodology that extends the life of a component through individual aircraft usage data

MAIN ROTOR HUB LIFE EXTENSION


COMPREHENSIVE SUPPORT

Pilot TrainingMaintenance TrainingAircraft DeliverySparesOverhaul & RepairAircraft ModificationOn Site SupportDepot ManagementAlerts and BulletinsAerospace Engineering24 Hour Hotline

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S-92 SAR Standard Presentation - Aircraft Sales & Leasing

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