Post on 25-Oct-2021
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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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EXPORT WARNING
These commodities, technical data or software are subject to the export control of either the International Traffic in Arms Regulations (ITAR) or the Export Administration Regulations (EAR) and cannot be exported without the authorization of
either the Department of State or the Department of Commerce prior to export. Export includes disclosure and or access to commodities, technical data or software by foreign nationals whether located in the United States or abroad. This requirement applies equally to foreign national employees of U.S. companies and their foreign subsidiaries. These
commodities, technology or software were exported from the United States in accordance with the Export Administration Regulations. Diversion contrary to U.S. law is prohibited.
Disclosure to citizens or entities of Cuba, Iran, North Korea, Sudan or Syria is prohibited by U.S. regulations.
WARNING
This document, or an embodiment of it in any media, discloses information which is proprietary, is the property of Sikorsky Aircraft Corporation, is an unpublished work protected under applicable copyright laws, and is delivered on the express
condition that it is not to be used, disclosed, reproduced in whole or in part, (including reproduction as a derivative work), or used for manufacture for anyone other than Sikorsky Aircraft Corporation without its written consent, and that no right is granted to disclose, or so use any information contained therein. All rights reserved. Any act in violation of applicable law
may result in civil and criminal penalties.
The proposed implementation of any planned or projected improvements is subject to change and should not be relied upon as a statement of present, or actual future capabilities.
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S-92® HELICOPTER
Overview FeaturesSafetyMaintenance and Support
Overview FeaturesSafetyMaintenance and Support
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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
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SAFE, RELIABLE MULTI-MISSION SOLUTION
Off Shore
Search And RescueVIP/HOS Transport
Utility
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S-92® HELICOPTER209 In-service Aircraft
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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
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S-92® FLEET HIGH TIME AIRCRAFT
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EXCEPTIONAL RELIABILITY
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More On Time Departures More Aircraft Revenue Opportunity
93% Fleet Wide Unscheduled Availability
* Estimated
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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
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S-92® HELICOPTER
Overview FeaturesSafety and SurvivabilityMaintenance and Support
Overview FeaturesSafety and SurvivabilityMaintenance and Support
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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
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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
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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."
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MODERN INTEGRATED PILOT WORKSTATION
Enhanced safety through intuitive design minimizes workload
Large Field Of View And Intuitive DisplaysFully Integrated To Enhance Situation AwarenessNVG Compatible
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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
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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
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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
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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
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S92
EC225
AW101AS332L2
*2013 Data (Scheduled and Unscheduled Maint.)
MAINTAINABILITYBest in Class MMH/FH
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S-92® CABIN Best in Class Passenger and Baggage Volume
Top View
Side View
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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
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S-92® Helicopter 10 Passenger and Two Crew Seats
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S-92® Helicopter 18-Passenger Seats and one Crew Seat
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S-92® HELICOPTER Search and Rescue
Six passengers, two crew, internal aux tanks and triple litter kit
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S-92® HELICOPTER Medical Evacuation
Five passenger seats, two crew seats and two three-patient litter kits
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S-92® HELICOPTER Cargo layout*
*The attendant seat is not FAA certified.
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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
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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
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MULTIUSE CABIN
Full Cabin Width Ramp Door Facilitates Rapid Loading/Unloading Operations
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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
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S-92® HELICOPTER
Overview FeaturesSafetyMaintenance and Support
Overview FeaturesSafetyMaintenance and Support
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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
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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
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DESIGNED FOR IMPROVED SURVIVABILITYCertified Protection To The Latest FAA Standards
Lightning Strike
Turbine Burst
High Intensity Radiated Fields
Bird Strike
Crash Loads
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DESIGNED FOR IMPROVED SURVIVABILITYS-92 meets latest version of CFR 29.561 for Crash Loads
Amendment 24 crash loadsS92 Crash Loads
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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
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EMERGENCY EGRESSExceeds FAA/JAA Requirements
Emergency Exit Lighting Large Push Out Windows Sponson Walk Area
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OVER-WATER SAFETY EQUIPMENTSea State 6 Enhanced Emergency Flotation System
Deploys Automatically Or Manually
Safe Guarded Against Spontaneous/Inadvertent Deployment
Sea State 6 Demonstrated
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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
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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
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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
43This page contains no technical data subject to the EAR or the ITARSikorsky Aircraf t Corporation Proprietary
S-92® HELICOPTER
Overview FeaturesSafety and SurvivabilityMaintenance and Support
Overview FeaturesSafety and SurvivabilityMaintenance and Support
44This page contains no technical data subject to the EAR or the ITARSikorsky Aircraf t Corporation Proprietary
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
45This page contains no technical data subject to the EAR or the ITARSikorsky Aircraf t Corporation Proprietary
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
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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
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COMPREHENSIVE SUPPORT
Pilot TrainingMaintenance TrainingAircraft DeliverySparesOverhaul & RepairAircraft ModificationOn Site SupportDepot ManagementAlerts and BulletinsAerospace Engineering24 Hour Hotline