S92-063_TI_Oil

Sikorsky S‑92 HelicopterOffshore Oil Configuration

S ‑ 9 2® T e c H n i c a l i n f o r m a T i o n

1S-92 Offshore Oil Technical Information

S92-063 3152 June 2010

Performance (estimated)

Sea level, standard day, maximum gross weight unless otherwise noted

Gross weight 26,500 lb 12,018 kg

Vne 165 kts 306 kph

Maximum cruise speed 147 kts 272 kph

Long range cruise speed * 137 ktas 254 kph

Range

- No reserve * 542 nm 1,005 km

- 30-minute reserve * 472 nm 874 km

- Average cruise speed* 135 ktas 250 kph

- Average fuel, flow* 1,270 pph 576 kph

Endurance, no reserve 4 42 hr

Hover out of ground effect 6,700 ft 2,042 m

Hover in ground effect 8,200 ft 2,499 m

Operational ceiling 15,000 ft 4,572 m

OEI service ceiling 5,500 ft 1,676 m

* Long Range Cruise speed @ 4,000 ft, ISA

fuel System

Normal 760 gal 2,877 l

Auxiliary 2 x 210 gal 2 x 795 l

Dimension

Main rotor diameter 56 33 ft 17 17 m

Tail rotor diameter 11 00 ft 3 35 m

Overall length 68 50 ft 20 88 m

Weights

Maximum gross weight, internal payload 26,500 lb 12,018 kg

Empty weight, utility configuration 15,824 lb 7,176 kg

Useful load, utility configuration 10,676 lb 4,842 kg

Maximum gross weight, external load 28,300 lb 12,834 kg

Maximum cargo hook load 8,000 lb 3,628 kg

Engines

Manufacturer/Type General Electric CT7-8AMaximum OEI power, 30-sec 2,740 shp 2,043 kw

Intermediate OEI power, 2-minute 2,523 shp 1,881 kw

Continuous OEI power 2,498 shp 1,864 kw

Takeoff power, 5 minutes 2,520 shp 1,879 kw

AEO, 30-minute power 2,336 shp 1,742 kw

Maximum continuous / cruise power 2,043 shp 1,524 kw

Specifications


S92-063 3152 June 2010

19-seat configuration at 32" pitch

cabin Dimensions

cabin Dimensions

Passenger cabin length 20 00 ft 6 10 mPassenger cabin width 6 58 ft 2 01 mPassenger cabin height 6 00 ft 1 83 mPassenger cabin area 128 sq ft 11 89 sq mPassenger cabin volume 700 cu ft 19 82 cu mBaggage compartment volume 140 cu ft 3 96 cu m

aircraft Dimensions


S92-063 3152 June 2010

• Superior ergonomics and pilot visibility

• Four Rockwell Collins 6” x 8” portrait-oriented multi-function displays

• Optional additional center-line-mounted multi-function display

• Universal Navigation UNS-1Esp Flight Management System (FMS) with imbedded GPS and MMMS

• Dual Collins RTU-4200 Radio Tuning Units (RTU’s)

• Dual Collins VHF-422D VHF/AM transceivers

• Dual Collins VIR-432 VOR/ILS/MKR receivers

• Collins TDR94D Mode S transponder (RTU control)

• Collins ADF 462 automatic direction finder

• Collins DME-442 distance measuring equipment

• dB Systems Model 380-014 intercom system

• Enhanced Ground Proximity Warning System (EGPWS)

• Three frequency Emergency Locator Transmitter (ELT) with COSPAS/SARSAT (Artex C-406-NHM) with GPS broadcast

• Honeywell KTA-970, Traffic advisory and Collision Avoidance System (TCAS 1)

cockpit instrument Display Panel


S92-063 3152 June 2010

airframe

• Nose electronics bay with hinged door

• Pilot and copilot heated glass windshields

• Dual windshield wiper and washers systems

• Pilot and copilot cup holders

• Pilot and copilot crashworthy seats with 5-point restrains

• Two jettisonable cockpit side windows

• 200-psf cabin floor with provisions for right side attendant’s seat

• Two-zone bleed air heating and ventilation system

• Air-conditioning system

• Right side clamshell cabin door (hinged upper, air stair lower)

• Three Type III Emergency exits

• Ten, double-pane jettisonable cabin windows

• Full retractable, energy-absorbing tricycle landing gear with emergency blow down capability

• Six exterior tiedown fittings

• Bleed air heating and defogging

• Provisions for Rotor Ice protection System (RIPS)

• Active vibration control system with three force generators and provisions for additional force generators

• External fuel sponsons with provisions for life rafts in the leading edge

• Hydraulically actuated cargo ramp

• Basic interior paint preparation and finish

• Exterior cover for the cargo hook bay

Propulsion

• Two General electric CT7-8A turboshaft engines with integral particle separators and pneumatic starters

• Engine inlet de-ice system

• Honeywell 36-150, 90-hp auxiliary power unit

• 760 gallons of fuel in crashworthy fuel cells located in external sponsons with self-sealing breakaway valves

• Single point pressure refueling or defueling

• Dual point gravity refueling

• Low level fuel warning system

• Engine and APU fire detection and dual-shot extinguishing systems

• External auxiliary pneumatic receptacle (maintenance use only)

• Engine drain collector system

• Single-point engine water wash system

• Main transmission Quick Change Unit with dual input accessory modules, chip detectors with fuzz burn off and oil cooler bypass valve

• Rotor brake

• Tail drive shaft system with diaphragm-type couplings

• Intermediate and tail gearboxes

rotor systems and controls

• Four-blade articulated main rotor system with elastomeric bearings, damage tolerant design and manual blade fold provisions

• Pitch change links equipped with elastomeric main and tail rod end bearings

• Composite main rotor blades with swept anhedral tips and de-ice capability

• Hub-mounted bifilar vibration attenuating system

• Four-blade flexbeam tail rotor with de-ice capability

• Dual redundant main rotor and tail rotor primary servos

• Tail rotor centering quadrant

• Dual, independent 4000-psi hydraulic systems

• Independent backup hydraulic system

Baseline (Green) configuration


S92-063 3152 June 2010

electrical

• 115-volt, 400 Hz, AC electrical power system powered by two 75 KVA oil-cooled generators and a single 35 KVA APU-powered generator

• 28-volt DC power system powered by two 400-amp converters 125 amp backup converter and a 15 AH battery

• Exterior lighting:

- Three position lights

- Upper and lower LED anti-collision lights

- Two fixed landing lights

- Retractable, controllable searchlight

• Pilot and copilot lighted approach plate holders

• Cargo loading light

• AC/DC cabin power receptacles

• Integral cockpit lighting

• Wide area cabin lighting

• Emergency lights

flight controls and instruments

• Dual, redundant pilot’s controls

• Redundant fully-coupled, four-axis Automatic Flight Control System (AFCS) with provisions for SAR capability

• Four Rockwell Collins 6” x 8” portrait-oriented multi-function displays with imbedded maintenance data computer and bearing monitor system

• Two Display Control Panels

• Two data concentrator units

• Dual LITEF Attitude heading Reference Systems (AHRS)

• Dual Goodrich/Rosemount air data computers

• Honeywell AA-300 radio altimeter

• Independent standby instruments: attitude, altitude, airspeed, heading and clock

• Engine Instrument and Caution Advisory System (ICAS)

• Universal Navigation UNS-1Esp Flight Management System (FMS) with imbedded GPS and MMMS

flight controls and instruments

• Honeywell Primus 660 weather avoidance radar with 12-inch antenna

• Dual Collins RTU-4200 Radio Tuning Units (RTU’s)

• Rockwell Collins Proline IV communication and navigation radios:

- Dual Collins VHF-422D VHF/AM transceivers

- Dual Collins VIR-432 VOR/ILS/MKR receivers

- Collins TDR94D Mode S transponder (RTU control)

- Collins ADF 462 automatic direction finder

- Collins DME-442 distance measuring equipment

• NAT Model 380-014 intercom system

• Penny and Giles multi-purpose flight data recorder

• Honeywell Enhanced Ground Proximity Warning System (EGPWS)

• Three-frequency Emergency Locater Transmitter (ELT) with COSPAS/SARSAT (Artex C-406-NHM) with GPS broadcast

• Goodrich Health and Usage Monitoring System (HUMS)

• Cockpit voice recorder/flight data recorder with underwater acoustic beacon

• Honeywell KTA-970, Traffic advisory and Collision Avoidance system (TCAS 1)

Baseline (Green) configuration


S92-063 3152 June 2010

The standard Offshore Oil configuration consists of the Baseline configuration plus the following options:

airframe

• Delete RIPS provisions• Dual life rafts with FAR 135.167 compatible survival packs and COSPAS/SARSAT PLB’s located in the leading edge of each sponson• Emergency flotation system

• Active Vibration system upgraded to six force generators

avionics

• HR Smith 15-503-134 Automatically Deployable ELT (ADELT)

electrical

• Helicopter Emergency Egress Lighting (HEEL) for all cockpit and cabin emergency exits and cabin jettisonable windows

interior

• Heads Up Technologies PBS 250 passenger briefing system• Page PA / chime amplifier• Standard Airline / Offshore interior: - Hard composite sidewall and ceiling panels with an attractive and durable bonded surface treatment - Forward and aft bulkheads - Cabin acoustics package - Illuminated no smoking / fasten seat belt signs - General cabin and emergency lighting - Overhead passenger service unit, including a light and fresh air grasper, for each seat - Four heat registers in the lower cabin sidewalls - Seven cabin speakers - Smoke detector in the baggage compartment• Additional cabin speakers• Night curtain• Cabin floor mat• Baggage compartment shelf• Nineteen passenger seats with four-point restraints on a 32-inch seat pitch

Standard offshore oil configuration: Tropical (faa)


S92-063 3152 June 2010

The standard Offshore Oil configuration consists of the Baseline configuration plus the following options:

airframe

• Dual life rafts with FAR 135.167 compatible survival packs and COSPAS/SARSAT PLB’s located in the leading edge of each sponson• Enhanced emergency flotation system five flotation cells• Active Vibration system upgraded to six force generators

• Provisions for 8,000-lb capacity cargo hook with load cell

avionics

• HR Smith 15-503-134 Automatically Deployable ELT (ADELT)• SkyTrac Systems ISAT-100 Flight Following System with cockpit display and voice capabilty• Additional fifth Multi-Purpose Display located in the center of the instrument panel• Honeywell Primus 701 weatehr avoidance / search radar (replaces standard Primus 660 radar)

• Pressure refueling cutoff switches in the cockpit

• Cabin ECS control

interior

• Helicopter Emergency Egress Lighting (HEEL) for all cockpit and cabin emergency exits and jettisonable windows• Heads Up Technologies PBS 250 pqssenger briefing system• Page PA / chime amplifier• Standard Airline / Offshore Interior: - Hard composite sidewall and ceiling panels with an attractive and durable bonded surface treatement - Forward and aft bulkheads - Cabin acoustics package - Illuminated no smoking / fasten seat belt signs - General cabin and emergency liughting - Overhead passenger service unit, including aa light and fresh air grasper, for each seat - Four heat registers in the lower cabin sidewalls - Seven cabin speakers - Smoke detector in the baggage comp[artment• Additional cabin speakers• Night curtain• Cabin floor mat• Baggage compartment shelf• Nineteen passenger seats with four-point restraints and headrests on the forward facing seats on 32-inch seat pitch• Improved comfort crew seats

Standard offshore oil configuration: north Sea (eaSa)

Performance


S92-063 June 2010

0 100 200 300 400 500 600

range (nautical miles)

20

18

16

14

12

10

8

6

4

2

0

Pas

seng

ers

(220

lb e

ach)

offshore oil configuration ‑ 19 Passengers

Payload/Range Performance - Tropical (FAA)

mission

• ISA + 20° C day

• Takeoff at maximum gross weight (26,500 lb)

• Cruise at 4,000 feet @ Long Range Cruise speed*

• Reserve of 30 minutes at Long Range Cruise speed*

• Average fuel flow: 1,300 pph at 138.5 ktas

* Speed for 99% best specific range

Weights

Empty weight (lb) 17,111Pilots (lb) 400Engine oil (lb) 33Windshield washer fluid (lb) 4Manuals (lb) 10 Operating weight (lb) 17,558

Performance


S92-063 June 2010

0 100 200 300 400 500 600

range (nautical miles)

20

18

16

14

12

10

8

6

4

2

0

Pas

seng

ers

(240

lb e

ach)

offshore oil configuration ‑ 19 Passengers

Payload/Range Performance - North Sea (EASA)

mission

• Standard day

• Takeoff at maximum gross weight (26,500 lb)

• Cruise at 4,000 feet @ Long Range Cruise speed*

• Reserve: 10% cruise + 30 minutes loiter

• Average fuel flow: 1,100 pph at 150 ktas

*Speed for 99% best specific range

WeightsEmpty weight (lb) 17,524Pilots (lb) 400Engine oil (lb) 33Windshield washer fluid (lb) 4Manuals (lb) 10 Operating weight (lb) 17,971

Performance


S92-063 June 2010

Updated 15 March 2010

0

2000

4000

6000

8000

10000

12000

14000

16000

16000 18000 20000 22000 24000 26000 28000

PR. A

LTIT

UD

E, F

T

GROSS WEIGHT, LB

S-92A HOVER CEILING OUT OF GROUND-EFFECT DUAL ENGINE TAKEOFF POWER

CLEAN AIRFRAME 105% NR

Civil GW Limit 26500 lbs

ISA

ISA+10 C

ISA+20 C

ISA+30 C

0 C 10 C 20 C 30 C 40 C 45 C

Updated 15 March 2010

0

2000

4000

6000

8000

10000

12000

14000

16000

14000 16000 18000 20000 22000 24000 26000 28000

PR. A

LTIT

UD

E, F

T

GROSS WEIGHT, LB

S-92A HOVER CEILING IN GROUND-EFFECT DUAL ENGINE TAKEOFF POWER

CLEAN AIRFRAME 105% NR

ISA

ISA+10 C

ISA+20 C

ISA+30 C

0 C 10 C 20 C 30 C 40 C 45 C

Civil GW Limit 26500 lbs

Performance


S92-063 June 2010

6/17/2010 S-92A Standard Aircraft Configurations 12:13 PM

CAT A Stay-Up CapabilityS-92A Clean Airframe Standard Charts 5-20-10

7500 8000 8500 9000 9500 10000 10500 11000 11500 12000 12500 13000 13500

0

500

1000

1500

2000

2500

3000

3500

4000

4500

0

2000

4000

6000

8000

10000

12000

14000

16000

16000 18000 20000 22000 24000 26000 28000 30000

Pres

sure

Alti

tude

(m)

Gross Weight (kg)

Pres

sure

Alti

tude

(ft)

Gross Weight (lb)

S-92A Standard Config: Cat "A" Stay-Up Capability OEI Continuous Rating ROC = 150fpm VBROC 1,000ft AGL

Max Civil GW 26,500 lb

(12,020 kg)

50 C

<-20 C

30 C

40 C

20 C

10 C 0 C

-10 C ISA

ISA+30

4170shp Transmission

ISA+20

6/21/2010 S-92A Standard Aircraft Configurations 8:40 AM

OEI Service CeilingS-92A Clean Airframe Standard Charts 5-20-10

7500 8000 8500 9000 9500 10000 10500 11000 11500 12000 12500 13000 13500

0

500

1000

1500

2000

2500

3000

3500

4000

4500

0

2000

4000

6000

8000

10000

12000

14000

16000

16000 18000 20000 22000 24000 26000 28000 30000

Pres

sure

Alti

tude

(m)

Gross Weight (kg)

Pres

sure

Alti

tude

(ft)

Gross Weight (lb)

S-92A Standard Config: Single Engine Service Ceiling OEI Continuous Rating ROC=100fpm VBROC


(12,020 kg)

50 C

-20 C

30 C

40 C

20 C

10 C 0 C -10 C

ISA ISA+20

ISA+30

Performance


S92-063 June 2010


CFR 50 ft-minS-92A Clean Airframe Standard Charts 5-20-10

7500 8000 8500 9000 9500 10000 10500 11000 11500 12000 12500 13000 13500

0

500

1000

1500

2000

2500

3000

3500

4000

4500

0

2000

4000

6000

8000

10000

12000

14000

16000

16000 18000 20000 22000 24000 26000 28000 30000

Pres

sure

Alti

tude

(m)

Gross Weight (kg)

Pres

sure

Alti

tude

(ft)

Gross Weight (lb)

S-92A Standard Config: Single Engine Service Ceiling* OEI Continuous Rating ROC=50fpm VBROC


(12,020 kg)

50 C

-20 C

30 C

40 C

20 C

10 C 0 C -10 C

ISA ISA+20

ISA+30

* CFR Part 135.181

Performance


S92-063 June 2010


FF SL ISAS-92A Clean Airframe Standard Charts 5-20-10

400

500

600

700

800

900

1000

1100

1200

800

1000

1200

1400

1600

1800

2000

2200

2400

2600

2800

40 60 80 100 120 140 160 180

Fuel

Flo

w (k

g/hr

)

Fuel

Flo

w (l

b/hr

)

Velocity (KTAS)

S-92A Clean Airframe: Level Flight Fuel Flow Sea Level Standard

Gross Weight - 1000lb

20 22 24

26 28

Best Endurance

Speed

Long Range Cruise Speed

Maximum Cruise Speed

Never Exceed Speed


FF SL ISA+20S-92A Clean Airframe Standard Charts 5-20-10

400

500

600

700

800

900

1000

1100

1200

800

1000

1200

1400

1600

1800

2000

2200

2400

2600

2800

40 60 80 100 120 140 160 180

Fuel

Flo

w (k

g/hr

)

Fuel

Flo

w (l

b/hr

)

Velocity (KTAS)

S-92A Clean Airframe: Level Flight Fuel Flow Sea Level ISA+ 20°C


20 22 24

26

28 Best

Endurance Speed



Never Exceed Speed

Performance


S92-063 June 2010


FF 2K ISA S-92A Clean Airframe Standard Charts 5-20-10

400

500

600

700

800

900

1000

1100

1200

800

1000

1200

1400

1600

1800

2000

2200

2400

2600

2800

40 60 80 100 120 140 160 180

Fuel

Flo

w (k

g/hr

)

Fuel

Flo

w (l

b/hr

)

Velocity (KTAS)

S-92A Clean Airframe: Level Flight Fuel Flow 2,000 ft ISA


20 22 24 26

28 Best

Endurance Speed



Never Exceed Speed


FF 2K ISA+20S-92A Clean Airframe Standard Charts 5-20-10

400

500

600

700

800

900

1000

1100

1200

800

1000

1200

1400

1600

1800

2000

2200

2400

2600

2800

40 60 80 100 120 140 160 180

Fuel

Flo

w (k

g/hr

)

Fuel

Flo

w (l

b/hr

)

Velocity (KTAS)

S-92A Clean Airframe: Level Flight Fuel Flow 2,000 ft ISA+20°C


20 22

24 26

28 Best Endurance

Speed



Never Exceed Speed

Performance


S92-063 June 2010


FF 4K ISAS-92A Clean Airframe Standard Charts 5-20-10

400

500

600

700

800

900

1000

1100

1200

800

1000

1200

1400

1600

1800

2000

2200

2400

2600

2800

40 60 80 100 120 140 160 180

Fuel

Flo

w (k

g/hr

)

Fuel

Flo

w (l

b/hr

)

Velocity (KTAS)



20

22 24

26

28 Best

Endurance Speed



Never Exceed Speed



400

500

600

700

800

900

1000

1100

1200

800

1000

1200

1400

1600

1800

2000

2200

2400

2600

2800

40 60 80 100 120 140 160 180

Fuel

Flo

w (k

g/hr

)

Fuel

Flo

w (l

b/hr

)

Velocity (KTAS)



20

22

24

26

28 Best Endurance

Speed



Performance


S92-063 June 2010



400

500

600

700

800

900

1000

1100

1200

800

1000

1200

1400

1600

1800

2000

2200

2400

2600

2800

40 60 80 100 120 140 160 180

Fuel

Flo

w (k

g/hr

)

Fuel

Flo

w (l

b/hr

)

Velocity (KTAS)



20

22 24

26

28 Best

Endurance Speed





400

500

600

700

800

900

1000

1100

1200

800

1000

1200

1400

1600

1800

2000

2200

2400

2600

2800

40 60 80 100 120 140 160 180

Fuel

Flo

w (k

g/hr

)

Fuel

Flo

w (l

b/hr

)

Velocity (KTAS)



20

22

24

26

28 Best Endurance

Speed



Performance


S92-063 June 2010



400

500

600

700

800

900

1000

1100

1200

800

1000

1200

1400

1600

1800

2000

2200

2400

2600

2800

40 60 80 100 120 140 160 180

Fuel

Flo

w (k

g/hr

)

Fuel

Flo

w (l

b/hr

)

Velocity (KTAS)



20

22

24

26

28 Best Endurance

Speed





400

500

600

700

800

900

1000

1100

1200

800

1000

1200

1400

1600

1800

2000

2200

2400

2600

2800

40 60 80 100 120 140 160 180

Fuel

Flo

w (k

g/hr

)

Fuel

Flo

w (l

b/hr

)

Velocity (KTAS)



20

22

24

26

28 Best Endurance

Speed



Performance


S92-063 June 2010



400

500

600

700

800

900

1000

1100

1200

800

1000

1200

1400

1600

1800

2000

2200

2400

2600

2800

40 60 80 100 120 140 160 180

Fuel

Flo

w (k

g/hr

)

Fuel

Flo

w (l

b/hr

)

Velocity (KTAS)



20

22

24

26

28 Best Endurance

Speed





400

500

600

700

800

900

1000

1100

1200

800

1000

1200

1400

1600

1800

2000

2200

2400

2600

2800

40 60 80 100 120 140 160 180

Fuel

Flo

w (k

g/hr

)

Fuel

Flo

w (l

b/hr

)

Velocity (KTAS)



20

22

24

26

28 Best

Endurance Speed




S92-063 3152 June 2010

notes


S92-063 3152 June 2010

notes

S92-063 3152 2C June 2010

6900 Main Street, Stratford, Connecticut 06615 USA +1 (800) WINGED-S (946-4337) or +1 (203) 386-4282www sikorsky com

Documents

S92-063_TI_Oil