1988 SIKORSKY S-76B
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Location: Wyoming, US
Equipment Specifications
Year 1988
Manufacturer SIKORSKY
Model S-76B
Price Call
Location Texas
Condition Used
General Information
VIP interior and quiet gearbox, Dual Digital Automatic Flight Control System. (Sperry SPZ 7000)
Detailed Description
Airframe:
Total Time. Airframe ( TTAF ): 3562.0 Hrs. as of 10/12/94
Total Time. Airframe ( TTAF ): 6497.8 Hrs. as of 03 July 2009
Empty Weight as Configured: 8549.0 lbs.
Total Landings: 5907 as of 10/12/94
- Hinged cockpit and cabin doors.
- Retractable passenger boarding steps at left and right cabin doors.
- Cockpit-controlled electric cabin door locks.
- Key. locks for cockpit. cabin and baggage compartments doors.
- Miscellaneous cockpit storage containers.
- Executive interior with ultrasuede covering on sidewalls and ceiling and
leather trim.
- Two executive seats with pull-up headrests and drop-down armrests. (These
two seats can be removed and a 4 place aft facing seat installed)
- Four-place forward-facing executive divan with fold-down table.
- Cabin / cockpit divider bulkhead with magazine racks.
- Floor-to-ceiling refreshment credenza with hot liquid containers. ice and
miscellaneous storage.
- Airborne telephone ( Wulfsberg Flitefone VI ) with pilot call bell.
- Therapeutic oxygen bottle ( portable )
- Portable litter kit installation (Keystone STC)
- Quiet Main Gear Box P/N. 76351-09600-045 installed on December 2007
Engine Specs:
#1 Engine TSN./TSO. TSN. 5970.4 Hrs. TSO. 3281.3
#2 Engine TSN./TSO. TSN. 6163.0 Hrs. TSO. 2754.8
- Two Pratt & Whitney Canada PT6B 36A turboshaft engines.
- Engine air particle separator system. ( EAPS )
- Engine fire detection and extinguishing systems.
- Two gravity-filled fuel tanks ( 281 us, gallons total capacity )
- Hinged/Lockable fuel filler caps.
- Dual independent suction fuel systems with crossfeed capability.
- High visibility main rotor blade paint.
- Provisions for main rotor tracker and tail rotor balancer.
- Inspection lights for intermediate and tail gearbox sight gauges.
- Manually actuated rotor brake system.
Avionics/Radios:
Avionics and Instruments :
- Dual Digital Automatic Flight Control System. ( Sperry SPZ 7000 )
- Electronic Flight INSTRUMENT system. ( Sperry EDZ 705 )
- Standby attitude indicator. ( Sfena H321 AFM with J.E.T. battery pack )
- Dual compass system. ( Sperry C 14 A )
- Dual digital electric clocks. ( Davtron 877 )
- Cabin air temperature digital display in cockpit..
- Density altitude / five function indicator. ( Davtron 655 2 )
- Radio altimeter ( Collins ALT 50A ) with dual expanded scale indicators.
- Dual VHF communications radios. ( Collins VHF 22A )
- Dual VOR navigation radios with ILS, Glideslope, and Marker Beacon.
( Collins VIR 32A )
- Dual DME. ( Collins DME 42 )
-Transponder Collins TDR-94D (Mode S) P/N.622-9210-006
- Single ADF. ( Collins ADF 60A with CTL 62 control head )
- Provisions for Microwave Landing System. ( Bendix MLS 21 )
- Navigation Management System ( Universal UNS 1A ) with GPS and LoranC sensor and fuel management )
- Weather radar ( Sperry Primus 500 with EFIS interface )
- Data Nav III ( Sperry ) with checklist function
- Stormscope ( 3M Ryan WX 11J )
- Moving map display ( Argus 5000 )
- Cockpit audio system ( Baker ) with LED annuciators, cockpit ICS
footswitches, and cabin ICS jack
- Cabin paging and chime system ( Baker )
- Cabin audio interphone system with four headsets ( Airman 750 Telex )
- Cockpit voice recorder ( Fairchild / Loral GA100 )
- Moving Terrain installed in Cockpit and 12 Display unit in Cabin by
Wiking Helikopter in Germany on December 2007
- Emergency Locator Transmitter : 406Mhz. Artex C406-1 HM P/N. 455 - 5016
S/N. 170 - 08612 installed by Wiking Helikopter in Istanbul on 16-04-2009
900 item spares and tools kit also available
Additional Equipment:
Systems and Equipment :
- Heated glass windshields.
- Dual windshield wipers and washers.
- Two independent 3000 PSI flight control hydraulic systems with
Quick disconnect fittings for ground hydraulic system connection.
- Retractable tricycle landing gear with self-centering and castering nose
wheel and main wheel brakes.
- Pneumatic emergency landing gear extension system.
- Cabin / cockpit bleed-air heating and ventilation system.
- Heated cockpit foot pads.
- Ram-air ventilation system.
- Freon air conditioning system. ( parker Hannifen )
- Emergency flotation system.
-Auxiliary Fuel Tank provisions installed on Oct. 1995 by
Air Hanson in England (50 gallon tank available)
Electrical systems and Lighting :
- Two 200VA DC starter / generators.
- DC external power receptacle with overvoltage protection.
- Dual 22 ampere-hour batteries. ( nose mounted )
- Dual digital battery temperature indicator. ( foxtronics )
- AC electric system with 10 KVA generator and dual static inverters.
- DC volt / ammeter, AC voltmeter, and AC frequency meter panel. ( Insco )
- Cabin emergency lighting system with battery power supply.
- Nose mounted controllable searchlight.
- 3 position strobe lights.
- Forward facing recognition lights.
- Landing lights on left and right main landing gear.
- Underfuselage high intensity LED strobe.
- Rotor disk recognition light.
- Pulselite system.
1988 SIKORSKY S-76B
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