Sikorsky S-76B - VIP Configuration Date Of Manufacture – 1989 Total Time – 4820.38 Hours

Year of Manufacture:	1989
Total Time Airframe:	4820.38 (as of 7.12.05)
Landings Since New	12,922 (as of 7.12.05)
Maximum Gross Weight:	11,700 lbs
Equipped EmptyWeight:	8,801 lbs (3992 kgs) AT STA 206.14
Last weighed	10 April 2002
Pratt & Whitney PT6B-36B Turboshaft Engines	#1 Engine Serial No: PCE 36208 TTE (1) : 2,137.25 hrs (TSN) TSO (1): = TSN
	#2 Engine Serial No: PCE PT0008 TTE (1): 1,907.49 hrs (TSN) TSO (1): = TSN

Exterior

All over matterhorn white with red and orange accent lines

Airframe and Systems
Hinged cockpit and cabin doors Key locks for cockpit, cabin, and baggage compartment doors Hinged fuel filler caps with key locks Cockpit-controlled electric door locks for cabin doors Left and right retractable cabin boarding steps (Synergetics Quick-Step) Ram-air ventilation system (NACA door scoops) Standard bleed-air cabin heating system with split cabin ceiling ducting Heated foot pads for pilot and copilot (Watlow) Freon air conditioning system (Keith) with R-134a refrigerant and compressor upgrade		Heated glass windshields Windshield wiper and washer system Vent window in pilot’s door Manual rotor brake system High-visibility main rotor blade paint Bonding jumpers for main and tail rotor heads Provisions for main and tail rotor tracker/balancer (Chadwick-Helmuth) DC electrical system with two 200A starter/generators and two nose-mounted 22-ampere-hour batteries AC electrical system with 10 KVA generator and dual static inverters		Nose-mounted controllable searchlight Fixed landing lights on left and right main gear struts Pulselite System 3-position strobe light system (Whelen) H.I.S.L. (High Intensity Strobe Light) on vertical stabilizer Rotor disc recognition light on forward upper fairing Gearbox sight gauge lights Landing gear emergency blow-down bottle pressure gauge in right nose window

Interior
Cockpit crew seats with beige leather upholstery and sheepskin inserts Black grospoint fabric on center console sides and collective sticks Gray instrument panel; black console, switch panels, and gauge faces Black suede leather glareshield covering Cockpit door-mounted map cases (2 per door) and additional storage behind crew seats Two cockpit map lights and overhead spot lights Cabin sidewalls and ceiling covered with light beige Ultrasuede Four-place forward-facing executive divan with fold-down armrests and writing surface Life vest storage compartments behind rear divan outboard seat backs		Three-place aft-facing executive divan with Refreshment cabinet between seats 2 and 3 Tan leather upholstery on cabin seats, sidewall armrests, and interior details Beige carpeting in cockpit, cabin, and lower sidewall panels Matching carpet runner for cabin Mirror on rear cabin bulkhead above divan with No Smoking/Fasten Seat Belt lights Glossy tan wood veneer on cabinetry and interior woodwork Colour coordinated cabin seat belts with 90° latches in polished chrome Full-length cabin armrests with door pulls, cup holders, and speakers		Magazine storage racks on left and right cabin doors Storage enclosure on forward right cabin window frame Bose-X headset panels at each cabin seat position Two hot-liquid containers with drip-tray in upper credenza Ice, condiment, and refreshment storage drawers in credenza Auxiliary heater for cabin and cockpit Baggage compartment floor protector with stainless steel sill plates Baggage compartment painted gloss white with beige pouches for landing gear pins

Avionics & Electrical Systems
Dual Digital Automatic Flight Control System (Honeywell SPZ-7000 DFCS) Electronic Flight Instrument System (Honeywell 5”x 5” EDZ-705, 4-tube EFIS) Single-pilot IFR capable Dual lighted approach plate holders Dual overhead master switch panels Radio Master Switches Dual C-14A compass system (Honeywell)		Dual IDC encoding altimeters with counter-drum-pointer display, millibar / in.hg. Readout, and altitude alert light Radio altimeter with digital readout on EADI’s and expanded-scale indicator (Honeywell AA-300) Standby vertical-card magnetic compass (Hamilton HI-400-28)		Standby self-contained attitude indicator (J.E.T. AI-904) with emergency power supply (J.E.T. PS 835) Standby ADI for single-pilot IFR backup Dual digital clocks (Davtron M-877) Fuel flow indicators and totalizer (Foxboro)

Avionics – Communications / Navigation Equipment
Dual Honeywell Primus II Comm/Nav system with digital cockpit audio Cockpit ICS foot switches Dual VHF communications radios (Honeywell Primus II) Third communications radio for clearance delivery and backup		Dual VOR navigation radios (Honeywell Primus II) Dual DME (Honeywell Primus II) ADF (Honeywell Primus II) Dual Transponders (Honeywell Primus II)		TCAS I system (Bendix/King CAS-66A) with dedicated display and radar interface Flight Management System (Universal UNS-1) Weather radar (Honeywell Primus) GPS Navigator (Garmin)

Emergency Equipment

Emergency flotation system and Cockpit Voice Recorder with float switch

Inspection Programme
Type of Program: S-76 Equalized Inspection Programme Last 12-Month Inspection: April 15, 2005 (4,608:18 Hrs.) Last 3-Year Hub/Swashplate Inspection: April 15, 2005 (4,608:18 Hrs.)		The aircraft is maintained using Sikorsky’s Equalized Inspection Programme for S-76B helicopters. A computerised system for maintenance tracking and reporting is maintained by PremiAir Aircraft Engineering. Engines are not enrolled in either the Pratt & Whitney Eagle Service Plan or the J.S.S.I. Program The Main, Intermediate, and Tail Rotor Gearboxes have been continuously enrolled in Sikorsky’s Powertrain Assurance Program (PAP)

Damage History
There is no record of, nor any evidence of: Hard Landings		Fire / Smoke damage Water / Hail / Wind damage Lightning Strikes		Accident / Incidents Water Landing / Immersion Sudden Rotor Stoppage

Aircraft subject to prior sale or withdrawal from the market. Specification subject to verification upon inspection of the aircraft.