Aircraft for sale

1996 Sikorsky S76b · # 760441

Airframe:

5,100 Hours Total; 13,500 Landings
Entry to Service – 8/19/1996
Maintenance Tracking by CAMP

Description
Engine Serial Number
Engine Time Since New
Engine Time Since Overhaul
Engine Cycles Since New
Engine Cycles Since Overhaul
Engine TBO
Pratt & Whitney PT6-36B
36224
4,788
1,100
10,204
3,500
4,000 hours
Pratt & Whitney PT6-36B
36225
4,950
1,250
11,700
3,630
4,000 hours

Gear Boxes:

Description
Main (Quiet Mod)
Intermediate
Tail Rotor
Reduction Gearbox
Main Rotor Blade Spindles
TSO
1,125
491
3,724
1,303
100
TBO
3,250
4,500
4,000
3,500
5,000
Time Remaining
2,125
4,009
276
2,197
4,900

Avionics:

The Sikorsky S76b is equipped with an integrated Honeywell Primus II avionics suite. A general summary of this aircraft’s Honeywell avionics suite is as follows:

  • Honeywell Dual Digital SPZ7000 AFCS
  • Honeywell EDS-756 4 Tube EFIS System
  • Honeywell Primus II Radio System
  • Honeywell Primus 700 Weather Radar
  • Honeywell MK XXII EGPWS
  • Honeywell TCAS I CAS 66A
  • Honeywell LP-850 Lightning Sensor
  • Honeywell Datanav III with Checklist
  • Heads Up Technologies XM Graphical Weather
  • Dual Litef AHRS C.S.N. 76-201
  • Clearance Delivery Radio
  • Universal UNS-1D+ WAAS and LPV Capable
  • Garmin GPS 400
  • Dual IVSI’s
  • Penny & Giles DADC
  • Cockpit Voice Recorder – CVR-30A
  • Global Wulfsburg Flitephone
  • Dual Davtron M877 Digital Clocks
  • Artex ELT C406-N HM Emergency Locator Transmitter
  • ARGUS 7000 Moving Map Navigation Display
  • Digital OAT Gauge/5 Function Display

 

Additional Highlights:

 

  • Keith Products Vapor Cycle Air Conditioning
  • C.S.N. 76-207B Vert Stab LE Replacement and Inspection Port Installation
  • Dual Retractable Boarding Steps Controlled by WOW switch
  • Automatic Cabin Temperature System
  • Pulse Light Landing Lights
  • Dual 22 AMP/Hr NiCad Batteries
  • Dual Controls
  • Electric Passenger Door Locks
  • Door Lock Indication System
  • Fixed Landing Lights Main Landing Gear
  • Main Rotor and Tail Rotor Blade Tracking Provisions
  • Emergency Flotation Systems
  • Rotor Disc Lights
  • Whelan 3-Position Strobe Light System
  • Heated Windscreens
  • Dual Anti Collision Lights
  • 2 Gooseneck Lights
  • Illuminated Chart Holder
  • Selectable Alternate Static Source
  • Controllable Grimes Search Light
  • Cabin Door Lock Controlled Lighting
  • Dual Inverter System
  • High Visibility Main Rotor Blades
  • Dual Cockpit Doors Vent Windows
  • Quiet Gearbox Mod

 

Exterior:

Matterhorn White with Medium Gray and Toreador Red accent stripes

Interior:

3-Place Aft-Facing Executive Divan opposite 4-Place Fwd-Facing Divan, Two Hot Liquid Containers, Ice Drawer and Life Vest Storage, Brushed Black Plating on all bright surfaces, Executive Credenza. Pilot and Co-Pilot’s Sheepskin Upholstery for Cockpit Seats. Cockpit JEPPs and Flight Manual Storage, Light brown patterned Wool Carpet, All seats covered in Black leather. Woodwork is medium Cherry.

Inspections:

Description
36 Month / 1250 hr Inspection
12 Month / 1500 hr Inspection
500 hr Tail Rotor Inspection
900 hr Main Blade Inspection
24 Month FAR Checks
Complied With
April 8th, 2010
Sept 21st, 2010
5,000
5,000
August 31st, 2011
Next Due Date
April 8th, 2013
Sept 21st, 2012
N/A
N/A
August 31st, 2013
Next Due Hours
5,814
6,166
5,500
5,900
N/A

Weights:

  • Empty Weight – 8,852 lb
  • Fuel Capacity – 1,870 lbs
  • Maximum Gross Weight – 11,700 lb

Maintenance tracking provided by CAMP and available upon request