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APPENDIX 13 SIKORSKY S92 - DESIGN INFORMATION (Aircraft data supplied courtesy of Sikorsky Helicopters - Please note that helidecks designed to facilitate S92 operations should use the higher MAUW to accommodate planned future growth. All other dimensions remain the same)

GENERAL DESIGN DATA

Overall Length (= D) = 20.88 m

Max. All Up Weight (current certified) Max. All Up Weight (planned growth)

= 11859 kg (t = 11.9) = 12837 kg (t = 12.8)

0.83D Obstacle Limit Dimension = 17.33 m

0.62D Obstacle Limit Dimension = 12.95 m

0.12D Inner Obstacle Limitation = 2.51 m @ Height 1044 mm

0.21D Outer Obstacle Limitation = 4.39 m @ Height 1044 to 3236 mm

Minimum Foam Application Rate (where D equals SLA)

= 1883 ltrs per min

RFF Category H1 / H2

Landing Net Size Large, 15m x 15m

Passenger Access Starboard Side at Front

Refuelling Method Pressure and Gravity

Refuelling Point Locations Gravity filling point at each sponson. Pressure connection on port sponson.

Fuel Type Jet A-1

Max. Fuel Load (Standard Tanks) 2877 ltrs (760 US galls)

Undercarriage Tricycle

UNDERCARRIAGE FOOTPRINT - LOADS FOR PLANNED AIRCRAFT GROWTH (Not to Scale)

3.18 m

Mainwheels (at max aft C of G): Static Load per u/c Gear: 4453 kg Static Contact Area per Tyre: 258.0 cm Dynamic Load per u/c Gear: 5788 kg Dynamic Contact Area per tyre: 316.7 cm

6.20 m

Nosewheels (at max fwd C of G): Static Load per u/c Gear: 4592 kg Static Contact Area per Tyre: 265.0 cm Dynamic Load per u/c Gear: 5970kg Dynamic Contact Area per tyre: 323.3 cm

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GENERAL ARRANGEMENT (Courtesy of Sikorsky Aircraft)