Vertipedia - Cicaré CH-14

The Cicare CH-14 is the first of a family of helicopters designed for armed forces, security, and civil markets. First flight was in Mar 2007.

Overview

Data on design, manufacture and status

Design authority: Cicaré S.A.

Primary manufacturer: Cicaré S.A.

Parent type: No type defined

Aircraft status: In development

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: 1-2 in Tandem arrangement

Landing gear: Skids

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

Layout and Dimensions

Weights and Performance

Engine Details

Primary Lift Device

Primary Control Device

Overall Dimensions
Overall Height:
Overall Length:	11.61 m	38.1 ft
Overall Width:

Airframe Dimensions
Airframe Length:	9.81 m	32.2 ft
Airframe Width:	1.10 m	3.6 ft
Airframe Height:	3.29 m	10.8 ft

Landing Gear Dimensions
Landing Gear Base:
Landing Gear Track:

Cabin Dimensions
Cabin Internal Height:
Cabin Internal Length:
Cabin Internal Width:

Weights
Max Gross Weight (ground):	1,450 kg	3,197 lb
Max Gross Weight (airborne):	1,828 kg	4,030 lb
Max Take-off Weight:	1,450 kg	3,197 lb
Empty Weight:	750 kg	1,653 lb

Climb Performance
Max Rate of Climb:

Hover Performance
Hover Ceiling IGE:
Hover Ceiling OGE:

Limitations
Max Level Flight Speed:	210 km/h	113 kts
Never Exceed Speed:	240 km/h	130 kts
Service Ceiling:	4,500 m	14,764 ft

Range and Endurance
Max Range:
Max Endurance:

Provided powerplant data is for uninstalled, sea level, static operations.

Powerplant
Number of engines:	1
Designation:	RR M250-C20B turbine
Manufacturer:	Rolls-Royce Corporation

Normal Ratings
Max continuous:	276 kW	370 hp
Take-off / rated:	313 kW	420 hp
Intermediate:
Maximum:

OEI Ratings
OEI contingency:
OEI continuous:
OEI 30-second:
OEI intermediate:

Main Rotor Characteristics
Diameter:	10.00 m	32.81 ft
RPM:
Direction of Rotation:	Unknown
Hub Type:	teetering hinge

Main Rotor Blade Characteristics
Blade Construction:
Blade Chord:
Blade Tip Geometry:
Blade Twist:
Number of Blades:	2

Main Rotor Derived Characteristics
Disc Area:	78.54 m²	845.4 ft²
Disc Loading:	18.46 kg/m²	3.781 lb/ft²
Solidity:

Main Rotor Blade Derived Characteristics
Blade area per blade:
Tip Speed:

Tail Rotor Characteristics
Diameter:	1.49 m	4.89 ft
Configuration:	Unknown
Direction of Rotation:	Unknown
RPM:

Tail Rotor Blade Characteristics
Number of Blades:	2
Blade Construction:
Blade Chord:
Blade Twist:

Tail Rotor Derived Characteristics
Disc Area:	1.74 m²	18.8 ft²
Solidity:

Tail Rotor Blade Derived Characteristics
Tip Speed:
Blade Area (per blade):

References

References and sources used

Cicare CH-14 Aguilucho helicopter(HeliStart)

Peter Goossen
http://www.helistart.com/helicopters/Cicare/CH-14_Aguilucho, January 10, 2017
Website

Helicopter CH-14

Cicare
Cicare product web site, 26 Jul 2015
Website

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Resources related to the CH-14 , provided by public sources across the internet.

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Images

Overview

Attribution

Layout

Attribution

Number of engines:	1 Turbine
Max Level Flight Speed:	210 km/h	113 kts
Max Range:
Max Endurance:

Main Rotor Diameter:	10.00 m	32.81 ft
Max Gross Weight (ground):	1,450 kg	3,197 lb