威翔航空科技股份有限公司
  • Company
    • Company Profile
    • Company Chronicle
    • Aircraft Design
    • Aircraft Manufacture
    • Corporate Culture
  • Products
    • CTLS Light Sport Aircraft
    • Full-Motion Flight Simulator
    • Static Flight Simulator
    • SVH-4 Helicopter Trainer
  • Aero Club
    • AeroJones Aero Club_Jiangsu
    • AeroJones Aero Club (XiaoHongShu)
  • News
    • News
    • Aviation Knowledge
    • Q/A
  • Customer Service
    • Before-sales Service
    • After-sales Service
    • Flying Training Center
    • Member Login
    • Documents and Media Download
    • Distributors
  • Contact
MENU
( English )
  • 繁體中文
  • 简体中文
  • English
query icon (0)
  Contact
CLOSE
  • Company
    • Company Profile
    • Company Chronicle
    • Aircraft Design
    • Aircraft Manufacture
    • Corporate Culture
  • Products
    • CTLS Light Sport Aircraft
    • Full-Motion Flight Simulator
    • Static Flight Simulator
    • SVH-4 Helicopter Trainer
  • Aero Club
    • AeroJones Aero Club_Jiangsu
    • AeroJones Aero Club (XiaoHongShu)
  • News
    • News
    • Aviation Knowledge
    • Q/A
  • Customer Service
    • Before-sales Service
    • After-sales Service
    • Flying Training Center
    • Member Login
    • Documents and Media Download
    • Distributors
  • Contact
  • ( English )
    • 繁體中文
    • 简体中文
    • English

Inquiry list(0)

CLOSE
Go to inquiry
CLOSE

Login

Captcha
Login Sign up
Forgot password | Resend verification letter
Forgot password
Account
Captcha
Captcha
Confirm submit
Resend verification letter
Account
Captcha
Captcha
Confirm submit

CTLS Light Sport Aircraft

  • Home
  • Products
  • CTLS Light Sport Aircraft 1
  • CTLS Light Sport Aircraft 2
  • CTLS Light Sport Aircraft 3
  • CTLS Light Sport Aircraft 4
  • CTLS Light Sport Aircraft 5
  • CTLS Light Sport Aircraft
  • CTLS Light Sport Aircraft
  • CTLS Light Sport Aircraft
  • CTLS Light Sport Aircraft
  • CTLS Light Sport Aircraft

CTLS Light Sport Aircraft

Add to inquiry box
Production information
The light sport aircraft (AeroJones CTLS, hereinafter referred to as AJCT) is made by AeroJones Aviation and is equipped with a composite fuselage, advanced digital instrument system, international satellite emergency transmitting system, standard rescue parachutes, and two carbon-fiber seats. AJCT was awarded an airworthiness certificate for ultralight aircraft issued by Germany in 1997. In April 2005, it obtained the FAA special aircraft airworthiness certificate for sport aircraft as one of the first manufacturers to obtain the airworthiness certificate. Furthermore, CT aircraft has such features as low cost, easy maintenance, and high safety with ISO9001 quality certification and production certification issued by the Light Aircraft Manufacturers Association (LAMA). CTLS has long had the best sales volume in the global sports aircraft market. In 2010, CTLS achieved the feat of flying 44,000 km around the world and set a stunning record of continuously flying 1800 km with 120 liters of gasoline in 2011, demonstrating its excellent performance and flexibility and completely overturning the Taiwanese people’s impressions of light aircraft. The unsurpassed performance of CTLS puts it in the position of No. 1 Sports Aircraft in the world.
  • Airframe Structure
  • Dynamical System
  • Performance Specifications
  • Comfortable Cabin
  • Advanced Equipment
  • Technical Data
  • Customized Service

The fuselage is designed as Carbon fiber sandwich construction using Aramide as inner laminate in the cockpit area. The main bulkhead is designed as Carbon / Aramide sandwich. The undercarriage is attached directly to the main bulkhead. There is a box section stiffener made of CFRP which reinforces the door and the window cut-outs. There is a CFRP tunnel in the cockpit floor, which contains the control rods. The tunnel begins from the engine bulkhead and ends behind the main fuselage bulkhead.

 

 

 

SUPPLIER


 

The aircraft is equipped with a Rotax 912 ULS/S engine, which is a super-strong and the most reliable engine for sports aircrafts. The horizontal, four-cylinder, four-stroke engine features a hydraulic valve tappet driven by a push rod of a central camshaft, a water-cooled cylinder head, a dry sump, and a lubricating system for the sliding pump.
 
Engine Type Rotax 912 ULS, horizontally opposed, four-cylinder, four-stroke
Cooling system Water-cooled cylinder head, air-cooled cylinder shaft
Lubricating System Dry sump lubrication system
Horsepower At 5800 RPM / Rated Power 73.5 KW / 100 HP
Torque 5100 RPM 128NM
Oil Supply System Constant pressure carburetor
Ignition Dual electronic ignition
Propeller & Gear Ratio 2.43:1
Engine Type Rotax 912 IS, horizontally opposed, four-cylinder, four-stroke
Cooling system Water-cooled cylinder head, air-cooled cylinder shaft
Lubricating System Dry sump lubrication system
Horsepower At 5800 RPM / Rated Power 73.5 KW / 100 HP
Torque 5500 RPM 132NM
Oil Supply System Electronic fuel injection
Ignition Dual electronic ignition
Propeller & Gear Ratio 2.43:1

 
 左右尚有資訊
Maximum Take-off Weight 600 Kg (1320 lb)
Total Fuel Capacity 130 L (34 gal)
Total Fuel Available 126 L (33 gal)
Approved types of fuel Premium Automotive unleaded per ASTM D 4814 Minimum AKI 91 EN 228 Super min. RON 95 EN 228 Super plus min. RON 95 CAN/CGSB-3.5 Quality 3 min. AKI 91AVGAS 100 LL ASTM D910 AVGAS UL 91 ASTM D7547
Maximum Engine Power 73.5 KW at 5800RPM
Maximum Endurance 10.0 hrs
Maximum Airspeed 222 km/h (120 kt) IAS, Altitude 5500 m
Typical cruise speed @ 9000 ft 91 knot (168 km/h) IAS
90 knot (166 km/h) CAS
106 knot (196 km/h) TAS
Flap -6°, 4500 rpm, 75%MCP
Best rate of climb (VY) at sea level (ISA 0) and MTOW Flap 0° 67 Knot (123 km/h) IAS 4.12 m/s (811 ft/m)
Best angle of climb (VX) Flap 0° 54 Knot (99 km/h) IAS 1:7.4 (7.8°)
Stall speed Flap -6 49 knot (92 km/h) IAS
Flap 0° 47 knot (87 km/h) IAS
Flap 15° 44 knot (81 km/h) IAS
Flap 30° 42 knot (78 km/h) IAS
CTLS has the most spacious cabin among sports aircrafts of the same class, allowing both the pilot and the passenger to enjoy the best flight view and comfortable space for their entire body. When the automatic navigation is activated, the body and mind of the crew can relax and enjoy an excellent visual experience with both ease and comfort.
 

Adjustable Three-bladed Propeller

Neuform three-blade composite propeller, adjustable on the ground.

Emergency Location Transmitting System ELT

Every CTLS features the most advanced Emergency Location Transmitting System ELT 460MHz of Cospas-Sarsat.


Whole Aircraft Rescue Parachute System BRS

In case of emergency, the pilot can activate the parachute system by pressing a single BRS button. Once the parachute is opened, the descending speed reduces to the minimum (about 518 meters per minute). The force generated by the impact on the ground is equivalent to that caused by falling from a height of four meters; as a result, the aircraft structure and cabin can be buffered to provide maximum protection to the crew.

Most Advanced Aircraft Instrument

The dual-screen interface Dynon Skyview SV-D1000 has been adopted to integrate traditional mechanical instruments and is equipped with Garmin GPS (Aera 795/796XM), radio Garmin GTR225, and the ELT 406 MHz emergency location transmitting system. All data and parameters of the aircraft’s instruments are integrated on the high-tech LCD screen, allowing the pilot to quickly comprehend all flight status factors.
Technical Data
Max. Length 6.604 m
Max. Height 2.342 m
Wing Span 8.594 m
VH:maximum horizon speed 222 km/h
VNE:maxium permissible airspeed 300 km/h
Take-off Distance 274 m
Maximum range 1800 km
Maximum Take-off Mass 600 kg
Total Fuel Capcity 130 L
Engine Rotax 912ULS 100 Hp
Seat 2
In order to meet more customers who are fond of AJCT aircraft and expand the scope of services, AeroJones Aviation has launched an exclusive customized unit, allowing customers to have a number of customized additional purchases and equipment combinations, which can be perfectly tailored to your personal preference.
 
 
   Moss Grey   
Click on the picture below to view...

 
   Checkered Black   
Click on the picture below to view...

 
   Honeycomb Black   
Click on the picture below to view...

 
   Honeycomb Brown   
Click on the picture below to view...

 
    Carbon Black   
Click on the picture below to view...

 
   Carbon Black-Blue   
Click on the picture below to view...

 
   Carbon Black-Red   
Click on the picture below to view...

 

 
 


Airframe Structure

The fuselage is designed as Carbon fiber sandwich construction using Aramide as inner laminate in the cockpit area. The main bulkhead is designed as Carbon / Aramide sandwich. The undercarriage is attached directly to the main bulkhead. There is a box section stiffener made of CFRP which reinforces the door and the window cut-outs. There is a CFRP tunnel in the cockpit floor, which contains the control rods. The tunnel begins from the engine bulkhead and ends behind the main fuselage bulkhead.

 

 

 

SUPPLIER


 

Dynamical System
The aircraft is equipped with a Rotax 912 ULS/S engine, which is a super-strong and the most reliable engine for sports aircrafts. The horizontal, four-cylinder, four-stroke engine features a hydraulic valve tappet driven by a push rod of a central camshaft, a water-cooled cylinder head, a dry sump, and a lubricating system for the sliding pump.
 
Engine Type Rotax 912 ULS, horizontally opposed, four-cylinder, four-stroke
Cooling system Water-cooled cylinder head, air-cooled cylinder shaft
Lubricating System Dry sump lubrication system
Horsepower At 5800 RPM / Rated Power 73.5 KW / 100 HP
Torque 5100 RPM 128NM
Oil Supply System Constant pressure carburetor
Ignition Dual electronic ignition
Propeller & Gear Ratio 2.43:1
Engine Type Rotax 912 IS, horizontally opposed, four-cylinder, four-stroke
Cooling system Water-cooled cylinder head, air-cooled cylinder shaft
Lubricating System Dry sump lubrication system
Horsepower At 5800 RPM / Rated Power 73.5 KW / 100 HP
Torque 5500 RPM 132NM
Oil Supply System Electronic fuel injection
Ignition Dual electronic ignition
Propeller & Gear Ratio 2.43:1
Performance Specifications

 
 左右尚有資訊
Maximum Take-off Weight 600 Kg (1320 lb)
Total Fuel Capacity 130 L (34 gal)
Total Fuel Available 126 L (33 gal)
Approved types of fuel Premium Automotive unleaded per ASTM D 4814 Minimum AKI 91 EN 228 Super min. RON 95 EN 228 Super plus min. RON 95 CAN/CGSB-3.5 Quality 3 min. AKI 91AVGAS 100 LL ASTM D910 AVGAS UL 91 ASTM D7547
Maximum Engine Power 73.5 KW at 5800RPM
Maximum Endurance 10.0 hrs
Maximum Airspeed 222 km/h (120 kt) IAS, Altitude 5500 m
Typical cruise speed @ 9000 ft 91 knot (168 km/h) IAS
90 knot (166 km/h) CAS
106 knot (196 km/h) TAS
Flap -6°, 4500 rpm, 75%MCP
Best rate of climb (VY) at sea level (ISA 0) and MTOW Flap 0° 67 Knot (123 km/h) IAS 4.12 m/s (811 ft/m)
Best angle of climb (VX) Flap 0° 54 Knot (99 km/h) IAS 1:7.4 (7.8°)
Stall speed Flap -6 49 knot (92 km/h) IAS
Flap 0° 47 knot (87 km/h) IAS
Flap 15° 44 knot (81 km/h) IAS
Flap 30° 42 knot (78 km/h) IAS
Comfortable Cabin
CTLS has the most spacious cabin among sports aircrafts of the same class, allowing both the pilot and the passenger to enjoy the best flight view and comfortable space for their entire body. When the automatic navigation is activated, the body and mind of the crew can relax and enjoy an excellent visual experience with both ease and comfort.
 
Advanced Equipment

Adjustable Three-bladed Propeller

Neuform three-blade composite propeller, adjustable on the ground.

Emergency Location Transmitting System ELT

Every CTLS features the most advanced Emergency Location Transmitting System ELT 460MHz of Cospas-Sarsat.


Whole Aircraft Rescue Parachute System BRS

In case of emergency, the pilot can activate the parachute system by pressing a single BRS button. Once the parachute is opened, the descending speed reduces to the minimum (about 518 meters per minute). The force generated by the impact on the ground is equivalent to that caused by falling from a height of four meters; as a result, the aircraft structure and cabin can be buffered to provide maximum protection to the crew.

Most Advanced Aircraft Instrument

The dual-screen interface Dynon Skyview SV-D1000 has been adopted to integrate traditional mechanical instruments and is equipped with Garmin GPS (Aera 795/796XM), radio Garmin GTR225, and the ELT 406 MHz emergency location transmitting system. All data and parameters of the aircraft’s instruments are integrated on the high-tech LCD screen, allowing the pilot to quickly comprehend all flight status factors.
Technical Data
Technical Data
Max. Length 6.604 m
Max. Height 2.342 m
Wing Span 8.594 m
VH:maximum horizon speed 222 km/h
VNE:maxium permissible airspeed 300 km/h
Take-off Distance 274 m
Maximum range 1800 km
Maximum Take-off Mass 600 kg
Total Fuel Capcity 130 L
Engine Rotax 912ULS 100 Hp
Seat 2
Customized Service
In order to meet more customers who are fond of AJCT aircraft and expand the scope of services, AeroJones Aviation has launched an exclusive customized unit, allowing customers to have a number of customized additional purchases and equipment combinations, which can be perfectly tailored to your personal preference.
 
 
   Moss Grey   
Click on the picture below to view...

 
   Checkered Black   
Click on the picture below to view...

 
   Honeycomb Black   
Click on the picture below to view...

 
   Honeycomb Brown   
Click on the picture below to view...

 
    Carbon Black   
Click on the picture below to view...

 
   Carbon Black-Blue   
Click on the picture below to view...

 
   Carbon Black-Red   
Click on the picture below to view...

 

 
 
Return to previous page

AeroJones Taiwan│AeroJones Xiamen
AeroJones JiangSu│AeroJones Germany

AeroJones Aviation Technology Co., Ltd.

ADD:No.5, Keyuan 1st Rd, Xitun Dist., Taichung City, Taiwan
TEL:+886-4-2461-8885
E-mail:aerojones@aerojones.com

NewsQ/ADocument Download
  • Privacy Policy
  • All rights reserved
256 bit SSL Encryption
Recommend using Chrome, Firefox, Safari latest version of the browser.
Designed by MIRACLEWeb Design
Call Now