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AEROSPOOL WT-9 Dynamic

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WT9
Aircraft
Name WT-9 Dynamic
Manufacturer AEROSPOOL
Body Narrow
Wing Fixed Wing
Position Low wing
Tail Regular tail, low set
WTC Light
APC A
Type code L1P
Engine Piston
Engine count Single
Position Nose mounted
Landing gear Tricycle retractable or fixed
Mass group 1


Manufacturered as:

AEROSPOOL Dynamic
AEROSPOOL WT-9 Dynamic


AEROSPOOL WT-9 Dynamic

AEROSPOOL WT-9 Dynamic AEROSPOOL WT-9 Dynamic 3D

Description

Two seat (one pilot and one passenger) ultralight aircraft.

Technical Data

Wing span 9.00 m29.528 ft
Length 6.40 m20.997 ft
Height 2.00 m6.562 ft
Powerplant 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke, 75 kW (101 hp)
Engine model Rotax 912

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
Descent
(to FL100)
Descent (FL100
& below)
Approach
V2 (IAS) kts IAS kts IAS kts IAS kts MACH TAS 130 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance 147 m ROC 1400 ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance 263 m
MTOW 450450 kg
0.45 tonnes
kg
Ceiling FL180 ROD ft/min APC A
WTC L Range 860860 nm
1,592,720 m
1,592.72 km
5,225,459.321 ft
NM

Accidents & Serious Incidents involving WT9

  • A319 / WT9, vicinity Stuttgart Germany, 2017 (On 26 June 2017, an Airbus A319 which had just taken off from Stuttgart came into conflict in Class ‘D’ airspace with a VFR light aircraft crossing its track and when, at 1,200 feet agl, the TCAS RA to descend which resulted was followed, an EGPWS Mode 3 Alert was generated. Clear of Conflict was annunciated after 10 seconds and climb resumed. The Investigation concluded that the light aircraft pilot had failed to follow the clearance which had been accepted and had caused the flight path conflict which was resolved by the response of the A319 to the TCAS RA.)