can we add the zlin 142?
I rlly like it
for some stunts and scenery hunting
i want this plane to be added in IF
so i requested this lovely plane to be added in IF
(source: https://en.wikipedia.org/wiki/Zlín_Z_42)
image source: https://en.wikipedia.org/wiki/Zlín_Z_42#/media/File:Zlin_Z-142.jpg
Zlín Z-142
Development continued, with the Zlín Z 142 , featuring a slightly enlarged two-seat airframe based on that of the Z 42 and the more powerful (157 kW (210 hp)) Walter (now LOM) M 337 fuel-injected inverted six-cylinder, supercharged air-cooled engine of the Z 43 replacing the unsupercharged LOM M137 engine of the Z 42. The prototype Z-142 first flew on 29 December 1978.[3]
In the late 1980s, further development work was initiated. The inverted inline engine was replaced with a four-cylinder horizontally-opposed Lycoming IO-360 engine. This variant is designated the Z 242 , and is immediately distinguishable by its relatively wide cowling which houses the flat-four engine.
Licence production of the Z 142 has been carried out in Algeria by ECA Fernas (sometimes known as just Fernas) as the ECA-Fernas 142 , complete with aerobatic modifications.[
General characteristics
- Crew: 1 or 2
- Capacity: (1 pax or student)
- Length: 7.07 m (23 ft 2 in)
- Wingspan: 9.11 m (29 ft 11 in)
9.19 m (30 ft) over tip-tanks
- Height: 2.69 m (8 ft 10 in)
- Wing area: 13.15 m2 (141.5 sq ft)
- Airfoil: NACA 632416.5
- Empty weight: 645 kg (1,422 lb)
- Max takeoff weight: 970 kg (2,138 lb) normal
920 kg (2,028 lb) aerobatic
- Fuel capacity: 130 l (34 US gal; 29 imp gal) in wing leading edges
- Powerplant: 1 × Avia M 137 AZ 6-cylinder inverted air-cooled in-line piston engine, 130 kW (180 hp)
- Propellers: 2-bladed Avia V 503, 2 m (6 ft 7 in) diameter fully automatic constant-speed propeller
Performance
- Maximum speed: 226 km/h (140 mph, 122 kn) TAS(aerobatic TOW) at 600 m (1,969 ft) ISA
- Cruise speed: 215 km/h (134 mph, 116 kn) TAS at 600 m (1,969 ft) ISA
- Stall speed: 89 km/h (55 mph, 48 kn) flaps down power off
- Never exceed speed: 315 km/h (196 mph, 170 kn) [25]
- Range: 530 km (330 mi, 290 nmi) standard fuel
- Ferry range: 1,200 km (750 mi, 650 nmi) with wingtip fuel tanks
- Service ceiling: 4,250 m (13,940 ft)
- g limits: +3.8 -1.5 normal
+6 -3.5 aerobatic
- Rate of climb: 5.2 m/s (1,020 ft/min)
- Wing loading: 74 kg/m2 (15 lb/sq ft) normal
70 kg/m2 (14 lb/sq ft)
- Power/mass: 0.138 kW/kg (0.084 hp/lb) normal
0.1457 kW/kg (0.0886 hp/lb) aerobatic
- Take-off run to 15 m (49 ft): 380 m (1,247 ft)
- Landing run from 15 m (49 ft): 410 m (1,345 ft)
Avionics
VHF radio and IFR instrumentation optional
i hope this plane gets added
i really like it