IAR.823 | F-AZLQ |

IAR.823 | F-AZLQ

Year of construction: 1975

Motor: Lycoming IO-540

Perfomance: 290 PS

MTOW: 1500 Kg

Dimensions: Length 8.25m / Span 10.00m

Home airport: EBZR

Owner: Jan Possemiers

Description: Armament : The aircraft has 2 underwing hardpoints, stressed for 100 kg each. Total maximum allowed weight of external stores is 200 kg. •BE-50 - 50 kg general purpose bomb •BEM-100 - 100 kg general purpose bomb •UB-4-57 - standard pod for 4 S-5K/M unguided rockets, caliber 57mm •7.62mm machine gun pod caliber 7.62x54R - Romanian designed •70 liters fuel drop tanks General characteristics Crew: Two, pilot and instructor Capacity: 3 passengers Length: 8.24 m (27 ft 0 in) Wingspan: 10.00 m (32 ft 10 in) Height: 2.52 m (8 ft 3 in) Wing area: 15.00 m2 (161.5 sq ft) Airfoil: NACA 23012 (modified) Empty weight: 900 kg (1,984 lb) Max takeoff weight: 1,500 kg (3,307 lb) Fuel capacity: 360 L (95 US gal; 79 imp gal) (internal) Powerplant: 1 × Lycoming IO-540-G1D5 air-cooled flat-six engine, 216 kW (290 hp) Performance Maximum speed: 310 km/h (190 mph, 170 kn) at sea level Cruise speed: 290 km/h (180 mph, 160 kn) (economy cruise, at 60% power) Stall speed: 98 km/h (61 mph, 53 kn) (flaps down, power off) Never exceed speed: 400 km/h (250 mph, 220 kn) Range: 1,800 km (1,100 mi, 970 nmi) Endurance: 6 hr Service ceiling: 5,600 m (18,400 ft) g limits: +6, -3G Rate of climb: 7.49 m/s (1,475 ft/min)