YL-KSA - 1994 ANTONOV AN 74

1994

ANTONOV

AN-74

365.470.98.957

YL-KSA

Used

An-74-200 in cargo configuration Max payload 7.500 kgs Number of aircraft 1 Number of crew members 4-6 Number of passengers 10 Max take-off weight 36,5 Max Length 28.07 m Wing span 31.89 m Height 8.75 m Cruising speed 550 km/hr Maximum speed 700 km/hr Flight altitude 10.100 km Flight range Load 1.5 T - 4.150 km Load 5 T - 2.800 km Load 7.5 T - 2.150km Dimensions of cargo compartment (bxhxl) 9.5 x 2.15 x 2.2 Cargo door size 2.4 x 2.27 m Volume of cargo compartment 45-50 m3 Engine two turbofan engines D-36 3A series, chapter III compliant

1125.0

S/N 365.470.98.957, YOM 10.06.1994

Left engine (Lotarev D-36 serial 3A), S/N 708036423A024, YOM 25.02.1993, TSN 1.167 Hrs, 665 cycles Right engine (Lotarev D-36 serial 3A), S/N 708036133A001, YOM 22.02.1993, TSN 1.167 Hrs, 665 cycles Auxiliary Power Unit TA-12, S/N 32012019, YOM 14.07.1993, TSN 156 Hrs, 813 start up

1167

SNEW

1167

SNEW

Magnetic compass: KI-13 (1 unit) Heading System: BSFK-1 (1 unit) Autopilot: SAU-72-03 (1 unit) Radar: BURAN-74 (1 unit) Radio airborne (118,000-136,975 MHz) VHF BAKLAN-20D1 8.33 KHz, FM immunity (2 units) Radio airborne (2,000-23,9999 KHz) HF JADRO (1 unit) Emergency Radio Station (121,5 MHz)R-855 (2 units) Navigation system (VOR and ILS)KURS-ÌP-70 FM immunity (2 units) Navigation system (DME)SD-75 (2 units) Transponder (A,C mode)SO-72 (1 unit) Modes S Transponder Level 4 (A, C mode) XS-950 (1 unit) Flight data recorder BUR-2-3 (1 unit) and K3-63 (1 unit) Cockpit voice recorder MARS-BM (1 unit) EGPWS MARK VI (1 unit) Radio Altimeters A-037D1 (2 units) Airborne Collision Avoidance System TCAS-2000 (1 unit) B-RNAV MALVA-4 (1 unit) NVS-74 (1 unit) GPS KLN-90B

2005

10

All checks are executed Operating since new: Frame 1.125 Hrs, 670 landings Left engine 1.167 Hrs, 665 cycles Right engine 1.167 Hrs, 665 cycles APU TA-12 156 Hrs, 813 start up