Engine / Powerplant | Technical Specifications | Pipistrel Virus SW-80 Microlite Aircraft | MCQ's

Virus SW-80 Microlite Aircraft

AIRPLANE SYSTEMS & STANDARD OPERATING PROCEDURES
Chapter III - Technical Specifications
MCQ's

ENGINE / POWERPLANT

(a) Engine Type - Rotax 912 A (80 HP)
4 Stroke 4 Cylinder
Horizontally Opposed
Spark Ignition
(b) Propeller - FP 02 – 80 Fixed Pitch
(c) Propeller diameter - 1650 mm
(d) Absolute ceiling at MTOW - 6200 metres / 20,300 feet
(e) Engine Performance - 58.0 KW (79 HP) at 5500 RPM
59.6 KW (81 HP) at 5800 RPM (Maximum 05 minutes)
(f) Torque - 103 Nm (75.9 foot pounds) at 4800 RPM
(g) Max permitted RPM - 5800 (Max 05 minutes)
(h) Compression Ratio - 9 : 1
(j) Cooling System - Water cooled Cylinder Heads
Ram Air cooled Cylinders
(k) Lubrication System - Dry Sump Forced Lubrication
(l) Ignition System - Dual Breakerless Capacitor Discharge
(m) Max coolant temperature - 120 deg C
(n) EGT Normal - 650 deg C – 885 deg C
(o) Max EGT - 900 deg C
(p) Max EGT difference - 30 deg C
(q) Oil Temperature Min - 50 deg C
Normal - 90 deg C – 110 deg C
Max - 140 deg C
(r) Oil Pressure Min - 1.0 Bar (14.5 PSI)
Max - 6.0 Bar (87.0 PSI)
(s) Engine RPM Max - 5500 (on ground)
(t) Max Permitted RPM - 5800 (Max 05 minutes)
(u) Magneto Drop Check at - 4000 RPM
(v) Single magneto drop Max - 300
Max difference in magneto Drop - 115
(w) Fuel Recommended - Unleaded Super Grade 93 or
above Max 10 % alcohol

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