CZAW SportCruiser Model Guide
CZAW SportCruiser · Model Guide
Overview
The CZAW SportCruiser is a two-seat, single-engine piston light aircraft with a Rotax 912 ULS engine rated at 73.5 kW (98.6 hp). The handbooks give a 600 kg maximum takeoff weight and 113 L of usable fuel. It is approved for day VFR only. The two handbooks supplied differ in places, so confirm which one applies to the airframe you are buying.
- Two seats, 600 kg max takeoff weight, 113 L usable fuel. Cruise is 93 knots at 75% power at 3,000 ft.
- Quoted range is 512 NM (Cruiser POH) or 516 NM (SportCruiser POH), with a 30 minute reserve.
- Day VFR only. IFR flight and intentional flight in icing conditions are prohibited.
- The two handbooks differ on empty weight, wing locker limit, stall speeds and service ceiling. Check which one matches the airframe.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at sprinkle.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Model Guide
- Year ·
- 2026
- File size ·
- 49 KB
- Copy found at ·
- sprinkle.com
Specifications & performance
Extracted from this document.
Specifications
- Height (ft) ·
- 7.78
- Length (ft) ·
- 21.33
- Wing span (ft) ·
- 28.9
- Engine power (hp) ·
- 98.6
- Usable fuel (gal) ·
- 29.86
- Cockpit width (in) ·
- 46
- Fuel capacity (gal) ·
- 30.12
- Propeller diameter (in) ·
- 68
Performance
- Range (nm) ·
- 516
- Cruise speed (kt) ·
- 93
- Rate of climb (fpm) ·
- 825
- Service ceiling (ft) ·
- 14,378
- Max speed sea level (kt) ·
- 116
- Stall speed flaps up (kt) ·
- 39
- Stall speed flaps down (kt) ·
- 32
V-speeds
- NEVER_EXCEED_KTS ·
- 138
- APPROACH_SPEED_KTS ·
- 60
- BEST_RATE_CLIMB_KTS ·
- 62
- BEST_ANGLE_CLIMB_KTS ·
- 56
- MANEUVERING_SPEED_KTS ·
- 88
- MAX_FLAP_EXTENDED_KTS ·
- 75
- MAX_STRUCTURAL_CRUISE_KTS ·
- 108
Weight & balance
- Empty weight (lb) ·
- 760
- Max fuel weight (lb) ·
- 180
- Max baggage rear (lb) ·
- 40
- Max takeoff weight (lb) ·
- 1,320
- Max baggage wing locker (lb) ·
- 44
- Max crew weight per seat (lb) ·
- 253
How far can it fly?
The CZAW SportCruiser handbooks quote 512 NM (Cruiser POH) and 516 NM (SportCruiser POH). Both assume 75% power at 3,000 ft, 113 L of usable fuel and a 30 minute reserve.
What fuel does it use?
The CZAW SportCruiser runs on MOGAS of min RON 95. Fuels with more than 5% ethanol are not permitted. AVGAS 100 LL is for vapor lock problems or when other gasoline is unavailable.
Can it be flown IFR?
No. The CZAW SportCruiser is approved for day VFR only. IFR flight and intentional flight in icing conditions are prohibited, and the minimum instrument list is for Day VFR.
How many people can it carry?
The CZAW SportCruiser has 2 seats, with a maximum of 115 kg on each seat. The minimum crew is one pilot on the left seat. Minimum crew weight is 55 kg in the Cruiser POH and 43 kg in the SportCruiser POH.
What is the CZAW SportCruiser Model Guide?
The CZAW SportCruiser Model Guide is a model guide for the CZAW SportCruiser, dated 2026.
What year was the CZAW SportCruiser Model Guide published?
The CZAW SportCruiser Model Guide — the CZAW SportCruiser model guide on file — is dated 2026.
Most owners only have the POH. Here's the essential set for the CZAW SportCruiser.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More CZAW SportCruisermanuals & documents
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- POH SportCruiserCZAW SportCruiser · Pilot's Operating Handbook
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- CESSNA C-165 Model GuideCESSNA C-165 · Model Guide
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In this document
Weights and loading
Max takeoff and landing weight is 600 kg. Max fuel weight is 82 kg and rear fuselage baggage is 18 kg. The wing locker limit is 10 kg each in the Cruiser POH and 20 kg each in the SportCruiser POH. Max empty weight is 405 kg (Cruiser POH). The SportCruiser POH lists 345 kg empty with minimum equipment. Max crew weight is 115 kg per seat. Actual empty weight is in Section 9, Supplement No. 02.
Engine and fuel
The Rotax 912 ULS makes 73.5 kW at 5,800 rpm (max 5 min) and 69 kW continuous at 5,500 rpm. Two wing tanks hold 57 L each, 114 L total, 113 L usable. MOGAS (min RON 95) is recommended, and fuels with more than 5% ethanol are not permitted. AVGAS 100 LL stresses the valve seats and builds deposits, so use it only for vapor lock problems or when other fuel is unavailable.
Takeoff, landing and climb (SportCruiser POH)
Figures are for 600 kg, ISA, sea level, with flaps 15° for takeoff. Takeoff run is 463 ft on concrete and 702 ft on grass. Distance over a 50 ft obstacle is 1,270 ft on concrete and 1,499 ft on grass. Landing over 50 ft is 1,188 ft on concrete. Rate of climb is 825 fpm at sea level and 355 fpm at 9000 ft.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Safety notes
- Day VFR only. IFR flight and intentional flight in icing conditions are prohibited.
- Do not exceed the 600 kg max takeoff weight. The emergency parachute is approved for up to 612 kg and 120 knots.
- Do not idle fully on final or in long descents: the engine can under-cool and lose power. 6 L of fuel allows only about 15 minutes of safe operation.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
CZAW SportCruiser Model Guide The CZAW SportCruiser is a two-seat, single-engine piston light aircraft with a Rotax 912 ULS engine rated at 73.5 kW (98.6 hp). The handbooks give a 600 kg maximum takeoff weight and 113 L of usable fuel. It is approved for day VFR only. The two handbooks supplied differ in places, so confirm which one applies to the airframe you are buying. • Two seats, 600 kg max takeoff weight, 113 L usable fuel. Cruise is 93 knots at 75% power at 3,000 ft. • Quoted range is 512 NM (Cruiser POH) or 516 NM (SportCruiser POH), with a 30 minute reserve. • Day VFR only. IFR flight and intentional flight in icing conditions are prohibited. • The two handbooks differ on empty weight, wing locker limit, stall speeds and service ceiling. Check which one matches the airframe. Weights and loading Max takeoff and landing weight is 600 kg. Max fuel weight is 82 kg and rear fuselage baggage is 18 kg. The wing locker limit is 10 kg each in the Cruiser POH and 20 kg each in the SportCruiser POH. Max empty weight is 405 kg (Cruiser POH). The SportCruiser POH lists 345 kg empty with minimum equipment. Max crew weight is 115 kg per seat. Actual empty weight is in Section 9, Supplement No. 02. Engine and fuel The Rotax 912 ULS makes 73.5 kW at 5,800 rpm (max 5 min) and 69 kW continuous at 5,500 rpm. Two wing tanks hold 57 L each, 114 L total, 113 L usable. MOGAS (min RON 95) is recommended, and fuels with more than 5% ethanol are not permitted. AVGAS 100 LL stresses the valve seats and builds deposits, so use it only for vapor lock problems or when other fuel is unavailable. Takeoff, landing and climb (SportCruiser POH) Figures are for 600 kg, ISA, sea level, with flaps 15° for takeoff. Takeoff run is 463 ft on concrete and 702 ft on grass. Distance over a 50 ft obstacle is 1,270 ft on concrete and 1,499 ft on grass. Landing over 50 ft is 1,188 ft on concrete. Rate of climb is 825 fpm at sea level and 355 fpm at 9000 ft. Safety notes: • Day VFR only. IFR flight and intentional flight in icing conditions are prohibited. • Do not exceed the 600 kg max takeoff weight. The emergency parachute is approved for up to 612 kg and 120 knots. • Do not idle fully on final or in long descents: the engine can under-cool and lose power. 6 L of fuel allows only about 15 minutes of safe operation.