CESSNA U206G STATIONAIR II Model Guide
CESSNA U206G STATIONAIR II · Model Guide
Overview
The CESSNA U206G STATIONAIR II is a six-seat, single-engine, high-wing piston aircraft with a 300 hp Teledyne Continental IO-520-F and a 3-bladed constant-speed propeller. It cruises at 147 kts, has a 3600 lb maximum takeoff weight, a 180 lb baggage allowance, and a 900 ft takeoff ground roll.
- 300 hp IO-520-F; 147 kts cruise at 75% power at 6500 ft, 156 kts maximum at sea level, service ceiling 14,800 ft.
- Maximum takeoff and landing weight is 3600 lbs. Useful load is 1441.5 lbs. Baggage limit is 180 lbs.
- Takeoff is 900 ft ground roll and 1780 ft over a 50-ft obstacle. Landing is 735 ft roll and 1395 ft over 50 ft.
- Fuel capacity varies by handbook and tank option: 61 gal or 80 gal long-range (1978), 92 gal (1981). Confirm the tanks fitted.
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 ·
- 50 KB
- Copy found at ·
- sprinkle.com
Specifications & performance
Extracted from this document.
Specifications
- Engine (hp) ·
- 300
- Empty weight (lb) ·
- 1,908
- Fuel capacity (gal) ·
- 61
- Max takeoff weight (lb) ·
- 3,600
Performance
- Max speed (kt) ·
- 156
- Cruise speed (kt) ·
- 147
- Rate of climb (fpm) ·
- 920
- Service ceiling (ft) ·
- 14,800
- Landing distance (ft) ·
- 735
- Takeoff distance (ft) ·
- 900
- Landing over 50ft (ft) ·
- 1,395
- Takeoff over 50ft (ft) ·
- 1,780
V-speeds
- VA_KTS ·
- 120
- VFE_KTS ·
- 140
- VNE_KTS ·
- 183
- VNO_KTS ·
- 149
- STALL_SPEED_CLEAN_KTS ·
- 62
- STALL_SPEED_LANDING_KTS ·
- 54
Weight & balance
- Useful load (lb) ·
- 1,441.5
- Max ramp weight (lb) ·
- 3,612
- Baggage allowance (lb) ·
- 180
- Basic empty weight (lb) ·
- 1,908
- Max landing weight (lb) ·
- 3,600
- Max takeoff weight (lb) ·
- 3,600
How fast is the CESSNA U206G STATIONAIR II?
The CESSNA U206G STATIONAIR II is listed at 156 kts maximum at sea level and 147 kts cruise at 75% power at 6500 ft. The 1978 handbook gives 450 nm range in 3.1 hrs with 59 gal usable fuel.
How much can the CESSNA U206G STATIONAIR II carry?
The CESSNA U206G STATIONAIR II has a 3600 lb maximum takeoff weight and a listed useful load of 1441.5 lbs. The baggage compartment is limited to 180 lbs. It seats six.
What fuel tanks does the CESSNA U206G STATIONAIR II have?
The CESSNA U206G STATIONAIR II is listed at 61 gal total in the standard tanks, with 59 gal usable, in the 1978 handbook. It also lists 80 gal long-range tanks. The 1981 handbook lists 92 gal total. Confirm the tanks fitted to the airplane.
What is the CESSNA U206G STATIONAIR II Model Guide?
The CESSNA U206G STATIONAIR II Model Guide is a model guide for the CESSNA U206G STATIONAIR II, dated 2026.
What year was the CESSNA U206G STATIONAIR II Model Guide published?
The CESSNA U206G STATIONAIR II Model Guide — the CESSNA U206G STATIONAIR II model guide on file — is dated 2026.
Most owners only have the POH. Here's the essential set for the CESSNA U206G STATIONAIR II.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More CESSNA U206G STATIONAIR IImanuals & documents
- RAPPORT D’ENQUETE DE SECURITEOther Documents
- AAIB Bulletin: 8/2015Service Bulletins
- PILOT'S OPERATING HANDBOOK Cessna STATIONAIR 6 1978 MODEL U206GPilot's Operating Handbook
- Aircraft Specifications – Serial Number U20604154, Registration N756KPSystems Description
- cessna model u206g - flight examinersV Speeds Reference
Related documents
- CESSNA U206F STATIONAIR Model GuideCESSNA U206F STATIONAIR · Model Guide
- CESSNA 206H STATIONAIR Model GuideCESSNA 206H STATIONAIR · Model Guide
- Cessna 206 Stationair Model GuideCessna 206 Stationair · Model Guide
- CESSNA T206H Model GuideCESSNA T206H · Model Guide
- cessna model u206g - flight examinersCESSNA U206G STATIONAIR II · V Speeds Reference
In this document
Powerplant and fuel
The IO-520-F is a normally aspirated, fuel-injected six-cylinder rated 300 BHP at 2850 RPM for 5 minutes and 285 BHP at 2700 RPM continuous. It takes 100LL or 100 grade fuel. The 1978 handbook lists 59 gal usable in standard tanks and 76 gal usable in long-range tanks. The 1981 handbook lists 88 gal usable.
Weights and loading
The 1978 handbook gives standard empty weight as 1908 lbs for the Stationair 6 and 1977 lbs for the Stationair 6 II. The 1981 handbook gives 1928 and 1989 lbs. Maximum ramp weight is 3612 lbs. Takeoff and landing weight is 3600 lbs. Baggage is limited to 180 lbs.
What to check when buying
One 1978 example is listed with 3061 hours airframe, 1440 hours since engine overhaul, complete logs, a February 2024 annual and an asking price of $389,900. Verify the engine and propeller hours, the logs, the fuel tank configuration, and the equipment list against the handbook.
Safety notes
- The owner's manual, as quoted by BEA, warns that a tank at or below one quarter capacity can starve the engine after prolonged uncoordinated flight such as sideslips.
- The AAIB 2015 report on a 1978 airframe describes an engine stoppage on downwind with fuel on board and no obvious cause found. The BEA 2022 report describes an engine shutdown in descent.
- Keep baggage within 180 lbs and the weight within 3600 lbs; the handbook has loading arrangements for seats removed.
Full document text
CESSNA U206G STATIONAIR II Model Guide The CESSNA U206G STATIONAIR II is a six-seat, single-engine, high-wing piston aircraft with a 300 hp Teledyne Continental IO-520-F and a 3-bladed constant-speed propeller. It cruises at 147 kts, has a 3600 lb maximum takeoff weight, a 180 lb baggage allowance, and a 900 ft takeoff ground roll. • 300 hp IO-520-F; 147 kts cruise at 75% power at 6500 ft, 156 kts maximum at sea level, service ceiling 14,800 ft. • Maximum takeoff and landing weight is 3600 lbs. Useful load is 1441.5 lbs. Baggage limit is 180 lbs. • Takeoff is 900 ft ground roll and 1780 ft over a 50-ft obstacle. Landing is 735 ft roll and 1395 ft over 50 ft. • Fuel capacity varies by handbook and tank option: 61 gal or 80 gal long-range (1978), 92 gal (1981). Confirm the tanks fitted. Powerplant and fuel The IO-520-F is a normally aspirated, fuel-injected six-cylinder rated 300 BHP at 2850 RPM for 5 minutes and 285 BHP at 2700 RPM continuous. It takes 100LL or 100 grade fuel. The 1978 handbook lists 59 gal usable in standard tanks and 76 gal usable in long-range tanks. The 1981 handbook lists 88 gal usable. Weights and loading The 1978 handbook gives standard empty weight as 1908 lbs for the Stationair 6 and 1977 lbs for the Stationair 6 II. The 1981 handbook gives 1928 and 1989 lbs. Maximum ramp weight is 3612 lbs. Takeoff and landing weight is 3600 lbs. Baggage is limited to 180 lbs. What to check when buying One 1978 example is listed with 3061 hours airframe, 1440 hours since engine overhaul, complete logs, a February 2024 annual and an asking price of $389,900. Verify the engine and propeller hours, the logs, the fuel tank configuration, and the equipment list against the handbook. Safety notes: • The owner's manual, as quoted by BEA, warns that a tank at or below one quarter capacity can starve the engine after prolonged uncoordinated flight such as sideslips. • The AAIB 2015 report on a 1978 airframe describes an engine stoppage on downwind with fuel on board and no obvious cause found. The BEA 2022 report describes an engine shutdown in descent. • Keep baggage within 180 lbs and the weight within 3600 lbs; the handbook has loading arrangements for seats removed.