CESSNA Turbo Skylane T182T Model Guide
CESSNA Turbo Skylane T182T · Model Guide
Overview
The CESSNA Turbo Skylane T182T is a single-engine piston airplane with 2+2 seating and a constant-speed 3-blade propeller. The POH lists a turbocharged 235 BHP engine and a 20,000 ft maximum operating altitude. It carries 87 gallons of usable fuel. Check which engine your specific airplane has, because the sources disagree.
- POH figures: 159 kt cruise at 88% power at 12,500 ft, 615 NM range, 20,000 ft maximum operating altitude.
- Max takeoff weight is 3100 lb with 87 gal usable fuel. Baggage is limited to 200 lb.
- POH short-field figures: 775 ft takeoff ground roll and 590 ft landing ground roll, in standard conditions.
- The engine in the sources is inconsistent (TIO-540-AK1A in the POH, O540-AB1A5 elsewhere). Verify it on the airplane.
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 power (hp) ·
- 235
- Usable fuel (gal) ·
- 87
- Fuel capacity (gal) ·
- 92
- Max ramp weight (lb) ·
- 3,112
- Baggage allowance (lb) ·
- 200
- Max landing weight (lb) ·
- 2,950
- Max takeoff weight (lb) ·
- 3,100
- Propeller diameter (in) ·
- 79
Performance
- Range (nm) ·
- 615
- Max speed (kt) ·
- 176
- Cruise speed (kt) ·
- 159
- Rate of climb (fpm) ·
- 1,040
- Service ceiling (ft) ·
- 20,000
- Best glide speed (kt) ·
- 76
- Landing ground roll (ft) ·
- 590
- Takeoff ground roll (ft) ·
- 775
V-speeds
- BEST_GLIDE_SPEED_KTS ·
- 76
- STALL_SPEED_FLAPS_UP_KTS ·
- 54
- STALL_SPEED_FLAPS_FULL_KTS ·
- 49
- BEST_RATE_OF_CLIMB_SPEED_KTS ·
- 80
- SHORT_FIELD_LIFTOFF_SPEED_KTS ·
- 49
- SHORT_FIELD_SPEED_AT_50FT_KTS ·
- 58
- SHORT_FIELD_LANDING_SPEED_AT_50FT_KTS ·
- 60
Weight & balance
- Max ramp weight (lb) ·
- 3,112
- Baggage total max (lb) ·
- 200
- Baggage area a max (lb) ·
- 120
- Max landing weight (lb) ·
- 2,950
- Max takeoff weight (lb) ·
- 3,100
- Baggage area b c max (lb) ·
- 80
How far can the CESSNA Turbo Skylane T182T fly?
The POH lists 615 NM at 88% power at 12,500 ft (4.0 hours) and 721 NM at 75% power at 10,000 ft. Max range is 971 NM at 10,000 ft. All figures use 87 gal usable fuel and a 45-minute reserve.
How much can the CESSNA Turbo Skylane T182T carry?
The POH gives a maximum useful load of 1083 lb in one place and 1089 lb in another, with a 200 lb baggage limit. Max takeoff weight is 3100 lb. Weigh the actual airplane to get its true useful load.
What short-field speeds apply to the CESSNA Turbo Skylane T182T?
At 3100 lb the charts show liftoff at 49 KIAS and 58 KIAS at 50 ft. Landing at 2950 lb uses 60 KIAS at 50 ft. Stall speed is 54 KCAS flaps up and 49 KCAS flaps full, both power idle.
What is the CESSNA Turbo Skylane T182T Model Guide?
The CESSNA Turbo Skylane T182T Model Guide is a model guide for the CESSNA Turbo Skylane T182T, dated 2026.
What year was the CESSNA Turbo Skylane T182T Model Guide published?
The CESSNA Turbo Skylane T182T Model Guide — the CESSNA Turbo Skylane T182T model guide on file — is dated 2026.
Most owners only have the POH. Here's the essential set for the CESSNA Turbo Skylane T182T.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More CESSNA Turbo Skylane T182Tmanuals & documents
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In this document
Performance (POH, standard conditions)
Maximum speed is 176 kt at 20,000 ft. Cruise is 159 kt at 88% power at 12,500 ft (615 NM, 4.0 hours) or 145 kt at 75% power at 10,000 ft (721 NM, 5.1 hours). Sea-level climb is 1040 fpm. Takeoff over a 50 ft obstacle takes 1385 ft and landing takes 1350 ft. Figures assume wheel and brake fairings.
Weights and loading
The POH lists ramp 3112 lb, takeoff 3100 lb and landing 2950 lb. Baggage Area A allows 120 lb, Areas B and C together allow 80 lb, and the total is 200 lb. The POH gives two standard empty weights (2029 lb and 2023 lb), so use the weighed empty weight and equipment list of the actual airplane.
Engine and avionics discrepancy
The POH describes the TIO-540-AK1A, a 541.5 cu in turbocharged six-cylinder rated 235 BHP at 2400 RPM. The library entry and a 2021 sales listing (429 hrs, G1000 NXi, GFC 700 autopilot) name a Lycoming O540-AB1A5. Confirm the engine data plate and logbooks against the paperwork.
Safety notes
- The POH copy supplied is not kept current and cannot replace the official POH, which must be carried in the airplane.
- Use only approved fuel: 100LL (blue) or 100 (green). Unapproved fuel may damage the engine and fuel system.
- Cessna's performance figures are calculated for standard, no-wind, dry hard-surface conditions. Your airplane will vary.
Full document text
CESSNA Turbo Skylane T182T Model Guide The CESSNA Turbo Skylane T182T is a single-engine piston airplane with 2+2 seating and a constant-speed 3-blade propeller. The POH lists a turbocharged 235 BHP engine and a 20,000 ft maximum operating altitude. It carries 87 gallons of usable fuel. Check which engine your specific airplane has, because the sources disagree. • POH figures: 159 kt cruise at 88% power at 12,500 ft, 615 NM range, 20,000 ft maximum operating altitude. • Max takeoff weight is 3100 lb with 87 gal usable fuel. Baggage is limited to 200 lb. • POH short-field figures: 775 ft takeoff ground roll and 590 ft landing ground roll, in standard conditions. • The engine in the sources is inconsistent (TIO-540-AK1A in the POH, O540-AB1A5 elsewhere). Verify it on the airplane. Performance (POH, standard conditions) Maximum speed is 176 kt at 20,000 ft. Cruise is 159 kt at 88% power at 12,500 ft (615 NM, 4.0 hours) or 145 kt at 75% power at 10,000 ft (721 NM, 5.1 hours). Sea-level climb is 1040 fpm. Takeoff over a 50 ft obstacle takes 1385 ft and landing takes 1350 ft. Figures assume wheel and brake fairings. Weights and loading The POH lists ramp 3112 lb, takeoff 3100 lb and landing 2950 lb. Baggage Area A allows 120 lb, Areas B and C together allow 80 lb, and the total is 200 lb. The POH gives two standard empty weights (2029 lb and 2023 lb), so use the weighed empty weight and equipment list of the actual airplane. Engine and avionics discrepancy The POH describes the TIO-540-AK1A, a 541.5 cu in turbocharged six-cylinder rated 235 BHP at 2400 RPM. The library entry and a 2021 sales listing (429 hrs, G1000 NXi, GFC 700 autopilot) name a Lycoming O540-AB1A5. Confirm the engine data plate and logbooks against the paperwork. Safety notes: • The POH copy supplied is not kept current and cannot replace the official POH, which must be carried in the airplane. • Use only approved fuel: 100LL (blue) or 100 (green). Unapproved fuel may damage the engine and fuel system. • Cessna's performance figures are calculated for standard, no-wind, dry hard-surface conditions. Your airplane will vary.