CESSNA T210N Model Guide
CESSNA T210N · Model Guide
Overview
CESSNA T210N is a single-engine piston Cessna 210 variant. It has a turbocharged, fuel-injected 310 hp Teledyne Continental TSIO-520-R and a 3-bladed constant speed propeller. The 1982 handbook lists a 4000 lb max takeoff weight, 90 gal fuel capacity (87 usable) and a 204 kt maximum speed.
- Max takeoff 4000 lb, ramp 4016 lb, landing 3800 lb. Standard empty weight is 2237 lb (Turbo Centurion), with a useful load of 1779 lb.
- Engine: 310 BHP for 5 minutes at takeoff, 285 BHP continuous. Avoid continuous operation at 1850-2150 RPM above 24 inches manifold pressure.
- Fuel: 90 gal total, 87 usable, 100LL or 100 grade. Baggage limit is 240 lb combined; the baggage door placard says 200 lb total.
- Mandatory McFarlane SB-14 (Dec 8, 2025) requires removing the MC0743624-2 shimmy dampener from 210N/T210N. No PMA replacement is offered.
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
- Engine (hp) ·
- 310
- Max speed (kt) ·
- 204
- Usable fuel (gal) ·
- 87
- Empty weight (lb) ·
- 2,237
- Fuel capacity (gal) ·
- 90
- Service ceiling (ft) ·
- 27,000
- Baggage allowance (lb) ·
- 240
- Max takeoff weight (lb) ·
- 4,000
Performance
- Max speed (kt) ·
- 204
- Rate of climb (fpm) ·
- 930
- Service ceiling (ft) ·
- 27,000
- Takeoff over 50ft (ft) ·
- 2,160
- Stall speed clean (kt) ·
- 67
- Takeoff ground roll (ft) ·
- 1,300
- Stall speed landing (kt) ·
- 58
V-speeds
- VA_KTS ·
- 130
- VFE_KTS ·
- 160
- VLE_KTS ·
- 203
- VLO_KTS ·
- 165
- VNE_KTS ·
- 203
- VNO_KTS ·
- 168
Weight & balance
- Empty weight (lb) ·
- 2,237
- Max ramp weight (lb) ·
- 4,016
- Max useful load (lb) ·
- 1,779
- Baggage allowance (lb) ·
- 240
- Max landing weight (lb) ·
- 3,800
- Max takeoff weight (lb) ·
- 4,000
How much can the CESSNA T210N carry?
The CESSNA T210N has a 4000 lb max takeoff weight and a 2237 lb standard empty weight for the Turbo Centurion. The handbook lists a 1779 lb maximum useful load. Combined baggage is limited to 240 lb.
What fuel does the CESSNA T210N use?
The CESSNA T210N uses 100LL (blue) or 100 (green) aviation fuel. Total capacity is 90 gal, of which 87 gal is usable. Takeoff and landing must be done on the BOTH tank position.
Is there an open service bulletin on the CESSNA T210N?
Yes. McFarlane SB-14, dated December 8, 2025, is mandatory. It covers the MC0743624-2 shimmy dampener, which interferes with the nose gear door. It must be removed from the CESSNA T210N, and no PMA replacement is currently offered.
What is the CESSNA T210N Model Guide?
The CESSNA T210N Model Guide is a model guide for the CESSNA T210N, dated 2026.
What year was the CESSNA T210N Model Guide published?
The CESSNA T210N Model Guide — the CESSNA T210N model guide on file — is dated 2026.
Common. More common than 99% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the CESSNA T210N.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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In this document
Performance and speeds
Handbook figures: 930 fpm climb at sea level, 27,000 ft service ceiling, 1300 ft takeoff ground roll and 2160 ft over a 50-ft obstacle. Stall is 67 KCAS flaps up and 58 KCAS flaps down. Vne is 203 KIAS, Vno 168 KIAS, Va 130 KIAS at 4000 lb. Gear operating speed is 165 KIAS.
Fuel, oil and engine care
Use 100LL (blue) or 100 (green) fuel. 3 gal of the 90 gal total is unusable. Take off and land on BOTH tanks. Oil capacity is 11 quarts total (10 in the sump). Use straight mineral oil for the first 50 hours or until consumption stabilizes, then ashless dispersant. Max cylinder head temperature is 460°F and max oil temperature is 240°F.
What to check when buying
Confirm the shimmy dampener part number and lot (104648, 110666 or 112303) against SB-14 and the log book entries. Check that the handbook is current: revision 1 dated 16 December 1981 is the latest listed. Verify installed equipment against the weight and balance. Icing is prohibited unless a known-icing package is 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.
Safety notes
- SB-14 is mandatory: remove the MC0743624-2 shimmy dampener on 210N/P210N/T210N (nose gear door interference) and return it to McFarlane.
- With 1/4 tank or less, prolonged uncoordinated flight is prohibited on either left or right tank. Single-tank use is for level flight only.
- Normal category only: no aerobatics or spins. Flight into known icing is prohibited unless the airplane has the known-icing equipment package.
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
CESSNA T210N Model Guide CESSNA T210N is a single-engine piston Cessna 210 variant. It has a turbocharged, fuel-injected 310 hp Teledyne Continental TSIO-520-R and a 3-bladed constant speed propeller. The 1982 handbook lists a 4000 lb max takeoff weight, 90 gal fuel capacity (87 usable) and a 204 kt maximum speed. • Max takeoff 4000 lb, ramp 4016 lb, landing 3800 lb. Standard empty weight is 2237 lb (Turbo Centurion), with a useful load of 1779 lb. • Engine: 310 BHP for 5 minutes at takeoff, 285 BHP continuous. Avoid continuous operation at 1850-2150 RPM above 24 inches manifold pressure. • Fuel: 90 gal total, 87 usable, 100LL or 100 grade. Baggage limit is 240 lb combined; the baggage door placard says 200 lb total. • Mandatory McFarlane SB-14 (Dec 8, 2025) requires removing the MC0743624-2 shimmy dampener from 210N/T210N. No PMA replacement is offered. Performance and speeds Handbook figures: 930 fpm climb at sea level, 27,000 ft service ceiling, 1300 ft takeoff ground roll and 2160 ft over a 50-ft obstacle. Stall is 67 KCAS flaps up and 58 KCAS flaps down. Vne is 203 KIAS, Vno 168 KIAS, Va 130 KIAS at 4000 lb. Gear operating speed is 165 KIAS. Fuel, oil and engine care Use 100LL (blue) or 100 (green) fuel. 3 gal of the 90 gal total is unusable. Take off and land on BOTH tanks. Oil capacity is 11 quarts total (10 in the sump). Use straight mineral oil for the first 50 hours or until consumption stabilizes, then ashless dispersant. Max cylinder head temperature is 460°F and max oil temperature is 240°F. What to check when buying Confirm the shimmy dampener part number and lot (104648, 110666 or 112303) against SB-14 and the log book entries. Check that the handbook is current: revision 1 dated 16 December 1981 is the latest listed. Verify installed equipment against the weight and balance. Icing is prohibited unless a known-icing package is fitted. Safety notes: • SB-14 is mandatory: remove the MC0743624-2 shimmy dampener on 210N/P210N/T210N (nose gear door interference) and return it to McFarlane. • With 1/4 tank or less, prolonged uncoordinated flight is prohibited on either left or right tank. Single-tank use is for level flight only. • Normal category only: no aerobatics or spins. Flight into known icing is prohibited unless the airplane has the known-icing equipment package.