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CESSNA 210N Model Guide

CESSNA 210N · Model Guide

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Overview

The CESSNA 210N is a retractable-gear, single-engine piston Cessna with a fuel-injected Continental engine (285 hp continuous, 300 hp for the takeoff rating) and a three-blade constant-speed propeller. The 1984 handbook lists 175 kt maximum speed, 168 kt cruise at 75% power and 765 NM range. Library data differs in places, so check the figures against the airplane's own handbook.

  • 1984 handbook: 175 kt max, 168 kt cruise at 75% power, 765 NM range with 45-minute reserve, 950 fpm climb, 17300 ft service ceiling.
  • Weights: 3800 lb takeoff, 3812 lb ramp, 1639 lb useful load (Centurion), 240 lb baggage with four people. Library data lists 3600 lb.
  • Takeoff: 1250 ft ground roll, 2030 ft over 50 ft. Landing: 765 ft roll, 1500 ft over 50 ft (standard day, hard runway, no wind).
  • The gear is retractable and a wheels-up landing is on record. The warning horn sounds below about 12 inches of manifold pressure.

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.

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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)
·
285
Length (ft)
·
28
Propeller
·
3-blade constant speed
Wingspan (ft)
·
36
Empty weight (lb)
·
2,173
Fuel capacity (gal)
·
90

Performance

Range (nm)
·
765
Max speed (kt)
·
175
Cruise speed (kt)
·
168
Rate of climb (fpm)
·
950
Service ceiling (ft)
·
17,300
Takeoff distance (ft)
·
2,030
Landing ground roll (ft)
·
765
Takeoff ground roll (ft)
·
1,250

Weight & balance

Useful load (lb)
·
1,639
Empty weight (lb)
·
2,173
Max ramp weight (lb)
·
3,812
Baggage allowance (lb)
·
240
Max takeoff weight (lb)
·
3,800
About this document
How fast and how far does the CESSNA 210N fly?

The 1984 handbook for the CESSNA 210N lists 175 kt maximum at sea level and 168 kt cruise at 75% power at 6500 ft. Range is 765 NM at 75% power, or 1025 NM at 10000 ft for maximum range. Both include a 45-minute reserve.

What can a CESSNA 210N carry?

The 1984 handbook for the CESSNA 210N gives a 3800 lb takeoff weight, 3812 lb ramp weight and 1639 lb useful load (Centurion). Baggage is 240 lb maximum with four people. The library lists 3600 lb instead, so check your airplane's handbook.

Why do the CESSNA 210N figures differ between sources?

The library entry for the CESSNA 210N gives 3600 lb, 65 gal fuel, an IO-520-U engine and 700 NM range. The 1984 handbook gives 3800 lb, 90 gal, an IO-520-L engine and 765 NM. Use the handbook supplied with the specific airplane.

Can a standby alternator be fitted to a CESSNA 210N?

Yes, for listed serials. The B&C STC covers CESSNA 210N serials 21062955 through 21064897 (1979 to 1984 models). It provides 20 amps if the primary alternator fails and moves the vacuum pump to the left accessory drive pad.

What is the CESSNA 210N Model Guide?

The CESSNA 210N Model Guide is a model guide for the CESSNA 210N, dated 2026.

What year was the CESSNA 210N Model Guide published?

The CESSNA 210N Model Guide — the CESSNA 210N model guide on file — is dated 2026.

How rare is it?
4,518CESSNA 210N registered worldwide · 4,487 active

Common. More common than 99% of the aircraft models we track.

Documentation completeness
3/7

Most owners only have the POH. Here's the essential set for the CESSNA 210N.

More CESSNA 210Nmanuals & documents

In this document

Verify before you buy

Library data and the 1984 handbook disagree. The library lists a 3600 lb maximum takeoff weight, 65 gal fuel, IO-520-U engine and 700 NM range. The handbook lists 3800 lb, 90 gal total fuel, IO-520-L and 765 NM. Confirm the engine model, fuel capacity and weight limits against the airplane's own handbook. The owner is responsible for keeping it current.

Upgrades and avionics

The B&C standby alternator (STC SA00846WI) is approved for 210N serials 21062955 through 21064897, the 1979 to 1984 models. It is rated at 20 amps and was listed at $2300 for the alternator and regulator plus $550 for the install kit. The S-TEC System 55 autopilot supplement limits use to 165 KIAS or less and flaps of 10 degrees or less. The autopilot must be off for takeoff and landing, and it is Category I only.

Family context only

The registry covers the whole Cessna 210 family, including the 210N, T210N and P210N. Across the family it shows up to 204 kt cruise, 1240 NM range, 28000 ft ceiling and 6 passengers. These are family maximums and are not CESSNA 210N figures.

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

  • ATSB: a CESSNA 210N landed gear-up at Broome in 2016 with no injuries. The pilot may have run the checklist only mentally and wore a noise-cancelling headset.
  • Autopilot malfunction: take control, overpower if needed, disconnect, and do not re-engage until the fault is fixed. No go-around or missed approach on autopilot.

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 210N Model Guide The CESSNA 210N is a retractable-gear, single-engine piston Cessna with a fuel-injected Continental engine (285 hp continuous, 300 hp for the takeoff rating) and a three-blade constant-speed propeller. The 1984 handbook lists 175 kt maximum speed, 168 kt cruise at 75% power and 765 NM range. Library data differs in places, so check the figures against the airplane's own handbook. • 1984 handbook: 175 kt max, 168 kt cruise at 75% power, 765 NM range with 45-minute reserve, 950 fpm climb, 17300 ft service ceiling. • Weights: 3800 lb takeoff, 3812 lb ramp, 1639 lb useful load (Centurion), 240 lb baggage with four people. Library data lists 3600 lb. • Takeoff: 1250 ft ground roll, 2030 ft over 50 ft. Landing: 765 ft roll, 1500 ft over 50 ft (standard day, hard runway, no wind). • The gear is retractable and a wheels-up landing is on record. The warning horn sounds below about 12 inches of manifold pressure. Verify before you buy Library data and the 1984 handbook disagree. The library lists a 3600 lb maximum takeoff weight, 65 gal fuel, IO-520-U engine and 700 NM range. The handbook lists 3800 lb, 90 gal total fuel, IO-520-L and 765 NM. Confirm the engine model, fuel capacity and weight limits against the airplane's own handbook. The owner is responsible for keeping it current. Upgrades and avionics The B&C standby alternator (STC SA00846WI) is approved for 210N serials 21062955 through 21064897, the 1979 to 1984 models. It is rated at 20 amps and was listed at $2300 for the alternator and regulator plus $550 for the install kit. The S-TEC System 55 autopilot supplement limits use to 165 KIAS or less and flaps of 10 degrees or less. The autopilot must be off for takeoff and landing, and it is Category I only. Family context only The registry covers the whole Cessna 210 family, including the 210N, T210N and P210N. Across the family it shows up to 204 kt cruise, 1240 NM range, 28000 ft ceiling and 6 passengers. These are family maximums and are not CESSNA 210N figures. Safety notes: • ATSB: a CESSNA 210N landed gear-up at Broome in 2016 with no injuries. The pilot may have run the checklist only mentally and wore a noise-cancelling headset. • Autopilot malfunction: take control, overpower if needed, disconnect, and do not re-engage until the fault is fixed. No go-around or missed approach on autopilot.