CESSNA P-210 Pressurized Centurion II Model Guide
CESSNA P-210 Pressurized Centurion II · Model Guide
Overview
The CESSNA P-210 Pressurized Centurion II is a turbocharged, pressurized, single-engine piston airplane that seats six including the pilot. Most figures here come from a June 1978 AOPA Pilot flight check of an early P210, listed as a P210N. Later airplanes may differ, so confirm each figure against the POH for the airframe you are buying.
- Normal cruise is 196 kt at 80% power at 20,000 ft, with 815 nm range and 45-min reserve. Certified ceiling is 23,000 ft (1978 data).
- Gross weight is 4,000 lb, empty weight 2,345 lb, useful load 1,671 lb. Fuel is 90 gal (89 usable), and the baggage limit is 200 lb.
- Cabin pressure depends on turbocharger boost. Keep manifold pressure near 20 in or above, and never let a tank run dry.
- Pilots new to pressurization were advised to expect a two- to three-hour systems briefing plus a three-hour in-flight checkup.
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 power (hp) ·
- 285
- Usable fuel (gal) ·
- 89
- Fuel capacity (gal) ·
- 90
- Propeller diameter (in) ·
- 80
Performance
- Max range (nm) ·
- 960
- Rate of climb (fpm) ·
- 930
- Service ceiling (ft) ·
- 23,000
- Max level speed (kt) ·
- 204
- Range normal cruise (nm) ·
- 815
- Takeoff ground roll (ft) ·
- 1,300
- Normal cruise speed (kt) ·
- 196
- Economy cruise speed (kt) ·
- 158
V-speeds
- STALL_CLEAN_KTS ·
- 67
- MAX_FLAP_10_SPEED_KTS ·
- 150
- STALL_GEAR_FLAPS_DOWN_KTS ·
- 58
- MAX_GEAR_EXTENDED_SPEED_KTS ·
- 140
Weight & balance
- Useful load (lb) ·
- 1,671
- Empty weight (lb) ·
- 2,345
- Gross weight (lb) ·
- 4,000
- Max ramp weight (lb) ·
- 4,016
- Baggage capacity (lb) ·
- 200
How fast and how far does it fly?
The CESSNA P-210 Pressurized Centurion II cruised at 196 kt at 80% power at 20,000 ft in the 1978 data. Range at normal cruise was 815 nm with a 45-minute reserve, and maximum range was 960 nm.
What can it carry?
The CESSNA P-210 Pressurized Centurion II seats six, with a useful load of 1,671 lb and a 200 lb baggage limit. Gross weight is 4,000 lb and maximum ramp weight is 4,016 lb.
What engine does it use?
The CESSNA P-210 Pressurized Centurion II in the 1978 flight check had a Continental TSIO-520-P rated at 285 hp, driving a three-blade McCauley constant-speed propeller 80 in in diameter.
How high can it fly?
The CESSNA P-210 Pressurized Centurion II is certified to 23,000 ft. Maximum pressure differential is 3.35 psi, which holds a 10,000 ft cabin at 20,000 ft.
What is the CESSNA P-210 Pressurized Centurion II Model Guide?
The CESSNA P-210 Pressurized Centurion II Model Guide is a model guide for the CESSNA P-210 Pressurized Centurion II, dated 2026.
What year was the CESSNA P-210 Pressurized Centurion II Model Guide published?
The CESSNA P-210 Pressurized Centurion II Model Guide — the CESSNA P-210 Pressurized Centurion II model guide on file — is dated 2026.
Most owners only have the POH. Here's the essential set for the CESSNA P-210 Pressurized Centurion II.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More CESSNA P-210 Pressurized Centurion IImanuals & documents
- 1985 Thru 1986 Model P210 Service ManualPilot's Operating Handbook
- Cessna's Pressurized CenturionPilot's Operating Handbook
- Performance Data for CESSNA P-210 Pressurized Centurion IIPerformance Data
- Cessna P210R Pressurized CenturionSpecifications
- Pilot's Operating Handbook Cessna P-210 Pressurized Centurion IIPilot's Operating Handbook
Related documents
- Cessna P210R Pressurized CenturionCESSNA P-210 Pressurized Centurion II · Specifications
- Cessna P210 Pressurized Centurion Model GuideCessna P210 Pressurized Centurion · Model Guide
- Cessna 210 Centurion Model GuideCessna 210 Centurion · Model Guide
- Cessna's Pressurized CenturionCESSNA P-210 Pressurized Centurion II · Pilot's Operating Handbook
- CESSNA 210 Model GuideCESSNA 210 · Model Guide
In this document
Performance and pressurization
Maximum pressure differential is 3.35 psi. At 20,000 ft the cabin can be held at 10,000 ft. The test airplane climbed to 20,000 ft in about 20 minutes. At 79% power (33 in, 2,500 rpm) it burned 19.2 gph for 198 kt true. At 55% power (25 in, 2,300 rpm) it burned 12.5 gph for 171 kt true.
What to check when buying
The 1985-86 P210R serial numbers run P21000835 to P21000874. The service manual's temporary revisions add a fuel injection nozzle cleaning interval, a Component Time Limits section and a fuel quantity indicating system operational test. Ask for records showing these were done. Inspect the single left main door, which has nine locking pins, and the half-size right emergency exit.
Handling and ownership notes
With two aboard and full fuel, a takeoff used almost 1,500 ft of a 3,800 ft runway, and the airplane felt heavy and a little sluggish. Plan descents early: ground speed in descent is 200 to 220 kt, so start about 80 miles out from 18,000 ft. Gear can be extended below 140 kt, and flaps at 10 degrees below 150 kt.
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
- Running a tank dry loses engine power and pressurization, and cabin altitude climbs abruptly.
- A quick cabin-altitude dial change or a large power reduction causes sudden ear pressure changes. Set cabin altitude above the destination field elevation before landing.
- The flight-check airplane had boots, prop heat and a windshield anti-ice plate but was not certified for flight in icing conditions.
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 P-210 Pressurized Centurion II Model Guide The CESSNA P-210 Pressurized Centurion II is a turbocharged, pressurized, single-engine piston airplane that seats six including the pilot. Most figures here come from a June 1978 AOPA Pilot flight check of an early P210, listed as a P210N. Later airplanes may differ, so confirm each figure against the POH for the airframe you are buying. • Normal cruise is 196 kt at 80% power at 20,000 ft, with 815 nm range and 45-min reserve. Certified ceiling is 23,000 ft (1978 data). • Gross weight is 4,000 lb, empty weight 2,345 lb, useful load 1,671 lb. Fuel is 90 gal (89 usable), and the baggage limit is 200 lb. • Cabin pressure depends on turbocharger boost. Keep manifold pressure near 20 in or above, and never let a tank run dry. • Pilots new to pressurization were advised to expect a two- to three-hour systems briefing plus a three-hour in-flight checkup. Performance and pressurization Maximum pressure differential is 3.35 psi. At 20,000 ft the cabin can be held at 10,000 ft. The test airplane climbed to 20,000 ft in about 20 minutes. At 79% power (33 in, 2,500 rpm) it burned 19.2 gph for 198 kt true. At 55% power (25 in, 2,300 rpm) it burned 12.5 gph for 171 kt true. What to check when buying The 1985-86 P210R serial numbers run P21000835 to P21000874. The service manual's temporary revisions add a fuel injection nozzle cleaning interval, a Component Time Limits section and a fuel quantity indicating system operational test. Ask for records showing these were done. Inspect the single left main door, which has nine locking pins, and the half-size right emergency exit. Handling and ownership notes With two aboard and full fuel, a takeoff used almost 1,500 ft of a 3,800 ft runway, and the airplane felt heavy and a little sluggish. Plan descents early: ground speed in descent is 200 to 220 kt, so start about 80 miles out from 18,000 ft. Gear can be extended below 140 kt, and flaps at 10 degrees below 150 kt. Safety notes: • Running a tank dry loses engine power and pressurization, and cabin altitude climbs abruptly. • A quick cabin-altitude dial change or a large power reduction causes sudden ear pressure changes. Set cabin altitude above the destination field elevation before landing. • The flight-check airplane had boots, prop heat and a windshield anti-ice plate but was not certified for flight in icing conditions.