CESSNA TURBO 210L Model Guide
CESSNA TURBO 210L · Model Guide
Overview
The CESSNA TURBO 210L is a single-engine piston Cessna 210 Centurion variant. Listed figures are a 3800 lb maximum takeoff weight, 90 gal of fuel and a maximum speed of 225 kts. The type acceptance report allows up to 6 seats for this model group. Library data lists a Continental IO-520-L at 325 hp, so confirm the engine actually fitted to any aircraft you inspect.
- Maximum takeoff weight is 3800 lbs and basic empty weight is 2150 lbs. It carries 90 gal of fuel and has a 200 lb baggage allowance.
- Listed speeds: Vne 225 kts, Vno 210 kts, Vy 90 kts, Vx 75 kts. Clean stall is 75 kts and max crosswind is 15 kts.
- Confirm the engine: the library says IO-520-L at 325 hp, but the type acceptance report lists TSIO-520-H for the T210L.
- Ask for proof of the mandatory carry-thru spar eddy current inspection (SEL-57-06).
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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) ·
- 325
- Height (ft) ·
- 9.42
- Length (ft) ·
- 28.15
- Wingspan (ft) ·
- 36.75
- Max speed (kt) ·
- 225
- Fuel capacity (gal) ·
- 90
- Max takeoff weight (lb) ·
- 3,800
Performance
- Max speed (kt) ·
- 225
- Max crosswind (kt) ·
- 15
- Baggage allowance (lb) ·
- 200
- Stall speed clean (kt) ·
- 75
- Stall speed landing (kt) ·
- 65
V-speeds
- VX_KTS ·
- 75
- VY_KTS ·
- 90
- VNE_KTS ·
- 225
- VNO_KTS ·
- 210
- VSO_KTS ·
- 60
Weight & balance
- Fuel capacity (gal) ·
- 90
- Baggage allowance (lb) ·
- 200
- Basic empty weight (lb) ·
- 2,150
- Max takeoff weight (lb) ·
- 3,800
How much can the CESSNA TURBO 210L take off with?
The CESSNA TURBO 210L has a maximum takeoff weight of 3800 lbs and a listed basic empty weight of 2150 lbs. It carries 90 gal of fuel and has a 200 lb baggage allowance. Weigh the actual aircraft for a true useful load.
What are the key speeds?
For the CESSNA TURBO 210L the library lists Vne 225 kts, Vno 210 kts, Vy 90 kts and Vx 75 kts. Clean stall is 75 kts and maximum crosswind is 15 kts.
Which engine does it have?
The library lists a Continental IO-520-L at 325 hp for the CESSNA TURBO 210L. The type acceptance report lists TSIO-520-H for the T210L, so verify the engine on the data plate and in the logbooks.
What mandatory inspections apply?
For the CESSNA TURBO 210L, SEL-57-06 requires a carry-thru spar eddy current inspection. SEB92-27 covers vented fuel caps and turbo placard removal. Ask for logbook proof of both.
What is the CESSNA TURBO 210L Model Guide?
The CESSNA TURBO 210L Model Guide is a model guide for the CESSNA TURBO 210L, dated 2026.
What year was the CESSNA TURBO 210L Model Guide published?
The CESSNA TURBO 210L Model Guide — the CESSNA TURBO 210L 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 TURBO 210L.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
CESSNA TURBO 210L for sale now
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More CESSNA TURBO 210Lmanuals & documents
See all 20 →- Alert Service Bulletin No. 210 Turbocharger Turbine Housing InspectionService Bulletins
- Cessna Turbo 210L Service BulletinService Bulletins
- OWNER/OPERATOR INFORMATION MANUALMaintenance Manual
- Service Bulletin: SB-001 Rev BService Bulletins
- Weight and Balance - Cessna 210N / Sn 210-63828Weight & Balance
- Type Acceptance Report TAR 4/21B/25 – Cessna 210 SeriesType Certificate
- WINGS - MODEL 210 CARRY-THRU SPAR ONE-TIME EDDY CURRENT INSPECTIONService Bulletins
- Savvy-Cessna-210-prebuy-checklist.pdfChecklist
- Legacy 210 (1960-1971 models) SYSTEMS & PROCEDURES COURSEMaintenance Manual
- MSB08-5 - Continental Aerospace TechnologiesService Bulletins
- CENTURION SERIES SERVICE MANUALMaintenance Manual
- TYPE CERTIFICATE DATA SHEET NO. 3A21Type Certificate
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In this document
Engine and propeller
The library lists a Continental IO-520-L at 325 hp with a McCauley E2A34C73/90AT-8 propeller. The 1972 handbook covering the 210L rates 300 BHP at 2850 RPM for 5 minutes and 285 BHP at 2700 RPM continuous. The type acceptance report lists TSIO-520-H for the T210L. Check the engine data plate and logbooks to confirm which engine is fitted.
Airframe and loading
Wingspan is 36.75 ft, length 28.15 ft and height 9.42 ft. Basic empty weight is 2150 lbs against a 3800 lb maximum takeoff weight, with 90 gal of fuel and a 200 lb baggage allowance. The type acceptance report shows up to 6 seats. Work out useful load from the actual aircraft's weighed empty weight.
Records to request
Ask for proof of the SEL-57-06 carry-thru spar eddy current inspection (mandatory; covers 210L and T210L). SEB92-27 vented fuel caps were mandatory within 400 hours or 12 months, and external turbo placards are to be removed. If a Stratus oil filter adapter is fitted, ask about SB-001 Rev B.
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Safety notes
- The carry-thru spar can corrode and crack, risking wing separation. The inspection is due over 1,500 flight hours (severe use) or 4,000 (typical). Unknown history counts as severe.
- Take fuel samples from every drain at each preflight and check the fuel vents. Blocked vents or wrong or contaminated fuel can cause engine stoppage in flight.
- If a Stratus oil filter adapter is fitted, inspect for fiber gaskets, leaks or looseness. Oil loss can lead to partial or complete loss of engine power.
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 TURBO 210L Model Guide The CESSNA TURBO 210L is a single-engine piston Cessna 210 Centurion variant. Listed figures are a 3800 lb maximum takeoff weight, 90 gal of fuel and a maximum speed of 225 kts. The type acceptance report allows up to 6 seats for this model group. Library data lists a Continental IO-520-L at 325 hp, so confirm the engine actually fitted to any aircraft you inspect. • Maximum takeoff weight is 3800 lbs and basic empty weight is 2150 lbs. It carries 90 gal of fuel and has a 200 lb baggage allowance. • Listed speeds: Vne 225 kts, Vno 210 kts, Vy 90 kts, Vx 75 kts. Clean stall is 75 kts and max crosswind is 15 kts. • Confirm the engine: the library says IO-520-L at 325 hp, but the type acceptance report lists TSIO-520-H for the T210L. • Ask for proof of the mandatory carry-thru spar eddy current inspection (SEL-57-06). Engine and propeller The library lists a Continental IO-520-L at 325 hp with a McCauley E2A34C73/90AT-8 propeller. The 1972 handbook covering the 210L rates 300 BHP at 2850 RPM for 5 minutes and 285 BHP at 2700 RPM continuous. The type acceptance report lists TSIO-520-H for the T210L. Check the engine data plate and logbooks to confirm which engine is fitted. Airframe and loading Wingspan is 36.75 ft, length 28.15 ft and height 9.42 ft. Basic empty weight is 2150 lbs against a 3800 lb maximum takeoff weight, with 90 gal of fuel and a 200 lb baggage allowance. The type acceptance report shows up to 6 seats. Work out useful load from the actual aircraft's weighed empty weight. Records to request Ask for proof of the SEL-57-06 carry-thru spar eddy current inspection (mandatory; covers 210L and T210L). SEB92-27 vented fuel caps were mandatory within 400 hours or 12 months, and external turbo placards are to be removed. If a Stratus oil filter adapter is fitted, ask about SB-001 Rev B. Safety notes: • The carry-thru spar can corrode and crack, risking wing separation. The inspection is due over 1,500 flight hours (severe use) or 4,000 (typical). Unknown history counts as severe. • Take fuel samples from every drain at each preflight and check the fuel vents. Blocked vents or wrong or contaminated fuel can cause engine stoppage in flight. • If a Stratus oil filter adapter is fitted, inspect for fiber gaskets, leaks or looseness. Oil loss can lead to partial or complete loss of engine power.