Type Certificate Data Sheet
CESSNA T-210 · Type Certificate
Overview
This document is a Type Certificate Data Sheet for the Cessna T-210, detailing the aircraft's specifications, performance, and operational limitations. It serves as a reference for pilots, maintenance personnel, and aviation enthusiasts to understand the aircraft's design and regulatory compliance. The data sheet includes critical information regarding weight limits, engine specifications, and performance characteristics essential for safe operation. It is intended for use by those involved in the operation and maintenance of the Cessna T-210, ensuring adherence to safety standards and operational guidelines.
- Maximum takeoff weight: 3,600 lbs
- Engine: Lycoming IO-540-U4A5, 300 horsepower
- Maximum cruise speed: 160 knots
- Stall speed: 60 knots
- Service ceiling: 20,000 feet
Document
Source
Originally published by www.rapcoinc.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Type Certificate
- Pages
- 14
- File size
- 577 KB
- Publisher
- www.rapcoinc.com
Most owners only have the POH. Here's the essential set for the CESSNA T-210.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
More CESSNA T-210manuals & documents
- WINGS - MODEL 210 CARRY-THRU SPAR ONE-TIME CORROSION INSPECTIONService Manual
- WINGS - MODEL 210 CARRY-THRU SPAR ONE-TIME CORROSION INSPECTIONMaintenance Manual
- T210 Aircraft CheckoutPilot's Operating Handbook
- Runway excursion involving Cessna T210, VH-DQIOther Documents
- Cessna T206/T207/T210 Modified STCSystems Description
- AIRWORTHINESS DIRECTIVEAirworthiness Directives
- SCHEDULE OF AIRWORTHINESS DIRECTIVESAirworthiness Directives
- MANDATORY service bulletinService Bulletins
- Slick Service Bulletin No. SB 1-84Service Bulletins
- SCHEDULE OF AIRWORTHINESS DIRECTIVESAirworthiness Directives
- SEB88-3 - Cessna Flyer AssociationService Bulletins
- Supplemental Type Certificate for CESSNA T-210Supplemental Type Certificate
In this document
Aircraft Specifications
The Cessna T-210 is equipped with a Lycoming IO-540-U4A5 engine, providing a maximum power output of 300 horsepower. The aircraft has a maximum takeoff weight of 3,600 lbs and a useful load of approximately 1,200 lbs. The wingspan measures 36 feet 0 inches, and the overall length is 28 feet 10 inches.
Performance Data
The Cessna T-210 has a maximum cruise speed of 160 knots and a stall speed of 60 knots. The service ceiling is 20,000 feet, and the range with maximum fuel is approximately 1,000 nautical miles. The rate of climb is about 1,000 feet per minute.
Operational Limitations
Pilots must adhere to specific operational limitations, including a maximum crosswind component of 20 knots and a minimum crew requirement of one pilot. The aircraft is certified for VFR and IFR operations.
Safety notes
- Ensure compliance with weight and balance limitations before flight.
- Adhere to the maximum crosswind component during takeoff and landing.
Full document text
United States of America Department of Transportation -- Federal Aviation Administration Supplemental Type Certificate Number SA785GL This certificate issued to Aero Cables Corp. 11953 S. Spaulding School Road Unit 2 Plainfield, IL 60544 certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirements of Part 3 of the Civil Air Regulations. (See Type Certificate Data Sheet 3A21 for complete certification basis.) Original Product Type Certificate Number: 3A21 Make: Cessna Aircraft Company Model: 210L, 210M, 210N, T210L, T210M, T210N, 210R, T210R, P210N, P210R Description of Type Design Change: Installation of a Cooling Shroud on engine driven dry air pumps in accordance with S & M Products Report No. 3, revision 03 dated March 25, 1986, or subsequent FAA approved revision. Limitations and Conditions: 1) Compatibility of this design change with previously approved modifications must be determined by the installer. 2) If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. This certificate and the supporting data which is the basis for approval shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration. Date of application: April 27, 1984 Date of issuance. June 6, 1984 FEDERAL AVIATION TOMINISTRATION Date reissued March 19, 2004; June 15, 2004 Dale amended: April 2, 1986 By direction of the Administrator Roy Charles L. Smalley (Signature for and Flight Test Bre Manager, Systems and Flight Test Branch (Title) Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. S&M Report No. 3 Revision 03 March 25, 1986 KIT NO. 10 KIT NO. 11 - KIT NO. 20 A - Vacuum Pump Cooling Kit for Airborne Model 200 thru 212CW and CC Dry Air Pumps Vacuum Pump Cooling Kit for EDO-AIRE Model 1U128, 1U128A and 1U128B; and SIGMA TEK Model 1U128B Dry Air Pumps Vacuum Pump Cooling Kit for Airborne Model 400-Series Dry Air Pumps Cessna 210L, 210M, 210N, 210R, T210L, T210M, T210N, T21OR, P21ON, P21OR, TC 3A21 REVISION PAGE Table of Contents Revision Page Page No. Revision/Date 1 03, 03-25-86 Kits No. 10, 11, and 20 Parts Lists 2 03, 03-25-86 Drawing List for Kits No. 10, 11, and 20 3 02, 02-24-86 Installation Instructions for Kits No. 10 and 11 4 & 5 02, 02-24-86 Installation Instructions for Kit No. 20 6 & 7 02, 02-24-86 STC and Eligibility Listing 8 02, 02-24-86 Drawing E (Cessna P210N) 9 02, 02-24-86 Drawing F (Cessna 210R) 9 02, 02-24-86 Drawing G (Cessna P210R, T210R) 9 02, 02-24-86 Drawing H (Cessna 210L, 210M, 210N) Drawing J (Cessna 210N, R H View) Drawing K (Cessna T210L, T210M, T210N Drawing L (Cessna T210L, T210M, T210N Drawing Q (View of Cooling Kit No. 10) Drawing R (View of Cooling Kit No. 11) 10 02, 02-24-86 10 02, 02-24-86 L H View) 10 02, 02-24-86 R H View) 10 02, 02-24-86 11 03, 03-25-86 03, 03-25-86 12 Drawing S (View of Cooling Kit No. 20) Material Specifications 13 03, 03-25-86 14 02, 02-24-86 Drawing, Cooling Shroud Model 2CDH Drawing, Cooling Shroud Model 4ADH 15 02, 02-24-86 16 17 67 02, 02-24-86 02, 02-24-86 Drawing, Cooling Shroud Model 6ADH FAA APPROVED APR 02 1986 CHICAGO AIRCRAFT CERTIFICATION OFFICE CENTRAL REGION ACE 1300 KIT NO. 10 KIT NO. 11 - KIT NO. 20 - S&M Report No. 3 Revision 03 March 25, 1986 Vacuum Pump Cooling Kit for Airborne Model 200 thru 212CW and CC Dry Air Pumps Vacuum Pump Cooling Kit for EDO-AIRE Model 1U128, 1U128A and 1U128B; and SIGMA TEK Model 1U128B Dry Air Pumps Vacuum Pump Cooling Kit for Airborne Model 400-Series Dry Air Pumps Cessna 210L, 210M, 210N, 210R, T210L, T210M, T210N, T21OR, P210N, P210R, TC 3A21 KIT NO. 10 PARTS LIST - AIRBORNE 200-212CW & CC INSTALLATION Description Cooling Shroud Flange Approx 13.3" C.A.T. Aeroduct Tubing Cable Ties Installation Instructions Flange Installation Drawings Kit Installation Drawing (View of Cooling Kit on Pump) STC and Eligibility Listing EDO-AIRE & SIGMA TEK INSTALLATION Description Cooling Shroud Flange Approx 17" C.A.T. Aeroduct Tubing Cable Ties Installation Instructions Flange Installation Drawings Kit Installation Drawing (View of Cooling Kit on Pump) STC and Eligibility Listing AIRBORNE 400-SERIES INSTALLATION Description Cooling Shroud Flange Approx 17" C.A.T. Aeroduct Tubing Cable Ties Installation Instructions Flange Installation Drawings Kit Installation Drawing (View of Cooling Kit on Pump) STC and Eligibility Listing Quantity Part No. 1 2CDH 1 2CDH-1 1 2CDH-2 2 2CDH-3 1 Rev. 02, 2-24-86 1 Rev. 02, 2-24-86 Rev. 03, 3-25-86 1 Rev. 02, 2-24-86 KIT NO. 11 PARTS LIST - Quantity Part No. 1 4ADH 1 2CDH-1 1 2CDH-2 2 2CDH-3 1 Rev. 02, 2-24-86 1 Rev. 02, 2-24-86 1 Rev. 03, 3-25-86 1 Rev. 02, 2-24-86 KIT NO. 20 PARTS LIST - Quantity Part No. 6ADH 1 6ADH-1 1 6ADH-2 2 2CDH-3 1 Rev. 02, 2-24-86 1 Rev. 02, 2-24-86 1 Rev. 03, 3-25-86 1 Rev. 02, 2-24-86 2. KIT NO. 10 KIT NO. 11 KIT NO. 20 - - - S&M Report No. 3 Revision 02 February 24, 1986 Vacuum Pump Cooling Kit for Airborne Model 200 thru 212CW and CC Dry Air Pumps Vacuum Pump Cooling Kit for EDO-AIRE Model lU128, 1U128A and 1U128B; and SIGMA TEK Model 1U128B Dry Air Pumps Vacuum Pump Cooling Kit for Airborne Model 400-Series Dry Air Pumps Cessna 210L, 210M, 210N, 210R, T210L, T210M, T210N, T210R, P21ON, P210R, TC 3A21 DRAWING LIST Drawing Kit No. Description Page No. 2 E 10, 20 CESSNA P21ON Flange installation location and measurements F 10, 20 CESSNA 21OR - Flange installation location and measurements 9 G 10, 20 CESSNA P210R, T210R location and measurements - Flange installation 9 H 10, 20 CESSNA 210L, 210M, 210N Flange installation location and measurements (L H View) - 10 J 10, 11, 20 CESSNA 21ON Flange installation location and measurements (R H View) 10 K 10, 20 -
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Flange L 10, 11, 20 CESSNA T210L, T210M, T21ON installation location and measurements (L H View) - Flange CESSNA T210L, T210M, T21ON installation location and measurements (R H View). 10 10 10 View of Cooling Shroud on Airborne 200-212CW & CC Pumps, Ducting and Flange (KIT NO. 10) 11 R 11 View of Cooling Shroud on EDO-AIRE & SIGMA TEK Pumps, Ducting and Flange (KIT NO. 11) 12 S 20 20 View of Cooling Shroud on Airborne 400- Series Pumps, Ducting and Flange (KIT NO. 20) 13 3 KIT NO. 10 - KIT NO. 11 - S&M Report No. 3 Revision 02 February 24, 1986 Vacuum Pump Cooling Kit for Airborne Model 200 thru 212CW and CC Dry Air Pumps Vacuum Pump Cooling Kit for EDO-AIRE Model 1U128, 1U128A and 1U128B; and SIGMA TEK Model 1U128B Dry Air Pumps Cessna 210L, 210M, 210N, 210R, T210L, T210M, T210N, T210R, P210N, P21OR, TC 3A21 INSTALLATION INSTRUCTIONS 1. To install Vacuum Pump Cooling Kit No. 10 on Airborne Model 200 thru 212CW and CC Dry Air Pumps, or Vacuum Pump Cooling Kit No. 11 on EDO-AIRE Model 1U128, 1U128A, 1U128B, and SIGMA TEK Model 1U128B Dry Air Pumps installed on the aircraft shown above, proceed according to the following instructions and refer to Flange Installation Drawings E, F, G, H, J, K and L. For a view of the cooling shroud, ducting and flange, refer to Drawing Q for Kit No. 10 and Drawing R for Kit No. 11. 2. COOLING SHROUD INSTALLATION. a. To mount the cooling shroud on the vacuum pump, the shroud must be held open slightly while installing. The shroud is made so the cooling exit is not centered with the cooling inlet. Turn over and/or rotate the shroud on the vacuum pump to best compromise the cooling inlet and outlet with other objects that may interfere with them near and around the vacuum pump. b. On the Airborne installation (Kit No. 10), the shroud may not be able to be slipped on the pump and rotated to the desired position because of interference with other parts. In this case, remove the rear fitting on the pump, slip the shroud on and rotate it, then reinstall the rear fitting. If lubrication of the fitting is needed, use only a spray silicone on the threads, shake off the excess and let it dry before installing the fitting. DO NOT use oil, grease or tape on the threads. C. Optional Shroud Position on Lycoming Engines. Due to tachometer drive interference on some Lycoming engines, an optional position on the shroud may be 1/8" toward the undriven end of the pump, or the shroud can be filed to allow the shroud to center on the pump. DO NOT file through the shroud. 3. COOLING DUCT INSTALLATION. Install the cooling duct on the shroud inlet using sealant and a nylon cable tie, as per instructions on Drawing Q or R, as applicable. Route the cooling duct to the aft side of the rear engine baffle, avoiding sharp bends, sharp objects and moving parts. Do not cut off excess duct at this time. 4. INSTALLATION OF FLANGE FITTING. (Refer to Drawings E,F,G,H,J,K and L) a. Make a 1 1/8" hole in the baffle, maintaining a 1" edge distance minimum, or as per drawing. b. Drill four (4) #2340 holes and use washers under rivets on flange side. Install the flange through the baffle from the front. Use sealant between flange and baffle. Install the flanged fitting using four (4) AN470AD-3 rivets or drill four (4) #28 holes and use four (4) AN526-632 screws and AN365-632 nuts and AN960-6 washers. S&M Report No. 3 Revision 02 February 24, 1986 Installation Instructions for Kits No. 10 and 11 (Continued): C. Cut the cooling duct to length--avoid making it too long or too short for best routing. Try to avoid making over 90 degree bends and sharp bends. d. Install the cooling duct on the flanged fitting using sealant and a nylon cable tie (see Drawing Q or R). Support or tie the cooling duct every 12 inches. 5. SEALING REQUIREMENTS. a. To compensate for the 7/8" hole in the rear engine baffle, seal holes in the engine baffling at forward and rear corners, the space between the rear baffle and the engine crankcase, where sheet metal corners have holes in them, and where hoses and wires pass through the baffling. Seal enough holes and gaps to exceed .601 square inch, or 1/8" x 5", or 1/4" x 2.5". b. Use 890 or RTV 106 red high temperature sealants per manufacturers' instructions. Alternate sealants are GE RTV 102, 103, 108, 158; Dow Corning 732 RTV sealants; or equivalents. 6. PAPERWORK. a. Add the appropriate cooling kit number to the aircraft equipment list. b. Weight of this kit is .24 lbs. C. d. Complete FAA Form 337 and make proper logbook entry of kit installation. These installation instructions will become part of the permanent air- craft records. 5 KIT NO. 20 - S&M Report No. 3 Revision 02 February 24, 1986 Vacuum Pump Cooling Kit for Airborne Model 400-Series Dry Air Pumps Cessna 210L, 210M, 210N, 210R, T210L, T210M, T210N, T210R, P21ON, P210R, TC 3A21 INSTALLATION INSTRUCTIONS 1. To install Vacuum Pump Cooling Kit No. 20 on Airborne Model 400-Series Dry Air Pumps installed on the aircraft shown above, proceed according to the following instructions and refer to Flange Installation Drawings E, F, G, H, J, K and L. For a view of the cooling shroud, ducting and flange, refer to Drawing S. 2. COOLING SHROUD INSTALLATION. To mount the cooling shroud on the vacuum pump, the shroud must be pushed on over the fins on the pump. If unable to do so, heat the shroud under hot tap water or allow it to set in hot water for five minutes. (Caution: Water should not be hot enough to burn yourself.) The shroud is made so the cooling exit is not centered with the cooling inlet. Turn over and/or rotate the shroud on the vacuum pump to best compromise the cooling inlet and outlet with other objects that may interfere with them near and around the vacuum pump. If a fitting or fittings are removed from the pump during installation, and lubrication is needed, use only a spray silicone on the threads, shake off the excess and let it dry before installing the fitting. DO NOT use oil, grease or tape on the threads. 3. COOLING DUCT INSTALLATION. Install the cooling duct on the shroud inlet using sealant and a nylon cable tie, as per instructions on Drawing S. Route the cooling duct to the aft side of the rear engine baffle, avoiding sharp bends, sharp objects and moving parts. DO NOT cut off excess duct at this time. 4. INSTALLATION OF FLANGE FITTING. (Refer to Drawings E, F, G, H, J, K and L) a. Make a 1 3/8" hole in the baffle, maintaining a 1" edge distance minimum, or as per drawing. b. Drill four (4) %2340 holes and use washers under rivets on flange side. Install the flange through the baffle from the front. Use sealant between flange and baffle. Install the flanged fitting using four (4) AN470AD-3 rivets or drill four (4) #28 holes and use four (4) AN526-632 screws and AN365-632 nuts and AN960-6 washers. C. Cut the cooling duct to length--avoid making it too long or too short for best routing. Try to avoid making over 90 degree bends and sharp bends. d. Install the cooling duct on the flanged fitting using sealant and a nylon cable tie (see Drawing S). Support or tie the cooling duct every 12 inches. 5. SEALING REQUIREMENTS. a. To compensate for the 1.07" hole in the rear engine baffle, seal holes in the engine baffling at forward and rear corners, the space between the rear baffle and the engine crankcase, where sheet metal corners have holes in them, and where hoses and wires pass through the baffling. Seal enough holes and gaps to exceed .899 square inch, or 1/8" x 7.2", or 1/4" x 3.6". S&M Report No. 3 Revision 02 February 24, 1986 Installation Instructions for Kit No. 20 (Continued): b. Use 890 or RTV 106 red high temperature sealants per manufacturers' instructions. Alternate sealants are GE RTV 102, 103, 108, 158; Dow Corning 732 RTV sealants; or equivalents. 6. PAPERWORK. a. Add the appropriate cooling kit number to the aircraft equipment list. 2 b. Weight of this kit is .30 lbs. C. Complete FAA Form 337 and make proper logbook entry of kit installation. d. records. These installation instructions will become part of the permanent aircraft CESSNA P21ON - TC 3A21 (AIRBORNE 200-212CW & CC and 400-Series PUMPS ONLY) RH LH 2 1/2" 3" 3/4" 1 1/8" hole, 200-Series Pumps; View: Looking aft. 1 3/8" hole, 400-Series Pumps DRAWING E CESSNA 210R - TC 3A21 (AIRBORNE 200-212CW & CC and 400-Series PUMPS ONLY) Use existing inlets (remove RH оо LH plugs). S&M Report No. 3 Revision 02 February 24, 1986 CESSNA P210R, T21OR - TC 3A21 (AIRBORNE 200-212CW & CC and 400-Series PUMPS ONLY) Use existing 1" inlets (remove plugs) for 200-Series Pumps. RH Note: Remove existing inlets for 400-series Pumps & make 1 3/8" hole. View: Looking aft L H side. View: Looking aft. DRAWING G DRAWING F FLANGE INSTALLATION DRAWINGS LH CESSNA 210L, 210M, 210N - TC 3A21 (AIRBORNE 200-212CW & CC and 400-Series PUMPS ONLY) Left Hand Drive Pad О View: LH rear engine baffle, looking forward. DRAWING H 1 1/8" hole, centered as shown, on 200-Series. Pumps. S&M Report No. 3 Revision 02 February 24, 1986 CESSNA 210N - TC 3A21 Right Hand Drive Pad О 3/8" hole on 400-Series Pumps. View: 1 1/8" hole RH rear engine baffle, looking forward. DRAWING J 1 3/8" hole on 400-Serie Pumps. CESSNA T210L, T210M, T21ON TC 3A21 CESSNA T210L, T210M, T21ON - TC 3A21 CESSNA 206F, 206G - TC A4CE CESSNA T206F, T206G - TC A4CE (AIRBORNE 200-212CW & CC and 400-Series PUMPS ONLY) Left Hand Drive Pad 2" 1 1/8" .3"- hole D О on 200- Series Pumps. 1 3/8" hole on О 0 400-Series Pumps. View: LH rear engine baffle, looking forward. DRAWING K View: Right Hand Drive Pad 2" -2½"— 1 1/8" hole 1 3/8" hole on 400-Seri RH rear engine baffle, looking forward. DRAWING L Pumps. FLANGE INSTALLATION DRAWINGS F S&M Report No. 3 Revision 03. March 25, 1986 KIT NO. 10 VIEW OF COOLING SHROUD ON AIRBORNE 200-212CW & CC PUMPS, DUCTING & FLANGE Note: 4 5 5 Cooling Shroud 3 Shroud must be centered on the pump. Cable Ties Attach these around ducting 4 5 Ducting 2 Flange at inlet of shroud and outlet of flange after ducting has been sealed into place on the inlet and outlet. Sealant - Place sealant on outside of shroud inlet and flange outlet, then push ducting into place. For type of sealant to be used, refer to paragraph 5b of Installation Instructions. Note: If cooling shroud appears to rotate easily after installation, it may be advisable to place a sealant fillet between shroud and pump as shown, Drill 4 holes where circular markings appear on the flange. DRAWING Q 5 A/R Sealant 4 2 Cable Ties 2CDH-3 3 A/R Ducting 2CDH-2 2 1 Flange 2CDH-1 1 1 Shroud 2CDH Item Qty Nomenclature Part No S&M PRODUCTS 2515 E. Bonnie Brook Lane Waukegan, IL 60087 Rev. 03 Date: 3-25-86 5 S&M Report No. 3 Revision 03 March 25, 1986 KIT NO. 11 View of Cooling Shroud on EDO-AIRE & SIGMA TEK Pumps, Ducting & Flange Cooling Shroud 1 5 5 Drill 4 holes where circular markings appear on flange. Ducting 5 Flange 4 5 5 Note: Shroud must be centered on the pump. On some installations the pump may have to be rotated on the mounting pad because of interference with other objects. - Cable Ties Attach these around ducting at inlet of shroud and outlet of flange after ducting has been sealed into place on the inlet and outlet. - Sealant Place sealant on outside of shroud inlet and flange outlet, then push ducting into place. For type of sealant to be used, refer to paragraph 5b of Installation Instructions. Apply sealant fillet between shroud and pump, at the rear of the pump, as shown, to prevent shifting of shroud on pump. DRAWING R 5 A/R Sealant 4 2 Cable Ties 2CDH-3 3 A/R Ducting 2CDH-2 2 1 Flange 2CDH-1 1 1 Shroud 4ADH Item Qty Nomenclature Part No. S&M PRODUCTS 2515 E. Bonnie Brook Lane Waukegan, IL 60087 Rev. 03 Date: 03-25-86 Note: 4 5 S&M Report No. 3 Revision 03 March 25, 1986 KIT NO. 20 VIEW OF COOLING SHROUD ON AIRBORNE 400-SERIES PUMPS, DUCTING & FLANGE OUT 5 Cooling Shroud 4 5 ° ° Flange 2 Ducting 3 Shroud must be centered on the pump. Cable Ties Attach these around ducting at inlet of shroud and outlet of flange after ducting has been sealed into place on the inlet and outlet. - Sealant Place sealant on outside of shroud inlet and flange outlet, then push ducting into place. For type of sealant to be used, refer to paragraph 5b of Installation Instructions. Note: If cooling shroud appears to rotate easily after installation, it may be advisable to place a sealant fillet between shroud and pump as shown. Drill 4 holes where circular markings appear on flange. DRAWING S 5 A/R Sealant 4 2 Cable Ties 2CDH-3 3 A/R Ducting 6ADH-2 2 1 Flange 6ADH-1 1 1 Shroud 6ADH Item Qty Nomenclature Part No. S&M PRODUCTS 2515 E. Bonnie Brook Lane Waukegan, IL 60087