Type Certificate Data Sheet for Cirrus SR22 G3
Cirrus SR22 G3 · Type Certificate
Overview
This document serves as the Type Certificate Data Sheet for the Cirrus SR22 G3, detailing the aircraft's specifications, performance, and compliance with regulatory standards. It is intended for use by pilots, maintenance personnel, and aviation enthusiasts who require detailed information about the aircraft's design and operational capabilities. The document outlines critical data such as weight limits, engine specifications, and performance metrics, ensuring that users have access to essential information for safe operation and maintenance of the aircraft.
- Maximum takeoff weight: 3,400 lbs (1,542 kg)
- Engine: Continental IO-550-N, 310 horsepower
- Maximum cruise speed: 183 knots
- Stall speed: 61 knots (landing configuration)
- Range: Approximately 1,000 nautical miles
- Service ceiling: 18,000 feet
- Equipped with Cirrus Airframe Parachute System (CAPS)
Document
Source
Originally published by www.insightavionics.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Type Certificate
- Pages
- 9
- File size
- 387 KB
- Publisher
- www.insightavionics.com
Most owners only have the POH. Here's the essential set for the Cirrus SR22 G3.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the SR22 G3 to your watchlist and track it in one place.
More Cirrus SR22 G3manuals & documents
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- 2008 CIRRUS SR22T G3 N778RPSystems Description
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- Cirrus SR20 and SR22 Flight Operations ManualFlight Manual
- Tech Sheet: Cirrus SR22Specifications
- Heritage Aviation Cirrus Service CenterAirworthiness Directives
- Cirrus SR22 G3 SpecificationsSpecifications
- SR22-G3-TN Weight and BalanceWeight And Balance
- SR22 G3 Weight & BalanceWeight And Balance
- Cirrus SR22-G3 Turbo Installation ExampleMaintenance Manual
- Airworthiness Directives for Cirrus SR22 G3Airworthiness Directives
If you fly the Cirrus SR22 G3, you may also be researching these.
In this document
Aircraft Specifications
The Cirrus SR22 G3 features a maximum takeoff weight of 3,400 lbs (1,542 kg) and a useful load of approximately 1,200 lbs (544 kg). The aircraft is powered by a Continental IO-550-N engine, producing 310 horsepower, and has a maximum cruise speed of 183 knots.
Performance Data
The SR22 G3 has a stall speed of 61 knots in landing configuration and a range of approximately 1,000 nautical miles with standard fuel capacity. The service ceiling is 18,000 feet, allowing for versatile flight operations.
Safety Features
Equipped with the Cirrus Airframe Parachute System (CAPS), the SR22 G3 enhances safety by providing a means of controlled descent in emergency situations. The aircraft also includes advanced avionics and autopilot systems for improved situational awareness.
Safety notes
- Always adhere to weight limits to ensure safe flight operations.
- Regular maintenance checks are essential for the reliability of safety systems like CAPS.
Full document text
Transport Canada Transports Canada Department of Transport Supplemental Type Certificate This approval is issued to: Insight Instrument Corporation 599 Industrial Drive Fort Erie, Ontario Number: SA09-30 Issue No.: 6 Approval Date: April 16, 2009 Issue Date: June 19, 2014 Canada L2A 5M1 Responsible Office: Aircraft/Engine Type or Model: Canadian Type Certificate or Equivalent: Description of Type Design Change: Ontario See TCCA Approved Model List (enclosed) See TCCA Approved Model List (enclosed) Installation of Insight Graphic Engine Monitor (GEM) 610C models G3, G2, G1 and 1200C model G4 as primary CHT, EGT & TIT instruments Installation/Operating Data, Required Equipment and Limitations: Manufacture must be in accordance with Insight Instrument Corporation Master Document List MDL 610C-000 Rev. 10 or later Transport Canada approved revisions. Installation must be in accordance with Installation Manual Document No. 070906 Rev. 1.3 or later Transport Canada approved revisions. (See continuation sheet) Conditions: This approval is only applicable to the type/model of aeronautical product specified therein. Prior to incorporating this modification, the installer shall establish that the interrelationship between this change and any other modification(s) incorporated will not adversely affect the airworthiness of the modified product. Sorin Camer For Minister of Transport Canada DESIGN APPROVAL DOCUMENT TRANSFER TRANSFERT DU DOCUMENT D'APPROBATION DE LA CONCEPTION Transfer of this design approval document requires the prior approval of the Minister and the reissue of this document in the name of the transferee. The reissue of this design approval document in the name of the transferee will be contingent on the holder and the transferee fulfilling their responsibilities as described in section 521.357 of the Canadian Aviation Regulations. L'approbation préalable du ministre est exigée en vue d'un transfert de ce document d'approbation de la conception et la réédition de ce document au nom du cessionnaire. La réédition de ce document d'approbation de la conception au nom du cessionnaire est conditionnelle à la satisfaction des exigences et des responsabilités, du titulaire et du cessionnaire, décrites dans l'article 521.357 du Règlement de l'aviation canadien. I have reviewed the above requirements and recognize that until the above requirements are met the certificate and all its privileges and obligations will not be transferred. J'ai examiné les conditions susmentionnées et je comprends que le transfert du certificat et des privilèges et des obligations s'y rattachant ne sera pas effectué tant que ces conditions n'auront pas été respectées. Signature of holder/signature du titulaire date/date 8799 (Continuation Sheet) Number: SA09-30 Issue 6 NOTE: THIS ADDENDUM SHALL REMAIN PART OF THE CERTIFICATE REFERRED TO THEREIN. Operation must be in accordance with Aircraft Flight Manual Supplements: 610C-FMS Issue 3 (models G3, G2, G1) approved February 20, 2012, and G4-FMS Issue 1 (model G4) approved October 26, 2012, or later Transport Canada approved revisions. Maintenance must be in accordance with Instructions for Continued Airworthiness: 610C-ICA Issue 4 (models G3, G2, G1) accepted February 22, 2012, and G4-ICA Issue 1 (model G4) accepted October 25, 2012, or later Transport Canada accepted revisions. Compliance with Chapter 4.0, "Airworthiness Limitations" of these, Instructions for Continued Airworthiness, is mandatory. TCCA Approved Model List ITEM MAKE MODEL Canadian TC FAA TC 1 American Champion Aircraft Corp. (Bellanca) 8KCAB (Decathlon), 8GCBC (Scout) A-116 A21CE 2 American Champion Aircraft Corp. (Belianca) 7AC, 7ACA, S7AC, 7BCM, 7CCM, S7CCM, 7DC, S7DC, 7EC, S7EC, 7ECA, 7FC, 7GC, 7GCA, 7GCAA, 7GCB, 7GCBA, 7GCBC, 7HC, 7JC, 7KC, 7KCAB A-759 3 | Augustair, Inc. (Varga) 2150, 2150A, 2180 4 BA Aircraft Group 5 Beechcraft 60 Beechcraft 7 Beechcraft Beagle B206-all D17S (UC-43, UC-43B, GB-1, GB-2), SD17S D17A (UC-43F) D17R (UC-43A) 8 Beechcraft E17B (UC-43D), E17L, SE17B 9 Beechcraft F17D, SF17D 10 Beechcraft 18A, S18A 11 Beechcraft 18D, S18D, A18A, SA18A, A18D, SA18D 4A19 A-121 A11EU A-649 TC 713 TC 638 TC 641 TC 689 TC 630 A-684 12 Beechcraft 18S, B18S 13 Beechcraft C18S (C-45, -45A, -45F, UC-45B, -45F, AT-7, -7A, -7B, -7C, JRB-1, -2, -3, -4, SNB-2, -2C) TC 710 A-757 Page 2 of 8 (Continuation Sheet) Number: SA09-30 Issue 6 NOTE: THIS ADDENDUM SHALL REMAIN PART OF THE CERTIFICATE REFERRED TO THEREIN. ITEM MAKE MODEL Canadian TC FAA TC 14 Beechcraft 3N, 3NM, 3TM, JRB-6, D18C, D18S, E18S, E18S-9700, G18S, H18, C-45G, TC-45G, C-45H, TC-45H, TC-45J, UC-45J (SNB-5), RC-45J (SNB-5P) A-765 AT-11, SNB-1 A-2-582 15 Beechcraft 16 Beechcraft 23-all, 24-all A1CE 17 Beechcraft 35, A35 thru G35, 35R A-777 18 Beechcraft 33-all, 36-all, 35-remaining models A-245 3A15 19 Beechcraft 45-all 5A3 20 Beechcraft 50-all 5A4 21 Beechcraft 55-all, 56TC-all, 58-all, 95-all A-259 3A16 22 Beechcraft 58P A23CE 23 Beechcraft 60-all A12CE 24 Beechcraft 65-all 3A20 25 Beechcraft 76-ali A29CE 26 Hawker Beechcraft B17L, SB17L, B17B ATC 560 21 Hawker Beechcraft C17L (UC-43J), SC17L, C17B (UC-43G), SC17B ATC 602 28 Hawker Beechcraft C17R (UC-43E), SC17R ATC 604 29 Hawker Beechcraft G17S TC 779 -30 Hawker Beechcraft 31 Hawker Beechcraft 32 Alexandria Aircraft LLC (Bellanca) 33 Alexandria Aircraft LLC D18C-T 77 Skipper 17-30A, -31A, -31ATC 14-19-all TC 770 (Bellanca) 17-30, 17-31-all 34 Bellanca 14-13-all 35 BN Group Ltd. (Britten BN-2A-all A30CE A18CE 1A3 A-773 A-92 A29EU Page 3 of 8 (Continuation Sheet) Number: SA09-30 Issue 6 NOTE: THIS ADDENDUM SHALL REMAIN PART OF THE CERTIFICATE REFERRED TO THEREIN. ITEM MAKE MODEL Canadian TC FAA TC Norman) 36 The Boeing Company (Douglas) DC3A-SCG, DC3A-SC3G, DC3A-S1CG, DC3A-S1C3G, (C-41, C-41A, C-48, C-48A, C-52, C-52A, C-52B, C-52C, C-53, C-53B, C-53C, C-53D, C-68, R4D-3, R4D-4) DC3A-S4C4G, DC3C-SC3G, DC3C-S1C3G, -S4C4G (C-47, C-47A, R4D-1, R4D-5) A-669
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DC3C-R-1830-90C, (C-47B, R4D-6) DC3D-R-1830-90C, (C-117A) 37 The Boeing Company (Douglas) DC3-G102, DC3-G102A (C-49E,C-50, C-50A, C-50B, C- 50C, C-50D, C-51) A-618 DC3-G103A, DC3-G202A (C-49, C-49A, C-49B, C-49C, C-49D, C-49J, C-49K, R4D-2) 38 39 39 40 41 The Boeing Company (Douglas) The Boeing Company (North American) The Boeing Company/ Transcontinental and Western Air Cal Pacific Airmotive Super DC-3, R4D-8, R4D-8Z 6A2 BC-1A, AT-6 (SNJ-2), AT-6A (SNJ-3), AT-6B, AT-6C (SNJ-4), AT-6D (SNJ-5), AT-6F (SNJ-6), SNJ-7, T-6G B-17E, B-17G/ A-2-575 A-44 (Restricted) L-1-3 (Limited) LTC-11 B-17F, B-17G (North American) 42 Cessna 433 Cessna 44 Cessna | P-51C, P-51D (F-51D), P-51K (F-51K) 120,140 140A 150,152-all 45 Cessna F150-all, F152, FA150-all, FA152, FRA150-all 46 Cessna 170-all 47 Cessna 172-all 48 Cessna F172-all 49 Cessna FR172-all 50 Cessna 175-all, P172-ALL, R172-ALL, 172RG, T-41-all Page 4 of 8 A-768 5A2 3A19 A13EU A-799 A-199 3A12 A4EU A18EU 3A17 (Continuation Sheet) Number: SA09-30 Issue 6 NOTE: THIS ADDENDUM SHALL REMAIN PART OF THE CERTIFICATE REFERRED TO THEREIN. ITEM MAKE MODEL Canadian TC FAA TC 51 Cessna 177-all A13CE 52 Cessna 177RG A20CE 53 Cessna F177RG A26EU 54 Cessna 180-all 5A6 55 Cessna 182-all A-204 3A13 • 56 Cessna 185-all 3A24 57 Cessna 188-all, A188-all, T188-all A-115 A9CE 58 Cessna 190, 195-all A-790 59 Cessna 205-all, 210-all 3A21 60 Cessna 206-all A-212 A4CE 61 Cessna 207-all A16CE 62 Cessna T303 A34CE 63 Cessna 64 Cessna 310-all 320-all, 340-all 3A10 3A25 55 Cessna 321 3A11 Cessna 336 A2CE 67 Cessna 337-all A6CE 68 Cessna F337-all A23EU 69 Cessna 401-ali, 402-ail, 411-all, 414-ali, 421-all, 425 A7CE 70 Cessna 404, 406 A25CE 71 Cessna (Lancair) LC40-550FG(300), LC42-550FG(350), LC41-550FG(400) A-225 A00003SE 72 Cirrus SR20, SR22 A-216 A00009CH 73 Windecker (Composite Aircraft AC-7 A7SW Corp.) Page 5 of 8 (Continuation Sheet) Number: SA09-30 Issue 6 NOTE: THIS ADDENDUM SHALL REMAIN PART OF THE CERTIFICATE REFERRED TO THEREIN. ITEM MAKE MODEL Canadian TC FAA TC 74 Diamond DA20-A1, DA20-C1 A-191 TA4CH 75 Diamond DA40, DA40F A-224 A47CE 76 Extra Flugzeugproduktions EA-300, EA-300/S, EA-300/L, EA-300/200 A67EU und Vertriebs GmbH 77 Extra Flugzeugproduktions EA-400 A43CE und Vertriebs GmbH 78 Found Aircraft Canada Inc. FBA-2C, FBA-2C1 79 GA 8 Airvan GA8, GA8-TC320 A67 A-235 A7EA A00011LA 80 Globe Swift GC-1A/1B A-766 81 Gulfstream (Grumman) G-44, G-44A (Widgeon) A-734 82 SOCATA (Grumman) GA-7 A-231 A17SO 83 Helio Aircraft LLC 84 Interceptor Aircraft (Meyers) H-250, H-295 (U-10D), HT-295, H-391 (YL-24), H-391B, H-395 (L-28A, U-10B), H-395A, H-700, H-800 200-ALL 1A8 3A18 85 Revo, Inc. (Lake/ Colonial)) Colonial C-1, C-2; Lake LA-4-All, Lake Model 250 1A13 86 Luscombe 8, 8A, 8B, 8C, 8D, 8E, 8F, T-8F - A-694 87 Maule 88 Mooney Aircraft Corp. M-4-all, M-5-all, M-6-all, M-7-ali, MX7-all M-20-all A-200 3A23 A-221 2A3 89 Mooney Aircraft Corp. M-22 A6SW 90 Vulcanair (Partenavia) P 68-all, P663-ali, P68C-all, P68TC-ali A-150 A31EU 91 FS 2003 Corp. (Piper) PA-12, PA-12S A-780 92 Piper 93 Piper PA-18-all PA-23-all 1A2 1A10 94 Piper 95 Piper PA24-all PA-28-all 1A15 2A13 Page 6 of 8 (Continuation Sheet) Number: SA09-30 Issue 6 NOTE: THIS ADDENDUM SHALL REMAIN PART OF THE CERTIFICATE REFERRED TO THEREIN. ITEM MAKE MODEL Canadian TC FAA TC 96 Piper PA-30, PA-39 A1EA 97 Piper PA31-all A8EA 98 Piper PA-32-all A-211 A3SO 99 Piper PA-34-all A-180 A7SO 100 Piper PA-42-ali A-168 A23SO 101 Piper PA-44-all A19SO 102 Piper PA-46-all A-222 A25SO 103 Piper PA-60-all A17WE 104 Pitts 105 Rockwell 106 Rockwell S1-all, S2-all 112-all, 114-all 500-all, 560-all, 680-all A8SO A12SO 2A4 107 Aermacchi F260-all A10EU (SIAI-Marchetti) 108 SOCATA (Groupe TB 9, TB 10, TB 20, TB 21, TB 200 A-153 A51EU Aerospatiale) 109 SOCATA (Groupe Aerospatiale) MS 880B, MS 885, MS 892A, MS 892E, MS 893A, MS 893E, MS 894A, MS 894E, Rallye-100S, 150T, 150ST, 235C, 235E 7A14 110 Sky Enterprises Inc. RC-3 A-769 STOL (Republic) 111 Sky International Inc. A-1, A-1A, A-1B, A-1C-180, A-1C-200 (Christen) 112 STOL Aircraft Corp. 113 Sierra Hotel Aero, inc. 114 115 True Flight Holdings LLC (American General) True Flight Holdings LLC (American General) UC-1 Navion-all AA-1, AA-1A, AA-1B, AA-1C AA-5, AA-5A, AA-5B, AG-5B A-165 A22NM A6EA A-782 A11EA A16EA Page 7 of 8 (Continuation Sheet) Number: SA09-30 Issue 6 NOTE: THIS ADDENDUM SHALL REMAIN PART OF THE CERTIFICATE REFERRED TO THEREIN. ITEM MAKE 116 Univair Aircraft (Stinson) 117 Viking Air Limited (deHavilland) 118 Viking Air Limited (deHavilland) 108-ALL MODEL DHC-2 Mk. I, DHC-2 Mk. II (Beaver) DHC-3 (Otter) - End - Page 8 of 8 Canadian TC FAA TC A-767 A-806 A-815







