# TCDS 3A11: Textron Aviation Inc. - Type: Type certificate data sheet - Status: Current - Holder: Textron Aviation Inc. - Revision: 7 - Revised: July 29, 2015 - Product: Aircraft, Small Airplane - Certification basis: CAR 3 - Data sheet PDF: https://openairdocs.org/files/sha256/4b/3b/4b3b83c4150abd37c1aa75cf211512c86706444c119e58ebc3884f81cd7da857 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/EFACF3CCDFE3847C86257ED2006A3F01.0001 - Page: https://openairdocs.org/tcds/3A11 ## Models (1) As the data sheet lists them. - 321 ((Navy OE-2)) ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 3 4 5 Rev. No. 7 5 6 6 7 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 3A11 Revision 7 Textron Aviation Inc. 321 (Navy OE-2) July 29, 2015 TYPE CERTIFICATE DATA SHEET NO. 3A11 This data sheet which is part of Type Certificate No. 3A11 prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder Textron Aviation Inc. One Cessna Boulevard Wichita, Kansas 67215 Type Certificate Holder Record Cessna Aircraft Company transferred to Textron Aviation Inc. on July 29, 2015 I. Model 321 (NAVY OE-2), 2 PCLM (Utility Category), Approved May 13, 1955 Engine Continental O-470-2 Fuel 100/130 Min. grade aviation gasoline (See NOTE 4 for alcohol-based fuels warning.) Engine Limits HP RPM MP IN.HG. ALT. Takeoff (one minute) 265 2600 36.0 S.L. Takeoff (one minute) 265 2600 32.4 8,500' Maximum continuous 250 2600 34.0 S.L. Maximum continuous 250 2600 30.5 10,000' (Straight line manifold pressure variation with altitude between points shown). Airspeed Limits Maneuvering 134 mph (116 knots) Maximum structural cruising 155 mph (135 knots) Never exceed 200 mph (174 knots) Flaps extended 105 mph ( 91 knots) C.G. Range (+33.6) to (+42.3) at 2150 lbs. (+36.0) to (+42.3) at 2650 lbs. Straight line variation between points shown. 3A11 2 Rev. 7 I. Model 321 (cont’d) C.G. Range (cont’d) 33 34 35 36 37 38 39 40 41 42 43 2000 2100 2200 2300 2400 2500 2600 2700 LBS. INCHES REAR LIMIT FRONT LIMIT Empty Weight C.G. Range None Maximum Weight 2650 lbs. No. Seats 2 (1 at +36, 1 at +76) Maximum Baggage 100 lbs. (+100) Fuel Capacity 52 gal. total, 44 gal. usable (two 26 gal. tanks in wings) (+45) (See NOTE 1 for weight of unusable fuel.) Oil Capacity 4 gal. (-15) (Unusable - 1.5 gal.) (See NOTE 1 for data on undrainable oil) Control Surface Wing flaps - Maximum Takeoff - 0 to 20° Movements Landing - 40° Ailerons Up 20° Down 14° Stabilizer Up 1.0° Down 9.0° Elevators Up 28° Down 22° With Stabilizer Full Down Rudder Right 22° Left 22° Serial Nos. Eligible 611 and 37000 through 37999. Prior to civil certification, OE-2 airplanes must be modified in accordance with Cessna Dwg. No. 1000003 which may be obtained from Cessna Aircraft Company, Wichita, Kansas. An appropriate representative of the Administrator, upon determination of compliance with the above-mentioned modification drawing, may issue an airworthiness certificate. Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: Items 1(a), (b), and (c), 101(a) and (b), 102, 103, 106, 107, 108, 201(a), 202(a), 204(a), 301, 302, 402, 601, 602 and 603. Rev. 7 3 3A11 Specifications Pertinent to all Models Datum Front face of firewall Leveling means Horizontal control stick torque tube Certification Basis: Type Certificate No. 3A11 (CAR 3 dated November 1, 1949, and Amendments through 3-10) Production Basis: (a) Production Certificate No. 4 for Serial Nos. 611, 37,000 through 37,024. (b) All other and/or subsequent serial Nos.: None. Prior to original certification of each aircraft a FAA representative must perform a detailed inspection for workmanship, materials, and conformity with the approved technical data, and a check of flight characteristics. Export eligibility Eligible for export to all countries subject to the provisions of MOP 2-4. Equipment: A plus (+) or minus (-) sign preceding the weight of an item of equipment indicates net weight change when that item is installed. Propellers and Propeller Accessories 1. McCauley, constant speed propeller (a) McCauley hub 2A36C1, blade 90M-0 64 lbs. (-40) Diameter: Not over 90 in., not under 88 in. Pitch settings at 36 in. sta.: Low 9.5°, high 23° (b) Propeller spinner (Cessna Dwg. 1052004) 4 lbs. (-40) (c) Propeller governor, Woodward 210105 4 lbs. (-34.5) Engine and Engine Accessories - Fuel and Oil System 101. Fuel pumps: (a) Engine-driven, Lear-Romec (RG-9080) Type G-18 1 lb. (-5) (b) Electric, Adel 29924 4 lbs. (+15) 102. Oil cooler, Harrison AP13AU10-01 6 lbs. (-34) 103. Carburetor air filter, Air Maze P/N 120310 1 lb. (-28) 104. Starter, Eclipse Type J-1 (AN 4116R1) 16 lbs. (-6.5) 105. Vacuum pump, Pesco 3P-194-F, Type B-11 5 lbs. (-5.5) 106. Flexible fuel and oil hose assemblies MS28741 (Mil-H-5511) 2 lbs. (-5) 107. Carburetor air heater (Cessna Dwg. 12321-79) 3 lbs. (-20) 108. Supercharger oil filter, Continental P/N 539609 (filter wt. included in engine wt.) Installation per Cessna Dwg/ No. 1050000 1 lb. (-2) Landing Gear 201. 2 Main wheel-brake assemblies, 6.00-6, Type III (a) Goodyear Model LF6HBD 13 lbs. (+17.5) Wheel assembly No. 511960-S Brake assembly No. 9530839 202. (a) 2 Main wheel 4-ply-rating tires, 7.00-6, Type III 22 lbs. (+17.5) (with regular tubes) 204. Tail wheel assembly - 8" pneumatic (a) Scott Model 3400, steerable, swiveling (Goodrich B-3 - 166AP 8 lbs. (+257) wheel, Goodyear tire 8x3.25, Type I, 6-ply nylon) Electrical Equipment 301. Generator, 24V-50 amp., Eclipse 1345-3-A 14 lbs. (-6.5) 302. Battery 24 Volt, 11 Amp. Hr. (AN 3154-1A) 34 lbs. (+4.5) 303. Two landing lights, G. E. 4591 2 lbs. (+25) 3A11 4 Rev. 7 Specifications Pertinent to all Models (cont’d) Interior Equipment 401. Cabin heater valve assembly (Cessna Dwg. 1013035) 1 lb. (-2) 402. Pilot Check List, Cessna Dwg. 1000007 See NOTE 3 for details. Miscellaneous (Not listed above) 601. Safe Flight stall warning indicator (Cessna Dwg. 12305-129) 1 lb. (+21) 602. Two rudder return springs (Cessna Dwg. 1033010) 2 lbs. (+55) 603. Elevator down spring (Cessna Dwg. 1060281) 1 lb. (+179) 604. Installation shoulder harness (Cessna Dwgs. 1010008 and 0610007) Use actual weight NOTE 1. Current weight and balance report including list of equipment included in certificated weight empty, and loading instructions, when necessary, must be in each aircraft at the time of original certification and at all times thereafter (except in the case of air carrier operators having an approved weight control system). The certificated weight empty and corresponding center of gravity location must include unusable fuel of 44.0 lbs. at (+45), (included in total fuel capacity), and undrainable oil of 1.5 lbs. at (-15), (not included in oil capacity). NOTE 2. The following placards must be displayed in the locations noted: A. In front of and in clear view of the pilot: "(1) This airplane must be operated as a utility category airplane in compliance with the operating limitations as stated in the form of placards, markings and manuals (pilot's check list)." "(2) No acrobatic maneuvers including spins approved. See pilot's check list for approved maneuvers." "(3)Maximum flap extended speed 91 knots (105 mph)." "(4) POWER CHART - 2600 RPM 100/130 Grade Fuel Take-off Power Limit One Minute Continental O-470-2 Engine - McCauley 2A36C1/90M-0 Propeller Altitude S.L. 2,000 4,000 6,000 8,000 10,000 M.C. Power 34.0 33.3 32.5 31.9 31.3 F.T. T.O. Power 36.0 34.5 33.6 33.0 32.5 - - - -" "(5)Solo front seat only." B. On Left and Right rear windows: "Do Not Open Window Above 126 knots (145 mph)" C. On Left and Right front windows: "Do Not Open Window Above 104 Knots (120 mph)" D. In baggage compartment: "Maximum Baggage 100 Pounds" E. Adjacent to fuel selector valve: "Usable Fuel Left Tank - 22.0 gallons" "Usable Fuel Right Tank - 22.0 gallons" "With full tanks take-off on left tank" Rev. 7 5 3A11 Specifications Pertinent to all Models (cont’d) NOTE 3. The following information shall be provided in the form of placards, markings, or manuals (pilot's check list): A. Maximum Weight - 2,650 lbs. C.G. limits (+33.6) to (+42.3) at 2,150 lbs. (+36.0) to (+42.3) at 2,650 lbs. Straight line variation between points. Datum - Forward face of firewall. B. The following limited acrobatic maneuvers are approved: Maneuvers Safe Entry Speeds Stalls Slow Deceleration Steep Turns 116 knots (134 mph) Spins Intentional spins prohibited Lazy Eights 116 Knots (134 mph) Chandelle 116 Knots (134 mph) C. Maximum Take-Off Flap Setting 20°. D. Airspeed and Load Factor Limitations: Never Exceed Speed 173.5 Knots (200 mph) Maximum Structural Cruise Speed 134.6 Knots (155 mph) Maneuvering Speed 116 Knots (134 mph) Flap Extended Speed 91 Knots (105 mph) Maximum Load Factors 0° Flaps - +4.4 to -1.8 Flaps Extended - +3.5 E. Fuel in tanks when gauges register "Empty" cannot be used safely in flight. F. With full fuel tanks, take off and operate on left tank for 30 minutes. G. Red arc on fuel gauge indicates no take-off. NOTE 4. WARNING: Use of alcohol-based fuels can cause serious performance degradation and fuel system component damage, and is therefore prohibited on Cessna airplanes. --- END --- ``` ## ADs (5, in force first) - [AD 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023 - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [AD 2000-01-16](https://openairdocs.org/ad/2000-01-16): Exhaust System · Cessna 320, 320-1, 320A and 28 more. Effective Feb 15, 2000 - [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. 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