TCDS A42EU

Page No. 1 2 3 4 5 6 7 8 9 10 11 Rev. No. 5 5 5 4 5 2 2 2 2 2 5 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A42EU Revision 5 Textron Aviation F182P F182Q FR182 April 1, 2019 WARNING: Use of alcohol-based fuels can cause serious performance degradation and fuel system component damage, and is therefore prohibited on Cessna airplanes. TYPE CERTIFICATE DATA SHEET NO. A42EU This data sheet, which is a part of Type Certificate No. A42EU, 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, KS 67215 Type Certificate Holder Record Cessna Aircraft Company transferred to Textron Aviation Inc. on July 29, 2015 Type Certificate A42EU was transferred from Reims Aviation S.A., 51 Aerodrome de Reims-Prunay, Reims, France, to Cessna Aircraft Company on December 11, 2006. Coincident with this transfer, the Federal Aviation Administration (FAA) has accepted the status of State of Design and State of Manufacture as defined by Annex 8 to the Convention of International Civil Aviation. Prior to December 11, 2006, products identified under Type Certificate A42EU were approved by the FAA in accordance with the Federal Aviation Regulation appropriate to Imported Products (FAR 21.29). Effective December 11, 2006, and after, these products are to be considered domestic products for the purpose of certification, and Federal Aviation Regulations 21.21 becomes appropriate. I. Model F182P, 4 PCLM (Normal Category), Approved June 18, 1976 Engine Continental O-470-S *Fuel 80/87 minimum grade aviation gasoline *Engine Limits For all operations, 2600 rpm (230 hp) Propeller and 1. McCauley constant speed Propeller Limits a) Hub 2A34C201/90DA-8 Diameter: not over 82 in., not under 80 in. Pitch settings at 30 in. sta.: low 13°, high 24.5° b) Cessna spinner 0752637 c) Woodward governor 210065, 210105, 210345, 210155, A210452 or Garwin 34-828-01-2A or McCauley C290D2/T1 or C290D3/T1 2. McCauley constant speed a) Hub 2A34C66/90AT-8 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 36 in. sta.: low 10.5°, high 22° b) Cessna spinner 0752637 c) Woodward governor 210065, 210105, 210155, 210345, 210452 or Garwin 34-828-01 or McCauley C290D2/T1 or C290D3/T1 Rev. 5 2 A42EU I. Model F182P (cont’d) Propeller and 3. McCauley constant speed Propeller Limits (cont’d) a) Hub 2A34C203/90DCA-8 blades Diameter: not over 82 in., not under 80.5 in. Pitch settings at 30 in. sta.: low 12.5°, high 25° b) Cessna spinner 0752637 c) Woodward governor 210065, 210155, 210345, 210105, 210452 or Garwin 34-828-01 or McCauley C290D2/T1 or C290D3/T1 *Airspeed Limits (IAS) Maneuvering 127 mph (110 knots) (See NOTE 4 Maximum structural cruising 162 mph (141 knots) on use of IAS) Never exceed 203 mph (176 knots) Flaps extended 110 mph ( 95 knots) C.G. Range (+39.5) to (+48.5) at 2950 lb. (+33.0) to (+48.5) at 2250 lb. or less Straight line variation between points given. Empty Weight C.G. Range None *Maximum Weight 2950 lb. No. of Seats 4 (2 front at +32.0 to +50.0) (2 rear at +74.0) Maximum Baggage 200 lb. (120 lb. at + 82.0 to +108.0) ( 80 lb. at +108.0 to +136.0) Fuel Capacity Standard Range Tanks: 61 gal. (56 gal. usable); two 30.5 gal. tanks in wings at +48 Long Range Tanks: 80 gal. (75 gal. usable); two 40.0 gal. tanks in wings at +48 See NOTE 1 for data on unusable fuel Oil Capacity 12 qt (-15)(7.5 qt usable) See NOTE 1 for data on unusable oil Control Surface Movements Wing Flaps Down 40° + 1°, -2° Elevator tab Up 25° + 2° Down 15° + 1° Ailerons Up 20° + 2° Down 15° + 2° Elevator (relative to stabilizer) Up 26° + 1° Down 17° + 1° Rudder (parallel to 0.00 W.L.) Right 24° + 1° Left 24° + 1° (perpendicular to hinge line) Right 27°13' + 1° Left 27°13' + 1° Serial Numbers Eligible F18200001 through F18200025 II. Model F182Q, 4 PCLM (Normal Category), Approved November 26, 1976 Engine Continental O-470-U *Fuel 100/130 minimum grade aviation gasoline (1977 Model) 100LL/100 aviation grade gasoline (1978 Model and on) *Engine Limits For all operations, 2400 rpm (230 hp) Rev. 5 3 A42EU III. Model F182Q (cont’d) Propeller and Propeller Limits 1. McCauley constant speed a) Hub C2A34C204/90DCB-8 Diameter: not over 82 in., not under 80.5 in. Pitch settings at 30 in. sta.: low 15°, high 29.4° b) Cessna spinner 0752637 c) McCauley governor C290D3/T14 *Airspeed Limits (IAS) Maneuvering 111 knots (See NOTE 4 Maximum structural cruising 143 knots on use of IAS) Never exceed 179 knots Flaps extended 95 knots C.G. Range (+39.5) to (+48.5) at 2950 lb. (+33.0) to (+48.5) at 2250 lb. or less Straight line variation between points given. Empty Weight C.G. Range None *Maximum Weight 2950 lb. No. of Seats 4 (2 front at +32.0 to +50.0) (2 rear at +74.0) Maximum Baggage 200 lb. (120 lb. at +82.0 to +108.0) ( 80 lb. at +108.0 to +136.0) Fuel Capacity Standard Range Tanks: 61 gal. (56 gal. usable); two 30.5 gal. tanks in wings at +48 (1977 and 1978 Models) Long Range Tanks: 80 gal. (75 gal. usable); two 40.0 gal. tanks in wings at +48 (1977 and 1978 Models) 92 gal. (88 gal. usable); two 46.0 gal. integral tanks in wing at +46.5 (1979 Model and on) See NOTE 1 for data on unusable fuel Oil capacity 12 qt (-15) (7.5 qt usable) See NOTE 1 for data on undrainable oil. Control surface movements Wing Flaps Down 40° + 1°, -2° Elevator tab Up 25° + 2° Down 15° + 1° Ailerons Up 20° + 2° Down 15° + 2° Elevator (relative to stabilizer) Up 26° + 1° Down 17° + 1° Rudder (parallel to 0.00 W.L.) Right 24° + 1° Left 24° + 1° (perpendicular to hinge line) Right 27°13' + 1° Left 27°13' + 1° Serial Numbers Eligible F18200026 through F18200169 III. Model FR182, 4 PCLM (Normal Category), Approved February 23, 1978 Engine Lycoming O-540-J3C5D *Fuel 100LL/100 aviation grade gasoline *Engine Limits For all operations, 2400 rpm (235 hp) Rev. 5 4 A42EU III. Model FR182 (cont’d) Propeller and Propeller Limits 1. McCauley constant speed a) Hub B2D34C214/90DHB-8 Diameter: not over 82 in., not under 80.5 in. Pitch settings at 30 in. sta.: low 15.8°, high 29.4° b) Cessna spinner 2250003 c) McCauley Governor C29D3/T16 *Airspeed Limits (IAS) Maneuvering 112 knots (See NOTE 4 Maximum structural cruising 144 knots (1978 Model) on use of IAS) 160 knots(1979 Model and on) Never exceed 182 knots Flaps extended 95 knots C.G. Range (+40.9) to (+47.0) at 3100 lb. (+35.5) to (+47.0) at 2700 lb. (+33.0) to (+47.0) at 2250 lb. or less Straight line variation between points given. Empty Weight C.G.Range None *Maximum Weight 3100 lb. No. of Seats 4 (2 front at +32.0 to +50.0) (2 rear at +74.0) Maximum Baggage 200 lb. (120 lb. at +82.0 to +110.0) ( 80 lb. at +110.0 to +134.0) Fuel Capacity A) 1978 Model: Standard Range Tanks: 61 gal. (75 gal. usable); two 40.0 gal. tanks in wings at +48 Long Range Tanks: 80 gal. (75 gal. usable); two 40.0 gal. tanks in wings at +48 B) 1979 Model and on: 92 gal. (88 gal. usable); two 46.0 gal. integral tanks in wings at +46.5 See NOTE 1 for data on unusable fuel Oil Capacity 9 qt (-15.7) Control Surface Movements Wing Flaps Down 40° + 1°, -2° Elevator tab Up 25° + 2° Down 15° + 1° Ailerons Up 20° + 2° Down 15° + 2° Elevator (relative to stabilizer) Up 28° + 1° Down 17° + 1° Rudder (parallel to 0.00 W.L.) Right 24° + 1° Left 24° + 1° (perpendicular to hinge line) Right 27°13' + 1° Left 27°13' + 1° Serial Numbers Eligible FR18200001 through FR18200070 Rev. 5 5 A42EU Data Pertinent To All Models Datum Front face of firewall Leveling means Upper door sill. Top surface centerline of tailcone (1977 Model) Jig located nutplates and screws on left of tailcone (1978 Model and on) Certification basis F182 Series Part 3 of the Civil Air Regulations dated November 1, 1949, as amended by 3-1 through 3-12 and paragraph 3.112 as amended October 1, 1959. In addition effective 1979 Model and on, FAR 23.1559 effective March 1, 1978. FAR 36 dated December 1, 1969, plus amendments 36-1 through 36-6 (Model F182Q and on). FR182 Series Part 3 of the Civil Air Regulations dated November 1, 1949, as amended by 3-1 through 3-12 and paragraph 3.112 as amended October 1, 1959; and Sections 23.729, 23.777(e), 23.781, 23.1555(e)(1) and (2), and 23.1563 of the Federal Aviation Regulations dated February 1, 1965, as amended February 14, 1975. In addition effective 1979 Model and on, FAR 23.1559 effective March 1, 1978 FAR 36 dated December 1, 1969, plus amendments 36-1 through 36-6. Application for Type Certificate dated June 30, 1976. Type Certificate No. A42EU issued June 18, 1976. Equivalent Safety Items: F182 Series Airspeed indicator CAR 3.757 (See NOTE 4 for use of IAS) Operating Limitations CAR 3.778 (a) FR182 Series Airspeed Indicator CAR 3.757 (See NOTE 4 for use of IAS) Operating Limitations CAR 3.778 (a) Fuel System CAR 3.430 Equipment The basic required equipment as prescribed in the applicable airworthiness requirements (see Certification Basis) must be installed in the aircraft for certification. This equipment must include a current Airplane Flight Manual effective 1979 Model and on. In addition, the following item of equipment is required: Stall warning indicator, Cessna Dwg 0511062 NOTE 1. Current weight and balance report including list of equipment included in certificated empty weight, and locating instructions when necessary, must be provided for each aircraft at the time of original certification. (a) Models F182P The certificated empty weight and the corresponding center of gravity location must include unusable fuel of 30 lb. at (+46) and undrainable oil of 0 lb. (b) Models F182Q (1977 and 1978 Models) The certificated empty weight and the corresponding center of gravity location must include unusable fuel of 30 lb. at (+46) and include oil of 22 lb. (-15.0). (c) Models F182Q (1979 Model and on) The certificated empty weight and the corresponding center of gravity location must include unusable fuel of 24 lb. at (+48) and full oil of 22.5 lb. at (-15.0). Rev. 5 6 A42EU Data Pertinent To All Models (cont’d) NOTE 1. (cont’d) (d) Models FR182 (1978 Model) The certificated empty weight and the corresponding center of gravity location must include unusable fuel of 30 lb. at (+46) and include oil of 16.5 lb. (-15.7) (e) Models FR182 (1979 Model and on) The certificated empty weight and the corresponding center of gravity location must include unusable fuel of 24 lb. at (+48) and include oil of 16.9 lb. (-15.7). NOTE 2. The following placards must be displayed as indicated: A. Applicable to Model F182P (1) In full view of the pilot: “This airplane must be operated as a normal category airplane in compliance with the operating limitations as stated in the form of placards, markings and manuals. Maximums Maneuvering speed (IAS) 110 knots Gross weight 2950 lb. Flight load factor Flaps up +3.8, -1.52 Flaps down +2.0 No acrobatic maneuvers, including spins, approved. Altitude loss in a stall recovery: 160 ft. Flight into known icing conditions prohibited. This airplane is certified for the following flight operations as of date of original airworthiness certificate: (DAY NIGHT VFR IFR) (As applicable)” (2) On the fuel selector valve plate: Standard range tanks: "Off. Left tank level flight only 29 gal. Both on for landing and takeoff all flight attitudes, 56 gal. Right tank level flight only 29 gal." Long range tanks: "Off. Left tank level flight only 37 gal. Both on for landing and takeoff all flight attitudes, 75 gal. Right tank level flight only 37 gal." (3) On the control lock: "Control lock - remove before starting engine". (4) On the baggage door: "Forward of baggage door latch, 120 lb. maximum baggage and/or auxiliary passenger. Aft of baggage door latch, 80 lb. maximum baggage including 25 lb. maximum in baggage wall hat shelf. Maximum 200 lb. combined. For additional loading instructions see weight and balance data". (5) On flap control indicator: (a) “0° to 10° - (Blue color code and 140 kts callout; also, mechanical detent at 10°) (b) “10° to 20° - Full (Indices at these positions with white color code and 95 kts callout; also, mechanical detent at 10° and 20°)." (6) Forward of the filler cap on the wing surface: Standard range tanks: "Service this airplane with 80/87 minimum aviation grade gasoline. Capacity 30.5 gal." Long range tanks: "Service this airplane with 80/87 minimum aviation grade gasoline. Capacity 40.0 gal." (7) On aft panel of baggage compartment: "Oxygen refill" (All models with oxygen) Rev. 5 7 A42EU Data Pertinent To All Models (cont’d) Note 2: (cont’d) (8) Adjacent to overvoltage light: "High voltage" (9) Above the left fuel gauge: "Do not turn off alternator in flight except in emergency" B. Applicable to Model F182Q (1) In full view of the pilot: (a) 1977 and 1978 Models: "This airplane must be operated as a normal category airplane in compliance with the operating limitations as stated in the form of placards, markings and manuals. Maximums Maneuvering speed (IAS) 111 knots Gross weight 2950 lb. Flight load factor Flaps up +3.8 -1.52 Flaps down +2.0 No acrobatic maneuvers, including spins, approved. Altitude loss in a stall recovery: 160 ft. Flight into known icing conditions prohibited. This airplane is certified for the following flight operations as of date of original airworthiness certificate: (DAY NIGHT VFR IFR) (As applicable)” (b) 1979 Model and on: "The markings and placards installed in this airplane contain operating limitations which must be complied with when operating this airplane in the Normal Category. Other operating limitations which must be complied with when operating this airplane in this category are contained in the Pilot's Operating Handbook and FAA approved Airplane Flight Manual. No acrobatic maneuvers, including spins, approved. Flight into known icing conditions prohibited. This airplane is certified for the following flight operations as of date of original airworthiness certificate: (DAY NIGHT VFR IFR) (As applicable)” (c) Near airspeed indicator (1979 Model and on): "Maneuver Speed 111 KIAS" (2) On the fuel selector valve plate: (a) 1977 and 1978 Models: Standard range tanks: "Off. Left - 29 gal. Level flight only. Both - 56 gal. All flight attitudes. Both on for takeoff and landing Right - 29 gal. Level flight only" Long range tanks: "Off. Left - 37 gal. Level flight only. Both - 75 gal. All flight attitudes. Both on for takeoff and landing. Right - 37 gal. Level flight only" Rev. 5 8 A42EU Data Pertinent To All Models (cont’d) NOTE 2: (cont'd) (b) 1979 Model and on: "Off Left - 44 gal. Level flight only. Both - 88 gal. All flight attitudes. Both on for takeoff and landing. Right - 44 gal. Level flight only" (3) On the control lock: "Control lock - remove before starting engine" (4) On the baggage door: "Forward of baggage door latch, 120 lb. maximum baggage and/or auxiliary passenger. Aft of baggage door latch, 80 lb. maximum baggage including 25 lb. maximum in baggage wall hat shelf. Maximum 200 lb. combined. For additional loading instructions see weight and balance data". (5) On flap control indicator: (a) “0° to 10° (Blue color code and 140 kts callout; also, mechanical detent at 10°) (b) 0° to 20° Full (Indices at these positions with white color code and 95 kts callout; also, mechanical detent at 10° and 20°)." (6) Forward of the filler cap on the wing surface: (a) 1977 Model Standard range tanks: "Service this airplane with 100/130 minimum aviation grade gasoline. Capacity 30.5 gal." Long range tanks: "Service this airplane with 100/130 minimum aviation grade gasoline. Capacity 40.0 gal." (b) 1978 Model Standard range tanks: "Service this airplane with 100LL/100 minimum aviation grade gasoline. Capacity 30.5 gal." Long range tanks: "Service this airplane with 100LL/100 minimum aviation grade gasoline. Capacity 40.0 gal." (c) 1979 Model and on "Fuel 100LL/100 minimum grade aviation gasoline. Capacity 46 U.S. gal., capacity 34.5 U.S. gal. to bottom of filler collar." (7) On aft panel of baggage compartment: "Oxygen refill" (All models with oxygen) (8) Adjacent to overvoltage light: (a) 1977 and 1978 Models "High Voltage" (b) 1979 Model and on "Low Voltage" C. Applicable to Model FR182 (1) In full view of the pilot: (a) 1978 Model "This airplane must be operated as a normal category airplane in compliance with the operating limitations as stated in the form of placards, markings and manuals. Rev. 5 9 A42EU Data Pertinent To All Models (cont’d) NOTE 2: (cont'd) Maximums Gross weight 3100 lb. Flight load factor Flaps up +3.8 -1.52 Flaps down +2.0 No acrobatic maneuvers, including spins, approved. Altitude loss in a stall recovery: 240 ft. Flight into known icing conditions prohibited. This airplane is certified for the following flight operations as of date of original airworthiness certificate: (DAY NIGHT VFR IFR) (As applicable)” (b) 1979 Model and on: "The markings and placards installed in this airplane contain operating limitations which must be complied with when operating this airplane in the Normal Category. Other operating limitations which must be complied with when operating this airplane in this category are contained in the Pilot's Operating Handbook and FAA approved Airplane Flight Manual. No acrobatic maneuvers, including spins, approved. Flight into known icing conditions prohibited. This airplane is certified for the following flight operations as of date of original airworthiness certificate: (DAY NIGHT VFR IFR) (As applicable)” (c) Near Airspeed Indicator: "MAX SPEED - KIAS Maneuver 112 Gear Oper. 140 Gear Down 140" (2) On the fuel selector valve plate: (a) 1978 Model: Standard range tanks: "Off. Left - 29 gal. Level flight only Both - 56 gal. All flight attitudes Both on for takeoff and landing Right - 29 gal. Level flight only" Long range tanks: "Off. Left - 37 gal. Level flight only Both - 75 gal. All flight attitudes Both on for takeoff and landing Right - 37 gal. Level flight only" (b) 1979 Model: "Off Left - 44 gal. Level flight only Both - 88 gal. All flight attitudes Both on for takeoff and landing Right - 44 gal. Level flight only" (3) On the control lock: "Control lock - remove before starting engine" Rev. 5 10 A42EU Data Pertinent To All Models (cont’d) NOTE 2: (cont'd) (4) On the baggage door: "120 Pounds Maximum Baggage and/or auxiliary passenger Forward of baggage door latch and 80 Pounds Maximum Baggage aft of baggage door latch Maximum 200 Pounds combined For additional loading instructions see Weight and Balance Data" (5) On flap control indicator: (a) “0° to 10° (Blue color code and 140 kts callout; also, mechanical detent at 10°) (b) 0° to 20° Full (Indices at these positions with white color code and 95 kts callout; also, mechanical detent at 10° and 20°)." (6) Forward of the filler cap on the wing surface: (a) 1978 Model Standard range tanks: "Service this airplane with 100LL/100 minimum aviation grade gasoline. Capacity 30.5 gal." Long range tanks: "Service this airplane with 100L/100 minimum aviation grade gasoline. Capacity 40.0 gal." (b) 1979 Model "Fuel 100LL/100 minimum grade aviation gasoline. Capacity 46 U.S. gal., capacity 34.5 U.S. gal. to bottom of filler collar." (7) Adjacent to overvoltage light: (a) 1978 Model "High Voltage" (b) 1979 Model "Low Voltage" (8) Near gear hand pump: "Manual Gear Extension 1. Select gear down. 2. Pull handle fwd. 3. Pump vertically CAUTION Do not pump with gear UP selected" NOTE 3. The cylinder head thermistors must be installed as follows: Model Engine and Cylinder Head Number O-470-S O-470-U O-540-J F182P 3 N/A F182Q N/A 3 FR182 N/A N/A 5 Rev. 5 11 A42EU NOTE 4. The marking of the airspeed indicator with IAS provides an equivalent level of safety to CAR 3.757 when the approved airspeed calibration data presented in Section V of the Pilots' Operating Handbooks, listed below is available to the pilot: MODEL CESSNA P/N MODEL YEAR F182P D1062-13 1976 Model F182Q D1087-13 1977 Model F182Q D1114-13 1978 Model F182Q D1141-13 1979 Model FR182 D1115-13 1978 Model FR182 D1142-13 1979 Model NOTE 5. Fourteen Volt Electrical System (F182 Series thru 1977 Model) Twenty Eight Volt Electrical System (F182 Series 1978 Model and on) (FR182 Series Model and on) In addition to the above specified placards, the prescribed operating limitations indicated by an asterisk (*) under Sections I through III of this data sheet must be also displayed by permanent markings. ---- END ----