TCDS 3A13

Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 Rev. No. 76 70 70 70 70 70 70 70 39 39 39 60 49 62 70 51 51 70 Page No. 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 Rev. No. 51 51 51 51 51 51 43 51 43 51 51 51 55 58 67 68 73 76 Page No. 37 38 39 40 41 42 Rev. No. 68 76 75 75 76 76 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 3A13 Revision 76 Textron Aviation 182 182K 182A 182L 182B 182M 182C 182N 182D 182P 182E 182Q 182F 182R 182G R182 182H T182 182J TR182 182S T182T 182T October 8, 2026 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. 3A13 This data sheet which is part of Type Certificate No. 3A13 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 182, Skylane, 4 PCLM (Normal Category), Approved March 2, 1956 Engine Continental O-470-L *Fuel 80 minimum grade aviation gasoline *Engine Limits For all operations, 2600 r.p.m. (230 hp.) 3A13 Page 2 of 42 Rev. 76 I. Model 182 (cont’d) Propeller and 1. Hartzell constant speed Propeller Limits (a) Hub HC82XF-1 or HCA2XF-1 or BHCA2XF-1 with 8433-2 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 30 in. sta.: low 12°, high 24° (b) Cessna spinner 0752006 (c) Woodward governor 210065, 210105, 210155 or 210340 2. McCauley constant speed (a) Hub 2A36C1-U/90M-8, 2A36C18/90M-8 or 2A36C29/90M-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 0752004 (c) Woodward governor 210065, 210105, 210155, 210345 or 210452, or McCauley C290D2/T1 or C290D3/T1 3. Hartzell constant speed (a) Hub BHC-C2YF-1 with 8468-2 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 30 in. sta.: low 13°, high 24° (b) Cessna spinner 0752619 (c) Woodward governor 210105AF, 210340 or 210451 4. McCauley constant speed (a) Hub 2A34C50/90A-8 or 2A34C66/90AT-8 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 36 in. sta.: low 10.5°, high 21.5° (b) Cessna spinner 0752004 (c) Woodward governor 210065, 210105, 210155, 210345 or 210452 or McCauley C290D2/T1 or C290D3/T1 5. Aircraft reworked per Cessna Service Kit SK182-121: McCauley constant speed (Threadless) (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 25.0° (b) Cessna spinner 0752004 (c) Woodward governor 210065, 210105, 210155, 210345, or 210452, or Garwin 34-828-01, or McCauley C290D2/T1 or C290D3/T1 *Airspeed Limits Maneuvering 122 m.p.h. (106 knots) (CAS) Maximum structural cruising 160 m.p.h. (139 knots) Never exceed 184 m.p.h. (160 knots) Flaps extended 100 m.p.h. ( 87 knots) C.G. Range (+39.5) to (+45.8) at 2550 lb. (+35.0) to (+45.8) at 2050 lb. or less Straight line variation between points given. Empty Wt. C.G. Range None *Maximum Weight 2550 lb. No. of Seats 4 (2 at +36, 2 at +70) Maximum Baggage 120 lb. (+95) Fuel Capacity 60 gal. (55 gal. usable); two 30 gal. tanks in wings at +48. (See NOTE 1 for data on unusable fuel). Rev. 76 Page 3 of 42 3A13 I. Model 182 (cont’d) Oil Capacity 12 qt. (-15) (6 qt. usable) (See NOTE 1 for data on undrainable oil). Control Surface Wing flaps Takeoff Retracted 0° Movements 1st notch 10° 2nd notch 20° Landing 3rd notch 30° 4th notch 40° Ailerons Up 20° ± 2° Down 14° ± 2° Adj. stabilizer Up 1° 50' ± 15 Down 8° 20' ± 15' Elevator Up 25° ± 1° Down 22° 50' ± 1° (With stabilizer full down) Rudder Right 24° ± 1° Left 24° ± 1° Serial Nos. Eligible 613 and 33000 thru 33842 (1956 Model) II. Model 182A, Skylane, 4 PCLM (Normal Category), Approved December 7, 1956 Engine Continental O-470-L *Fuel 80 minimum grade aviation gasoline *Engine Limits For all operations, 2600 r.p.m. (230 hp.) Propeller and 1. Hartzell constant speed Propeller Limits (a) Hub HC82XF-1 or HCA2XF-1 or BHCA2XF-1 with 8433-2 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 30 in. sta.: low 12°, high 24° (b) Cessna spinner 0752006 (c) Woodward governor 210065, 210105, 210155 or 210340 2. McCauley constant speed (a) Hub 2A36C1-U/90M-8, 2A36C18/90M-8 or 2A36C29/90M-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 0752004 (c) Woodward governor 210065, 210105, 210155 or 210452, or McCauley C290D2/T1 or C290D3/T1 3. Hartzell constant speed (a) Hub BHC-C2YF-1 with 8468-2 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 30 in. sta.: low 13°, high 24° (b) Cessna spinner 0752619 (c) Woodward governor 210105AF, 210340 or 210451 4. McCauley constant speed (a) Hub 2A34C50/90A-8 or 2A34C66/90AT-8 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 36 in. sta.: low 10.5°, high 21.5° (b) Cessna spinner 0752004 (c) Woodward governor 210065, 210105, 210155, 210345, 210452, or McCauley C290D2/T1 or C290D3/T1 3A13 Page 4 of 42 Rev. 76 II. Model 182A (cont’d) Propeller and Propeller Limits (cont’d) 5. Aircraft reworked per Cessna Service Kit SK182-121: McCauley constant speed (Threadless) (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 25.0° (b) Cessna spinner 0752004 (c) Woodward governor 210065, 210105, 210155, 210345, or 210452, or Garwin 34-828-01, or McCauley C290D2/T1 or C290D3/T1 *Airspeed Limits Maneuvering 122 m.p.h. (106 knots) (CAS) Maximum structural cruising 160 m.p.h. (139 knots) Never exceed 184 m.p.h. (160 knots) Flaps extended 100 m.p.h. ( 87 knots) C.G. Range (+40.0) to (+45.8) at 2650 lb. (+33.5) to (+45.8) at 2100 lb. or less Straight line variation between points given. Empty Wt. C.G. Range None *Maximum Weight 2650 lb. No. of Seats 4 (2 at +36, 2 at +70) Maximum Baggage 120 lb. (+95) Fuel Capacity 65 gal. (55 gal. usable); two 32.5 gal. tanks in wings at +48 (See NOTE 1 for data on unusable fuel). Oil Capacity 12 qt. (-15) (6 qt. usable) (See NOTE 1 for data on undrainable oil). Control Surface Wing flaps Takeoff Retracted 0° Movements 1st notch 10° 2nd notch 20° Landing 3rd notch 30° 4th notch 40° Ailerons Up 20° ± 2° Down 14° ± 2° Adj. stabilizer Up 1° 50' ± 15' Down 8° 20' ± 15' Elevator Up 25° ± 1° Down 22° 50' ± 1° (With stabilizer full down) Rudder Right 24° ± 1° Left 24° ± 1° Serial Nos. Eligible 33843 thru 34753 (1957 Model) 34755 thru 34999 and 51001 thru 51556 (1958 Model) III. Model 182B, Skylane, 4 PCLM (Normal Category), Approved August 22, 1958 Engine Continental O-470-L *Fuel 80 minimum octane aviation gasoline *Engine Limits For all operations, 2600 r.p.m. (230 hp.) Rev. 76 Page 5 of 42 3A13 III. Model 182B (cont’d) Propeller and 1. Hartzell constant speed Propeller Limits (a) Hub HC82XF-1 or HCA2XF-1 or BHCA2XF-1 with 8433-2 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 30 in. sta.: low 12°, high 24° (b) Cessna spinner 0752006 (c) Woodward governor 210065, 210105, 210155, or 210340 2. McCauley constant speed (a) Hub 2A36C1-U/90M-8, 2A36C18/90M-8 or 2A36C29/90M-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 0752004 (c) Woodward governor 210065, 210105, 210155, 210345, 210452, or McCauley C290D2/T1 or C290D3/T1 3. Hartzell constant speed (a) Hub BHC-C2YF-1 with 8468-2 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 30 in. sta.: low 13°, high 24° (b) Cessna spinner 0752619 (c) Woodward governor 210105AF, 210340, or 210451 or McCauley C290D2/T1 or C290D3/T1 4. McCauley constant speed (a) Hub 2A34C50/90A-8 or 2A34C66/90AT-8 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 36 in. sta.: low 10.5°, high 21.5° (b) Cessna spinner 0752004 (c) Woodward governor 210065, 210105, 210155, 210345, 210452, 5. Aircraft reworked per Cessna Service Kit SK182-121: McCauley constant speed (Threadless) (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 25.0° (b) Cessna spinner 0752004 (c) Woodward governor 210065, 210105, 210155, 210345, or 210452, or Garwin 34-828-01, or McCauley C290D2/T1 or C290D3/T1 *Airspeed Limits Maneuvering 122 m.p.h. (106 knots) (CAS) Maximum structural cruising 160 m.p.h. (139 knots) Never exceed 184 m.p.h. (160 knots) Flaps extended 100 m.p.h. ( 87 knots) C.G. Range (+40.0) to (+45.8) at 2650 lb. (+33.5) to (+45.8) at 2100 lb. or less Straight line variation between points given. Empty Wt. C.G. Range None *Maximum Weight 2650 lb. No. of Seats 4 (2 at +36, 2 at +70) Maximum Baggage 120 lb. (+95) Fuel Capacity 65 gal. (55 gal. usable); two 32.5 gal. tanks in wings at +48 (See NOTE 1 for data on unusable fuel). 3A13 Page 6 of 42 Rev. 76 III. Model 182B (cont’d) Oil Capacity 12 qt. (-15) (6 qt. usable) (See NOTE 1 for data on undrainable oil). Control Surface Wing flaps Takeoff Retracted 0° Movements 1st notch 10° 2nd notch 20° Landing 3rd notch 30° 4th notch 40° Ailerons Up 20° +2° Down 14° +2° Adj. stabilizer Up 1° 50' +15' Down 8° 20' +15' Elevator Up 25° +1° Down 22° 50' +1° (With stabilizer full down) Rudder Right 24° +1° Left 24° +1° Serial Nos. Eligible 34754, 51557 thru 52358 except 51623 (1959 Model) IV. Model 182C, Skylane, 4 PCLM (Normal Category), Approved July 8, 1959 Model 182D, Skylane, 4 PCLM (Normal Category), Approved June 14, 1960 Engine Continental O-470-L *Fuel 80 minimum octane aviation gasoline *Engine Limits For all operations, 2600 r.p.m. (230 hp.) Propeller and 1. Hartzell constant speed Propeller Limits (a) Hub HC82XF-1 or HCA2XF-1 or BHCA2XF-1 with 8433-2 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 30 in. sta.: low 12°, high 24° (b) Cessna spinner 0752006 (c) Woodward governor 210065, 210105, 210155, or 210340 2. McCauley constant speed (a) Hub 2A36C1-U/90M-8, 2A36C18/90M-8 or 2A36C29/90M-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 0752004 (c) Woodward governor 210065, 210105, 210155, 210345, 210452, or McCauley C290D2/T1 or C290D3/T1 3. Hartzell constant speed (a) Hub BHC-C2YF-1 with 8468-2 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 30 in. sta.: low 13°, high 24° (b) Cessna spinner 0752619 (c) Woodward governor 210105AF, 210340, or 210451 4. McCauley constant speed (a) Hub 2A34C50/90A-8 or 2A34C66/90AT-8 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 36 in. sta.: low 10.5°, high 21.5° (b) Cessna spinner 0752004 (c) Woodward governor 210065, 210105, 210155, 210345, 210452, or McCauley C290D2/T1 or C290D3/T1 Rev. 76 Page 7 of 42 3A13 IV. Model 182C, Model 182D (cont’d) Propeller and 5. Aircraft reworked per Cessna Service Kit SK182-121: Propeller Limits (cont’d) McCauley constant speed (Threadless) (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 25.0° (b) Cessna spinner 0752004 (c) Woodward governor 210065, 210105, 210155, 210345, or 210452, or Garwin 34-828-01, or McCauley C290D2/T1 or C290D3/T1 *Airspeed Limits Maneuvering 122 m.p.h. (106 knots) (CAS) Maximum structural cruising 160 m.p.h. (139 knots) Never exceed 184 m.p.h. (160 knots) Flaps extended 100 m.p.h. ( 87 knots) C.G. Range (+40.0) to (+45.8) at 2650 lb. (+33.5) to (+45.8) at 2100 lb. or less Straight line variation between points given. Empty Wt. C.G. Range None *Maximum Weight 2650 lb. No. of Seats 4 (2 at +36, 2 at +70) Maximum Baggage 120 lb. (+95) Fuel Capacity 65 gal. (55 gal. usable); two 32.5 gal. tanks in wings at +48 See NOTE 1 for data on unusable fuel Oil Capacity 12 qt. (-15) (6 qt. usable) See NOTE 1 for data on undrainable oil Control Surface Wing flaps Takeoff 0°, 10°, 20° Movements Landing 30°, 40° Ailerons Up 20° +2° Down 14° +2° Adj. stabilizer Up 0° 45' +15' Down 8° 45' +15' Elevator Up 25° +1° Down 22° 50' +1° (With stabilizer full down) Rudder Right 24° +1° Left 24° +1° (Measured parallel to 0.0.W.L.) Serial Nos. Eligible Model 182C: 631, 52359 thru 53007 (1960 Model) Model 182D: 51623, 18253008 thru 18253598 (1961 Model) V. Model 182E, Skylane, 4 PCLM (Normal Category), Approved June 27, 1961 Model 182F, Skylane, 4 PCLM (Normal Category), Approved August 1, 1962 Model 182G, Skylane, 4 PCLM (Normal Category), Approved July 19, 1963 Engine Continental O-470-L or 0-470-R *Fuel 80/87 minimum grade aviation gasoline *Engine Limits For all operations, 2600 r.p.m. (230 hp.) 3A13 Page 8 of 42 Rev. 76 V. Models 182E, 182F, 182G (cont’d) Propeller and 1. Hartzell constant speed Propeller Limits (a) Hub HC82XF-1 or HCA2XF-1 or BHCA2XF-1 with 8433-2 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 30 in. sta.: low 12°, high 24° (b) Cessna spinner 0752006 (c) Woodward governor 210065, 210105, 210155, or 210340 (Not eligible on O-470-R engine installation) 2. McCauley constant speed (a) Hub 2A36C1-U/90M-8, 2A36C18/90M-8 or 2A36C29/90M-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 0752004 (c) Woodward governor 210065, 210105, 210155, 210345, or 210452, or McCauley C290D2/T1 or C290D3/T1 3. Hartzell constant speed (a) Hub BHC-C2YF-1 with 8468-2 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 30 in. sta.: low 13°, high 24° (b) Cessna spinner 0752619 (c) Woodward governor 210105AF, 210340, or 210451 4. McCauley constant speed (a) Hub 2A34C50/90A-8 or 2A34C66/90AT-8 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 36 in. sta.: low 10.5°, high 21.5° (b) Cessna spinner 0752004 (c) Woodward governor 210065, 210105, 210155, 210345, or 210452, or Garwin 34-828-01, or McCauley C290D2/T1 or C290D3/T1 5. Aircraft reworked per Cessna Service Kit SK182-121: McCauley constant speed (Threadless) (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 25.0° (b) Cessna spinner 0752004 (c) Woodward governor 210065, 210105, 210155, 210345, or 210452, or Garwin 34-828-01, or McCauley C290D2/T1 or C290D3/T1 *Airspeed Limits Maneuvering 128 m.p.h. (111 knots) (CAS) Maximum structural cruising 160 m.p.h. (139 knots) Never exceed 193 m.p.h. (168 knots) Flaps extended 110 m.p.h. ( 96 knots) C.G. Range (+38.4) to (+47.4) at 2800 lb. (+33.0) to (+47.4) at 2250 lb. or less Straight line variation between points given. Empty Wt. C.G. Range None *Maximum Weight 2800 lb. No. of Seats 4 (2 at +36, 2 at +71) Maximum Baggage 120 lb. (+97) Rev. 76 Page 9 of 42 3A13 V. Models 182E, 182F, 182G (cont’d) Fuel Capacity 65 gal. (60 gal. usable); two 32.5 gal. tanks in wings at +48 (See NOTE 1 for data on unusable fuel). Oil Capacity 12 qt. (-15) (6 qt. usable) (See NOTE 1 for data on undrainable oil). Control Surface Wing flaps 40° +1°, -2° Movements 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 Right 24° +1° Left 24° +1° Serial Nos. Eligible Model 182E: 18253599 thru 18254423 (1962 Model) Model 182F: 18254424 thru 18255058 (1963 Model) Model 182G: 18255059 thru 18255844 (1964 Model) VI. Model 182H, Skylane, 4 PCLM (Normal Category), Approved September 17, 1964 Model 182J, Skylane, 4 PCLM (Normal Category), Approved October 20, 1965 Model 182K, Skylane, 4 PCLM (Normal Category), Approved August 3, 1966 Model 182L, Skylane, 4 PCLM (Normal Category), Approved July 28, 1967 Engine Continental O-470-R *Fuel 80/87 minimum grade aviation gasoline *Engine Limits For all operations, 2600 r.p.m. (230 hp.) Propeller and 1. McCauley constant speed Propeller Limits (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, or 210452, or Garwin 34-828-01, or McCauley C290D2/T1 or C290D3/T1 2. Aircraft reworked per Cessna Service Kit SK182-121: McCauley constant speed (Threadless) (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 25.0° (b) Cessna spinner 0752637 (c) Woodward governor 210065, 210105, 210155, 210345, or 210452, or Garwin 34-828-01, or McCauley C290D2/T1 or C290D3/T1 *Airspeed Limits Maneuvering 128 m.p.h. (111 knots) (CAS) Maximum structural cruising 160 m.p.h. (139 knots) Never exceed 193 m.p.h. (168 knots) Flaps extended 110 m.p.h. ( 96 knots) C.G. Range (+38.4) to (+47.4) at 2800 lb. (+33.0) to (+47.4) at 2250 lb. or less Straight line variation between points given. Empty Wt. C.G. Range None *Maximum Weight 2800 lb. 3A13 Page 10 of 42 Rev. 76 VI. Models 182H, 182J, 182K, 182L (cont’d) No. of Seats 4 (2 at +36, 2 at +71) Maximum Baggage 120 lb. (+97) Fuel Capacity 65 gal. (60 gal. usable); two 32.5 gal. tanks in wings at +48 See NOTE 1 for data on unusable fuel Oil Capacity 12 qt. (-15) (6 qt. usable) See NOTE 1 for data on undrainable oil Control Surface Wing flaps 40° +1°, -2° Movements 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 Right 24° +1° Left 24° +1° Serial Nos. Eligible Model 182H: 634, 18255846 thru 18256684 (1965 Model) Model 182J: 18256685 thru 18257625 (1966 Model) Model 182K: 18255845, 18257626 thru 18257698, 18257700 thru 18258505 (1967 Model) Model 182L: 18258506 thru 18259305 (1968 Model) VII. Model 182M, Skylane, 4 PCLM (Normal Category), Approved September 19, 1968 Engine Continental O-470-R *Fuel 80/87 minimum grade aviation gasoline *Engine Limits For all operations, 2600 r.p.m. (230 hp.) Propeller and 1. McCauley constant speed Propeller Limits (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, or 210452, or Garwin 34-828-01, or McCauley C290D2/T1 or C290D3/T1 2. McCauley constant speed (a) Hub 2A34C201/90DA-8 blades 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, 210155, 210345, or 210452, or Garwin 34-828-01, or McCauley C290D2/T1 or C290D3/T1 3. McCauley constant speed (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, 210105, 210155, 210345, or 210452, or Garwin 34-828-01, or McCauley C290D2/T1 or C290D3/T1 Rev. 76 Page 11 of 42 3A13 VII. Model 182M (cont’d) *Airspeed Limits Maneuvering 128 m.p.h. (111 knots) (CAS) Maximum structural cruising 160 m.p.h. (139 knots) Never exceed 193 m.p.h. (168 knots) Flaps extended 110 m.p.h. ( 96 knots) C.G. Range (+38.4) to (+47.4) at 2800 lb. (+33.0) to (+47.4) at 2250 lb. or less Straight line variation between points given Empty Wt. C.G. Range None *Maximum Weight 2800 lb. No. of Seats 4 (2 at +36, 2 at +71) Maximum Baggage 120 lb. (+97) Fuel Capacity 65 gal. (60 gal. usable); two 32.5 gal. tanks in wings at +48 (See NOTE 1 for data on unusable fuel). Oil Capacity 12 qt. (-15) (6 qt. usable) (See NOTE 1 for data on undrainable oil). Control Surface Wing flaps 40° +1°, -2° Movements 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 Right 24° +1° Left 24° +1° Serial Nos. Eligible 18257699, 18259306 thru 18260055 (1969 Model) VIII. Model 182N, Skylane, 4 PCLM (Normal Category), Approved September 17, 1969 Engine Continental O-470-R Continental O-470-S (See NOTE 4) *Fuel 80/87 minimum grade aviation gasoline *Engine Limits For all operations, 2600 r.p.m. (230 hp.) Propeller and 1. McCauley constant speed Propeller Limits (a) Hub 2A34C201/90DA-8 blades 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, 210155, 210345, or 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, or 210452, or Garwin 34-828-01, or McCauley C290D2/T1 or C290D3/T1 3A13 Page 12 of 42 Rev. 76 VIII. Model 182N (cont’d) Propeller and Propeller Limits (cont’d) 3. McCauley constant speed (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, 210105, 210155, 210345, or 210452, or Garwin 34-828-01, or McCauley C290D2/T1 or C290D3/T1 *Airspeed Limits Maneuvering 131 m.p.h. (114 knots) (CAS) Maximum structural cruising 160 m.p.h. (139 knots) Never exceed 198 m.p.h. (172 knots) Flaps extended 110 m.p.h. ( 96 knots) C.G. Range (+39.9) to (+47.4) at 2950 lb. (+38.4) to (+47.4) at 2800 lb. (+33.0) to (+47.4) at 2250 lb. or less Straight line variation between points given Empty Wt. C.G. Range None *Maximum Weight 2950 lb. takeoff only, 2800 lb. landing No. of Seats 4 Front standard (2 at +36 to +49) Optional (2 at +32 to +44) Rear (2 at +74) Maximum Baggage 120 lb. (+97) (S/N 18260056 thru 18260445) 120 lb. (+97) and 80 lb. (+117) (S/N 18260446 and On) Fuel Capacity 65 gal. (60 gal. usable); two 32.5 gal. tanks in wings at +48 (See NOTE 1 for data on unusable fuel). Oil Capacity 12 qt. (-15) (6 qt. usable) (See NOTE 1 for data on undrainable oil). Control Surface Wing flaps Down 40° +1°, -2° Movements Elevator tab Up 25° +2° Down 15° +1° Ailerons Up 20° +2° Down 15° +2° Elevator (rel. 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°