# TCDS 3A13: Textron Aviation Inc. - Type: Type certificate data sheet - Status: Current - Holder: Textron Aviation Inc. - Revision: 76 - Revised: October 8, 2026 - Product: Aircraft, Small Airplane - Certification basis: Part 23, CAR 3 - Registered aircraft: 13,936, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/ef/59/ef592b4f51febf5b7b82d159405ff159cb9133619bb83df2c8b7729aef6b8e38 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164282123520261008150658.0001 - Page: https://openairdocs.org/tcds/3A13 ## Models (23) As the data sheet lists them. - 182D - 182A - 182J - 182P - 182B - TR182 - 182L - 182G - 182Q - 182N - 182E - 182M - 182H - 182F - 182K - 182 - T182T - 182C - 182R - T182 - 182S - 182T - R182 ## 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 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° Serial Nos. Eligible 18260056 thru 18260445 (1970 Model) 18260446 thru 18260825 (1971 Model) Rev. 76 Page 13 of 42 3A13 IX. Model 182P, Skylane, 4 PCLM (Normal Category), Approved October 8, 1971 Engine Continental O-470-R, Aircraft S/N 18260826 through 18263475 Continental O-470-S, Aircraft S/N 18260826 and up (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 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 (S/N 675, 18260826 thru 18264295) (CAS) Maneuvering 126 m.p.h. (109 knots) 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) *Airspeed Limits (S/N 18264296 thru 18265175) (IAS) Maneuvering 110 knots (See NOTE 5 on use of IAS) Maximum structural cruising 141 knots Never exceed 176 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 Wt. C.G. Range None *Maximum Weight 2950 lb. No. of Seats 4 (2 front at +32.0 to +50.0) (2 rear at +74) 3A13 Page 14 of 42 Rev. 76 IX. Model 182P (cont’d) Maximum Baggage S/N 18260826 thru 18263475 200 lb. (120 lb. at + 82.0 to +108.0) (80 lb. at +108.0 to +124.0) S/N 675 and 18263476 thru 18265175 200 lb. (120 lb. at + 82.0 to +108.0) (80 lb. at +108.0 to +136.0) Fuel Capacity (S/N 675, 18260826 thru 18262250) Standard Range Tanks: 65 gal. (60 gal. usable); two 32.5 gal. tanks in wings at +48 Long Range Tanks: 84 gal. (79 gal. usable); two 42.0 gal. tanks in wings at +48 (S/N 18262251 thru 18265175) Standard Range Tanks: 61 gal. (56 gal. usable); two 29 gal. tanks in wings at +48 Long Range Tanks: 80 gal. (75 gal. usable); two 37 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° Serial Nos. Eligible 18260826 thru 18261425 (1972 Model) 18261426 thru 18262465 (1973 Model) 18262466 thru 18263475 (1974 Model) 675, 18263476 thru 18264295 except 18263479 (1975 Model) 18264296 thru 18265175 (1976 Model) X. Model 182Q, Skylane, 4 PCLM (Normal Category), Approved July 28, 1976 Engine Continental O-470-U *Fuel 100/130 minimum aviation grade gasoline (S/N 18265176 through 18265965) 100LL/100 aviation grade gasoline (S/N 18265966 through 18267715) *Engine Limits For all operations, 2400 r.p.m. (230 hp.) Propeller and McCauley constant speed Propeller Limits (a) Hub C2A34C204/90DCB-8 blades 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 Maneuvering 111 knots (IAS) Maximum structural cruising 143 knots (See NOTE 5 on use of IAS) Never exceed 179 knots Flaps extended 95 knots Rev. 76 Page 15 of 42 3A13 X. Model 182Q (cont’d) 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 Wt. C.G. Range None *Maximum Weight 2950 lb. No. of Seats 4 (2 front at +32.0 to +50.0) (2 rear at +74) 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 (S/N 18263479, 18265176 thru 18266590) Long Range Tanks: 80 gal. (75 gal. usable); two 40.0 gal. tanks in wings at +48 (S/N 18263479, 18265176 thru 18266590) 92 gal. (88 gal. usable); two 46.0 gal. integral tanks in wings at +46.5 (S/N 18266591 thru 18267715) (See NOTE 1 for data on unusable fuel). Oil Capacity 12 qt. (-15.0) (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° Serial Nos. Eligible 18265176 thru 18265965 (1977 Model) 18263479, 18265966 thru 18266590 (1978 Model) 18266591 thru 18267300 (1979 Model) 18267301 thru 18267715, except 18267302 (1980 Model) XI. Model R182, Skylane RG, 4 PCLM (Normal Category), Approved July 7, 1977 Model TR182, Turbo Skylane RG, 4 PCLM (Normal Category), Approved September 12, 1978 Model R182 Engine Lycoming O-540-J3C5D, rated at 235 hp. *Fuel 100LL/100 aviation grade gasoline *Engine Limits Full throttle for all operations, 2400 r.p.m. 3A13 Page 16 of 42 Rev. 76 XI. Models R182, TR182 (cont’d) Model R182 (cont’d) Propeller and 1. McCauley constant speed (S/N R18200002 thru R18201313) Propeller Limits (a) Hub B2D34C214/90DHB-8 blades Diameter: not over 82 in., not under 80.5 in. Pitch settings at 30 in. sta.: low 15.8°, high 29.4° (b) Cessna prop & spinner installation 2250003 Cessna spinner installation 1750050 (c) McCauley governor C290D3/T16 (d) McCauley governor DC290D1/T4 2. McCauley constant speed (S/N R18201314 and On) (a) Hub B2D34C218/90DHB-8 blades Diameter: not over 82 in., not under 80.5 in. Pitch settings at 30 in. sta.: low 15.8°, high 29.4° (b) Cessna prop & spinner installation 2250124 Cessna spinner installation 2250123 (c) McCauley governor C290D3/T22 (d) McCauley governor DC290D1/T8 3. McCauley constant speed (S/N R18201629 thru R18202041 and aircraft reworked per SK182-71) (a) Hub B3D32C407/82NDA-3 blades Diameter: not over 79 in., not under 78 in. Pitch settings at 30 in. sta.: low 16.0°, high 31.7° (b) Cessna prop & spinner installation 2252076 Cessna spinner installation 2252074 (c) McCauley governor C290D3/T22 (d) McCauley governor DC290D1/T8 Model TR182 Engine Lycoming O-540-L3C5D, rated at 235 hp. (Turbocharged in accordance with Cessna Drawing No. 2250065) *Fuel 100LL/100 aviation grade gasoline *Engine Limits For all operations, 2400 r.p.m., 31 in. hg. mp. Propeller and 1. McCauley constant speed (S/N R18200001, R18200584 through Propeller Limits R18201313) (a) Hub B2D34C217/90DHB-8 blades Diameter: not over 82 in., not under 80.5 in. Pitch settings at 30 in. sta.: low 15.8°, high 31.9° (b) Cessna prop & spinner installation 2250003 Cessna spinner installation 1750050 (c) McCauley governor C290D3/T21 (d) McCauley governor DC290D1/T7 Rev. 76 Page 17 of 42 3A13 XI. Models R182, TR182 (cont’d) Model TR182 (cont’d) Propeller and 2. McCauley constant speed (S/N R18201314 and on) Propeller Limits (cont’d) (a) Hub B2D34C219/90DHB-8 blades Diameter: not over 82 in., not under 80.5 in. Pitch settings at 30 in. sta.: low 15.8°, high 31.9° (b) Cessna prop & spinner installation 2250124 Cessna spinner installation 2250123 (c) McCauley governor C290D3/T22 (d) McCauley governor DC290D1/T8 3. McCauley constant speed (S/N R18201315, R18201629 and on and aircraft reworked per SK182-71 or SK182-72) (a) Hub B3D32C407/82NDA-3 blades Diameter: not over 79 in., not under 78 in. Pitch settings at 30 in. sta.: low 16.0°, high 31.7° (b) Cessna prop & spinner installation 2252076 Cessna spinner installation 2252074 (c) McCauley governor C290D3/T22 (d) McCauley governor DC290D1/T8 *Airspeed Limits 1978 Model R182 Maneuvering 112 knots (IAS) Maximum structural cruising 143 knots (See NOTE 5 on use of IAS) Never exceed 182 knots Flaps extended 95 knots Landing gear extension 140 knots 1979 Model R182 Maneuvering 112 knots Maximum structural cruising 160 knots Never exceed 182 knots Flaps extended 95 knots Landing gear extension 140 knots Model TR182 Maneuvering 112 knots Maximum structural cruising 157 knots Never exceed 179 knots Flaps extended 95 knots Landing gear extension 140 knots 1980 and up Model R182 Maneuvering 112 knots Maximum structural cruising 159 knots Never exceed 181 knots Flaps extended 95 knots Landing gear extension 140 knots Model TR182 Maneuvering 112 knots Maximum structural cruising 157 knots Never exceed 178 knots Flaps extended 95 knots Landing gear extension 140 knots C.G. Range (a) S/N R18200001 through R18201628 except R18200975 & R18201315 (+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 Moment change due to retracting gear (+3052 in.-lb.) (b) S/N R18200975, R18201315, R18201629 through R18202041 (+40.9) to (+46.0) at 3100 lb. (+35.5) to (+46.0) at 2700 lb. (+33.0) to (+46.0) at 2250 lb. or less Straight line variation between points given Moment change due to retracting gear (+3052 in.-lb.) 3A13 Page 18 of 42 Rev. 76 XI. Models R182, TR182 (cont’d) Model TR182 (cont’d) Empty Wt. 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) S/N R18200002 thru R18200583 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 (b) S/N R18200001, R18200584 thru R18202041 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. (-14.8) (See NOTE 1 for data on oil). Control Surface (a) S/N R18200001 thru R18201628 except R18200975 & R18201315 Movements Wing flaps Down 40° +1°, -2° Elevator tab Up 25° +2° Down 15° +1° Ailerons Up 20° +2° Down 15° +2° Elevator (rel. 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° (b) S/N R18200975, R18201629 thru R18201798 Wing flaps Down 40° +1°, -2° Elevator tab Up 24° +2° Down 15° +1° Ailerons Up 20° +2° Down 15° +2° Elevator (rel. to stabilizer) Up 28° +1° Down 21° +1° Rudder (parallel to 0.00 W.L.) Right 24° +0°, -1° Left 24° +0°, -1° (Perpendicular to hinge line) Right 27° 13' +0°, -1° Left 27° 13' +0°, -1° (c) S/N R18201315, R18201799 thru R18202041 Wing flaps Down 38° +0°, -1° Elevator tab Up 24° +2° Down 15° +1° Ailerons Up 20° +1° Down 15° +2° Elevator (rel. to stabilizer) Up 28° +1° Down 21° +1° Rudder (parallel to 0.00 W.L.) Right 24° +0°, -1° Left 24° +0°, -1° (Perpendicular to hinge line) Right 27° 13' +0°, -1° Left 27° 13' +0°, -1° Serial Nos. Eligible Model R182: R18200002 thru R18200583 (1978 Model) Model R182/TR182: R18200001, R18200584 thru R18201313 (1979 Model) Model R182/TR182: R18201314 thru R18201628 except R18201315 (1980 Model) Model R182/TR182: R18201629 thru R18201798 (1981 Model) Model R182/TR182: R18201799 thru R18201928 (1982 Model) Model R182/TR182: R18201929 thru R18201973 (1983 Model) Model R182/TR182: R18201974 thru R18201999 (1984 Model) Model R182/TR182: R18201315, R18202000 thru R18202031 (1985 Model) Model R182/TR182: R18202032 thru R18202041 (1986 Model) Rev. 76 Page 19 of 42 3A13 XII. Model 182R, 4 PCLM (Normal Category), Approved August 29, 1980 Model T182, 4 PCLM (Normal Category), Approved August 15, 1980 Model 182R Engine Continental O-470-U *Fuel 100LL/100 aviation grade gasoline *Engine Limits For all operations, 2400 r.p.m. (230 hp.) Propeller and McCauley constant speed Propeller Limits (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 Model T182 Engine Lycoming 0-540-L3C5D, rated at 235 hp. (Turbocharged in accordance with Cessna Drawing No. 2250065) *Fuel 100LL/100 aviation grade gasoline *Engine Limits For all operations, 2400 r.p.m., 31 in. Hg. mp. Propeller and 1. McCauley constant speed Propeller Limits (a) Hub B2D34C219/90DHB-8 Diameter: not over 82 in., not under 80.5 in. Pitch settings at 30 in. sta.: low 15.8°, high 31.9° (b) Cessna spinner 2250124 (c) McCauley governor C290D3/T22 (d) McCauley governor DC290D1/T8 2. McCauley constant speed (a) Hub B3D32C407/82NDA-3 Diameter: not over 79 in., not under 78 in. Pitch settings at 30 in. sta.: low 16.0°, high 31.7° (b) Cessna spinner 2252076 (c) McCauley governor C290D3/T22 (d) McCauley governor DC290D1/T8 *Airspeed Limits Model 182R Maneuvering 111 knots (IAS) Maximum structural cruising 143 knots (See NOTE 5 on use of IAS) Never exceed 179 knots Flaps extended 95 knots Model T182 Maneuvering 111 knots Maximum structural cruising 140 knots Never exceed 178 knots Flaps extended 95 knots C.G. Range Model 182R (+40.9) to (+46.0) at 3100 lb. (+33.0) to (+46.0) at 2250 lb. or less Straight line variation between points given Model T182 (+40.9) to (+46.0) at 3100 lb. (+35.5) to (+46.0) at 2700 lb. (+33.0) to (+46.0) at 2250 lb. or less Straight line variation between points given Empty Wt. C.G. Range None 3A13 Page 20 of 42 Rev. 76 XII. Models 182R, T182 (cont’d) *Maximum Weight 3100 lb. takeoff/flight 2950 lb. landing No. of Seats 4 (2 front at +32.0 to +50.0) (2 rear at +74.0) Maximum Baggage 200 lb. (120 lb. at +92.0 to +108.0) (80 lb. at +108.0 to +136.0) Fuel Capacity 92 gal. (88 gal. usable); two 46 gal. integral tanks in wings at +46.5 (See NOTE 1 for data on unusable fuel). Oil Capacity Model 182R Model T182 12 qt. (-15.0) 9 qt (-14.8) (6 qt. usable) (6 qt. usable) (thru S/N 18268055) 12 qt. (-14.1) (6 qt. usable) (S/N 18268056 and On) (See NOTE 1 for data on oil) Control Surface (a) S/N 18267716 thru 18268055 Movements Wing flaps Down 40° +1°, -2° Elevator tab Up 24° +2° Down 15° +1° Ailerons Up 20° +2° Down 15° +2° Elevator (rel. to stabilizer) Up 28° +1° Down 21° +1° Rudder (parallel to 0.00 W.L.) Right 24° +0°, -1° Left 24° +1°, -0° (Perpendicular to hinge line) Right 27° 13' +0°, -1° Left 27° 13' +0°, -1° (b) S/N 18268056 thru 18268586 Wing flaps Down 38° +0°, -1° Elevator tab Up 24° +2° Down 15° +1° Ailerons Up 20° +2° Down 15° +2° Elevator (rel. to stabilizer) Up 28° +1° Down 21° +1° Rudder (parallel to 0.00 W.L.) Right 24° +0°, -1° Left 24° +0°, -1° (Perpendicular to hinge line) Right 27° 13' +0°, -1° Left 27° 13' +0°, -1° Serial Nos. Eligible Model 182R/T182: 18267302, 18267716 through 18268055 (1981 Model) Model 182R/T182: 18268056 through 18268293 (1982 Model) Model 182R/T182: 18268294 through 18268368 (1983 Model) Model 182R/T182: 18268369 through 18268434 (1984 Model) Model 182R/T182: 18268435 through 18268541 (1985 Model) Model 182R: 18268542 through 18268586 (1986 Model) Rev. 76 Page 21 of 42 3A13 Data Pertinent to Model Items I through XII Datum Front face of firewall Leveling Means Upper door sill. Top surface centerline of tailcone (S/N 18253599 thru 18265965) Jig located nutplates and screws on left of tailcone (S/N 18263479, 18265966 thru 18268586) (S/N R18200001 thru 18202041) Certification Basis: Model 182 Series Part 3 of the Civil Air Regulations (CAR), dated November 1, 1949, as amended by 3-1 through 3-12 and Paragraph 3.112 as amended October 1, 1959, for Model 182E and On. In addition, effective S/N 18266591 through 18268586, FAR 23.1559 effective March 1, 1978. FAR Part 36 dated December 1, 1969, plus Amendments 36-1 through 36-6 for Model 182Q and On. In addition, effective S/N 18268435 through 18268586, 23.1545(a) Amendment 23-23 dated December 1, 1978. Model T182 CAR Part 3 dated November 1, 1949, as amended by 3-1 through 3-12 and Paragraph 3.112 as amended October 1, 1959. FAR Part 23 dated February 1, 1965, 23.901, 23.909, 23.1041, 23.1043, 23.1143, 23.1305 as amended February 14, 1975; 23.1559 effective March 1, 1978; FAR Part 36 dated December 1, 1969, plus Amendments 36-1 through 36-10. In addition, effective S/N 18268435 through 18268541, 23.1545(a) Amendment 23-23 dated December 1, 1978. Model R182 CAR Part 3 dated November 1, 1949, as amended by 3-1 through 3-12 and Paragraph 3.112 as amended October 1, 1959. FAR Part 23 dated February 1, 1965, 23.729, 23.777(e), 23.781, 23.1555(e)(1)(2), 23.1563 as amended February 14, 1975. In addition, effective S/N R18200001, R18200584 and On; 23.1559 effective March 1, 1978. FAR Part 36 dated December 1, 1969, plus Amendments 36-1 through 36-6. In addition, effective at S/N R18202000 through R18202041, 23.1545(a) Amendment 23-23 dated December 1, 1978. Model TR182 CAR Part 3 dated November 1, 1949, as amended by 3-1 through 3-12 and Paragraph 3.112 as amended October 1, 1969. FAR Part 23 dated February 1, 1965, 23.729, 23.777(e), 23.781, 23.901, 23.909, 23.1041, 23.1043, 23.1143, 23.1305, 23.1555(e)(1)(2), 23.1563 as amended February 14, 1975; 23.1559 effective March 1, 1978; FAR Part 36 dated December 1, 1969, plus Amendments 36-1 through 36-9. In addition, effective at S/N R18202000 through R18202041, 23.1545(a) Amendment 23-23 dated December 1, 1978. Application for Type Certificate dated July 11, 1955. Type Certificate No. 3A13 issued March 2, 1956, obtained by the manufacturer under delegation option procedures. Equivalent Safety Items: S/N 18263479, 18264296 through 18267715 Airspeed Indicator CAR 3.757 (See NOTE 5 on use of IAS) Operating Limitations CAR 3.778(a) S/N 18267716 through 18268586 Airspeed Indicator CAR 3.757 (See NOTE 5 on use of IAS) (S/N 18267716 through 18268434) Operating Limitations CAR 3.778(a) Fuel System CAR 3.430 S/N R18200001 through R18202041 Airspeed Indicator CAR 3.757 (See NOTE 5 on use of IAS) (S/N R18200001 through R18201999) Operating Limitations CAR 3.778(a) Fuel System CAR 3.430 3A13 Page 22 of 42 Rev. 76 Data Pertinent to Model Items I through XII (cont’d) Production Basis: Production Certificate No. 4. Delegation Option Manufacturer No. CE-1 authorized to issue airworthiness certificates under delegation option provisions of Part 21 of the Federal Aviation Regulations. 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 AFM, effective at S/N 18266591 thru 18268586 and R18200584 thru R18202041. In addition, the following item of equipment is required: Stall warning indicator, Cessna Dwg. S1672-5. The equipment portion of Aircraft Specification 3A13, Revision 15, or Cessna Publication TS3000-13 should be used for equipment references on all aircraft prior to the Model 182G. Refer to the applicable Equipment List for the Model 182G and subsequent models. NOTE 1: Current weight and balance report including list of equipment included in certificated empty weight, and loading instructions when necessary, must be provided for each aircraft at the time of original certification. Serial Numbers: 613 and 33000 thru 34999 631 and 51001 thru 53007 18253008 thru 18264295 except 18263479 The certificated empty weight and corresponding center of gravity location must include unusable fuel of 30 lb. (+46) on Models 182, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P through S/N 18264295 and 60 lb. (+46) on Models 182A, 182B, 182C, 182D and undrainable oil of (0) lb. Serial Numbers: 18263479, 18264296 thru 18266590 The certificated empty weight and corresponding center of gravity location must include unusable fuel of 30 lb. (+46) and full oil of 22.5 lb. at (-15.0). Serial Numbers: 18266591 thru 18268055 The certificated empty weight and corresponding center of gravity location must include unusable fuel of 24 lb. at (+48) and full oil of 22.5 lb. at (-15.0) for Models 182Q, 182R, and include oil of 16.9 lb. at (-14.8) for Model T182. Serial Numbers: 18268056 thru 18268586 The certificated empty weight and corresponding center of gravity location must include unusable fuel of 24 lb. at (+48) and full oil of 24.4 lb. at (-14.1) for Model 182R and include oil of 16.9 lb. at (-14.8) for Model T182. Serial Numbers: R18200002 thru R18200583 The certificated empty weight and corresponding center of gravity location must include unusable fuel of 30 lb. (+46) and include oil of 16.9 lb. (-15.7). Serial Numbers: R18200001, R18200584 thru R18202041 The certificated empty weight and corresponding center of gravity location must include unusable fuel of 24 lb. (+48) and include oil of 16.9 lb. (-14.8). Rev. 76 Page 23 of 42 3A13 NOTE 2: The following placards must be displayed in locations as indicated: A. Applicable to Model 182 only: (1) In full view of the pilot: (a) "This airplane must be operated as a normal category airplane in compliance with operating limitations stated in the form of placards, markings and manuals. No acrobatic maneuvers including spins approved. Flight Maneuvering Load Factors Flaps Up +3.8 -1.52 Flaps Down +3.5 Maximum design weight 2550 lb. Reference weight and balance data for loading instructions." (b) "Both tanks on for takeoff and landing." (c) "Flaps - Pull to extend Takeoff Retracted 0° 1st Notch 10° 2nd Notch 20° Landing 3rd Notch 30° 4th Notch 40° (2) In baggage compartment "Maximum baggage 120 lb. For additional loading instructions see weight and balance data." B. Applicable to Models 182A, 182B, 182C, 182D (1) In full view of the pilot: (a) "This airplane must be operated as a normal category airplane in compliance with operating limitations stated in the form of placards, markings and manuals. No acrobatic maneuvers including spins approved. Flight Maneuvering Load Factors Flaps Up +3.8 -1.52 Flaps Down +3.5 Maximum design weight 2650 lb. Reference weight and balance data for loading instructions." (b) "Both tanks on for takeoff and landing." (c) "Flaps - Pull to extend Takeoff Retracted 0° 1st Notch 10° 2nd Notch 20° Landing 3rd Notch 30° 4th Notch 40°" (2) In baggage compartment "Maximum baggage 120 lb. For additional loading instructions see weight and balance data." C. Applicable to Models 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M (1) In full view of the pilot: (a) "This airplane must be operated as a normal category airplane in compliance with operating limitations stated in the form of placards, markings and manuals. No acrobatic maneuvers including spins approved. Flight Maneuvering Load Factors Flaps Up +3.8 -1.52 Flaps Down +3.5 Maximum design weight 2800 lb. Reference weight and balance data for loading instructions." (2) On the fuel selector valve plate: "Both off. Left tank level flight only 31 gal. Both on for landing and takeoff all flight attitudes 60 gal. Right tank level flight only 31 gal." (3) On the control lock: "Control lock - Remove before starting engine." (4) On the baggage door: "120 lb. maximum baggage and/or auxiliary seat passengers. For additional loading instructions, see weight and balance data. 3A13 Page 24 of 42 Rev. 76 Data Pertinent to Model Items I through XII (cont’d) D. Applicable to Models 182N: (1) In full view of the pilot: (a) S/N 18260056 thru 18260445 "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. No acrobatic maneuvers approved, including spins. Maximums Design weight 2950 lb. takeoff Alt. loss in stall recovery-160 ft. 2800 lb. landing Flight Maneuvering Load Factors Maneuvering speed 131 m.p.h.-CAS Flaps up +3.8, -1.52, Flaps down +3.5 Reference weight and balance data for loading instructions" (b) S/N 182670446 thru 18260825 "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 131 m.p.h. CAS (114 knots) Gross weight Takeoff 2950 lb. Landing 2800 lb. Flight load factor Flaps up +3.8, -1.52 Flaps down +3.5 No acrobatic maneuvers approved, including spins. Altitude loss in a stall recovery 160 ft. Known icing conditions to be avoided. 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: "Both off. Left tank level flight only 31 gal. Both on for landing and takeoff all flight attitudes, 60 gal. Right tank level flight only 31 gal." (3) On the control lock: "Control lock - Remove before starting engine." (4) On the baggage door: (a) "120 lb. maximum baggage and/or auxiliary seat passengers. For additional loading instructions, see weight and balance data." Applicable to Model 182N, S/N 18260056 thru 18260445. (b) "120 lb. maximum baggage and/or auxiliary passenger forward of baggage door latch, and 80 pounds maximum baggage aft of baggage door latch. Maximum 200 lb. combined. For additional loading instructions see weight and balance data." Applicable to Model 182N, S/N 18260446 and On. (5) On flap control indicator: (a) "0° to 20° - T.O." (b) "10° - 20° - Full. (Indices at these positions with blue color code and 160 m.p.h. callout, and white color code with 110 m.p.h. callout; mechanical detent at 10° and 20°)" Rev. 76 Page 25 of 42 3A13 Data Pertinent to Model Items I through XII (cont’d) E. Applicable to Model 182P: (1) In full view of the pilot: (S/N 675, 18260826 through 18264295) (a) "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 126 m.p.h. CAS (109 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. Known icing conditions to be avoided. This airplane is certified for the following flight operations as of date of original airworthiness certificate: DAY-NIGHT-VFR-IFR." (as applicable) (S/N 18264296 through 18265175) NOTE 2. (cont’d) E. Applicable to Model 182P: (cont’d) (b) "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 approved, including spins. 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: (S/N 675, 18260826 thru 18262250) Standard range tanks: "Off. Left tank level flight only 31 gal. Both on for landing and takeoff all flight attitudes, 60 gal. Right tank level flight only 31 gal." Long range tanks: "Off. Left tank level flight only 39 gal. Both on for landing and takeoff all flight attitudes, 79 gal. Right tank level flight only 39 gal." On the fuel selector valve plate: (S/N 182622251 thru 18265175) 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: (S/N 18260826 thru 18263475) "120 lb. maximum baggage and/or auxiliary passenger forward of baggage door latch, and 80 lb. maximum baggage aft of baggage door latch. Maximum 200 lb. combined. For additional loading instructions, see weight and balance data." On the baggage door: (S/N 675, 18263476 through 18265175) "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: (S/N 675, 18260826 thru 18264295) "(a) 0° to 10° - (Blue color code and 160 m.p.h. callout; also, mechanical detent at 10°) (b) 10° to 20°- Full (Indices at these positions with white color code and 3A13 Page 26 of 42 Rev. 76 110 m.p.h. callout; also, mechanical detent at 10° and 20°)" On flap control indicator (S/N 18264296 thru 18265175) "(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°)" Rev. 76 Page 27 of 42 3A13 Data Pertinent to Model Items I through XII (cont’d) NOTE 2. (cont’d) (6) Forward of the filler cap on the wing surface: (S/N 675, 18260826 through 18262250) Standard range tanks: "Service this airplane with 80/87 minimum aviation grade gasoline. Capacity 32.5 gal." Long range tanks: "Service this airplane with 80/87 minimum aviation grade gasoline. Capacity 42.0 gal." Forward of the filler cap on the wing surface: (S/N 18262251 through 18265175) 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) (8) Adjacent to overvoltage light: "High voltage." (9) Above the left fuel gauge: "Do not turn off alternator in flight except in emergency." (Model 182P, S/N 18260826 thru 18261425) F. Applicable to Model 182Q: (1) In full view of the pilot: (a) S/N 18263479, 18265176 thru 18266590 "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) S/N 18266591 thru 18267715 "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 POH/AFM. 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) (b) Near airspeed indicator: S/N 18266591 thru 18267715 "Maneuver Speed 111 KIAS" 3A13 Page 28 of 42 Rev. 76 Data Pertinent to Model Items I through XII (cont’d) NOTE 2. (cont’d) (2) On the fuel selector valve plate: S/N 18263479, 18265176 through 18266590 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." S/N 18266591 thru 18267715 "Take Off - Both - Landing, All Flight - 88.0 Gal. - Attitudes Left - 44.0 Gal. Level Flight Only Right - 44.0 Gal. Level Flight Only Off." (3) On the control lock: "Control lock - remove before starting engine." (4) On the baggage door: "Forward of baggage door latch, 120 pounds maximum baggage and/or auxiliary passenger. Aft of baggage door latch, 80 pounds maximum baggage including 25 pounds maximum in baggage wall hat shelf. Maximum 200 pounds combined. For additional loading instructions, see weight and balance data." (5) On flap control indicator: "0° to 10° - (Blue color code and 140 KTS callout; also, mechanical detent at 10°)" "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: S/N 18265176 thru 18265965 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." S/N 18263479, 18265966 thru 18266590 Standard range tanks: "Service this airplane with 100LL/100 aviation grade gasoline. Capacity 30.5 gal." Long range tanks: "Service this airplane with 100LL/100 aviation grade gasoline. Capacity 40.0 gal." S/N 18266591 thru 18267715 "Fuel 100LL/100 minimum grade aviation gasoline. Capacity 46 U.S. gal. Capacity 34.5 U.S. gal. To bottom of filler collar." Rev. 76 Page 29 of 42 3A13 Data Pertinent to Model Items I through XII (cont’d) NOTE 2. (cont’d) (7) On aft panel of baggage compartment: "Oxygen refill." (All models with oxygen) (8) Adjacent to overvoltage light: S/N 18263479, 18265176 through 18266590 "High Voltage" S/N 18266591 through 18267715 "Low Voltage" G. Applicable to Models R182, TR182, S/N R18200001 thru R18201928: (1) In full view of the pilot: (a) S/N R18200002 thru R18200583 "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 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) S/N R18200001, R18200584 thru R18202041 "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) S/N R18200002 thru R18200583 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." 3A13 Page 30 of 42 Rev. 76 Data Pertinent to Model Items I through XII (cont’d) NOTE 2. (cont’d) (b) S/N R18200001, R18200584 thru R18201798 "Take Off - Both - Landing, All Flight - 88.0 Gal. - Attitudes Left - 44.0 Gal. Level Flight Only Right - 44.0 Gal. Level Flight Only Off." (c) S/N R18201799 thru R18202041 "Both - 88.0 Gal. - Take Off - Landing - All Flight Attitudes; Left - 44.0 Gal. - Level Flight Only Right - 44.0 Gal. - Level Flight Only Off - Off." (3) On the control lock: (a) S/N R18200001 thru R18201798 "Control lock - Remove before starting engine." (b) S/N R18201799 thru R18202041 "Caution! Control Lock - Remove before starting engine." (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 the flap control indicator: "0° to 10° - (Blue color code and 140 KTS callout; also, mechanical detent at 10°)" "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) S/N R18200002 thru R18200583 Standard range tanks: "Service this airplane with 100LL/100 aviation grade gasoline. Capacity 30.5 gal." Long range tanks: "Service this airplane with 100LL/100 aviation grade gasoline. Capacity 40.0 gal." (b) S/N R18200001, R18200584 thru R18202041 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) S/N R18200002 through R18200583 "High Voltage" (b) S/N R18200001, R18200584 through R18202041 "Low Voltage" Rev. 76 Page 31 of 42 3A13 Data Pertinent to Model Items I through XII (cont’d) NOTE 2. (cont’d) (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" (9) Forward of each fuel filler cap: "Fuel Cap Forward - Arrow Alignment, Cap Must Not Rotate During Closing." H. Applicable to Models 182R and T182, S/N 18267302, 18267716 through 18268293: (1) In full view of the pilot: (a) "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 (POH) and FAA Approved Airplane Flight Manual (AFM). 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) (b) Near airspeed indicator: "Maneuver Speed 111 KIAS" (2) On the fuel selector valve plate: (a) S/N 18267716 thru 18268055 "Take Off - Both - Landing, - All Flight - 88.0 Gal. - Attitudes Left - 44.0 Gal. Level Flight Only Right - 44.0 Gal. Level Flight Only Off." (b) S/N 18268056 thru 18268586 "Both - 88.0 Gal. - Takeoff - Landing - All Flight Attitudes Left - 44.0 Gal. - Level Flight Only Right - 44.0 Gal. - Level Flight Only Off - Off." (3) On the control lock: (a) S/N 18267716 thru 18268055 "Control Lock - Remove before starting engine." (b) S/N 18268056 thru 18268586 "Caution! Control Lock - Remove before starting engine." (4) On 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" 3A13 Page 32 of 42 Rev. 76 Data Pertinent to Model Items I through XII (cont’d) NOTE 2. (cont’d) (5) On flap control indicator: "0° to 10° - (Blue color code and 140 KTS callout; also, mechanical detent at 10°)" "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: "Fuel 100LL/100 minimum grade aviation gasoline. Capacity 46 U.S. gal. Capacity 34.5 U.S. gal. To bottom of filler collar." (7) Forward of each fuel filler cap: "Fuel cap fwd - arrow alignment, cap must not rotate during closing." (8) Adjacent to overvoltage light: "Low Voltage" I. Applicable to Models R182 and TR182, S/N R18201929 thru R18202041: All placards required in the POH/AFM must be installed in the appropriate locations. J. Applicable to Models 182R and T182, S/N 18268294 thru 18268586: All placards required in the POH/AFM must be installed in the appropriate locations. NOTE 3. The cylinder head thermistors must be installed as follows: Model Engine and Cylinder Head Number O-470-R O-470-S O-470-U O-540-J O-540-L 182N (1970 and 1971 Model) 3 3 N/A N/A N/A 182P (1972 and 1973 Model) 2 3 N/A N/A N/A 182P (1974 Model) 1 3 N/A N/A N/A 182P (1975 and 1976 Model) N/A 3 N/A N/A N/A 182Q (1977 through 1980 Model) N/A N/A 3 N/A N/A 182R (1981 Model through 18268160) N/A N/A 5 N/A N/A 182R (18268161 through 18268586) N/A N/A 3 N/A N/A T182 (1981 Model through 1985 Model) N/A N/A N/A N/A 1 R182 (1978 and 1979 Model) N/A N/A N/A 5 N/A R182 (1980 Model through 1986 Model) N/A N/A N/A 4 N/A TR182 (1979 Model) N/A N/A N/A N/A 3 TR182 (1980 Model through 1986 Model) N/A N/A N/A N/A 5 NOTE 4. The installation of the 0-470-S engine in Model 182N, 182P (1970 through 1974) will require a change of the oil temperature gauge. Reference Cessna Service Letter SE75-2 for information and instructions for this change. NOTE 5. 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 POH listed below is available to the pilot: 182P Cessna P/N D1062-13 S/N 18264296 thru 18265175 182Q Cessna P/N D1087-13 S/N 18265176 thru 18265965 182Q Cessna P/N D1114-13 S/N 18263479, 18265966 thru 18266590 182Q Cessna P/N D1141-13PH S/N 18266591 thru 18267300 182Q Cessna P/N D1176-13PH S/N 18267301 thru 18267715 Rev. 76 Page 33 of 42 3A13 Data Pertinent to Model Items I through XII (cont’d) NOTE 5. (cont’d) 182R Cessna P/N D1196-13PH S/N 18267716 thru 18268055 182R Cessna P/N D1215-13PH S/N 18268056 thru 18268293 182R Cessna P/N D1233-13PH S/N 18268294 thru 18268368 182R Cessna P/N D1254-13PH S/N 18268369 thru 18268434 T182 Cessna P/N D1197-13PH S/N 18267302, 18267716 thru 18268055 T182 Cessna P/N D1216-13PH S/N 18268056 thru 18268293 T182 Cessna P/N D1234-13PH S/N 18268294 thru 18268368 T182 Cessna P/N D1234R1-13PH (Special) S/N 18268365 T182 Cessna P/N D1255-13PH S/N 18268369 thru 18268434 R182 Cessna P/N D1115-13 S/N R18200002 thru R18200583 R182 Cessna P/N D1142-13PH S/N R18200584 thru R18201313 R182 Cessna P/N D1177-13PH S/N R18201314 thru R18201628 R182 Cessna P/N D1198-13PH S/N R18201629 thru R18201798 R182 Cessna P/N D1217-13PH S/N R18201799 thru R18201928 R182 Cessna P/N D1235-13PH S/N R18201929 thru R18201973 R182 Cessna P/N D1256-13PH S/N R18201974 thru R18201999 R182 Cessna P/N D1277-13PH S/N R18202000 thru R18202031 R182 Cessna P/N D1299-13PH S/N R18202032 thru R18202041 TR182 Cessna P/N D1143-13PH S/N R18200001, R18200584 thru R18201313 except R18200975 TR182 Cessna P/N D1143-2-13PH (Special) S/N R18200975 TR182 Cessna P/N D1178-13PH S/N R18201314 thru R18201628 except R18201315 TR182 Cessna P/N D1199-13PH S/N R18201629 thru R18201798 TR182 Cessna P/N D1218-13PH S/N R18201799 thru R18201928 TR182 Cessna P/N D1236-13PH S/N R18201929 thru R18201973 TR182 Cessna P/N D1257-13PH S/N R18201974 thru R18201999 TR182 Cessna P/N D1278-13PH S/N R18201315, R18202000 thru R18202031 TR182 Cessna P/N D1300-13PH S/N R18202032 thru R18202041 NOTE 6. 14-volt electrical system (182 series through S/N 18265965 except 18263479) 28-volt electrical system (182 series S/N 18263479, 18265966 thru 18268586) (R182 and TR182 series S/N R18200001 thru R18202041) NOTE 7. Special Ferry Flight Authorization. Flight Standards District Offices are authorized to issue Special overweight ferry flight authorizations. These airplanes are structurally satisfactory for ferry flight if maintained within the following limits: 1. Takeoff weight must not exceed 130% of the maximum weight for Normal Category. 2. The Never Exceed Airspeed (VNE) and Maximum Structural Cruising Speed (VC) must be reduced by 30%. 3. Forward and aft center of gravity limits may not be exceeded. 4. Structural load factors of +2.5 g. to -1.0 g. may not be exceeded. Requirements for any additional engine oil should be established in accordance with AC 23.1011-1. Increased stall speeds and reduced climb performance should be expected for the increased weights. Flight characteristics and performance at the increased weights have not been evaluated. Procedures for issuing a Flight Permit for operations of overweight aircraft may be found in AC 21-4B. In addition to the above specified placards, the prescribed operating limitations indicated by an asterisk (*) under Sections I through XII must also be displayed by permanent markings. 3A13 Page 34 of 42 Rev. 76 XIII. Model 182S, Skylane, 4 PCLM (Normal Category), Approved 03 October 1996. Model 182T, Skylane, 4 PCLM (Normal Category), Approved 23 February 2001. Engine Lycoming IO-540-AB1A5. Rated 230 Horsepower Fuel 100/100LL minimum grade aviation gasoline Engine Limits For all operations, 2400 RPM Propeller (1) McCauley Constant Speed (182S) (a) Hub B2D34C235/90DKB-8 (2 blades) Diameter: not over 82 in., not under 80.5 in. Pitch settings at 30 in. sta.: Low 17.0º, High 31.8º (b) McCauley Spinner: D-7267-2 (c) McCauley Governor: DC290D1/T8 (2) McCauley Constant Speed (182S, 182T) (a) Hub B3D36C431/80VSA-1 (3 blades) Diameter: not over 79 in., not under 77.5 in. Pitch settings at 30 in. sta.: Low 14.9º, High 31.7º (b) McCauley Spinner: D-7261-2 (c) McCauley Governor: DC290D1/T8 Propeller Limits Static RPM at full throttle: Not over 2400; Not under 2300. Airspeed Limits (182S) Maneuvering 110 Knots IAS (108 Knots CAS) Max Structural Cruising 140 Knots IAS (138 Knots CAS) Never Exceed 175 Knots IAS (170 Knots CAS) Flaps Extended 100 Knots IAS ( 99 Knots CAS) Airspeed Limits (182T) Maneuvering 110 Knots IAS (108 Knots CAS) Max Structural Cruising 140 Knots IAS (136 Knots CAS) Never Exceed 175 Knots IAS (171 Knots CAS) Flaps Extended 100 Knots IAS ( 99 Knots CAS) C.G. Range (182S) Normal Category (1) Aft Limits: 46.0 inches aft of datum at 3100 lbs. or less. (2) Forward Limits: Linear variation from 40.9 inches aft of datum at 3100 pounds to 33.0 inches aft of datum at 2250 lbs.; 33.0 inches aft of datum at 2250 lbs. or less. C.G. Range (182T) Normal Category (1) Aft Limits 46.0 inches aft of datum at 3,100 pounds or less. (2) Forward Limits Linear variation from 40.9 inches aft of datum at 3,100 pounds, to 35.5 inches aft of datum at 2,700 pounds, to 33.0 inches aft of datum at 2,250 pounds; 33.0 inches aft of datum at 2,250 pounds or less. Empty Wt. C.G. Range None Reference Datum Lower portion of front face of firewall MAC 58.8 inches; Leading edge of MAC 25.98 inches aft of datum Leveling Means Left side of Tailcone at 139.65 inches and 171.65 inches aft of datum. Maximum Weights Normal Category (see Note 5) Maximum Ramp 3,110 pounds Maximum Takeoff 3,100 pounds Maximum Landing 2,950 pounds Rev. 76 Page 35 of 42 3A13 XIII. Model 182S, Model 182T (cont’d) No. of Seats 4 (2 at 32.0 to 50.0 inches aft of datum; 2 at 74.0 inches aft of datum) Maximum Baggage 120 pounds at 82.0 to 109.0 inches aft of datum 80 pounds at 109.0 to 134.0 inches aft of datum (Max. combined weight capacity for baggage areas is 200 pounds) Fuel Capacity (Gal.) 182S: 92 gallons total: 88 gallons usable 182T: 92 gallons total; 87 gallons usable (Two 46 gallon tanks in wings at 46.5 inches aft of datum) (See NOTE 1 for data on usable fuel). Oil Capacity (Gal.) 9.0 quarts at 14.8 inches forward of datum 5.0 quarts usable Control Surface Movements Wing flaps Down 38° +0°, -1° Elevator tab Up 24° ± 2° Down 15° ± 1° Ailerons Up 20° ± 2° Down 15° ± 2° Elevator Up 28° ± 1° Down 21° ± 1° (Relative to stabilizer) Rudder: Right: 24° +0°, -1° Left: 24° +0°,-1° (Parallel to 0.00 W.L.) Right: 27°13’ +0°, -1° Left: 27°13’ +0°,-1° (Perpendicular to hinge line) Serial Numbers Eligible 182S: 18280001 thru 18280944 182T: 18280945 and On Data Pertinent to Models 182S and 182T Certification Basis: FAR Part 23, effective February 1, 1965, as amended by 23-1 through 23-6, except as follows: FAR 23.423; 23.611; 23.619; 23.623; 23.689; 23.775; 23.871; 23.1323; and 23.1563 as amended by Amendment 23-7. 23.807 and 23.1524 as amended by Amendment 23-10. 23.507; 23.771; 23.853(a)(b)(c); and 23.1365 as amended by Amendment 23-14. 23.951 as amended by Amendment 23-15. 23.607; 23.675; 23.685; 23.733; 23.787; 23.1309 and 23.1322 as amended by Amendment 23-17. 23.1301 as amended by Amendment 23-20. 23.1353; and 23.1559 as amended by Amendment 23-21. FAR 23.603; 23.605; 23.613; 23.1329 and 23.1545 as amended by Amendment 23-23. 23.441 and 23.1549 as amended by Amendment 23-28. 23.779 and 23.781 as amended by Amendment 23-33. 23.1; 23.51 and 23.561 as amended by Amendment 23-34. 23.301; 23.331; 23.351; 23.427; 23.677; 23.701; 23.735; and 23.831 as amended by Amendment 23-42. 23.961; 23.1093; 23.1143(g); 23.1147(b); 23.1303; 23.1357; 23.1361 and 23.1385 as amended by Amendment 23-43. 23.562(a)(b)(2)(c)(1)(2)(3)(4) as amended by Amendment 23-44. 23.33; 23.53; 23.305; 23.321; 23.485; 23.621; 23.655 and 23.731 as amended by Amendment 23-45. FAR 36, dated December 1, 1969, as amended by Amendments 36-1 through 36-21. Equivalent Safety Items, Model 182S: 1. Introduction System Icing Protection 23.1093. 2. Throttle Control 23.1143(g) 3. Mixture Control 23.1147(b) Date of Application for Amended Type Certificate was January 22, 1996. Type Certificate No. 3A13 was amended October 3, 1996. 3A13 Page 36 of 42 Rev. 76 Data Pertinent to Model 182S and 182T (cont’d) Equivalent Safety Items, 182T: 1. Induction System Icing Protection 23.1093, refer to FAA letter dated 12/19/2000 2. Throttle Control 23.1143(g), refer to FAA letter dated 12/19/2000 3. Mixture Control 23.1147(b), refer to FAA letter dated 12/19/2000 4. Anti-collision Lights 23.1401(d), refer to FAA letter dated 2/20/2001 5. Aviation White Color Requirement 23.1397(c), refer to ACE-07-11, FAA letter dated 11/29/2007 Additions for the Garmin G1000 Integrated Cockpit System (ICS) Only: 14 CFR 23.303, 23.307, 23.601, 23.1163(a)(1)(2), 23.1367, 23.1381 as amended by Amendment 23-N/C. 23.1589 as amended by Amendment 23-13. 23.771(a) as amended by Amendment 23-14. 23.607 and (Electrical System) 23.1309(a)(1)(2)(c) as amended by Amendment 23-17. 23.1301, 23.1327, 23.1547(e) as amended by Amendment 23-20. 23.1501, 23.1541(a)(1)(2)(b)(1)(2) as amended by Amendment 23-21. 23.603, 23.605 as amended by Amendment 23-23. 23.1529 as amended by Amendment 23-26. 23.561(e), 23.1523; 23.1581(a)(2), 23.1583(a)(1)(2)(b)(h), 23.1585(a)(b)(d) as amended by Amendment 23-34. 23.301 as amended by Amendment 23-42. 23.1322, 23.1331, 23.1357(a)(b)(c)(d) as amended by Amendment 23-43. 23.305, 23.773(a)(1)(2), 23.1525, 23.1549 as amended by Amendment 23-45. 23.1303(a)(b)(c)(f), 23.1309(a)(1)(i)(ii)(2)(b)(1)(2)(i)(ii)(3)(4)(i)(ii)(iii)(iv)(c)(1)(2)(iii)(3)(d)(e)(f)(1), 23.1311, 23.1321(a)(c)(d)(e), 23.1323(a)(b)(1)(2)(c); 23.1329(g)(h), 23.1351(a)(1)(2)(i)(b)(1)(iii)(2)(3)(c)(4)(d)(1), 23.1353(a)(b)(c)(d)(e), 23.1359(c), 23.1361, 23.1365(a)(b)(d)(e)(f), 23.1431(a)(b)(d)(e) as amended by Amendment 23-49. 23.1325(a)(b)(1)(2)(i)(3)(c)(d)(e), 23.1543(b)(c), 23.1545(a)(b)(1)(2)(3)(4), 23.1553, 23.1555(a)(b), 23.1563(a), 23.1567(a) as amended by Amendment 23-50. 23.777(a)(b), 23.955(a)(2), 23.1337(a)(1)(2)(b)(1)(c) as amended by Amendment 23-51. 23.1305(a)(1)(2)(3)(b)(2)(3)(i) (4)(i)(5)(6)(i) as amended by Amendment 23-52. 23.901(a)(b) as amended by Amendment 23-53. Additions for the Garmin GFC-700 Automatic Flight Control System (AFCS) Only: 14 CFR 23.1335 as amended by Amendment 23-20. 23.1329 (a)(c)(d)(e)(f) as amended by Amendment 23-49. Additions for the Garmin GI 275 Electronic Flight Instrument Only: 14 CFR 23.1327 as amended by Amendment 23-20. 23.1501 as amended by Amendment 23-21. 23.1529 as amended by Amendment 23-26. 23.1523(b), 23.1581(a)(1)(2) as amended by Amendment 23-34. 23.1322, 23.1331 as amended by Amendment 23-43. 23.1525 as amended by Amendment 23-45. 23.1303(a)(b)(f), 23.1309(a)(1)(2)(b)(c)(1)(2)(iii)(3)(d)(e)(f), 23.1311(a)(b), 23.1321(a)(c)(d)(e), 23.1323(a)(c), 23.1351(a)(1)(2)(i), 23.1359(c), 23.1365(a)(d)(e), 23.1431(a)(b) as amended by Amendment 23-49. 23.1325(a)(b)(1)(i)(ii)(iii)(2)(i), 23.1543(b)(c), 23.1545(a)(b)(1)(2)(3)(4), 23.1555(a)(b) as amended by Amendment 23-50. 23.777(a)(b) as amended by Amendment 23-51. 23.1308(a)(b)(c) as amended by Amendment 23-57; 23.1306(a)(b) as amended by Amendment 23-61. 23.2010, 23.2510 as amended by Amendment 23-64(see NOTE 8). Effective at S/N 18283135 and On. Additions for 14 CFR Part 23 Amendment 64: 14 CFR 23.2000, 23.2005, 23.2010 as amended by Amendment 23-64 (see NOTE 9). Effective at S/N 18283135 and On. Additions for the Garmin G1000 NXi Integrated Cockpit System Only: 14 CFR 23.683, 23.867 as amended by Amendment 23-7. 23.613(a)(b) as amended by Amendment 23-45. 23.301(a), 23.337, 23.561(a)(b)(3)(e), 23.607(a)(b), 23.611 as amended by Amendment 23-48. 23.1329(b), 23.1351(g), 23.1353(h), 23.1359(a)(b), as amended by Amendment 23-49. 23.143(c), 23.1555(e)(2), 23.1581(a)(b)(1)(3)(c)(d)(f), 23.1583(h)(m), 23.1585(j) as amended by Amendment 23-50. 23.1337(b)(c) as amended by Amendment 23-51. 23.2515, 23.2520 as amended by Amendment 23-64 (see NOTE 10). Effective at S/N 18283280 and On. Additions for the Dual Electronic Ignition System Only: 14 CFR 23.1309(a)(1)(2), 23.1353(h), 23.1431(b) as amended by Amendment 23-49. 23.1581(a)(2) as amended by Amendment 23-50. 23.901(a)(1)(2)(b)(1)(2) as amended by Amendment 23-53. Effective at S/N 18283359 and On. Additions for new or changed non-rechargeable lithium battery installations: 14 CFR Part 23 regulations as amended by Amendment 23-64 (see NOTE 11): 14 CFR 23.2010 and 23.2325(g). Effective at S/N 18283359 and On. Additions for new or changed installations affecting aeronautical security (cybersecurity): 14 CFR Part 23 regulations as amended by Amendment 23-64 (see NOTE 12): 14 CFR 23.2010, 23.2500, 23.2505 and 23.2510. Effective at S/N 18283359 and On. Special Conditions as follows: No. 23-146-SC, “Cessna Aircraft Company, Cessna Model 182T/T182T Airplane: Installation of Electronic Flight Instrument System and the Protection of the System from High Intensity Radiated Fields (HIRF). Rev. 76 Page 37 of 42 3A13 Data Pertinent to Model 182S and 182T (cont’d) Production Basis (Model 182S) Production Certificate No. PC-4 issued June 30, 1997. Applies to S/N 18280013, 18280016, 18280017, 18280019 and On. Airplane serial numbers not listed were produced under Type Certificate only. Cessna is authorized to issue airworthiness certificates under the delegation provisions of Delegation Option Authorization No. CE-1 in accordance with Part 21 of the FAR. Production Basis (Model 182T) Production Certificate No. 4 issued March 8, 2001. Applies to S/N 18280945 and On. Cessna is authorized to issue airworthiness certificates under the delegation provisions of Delegation Option Authorization No. DOA-100129-CE in accordance with Part 21 of the FAR. Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the airplane for certification. NOTE 1. Weight and Balance: Model 182S, S/N 18280001 thru 18280944 The certificated basic empty weight and corresponding center of gravity location must include unusable fuel of 24 lbs. at 48 inches aft of datum, and full oil of 16.2 lb. at 14.8 inches forward of datum. Model 182T, S/N 18280945 and On The certificated basic empty weight and corresponding center of gravity location must include unusable fuel of 30 lbs. at 48 inches aft of datum, and full oil of 16.2 lb. at 14.8 inches forward of datum. NOTE 2. FAA Approved AFM: P/N 182SPHUS00, or later FAA approved revision, are applicable to Model 182S. The airplane must be operated according to the appropriate AFM. Required placards are included in the AFM, the applicable operating rules, or the certification basis must be installed as specified via the parts list for 070810, Airplane Assembly. A useful placarding reference is the Textron Aviation Illustrated Parts Catalogue (IPC). Any discrepancies identified between the IPC and an aircraft under inspection need to be reconciled using the previously stated parts list. FAA Approved AFM: P/N 182TPHUS00, or later FAA approved revision, is applicable to the Model 182T. The airplane must be operated according to the appropriate AFM. Required placards are included in the AFM, the applicable operating rules, or the certification basis must be installed as specified via the parts list for 070810, Airplane Assembly. A useful placarding reference is the Textron Aviation IPC. Any discrepancies identified between the IPC and an aircraft under inspection need to be reconciled using the previously stated parts list. FAA Approved AFM: P/N 182TPHAUS-00, or later FAA approved revision, are applicable to the Model 182T equipped with Garmin G1000 Integrated Cockpit System. The airplane must be operated according to the appropriate AFM. Required placards are included in the AFM, the applicable operating rules, or the certification basis must be installed as specified via the parts list for 070810, Airplane Assembly. A useful placarding reference is the Textron Aviation IPC. Any discrepancies identified between the IPC and an aircraft under inspection need to be reconciled using the previously stated parts list. FAA Approved AFM: P/N 182TPHBUS-00, or later FAA approved revision, are applicable to the Model 182T equipped with Garmin G1000 Integrated Cockpit System and Garmin GFC-700 AFCS. The airplane must be operated according to the appropriate AFM. Required placards are included in the AFM, the applicable operating rules, or the certification basis must be installed as specified via the parts list for 070810, Airplane Assembly. A useful placarding reference is the Textron Aviation IPC. Any discrepancies identified between the IPC and an aircraft under inspection need to be reconciled using the previously stated parts list. 3A13 Page 38 of 42 Rev. 76 Data Pertinent to Model 182S and 182T (cont’d) NOTE 2. (cont’d) FAA Approved AFM, P/N 182TPHCUS-00, or later FAA approved revision, are applicable to the Model T182T equipped with Garmin G1000 NXi Integrated Cockpit System. The airplane must be operated according to the appropriate AFM. Required placards are included in the AFM, the applicable operating rules, or the certification basis must be installed as specified via the parts list for 070810, Airplane Assembly. A useful placarding reference is the Textron Aviation IPC. Any discrepancies identified between the IPC and an aircraft under inspection need to be reconciled using the previously stated parts list. NOTE 3. The CHT probe must be installed on Head No. 1 (182S) or No. 3 (182T). NOTE 4. Special Ferry Flight Authorization. Flight Standards District Offices are authorized to issue Special overweight ferry flight authorizations. These airplanes are structurally satisfactory for ferry flight if maintained within the following limits: 1. Takeoff weight must not exceed 130% of the maximum weight for Normal Category. 2. The Never Exceed Airspeed (VNE) and Maximum Structural Cruising Speed (VC) must be reduced by 30%. 3. Forward and aft center of gravity limits may not be exceeded. 4. Structural load factors of +2.5 g. to -1.0 g. may not be exceeded. Requirements for any additional engine oil should be established in accordance with AC 23.1011-1. Increased stall speeds and reduced climb performance should be expected for the increased weights. Flight characteristics and performance at the increased weights have not been evaluated. Procedures for issuing a Flight Permit for operations of overweight aircraft may be found in AC 21-4B. NOTE 5. Model 182S S/N 18280617 thru 18280670 may differ structurally and are, therefore, not eligible for any weight increases above the approved maximum takeoff weight limit of 3,100 pounds. Any exceptions must first be coordinated with the Wichita ACO Branch. Exceptions to this limitation have been inspected and found to comply with type data for Model 182S and includes the following S/N: 18280620. NOTE 6. The following serials numbers are manufactured under the name Cessna Aircraft Company: Model 182S: 18280001 thru 18280944; Model 182T: 18280945 thru 18282368. NOTE 7. Company name change effective 7/29/15. The following serials numbers are manufactured under the name Textron Aviation Inc.: Model 182T: 18282369 and On. NOTE 8. Means of Compliance for 23.2510 [23-64] is draft AC 20-184A. NOTE 9. 14 CFR 23.2005 Certification Level and Performance Level: Level 2, Low Speed NOTE 10. Means of Compliance for 23.2515 [23-64] and 23.2520 [23-64] is FAA Policy PS-ACE-23-10 NOTE 11. Means of Compliance for 23.2010 [23-64] and 23.2325(g) [23-64] is CPP-23.2525-1 (signed 2023.10.19). NOTE 12. Means of Compliance for 23.2010, 23.2500, 23.2505, and 23.2510 as amended by Amendment 23-64 is ASTM F3532-22. XIV. Model T182T, Skylane, 4 PCLM (Normal Category), Approved 23 February 2001 Engine Lycoming TIO-540-AK1A. Rated 235 Horsepower Fuel 100/100LL minimum grade aviation gasoline Engine Limits For all operations, 2,400 RPM Propeller McCauley Constant Speed (a) Hub B3D36C442/80VSB-1 Diameter: not over 79 inches; not under 77.5 inches Pitch settings at 30 in. sta.: Low 15.1º, High 35.4º Note: A low pitch setting of 15.3º is also acceptable for this model number prop. (b) McCauley Spinner: D-7261-2 (c) McCauley Governor: DC290D1/T8 Rev. 76 Page 39 of 42 3A13 XIV. Model T182T (cont’d) Propeller Limits Static RPM at full throttle: Not over 2400; Not Under 2300 Airspeed Limits Maneuvering 110 Knots IAS (110 Knots CAS) Max Structural Cruising 140 Knots IAS (137 Knots CAS) Never Exceed 175 Knots IAS (170 Knots CAS) Flaps Extended 100 Knots IAS (100 Knots CAS) C.G. Range Normal Category (1) Aft Limits 46.0 inches aft of datum at 3,100 pounds or less. (2) Forward Limits Linear variation from 40.9 inches aft of datum at 3,100 pounds, to 35.5 inches aft of datum at 2,700 pounds, to 33.0 inches aft of datum at 2,250 pounds; 33.0 inches aft of datum at 2,250 pounds or less. Empty Wt. C.G. Range None Reference Datum Lower portion of front face of firewall MAC 58.8 inches; Leading edge of MAC 25.98 inches aft of datum Leveling Means Left side of Tailcone at 139.65 inches and 171.65 inches aft of datum Maximum Weights Normal Category Maximum Ramp 3,110 pounds Maximum Takeoff 3,100 pounds Maximum Landing 2,950 pounds No. of Seats 4 (2 at 32.0 to 50.0 inches aft of datum; 2 at 74.0 inches aft of datum) Maximum Baggage 120 pounds at 82.0 to 109.0 inches aft of datum 80 pounds at 109.0 to 134.0 inches aft of datum (Max. combined weight capacity for baggage areas is 200 pounds) Fuel Capacity (Gal.) 92 gallons total; 87 gallons usable (Two 46 gallon tanks in wings at 46.5 inches aft of datum) See NOTE 1 for data on usable fuel. Oil Capacity (Qts.) 9.0 quarts at 14.8 inches forward of datum 5.0 quarts usable Control Surface Movements Wing flaps Down 38° +0°, -1° Elevator tab Up 24° ± 2° Down 15° ± 1° Ailerons Up 20° ± 2° Down 15° ± 2° Elevator Up 28° ± 1° Down 21° ± 1° (Relative to stabilizer) Rudder: Right: 24° +0°, -1° Left: 24° +0°, -1° (Parallel to 0.00 W.L.) Right: 27°13’ +0°, -1° Left: 27°13’ +0°, -1° (Perpendicular to hinge line) Serial Numbers Eligible T18208001 and On 3A13 Page 40 of 42 Rev. 76 Data Pertinent to Model T182T Certification Basis FAR Part 23, effective February 1, 1965, as amended by 23-1 through 23-6, except as follows: 14 CFR 23.423, 23.611, 23.619, 23.623, 23.689, 23.775, 23.871, 23.1323, 23.1563 as amended by Amendment 23-7. 23.807, 23.1524 as amended by Amendment 23-10. 23.507, 23.771, 23.853(a)(b)(c), 23.1365 as amended by Amendment 23-14. 23.951 as amended by Amendment 23-15. 23.607, 23.675, 23.685, 23.733, 23.787, 23.1309, 23.1322 as amended by Amendment 23-17. 23.1301 as amended by Amendment 23-20. 23.1353, 23.1559 as amended by Amendment 23-21. 23.603, 23.605, 23.613, 23.1329, 23.1545 as amended by Amendment 23-23. 23.441, 23.1549 as amended by Amendment 23-28. 23.779, 23.781 as amended by Amendment 23-33. 23.1, 23.51, 23.561 as amended by Amendment 23-34. 23.301, 23.331, 23.351, 23.427, 23.677, 23.701, 23.735, 23.831 as amended by Amendment 23-42. 23.961, 23.1093, 23.1143(g), 23.1147(b), 23.1303, 23.1357, 23.1361, 23.1385 as amended by Amendment 23-43. 23.562(a)(b)(2)(c)(1)(c)(2)(3)(4) as amended by Amendment 23-44. 23.33, 23.53, 23.305, 23.321, 23.485, 23.621, 23.655, 23.731 as amended by Amendment 23-45. FAR Part 36, dated December 1, 1969, as amended by Amendments 36-1 through 36-22. Equivalent Level of Safety Items: 1. Throttle Control 23.1143(g), refer to FAA letter dated 12/19/2000 2. Mixture Control 23.1147(b), refer to FAA letter dated 12/19/2000 3. Anti-collision Lights 23.1401(d), refer to FAA letter dated 02/20/2001 4. Aviation White Color Requirement 23.1397(c), refer to ACE-07-11, FAA letter dated 11/29/2007 Additions for the Garmin G1000 Integrated Cockpit System (ICS) Only: 14 CFR 23.303, 23.307, 23.601, 23.1163(a)(1)(2), 23.1367, 23.1381 as amended by Amendment 23-N/C. 23.1589 as amended by Amendment 23-13. 23.771(a) as amended by Amendment 23-14. 23.607 and (Electrical System) 23.1309(a)(1)(2)(c) as amended by Amendment 23-17. 23.1301, 23.1327, 23.1547(e) as amended by Amendment 23-20. 23.1501, 23.1541(a)(1)(2)(b)(1)(2) as amended by Amendment 23-21. 23.603, 23.605 as amended by Amendment 23-23. 23.1529 as amended by Amendment 23-26. 23.561(e), 23.1523, 23.1581(a)(2), 23.1583(a)(1)(2)(b)(h), 23.1585(a)(b)(d) as amended by Amendment 23-34. 23.301 as amended by Amendment 23-42. 23.1322, 23.1331, 23.1357(a)(b)(c)(d) as amended by Amendment 23-43. 23.305, 23.773(a)(1)(2), 23.1525, 23.1549 as amended by Amendment 23-45. 23.1303(a)(b)(c)(f), 23.1309(a)(1)(i)(ii)(2)(b)(1)(2)(i)(ii)(3)(4)(i)(ii)(iii)(iv)(c)(1)(2)(iii)(3)(d)(e)(f)(1), 23.1311, 23.1321(a)(c)(d)(e), 23.1323(a)(b)(1)(2)(c), 23.1329(g)(h), 23.1351(a)(1)(2)(i)(b)(1)(iii)(2)(3)(c)(4)(d)(1), 23.1353(a)(b)(c)(d)(e), 23.1359(c), 23.1361, 23.1365(a)(b)(d)(e)(f) and 23.1431(a)(b)(d)(e) as amended by Amendment 23-49. 23.1325(a)(b)(1)(2)(i)(3)(c)(d)(e); 23.1543(b)(c), 23.1545(a)(b)(1)(2)(3)(4), 23.1553, 23.1555(a)(b), 23.1563(a), 23.1567(a) as amended by Amendment 23-50. 23.777(a)(b), 23.955(a)(2), 23.1337(a)(1)(2)(b)(1)(c) as amended by Amendment 23-51. 23.1305(a)(1)(2)(3)(b)(2)(3)(i) (4)(i)(5)(6)(i) as amended by Amendment 23-52. 23.901(a)(b) as amended by Amendment 23-53. Additions for the Garmin GFC-700 Automatic Flight Control System (AFCS) Only: 14 CFR 23.1335 as amended by Amendment 23-20. 23.1329(a)(c)(d)(e)(f) as amended by Amendment 23-49. Additions for the Garmin GI 275 Electronic Instrument Only: 14 CFR 23.1327 as amended by Amendment 23-20. 23.1501 as amended by Amendment 23-21. 23.1529 as amended by Amendment 23-26. 23.1523(b), 23.1581(a)(1)(2) as amended by Amendment 23-34. 23.1322, 23.1331 as amended by Amendment 23-43. 23.1525 as amended by Amendment 23-45. 23.1303(a)(b)(f); 23.1309(a)(1)(2)(b)(c)(1)(2)(iii)(3)(d)(e)(f), 23.1311(a)(b), 23.1321(a)(c)(d)(e), 23.1323(a)(c), 23.1351(a)(1)(2)(i), 23.1359(c), 23.1365(a)(d)(e), 23.1431(a)(b) as amended by Amendment 23-49. 14 CFR 23.1325(b)(1)(i)(ii)(iii)(2)(i), 23.1543(b)(c), 23.1545(a)(b)(1)(2)(3)(4), 23.1555(a)(b) as amended by Amendment 23-50. 23.777(a)(b) as amended by Amendment 23-51. 23.1308(a)(b)(c) as amended by Amendment 23-57. 23.1306(a)(b) as amended by Amendment 23-61. 23.2010, 23.2325(g)(1)(2), 23.2510 as amended by Amendment 23-64 (see NOTE 7). Effective at S/N T18209101 and On. Additions for 14 CFR Part 23 Amendment 64: 14 CFR 23.2000, 23.2005, 23.2010 as amended by Amendment 23-64 (see NOTE 8). Effective at S/N T18209101 and On. Rev. 76 Page 41 of 42 3A13 Data Pertinent to Model T182T (cont’d) Certification Basis (cont’d) Additions for the Garmin G1000 NXi Integrated Cockpit System Only: 14 CFR 23.683; 23.867 as amended by Amendment 23-7; 23.613(a)(b) as amended by Amendment 23-45; 23.301(a); 23.337; 23.561(a)(b)(3)(e); 23.607(a)(b); 23.611 as amended by Amendment 23-48; 23.1329(b); 23.1351(g); 23.1353(h); 23.1359(a)(b) as amended by Amendment 23-49; 23.143(c); 23.1555(e)(2); 23.1581(a)(b)(1)(3)(c)(d)(f); 23.1583(h)(m); 23.1585(j) as amended by Amendment 23-50; 23.1337(b)(c) as amended by Amendment 23-51; 23.2515; 23.2520 as amended by Amendment 23-64 (see NOTE 9). Effective at S/N T18209159 and On. Additions for the Dual Electronic Ignition System Only: 14 CFR 23.1309(a)(1)(2), 23.1353(h), 23.1431(b) as amended by Amendment 23-49. 23.1581(a)(2) as amended by Amendment 23-50. 23.901(a)(1)(2)(b)(1)(2) as amended by Amendment 23-53. Effective for S/N’s T18208204, T18208714, and T18209210 and On. Additions for new or changed non-rechargeable lithium battery installations: 14 CFR Part 23 regulations as amended by Amendment 23-64 (see NOTE 10): 14 CFR 23.2010 and 23.2325(g). Effective for S/N’s T18208204, T18208714, and T18209210 and On. Additions for new or changed installations affecting aeronautical security (cybersecurity): 14 CFR Part 23 regulations as amended by Amendment 23-64 (see NOTE 11): 14 CFR 23.2010, 23.2500, 23.2505 and 23.2510. Effective for S/N’s T18208204, T18208714, and T18209210 and On. Special Conditions as follows: No. 23-146-SC, “Cessna Aircraft Company, Cessna Model 182T and T182T: Installation of Electronic Flight Instrument System and the Protection of the System from High Intensity Radiated Fields (HIRF). Production Basis (Model T182T) Production Certificate No. 4 issued March 8, 2001. Applies to airplane S/N T18208001 and On. Cessna is authorized to issue airworthiness certificates under the delegation provisions of Delegation Option Authorization No. DOA-100129-CE in accordance with Part 21 of the FAR. Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the airplane for certification. NOTE 1. Weight and Balance: S/N T18208001 and On (Model T182T) The certificated empty weight and corresponding center of gravity location must include unusable fuel of 30 lb. at 48 inches aft of datum, and full oil of 16.2 lb. at 14.8 inches forward of datum. NOTE 2. The POH/AFM, P/N T182TPHUS00, or later FAA approved revision, is applicable to Model T182T. The airplane must be operated according to the appropriate POH/AFM. Required placards are included in the AFM, the applicable operating rules, or the certification basis must be installed as specified via the parts list for 070811, Airplane Assembly. A useful placarding reference is the Textron Aviation IPC. Any discrepancies identified between the IPC and an aircraft under inspection need to be reconciled using the previously stated parts list. FAA Approved AFM, P/N T182TPHAUS-00, or later FAA approved revision, are applicable to the Model 182T equipped with Garmin G1000 Integrated Cockpit System. The airplane must be operated according to the appropriate AFM. Required placards are included in the AFM, the applicable operating rules, or the certification basis must be installed as specified via the parts list for 070811, Airplane Assembly. A useful placarding reference is the Textron Aviation IPC. Any discrepancies identified between the IPC and an aircraft under inspection need to be reconciled using the previously stated parts list. FAA Approved AFM, P/N T182TPHBUS-00, or later FAA approved revision, are applicable to the Model T182T equipped with Garmin G1000 Integrated Cockpit System and Garmin GFC-700 AFCS. The airplane must be operated according to the appropriate AFM. Required placards are included in the AFM, the applicable operating rules, or the certification basis must be installed as specified via the parts list for 070811, Airplane Assembly. A useful placarding reference is the Textron Aviation IPC. Any discrepancies identified between the IPC and an aircraft under inspection need to be reconciled using the previously stated parts list. 3A13 Page 42 of 42 Rev. 76 Data Pertinent to Model T182T (cont’d) NOTE 2. (cont’d) FAA Approved AFM, P/N T182TPHCUS-00, or later FAA approved revision, are applicable to the Model T182T equipped with Garmin G1000 NXi Integrated Cockpit System. The airplane must be operated according to the appropriate AFM. Required placards are included in the AFM, the applicable operating rules, or the certification basis must be installed as specified via the parts list for 070811, Airplane Assembly. A useful placarding reference is the Textron Aviation IPC. Any discrepancies identified between the IPC and an aircraft under inspection need to be reconciled using the previously stated parts list. NOTE 3. The CHT probe must be installed on Head No. 4. NOTE 4. Special Ferry Flight Authorization. Flight Standards District Offices (FSDO) are authorized to issue Special overweight ferry flight authorizations. This airplane is structurally satisfactory for ferry flight if maintained within the following limits: 1. Takeoff weight must not exceed 130% of the maximum weight for Normal Category. 2. The Never Exceed Airspeed (VNE) and Maximum Structural Cruising Speed (VC) must be reduced by 30%. 3. Forward and aft center of gravity limits may not be exceeded. 4. Structural load factors of +2.5 g. to -1.0 g. may not be exceeded. Requirements for any additional engine oil should be established in accordance with AC 23.1011-1. Increased stall speeds and reduced climb performance should be expected for the increased weights. Flight characteristics and performance at the increased weights have not been evaluated. Procedures for issuing a Flight Permit for operations of overweight aircraft may be found in AC 21-4B. NOTE 5. The following serials numbers are manufactured under the name Cessna Aircraft Company: T18208001 thru T18209100. NOTE 6. Company name change effective 7/29/15. The following serials numbers are manufactured under the name Textron Aviation Inc.: T18209101 and On. NOTE 7. Means of Compliance for 23.2510 [23-64] is draft AC 20-184A. NOTE 8. 14 CFR 23.2005 Certification Level and Performance Level: Level 2, Low Speed. NOTE 9. Means of Compliance for 23.2515 [23-64] and 23.2520 [23-64] is FAA Policy PS-ACE-23-10. NOTE 10. Means of Compliance for 23.2010 [23-64] and 23.2325(g) [23-64] is CPP-23.2525-1 (signed 2023.10.19). NOTE 11. Means of Compliance for 23.2010, 23.2500, 23.2505, and 23.2510 as amended by Amendment 23-64 is ASTM F3532-22. --- END --- ``` ## ADs (74, first 50, in force first) - [AD 2025-23-08](https://openairdocs.org/ad/2025-23-08): Hoses and Tubes · Textron 182Q and 182R with STC SA03302AT. Effective Dec 2, 2025 - [AD 2024-14-03](https://openairdocs.org/ad/2024-14-03): Autopilot System · Garmin GFC 500 Autopilot (STC SA01866WI). Effective Aug 20, 2024 - [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 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022 - [AD 2020-21-22](https://openairdocs.org/ad/2020-21-22): Fuselage; Stabilizers · Textron 180, 180A, 180B and 21 more. Effective Dec 7, 2020 - [AD 2020-18-01](https://openairdocs.org/ad/2020-18-01): Fuselage · Textron 172N, 172P, 172Q and 62 more. Effective Nov 12, 2020 - [AD 2013-11-11](https://openairdocs.org/ad/2013-11-11): Engine Oil Pressure · Cessna 172R, 172S, 182S and 4 more. Effective Aug 1, 2013 - [AD 2011-10-09](https://openairdocs.org/ad/2011-10-09): Seat Rails and Roller Housing Inspections · Cessna 150A, 150B, 150C and 221 more. Effective Jun 17, 2011 - [AD 2009-04-05](https://openairdocs.org/ad/2009-04-05): Intercooler inlet and outlet hoses · Cessna 182Q and 182R with STC SA03302AT. Effective Mar 27, 2009 - [AD 2008-26-10](https://openairdocs.org/ad/2008-26-10): Alternate static air source selector valve · Cessna 172, 172A, 172B and 179 more. Effective Jan 5, 2009 - [AD 2008-10-02](https://openairdocs.org/ad/2008-10-02): Part number identification placard · Cessna 172, 172R, 172RG and 64 more. Effective May 12, 2008 - [AD 2008-05-09](https://openairdocs.org/ad/2008-05-09): Crew seats · Cessna 172R, 172S, 182T and 3 more. Effective Apr 8, 2008 - [AD 2008-02-18](https://openairdocs.org/ad/2008-02-18): Pick-up collar support and nylon screws · BRS-172 parachute recovery system (Ballistic Recovery Systems STC SA01679CH or SA01999CH). Effective Feb 28, 2008 - [AD 2008-02-06](https://openairdocs.org/ad/2008-02-06): GSM 85 servo gearbox units · Cessna 182T, 206H, LC40-550FG and 11 more. Effective Feb 26, 2008 - [AD 2007-08-03](https://openairdocs.org/ad/2007-08-03): Flexible fuel hoses · Cessna 172R, 172S, 182T and 3 more. Effective May 2, 2007 - [AD 2007-09-01](https://openairdocs.org/ad/2007-09-01): Ground power electrical cable, the fuel strainer cable, and the fuel line · Cessna 182H, 182J, 182K and 6 more. Effective Apr 25, 2007 - [AD 2007-05-10](https://openairdocs.org/ad/2007-05-10): Steel lock rod/bar on both crew seat back cylinder lock assemblies · Cessna 172R, 172S, 182S and 4 more. Effective Apr 11, 2007 - [AD 2006-17-04](https://openairdocs.org/ad/2006-17-04): Flexible fuel hoses located in the engine compartment · Cessna 172R, 172S, 182T and 3 more. Effective Sep 1, 2006 - [AD 2006-12-07](https://openairdocs.org/ad/2006-12-07): ECi cylinder assemblies · Aerostar AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 386 more. Effective Jul 11, 2006 - [AD 2006-03-08](https://openairdocs.org/ad/2006-03-08): Vacuum pumps · Aero Advantage 14-19, 14-19-2, 14-19-3 and 299 more. Effective Mar 10, 2006 - [AD 2005-13-10](https://openairdocs.org/ad/2005-13-10): Main electrical power junction box circuit breakers · Cessna 172R, 172S, 182T and 3 more. Effective Aug 9, 2005 - [AD 2005-05-53 R1](https://openairdocs.org/ad/2005-05-53-R1): Flight control system · Cessna 172R, 172S, 182T and 1 more. Effective Mar 21, 2005 - [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005 - [AD 2004-19-01](https://openairdocs.org/ad/2004-19-01): Upper shoulder harness adjusters · Cessna F150G, F150H, F150J and 129 more. Effective Nov 1, 2004 - [AD 2004-15-18](https://openairdocs.org/ad/2004-15-18): Honeywell KAP 140 Autopilot Computer System · Cessna 172R, 172S, 182S and 4 more. Effective Sep 12, 2004 - [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001 - [AD 2000-06-01](https://openairdocs.org/ad/2000-06-01): Fuel Strainer Assembly · Cessna 150F, 150G, 150H and 163 more. Effective May 5, 2000 - [AD 98-21-21 R1](https://openairdocs.org/ad/98-21-21-R1): Electric Inflatable Door Seals · Cessna 17-30, 17-30A, 17-31 and 267 more. Effective May 1, 2000 - [AD 2000-02-14](https://openairdocs.org/ad/2000-02-14): Exhaust Muffler End Plates · Cessna 182S. Effective Mar 17, 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. Effective Dec 22, 1998 - [AD 98-16-04](https://openairdocs.org/ad/98-16-04): Inspect Angle Stiffener Along Lower Spar Cap · Cessna 180, 180A, 180B and 37 more. Effective Sep 21, 1998 - [AD 98-14-03](https://openairdocs.org/ad/98-14-03): Transponders · Cessna 172, 172A, 172B and 230 more. Effective Aug 16, 1998 - [AD 98-01-14](https://openairdocs.org/ad/98-01-14): Engine Exhaust Muffler · Cessna 182S. Effective Feb 23, 1998 - [AD 98-01-01](https://openairdocs.org/ad/98-01-01): Placard in Cockpit · Cessna 172R and 182S. Effective Feb 2, 1998 - [AD 97-01-13](https://openairdocs.org/ad/97-01-13): Fuel, Oil and Hydraulic Hoses · Cessna 150, 150A, 150B and 232 more. Effective Feb 3, 1997 - [AD 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996 - [AD 84-10-01 R1](https://openairdocs.org/ad/84-10-01-R1): Bladder Fuel Cells · Cessna 180, 180A, 180B and 103 more. Effective Jul 5, 1988 - [AD 79-10-14 R1](https://openairdocs.org/ad/79-10-14-R1): Fuel Tank Venting · Cessna 140A, 150, 150A and 172 more. Effective May 30, 1988 - [AD 86-24-07](https://openairdocs.org/ad/86-24-07): Engine Controls Installation · Cessna 150C, 150D, 150E and 142 more. Effective Jan 7, 1987 - [AD 85-23-07](https://openairdocs.org/ad/85-23-07): Autopilot Systems · Aerostar PA-60-700P (Aerostar 700P), 172L, 172P and 37 more. Effective Jan 27, 1986 - [AD 72-03-03 R3](https://openairdocs.org/ad/72-03-03-R3): Wing Flap Actuators Jack Screw · Cessna F150F, F150G, F150H and 83 more. Effective Oct 15, 1984 - [AD 83-22-06](https://openairdocs.org/ad/83-22-06): Aileron Hinge Pin · Cessna 152, 172N, 172P and 18 more. Effective Nov 8, 1983 - [AD 83-17-06](https://openairdocs.org/ad/83-17-06): Aileron Balance Weights · Flap actuated aileron droop system (Sierra Industries STC SA1382WE or 5 others). Effective Sep 1, 1983 - [AD 83-13-01](https://openairdocs.org/ad/83-13-01): Placard-Improper Fuel Cap Sealing · Cessna 182, 182A, 182B and 14 more. Effective Aug 1, 1983 - [AD 80-25-07 R1](https://openairdocs.org/ad/80-25-07-R1): Oil Coolers · American Champion 7ECA, 7GCAA, 7GCBC and 39 more. Effective Sep 24, 1981 - [AD 81-19-04](https://openairdocs.org/ad/81-19-04): Hose Assembly · Rajay Hose Assemblies, 500A, 500B and 87 more. Effective Sep 17, 1981 - [AD 81-15-03](https://openairdocs.org/ad/81-15-03): Engine Inlet Air Filters · Replace existing engine induction air filter (Brackett Aero Filters STC SA693CE or SA71GL). Effective Jul 20, 1981 - [AD 79-25-07](https://openairdocs.org/ad/79-25-07): Alternator Ground · Cessna 180, 180A, 180B and 95 more. Effective Dec 13, 1979 - [AD 79-08-03](https://openairdocs.org/ad/79-08-03): Electrical System · Cessna 120, 140, 140A and 152 more. Effective Jun 6, 1979 All 74: https://openairdocs.org/tcds/3A13/ads.md ## Registered aircraft by registry model (OpenAirDocs) - [Cessna 182P](https://openairdocs.org/model/cessna-182p): 2,099 aircraft (registry code 2075816) - [Cessna 182Q](https://openairdocs.org/model/cessna-182q): 1,565 aircraft (registry code 2072732) - [Cessna 182T](https://openairdocs.org/model/cessna-182t): 969 aircraft (registry codes 2072703, 2072707, 2072705) - [Cessna 182A](https://openairdocs.org/model/cessna-182a): 784 aircraft (registry code 2072704) - [Cessna T182T](https://openairdocs.org/model/cessna-t182t): 781 aircraft (registry codes 2072738, 2072739) - [Cessna R182](https://openairdocs.org/model/cessna-r182): 706 aircraft (registry code 2072734) - [Cessna 182S](https://openairdocs.org/model/cessna-182s): 606 aircraft (registry code 2072701) - [Cessna 182J](https://openairdocs.org/model/cessna-182j): 487 aircraft (registry code 2072722) - [Cessna 182R](https://openairdocs.org/model/cessna-182r): 487 aircraft (registry code 2072731) - [Cessna TR182](https://openairdocs.org/model/cessna-tr182): 465 aircraft (registry code 2072735) - [Cessna 182](https://openairdocs.org/model/cessna-182): 446 aircraft (registry code 2072702) - [Cessna 182M](https://openairdocs.org/model/cessna-182m): 432 aircraft (registry code 2072728) - [Cessna 182H](https://openairdocs.org/model/cessna-182h): 423 aircraft (registry code 2072718) - [Cessna 182K](https://openairdocs.org/model/cessna-182k): 413 aircraft (registry code 2072724) - [Cessna 182L](https://openairdocs.org/model/cessna-182l): 411 aircraft (registry code 2072726) - [Cessna 182B](https://openairdocs.org/model/cessna-182b): 406 aircraft (registry code 2072706) - [Cessna 182G](https://openairdocs.org/model/cessna-182g): 391 aircraft (registry code 2072716) - [Cessna 182E](https://openairdocs.org/model/cessna-182e): 380 aircraft (registry code 2072712) - [Textron 182T](https://openairdocs.org/model/textron-182t): 347 aircraft (registry code 2072723) - [Cessna 182N](https://openairdocs.org/model/cessna-182n): 336 aircraft (registry code 2072730) - [Cessna 182F](https://openairdocs.org/model/cessna-182f): 293 aircraft (registry code 2072714) - [Cessna 182C](https://openairdocs.org/model/cessna-182c): 282 aircraft (registry code 2072708) - [Cessna 182D](https://openairdocs.org/model/cessna-182d): 270 aircraft (registry code 2072710) - [Textron T182T](https://openairdocs.org/model/textron-t182t): 96 aircraft (registry code 2072779) - [Cessna T182](https://openairdocs.org/model/cessna-t182): 58 aircraft (registry code 2072736) - [Cessna Wren 182F 460](https://openairdocs.org/model/cessna-wren-182f-460): 1 aircraft (registry code 2075807) - [Cessna Wren 182G 460](https://openairdocs.org/model/cessna-wren-182g-460): 1 aircraft (registry code 2075802) - [Cessna Wren 182H 460](https://openairdocs.org/model/cessna-wren-182h-460): 1 aircraft (registry code 2075806) - [Cessna/Anglin M D JR 182N](https://openairdocs.org/model/cessna-anglin-m-d-jr-182n): 0 aircraft (registry code 2072719) - [Cessna/Hermon 182F](https://openairdocs.org/model/cessna-hermon-182f): 0 aircraft (registry code 2072715) - [Textron 182](https://openairdocs.org/model/textron-182): 0 aircraft (registry code 2072700) ## STCs approved under this data sheet (958, first 50) - [STC SA00709CH](https://openairdocs.org/stc/SA00709CH): Installation of replacement wing root vent described by Dwg Nos. 8-30-96-1& 8-30-96-2, no rev, both dtd 8/30/96, or later FAA app rev.. Gallagher Aviation, LLC - [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).. Garmin International Inc. - [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.. TCW Technologies, LLC - [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC - [STC SA01844WI](https://openairdocs.org/stc/SA01844WI): Installation of Garmin GFC 600 Automatic Flight Control System. Garmin International Inc. - [STC SA12428CH](https://openairdocs.org/stc/SA12428CH): Installation of the Lycoming Engines Electronic Ignition System (EIS). Lycoming Engines, An Operating Division of AVCO Corporation - [STC SA02069AK](https://openairdocs.org/stc/SA02069AK): Fabrication and installation of the Airglas, Inc., Landes PA32-206LA Nose Fork equipped with up to a 8.50 x 6 tire. Airglas Inc. - [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies - [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC - [STC SA01134DE](https://openairdocs.org/stc/SA01134DE): Installation of EarthX ETX680-24-TSO Lithium Battery. EarthX Inc. - [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc. - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder.. Garmin International Inc. - [STC SA04439NY](https://openairdocs.org/stc/SA04439NY): Installation of an X cam Pod. J & C Engineering Services LTD - [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc. - [STC SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies - [STC SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation - [STC SA00152WI](https://openairdocs.org/stc/SA00152WI): 1) Installation of Continental IO-520-D engine and Hartzell PHC-L3YF-1RF/F7691 propeller OR 2) Installation of Continental IO-550-D engine and Hartzell PHC-L3YF-1RF/F7691 or PHC-G3YF-1RF/F8468A()-6R propeller. Air Plains Services Corporation - [STC SA01302AT](https://openairdocs.org/stc/SA01302AT): Installation of Teledyne Continental Motors Model IO-520-D engine and either a McCauley Model D3A34C401/90DFA-10 or Hartzell Model PHC-C3YF-1RF/F8468A( )-6R or PHC-C3YF-1RF/F7691( ) or PHC-G3YF-1RF/F8468A( )-6Ror PHC-G3YF-1RF/F7691( ) 3-blade propeller.. Air Plains Services Corporation - [STC SA01218AT](https://openairdocs.org/stc/SA01218AT): Installation of a Teledyne Continental Motors Model IO-550-D engine and either a Hartzell Model PHC-C3YF-1RF/F8468A( )-6R or PHC-C3YF-1RF/F7691( ) or PHC-G3YF-1RF/F8468A( )-6R or PHC-G3YF-1RF/F7691( )or McCauley Mod D3A34C401/90DFA-10 3-blade propeller.. Air Plains Services Corporation - [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc. - [STC SA12284IB](https://openairdocs.org/stc/SA12284IB): Installation of Bulkhead Reinforcing Kit. Acorn Welding Ltd. - [STC SA3608WE](https://openairdocs.org/stc/SA3608WE): Installation of replacement flexible fuel cell in wings. Aerosport Fuel Cells, LLC - [STC SA01866WI](https://openairdocs.org/stc/SA01866WI): Installation of Garmin GFC 500 Autopilot with Electronic Stability and Protection. Garmin International Inc. - [STC SA12276IB](https://openairdocs.org/stc/SA12276IB): Payload System Installation. Icarus Aero Inc. - [STC SA04075CH](https://openairdocs.org/stc/SA04075CH): Installation of Dynon EFIS-D10A EAA sales kit part number 102778-000. Dynon Avionics Inc. - [STC SA01005DE](https://openairdocs.org/stc/SA01005DE): Installation of a EarthX ETX900-TSO Lithium battery. EarthX Inc. - [STC SA01709WI](https://openairdocs.org/stc/SA01709WI): To increase the takeoff weight 150 lbs to 2950 lbs, while the landing weight remains the same at 2800 lbs. Adventure 112 LLC - [STC SA02266AK](https://openairdocs.org/stc/SA02266AK): Replacement of Rudder and Elevator Hinge Bearings with P. Ponk Aviation Bearing p/n PPA-1401.. McFarlane Aviation LLC - [STC SA2517NM](https://openairdocs.org/stc/SA2517NM): Installation of a replacement flexible fuel cell in the wings.. Aerosport Fuel Cells, LLC - [STC SA12073WI](https://openairdocs.org/stc/SA12073WI): Installation of VCU system provisions. Daedalean Inc. - [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector.. Alcor LLC - [STC SA5770SW](https://openairdocs.org/stc/SA5770SW): Installation of ALCOR fuel/ totalizer system 24606.. Alcor LLC - [STC SA270SO](https://openairdocs.org/stc/SA270SO): Water and ice detector in fuel gascolator and carburetor.. LegacySTC.com - [STC SA316SO](https://openairdocs.org/stc/SA316SO): Carburetor ice detector.. LegacySTC.com - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc. - [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc. - [STC SA04491CH](https://openairdocs.org/stc/SA04491CH): Installation of Hartzell Propeller Model HC-( )3YF-1RF/F8429(K,B)-( ) 3 bladed metal propeller in accordance with the installation instructions specified on FAA Approved Model List (AML) No. SA04491CH.. Hartzell Propeller LLC - [STC SA01330LA](https://openairdocs.org/stc/SA01330LA): Installation of alternate avionics support assembly.. Radiorax Aviation Systems LLC - [STC SA04643CH](https://openairdocs.org/stc/SA04643CH): Installation of Hartzell Propeller model HC-(C,G,J)3YF-1N/NM8411-( ). Hartzell Propeller LLC - [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd. - [STC SA01120SE](https://openairdocs.org/stc/SA01120SE): Installation of Door Steward.. Mountain View Aviation LLC - [STC SA865SO](https://openairdocs.org/stc/SA865SO): Installation of portable hand control.. Union Aviation LLC - [STC SA39CH](https://openairdocs.org/stc/SA39CH): Installation of an Amphibian Landing Gear Position Advisory System/Laser Gear Advisory System. Wipaire Inc. - [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics - [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC - [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC - [STC SA00622DE](https://openairdocs.org/stc/SA00622DE): Installation of John Deere AGRI Services, Inc. JD3 Aerial Imaging System,. Aeroptic LLC - [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation - [STC SA02006CH](https://openairdocs.org/stc/SA02006CH): Installation of air conditioning system.. Kelly Aerospace Thermal Systems LLC All 958: https://openairdocs.org/tcds/3A13/stcs.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.