DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 3A12 Revision 83 CESSNA 172 172I 172A 172K 172B 172L 172C172M 172D 172N 172E 172P 172F (USAF T-41A) 172Q 172G 172R 172H (USAF T-41A) 172S December 4, 2012 “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. 3A12 This data sheet which is part of Type Certificate No. 3A12 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 Cessna Aircraft Company P.O. Box 7704 Wichita, Kansas 67277 I. Model 172, 4 PCLM (Normal Category), approved November 4, 1955; 2 PCLM (Utility Category), approved December 14, 1956 Engine *Fuel *Engine Limits Propeller and Propeller Limits Continental O-300-A or O-300-B 80/87 minimum grade aviation gasoline For all operations, 2700 rpm (145 hp) 1. Propeller (a) McCauley 1A170/DM Static rpm at maximum permissible throttle setting: Not over 2360, not under 2230 No additional tolerance permitted Diameter: not over 76 in., not under 74.5 in. (b) Spinner, Dwg. 0550162 Propeller (a) Sensenich M74DR or 74DR Static rpm at maximum permissible throttle setting: Not over 2430, not under 2300 No additional tolerance permitted Diameter: not over 74 in., not under 72.0 in. (b) Spinner, Dwg. 0550162 2. Page No. Rev. No. Page No. Rev. No. 1 83 21 50 2 60 22 72 3 60 23 59 4 60 24 83 5 60 25 81 6 57 26 80 7 64 27 76 8 60 28 77 9 82 29 77 10 60 30 80 11 51 31 76 12 60 13 67 14 81 15 78 16 59 17 50 18 50 19 55 20 55 3A12 2 Rev. 82 I. Model 172 (cont'd) 3. Propeller (a) McCauley 1C172/MDM 7652, 53, or 55 30 lb. (-39.0) Static rpm at maximum permissible throttle setting: Not over 2350, not under 2250 No additional tolerance permitted Diameter: not over 76 in., not under 74.5 in. (b) Spinner, Dwg. 0550216 115 mph (100 knots) 140 mph (122 knots) 100 mph ( 87 knots) to to to to (+46.4) (+46.4) (+40.3) (+40.3) at 2200 lbs. at 1733 lbs. at 1950 lbs. at 1733 lbs. or less Propeller and Propeller Limits (cont’d) *Airspeed Limits (CAS) Maneuvering Maximum structural cruising Never exceed160 mph (139 knots) Flaps extended Normal C.G. Range (+40.8) (+36.4) Utility category (+38.4) (+36.4) Straight line variation between points given. None Normal category Utility category 2200 lbs. 1950 lbs. Empty Weight C.G. Range *Maximum Weight Number of Seats Maximum Baggage Fuel Capacity 4 (2 at +36, 2 at +70) (For child's optional jump seat, refer to Equipment List.) 120 lbs. (+95) 42 gal. total, 37 gal. usable (two 21 gal. tanks in wings at +48) See Note 1 for weight of unusable fuel and oil. 2 gal. (-20), includes 1 gal. unusable Wing flaps Takeoff Landing Retracted 1st notch 2nd notch 3rd notch 4th notch Down Down Down Left 0° 10° 20° 30° 40° 14° 13° 26° 16° Oil capacity Control Surface Movements Ailerons Elevator tab Elevator Rudder Serial Numbers Eligible Up 20° Up 28° Up 28° Right 16° 610, 612, 615, 28000 through 29999, 36000 through 36999 and 46001 through 46754 II. Model 172A, 4 PCL-SM (Normal Category), 2 PCLM (Utility Category), approved July 16, 1959; Model 172B, Skyhawk, 4 PCL-SM (Normal Category), 2 PCLM (Utility Category), approved June 14, 1960 Engine *Fuel *Engine Limits Continental O-300-C or O-300-D 80/87 minimum grade aviation gasoline For all operations, 2700 rpm (145 hp) Rev. 82 3 3A12 II. Model 172A, Model 172B Propeller and Propeller Limits (cont'd) 1. Propeller (a) McCauley 1C172/EM 7652, 53, or 55 Static rpm at maximum permissible throttle setting: Not over 2350, not under 2230 No additional tolerance permitted Diameter: not over 76 in., not under 74.5 in. (b) Spinner, Dwg. 0550216, 0550221 or 0550228 Propeller (seaplane only) (a) McCauley 1A175/SFC 8040 Static rpm at maximum permissible throttle setting: Not over 2480, not under 2380 No additional tolerance permitted Diameter: not over 80 in., not under 78.4 in. (b) Spinner, Dwg. 0550216 or 0550221 Propeller (a) Sensenich 74DC-0-56 Static rpm at maximum permissible throttle setting: Not over 2420, not under 2300 No additional tolerance permitted Diameter: not over 74 in., not under 72.5 in. 115 mph 140 mph 160 mph 100 mph (100 knots) (122 knots) (139 knots) ( 87 knots) 2. 3. *Airspeed Limits (CAS) Maneuvering Maximum structural cruising Never exceed Flaps extended Landplane (Model 172A): Normal category C.G. Range (+40.8) (+36.4) Utility category (+38.4) (+36.4) Straight line variation between points given. Landplane (Model 172B): Normal category Utility category to to to to (+46.4) (+46.4) (+40.3) (+40.3) at 2200 lbs. at 1733 lbs. or less at 1950 lbs. at 1733 lbs. or less (+40.4) (+36.4) (+37.4) (+36.4) to to to to (+46.4) (+46.4) (+40.3) (+40.3) at 2200 lbs. at 1850 lbs. or less at 1950 lbs. at 1850 lbs. or less Seaplane (Models 172A and 172B): Normal category (+39.8) to (+45.5) at 2220 lbs. (+36.4) to (+45.5) at 1825 lbs. or less Straight line variation between points given. Empty Weight C.G. Range *Maximum Weight None Landplane: Normal category Utility category Seaplane: Normal category 2200 lb. 1950 lb. 2220 lb. Number of Seats Maximum Baggage Fuel Capacity 4 (2 at +36, 2 at +70) (For child's optional jump seat, refer to Equipment List.) 120 lb. (+95) 42 gal. total, 37 gal. usable (172A); 39 gal. usable (172B) (two 21 gal. tanks in wings at +48) See Note 1 for weight of unusable fuel and oil. 2 gal. (-20), 1 gal. usable Oil Capacity 3.G. Propeller (a) McCauley 1C172/EM 7652.4) to (+45. 0550221 or 0550228 Propeller (seaplane only) (a) McCauley 1A175/SFC 8040 Static rpm.L. approved July 18. 0550216. not under 2380 No additional tolerance permitted Diameter: not over 80 in.8) to (+45. not under 2300 No additional tolerance permitted Diameter: not over 74 in.) Serial Numbers Eligible 20° 28° 28° 16° 19° Model 172A: 622. Dwg.5 in. or less at 1950 lbs. not under 78. Model 172B Control Surface Movements (cont'd) Wing flaps Takeoff Landing Retracted 1st notch 2nd notch 3rd notch 4th notch Down Down Down Left Left 0° 10° 20° 30° 40° 15° 13° 26° 16° 15° Ailerons Up Elevator tab Up Elevator Up Rudder (landplane) Right (seaplane) Right (Measured parallel to W. not under 74. not under 72. 2 PCLM (Utility Category).3) (+40. Model 172C. at maximum permissible throttle setting: Not over 2480.5 in.4) (+37. . (b) Spinner. at maximum permissible throttle setting: Not over 2350. 82 II.5) at 2220 lbs. 1961 Engine *Fuel *Engine Limits Propeller and Propeller Limits Continental O-300-C or O-300-D 80/87 minimum grade aviation gasoline For all operations. at 1850 lbs. not under 2230 No additional tolerance permitted Diameter: not over 76 in. 53.3) at 2250 lbs. 625. 0550216 or 0550221 Propeller (a) Sensenich 74DC-0-56 Static rpm at maximum permissible throttle setting: Not over 2420. 115 mph 140 mph 160 mph 100 mph (100 knots) (122 knots) (139 knots) ( 87 knots) 2. 4 PCL-SM (Normal Category). 46755 through 47746 Model 172B: 630. (+36. Range (+40.5) at 1825 lbs. Dwg.4) to to to to (+46. (b) Spinner. or 55 Static rpm..4) (+40. or less Straight line variation between points given. Model 172A. or less Seaplane Normal category (+39.4) (+46.4 in... at 1850 lbs.3A12 4 Rev. 17247747 through 17248734 III. *Airspeed Limits (CAS) Maneuvering Maximum structural cruising Never exceed Flaps extended Landplane Normal category Utility category C.4) (+36. 2700 rpm (145 hp) 1.5) (+36. 2 PCLM (Utility Category). 36 gal. 4 PCL-SM (Normal Category).5 in. unusable Wing flaps Takeoff Landing Retracted 1st notch 2nd notch 3rd notch 4th notch Down Down Down Left Left 0° 10° 20° 30° 40° 15° 13° 26° 16° 15° Oil Capacity Control Surface Movements Ailerons Up Elevator tab Up Elevator Up Rudder (Landplane) Right (Seaplane) Right (Measured parallel to W. tanks in wings at +48) See Note 1 for weight of unusable fuel and oil. Range *Maximum Weight 2250 lbs. Propeller (a) McCauley 1C172/EM 7652. approved June 19. E. 1966 Engine *Fuel *Engine Limits Propeller and Propeller Limits Continental O-300-C or O-300-D 80/87 minimum octane aviation gasoline For all operations. not under 78. total. (b) Spinner Model 172D.) Serial Numbers Eligible 17248735 through 17249544 20° 28° 28° 16° 19° IV. approved June 15. F. 1950 lbs.5 gal. Dwg. approved April 21. H. 2 PCLM (Utility Category). (-20). approved June 7. 4 PCL-SM (Normal Category). usable (two 19. 2 PCLM (Utility Category). 1965 Model 172H (USAF) T-41A). not under 2230 No additional tolerance permitted Diameter: not over 76 in.. Model 172C (cont'd) None Landplane Normal category Utility category Seaplane Normal category Empty Weight C. 2. includes 1 gal. 1962 Model 172E.L. 0550221 or 0550228 Model 172G.G. not under 2380 No additional tolerance permitted Diameter: not over 80 in. 2220 lbs. refer to Equipment List. 53 Static rpm at maximum permissible throttle setting: Not over 2420. 2 PCLM (Utility Category). 4 PCL-SM (Normal Category). Dwg.. approved June 27. 1964 Model 172G. . 1963 Model 172F (USAF T-41A). 82 5 3A12 III. 2 PCLM (Utility Category). (+95) 39 gal.Rev. Number of Seats Maximum Baggage Fuel Capacity 4 (2 at +36. 2 gal.4 in. 2 at +70) (For child's optional jump seat. 2700 rpm (145 hp) 1. 0550216. Model 172D. 0550236 Propeller (seaplane only) (a) McCauley 1A175/SFC 8040 Static rpm at maximum permissible throttle setting: Not over 2480. not under 74. 4 PCL-SM (Normal Category). 4 PCL-SM (Normal Category).) 120 lbs. at 1950 lbs. H. Empty Weight C. Model 172H Propeller and Propeller Limits (cont’d) 2.3) (+40. usable Retracted 0° 1st notch 10° Landing 0° 40° Ailerons Up 20° Down 15° Elevator tab Up 28° Down 13° Elevator Up 28° Down 23° (Neutral position is with bottom of balance area flush with bottom of stabilizer. 2220 lbs. Model 172E. 36 gal. Number of Seats Maximum Baggage Fuel Capacity 4 (2 at +36. total.8) to (+45.5) at 2220 lbs. Range *Maximum Weight None Landplane: Normal category Utility category Seaplane: Normal category 2300 lbs. or less Seaplane Normal category (+39. 0550236 122 mph 142 mph 174 mph 100 mph (106 knots) (122 knots) (151 knots) ( 87 knots) *Airspeed Limits (CAS) Maneuvering Maximum structural cruising Never exceed Flaps extended Landplane Normal category Utility category C. Model 172G.5 gal. usable (two 19.0) to to to to (+47.5) (+40.5) (+35. 82 IV.5) at 1825 lbs. Dwg. or less at 2000 lbs.3) (+47. F. E. Model 172F. Range (+38. (cont'd) Propeller (seaplane only) (cont’d) (b) Spinner Model 172D.5) at 2300 lbs. Dwg. (+95) 39 gal.G. or less Straight line variation between points given. 2 at +70) (For child's optional jump seat. 0550221 Model 172G. (+36.5) (+35. 2000 lbs.) 120 lbs.3A12 6 Rev.4) to (+45. tanks in wings at +48) See Note 1 for weight of unusable fuel and oil. 17250573 through 17251822 17251823 through 17253392 17253393 through 17254892 638. at 1950 lbs. (-20). Model 172D.G. 2 gal.0) (+35. 0550216.) Rudder (landplane) Right 16° Left 16° (seaplane) Right 19° Left 15° Wing flaps Takeoff Model 172D: Model 172E: Model 172F: Model 172G: Model 172H: 17249545 through 17250572 639. 1 gal. refer to Equipment List. 17254893 through 17256512 (except 17256493) Oil Capacity Control Surface Movements Serial Numbers Eligible . not under 2380 No additional tolerance permitted (see Note 3) Diameter: not over 80 in.3) (+47. 2 PCLM (Utility Category).5) (+35.5) (+35. not under 74 in.5) at 1825 lbs.8) to (+45. 2700 rpm (150 hp) 1. Model 172I. not under 2380 No additional tolerance permitted (see Note 3) Diameter: not over 80 in. *Airspeed Limits (CAS) Maneuvering Maximum structural cruising Never exceed Flaps extended Landplane Normal category Utility category C. at 1950 lbs. 1967 Model 172K.3) (+40..4 in. Dwg. 0550320 122 mph 140 mph 174 mph 100 mph (106 knots) (122 knots) (151 knots) ( 87 knots) 2..5) at 2300 lbs. 4 PCL-SM (Normal Category). Dwg. not under 78. 82 7 3A12 V.0) (+35. Dwg.4) to (+45.5) at 2220 lbs. Dwg. 4. not under 2270 No additional tolerance permitted (see Note 3) Diameter: not over 75 in.0) to to to to (+47. (b) Spinner. not under 2270 No additional tolerance permitted (see Note 3) Diameter: not over 75 in. approved May 9. Range (+38. 1968 Engine *Fuel *Engine Limits Propeller and Propeller Limits Lycoming O-320-E2D 80/87 minimum grade aviation gasoline For all operations. Propeller (a) McCauley 1C172/MTM 7653 Static rpm at maximum permissible throttle setting: Not over 2360. approved December 15. 0550320 Propeller (a) McCauley 1C160/CTM 7553 Static rpm at maximum permissible throttle setting: Not over 2370. not under 74 in.. (b) Spinner. . or less Straight line variation between points given.Rev. at 1950 lbs..4 in. (b) Spinner. Dwg. not under 2260 No additional tolerance permitted (see Note 3) Diameter: not over 76 in. or less at 2000 lbs.G.. (b) Spinner. 0550320 Propeller (seaplane only) (a) McCauley 1A175/ETM 8042 Static rpm at maximum permissible throttle setting: Not over 2480. 2 PCLM (Utility Category). or less Seaplane (Edo 89-2000 or 89A2000 floats) Normal category (+39. 4 PCL-SM (Normal Category).5) (+40. not under 74 in. 3. (b) Spinner. 5. not under 78. (+36. 0550321 Propeller (a) McCauley 1C160/DTM 7553 Static rpm at maximum permissible throttle setting: Not over 2370. 0550320 Propeller (seaplane only) (a) McCauley 1A175/ATM 8042 Static rpm at maximum permissible throttle setting: Not over 2480. 2700 rpm (150 hp) 1. -0° Down 23° +1°. 0550320 Propeller (seaplane only) (a) McCauley 1A175/ATM 8042 Static rpm at maximum permissible throttle setting: Not over 2480. 82 V. 2 gal. 0550320 2. Propeller (a) McCauley 1C172/MTM 7653 Static rpm at maximum permissible throttle setting: Not over 2360. Range *Maximum Weight (cont'd) None Landplane: Normal category Utility category Seaplane: Normal category 2300 lbs.G.10° Landing 0° .40° ±2° Ailerons Up 20° ±1° Down 15° ±1° Elevator tab Up 28° +1°. 1970 Engine *Fuel *Engine Limits Propeller and Propeller Limits Lycoming O-320-E2D 80/87 minimum grade aviation gasoline For all operations.) Rudder (landplane) Right 16° ±1° Left 16° ±1° (seaplane) Right 19° ±1° Left 15° ±1° (Measured parallel to W. Model 172K Empty Weight C.3A12 8 Rev. tanks in wings at +48) See Note 1 for weight of unusable fuel and oil. usable (two 21 gal.4 in.. Model 172L..L. Model 172I. usable Takeoff 0° . total. not under 2380 No additional tolerance permitted (see Note 3) Diameter: not over 80 in. not under 78. (b) Spinner. approved May 13. Dwg. not under 74 in. 1-1/2 gal. 2000 lbs. 2 at +73) (Occupant on child's optional jump seat at +93) 120 lb. (b) Spinner. -0° Down 13° +1°. -0° (Neutral position is with bottom of balance area flush with bottom of stabilizer. 4 PCL-SM (Normal Category). 2220 lbs. . -0° Elevator Up 28° +1°. Number of Seats Maximum Baggage Fuel Capacity 4 (2 at +34 to +46. at +95 42 gal. 38 gal. not under 2260 No additional tolerance permitted (see Note 3) Diameter: not over 76 in. Dwg. 2 PCLM (Utility Category). (-14.0).) Wing flaps Model 172I: Model 172K: 17256513 through 17257161 17257162 through 17258486 (1969 model) 17258487 through 17259223 (1970 model) Oil Capacity Control Surface Movements Serial Numbers Eligible VI. Model 172L (cont'd) 3. (b) Spinner.3) (+40. or less at 2000 lbs. (+36.Rev.5) at 2300 lbs.5) (+35. Range *Maximum Weight None Landplane: Normal category Utility category Seaplane: Normal category 2300 lbs. or less Seaplane (Edo 89-2000 or 89A2000 floats) Normal category (+39.. 2 at +73) (Occupant on child's optional jump seat at +96) 120 lb.5) (+40. not under 74 in. to to to to (+47. Dwg. Dwg. at +95 42 gal. not under 78. 2220 lbs.5) (+35. 0550320 Propeller (a) McCauley 1C160/DTM 7553 Static rpm at maximum permissible throttle setting: Not over 2370.G. at 1950 lbs. Dwg. *Airspeed Limits (CAS) Maneuvering Maximum structural cruising Never exceed Flaps extended Landplane Normal category C. 5. not under 2270 No additional tolerance permitted (see Note 3) Diameter: not over 75 in. not under 2270 No additional tolerance permitted (see Note 3) Diameter: not over 75 in.0) Straight line variation between points given.0) Utility category (+35. usable (two 21 gal. 0550320 Propeller (Seaplane only) (a) McCauley 1A175/ETM 8042 Static rpm at maximum permissible throttle setting: Not over 2480. 82 9 3A12 VI. total. .3) (+47. not under 2380 No additional tolerance permitted (see Note 3) Diameter: not over 80 in. (b) Spinner.G. or less Straight line variation between points given. Range (+38. not under 74 in.. at 1950 lbs. tanks in wings at +48) See Note 1 for weight of unusable fuel. 38 gal.5) at 2220 lbs.5) at 1825 lbs. Propeller (a) McCauley 1C160/CTM 7553 Static rpm at maximum permissible throttle setting: Not over 2370.8) to (+45. Number of Seats Maximum Baggage Fuel Capacity 4 (2 at +34 to +46.4 in. (b) Spinner.. Empty Weight C.4) to (+45. 0550321 122 mph 140 mph 174 mph 100 mph (106 knots) (122 knots) (151 knots) ( 87 knots) Propeller and Propeller Limits (cont’d) 4. 2000 lbs. 0550320 Propeller (seaplane only) (a) McCauley 1A175/ETM 8042 Static rpm at maximum permissible throttle setting: Not over 2545.4 in. 82 VI.. 3. -0° Elevator Up 28° +1°. 4 PCL-SM (Normal Category). (b) Spinner: Dwg.40° ±2° Ailerons Up 20° ±1° Down 15° ±1° Elevator tab Up 28° +1°. not under 78. Takeoff 0° . not under 74 in.0). (b) Spinner. not under 78. (b) Spinner. Dwg. 17260759 through 17265684 Maneuvering 112 mph Maximum structural cruising 145 mph Never exceed 182 mph Flaps extended 100 mph ( 97 knots) (126 knots) (158 knots) ( 87 knots) . 1-1/2 gal.3A12 10 Rev. 2700 rpm (150 hp) 1. 0550320 Propeller (seaplane only) (a) McCauley 1A175/ATM 8042 Static rpm at maximum permissible throttle setting: Not over 2545. -0° (Neutral position is with bottom of balance area flush with bottom of stabilizer.) Rudder (landplane) Right 16° ±1° Left 16° ±1° (seaplane) Right 19° ±1° Left 15° ±1° (Measured parallel to W. not under 2270 No additional tolerance permitted (see Note 3) Diameter: not over 75 in. usable See Note 1 for data on undrainable oil. (b) Spinner. not under 2270 No additional tolerance permitted (see Note 3) Diameter: not over 75 in. Model 172M. Dwg. -0° Down 13° +1°..4 in. -0° Down 23° +1°. *Airspeed Limits (CAS) 17256493. not under 74 in. 2 PCLM (Utility Category. approved May 12.10° Landing 0° ... 1972 Engine Lycoming O-320-E2D 80/87 minimum grade aviation gasoline For all operations. 0550320 Propeller (a) McCauley 1C160/DTM 7553 Static rpm at maximum permissible throttle setting: Not over 2370. 0550320 *Fuel *Engine Limits Propeller and Propeller Limits 2. Propeller (a) McCauley 1C160/CTM 7553 Static rpm at maximum permissible throttle setting: Not over 2370. not under 2445 No additional tolerance permitted (see Note 3) Diameter: not over 80 in. 4.) Wing flaps Model 172L: Model 172L: 17259224 through 17259903 (1971 model) 17259904 through 17260758 (1972 model) Control Surface Movements Serial Numbers Eligible VII. (-14.L. not under 2445 No additional tolerance permitted (see Note 3) Diameter: not over 80 in. Skyhawk. Model 172L Oil Capacity (cont'd) 2 gal. Dwg. 2 at +73) (Occupant on child's optional jump seat at +96) 120 lb. (+36. 1950 lbs. or less Seaplane: (Edo 89-2000 or 89A2000 floats) Normal category (+39. Range *Maximum Weight None Normal category: 2300 lb. at +95 42 gal. 2220 lb. 38 gal. Model 172N. or less Straight line variation between points given.40° +0°.0).0) (+35. -2° (landplane) 0° . 17269310 through 17274009) . (landplane).Rev. -0° Down 13° +1°.L. 2 gal. 2 PCLM (Utility Category). Model 172M (cont'd) 17265685 through 17267584 Maneuvering Maximum structural cruising Never exceed Flaps extended Landplane: Normal category Utility category *Airspeed Limits (CAS) (See Note 4 on use of CAS) 97 knots 128 knots 160 knots 85 knots C. total.8) to (+45. (landplane) 4 (2 at +34 to +46.G. -0° Elevator Up 28° +1°. -0° Down 23° +1°.5) (+35. 17260759 through 17261898 (1973 model) (except 17261445 and 17261578) 17261899 through 17263458 (1974 model) 17263459 through 17265684 (1975 model) 17265685 through 17267584 (1976 model) Number of Seats Maximum Baggage Fuel Capacity Oil Capacity Control Surface Movements Serial Numbers Eligible VIII. 17267585 through 17269309) 100LL/100 minimum grade aviation gasoline (S/N 17261578.5) at at at at 2300 lbs.) Rudder (landplane) Right 16° ±1° Left 16° ±1° (landplane) (seaplane) Right 19° ±1° Left 15° ±1° (seaplane) (Measured parallel to W. 0° . 4 PCL-SM (Normal Category). Range (+38. tanks in wings at +48) See Note 1 for data on unusable fuel.0) to to to to (+47.G.5) (+35. Empty Weight C. usable (two 21 gal. 82 11 3A12 VII. usable See Note 1 for data on undrainable oil.5) at 1825 lbs. 1950 lbs.5) at 2220 lbs. 1976 Engine *Fuel Lycoming O-320-H2AD 100/130 minimum grade aviation gasoline (S/N 17261445.) Wing flaps Takeoff Landing 17256493.10° (landplane) (seaplane) 0° . approved May 17. 1-1/2 gal. (-14. Skyhawk.4) to (+45.30° ±2° (seaplane) Ailerons Up 20° ±1° Down 15° ±1° Elevator tab Up 28° +1°. -0° (Neutral position is with bottom of balance area flush with bottom of stabilizer. or less 2000 lbs.3) (+47.3) (+40. (seaplane) Utility category: 2000 lb.5) (+40. G.5) at 1825 lbs. 1. 2220 lb. 1950 lbs. at +95 42 gal.3A12 12 Rev. or less Seaplane: (Edo 89-2000 or 89A2000 floats) Normal category (+39.5) (+40. 0550320 2.5 in. not under 2280 No additional tolerance permitted Diameter: not over 75 in.0 gal. or less 2000 lbs. (+36. (seaplane) Utility category: 2000 lb. 82 VIII.0) to to to to (+47. 2700 rpm (160 hp) 1. not under 78. 40 gal. tanks in wings at +48) See Note 1 for data on unusable fuel.3) (+40. *Airspeed Limits (CAS) (See Note 4 on use of CAS) 1977 Model through 1979 Model: Maneuvering Maximum structural cruising Never exceed Flaps extended 1980 Model: Maneuvering Maximum structural cruising Never exceed Flaps extended 97 knots 128 knots 160 knots 85 knots 97 knots 127 knots 158 knots 85 knots C. 1.3) (+47. (landplane). Range Landplane: Normal category Utility category (+38.4) to (+45. total.5) (+35. Range *Maximum Weight None Normal category: 2300 lb. (b) Spinner: Dwg. Propeller (a) McCauley 1C160/DTM 7557 Static rpm at maximum permissible throttle setting: Not over 2400. usable Number of Seats Maximum Baggage Fuel Capacity Oil Capacity .8) to (+45.0) (+35. (b) Spinner: Dwg.5 gal.5) at at at at 2300 lbs. not under 2470 No additional tolerance permitted Diameter: not over 80 in. or less Straight line variation between points given. 0550320 Propeller (seaplane only) (a) McCauley 1A175/ETM 8042 Static rpm at maximum permissible throttle setting: Not over 2570.5) (+35. 2 at +73) (Occupant on child's optional jump seat at +96) 120 lb.G. Model 172N (cont'd) *Engine Limits Propeller and Propeller Limits For all operations.5) at 2220 lbs. (landplane) 4 (2 at +34 to +46. Empty Weight C. not under 74 in.5 gal. 1950 lbs.. (-14. usable (two 21..0). L.30° ±2° (seaplane) Ailerons Up 20° ±1° Down 15° ±1° Elevator tab Up 28° +1°.5) (+35. 17269310 through 17271034 (1978 model) (except 17270050) 17271035 through 17272884 (1979 model) 17270050. 4 PCL-SM (Normal Category). *Airspeed Limits (CAS) (See Note 4 on use of CAS) Maneuvering Maximum structural cruising Never exceed Flaps extended Landplane: Normal category Utility category C. not under 2300 No additional tolerance permitted Diameter: not over 75 in. (b) Spinner: Dwg. (b) Spinner: Dwg. 1980 Engine *Fuel *Engine Limits Propeller and Propeller Limits Lycoming O-320-D2J 100LL/100 minimum grade aviation gasoline For all operations. or less 2100 lbs. Range (+39. 17272885 through 17274009 (1980 model) Control Surface Movements Serial Numbers Eligible IX.8) to (+45. -0° Down 23° +1°. not under 78. Model 172P. -2° (landplane) 0° .0) (+36.. Empty Weight C.5) at 2220 lbs. 82 13 3A12 VIII.5 in.Rev.) Rudder (landplane) Right 16° ±1° Left 16° ±1° (landplane) (seaplane) Right 19° ±1° Left 15° ±1° (seaplane) (Measured parallel to W..G.G.5) at 1825 lbs. 2 PCLM (Utility Category).10° (landplane) (seaplane) 0° . not under 2470 No additional tolerance permitted Diameter: not over 80 in.40° +0°. 17267585 through 17269309 (1977 model) 17261578.5) (+40.3) (+47. or less Seaplane: (Edo 89-2000 or 89A2000 floats) Normal category (+39.4) to (+45. -0° Down 13° +1°.5) (+35. -0° Elevator Up 28° +1°. -0° (Neutral position is with bottom of balance area flush with bottom of stabilizer. Model 172N (cont'd) 0° . Range None .3) (+40.5) at at at at 2400 lbs. 1950 lbs.0) to to to to (+47. Skyhawk. or less Straight line variation between points given. not under 74 in. 0550320 99 knots (landplane) 96 knots (floatplane) 127 knots 158 knots 85 knots 2. approved May 13. (+36.) Wing flaps Takeoff Landing 17261445. 1950 lbs. 2700 rpm (160 hp) 1. 0550320 Propeller (floatplane only) (a) McCauley 1A175/ETM 8043 Static rpm at maximum permissible throttle setting: Not over 2570. Propeller (a) McCauley 1C160/DTM 7557 Static rpm at maximum permissible throttle setting: Not over 2420. 0) to (+47.) Rudder (landplane) Right 16° ±1° Left 16° ±1° (landplane) (seaplane) Right 19° ±1° Left 15° ±1° (seaplane) (Measured parallel to W. -0° Down 23° +1°. (landplane) 4 (2 at +34 to +46. 82 IX. 2 at +73) (Occupant on child's optional jump seat at +96) 120 lb.3) at 2550 lbs. 2700 rpm (180 hp) 1. usable Takeoff 0° . Model 172P (cont'd) Normal category: 2400 lb.5 gal.. -2° Ailerons Up 20° ±1° Down 15° ±1° Elevator tab Up 28° +1°. -0° (floatplane) Up 22° +1°. 40 gal.0) to (+47. 4 PCLM (Normal Category).G.1). 1982 Engine *Fuel *Engine Limits Propeller and Propeller Limits Lycoming O-360-A4N 100LL/100 minimum grade aviation gasoline For all operations. 2 gal.3A12 14 Rev. (seaplane) Utility category: 2100 lb. 1. -0° Down 19° +1°. Model 172Q.5 in. None Normal category: 2550 lb.30° +0°. (b) Spinner: Dwg. (+35.10° Landing 0° . -0° (landplane) Elevator Up 28° +1°. -0° (Neutral position is with bottom of balance area flush with bottom of stabilizer. not under 2350 No additional tolerance permitted Diameter: not over 76 in.L. Empty Weight C.3) at 1950 lbs. or less Straight line variation between points given. approved October 15. 0509077 105 knots 127 knots 158 knots 85 knots *Airspeed Limits Maneuvering Maximum structural cruising Never exceed Flaps extended Normal category C.) Wing flaps 17274010 through 17275034 17275035 through 17275759 17275760 through 17276079 17276080 through 17276259 17276260 through 17276516 17276517 through 17276654 (1981 model) (1982 model) (1983 model) (1984 model) (1985 model) (1986 model) *Maximum Weight Number of Seats Maximum Baggage Fuel Capacity Oil Capacity Control Surface Movements Serial Numbers Eligible X. total. (-13. 2220 lb. usable (two 21. -0° Down 13° +1°. (landplane). Propeller (a) McCauley 1A170E/JFA 7658 Static rpm at maximum permissible throttle setting: Not over 2450. Cutlass. not under 74. Range (+41. at +95 42 gal.G. tanks in wings at +48) See Note 1 for data on unusable fuel.5 gal. Range *Maximum Weight . 5. 1978. 1949. Amendment 23-23 effective December 1. In addition.1559 effective March 1.1545(a). 1978. 9 qt. 3A12 issued November 4. 1978. 1978. FAR 23. Equivalent Safety Items Airspeed Indicator Operating Limitations 17261445. FAR 23. unusable Takeoff 0° . 1974.L. 17265685 CAR 3. usable (two 27 gal.951(b)(2). plus Amendments 36-1 through 36-12 for Model 172P through 172Q. 1969. 1955. at +95 54 gal. 50 gal. FAR 36 dated December 1. FAR 23. plus Amendments 36-1 through 36-5 for Model 172N. Model 172Q (cont'd) 4 (2 at +34 to +46. 1969. FAR 23. FAR 36 dated December 1. Amendment 23-23 dated December 1. In addition. 82 15 3A12 X. total. and FAR 23. effective S/N 17271035 and on. CE-1 authorized to issue airworthiness certificates under delegation option provisions of Part 21 of the Federal Aviation Regulations.757 (see Note 4 on use of CAS) (17261445.) Wing flaps 17275869 through 17276054 (1983 model) 17276101 through 17276211 (1984 model) Number of Seats Maximum Baggage Fuel Capacity Oil Capacity Control Surface Movements Serial Numbers Eligible DATA PERTINENT TO ALL MODELS 172 THROUGH 172Q Datum Front face of firewall (28000 through 47746) Lower front face of firewall (17247747 through 17276654) Upper doorsill Models 172 through 172P Part 3 of the Civil Air Regulations effective November 1. -0° Down 19° +1°. 1955. -2° Ailerons Up 20° ±1° Down 15° ±1° Elevator tab Up 22° +1°. -0° Elevator Up 28° +1°. 4. obtained by the manufacturer under Delegation Option Procedures. 1969. 2 qt. tanks in wings at +48) See Note 1 for data on unusable fuel.778(a) Leveling Means Certification Basis Model 172Q Part 3 of the Civil Air Regulations dated November 1.30° +0°. at -15. 17261578. Delegation Option Manufacturer No.Rev. 1949. -0° (Neutral position is with bottom of balance area flush with bottom of stabilizer. . as amended by 3-1 through 3-12.1559 effective March 1. plus amendments 36-1 through 36-12. Type Certificate No. as amended by 3-1 through 3-12. 17265685 through 17276259) CAR 3. effective S/N 17276260 and on. In addition.10° Landing 0° . Amendment 23-15 effective October 31. Application for Type Certificate dated July 11. -0° Down 23° +1°.) Rudder Right 16° ±1° Left 16° ±1° (Measured parallel to W. FAR 36 dated December 1. 17261578.1545(a). Production Basis Production Certificate No. 2 at +73) (Occupant on optional child's seat at +96) 120 lbs. 76 . markings. 17275869 through 17276211. Refer to applicable equipment list for the Model 172E and subsequent models. at (-13.5). UTILITY CATEGORY Maximum design weight 1950 lbs. Maneuver Entry speed Chandelles 115 mph (100 knots) Lazy eights 115 mph (100 knots) Steep turns 115 mph (100 knots) Spins Slow deceleration Stalls (except whip stalls) Slow deceleration" -1. 17247747 through 17265684 The certificated empty weight and corresponding center of gravity location must include unusable fuel of 30 lbs. 17261578. Baggage compartment and rear seat must not be occupied Flight maneuvering load factors Flaps up +4. In full view of the pilot: (1) Models 172. at (+46) and full oil of 15 lb.4 Flaps down +3. or 18 lbs. NORMAL CATEGORY Maximum design weight 2200 lbs. at (+46) through 172M (17267584) or 18 lbs. 172A and 172B "This airplane must be operated in compliance with the operating limitations stated in the form of placards. at (+46) 17267585 and on and full oil of 11. Model 172H and on: Stall warning indictor. Flight maneuvering load factors Flaps up +3. at (+46) on Models 172 and 172A. 36000 through 36999 and 46001 through 47746. NOTE 1: Current weight and balance report including list of equipment included in certificated empty weight. 0511062. 17261445. at (-15.1). 28000 through 29999. 0523112. 2.8 Flaps down +3. Serial Nos. 1.5 No acrobatic maneuvers approved except those listed below.3A12 16 Rev. at (-14). or Cessna Publication TS1000-13 should be used for equipment references on all aircraft prior to the Model 172E. Serial Nos. The equipment portion of Aircraft Specification 3A12.3 lb. Revision 17. at (+46) and full oil of 16.52 -1. Serial Nos. 17265685 through 17274009 The certificated empty weight and corresponding center of gravity location must include unusable fuel of 24 lbs. Serial Nos. 17274010 through 17276654: (Model 172P) The certificated empty weight and corresponding center of gravity location must include unusable fuel of 18 lb. Dwg. Refer to weight and balance data for loading instructions.88 lb. 82 DATA PERTINENT TO ALL MODELS 172 THROUGH 172Q (cont'd) Equipment: The basic required equipment as prescribed in the applicable airworthiness requirements (see Certification Basis) must be installed in the aircraft for certification.5 No acrobatic maneuvers including spins approved. Dwg. NOTE 2. or 24 lbs. The following placards must be displayed as indicated: A. at (+46) for Models 172I through 172M (17265684) and undrainable oil of (0) lb. This equipment must include a current Airplane Flight Manual effective S/N 17271035 and on. and loading instructions when necessary must be provided for each aircraft at the time of original certification. Model 172 through 172G: Stall warning indicator. at (+46) for Models 172B through 172H. at -20) for 172 through 172H and (0) lb. at (-14) for 172I through 172M (17265684). (Model 172Q) The certificated empty weight and corresponding center of gravity location must include unusable fuel of 24 lb. and manuals. Flight maneuvering load factors Flaps up +3. and 172K "This airplane must be operated in compliance with the operating limitations stated in the form of placards. markings. Maneuver Max. 82 17 3A12 DATA PERTINENT TO ALL MODELS 172 THROUGH 172Q (cont'd) NOTE 2.8 Flaps down +3.52 -1. Baggage compartment and rear seat must not be occupied. Maneuver Entry speed Chandelles 115 mph (100 knots) Lazy eights 115 mph (100 knots) Steep turns 115 mph (100 knots) Spins Slow deceleration Stalls (except whip stalls) Slow deceleration" (3) Models 172D. Entry speed Chandelles 122 mph (106 knots) Lazy eights 122 mph (106 knots) Steep turns 122 mph (106 knots) Spins Slow deceleration Stalls (except whip stalls) Slow deceleration" -1. Flight maneuvering load factors Flaps up +3. and manuals.76 .8 Flaps down +3.4 Flaps down +3. 172F.5 No acrobatic maneuvers including spins approved. (cont’d) A. Flight maneuvering load factors Flaps up +4. Refer to weight and balance data for loading instructions. 172E. NORMAL CATEGORY Maximum design weight 2250 lbs.5 No acrobatic maneuvers including spins approved. and manuals.76 -1.5 No acrobatic maneuvers except those listed below. NORMAL CATEGORY Maximum design weight 2300 lbs. 172H. Baggage compartment and rear seat must not be occupied. 172I. Refer to weight and balance data for loading instructions.4 Flaps down +3. markings.52 -1. UTILITY CATEGORY Maximum design weight 1950 lbs. Flight maneuvering load factors Flaps up +4.Rev. (2) Model 172C "This airplane must be operated in compliance with the operating limitations stated in the form of placards. UTILITY CATEGORY Maximum design weight 2000 lbs.5 No acrobatic maneuvers approved except those listed below. 172G. No acrobatic maneuvers including spins approved . markings. and manuals: MAXIMUMS Normal Category Utility Category 122 mph (106 knots) 122 mph (106 knots) 2300 lbs.neutralize controls.5 -1. +3. No acrobatic maneuvers approved except those listed below.8 +3.neutralize controls Known icing conditions to be avoided.5 -1.52 +4. No acrobatic maneuvers approved except those listed below.4 +3. +3.Baggage compartment and rear seat must not be occupied. Known icing conditions to be avoided. 2000 lbs. Maneuver Max.4 +3. (cont’d) A. and manuals.52 +4.forward elevator .No acrobatic maneuvers including spins approved . Intentional spins with flaps extended are prohibited. This airplane is certified for the following flight operations as of date of original airworthiness certificate: (DAY NIGHT VFR IFR)" (as applicable) . (4) Model 172L (1971 model) "This airplane must be operated in compliance with the operating limitations stated in the form of placards. 82 DATA PERTINENT TO ALL MODELS 172 THROUGH 172Q (cont'd) NOTE 2.76 Maneuvering speed (CAS) Gross weight Flight load factor Flaps up Flaps down Normal category Utility category .5 -1. MAXIMUMS Normal Category Utility Category 122 mph (106 knots) 122 mph (106 knots) 2300 lbs.Baggage compartment and rear seat must not be occupied.76 Maneuvering speed (CAS) Gross weight Flight load factor Flaps up Flaps down Normal category Utility category . markings.5 -1. This airplane is certified for the following flight operations as of date of original airworthiness certificate: (DAY NIGHT VFR IFR)" (as applicable) (5) Model 172L (1972 model) "This airplane must be operated in compliance with the operating limitations as stated in the form of placards.3A12 18 Rev.forward elevator . Maneuver Entry speed Chandelles 122 mph (106 knots) Lazy eights 122 mph (106 knots) Steep turns 122 mph (106 knots) Spins Slow deceleration Stalls (except whip stalls) Slow deceleration" Spin recovery: opposite rudder . 2000 lbs. Entry speed Chandelles 122 mph (106 knots) Lazy eights 122 mph (106 knots) Steep turns 122 mph (106 knots) Spins Slow deceleration Stalls (except whip stalls) Slow deceleration" Spin recovery: opposite rudder .8 +3. flight. Altitude loss in a stall recovery .neutralize controls Intentional spins with flaps extended are prohibited. 17260759 through 17265684 except 17261445 and 17261578 "This airplane must be operated as a normal category airplane in compliance with the operating limitations as stated in the form of placards. Abrupt use of the controls prohibited above 112 mph Spin recovery: opposite rudder -.8 +3.52 Flaps down +3. 17260759 through 17265684 except 17261445 and 17261578 "This airplane must be operated in compliance with the operating limitations as stated in the form of placards.Baggage compartment and rear seat must not be occupied. Flight into known icing conditions prohibited.52 +4.No acrobatic maneuvers including spins approved . including spins approved.0 -1. -1. and manuals.76 Maneuvering speed (CAS) Gross weight Flight load factor Flaps up Flaps down Normal category Utility category . +3. MAXIMUMS Maneuvering speed Gross weight Flight load factor 110 mph (96 knots) (CAS) 2220 lbs.200 ft. 82 19 3A12 DATA PERTINENT TO ALL MODELS 172 THROUGH 172Q (cont'd) NOTE 2. This airplane is certified for the following flight operations as of date of original airworthiness certificate: (DAY NIGHT VFR IFR)" (as applicable) . retract for takeoff. (cont’d) A. Flight into known icing conditions prohibited. and manuals. markings.8. This airplane is certified for the following flight operations as of date of original airworthiness certificate: (DAY NIGHT VFR IFR)" (as applicable) Model 172M (Floatplane) 17256493. Recommended Recommended Maneuver Entry speed Maneuver Entry Speed Chandelles 120 mph (104 knots) Spins Slow deceleration Lazy eights 120 mph (104 knots) Stalls (except Slow deceleration Steep turns 112 mph ( 97 knots) whip stalls) Altitude loss in stall recovery -. (6) Model 172M (Landplane) 17256493. No acrobatic maneuvers approved except those listed below.180 feet.4 +3. and landing. Flaps up +3.0 -1.Rev.forward elevator -. markings. No acrobatic maneuvers.0 WATER RUDDER: Extend for taxi. 2000 lbs. MAXIMUMS Normal Category Utility Category 112 mph (97 knots) 112 mph (97 knots) 2300 lbs. Utility category . and manuals. Altitude loss in a stall recovery 200 ft. (DAY NIGHT VFR IFR)" (as applicable) Model 172M and 172N (Floatplane) (17265685 through 17271034) FLOATPLANE "This airplane must be operated as a normal category airplane in compliance with the operating limitations as stated in the form of placards. NIGHT VFR IFR)" (as applicable) Forward of fuel selector valve: (All models through S/N 17265684 except 17261445 and 17261578) "Both tanks on for takeoff and landing. (cont’d) A.neutralize controls. Flight into known icing conditions prohibited. Flaps up Flaps down +3. +3. MAXIMUMS Maneuvering speed (CAS) Gross weight Flight load factor 96 knots 2220 lbs. (7) Model 172M and 172N (Landplane) (17261445.52 +3. and manuals. Abrupt use of the controls prohibited above 97 knots Spin recovery: opposite rudder .Baggage compartment and rear seat must not be occupied." . This airplane is certified for the following flight operations as of date of original airworthiness certificate. including spins approved. 82 DATA PERTINENT TO ALL MODELS 172 THROUGH 172Q (cont'd) NOTE 2.forward elevator . Intentional spins with flaps extended are prohibited.8. MAXIMUMS Normal Category Utility Category 97 knots 97 knots 2300 lbs. No acrobatic maneuvers. markings.4 +3.76 Maneuvering speed (CAS) Gross weight Flight load factor Flaps up Flaps down Normal category . 17261578.180 feet.0 -1. -1.3A12 20 Rev. retract for takeoff.8 +3. Flight into known icing conditions prohibited. flight and landing. 2000 lbs.0 Water Rudder: Extend for taxi. markings. 17265685 through 17271034 except 17270050) "This airplane must be operated in compliance with the operating limitations stated in the form of placards.52 +4. NO ACROBATIC MANEUVERS EXCEPT THOSE LISTED BELOW: Recommended Recommended Maneuver Entry speed Maneuver Entry Speed Chandelles 105 knots Spins Slow deceleration Lazy eights 105 knots Stalls (except Slow deceleration Steep turns 95 knots) whip stalls) Altitude loss in stall recovery . This airplane is certified for the following flight operations as of date of original airworthiness certificate: (DAY B.0 -1.No acrobatic maneuvers including spins approved. 19. maximum baggage and/or auxiliary seat passenger. 17261578. Models 172 through 172E (1) "Flaps . maximum baggage and/or auxiliary passenger forward of baggage door latch. G.Rev. and 172H "Both 36 gal. Off" (2) Model 172B "Both Left Right Off" 39 gal." Near flap indicator Models 172F (electric flaps) through 17271034. For additional loading instructions see weight and balance data. Off" (4) Model 172I through 172M (except 17261445 and 17261578) "Both 38 gal. 82 21 3A12 DATA PERTINENT TO ALL MODELS 172 THROUGH 172Q (cont'd) NOTE 2." In baggage compartment: (1) Models 172 through 172B "Maximum baggage 120 lb. (3) Model 172C." (2) Model 172C through 172M (1973 model) "120 lb. On the fuel selector valve (at appropriate location) (1) Model 172 and 172A "Both 37 gal.40° (2) "Avoid slips with flaps down. Left 18." Near ammeter (Models 17258487 through 17259903) "Do not turn off alternator in flight except in emergency. (all flight altitudes) (Takeoff-landing) Left 20 gal. excluding 17270050 "120 lb. (level flight only) Right 19 gal.5 gal.Pull to extend Takeoff Retract 0° 1st notch 10° Landing 0° . see weight and balance data. On flap handle. 172F. (level flight only) Right 20 gal. (level flight only) Off" (5) Model 172N (17261445. 172G.5 gal." (3) 17261899 through 17271034. Left 18 gal. (level flight only) Off" D. maximum baggage aft of baggage door latch maximum 120 lb. For additional loading instructions. (all flight attitudes) Left 19 gal. (cont’d) C. excluding 17270050) "Avoid slips with flaps extended.5 gal. 172E." E. 172D. 19. Right 18 gal.5 gal. For additional loading instructions see weight and balance data." "50 lb. . Right 18. excluding 17270050) "Both 40 gal. combined. 17267585 through 17271034. F. " Near ammeter and adjacent to overvoltage light: (1) Model 172L (1972) through Model 172N (1978) "High Voltage" J. AND MANUALS. NIGHT VFR IFR" (as applicable) Near tachometer on Models 172I.1st notch -10° Water rudder . retract for takeoff. Above 75 percent power in cruise 2. (1) Model 172A through 172I in full view of the pilot. Flaps . .takeoff. This airplane is certified for the following flight operations as of date of original airworthiness certificate: DAY I. "Operate as normal category airplane except: Maximum weight 2220 lbs. approved. -1. flight and landing . Extend: Taxi. "MAXIMUMS Maneuvering speed Gross weight Flight load factor Flaps up Flaps down +3. Refer to weight and balance data for loading instructions. -1. Flaps .30°. Maximum altitude loss in stall recovery . Known icing conditions to be avoided. Maximum altitude loss in stall recovery 120 ft.8.10° . . (cont’d) H. +3.takeoff .3A12 22 Rev.pull to extract Retract . MARKINGS. Flight maneuvering load factors Flaps up Flaps down No acrobatic maneuvers including spins approved.120 ft. FLAPS: 10° for takeoff No acrobatic maneuvers.8." (3) Model 172F through 17271034. AND MANUALS NORMAL CATEGORY .52 +3. .taxi.120 ft. Water rudder: Pull to retract . flight and landing. flight and landing Extend . .FLOATPLANE Maximum weight 2220 lb. excluding 17270050. .5 122 mph CAS (106 knots) 2220 lbs.5 WATER RUDDER: Extend for taxi.52 +3. Altitude loss in stall recovery . . . . Above 2500 rpm in full throttle climb. in full view of the pilot. 172K and 172L (with IC172/MTM propeller): "Avoid continuous operation 1. Flaps: Takeoff . MARKINGS. 82 DATA PERTINENT TO ALL MODELS 172 THROUGH 172Q (cont'd) NOTE 2. Retract: Takeoff. including spins. Additional placards required in seaplane." (4) Model 172L in full view of the pilot: "FLOATPLANE THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN COMPLIANCE WITH THE OPERATING LIMITATIONS AS STATED IN THE FORM OF PLACARDS." (2) Model 172K in full view of the pilot: "THIS AIRPLANE MUST BE OPERATED IN COMPLIANCE WITH THE OPERATING LIMITATIONS AS STATED IN THE FORM OF PLACARDS. "Floatplane Max. 757 when approved airspeed calibration data presented in Section V of the Pilot's Operating Handbooks listed below is available to the pilot (TIAS is exactly equal to CAS): 172M.S." L." (4) Model 172N (17261445. Cessna P/N D1057-13 (S/N 17265685 through 17267584) 172N. grade aviation gasoline Cap. 172A and 172B "FUEL 80/87 min. Near fuel tank filler (1) Model 172. 82 23 3A12 DATA PERTINENT TO ALL MODELS 172 THROUGH 172Q (cont'd) NOTE 2. Cessna P/N D1192-13PH (S/N 17274010 through 17275034) 172P. gal. except 17258105 through 17258112 and 17261578) 28-volt electrical system (S/N 17258105 through 17258112. 21. Compliance with Service Letter SE74-16 . grade aviation gasoline Cap. Near fuel selector valve on models with serial numbers 28000 through 17258855. 17269310 through 17271034 except 17270050) 172N.5 US." M.allows rpm's as follows: Landplane: not over 2420. 19. (cont’d) K. 21 US. grade aviation gasoline Cap. Effective 17270050. 21 U. not under 2445 The marking of the airspeed indicator in CAS provides an equivalent level of safety to CAR 3. and 172H "FUEL 80/87 min. Cessna P/N D1082-13 (S/N 17261445. 172D.Carburetor Nozzle Replacement ." (2) Model 172C. Cessna P/N D1138-13PH (S/N 17271035 through 17272884) 172N. 172E. gal. Cessna P/N D1231-13PH (S/N 17275760 through 17276079) 172P.Rev. grade aviation gasoline Cap. 172F. 17267585 through 17269309) 172N. SK-172-31B or SK-172-32 installed: "SWITCH TO SINGLE TANK OPERATION IMMEDIATELY UPON REACHING CRUISE ALTITUDES ABOVE 5000 FEET.S. not under 2300 Seaplane: not over 2570. excluding 17270050) "FUEL 100LL/100 min." (5) Model 172N (17261578. gal. grade aviation gasoline Cap. gal. Cessna P/N D1109-13 (S/N 17261578. 17271035 through 17276654 All placards required in the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual must be installed in the appropriate locations. except those with Cessna Kit No. Cessna P/N D1251-13PH (S/N 17276080 through 17276259) 14-volt electrical system (172 series through S/N 17269309. NOTE 5. 17261578 and 17269310 through 17276654) NOTE 4. 21. gal.5 US.5 U. 17269310 through 17271034. 172G. Cessna P/N D1172-13PH (S/N 17270050. 17267585 through 17269309) "FUEL 100/130 min. 17272885 through 17274009) 172P." (3) Model 172I through 172M (except 17261445 and 17261578) "FUEL 80/87 min. NOTE 3. . Cessna P/N D1212-13PH (S/N 17275035 through 17275759) 172P. 065 No Additional Tolerance Permitted Diameter: Not over 75 inches.5 g.300 No Additional Tolerance Permitted Diameter: Not over 76 inches.1011-1. and (3) Forward and aft center of gravity limits may not be exceeded. 0550236 Propeller Limits Static RPM at full throttle: Not over 2. Increased stall speeds and reduced climb performance should be expected for the increased weights. 2.400 RPM When Modified by Cessna Modification Kit MK172-72-01 (See NOTE 4) For all operations. Flight characteristics and performance at the increased weights have not been evaluated.3A12 24 Rev. Approved June 21. 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. 4 PCLM (Normal Category). 2. and (2) The Never Exceed Airspeed (VNE) and Maximum Structural Cruising Speed (VC) must be reduced by 30%. Not Under 2. Requirements for any additional oil should established in accordance with Advisory Circular AC23. to -1.400. not under 74 inches When Modified by Cessna Modification Kit MK172-72-01 (See NOTE 4) Static RPM at full throttle: Not over 2. Not Under 2.165.Model 172R. 1996 Engine Lycoming IO-360-L2A. the prescribed operating limitations indicated by an asterisk (*) under Sections I through X of this data sheet must also be displayed by permanent markings. XI . 0550236 When Modified by Cessna Modification Kit MK172-72-01 (See NOTE 4) (a) McCauley Model 1A170E/JHA7660 (b) Spinner: Drawing No. Rated 180 Horsepower Fuel Engine Limits 100/100LL minimum grade aviation gasoline For all operations.700 RPM Propeller (a) McCauley Model 1C235/LFA7570 (b) Spinner: Drawing No. 82 DATA PERTINENT TO ALL MODELS 172 THROUGH 172Q (cont'd) NOTE 6: Special Ferry Flight Authorization. and (4) Structural load factors of +2. Skyhawk. 2 PCLM (Utility Category). may not be exceeded. Flight Permit for operations of overweight aircraft may be found in Advisory Circular AC21-4B In addition to the placards specified above. not under 75 inches Airspeed Limits Maneuvering Max Structural Cruising Never Exceed Flaps Extended 99 Knots IAS 129 Knots IAS 163 Knots IAS 85 Knots IAS ( 97 Knots CAS) (126 Knots CAS) (160 Knots CAS) ( 84 Knots CAS) When Modified by Cessna Modification Kit MK172-72-01 (See NOTE 4) Maneuvering 105 Knots IAS (102 Knots CAS) Max Structural Cruising 129 Knots IAS (126 Knots CAS) Never Exceed 163 Knots IAS (160 Knots CAS) Flaps Extended 85 Knots IAS ( 84 Knots CAS) .0 g. Rated 160 Horsepower When Modified by Cessna Modification Kit MK172-72-01 (See NOTE 4) Lycoming IO-360-L2A. Flight Standards District Offices are authorized to issue Special overweight ferry flight authorizations. 0 inches aft of datum at 1.100 pounds to 35.0 inches aft of datum When Using POH. (2) Forward Limits Linear variation from 41.8 inches.0 inches aft of datum at 2.200 pounds to 35.Model 172R C.457 pounds Maximum Takeoff and Landing 2. 35.5 inches aft of datum at 2.AFM 172RPHUS-00 or later rev or 172RPHAUS-00 thru -03 Normal Category (1) Aft Limits 47.950 pounds or less.0 inches aft of datum at 1.0 inches aft of datum at 1. Range (cont’d) When Using POH.950 pounds or less.0 inches aft of datum at 2. Range Reference Datum MAC Leveling Means Maximum Weights None Lower portion of front face of firewall 58.950 pounds.5 inches aft of datum at 2.0 inches aft of datum at 1.950 pounds or less.200 pounds or less.200 pounds .3 inches aft of datum at 2.Rev.550 pounds or less.AFM 172RPHAUS-04 or later rev or 172RPHBUS-00 or later rev Normal Category (1) Aft Limits 47. Leading edge of MAC 25.0 inches aft of datum at 2.950 pounds.0 inches aft of datum at 1. Utility Category (1) Aft Limits 40. (2) Forward Limits Linear variation from 40.950 pounds or less. 82 25 3A12 XI .G.0 inches aft of datum at 1.3 inches aft of datum at 2.100 pounds When Using POH. Utility Category (1) Aft Limits 40.0 inches aft of datum at 1. (2) Forward Limits Linear variation from 36.450 pounds or less.0 inches aft of datum at 1.950 pounds. Empty Wt. When Using POH.3 inches aft of datum at 2.200 pounds or less.450 pounds to 35.5 inches aft of datum at 2. 35. C.950 pounds.450 pounds Utility Category Maximum Ramp Maximum Takeoff and Landing 2.0 inches aft of datum at 1.AFM 172RPHAUS-04 or later rev or 172RPHBUS-00 or later rev Normal Category Maximum Ramp 2.950 pounds.450 pounds or less.950 pounds.0 inches aft of datum at 1. (2) Forward Limits Linear variation from 37. 35.207 pounds 2.AFM 172RPHUS-00 or later rev or 172RPHAUS-00 thru -03 Normal Category Maximum Ramp 2.5 inches aft of datum at 2.5 inches aft of datum at 2.450 pounds Utility Category Maximum Ramp Maximum Takeoff and Landing 2.5 inches aft of datum at 2. Utility Category (1) Aft Limits 40. (2) Forward Limits Linear variation from 40.100 pounds or less.950 pounds or less.0 inches aft of datum at 1.0 inches and 142. 35.450 pounds to 35. 35. 35. When Modified by Cessna Modification Kit MK172-72-01 (See NOTE 4) Normal Category (1) Aft Limits 47.457 pounds Maximum Takeoff and Landing 2.200 pounds to 35. (2) Forward Limits Linear variation from 37.0 inches aft of datum at 1.9 inches aft of datum Left side of Tailcone at 108.G.107 pounds 2.950 pounds or less.550 pounds to 35. 23.1 inches forward of datum 3. FAR 23.605.775.787. 23.331.) Control Surface Movements Wing flaps Takeoff 0º .1524 as amended by Amendment 23-10.1357. as amended by 23-1 through 23-6. FAR 23. 23.10º Landing 0º .0 inches aft of datum) See NOTE 1 for data on unusable fuel.1093.871.731 as amended by Amendment 23-45.701. FAR 23.0 inches aft of datum When Modified by Cessna Modification Kit MK172-72-01 (See NOTE 4) 120 pounds at 82. 23.0 inches aft of datum (Maximum combined weight capacity for baggage areas is 120 pounds. FAR 23.771.562(b)2.1303. 1965.33.1361 and 23.0 inches aft of datum 50 pounds at 108.781 as amended by Amendment 23-33. and 23.619.1385 as amended by Amendment 23-43.689.) 56 gallons total. 23. 23. .423.5 quarts usable When Modified by Cessna Modification Kit MK172-72-01 (See NOTE 4) 2.) Fuel Capacity (Gal. 23.): Right 16° 10’± 1° Left 16° 10’ ± 1° Rudder (Measured perpendicular to Hinge: Right 17° 44’ ± 1° Left 17° 44’ ± 1° Certification Basis Part 23 of the Federal Aviation Regulations effective February 1. 23.735.1143(g).485. and 23. 23. 23.685.675.1545 as amended by Amendment 23-23. and 23. FAR 23.562(c)1. 23. FAR 23. 23.321.1309 and 23.0 inches aft of datum. 23.1 inches forward of datum 3.53.623.0 to 46.951 as amended by Amendment 23-15. and 23. FAR 23. 23. 23.1563 as amended by Amendment 23-7.301. 53 gallons usable (Two 28 gallon tanks in wings at 48. 82 XI . FAR 36 dated December 1.853(a).733.1549 as amended by Amendment 23-28. FAR 23. 23.0 gallons at 13.1365 as amended by Amendment 23-14. 23.1. FAR 23. 23.562(c)2. 23. 23.961.1353. 23.831 as amended by Amendment 23-42.603.0 quarts usable Oil Capacity (Gal. FAR 23.562(c)4 as amended by Amendment 23-44. 2 at 73.507. 23.200 pounds No. FAR 23.305. 23.677. 23.427.351. 23.562(a). 23.1322 as amended by Amendment 23-17.0 to 142.1329 and 23.779 and 23.1559 as amended by Amendment 23-21.1323.550 pounds Utility Category Maximum Ramp Maximum Takeoff and Landing 2.208 pounds 2. FAR 23. 23. except as follows: FAR 23.562(c)3. 23.607.3A12 26 Rev.30º + 0°/-2° Ailerons Up 20° ± 1° Down 15° ± 1° Elevator tab Up 22° + 1°/-0° Down 19° + 1°/-0° Elevator Up 28° + 1°/-0° Down 23° + 1°/-0° (Neutral position is with bottom of balance area flush with bottom of stabilizer) Rudder (Measured parallel to W. 23. 23. FAR 23.655 and 23. 23. 23.621. 23.1301 as amended by Amendment 23-20. 23. 23.558 pounds Maximum Takeoff and Landing 2.611. FAR 23.L.1147(b).561 as amended by Amendment 23-34. as amended by Amendments 36-1 through 36-21.0 gallons at 13.0 inches aft of datum) 120 pounds at 95.0 to 108.807 and 23.613. 2. and 23. 23. 23. 23.441 and 23. of Seats Maximum Baggage 4 (2 at 34. 1969.Model 172R (cont’d) When Modified by Cessna Modification Kit MK172-72-01 (See NOTE 4) Normal Category Maximum Ramp 2. 23.51 and 23.(b) and (c). 23. 1301. 1996. 14 CFR 23. 14 CFR 23.1309(a)(1)(2).1309(a)(1)(i).1567(a) as amended by Amendment 23-50. 23. 23. (e).1329 (g)(h).1553.1501 and 23. and 17280031 and on.1351(a)(1).1431(a)(b)(d)(e) as amended by Amendment 23-49. 23. (b)(4)(ii).1563(a) and 23.1529 as amended by Amendment 23-26.N/C. (a)(3). Refer to ACE-07-10.1322.605 as amended by Amendment 23-23. 14 CFR 23.1329 (a)(c)(d)(e)(f) as amended by Amendment 23-49. Applies to airplane serial numbers 17280014. 82 27 3A12 XI . (c)(3).Rev. 23. (b)(2)(i). (b)(3)(i). 23. 14 CFR 23. (b)(3). and 23. (a)(2). 23. 23.303. 23. and 23.1321 (a)(c)(d)(e).1311. (d). 17280021 through 17280029. 17280017. 23.1365(a)(b)(d)(e)(f) and 23.1331 and 23. 23. Cessna Model 172R Airplane. (b)(1). 1995.(b)(4)(i). (b)(3). (b)(5). (b)(2) as amended by Amendment 23-21.1525and 23. (b)(4).1303(a)(b)(c)(f). 23. 14 CFR 23. Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the airplane for certification. Refer to FAA letter dated 3/22/96 14 CFR § 23." Data Pertinent to Model 172R: Production Basis Production Certificate No. PC-4 issued March 28. Type Certificate No. (b)(3). 14 CFR 23. Installation of Electronic Flight Instrument System and and the Protection of the System From High Intensity Radiated Fields (HIRF). (c). CE-1 in accordance with Part 21 of the Federal Aviation Regulations. (d)(1). 23-159-SC. (d). 14 CFR 23. (a)(2). (b)(1). (a)(2).1093.777(a)(b). (c)(d)(e).1147(b). Equivalent Safety Items (1) Induction System Icing Protection (2) Throttle Control (3) Mixture Control (4) Anti-Collision Light System (5) Aviation White Color Reqmt FAR § 23.1367 and 23. (f)(1).603 and 23. 23. (b)(2)(3).901(a)(b) as amended by Amendment 23-53.1323(a). Airplane serial numbers not listed were produced under Type Certificate only. 23. (c) as amended by Amendment 23-17.1555(a)(b). (b)(2). (b)(2)(ii).1583(a). (a)(2). Refer to FAA letter dated 3/22/96 FAR § 23.1585(a)(b)(d) as amended by Amendment 23-34. 23.771(a) as amended by Amendment 23-14. (b)(4)(iii). (b)(1). 23.305. (c)(2)(iii).1325(a).Model 172R (cont’d) Additions for the Garmin G1000 Integrated Cockpit System (ICS) Only: 14 CFR 23. 14 CFR 23.301 as amended by Amendment 23-42. 23. 23. 14 CFR 23. (b)(2). 14 CFR 23.607 and (Electrical System) 23. 14 CFR 23. 23. FAA letter dated 11/29/07 Date of Application for Amended Type Certificate was September 25. (a)(2)(i). 23.1353(a)(b)(c)(d)(e). (b)(1). 17280015. (b)(4)(iv). (a)(1)(ii).1545(a).955(a)(2).1589 as amended by Amendment 23-13.1381 as amended by Amendment 23. (b)(1)(iii).561(e). “Special Conditions: Cessna Aircraft Company. (c)(4). Certification Basis (cont’d) Additions for the Garmin GFC-700 Automatic Flight Control System (AFCS) only: 14 CFR 23.1143(g). FAA letter dated 10/12/07 14 CFR § 23.1357(a)(b)(c)(d) as amended by Amendment 23-43. (c) as amended by Amendment 23-51. (b)(1).1397(c). 23. 23. (b)(2)(i).1581(a)(2).1359(c). (b)(6)(i) as amended by Amendment 23-52. 14 CFR 23. (a)(2). (c)(1). 3A12 was amended June 21.773(a)(1).601. 14 CFR 23.1305(a)(1). 23.1549 as amended by Amendment 23-45. 23.1401(d).307. Cessna is authorized to issue airworthiness certificates under the delegation provisions of Delegation Option Authorization No. 23. 14 CFR 23. 14 CFR 23. (b)(2).1523. 1997. (b)(1).1361. .1547(e) as amended by Amendment 23-20.1335 as amended by Amendment 23-20. 14 CFR 23. Serial Numbers Eligible 17280001 and On Special Conditions as follows: No. 14 CFR 23. (c). 23.1163(a). Refer to FAA letter dated 5/3/96 FAR § 23. Refer to ACE-07-09. 23.1327 and 23. (b)(4)(i).1337(a)(1). (f).1541(a)(1). 23.1543(b)(c). may not be exceeded. Applicable serial numbers are as follows: 17280159 17280262 17280426 17280609 17280621 17280632 17280640 17280653 17280664 17280672 17280707 17280242 17280281 17280488 17280610 17280622 17280633 17280646 17280659 17280667 17280673 17280251 17280292 17280606 17280613 17280623 17280634 17280647 17280660 17280668 17280674 17280253 17280301 17280607 17280614 17280624 17280638 17280648 17280661 17280669 17280675 17280257 17280305 17280608 17280616 17280631 17280639 17280652 17280662 17280670 17280701 NOTE 4: .5 g. The airplane must be operated according to the appropriate AFM. Only certain Model 172R airplane serial numbers are eligible for modification by Cessna Modification Kit MK172-72-01. NOTE 2: The airplane must be operated according to the appropriate Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual (POH/AFM). POH/AFM part number 172RPHUS00 (or later approved revision) is applicable to Production Model 172R. and (4) Structural load factors of +2. Requirements for any additional oil should be established in accordance with Advisory Circular AC23. Increased stall speeds and reduced climb performance should be expected for the increased weights. unless specifically noted otherwise in the Supplement. part number 172RMM00 (or later revision) . Flight Permit for operations of overweight aircraft may be found in Advisory Circular AC21-4B. NOTE 3: Special Ferry Flight Authorization. and full oil of 15.” FAA Approved Airplane Flight Manual (AFM): Part Number 172RPHAUS-00 (or later FAA approved revisions) is applicable to the Model 172R equipped with Garmin G1000 Integrated Cockpit System. All FAA required placards are included in Section 2 of the applicable POH/AFM.3A12 28 Rev. FAA Approved Airplane Flight Manual (AFM): Part Number 172RPHBUS-00 (or later FAA approved revisions) are applicable to the Model 172R equipped with Garmin G1000 Integrated Cockpit System and Garmin GFC-700 AFCS. Required placards are included in the AFM. “Placards and Markings. Required placards are included in the AFM. 17280001 and On The certificated empty weight and corresponding center of gravity location must include unusable fuel of 18 pounds at 46. Chapter Eleven (11).0 g. are also applicable to part number 172R180PH00. Flight Standards District Offices are authorized to issue Special overweight ferry flight authorizations. and (3) Forward and aft center of gravity limits may not be exceeded. 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.0 pounds at 13.1011-1. and (2) The Never Exceed Airspeed (VNE) and Maximum Structural Cruising Speed (VC) must be reduced by 30%. Placards may also be found in the Maintenance Manual. to -1. All POH/AFM Supplements approved for part number 172RPHUS00.0 inches aft of datum. POH/AFM part number 172R180PH00 (or later approved revision) is applicable to Production Model 172R airplanes when modified by Cessna Modification Kit MK172-72-01. The airplane must be operated according to the appropriate AFM. 82 Data Pertinent to Model 172R: (cont’d) NOTE 1: Weight and Balance: Serial Nos.1 inches forward of datum. Flight characteristics and performance at the increased weights have not been evaluated. Utility Category (1) Aft Limits (2) Forward Limits 40. 35.0 inches aft of datum Normal Category Maximum Ramp Maximum Takeoff and Landing Utility Category Maximum Ramp Maximum Takeoff and Landing 2. Approved May 1.0 inches aft of datum (Max. Not Under 2300 Diameter: Not over 76 inches. Linear variation from 41.0 inches aft of datum) See NOTE 1 for data on unusable fuel. 8.200 pounds to 35.0 inches aft of datum at 1.700 RPM (a) McCauley Model 1A170E/JHA7660 (b) Spinner: Drawing No. 2.G.550 pounds to 35. 1998 Engine Fuel Engine Limits Propeller Lycoming IO-360-L2A.950 pounds or less.0 to 46.950 pounds or less. C.550 pounds or less.200 pounds or less.0 inches aft of datum at 1.0 to 108.1 inches forward of datum 3.8 inches.Model 172S. 35.0 inches aft of datum) 120 pounds at 82.0 inches aft of datum at 1. Skyhawk SP.208 pounds 2. 0550236 Static RPM at full throttle: Not over 2400.9 inches aft of datum Left side of Tailcone at 108.0 inches aft of datum.950 pounds.) .0 to 142.) Oil Capacity (Gal.950 pounds.0 inches and 142. Rated 180 Horsepower 100/100LL minimum grade aviation gasoline For all operations. 53 gallons usable (Two 28 gallon tanks in wings at 48.0 quarts at 13. combined weight capacity for baggage areas is 120 pounds) 56 gallons total. Leading edge of MAC 25. Range 47.550 pounds 2.0 quarts usable Fuel Capacity (Gal. of Seats Maximum Baggage 4 (2 at 34.558 pounds 2.0 inches aft of datum at 1.0 inches aft of datum 50 pounds at 108. 4 PCLM (Normal Category). 2 at 73.3 inches aft of datum at 2. Linear variation from 37. 82 29 3A12 XII . not under 75 inches Maneuvering Max Structural Cruising Never Exceed Flaps Extended Normal Category (1) Aft Limits (2) Forward Limits 105 Knots IAS 129 Knots IAS 163 Knots IAS 85 Knots IAS (102 Knots CAS) (126 Knots CAS) (160 Knots CAS) ( 85 Knots CAS) Propeller Limits Airspeed Limits C. Empty Wt. Range Reference Datum MAC Leveling Means Maximum Weights None Lower portion of front face of firewall 58.Rev.0 inches aft of datum at 2.5 inches aft of datum at 2.G.200 pounds No. 2 PCLM (Utility Category).5 inches aft of datum at 2. FAR 23. 23. Certification Basis (cont’d) Additions for the Garmin G1000 Integrated Cockpit System (ICS) Only: Additions for the Garmin G1000 Integrated Cockpit System (ICS) Only: 14 CFR 23. 23. FAR 23. (c)(2)(iii). 23. 23. 23. FAR 23.607 and (Electrical System) 23.1303(a)(b)(c)(f).1337(a)(1). 23. 14 CFR 23.1555(a)(b). (c)(1).1563 as amended by Amendment 23-7.619.871. 23. (a)(2).951 as amended by Amendment 23-15.1367 and 23.427.562(a).1563(a) and 23. 23. 23.1585(a)(b)(d) as amended by Amendment 23-34. and 23.1525 and 23. 23.613. 23. 23. (d)(1).562(c)2.1321 (a)(c)(d)(e).1329 (a)(c)(d)(e)(f) as amended by Amendment 23-49.1353(a)(b)(c)(d)(e). 23.1501 and 23. 23.601. (f) and 23.735.777(a)(b). 23. as amended by 23-1 through 23-6. FAR 23. (b)(4)(iii).1524 as amended by Amendment 23-10. 23.1323(a). FAR 23.731 as amended by Amendment 23-45. (c)(d)(e). 23.1357. 14 CFR 23.1303.1309(a)(1)(i). 14 CFR 23.1545(a). except as follows: FAR 23. (a)(2). 23. FAR 23. 14 CFR 23.441 and 23.1311.331.1093. 1965. 14 CFR 23.1323. (d).1381 as amended by Amendment 23.1322.1365 as amended by Amendment 23-14. 14 CFR 23.603.507.831 as amended by Amendment 23-42. 23.1335 as amended by Amendment 23-20. 23. (c)(3).321.562(c)4 as amended by Amendment 23-44. FAR 23. 23. (b)(2).675. (c) as amended by Amendment 23-51. 14 CFR 23. 23. 14 CFR 23. (b)(3)(i). (b)(1)(iii).621. FAR 23. 23.(b)(4)(i).305. 23.561(e). 23.853(a). 23.N/C.775. 23. Certification Basis .1329 (g)(h). 23.1309 and 23. as amended by Amendments 36-1 through 36-21.1567(a) as amended by Amendment 23-50.301 as amended by Amendment 23-42. 23. (b)(5). (b)(1). 14 CFR 23.1325(a).605 as amended by Amendment 23-23. 23.562(c)1.779 and 23.1523.955(a)(2). (b)(4). and 23. 1969.1357(a)(b)(c)(d) as amended by Amendment 23-43.807 and 23. (c). 23. FAR 36 dated December 1. (b)(1). 23. 23. (f)(1).1163(a).1549 as amended by Amendment 23-28. 14 CFR 23. (b)(2)(i).33. 23. (b)(3). (b)(2)(ii).1559 as amended by Amendment 23-21. (a)(2).10º Landing 0º .): Right 16° 10’± 1° Left 16° 10’ ± 1° Rudder (Measured perpendicular to Hinge: Right 17° 44’ ± 1° Left 17° 44’ ± 1° Part 23 of the Federal Aviation Regulations effective February 1.3A12 30 Rev.(b) and (c). (c) as amended by Amendment 23-17. 23.Model 172S (cont’d) Control Surface Movements Wing flaps Takeoff 0º . 82 XII . (b)(3).1322 as amended by Amendment 23-17. 23. 23. 23. (b)(2). and 23.305.1331 and 23.1385 as amended by Amendment 23-43.351.30º + 0°/-2° Ailerons Up 20° ± 1° Down 15° ± 1° Elevator tab Up 22° + 1°/-0° Down 19° + 1°/-0° Elevator Up 28° + 1°/-0° Down 23° + 1°/-0° (Neutral position is with bottom of balance area flush with bottom of stabilizer) Rudder (Measured parallel to W. (c). FAR 23. (a)(2)(i).1361 and 23.771(a) as amended by Amendment 23-14. 23.689. 23.781 as amended by Amendment 23-33.1147(b).1545 as amended by Amendment 23-23. (a)(1)(ii). FAR 23. 23. 23. 14 CFR 23.605. 23.1301 as amended by Amendment 23-20. 23. (b)(1). 14 CFR 23.1547(e) as amended by Amendment 23-20.485.771.562(c)3. 23.611.562(b)2.1327 and 23. FAR 23. (d).303. and 23.1583(a).603 and 23. 23. 14 CFR 23.1351(a)(1). FAR 23. and 23. (c)(4). (b)(6)(i) as amended by Amendment 23-52. (b)(2)(i).1431(a)(b)(d)(e) as amended by Amendment 23-49.1541(a)(1).301. (b)(2) as amended by Amendment 23-21. 14 CFR 23. 23.1361.561 as amended by Amendment 23-34. (b)(4)(i).607. 14 CFR 23. 14 CFR 23.1329 and 23.1549 as amended by Amendment 23-45. 23. (b)(1). 23. 23. 23. (b)(2)(3).961.1543(b)(c). (e). 23. Additions for the Garmin GFC-700 Automatic Flight Control System (AFCS) only: 14 CFR 23.423.623. 23.1365(a)(b)(d)(e)(f) and 23. (b)(1).1143(g). 23. 23. (a)(2).1553. 23.1589 as amended by Amendment 23-13. 23. (b)(1). 23.1359(c). and 23. (b)(3).677. (b)(4)(ii).901(a)(b) as amended by Amendment 23-53. 23. FAR 23.701.773(a)(1). 23.L.1309(a)(1)(2).685.53. 23. 23. (b)(4)(iv).1. (a)(3). (a)(2).1529 as amended by Amendment 23-26. (b)(2).1305(a)(1). 14 CFR 23.1353. FAR 23.787. 23.307.51 and 23. 23. 23. 23.655 and 23. 23.1301.733.1581(a)(2). 1397(c).1143(g). Flight Permit for operations of overweight aircraft may be found in Advisory Circular AC21-4B NOTE 2: . 82 31 3A12 XII . Required placards are included in the AFM. Chapter 11.1147(b).1093. Refer to FAA letter dated 5/1/98 FAR § 23... Flight Standards District Offices are authorized to issue Special overweight ferry flight authorizations.1011-1. FAA Approved Airplane Flight Manual (AFM): Part Number 172SPHBUS-00 (or later FAA approved revisions) are applicable to the Model 172S equipped with Garmin G1000 Integrated Cockpit System and Garmin GFC-700 AFCS.” FAA Approved Airplane Flight Manual (AFM): Part Number 172SPHAUS-00 (or later FAA approved revisions) is applicable to Model 172S equipped with Garmin G1000 Integrated Cockpit System. Installation of Electronic Flight Instrument System and the Protection of the System From High Intensity Radiated Fields (HIRF). Refer to FAA letter dated 5/1/98 14 CFR § 23. 3A12 was amended May 1." Data Pertinent to Model 172S: Production Basis Production Certificate No. NOTE 1: Weight and Balance: Serial Nos. Required placards are included in the AFM. and (2) The Never Exceed Airspeed (VNE) and Maximum Structural Cruising Speed (VC) must be reduced by 30%.Rev. Cessna is authorized to issue airworthiness certificates under the delegation provisions of Delegation Option Authorization No. Applies to airplane serial numbers 172S8003 and on. CE-1 in accordance with Part 21 of the Federal Aviation Regulations. Requirements for any additional oil should be established in accordance with Advisory Circular AC23. and (4) Structural load factors of +2. Flight characteristics and performance at the increased weights have not been evaluated. All FAA required placards are included in Section 2 of the POH/AFM. Increased stall speeds and reduced climb performance should be expected for the increased weights. Type Certificate No. to -1. The airplane must be operated according to the appropriate AFM. Refer to FAA letter dated 5/1/98 FAR § 23. 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.. part number 172RMM02 (or later revision) for the Model 172S. Refer to ACE-07-10. may not be exceeded. FAA letter dated 11/29/07 Date of Application for Amended Type Certificate for the 172S was November 13. “Special Conditions: Cessna Aircraft Company.0 inches aft of datum.0 g. Refer to ACE-07-09.1401(d). FAA letter dated 10/12/07 14 CFR § 23. . Airplane serial numbers not listed were produced under Type Certificate only. 1998.1 inches forward of datum. 1997. 23-159-SC. and (3) Forward and aft center of gravity limits may not be exceeded.. The airplane must be operated according to the appropriate AFM. and full oil of 15.Model 172S (cont’d) Equivalent Safety Items (1) Induction System Icing Protection (2) Throttle Control (3) Mixture Control (4) Anti-Collision Light System (5) Aviation White Color Reqmt FAR § 23. PC-4 issued August 27.5 g.. Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the airplane for certification. END .. The airplane must be operated according to the appropriate POH/AFM. NOTE 3: Special Ferry Flight Authorization. Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual (POH/AFM): part number 172SPHUS-00 (or later approved revision) is applicable to the Model 172S. Placards may also be found in the Maintenance Manual. Placards and Markings. 172S8001 and On The certificated empty weight and corresponding center of gravity location must include unusable fuel of 18 pounds at 46.. Serial Numbers Eligible 172S8001 and on Special Conditions as follows: No. 1998 for the Model 172S.0 pounds at 13. Cessna Model 172S Airplane.