# TCDS 5A6: Textron Aviation Inc.

- Type: Type certificate data sheet
- Status: Current
- Holder: Textron Aviation Inc.
- Revision: 68
- Revised: July 29, 2015
- Product: Aircraft, Small Airplane
- Certification basis: CAR 3
- Registered aircraft: 2,605, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/54/4a/544a1ef62694cf2f56066cb307bac5141543e56bd02af0fe3013c17d6f1c6cea
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7FF347D37863833086257ED2006F6A9F.0001
- Page: https://openairdocs.org/tcds/5A6

## Models (11)

As the data sheet lists them.

- 180E
- 180J
- 180F
- 180H
- 180A
- 180
- 180B
- 180D
- 180K
- 180G
- 180C

## 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 
Rev. No. 68 54 64 58 64 64 59 64 59 59 67 64 60 
Page No. 14 15 16 17 18 19 20 21 22 23 24   
Rev. No. 65 54 63 63 67 67 67 67 67 63 63   
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
 5A6  
 Revision 68  
Textron Aviation Inc.  
180 180F  
180A 180G   
180B 180H   
180C 180J   
180D 180K   
180E   
 July 29, 2015  
 
TYPE CERTIFICATE DATA SHEET NO. 5A6 
 
This data sheet which is part of Type Certificate No. 5A6 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 180, 4 PCL-SM (Normal Category), approved December 23, 1952 
 
 Engine Continental O-470-A, O-470-J or O-470-K 
 
 *Fuel 80/87 minimum grade aviation gasoline 
 
WARNING:  Use of alcohol-based fuels can cause serious performance degradation and fuel system 
component damage, and is therefore prohibited on Cessna airplanes. 
 
 *Engine limits For all operations, O-470-A, 2600 rpm (225 hp) 
   O-470-J,  2550 rpm (225 hp) 
   O-470-K, 2600 rpm (230 hp) 
 
 Propeller and 1. Hartzell constant speed propeller 
   Propeller Limits   (a) Hub HC82XF-1 or HC82XF-6, blades 8833 
    Diameter:  not over 88 in., not under 86 in. 
    Pitch settings at 30 in. sta.: 
     Low 12°, high 24° or 28° 
   (b) Spinner, Hartzell HC82XF-1 or Cessna 0752006 
   (c) Governor, Woodward 4M12V, 210065 or 210340 or 210105 
  2. McCauley constant speed propeller 
   (a) Hub 2A36C, blades 90M-8 
    Diameter:  not over 82 in., not under 80 in. 
    Pitch settings at 36 in. sta.: 
     Low 10.5°, high 22° 
   (b) Spinner, Cessna 0752004 
   (c) Governor, Woodward 4M12-V, 210105, 210065, 210345 or  
    A210452.  Garwin 34-828-01 
    McCauley  C290D2/T-1 or C290D3/T1

5A6 2 Rev. 68 
I. Model 180  (cont’d) 
 
 Propeller and 3. Hartzell constant speed propeller (seaplane installation approved by 
   Propeller Limits (cont’d)  Cessna DOA) 
   (a) Hub HC82XF-1 or HC82XF-6, blades 8433 
    Diameter:  not over 84 in., not under 82-1/2 in. 
    Pitch settings at 30 in. sta.: 
     Low 12°, high 24° or 28° 
   (b) Spinner, Hartzell HC82XF-1 or Cessna 0752006 
   (c) Governor, Woodward 4M12-V, 210065, 210105 or 210340 
  4. McCauley constant speed propeller 
   (a) Hub 2A36C, blades 90M-2 
    Diameter:  not over 88 in., not under 86 in. 
    Pitch settings at 36 in. sta.: 
     Low 8°, high 22° 
   (b) Spinner, Cessna 0752004 
   (c) Governor, Woodward 210065, 210105, 210345 or 
    A210452.  Garwin 34-828-01.  McCauley C290D2/T-1 
    or C290D3/T-1. 
  5. Hartzell constant speed propeller 
   (a) Hub HCA2XF-1 blades 8433 or 8833 
    Diameter: 
    (For 8433 blades)  -  not over 84 in., not under 82 in. 
    (For 8833 blades)  -  not over or under 88 in. 
    Pitch settings at 30 in. sta.: 
     Low 12°, high 24° 
   (b) Spinner, Cessna 07502006 
   (c) Governor, Woodward 4M12-V, 210065, 210105 or 210340 
  6. McCauley constant speed propeller 
   (a) Hub 2A34C, blades 90A-8 
    Diameter:  not over 82 in., not under 80 in. 
    Pitch settings at 36 in. sta.: 
     Low 10.5°, high 22° 
   (b) Spinner, Cessna 0752004 
   (c) Governor, Woodward 210065, 210105, 210345 or A210452. 
    Garwin 34-828-01.  McCauley C290D2/T-1 or C290D3/T-1. 
  7. McCauley constant speed propeller 
   (a) Hub 2A34C, blades 90A-2 
    Diameter:  not over 88 in., not under 86 in. 
    Pitch settings at 36 in. sta.: 
     Low 10.5°, high 22° 
   (b) Spinner, Cessna 0752004 
   (c) Governor, Woodward 210065, 210105, 210345 or A210452. 
    Garwin 34-828-01.  McCauley C290D2/T1 or 290D3/T1. 
  8. McCauley constant speed propeller 
   (a) Hub 2A34C66, blades 90AT-8 
    Diameter:  not over 82 in., not under 80 in. 
    Pitch settings at 36 in. sta.: 
     Low 10.5°, high 22° 
   (b) Spinner, Cessna 0752004 
   (c) Governor, Woodward 210065, 210105, 210345 or A210452. 
    Garwin 34-828-01.  McCauley C290D2/T-1 or C290D3/T-1. 
  9. McCauley constant speed propeller 
   (a) Hub 2A34C66, blades 90AT-2 
    Diameter:  not over 88 in., not under 86 in. 
    Pitch settings at 36 in. sta.: 
     Low 8°, high 22° 
   (b) Spinner, Cessna 0752004 
   (c) Governor, Woodward 210065, 210105, 210345 or A210452. 
    Garwin 34-828-01.  McCauley C290D2/T-1 or C290D3/T-1.

Rev. 68 3 5A6 
I. Model 180  (cont’d) 
 
 Propeller and 10. Aircraft reworked per Cessna Service Kit SK180-45: 
   Propeller Limits (cont’d)  McCauley constant speed propeller (Threadless) (Landplane, Skiplane) 
   (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) Spinner, Cessna 0752004 
   (c) Governor, Woodward 4M12-V, 210065, 210105, 210345 or A210452. 
    Garwin 34-828-01. McCauley C290D2/T1 or C290D3/T1. 
  11. Aircraft reworked per Cessna Service Kit SK180-46: 
   McCauley constant speed propeller (Threadless) (Floatplane, Amphibian,  
   Landplane, Skiplane) 
   (a) Hub 2A34C203/90DCA-2 blades 
  Diameter: not over 88 in., not under 86.5 in. 
     Pitch settings at 30 in. sta.:  
   Low 10°, high 24.5° 
(b) Spinner, Cessna 0752004 
(c) Governor, Woodward 4M12-V, 210065, 210105, 210345 or     
     A210452. Garwin 34-828-01. McCauley C290D2/T1 or C290D3/T1. 
 
 *Airspeed Limits (TIAS)  Landplane & Floatplane Amphibian 
  Never exceed 184 mph (160 knots) 164 mph (143 knots) 
  Maneuvering 122 mph (106 knots) 129 mph (112 knots) 
  Max. structural cruising 160 mph (139 knots) 130 mph (113 knots) 
  Flaps extended 100 mph (  87 knots) 100 mph (  87 knots) 
 
 C.G. Range Landplane (+39.5)  to  (+45.8)  at  2550 lbs. 
   (+35.0)  to  (+45.8)  at  2050 lbs. or less 
  Floatplane with Edo 44-2425 (+39.3)  to  (+43.9)  at  2700 lbs. 
   (+35.0)  to  (+43.9)  at  2040 lbs. or less 
  Floatplane with Edo 249-2870 (+40.2)  to  (+43.9)  at  2820 lbs. 
   (+35.0)  to  (+43.9)  at  2125 lbs. or less 
  Amphibian with Edo 289-2700 (+38.3)  to  (+43.9)  at  2850 lbs. 
   (+36.0)  to  (+43.9)  at  2400 lbs. or less 
  Straight line variation between points given. 
 
 Empty weight C.G. Range None 
 
 *Maximum Weight Landplane 2550 lb. 
  Floatplane Edo 44-2425 2700 lb. 
   Edo 249-2870 2820 lb. 
  Amphibian 2850 lb. 
 
 Number of Seats 4  (2 at +36, 2 at +70) 
 
 Maximum Baggage 120 lb.  (+95) 
 
 Fuel Capacity 60 gal. total, 55 gal. usable (two 30 gal. tanks in wings at +48) 
  See Note 1 for weight of unusable fuel. 
 
 Oil Capacity 12 qt. (-15) includes 6 qt. usable 
  See Note 1 for data on undrainable oil. 
 
 Control Surface Movements Wing flaps Takeoff  0°  & 20° 
   Landing  30°  & 40° 
  Ailerons Up 20° Down 15° 
  Stabilizer Up   1° 30' Down   8° 30' 
  Elevators (with stabilizer Up 25° Down 23° 
    full down) 
  Rudder Right 24° Left 24°

5A6 4 Rev. 68 
I. Model 180  (cont’d) 
 
 Serial Numbers Eligible 604, 614, 30000 through 32661.  Under delegation option provisions of Part 21 of  
  the Federal Aviation Regulations, Delegation Option Manufacturer No. CE-1 is 
  authorized to issue airworthiness certificates for airplanes S/N 30938 and up and 
  approve repairs and alterations of airplanes S/N 604, 614, 30000 through 32661. 
 
 
II. Model 180A, 4 PCL-SM  (Normal Category), approved December 17, 1956 
 Model 180B, 4 PCL-SM  (Normal Category), approved August 22, 1958 
 
 Engine Continental O-470-K 
 
 *Fuel 80/87 minimum grade aviation gasoline 
 
 *Engine Limits For all operations, 2600 rpm  (230 hp) 
 
 Propeller and  1. Hartzell constant speed propeller 
   Propeller Limits   (a) Hub HC82XF-1 or HC82XF-6, blades 8833 
    Diameter:  not over or under 88 in. 
    Pitch settings at 30 in. sta.: 
     Low 12°, high 24° or 28° 
   (b) Spinner, Hartzell HC82XF-1 or Cessna 0752006 
   (c) Governor, Woodward 4M12-V, 210065, 210105 or 210340 
  2. McCauley constant speed propeller 
   (a) McCauley hub 2A36C, blades 90M-8 
    Diameter:  not over 82 in., not under 80 in. 
    Pitch settings at 36 in. sta.: 
     Low 10.5°, high 22° 
   (b) Spinner, Cessna 0752004 
   (c) Governor, Woodward 4M12-V, 210065, 210105, 210345 or 
    A210452.  Garwin 34-828-01. 
    McCauley C290D2/T-1 or C290D3/T-1 
  3. Hartzell constant speed propeller (seaplane installation approved by DOA) 
   (a) Hub HC82XF-1 or HC82XF-6, blades 8433 
    Diameter:  not over 84 in., not under 82-1/2 in. 
    Pitch settings at 30 in. sta.: 
     Low 12°, high 24° or 28° 
   (b) Spinner, Hartzell HC82XF-1 or Cessna 0752006 
   (c) Governor, Woodward 4M12-V, 210065, 210105 or 210340 
  4. McCauley constant speed propeller 
   (a) McCauley hub 2A36C, blades 90M-2 
    Diameter:  not over 88 in., not under 86 in. 
    Pitch settings at 36 in. sta.: 
     Low 8°, high 22° 
   (b) Spinner, Cessna 0752004 
   (c) Governor, Woodward 210065, 210105, 210345 or  
    A210452.  Garwin 34-828-01. 
    McCauley C290D2/T-1 or C290D3/T-1 
  5. Hartzell constant speed propeller 
   (a) Hub HCA2XF-1, blades 8433 or 8833 
    Diameter: 
     (For 8833 blades)  not over or under 88 in. 
     (For 8433 blades)  not over 84 in., not under 82 in. 
    Pitch settings at 30 in. sta.: 
     Low 12°, high 24° 
   (b) Spinner, Cessna 0752006 
   (c) Governor, Woodward 4M12-V, 210065, 210105 or 210340

Rev. 68 5 5A6 
II. Models 180A, 180B  (cont’d) 
 
 Propeller and 6. McCauley constant speed propeller 
   Propeller Limits (cont’d)  (a) McCauley hub 2A34C, blades 90A-8 
    Diameter:  not over 82 in., not under 80 in. 
    Pitch settings at 36 in. sta.: 
     Low 10.5°, high 22° 
   (b) Spinner, Cessna 0752004 
   (c) Governor, Woodward 210065, 210105, 210345 or 
    A210452.  Garwin 34-828-01. 
    McCauley C290D2/T-1 or C290D3/T-1 
  7. McCauley constant speed propeller 
   (a) McCauley hub 2A34C, blades 90A-2 
    Diameter:  not over 88 in., not under 86 in. 
    Pitch settings at 36 in. sta.: 
     Low 10.5°, high 22° 
   (b) Spinner, Cessna 0752004 
   (c) Governor, Woodward 210065, 210105, 210345 or 
    A210452.  Garwin 34-828-01. 
    McCauley C290D2/T1 or C290D3/T-1 
  8. McCauley constant speed propeller 
   (a) Hub 2A34C66, blades 90AT-8 
    Diameter:  not over 82 in., not under 80 in. 
    Pitch settings at 36 in. sta. 
     Low 10.5°, high 22° 
   (b) Spinner, Cessna 0752004 
   (c) Governor, Woodward 210065, 210105, 210345 or 
    A210452.  Garwin 34-828-01. 
    McCauley C290D2/T-1 or C290D3/T-1 
  9. McCauley constant speed propeller 
   (a) Hub 2A34C66, blades 90AT-2 
    Diameter:  not over 88 in., not under 86 in. 
    Pitch settings at 36 in. sta.: 
     Low 8°, high 22° 
   (b) Spinner, Cessna 0752004 
   (c) Governor, Woodward 210065, 210105, 210345 or A210452. 
    Garwin 34-828-01. 
    McCauley C290D2/T-1 or C290D3/T-1. 
  10. Aircraft reworked per Cessna Service Kit SK180-45: 
   McCauley constant speed propeller (Threadless) (Landplane, Skiplane) 
(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) Spinner, Cessna 0752004 
(c) Governor, Woodward 4M12-V, 210065, 210105, 210345 or A210452. Garwin 
     34-828-01. McCauley C290D2/T1 or C290D3/T1. 
  11. Aircraft reworked per Cessna Service Kit SK180-46: 
   McCauley constant speed propeller (Threadless) (Floatplane, Amphibian, 
   Landplane, Skiplane) 
   (a) Hub 2A34C203/90DCA-2 blades 
     Diameter: not over 88 in., not under 86.5 in. 
     Pitch settings at 30 in. sta.:  
      Low 10°, high 24.5° 
   (b)  Spinner, Cessna 0752004 
   (c) Governor, Woodward 4M12-V, 210065, 210105, 210345 or A210452.   
    Garwin 34-828-01. McCauley C290D2/T1 or C290D3/T1.

5A6 6 Rev. 68 
II. Models 180A, 180B  (cont’d) 
 
 *Airspeed Limits (TIAS)  Landplane & Floatplane Amphibian 
  Never exceed 184 mph (160 knots) 164 mph (143 knots) 
  Maneuvering 122 mph (106 knots) 129 mph (112 knots) 
  Max. structural cruising 160 mph (139 knots) 130 mph (113 knots) 
  Flaps extended 100 mph (  87 knots) 100 mph (  87 knots) 
 
 C.G. Range Landplane (+40.0)  to  (+45.8)  at  2650 lbs. 
   (+34.5)  to  (+45.8)  at  2100 lbs. or less 
  Floatplane with Edo 44-2425 (+39.3)  to  (+43.9)  at  2700 lbs. 
   (+35.0)  to  (+43.9)  at  2050 lbs. or less 
  Floatplane with Edo 249-2870 (+40.2)  to  (+43.9)  at  2820 lbs. 
   (+35.0)  to  (+43.9)  at  2125 lbs. or less 
  Amphibian with Edo 289-2700 (+38.3)  to  (+43.9)  at  2850 lbs. 
   (+36.0)  to  (+43.9)  at  2400 lbs. or less 
  Straight line variation between points given. 
 
 Empty Weight C.G. Range None 
 
 *Maximum Weight Landplane 2650 lb. 
  Floatplane Edo 44-2425 2700 lb. 
   Edo 249-2870 2820 lb. 
  Amphibian 2850 lb. 
 
 Number of Seats 4  (2 at +36, 2 at +70) 
 
 Maximum Baggage 120 lb.  (+95) 
 
 Fuel Capacity 60 gal. total, 55 gal. usable (two 32-1/2 gal. tanks in wings at +48) 
  See Note 1 for weight of unusable fuel. 
 
 Oil Capacity 12 qt. (-15) includes 6 qt. usable 
  See Note 1 for data on undrainable oil. 
 
 Control Surface Movements Wing flaps Takeoff  0°  & 20° 
   Landing  30°  & 40° 
  Ailerons Up 20° Down 15° 
  Stabilizer Up   1° 30' Down   8° 30' 
  Elevators (with stabilizer Up 25° Down 23° 
    full down) 
  Rudder Right 24° Left 24° 
 
 Serial Numbers Eligible Model 180A: 32662 through 32999, 50001 through 50355 
  Model 180B: 50356 through 50661 
 
 
III. Model 180C, 4 PCL-SM (Normal Category), approved July 8, 1959 
 Model 180D, 4 PCL-SM (Normal Category), approved June 14, 1960 
 Model 180E, 4 PCL-SM (Normal Category), approved September 21, 1961 
 Model 180F, 4 PCL-SM (Normal Category), approved June 25, 1962 
 
 Engine Continental O-470-L or O-470-R 
 
 *Fuel 80/87 minimum grade aviation gasoline 
 
 *Engine Limits For all operations, 2600 rpm  (230 hp)

Rev. 68 7 5A6 
III. Models 180C, 180D, 180E, 180F   (cont’d) 
 
 Propeller and  1. McCauley constant speed propeller 
   Propeller Limits   (a) Hub 2A36C, blades 90M-8 
    Diameter:  not over 82 in., not under 80 in. 
    Pitch settings at 36 in. sta.: 
     Low 10.5°, high 22° 
   (b) Spinner, Cessna 0752004 
   (c) Governor, Woodward 4M12-V, 210065, 210105, 210345 or 
    A210452.  Garwin 34-328-01. 
    McCauley C290D2/T-1 or D290D3/T-1 
  2. McCauley constant speed propeller 
   (a) Hub 2A36C, blades 90M-2 
    Diameter:  not over 88 in., not under 86 in. 
    Pitch settings at 36 in. sta.: 
     Low 8°, high 22° 
   (b) Spinner, Cessna 0752004 
   (c) Governor, Woodward 210065, 210105, 210345 or A210452. 
    Garwin 34-828-01. 
    McCauley C290D2/T-1 or C290D3/T-1 
  3. McCauley constant speed propeller 
   (a) Hub 2A34C, blades 90A-8 
    Diameter:  not over 82 in., not under 80 in. 
    Pitch settings at 36 in. sta.: 
     Low 10.5°, high 22° 
   (b) Spinner, Cessna 0752004 
   (c) Governor, Woodward 210065, 210105, 210345 or A210452. 
    Garwin 34-828-01. 
    McCauley C290D2/T-1 or C290D3/T-1 
  4. McCauley constant speed propeller 
   (a) Hub 2A34C, blades 90A-2 
    Diameter:  not over 88 in., not under 86 in. 
    Pitch settings at 36 in. sta.: 
     Low 10.5°, high 22° 
   (b) Spinner, Cessna 0752004 
   (c) Governor, Woodward 210065, 210105, 210345 or A210452. 
    Garwin 34-828-01. 
    McCauley C290D2/T-1 or C290D3/T-1 
  5. McCauley constant speed propeller 
   (a) Hub 2A34C66, blades 90AT-8 
    Diameter:  not over 82 in., not under 80 in. 
    Pitch settings at 36 in. sta.: 
     Low 10.5°, high 22° 
   (b) Spinner, Cessna 0752004 
   (c) Governor, Woodward 210065, 210105, 210345 or A210452. 
    Garwin 34-828-01. 
    McCauley C290D2/T-1 or C290D3/T-1 
  6. McCauley constant speed propeller 
   (a) Hub 2A34C66, blades 90AT-2 
    Diameter:  not over 88 in., not under 86 in. 
    Pitch settings at 36 in. sta.: 
     Low 8°, high 22° 
   (b) Spinner, Cessna 0752004 
   (c) Governor, Woodward 210065, 210105, 210345 or A210452. 
    Garwin 34-828-01. 
    McCauley C290D2/T-1 or C290D3/T-1

5A6 8 Rev. 68 
III. Models 180C, 180D, 180E, 180F   (cont’d) 
 
 Propeller and 7. Hartzell constant speed propeller (not eligible on the O-470-R engine installation) 
   Propeller Limits (cont’d)  (a) Hub HC82XF-1 or -6, blades 8433 or 8833  
    Diameter:   
     (For blade 8433) not over 84 in., not under 82.5 in. 
     (For blade 8833) not over or under 88 in. 
    Pitch setting at 30 in. sta.: 
     Low 12°, high 24° or 28° 
   (b) Spinner, Hartzell HC82XF-1 or Cessna 0752006 
   (c) Governor, Woodward 4M12-V, 210065, 210105 or 210340 
  8. Hartzell constant speed propeller (not eligible on the O-470-R engine installation) 
   (a) Hub HCA2XF-1 or BHCA2XF-1, blades 8433 or 8833 
    Diameter: 
     (For blade 8433) not over 84 in., not under 82 in. 
     (For blade 8833) not over or under 88 in. 
    Pitch setting at 30 in. sta.: 
     Low 12°, high 24° 
   (b) Spinner, Cessna 0752006 
  (c) Governor, Woodward 4M12-V, 210065, 210105 or 210340 
  9. Aircraft reworked per Cessna Service Kit SK180-45: 
   McCauley constant speed propeller (Threadless) (Landplane, Skiplane) 
  (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) Spinner, Cessna 0752004 
   (c) Governor, Woodward 4M12-V, 210065, 210105, 210345 or A210452. Garwin 
    34-828-01. McCauley C290D2/T1 or C290D3/T1. 
 10. Aircraft reworked per Cessna Service Kit SK180-46: 
  McCauley constant speed propeller (Threadless) (Floatplane, Amphibian,        
  Landplane, Skiplane) 
  (a) Hub 2A34C203/90DCA-2 blades 
    Diameter: not over 88 in., not under 86.5 in. 
    Pitch settings at 30 in. sta.:  
     Low 10°, high 24.5° 
  (b) Spinner, Cessna 0752004 
   (c) Governor, Woodward 4M12-V, 210065, 210105, 210345 or A210452. Garwin  
    34-828-01. McCauley C290D2/T1 or C290D3/T1. 
 
 *Airspeed Limits (TIAS)  Landplane & Floatplane Amphibian 
  Never exceed 184 mph (160 knots) 164 mph (143 knots) 
  Maneuvering 122 mph (106 knots) 129 mph (112 knots) 
  Max. structural cruising 160 mph (139 knots) 130 mph (113 knots) 
  Flaps extended 100 mph (  87 knots) 100 mph (  87 knots) 
 
 C.G. Range Landplane (+40.0)  to  (+45.8)  at  2650 lbs. 
   (+34.5)  to  (+45.8)  at  2100 lbs. or less 
  Floatplane with Edo 44-2425 (+39.3)  to  (+43.9)  at  2700 lbs. 
   (+35.0)  to  (+43.9)  at  2050 lbs. or less 
  Floatplane with Edo 249-2870 (+40.2)  to  (+43.9)  at  2820 lbs. 
   (+35.0)  to  (+43.9)  at  2125 lbs. or less 
  Amphibian with Edo 289-2700 (+38.3)  to  (+43.9)  at  2850 lbs. 
   (+36.0)  to  (+43.9)  at  2400 lbs. or less 
  Straight line variation between points given. 
 
 Empty Weight C.G. Range None

Rev. 68 9 5A6 
III. Models 180C, 180D, 180E, 180F   (cont’d) 
 
 *Maximum Weight Landplane 2650 lb. 
  Floatplane Edo 44-2425 2700 lb. 
   Edo 249-2870 2820 lb. 
  Amphibian 2850 lb. 
 
 Number of Seats 4  (2 at +36, 2 at +70) 
 
 Maximum Baggage 120 lb.  (+95) 
 
 Fuel Capacity 65 gal. total, 55 gal. usable 180C, 180D; 60 gal. usable 180E, 180F 
  (two 32-1/2 gal. tanks in wings at +48) 
  See Note 1 for weight of unusable fuel. 
 
 Oil Capacity 12 qt. (-15) includes 6 qt. usable 
  See Note 1 for data on undrainable oil. 
 
 Control Surface Movements Wing flaps Takeoff  0°  & 20° 
   Landing  30°  & 40° 
  Ailerons Up 20° Down 15° 
  Stabilizer Up   1° Down   8° 45' 
  Elevators (with stabilizer Up 25° Down 23° 
    full down) 
  Rudder Right 24° Left 24° 
 
 Serial Numbers Eligible Model 180C: 624, 50662 through 50911 
  Model 180D: 18050912 through 18051063 
  Model 180E: 18051064 through 18051183 
  Model 180F: 18051184 through 18051312 
 
 
IV. Model 180G, 6 PCL-SM  (Normal Category), approved July 19, 1963 
 Model 180H, Skywagon, 6 PCL-SM (Normal Category), approved June 17, 1964 
 
 Engine Continental O-470-L or O-470-R 
 
 *Fuel 80/87 minimum grade aviation gasoline 
 
 *Engine Limits For all operations, 2600 rpm  (230 hp) 
 
 Propeller and 1. McCauley constant speed propeller 
   Propeller Limits  (a) Hub 2A36C, blades 90M-8 
    Diameter:  not over 82 in., not under 80 in. 
    Pitch settings at 36 in. sta.: 
     Low 10.5°, high 22° 
   (b) Spinner, Cessna 0752004 (through S/N 18051774) 
    Spinner, Cessna 0752042-1 and Fillet 0752044-1  (S/N 18051775 and on) 
   (c) Governor, Woodward 4M12-V, 210065, 210105, 210345 or 
    A210452.  Garwin 34-328-01. 
    McCauley C290D2/T-1 or D290D3/T-1 
  2. McCauley constant speed propeller 
   (a) Hub 2A36C, blades 90M-2 
    Diameter:  not over 88 in., not under 86 in. 
    Pitch settings at 36 in. sta.: 
     Low 8°, high 22° 
   (b) Spinner, Cessna 0752004  (through S/N 18051774) 
    Spinner, Cessna 0752042-1 and Fillet 0752044-1 (S/N 18051775 and on) 
   (c) Governor, Woodward 210065, 210105, 210345 or A210452. 
    Garwin 34-828-01. 
    McCauley C290D2/T-1 or C290D3/T-1

5A6 10 Rev. 68 
IV. Models 180G, 180H    (cont’d) 
 
 Propeller and 3. McCauley constant speed propeller 
   Propeller Limits (cont’d)  (a) Hub 2A34C, blades 90A-8 
    Diameter:  not over 82 in., not under 80 in. 
    Pitch settings at 36 in. sta.: 
     Low 10.5°, high 22° 
   (b) Spinner, Cessna 0752004 (through S/N 18051774) 
    Spinner, Cessna 0752042-1 and Fillet 0752044-1 (S/N 18051775 and on) 
   (c) Governor, Woodward 210065, 210105, 210345 or A210452. 
    Garwin 34-828-01. 
    McCauley C290D2/T-1 or C290D3/T-1 
  4. McCauley constant speed propeller 
   (a) Hub 2A34C, blades 90A-2 
    Diameter:  not over 88 in., not under 86 in. 
    Pitch settings at 36 in. sta.: 
     Low 10.5°, high 22° 
   (b) Spinner, Cessna 0752004 (through S/N 18051774) 
    Spinner, Cessna 0752042-1 and Fillet 0752044-1 (S/N 18051775 and on) 
   (c) Governor, Woodward 210065, 210105, 210345 or A210452.  Garwin 34-828-01. 
    McCauley C290D2/T-1 or C290D3/T-1 
  5. McCauley constant speed propeller 
   (a) Hub 2A34C66, blades 90AT-8 
    Diameter:  not over 82 in., not under 80 in. 
    Pitch settings at 36 in. sta.: 
     Low 10.5°, high 22° 
   (b) Spinner, Cessna 0752004 (through S/N 18051774) 
    Spinner, Cessna 0752042-1 and Fillet 0752044-1 (S/N 18051775 and on) 
   (c) Governor, Woodward 210065, 210105, 210345 or A210452. 
    Garwin 34-828-01. 
    McCauley C290D2/T-1 or C290D3/T-1 
  6. McCauley constant speed propeller 
   (a) Hub 2A34C66, blades 90AT-2 
    Diameter:  not over 88 in., not under 86 in. 
    Pitch settings at 36 in. sta.: 
     Low 8°, high 22° 
   (b) Spinner, Cessna 0752004 (through S/N 18051774) 
    Spinner, Cessna 0752042-1 and Fillet 0752044-1 (S/N 18051775 and on) 
   (c) Governor, Woodward 210065, 210105, 210345 or A210452. 
    Garwin 34-828-01. 
    McCauley C290D2/T-1 or C290D3/T-1 
  7. McCauley constant speed propeller (O-470-R engine only) 
   (a) Hub 2A34C201, blade 90DA-8 (Cessna P/N C161009-0101) 
    Diameter:  not over 82 in., not under 80 in. 
    Pitch settings at 30 in. sta.: 
     Low 13.0°, high 24.5° 
   (b) Spinner, Cessna 0752042-5 and Fillet 0752044-3 
   (c) Governor, Woodward 210345 or A210452.  Garwin 34-828-01, 
    McCauley C290D2/T-1 or C290D3/T-1 
  8. McCauley constant speed propeller (O-470-R engine only) 
   (a) Hub 2A34C201, blade 90DA-2 (Cessna P/N C161009-0102) 
    Diameter:  not over 88 in., not under 86.5 in. 
    Pitch setting at 30 in. sta.: 
     Low 10.5°, high 24.5° 
   (b) Spinner, Cessna 0752042-5 and Fillet 0752044-3 
   (c) Governor, Woodward 210345 or A210452, Garwin 34-828-01, 
    McCauley C290D2/T-1 or C290D3/T1.

Rev. 68 11 5A6 
IV. Models 180G, 180H    (cont’d) 
 
 Propeller and 9. McCauley constant speed propeller (O-470-R engines only) 
   Propeller Limits (cont’d)  (a) Hub 2A34C203, blade 90DCA-8 (Cessna P/N C161009-0104) 
    Diameter:  not over 82 in., not under 80.5 in. 
    Pitch settings at 30 in. sta.: 
     Low 12.5°, high 25.0° 
   (b) Spinner, Cessna 0752042-5 and fillet 0752044-3 
   (c) Governor, Woodward 210345 or A210452, Garwin 34-828-01, 
    McCauley C290D2/T-1 or C290D3/T-1. 
  10. McCauley constant speed propeller (O-470-R engines only) 
   (a) Hub 2A34C203, blade 90DCA-2 (Cessna P/N C161009-0105) 
    Diameter:  not over 88 in., not under 86.5 in. 
    Pitch settings at 30 in. sta.: 
     Low 10.0°, high 24.5° 
   (b) Spinner, Cessna 0752042-5 and fillet 0752044-3 
   (c) Governor, Woodward 210345 or A210452, Garwin 34-828-01, 
    McCauley C290D2/T-1 or C290D3/T-1. 
  11. Aircraft reworked per Cessna Service Kit SK180-45: 
   McCauley constant speed propeller (Threadless) (Landplane, Skiplane) 
(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) Spinner, Cessna 0752004 (through S/N 18051774) 
     Spinner, Cessna 0752042-5 and fillet 0752044-3 (S/N 18051775 and on) 
(c) Governor, Woodward 4M12-V, 210065, 210105, 210345 or A210452.  
     Garwin 34-828-01. McCauley C290D2/T1 or C290D3/T1. 
12. Aircraft reworked per Cessna Service Kit SK180-46: 
   McCauley constant speed propeller (Threadless) (Floatplane, Amphibian,  
   Landplane, Skiplane) 
   (a) Hub 2A34C203/90DCA-2 blades 
     Diameter: not over 88 in., not under 86.5 in. 
     Pitch settings at 30 in. sta.:  
      Low 10°, high 24.5° 
   (b) Spinner, Cessna 0752004 (through S/N 18051774) 
     Spinner, Cessna 0752042-5 and fillet 0752044-3 (S/N 18051775 and on) 
   (c) Governor, Woodward 4M12-V, 210065, 210105, 210345 or 
    A210452. Garwin 34-828-01. McCauley C290D2/T1 or C290D3/T1. 
 
 *Airspeed Limits (TIAS)  Landplane & 249A-2870 597-2790 Amphibian & 
              Floatplane 628-2960 Floatplane 
  Never exceed 192 mph (167 knots) 164 mph (143 knots) 
  Maneuvering 128 mph (111 knots) 130 mph (113 knots) 
  Max. structural cruising 160 mph (139 knots) 130 mph (113 knots) 
  Flaps extended 110 mph (  96 knots) 110 mph (  96 knots) 
 
 C.G. Range Landplane (+38.5)  to  (+47.0)  at  2800 lbs. 
   (+33.5)  to  (+47.0)  at  2100 lbs. or less 
  Floatplane with Edo 249A-2870 (+40.2)  to  (+43.9)  at  2820 lbs. 
   (+35.0)  to  (+43.9)  at  2125 lbs. or less 
  Floatplane with Edo 628-2960 (+41.2)  to  (+43.9)  at  2950 lbs. 
   (+35.0)  to  (+43.9)  at  2125 lbs. or less 
  Amphibian with Edo 597-2790 (+38.8)  to  (+43.9)  at  2950 lbs. 
   (+36.0)  to  (+43.9)  at  2400 lbs. or less 
  Straight line variation between points given. 
 
 Empty Weight C.G. Range None

5A6 12 Rev. 68 
IV. Models 180G, 180H  (cont’d) 
 
 *Maximum Weight Landplane 2800 lb. 
  Floatplane Edo 249A-2870 2820 lb. 
   Edo 628-2960 2950 lb. 
  Amphibian 2950 lb. 
 
 Number of Seats 6  (2 at +36 to +50, 2 at +65 or +73, 2 at +97) 
 
 Maximum Baggage Refer to weight and balance data. 
 
 Fuel Capacity 65 gal. total, 60 gal. usable   (two 32.5 gal. tanks in wings at +48) 
  See Note 1 for weight of unusable fuel. 
 
 Oil Capacity 12 qt. (-15) includes 6 qt. usable 
  See Note 1 for data on undrainable oil. 
 
 Control Surface Movements Wing flaps   Down  38° +2°, -1° 
  Ailerons Up 20° ±2° Down 14° ±2° 
  Stabilizer Up   0° 45' ±15' Down   8° 45' ±15' 
  Elevators (with stabilizer Up 25° ±1° Down 23° ±1° 
    full down) 
  Rudder (parallel to W.L. or 
    perpendicular to hinge) Right 24° ±1° Left 24° ±1° 
 
 Serial Numbers Eligible Model 180G: 18051313 through 18051445 
  Model 180H: 645, 18051446 through 18052284 
 
 
V. Model 180J, Skywagon, 6 PCL-SM (Normal Category), approved October 13, 1972 
 
 Engine Continental O-470-R, S/N 18052285 through 18052500 
  Continental O-470-S, S/N 18052501 and up (see Note 5) 
 
 *Fuel 80/87 minimum grade aviation gasoline 
 
 *Engine limits For all operations, 2600 rpm  (230 hp) 
 
 Propeller and  1. McCauley constant speed propeller  (landplane-skiplane) 
   Propeller Limits   (a) Hub 2A34C66, Blades 90AT-8 
    Diameter:  not over 82 in., not under 80 in. 
    Pitch settings at 36 in. sta.: 
     Low 10.5°, high 22° 
   (b) Spinner, Cessna 0752042-1 and Fillet 0752044-1 
   (c) Governor, Woodward 210065, 210105, 210345 or A210452. 
    Edo-Aire 34-828-01.  McCauley C290D2/T-1 or C290D3/T-1 
  2. McCauley constant speed propeller 
   (Floatplane, Amphibian, Landplane, Skiplane) 
   (a) Hub 2A34C66, Blades 90AT-2 
    Diameter:  not over 8° in., not under 86 in. 
    Pitch settings at 36 in. sta.: 
     Low 8°, high 22° 
   (b) Spinner, Cessna 0752042-1 and Fillet 0752044-1 
   (c) Governor, Woodward 210065, 210105, 210345 or A210452. 
    Edo-Aire 34-828-01.  McCauley C290D2/T-1 or C290D3/T-1

Rev. 68 13 5A6 
V. Model 180J  (cont’d) 
 
 Propeller and 3. McCauley constant speed propeller (threadless) (Landplane, Skiplane) 
   Propeller Limits (cont’d)  (a) Hub 2A34C201, blade 90DA-8  (C161009-0101) 
    Diameter:  not over 82 in., not under 80 in. 
    Pitch settings at 30 in. sta.: 
     Low 13.0°, high 24.5° 
   (b) Spinner, Cessna 0752042-5 and Fillet 0752044-3 
   (c) Governor, Woodward 210345 or A210452.  Edo-Aire 34-828-01. 
    McCauley C290D2/T-1 or C290D3/T-1 
  4. McCauley constant speed propeller (threadless) 
   (Floatplane, Amphibian, Landplane, Skiplane) 
   (a) Hub 2A34C201, Blade 90DA-2 (C161009-0102) 
    Diameter:  not over 88 in., not under 86.5 in. 
    Pitch settings at 30 in. sta.: 
     Low 10.5°, high 24.5° 
   (b) Spinner, Cessna 0752042-5 and Fillet 0752044-3 
   (c) Governor, Woodward 210345 or A210452.  Edo-Aire 34-828-01. 
    McCauley C290D2/T-1 or C290D3/T-1 
  5. McCauley constant speed propeller (threadless) (Landplane, Skiplane) 
   (a) Hub 2A34C203, Blade 90DCA-8 
    Diameter:  not over 82 in., not under 80.5 in. 
    Pitch settings at 30 in. sta.: 
     Low 12.5°, high 25.0° 
   (b) Spinner, Cessna 0752042-5 and Fillet 0752044-3 
   (c) Governor, Woodward 210345 or A210452.  Edo-Aire 34-828-01. 
    McCauley C290D2/T-1 or C290D3/T-1 
  6. McCauley constant speed propeller (threadless) 
   (Floatplane, Amphibian, Landplane, Skiplane) 
   (a) Hub 2A34C203, Blade 90DCA-2 
    Diameter:  not over 88 in., not under 86.5 in. 
    Pitch settings at 30 in. sta.: 
     Low 10.0°, high 24.5° 
   (b) Spinner, Cessna 0752042-5 and Fillet 0752044-3 
   (c) Governor, Woodward 210345 or A210452.  Edo-Aire 34-828-01. 
    McCauley C290D2/T-1 or C290D3/T-1 
 
 *Airspeed Limits (CAS) S/N 18052285 through 18052620 
  Landplane, 628-2960 Floatplane and 597-2790 Amphibian 
  Never exceed   192 mph  (167 knots) 
  Maneuvering   123 mph  (107 knots) 
  Maximum structural cruising 160 mph  (139 knots) 
  Flaps extended  110 mph  (  96 knots 
 (IAS)  S/N 18052621 and up 
 (See Note 6 for use of IAS.) Landplane, 628-2960 Floatplane and 597-2790 Amphibian 
   Never exceed   169 knots  (194 mph) 
   Maneuvering (landplane) 108 knots  (124 mph) 
    (Floatplane with Edo 628-2960) 106 knots  (122 mph) 
    (Amphibian with Edo 597-2790) 106 knots  (122 mph) 
   Maximum structural cruising 139 knots  (160 mph) 
   Flaps extended 10° 120 knots  (138 mph) 
       20°  -  40°   90 knots  (104 mph) 
 
 C.G. Range  Landplane  (+38.5)  to  (+47.0)  at  2800 lbs. 
       (+33.5)  to  (+47.0)  at  2100 lbs. or less 
   628-2960 Floatplane (+38.8)  to  (+43.9)  at  2950 lbs. 
   and 597-2790 Amphibian (+36.0)  to  (+43.9)  at  2400 lbs. or less 
    Straight line variation between points given. 
 
 Empty Weight C.G. Range  None

5A6 14 Rev. 68 
V. Model 180J  (cont’d) 
 
 *Maximum Weight  Landplane  2800 lbs. 
    Seaplane   2950 lbs. 
    Amphibian  2950 lbs. 
    
 Number of Seats (Max.) 6  (2 at +36 to +50, 2 at +65 or +73, 2 at +97) 
 
 Maximum Baggage Refer to weight and balance data. 
 
 Fuel Capacity 65 gal. total, 60 gal. usable (two 32.5 gal. tanks in wings at +48) 
  Through S/N 18052363. 
  61 gal. total, 56 gal. usable (two 29 gal. tanks in wings at +48) 
  S/N 18052364 and on. 
  See Note 1 for unusable fuel. 
 
 Oil Capacity 12 qt. (-15) includes 6 qt. usable 
  See Note 1 for data on undrainable oil. 
 
 Control Surface Movements Wing flaps   Down  40° +0°, -2° 
  Ailerons Up 20° ±2° Down 14° ±2° 
  Stabilizer Up   0° 45' ±15' Down   8° 45' ±15' 
  Elevators (with stabilizer Up 25° ±1° Down 23° ±1° 
    full down) 
  Rudder (parallel to W.L. or 
    perpendicular to hinge) Right 24° ±1° Left 24° ±1° 
  
 Serial Numbers Eligible Model 180J:  18052285 through 18052770, except 18052490 
 
 
VI. Model 180K, Skywagon, 6 PCL-SM (Normal Category), approved August 19, 1976 
 
 Engine Continental O-470-U 
 
 *Fuel 100/130 minimum grade aviation gasoline (S/N 18052771 through 18052905) 
  100LL/100 minimum grade aviation gasoline (S/N 18052906 and on) 
 
 *Engine Limits For all operations, 2400 rpm  (230 hp) 
 
 Propeller and  1. McCauley constant speed propeller (threadless) (landplane, skiplane) 
   Propeller Limits   (a) Hub C2A34C204, blade 90DCB-8 
    Diameter:  not over 82 in., not under 80.5 in. 
    Pitch settings at 30 in. sta.: 
     Low 15.0°, high 29.4° 
   (b) Spinner, Cessna 0752042-5 and Fillet 0752044-3 
   (c) Governor, McCauley C290D3/T-14 or C290D3B/T-14 
  2. McCauley constant speed propeller (threadless) (Floatplane, Amphibian, 
   Landplane, Skiplane) 
   (a) Hub C2A34C204, blade 90DCB-0 
    Diameter:  not over 90 in., not under 88.5 in. 
    Pitch settings at 30 in. sta.: 
     Low 12.9°, high 26.0°  
   (b) Spinner, Cessna 0752042-5 and Fillet 0752044-3 
   (c) Governor, McCauley C290D3/T-14 or C290D3B/T-14

Rev. 68 15 5A6 
VI. Model 180K  (cont’d) 
 
 *Airspeed Limits (IAS) Effective S/N 18052771 through 18053115 
 (See Note 6 for use of IAS) Landplane, 628-2960 Floatplane and 597-2790 Amphibian 
  Never exceed   169 knots  (194 mph) 
  Maneuvering (Landplane) 109 knots  (125 mph) 
   (Floatplane with Edo 628-2960) 109 knots  (125 mph) 
   (Amphibian with Edo 597-2790) 109 knots  (125 mph) 
  Maximum structural cruising 139 knots  (160 mph) 
  Flaps extended 10° 120 knots  (138 mph) 
      20° - 40°   90 knots  (104 mph) 
  S/N 18053116 and on 
   Landplane, 628-2960 Floatplane and 597-2790 Amphibian 
   Never exceed   169 knots  (194 mph) 
   Maneuvering (landplane) 109 knots  (125 mph) 
    (Floatplane with Edo 628-2960) 109 knots  (125 mph) 
    (Amphibian with Edo 597-2790) 109 knots  (125 mph) 
   Maximum structural cruising 139 knots  (160 mph) 
   Flaps extended 10° 120 knots  (138 mph) 
       20° 110 knots  (127 mph) 
       30° - 40°   90 knots  (104 mph) 
 
 C.G. Range  Landplane  (+38.5)  to  (+47.0)  at  2800 lbs. 
       (+33.5)  to  (+47.0)  at  2100 lbs. or less 
   628-2960 Floatplane (+38.8)  to  (+43.9)  at  2950 lbs. 
   and 597-2790 Amphibian (+36.0)  to  (+43.9)  at  2400 lbs. or less 
    Straight line variation between points given. 
 
 Empty Weight C.G. Range  None 
 
 *Maximum Weight  Landplane  2800 lbs. 
    Seaplane   2950 lbs. 
    Amphibian  2950 lbs. 
    
 Number of Seats (max.) 6  (2 at +36 to +50, 2 at +65 or +73, 2 at +97) 
 
 Maximum Baggage Refer to weight and balance data. 
 
 Fuel Capacity 61 gal. total, 56 gal. usable (two 30.5 gal. tanks in wings at +48) 
  Through S/N 18053000. 
  88 gal., (84 gal. usable, two 44.0 gal. tanks in wings at +46.5) 
  S/N 18053001 and on. 
  See Note 1 for unusable fuel. 
 
 Oil Capacity 12 qt. (-15) includes 6 qt. usable 
  See Note 1 for data on undrainable oil. 
 
 Control Surface Movements Wing flaps   Down  40° +0°, -2° 
  Ailerons Up 20° ±2° Down 14° ±2° 
  Stabilizer Up   0° 45' ±15' Down   8° 45' ±15' 
  Elevators (with stabilizer Up 25° ±1° Down 23° ±1° 
    full down) 
  Rudder (parallel to W.L. or 
    perpendicular to hinge) Right 24° ±1° Left 24° ±1° 
 
 Serial Numbers Eligible Model 180K:  18052771 through 18052905 (1977) 
      18052906 through 18053000 (1978) 
      18052490, 18053001 thru 18053115 (1979) 
      18053116 through 18053167 (1980) 
      18053168 through 18053203 (1981)

5A6 16 Rev. 68 
DATA PERTINENT TO ALL MODELS 
Datum Front face of firewall 
 
Leveling Means Upper door sill 
 
Certification Basis  
Models 180, 180A and 180B:  Part 3 of the Civil Air Regulations dated November 1, 1949, as amended by 3-1 through 3-8 
except Paragraphs 3.265and 3.668 of 3-7. 
 
Models 180C, 180D, 180E, 180F, 180G and 180H:  Part 3 of the Civil Air Regulations dated November 1, 1949, as amended by 
3-1 through 3-12 except Paragraph 3.265 of 3-7; Part 3 of the Civil Air Regulations dated May 15, 1956, paragraph 3.668 only, 
as amended by 3-3. 
 
Models 180J and 180K:  Part 3 of the Civil Air Regulations dated November 1, 1949, as amended by 3-1 through 3-12 except 
Paragraphs 3.265 and 3.668 and Subpart B; Subpart B of Part 3 of the Civil Air Regulations dated May 15, 1956, as amended by 
3-1 through 3-5.  In addition, effective S/N 18052490, 18053001 and on, FAR 23.1559 effective March 1, 1978.  FAR 36 dated 
December 1, 1969, plus Amendments 36-1 through 36-4 for S/N 18052771 and on. 
 
Application for Type Certificate dated December 11, 1951. 
Type Certificate No. 5A6 issued December 23, 1952.  Model 180A andsubsequent certificated under delegation option 
procedures. 
 
Equivalent Safety Items  18052621 and on 
Airspeed Indicator CAR 3.757 (See Note 6 on use of IAS) 
 
Operating Limitations CAR 3.778(a) 
 
Production Basis  
Production Certificate No. 4. Delegation Option Manufacturer No. CE-1authorized 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 regulations (see Certificat ion Basis) must be installed 
I the aircraft for certification.  This equipment must include a current Airplane Flight Manual effective S/N 18052490, 18053001 
and on.  In addition, the following item of equipment is required. 
 
  1. Stall Warning Indicator, Cessna Dwg. 0511062 through S/N 18051823. 
 
  2. Stall Warning Indicator, Cessna Dwg. 0700185 effective S/N 18051824 and on. 
 
The equipment portion of Aircraft Specification 5A6, Revision 34, or Cessna Publication TS2000-12 should be used for 
equipment references on all aircraft prior to the Model 180G.  Refer to the applicable  Equipment List for the Model 180G and 
subsequent models. 
 
NOTE 1. Current weight and balance report together with 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.  
The certificated empty weight and corresponding C.G. location must include unusable fuel of 30 lb. at (+46) 
on Models 180, 180E, 180F, 180G, 180H, 180J, and 180K through S/N 18053000, and 60 lbs. at (+48) on 
Models 180A, 180B, 180C and 180D, and undrainable oil of 0.0 lbs. at -15.0 through S/N 1805260; full oil 
of 22.0 lbs. at -15.0 S/N 18052621 and on. 
 
  The certificated empty weight and corresponding center of gravity locations must include unusable fuel of 24 
lb. at +48 (S/N 18052490, 18053001 and on). 
 
  Specific floatplane gross weights are those shown with float models under C.G. range.

Rev. 68 17 5A6 
DATA PERTINENT TO ALL MODELS (cont’d) 
 
NOTE 2. A. The following placards must be displayed in front of and in full view of the pilot: 
   (1) On Models 180, 180A and 180B 
    (a) "This airplane must be operated as a normal category airplane in compliance with the 
     Flight Manual." 
    (b) "No acrobatic maneuvers, including spins, approved." 
    (c) "Both tanks on for takeoff and landing." 
    (d) As floatplane:  "Retract water rudder during takeoff and landing." 
    (e) When wheel skis are installed, "Do not extend or retract while in motion on the ground." 
   (2) On Models 180C, 180D, 180E and 180F 
    (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 lbs." 
  (b) "Both tanks on for takeoff and landing." 
  (c) "Flaps  -  Pull to extend 
     Retracted   0° 
  Takeoff  1st notch 10° 
     2nd notch 20° 
  Landing  3rd notch 30° 
     4th notch 40° 
  (d) As seaplane or amphibian:  "Retract water rudder during takeoff and landing." 
 (3) On Models 180G and 180H 
  (a) Operational Limitations Placards 
   Serials 18051313 through 18052175 
   "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 lbs. 
  Maximum maneuvering speed, 128 mph  - CAS 
  Maximum altitude loss in stall recovery, 200 ft. 
  Avoid sideslips with flaps extended." 
  1. Serials 18052176 and on 
   "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  128 mph CAS (111 knots) 
  Gross weight  2800 lb. 
  Flight load factor Flaps up +3.8, -1.52 
     Flaps down +3.5 
 
  Avoid sideslips with flaps extended.  No acrobatic maneuvers, including spins, 
  approved.  Known icing conditions to be avoided.  This airplane is certified for 
  the following flight operations as of date of original airworthiness certification. 
    DAY   -   NIGHT   -   VFR   -   IFR"    (as applicable) 
 
  (b) "Reference weight and balance data for loading instructions. 
  (c) "Flaps  -  Pull to extend 
   Takeoff Retracted   0° 
     1st notch 10° 
     2nd notch 20° 
   Landing 3rd notch 30° 
     4th notch 40° 
  (d) "Both tanks on for takeoff and landing." 
  (e) As floatplane or amphibian:  "Retract water rudder during takeoff and landing."

5A6 18 Rev. 68 
DATA PERTINENT TO ALL MODELS (cont’d) 
NOTE 2. (cont’d)  
  A. (4) Model 180J 
  (a) In full view of pilot 
   1. Serial 18052285 through 18052620 
     "This airplane must be operated as a normal category airplane in compliance with 
    the operating limitations as stated in the form of markings, placards and manuals. 
 
MAXIMUMS 
 Landplane 
 
Amphibian 
Edo 597-2790 
Floatplane 
Edo 628-2960 
Maneuvering speed (CAS) 
   
123 mph 
107 knots 
123 mph 
107 knots 
123 mph 
107 knots 
Gross Weight 2800 lb. 2950 lb. 2950 lb. 
Flight load factor Flaps Up +3.8, -1.52 Flaps Down +2.0 
 
    Avoid slips with flaps extended.  No acrobatic maneuvers, including spins, approved. 
    Altitude loss in stall recovery  -  200 ft.  Flight into known icing conditions prohibited.  
    This airplane is certified for the following flight operations as of the date of original 
    airworthiness certificate. 
 
     DAY   -   NIGHT   -   VFR   -   IFR"   (as applicable) 
 
     2. Serial 18052621 and on 
   “This airplane must be operated as a normal category airplane in compliance with 
    the operating limitations as stated in the form of markings, placards and manuals. 
 
MAXIMUMS 
 Landplane 
 
Amphibian 
Edo 597-2790 
Floatplane 
Edo 628-2960 
Maneuvering speed (IAS) 108 knots 106 knots 106 knots 
Gross Weight 2800 lb. 2950 lb. 2950 lb. 
Flight load factor Flaps Up +3.8, -1.52 Flaps Down +2.0 
 
     3. Avoid slips with flaps extended.  No acrobatic maneuvers, including spins,  
      approved.  Altitude loss in stall recovery  -  200 ft.  Flight into known icing  
      conditions prohibited.  This airplane is certified for the following flight operations  
      as of the date of original airworthiness certificate: 
 
       DAY   -   NIGHT   -   VFR   -   IFR”    (as applicable) 
 
  (b) On the flap lever: “FLAPS  -  PULL TO EXTEND 
      Retracted     0º 
      Takeoff  1st notch  10º 
      2nd notch  20º 
      Landing  3rd notch  30º 
      4th notch  40º”

Rev. 68 19 5A6 
DATA PERTINENT TO ALL MODELS (cont’d) 
NOTE 2. (cont’d) 
  A. (4) (c) On fuel selector plate: 
   (Standard range tanks): “Take-off, landing, both on, 60 gal., all flight 
      attitudes; right on, 31 gal., level flight only; left 
      on, 31 gal., level flight only; both off; fuel.” 
      (Through S/N 18052363) 
   (Standard range tanks): “Take-off, landing, both on, 56 gal., all flight 
      attitudes; right on 29 gal., level flight only; left 
      on 29 gal., level flight only; both off; fuel.” 
      (S/N 18052364 and on) 
   (Long range tanks): “Take-off, landing, both on, 79 gal., all flight 
      attitudes; right on, 39 gal., level flight only; left 
      on, 39 gal., level flight only; both off; fuel.” 
      (Through S/N 18052363). 
   (Long range tanks): “Take-off, landing, both on, 75 gal., all flight 
      attitudes; right on, 37 gal., level flight only; left 
      on, 37 gal., level flight only; both off; fuel.” 
      (S/N 18052364 and on) 
  (d) Forward of fuel tank filler cap: 
   (Standard range tanks) “Service this airplane with 80/87 min. aviation grade 
      gasoline  -  capacity 32.5 gal.” 
      (Through S/N 18052363) 
   (Standard range tanks) “Service this airplane with 80/87 min. aviation grade 
      gasoline  -  capacity 30.5 gal.”  (S/N 18052364 and on) 
   (Long range tanks) “Service this airplane with 80/87 min. aviation grade 
      gasoline  -  capacity 42.0 gal.” 
      (Through S/N 18052363) 
   (Long range tanks) “Service this airplane with 80/87 min. aviation grade 
      gasoline  -  capacity 40.0 gal.”  (S/N 18052364 and on) 
  (e) On control lock: “Control lock  -  remove before starting engine.” 
  (f) On inside of baggage door: 
      “Refer to weight and balance data for baggage/cargo  
      loading.” 
  (g) Additional placards if floats are installed: 
   1. Applicable to floatplanes with long range fuel tanks: 
    (At inbd fuel filler cap) 
     “Service this airplane with 80/87 min. aviation grade gasoline  -  
     capacity 37.0 gal.”  (through S/N 18052363) 
    (At inbd fuel filler cap) 
     “Service this airplane with 80/87 min. aviation grade gasoline  - 
     capacity 35.0 gal.”  (S/N 18052364 and on) 
    (At outbd fuel filler cap) 
     “Service this airplane with 80/87 min. aviation grade gasoline  - 
     capacity 42.0 gal.”  (through S/N 18052363) 
    (At oubd fuel filler cap) 
     “Service this airplane with 80/87 min. aviation grade gasoline  - 
     capacity 40.0 gal.”  (S/N 18052364 and on) 
    (At inbd fuel filler cap) 
     “To fill tanks to max. capacity use outboard fillers.” 
     2. Near water rudder control: 
     “Water rudder extend” 
     “Retract water rudder” 
     “Water rudder always up except water taxiing”

5A6 20 Rev. 68 
DATA PERTINENT TO ALL MODELS (cont’d) 
NOTE 2. (cont’d)  
  A. (4) (g) 3. Applicable to amphibian floatplanes: 
    a. With Edo amphibian float installation 597-11 
     (Engine driven hydraulic gear system) 
     (Adjacent to the landing gear control): 
     “Up on water/in air” 
     “Wheels” 
     “Down on land” 
     (Forward of hydraulic hand pump):  “Emergency operation 
     If engine driven hydraulic pump (when installed) 
     fails, use hand-operated hydraulic pump to retract 
     and extend landing gear.  Land on sod if gear position 
     is unknown.  Do not land on water unless gear is fully 
     retracted.” 
     (On hydraulic hand pump handle):  “Landing gear hydraulic pump” 
    b. With Edo amphibian float installation 597-12 
     (Electro-hydraulic gear system) 
     (In plain view of the pilot):  “Emergency landing gear operation 
      If electric driven hydraulic pump fails, use hand  
      operated pump to retract and extend landing gear 
      (see instructions).  Land on sod if gear position is 
      unknown.  Do not land on water unless gear is fully 
      retracted.” 
     (Near the emergency gear hand pump):  
      “Emergency hand pump operating instructions 
      1. Pull landing gear motor circuit breaker. 
      2. Move landing gear position switch to 
       desired position. 
      3. Rotate emergency gear selector valve to 
       desired position. 
      4. Pump emergency gear hydraulic pump until 
       gear locks in desired position. 
      Always keep gear selector valve in off position 
      (detent engaged) except for emergency operation.” 
   4. On instrument panel for floatplane and amphibian:  (S/N 18052501 and on 
    an aircraft modified by Service Kit SK180-33 or SK180-34) 
      “WARNING 
      IN FLOATPLANE AND AMPHIBIAN RETRACT FLAPS TO 
      20° IMMEDIATELY AFTER APPLYING POWER FOR 
      BALKED LANDING GO AROUND.” 
  (h) Additional placard if skis are installed: 
   1. On instrument panel:  “Avoid slips with flaps extended while on skis” 
   2. Applicable to skiplane with retractable skis:  (On instrument panel) 
    (S/N 18052285 through 18052620)  “Do not extend or retract skis at speeds over 140 mph.” 
      “Do not extend or retract skis while in motion on the ground.” 
    (S/N 18052621 and up)   “Do not extend or retract skis at speeds over 125 knots.” 
      “Do not extend or retract skis while in motion on the ground.” 
   3. On instrument panel:  (S/N 18052501 and on and aircraft modified by  
    Service Kit SK180-33 or SK180-34) 
      “WARNING 
      IN SKIPLANE RETRACT FLAPS TO 20° IMMEDIATELY 
      AFTER APPLYING POWER FOR BALKED LANDING GO AROUND.” 
    (i) Near airspeed indicator:  (S/N 18052621 and up) 
      “Maximum Speed  (IAS) 
      Flaps 10° 120 knots 
      Flaps 20° - 40°   90 knots

Rev. 68 21 5A6 
DATA PERTINENT TO ALL MODELS (cont’d) 
NOTE 2. (cont’d)  
A. (5) Model 180K 
  (a) In full view of pilot 
   1. S/N 18052771 through 18053000 
    “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 
 Landplane 
 
Amphibian 
Edo 597-2790 
Floatplane 
Edo 628-2960 
Maneuvering speed (IAS) 109 knots 109 knots 109 knots 
Gross Weight 2800 lb. 2950 lb. 2950 lb. 
Flight load factor Flaps Up +3.8, -1.52 Flaps Down +2.0 
 
    Avoid side slip with flaps extended.  No acrobatic maneuvers, including spins, 
    approved.  Flight into known icing conditions prohibited.  Altitude loss in 
    stall recovery - 200 ft.  This airplane is certified for the following flight 
    operations as of date of original airworthiness certificate. 
 
      DAY   -   NIGHT   -   VFR   -   IFR    (as applicable)” 
 
   2. S/N 18052490, 18053001 and on 
    “The markings and placards installed in this airplane contain operating 
    limitations which must be complied with when operating this airplane 
    in the Normal Category.  Other operating limitations which must be 
    complied with when operating this airplane in this category are contained 
    in the Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual. 
 
     No acrobatic maneuvers, including spins, approved. 
     Flight into known icing conditions prohibited. 
 
    This airplane is certified for the following flight operations as of date of 
    original airworthiness certificate: 
 
     DAY   -   NIGHT   -   VFR   -   IFR    (as applicable)” 
 
  (b) On the flap lever: “FLAPS  -  PULL TO EXTEND 
      Retracted     0º 
      Takeoff  1st notch  10º 
      2nd notch  20º 
      Landing  3rd notch  30º 
      4th notch  40º” 
  (c) On fuel selector plate: “Takeoff, landing, both on, 56 gal., all flight 
   (Standard range tanks) attitudes; right on 29 gal., level flight only; 
        left on 29 gal., level flight only; both off; fuel.” 
        (through S/N 18053000; 18053168 and on) 
   (Long range tanks)  “Takeoff, landing, both on, 75 gal., all flight 
        attitudes; right on, 37 gal., level flight only; 
        left on, 37 gal., level flight only; both off; fuel.” 
        (through S/N 18053000; 18053168 and on) 
   (Integral fuel cells)  “Takeoff, landing, both on, 84 gal., all flight 
        attitudes; right on 40 gal., level flight only; 
        left on 40 gal., level flight only; off; fuel.” 
        (S/N 18052490, 18053001 and on)

5A6 22 Rev. 68 
DATA PERTINENT TO ALL MODELS (cont’d) 
NOTE 2. (cont’d) 
 
  A. (5) (d) Forward of fuel tank filler cap: 
   (Standard range tanks) “Service this airplane with 100/130 min. 
        aviation grade gasoline - capacity 30.5 gal.” 
        (through S/N 18052905) 
        “Service this airplane with 100LL/100 min. 
        aviation grade gasoline - capacity 30.5 gal.” 
        (effective S/N 18052906 through S/N 
        18053000; 18053168 and on) 
        “Fuel cap fwd. ↑ arrow alignment, cap 
        must not rotate during closing.” effective 
        S/N 18052490, 18053001 and on) 
   (Long range tanks)  “Service this airplane with 100/130 min. 
        aviation grade gasoline, capacity 40.0 gal.” 
        (through S/N 18052905) 
        “Service this airplane with 100LL/100 min. 
        aviation grade gasoline - capacity 40.0 gal.” 
        (effective S/N 18052906 through 18053000; 
        18053168 and on) 
        “Fuel cap fwd. ↑ arrow alignment, cap 
        must not rotate during closing.” 
        (effective S/N 18052490, 18053001 and on) 
   (Integral fuel cells)  “Fuel, 100LL/100 min. grade aviation gasoline, 
        capacity 44.0 U.S. gal., capacity 34.5 U.S. gal. 
        to bottom of filler collar.”  (effective S/N  
        18052490, 18053001 and on) 
        “Fuel cap fwd. ↑ arrow alignment, cap must 
        not rotate during closing.”  (effective 
        S/N 18052490, 18053001 and on) 
  (e) On control lock:  “Control lock - remove before starting engine.” 
  (f) On inside of baggage door: “Refer to weight and balance data for baggage/ 
        cargo loading.” 
  (g) Additional placards if floats are installed: 
   1. Applicable to floatplane with long range fuel tanks: 
    (At inbd. fuel filler cap) 
     “Service this airplane with 100/130 min. aviation grade gasoline  
     -  capacity 35.0 gal.” (through S/N 18052905) 
     “Service this airplane with 100LL/100 min. aviation grade gasoline 
     -  capacity 35.0 gal.” (effective S/N 18052906 through S/N 18053000; 
     18053168 and on) 
    (At outbd. fuel filler cap) 
     “Service this airplane with 100/130 min. aviation grade gasoline - capacity 
     40.0 gal.”  (through S/N 18052905) 
     “Service this airplane with 100LL/100 min. aviation grade gasoline - 
     capacity 40.0 gal.” (effective S/N 18052906 through S/N 18053000;  
     18053168 and on) 
    (At inbd. fuel filler cap) 
     “To fill tanks to maximum capacity use outboard fillers.”  (through 
     S/N 18053000; S/N 18053168 and on) 
   2. Near water rudder control: “Water rudder extend” 
        “Retract water rudder” 
        “Water rudder always up except water taxiing.”

Rev. 68 23 5A6 
DATA PERTINENT TO ALL MODELS (cont’d) 
NOTE 2. (cont’d) 
 
A. (5) (g) 3. Applicable to amphibian floatplanes with electric driven hydraulic system: 
    (Near the emergency landing gear pump handle): 
        EMERGENCY 
       LANDING GEAR OPERATION 
      If electric driven hydraulic pump fails, use hand operated 
      pump to retract and extend landing gear. 
      (See instructions.) 
      Land on sod if gear position is unknown. 
       DO NOT LAND ON WATER UNLESS 
       GEAR IS FULLY RETRACTED 
    (Near the emergency gear hand pump): 
       EMERGENCY HAND PUMP 
       OPERATING INSTRUCTIONS 
     1. Pull landing gear motor circuit breaker. 
     2. Move landing gear position switch to desired position. 
     3. Rotate emergency gear selector valve to desired position. 
     4. Pump emergency gear hydraulic pump until gear locks in 
      desired position. 
     Always keep gear selector valve in OFF position (detent engaged) 
     except for emergency operation.” 
    
    (On instrument panel in view of pilot): 
     “In floatplane, amphibian, and skiplane retract flaps 20° 
     immediately after applying power for balked landing go-around.” 
    (Near water rudder control): 
     “Water rudder always up except water taxiing.” 
   4. On instrument panel for floatplane and amphibian: 
     “IN FLOATPLANE, AMPHIBIAN, AND SKIPLANE RETRACT 
     FLAPS TO 20° IMMEDIATELY AFTER APPLYING POWER FOR 
     BALKED LANDING GO AROUND.” 
   5. On instrument panel:  (S/N 18052490, 18053001 through 18053115) 
     “Caution, when floats are installed, it is possible to exceed maximum 
     gross weight with all seats occupied and minimum fuel.  Check 
     weight and balance.” 
  (h) Additional placards if skis are installed: 
   1. On instrument panel:  (effective through S/N 18053000) 
     “Avoid slips with flaps extended while on skis.” 
   2. Applicable to skiplane with retractable skis: (On instrument panel) 
     “Do not extend or retract skis at speeds above 125 knots.” 
     “Do not extend or retract skis while in motion on the ground.” 
   3. On instrument panel:   
     “IN FLOATPLANE, AMPHIBIAN, AND SKIPLANE 
     RETRACT FLAPS TO 20° IMMEDIATELY AFTER APPLYING 
     POWER FOR BALKED LANDING GO AROUND.” 
  (i) Near airspeed indicator:  (effective through S/N 18053000) 
     “Maximum speed (IAS) 
     Flaps 10°  120 knots 
     Flaps 20° - 40°   90 knots” 
       (effective S/N 18052490, 18053001 through 18053115) 
     “Maximum Speed 
     Maneuver  109 KIAS 
     Flaps 10°  120 KIAS 
     Flaps 20° - 40°   90 KIAS” 
     (effective S/N 18053116 and on) 
     “Maximum speed 
     Maneuver  109 KIAS 
     Flaps 10°  120 KIAS 
     Flaps 20°  110 KIAS 
     Flaps 30° - 40°   90 KIAS”

5A6 24 Rev. 68 
Data Pertinent To All Models (cont’d) 
NOTE 2. (cont’d) 
 
A. (5) (j) On instrument panel above horizon gyro:  (Effective S/N 18052490, 18053001 and on) 
    “Avoid slips with flaps extended.” 
  (k) On instrument panel near RNAV when installed:  (Effective S/N 18052490, 
   18053001 and on) 
    “RNAV for VFR flight only.  Tune DME and NAV 1 to same Vortac for 
    RNAV operation.” 
B. The following placard must be displayed on the baggage compartment door: 
  “Maximum baggage 120 lb. for additional loading instructions see weight and balance data.” 
  Models 180G and on: 
  “Refer to weight and balance data for baggage/cargo loading.” 
  C. Models 180H, S/N 18052104 and on: 
    Adjacent to ammeter:  “Do not turn off alternator in flight except in emergency.” 
 
NOTE 3. Reserved. 
 
NOTE 4. The cylinder head temperature probe location is No. 2 cylinder through S/N 18051445, No. 1 
  cylinder S/N 18051446 through S/N 18052500, No. 3 cylinder S/N 18052501 and up. 
 
NOTE 5. The installation of the O-470-S engine in Model 180J (1973 and 1974) will require a change 
  of the oil temperature gauge and the cylinder head temperature probe location.  Reference  
  Cessna Service Letter 75-2 for information and instructions for this change. 
 
NOTE 6. 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 Pilot’s 
  Operating Handbooks listed below is available to the pilot: 
 
  180J, Cessna P/N D1061-13 
  180K, Cessna P/N D1086-13  (S/N 18052771 through 18052905) 
  180K, Cessna P/N D1113-13  (S/N 18052906 through 18053000) 
  180K, Cessna P/N D1140-13PH (S/N 18052490, 18053001 through 18053115) 
  180K, Cessna P/N D1175-13PH (S/N 18053116 through 18053167) 
  180K, Cessna P/N D1195-13PH  (S/N 18053168 through 18053203) 
 
NOTE 7. 14 volt electrical system 
  (180 series through S/N 18052905) 
 
  28 volt electrical system 
  (180 series through S/N 18052906 and on) 
 
In addition to the placards specified above, the prescribed operating limitations indicated by an asterisk (*) under Sections 
I through VI of this data sheet must also be displayed by permanent markings. 
 
--- END ---
```

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- [AD 90-21-08](https://openairdocs.org/ad/90-21-08): Fuel Tank (Bladder) · Cessna 180, 180A, 180B and 8 more. Effective Nov 13, 1990
- [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
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- [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
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- [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
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- [AD 62-17-04](https://openairdocs.org/ad/62-17-04): Float Installations · Edo Model 249A2870 seaplane floats (Kenmore Air EDO Floats STC SA1-622). Effective Aug 14, 1962
- [AD 55-04-01](https://openairdocs.org/ad/55-04-01): Wheel Skis · Cessna 180 and Wheel Skis
- [AD 59-10-03](https://openairdocs.org/ad/59-10-03): Flasher Switch · Cessna 172, 180, 180A and 2 more
- [AD 87-20-03 R2](https://openairdocs.org/ad/87-20-03-R2) (historical): Seat Tracks · Cessna 150A, 150B, 150C and 212 more. Effective Sep 24, 1990
- [AD 86-26-04](https://openairdocs.org/ad/86-26-04) (historical): Shoulder Harness Adjuster · Cessna Aircraft Company, The 120, 140, 140A and 134 more. Effective Jan 6, 1987
- [AD 80-10-01](https://openairdocs.org/ad/80-10-01) (historical): Placard - Airspeed · Fabrication of attaching and rigging parts (Airglas STC SA213AL). Effective May 12, 1980

## Registered aircraft by registry model (OpenAirDocs)

- [Cessna 180](https://openairdocs.org/model/cessna-180): 1,177 aircraft (registry code 2072602)
- [Cessna 180H](https://openairdocs.org/model/cessna-180h): 366 aircraft (registry code 2072618)
- [Cessna 180K](https://openairdocs.org/model/cessna-180k): 274 aircraft (registry code 2072624)
- [Cessna 180J](https://openairdocs.org/model/cessna-180j): 266 aircraft (registry code 2072622)
- [Cessna 180A](https://openairdocs.org/model/cessna-180a): 206 aircraft (registry code 2072604)
- [Cessna 180B](https://openairdocs.org/model/cessna-180b): 94 aircraft (registry code 2072606)
- [Cessna 180C](https://openairdocs.org/model/cessna-180c): 56 aircraft (registry code 2072608)
- [Cessna 180D](https://openairdocs.org/model/cessna-180d): 51 aircraft (registry code 2072610)
- [Cessna 180F](https://openairdocs.org/model/cessna-180f): 42 aircraft (registry code 2072614)
- [Cessna 180G](https://openairdocs.org/model/cessna-180g): 40 aircraft (registry code 2072616)
- [Cessna 180E](https://openairdocs.org/model/cessna-180e): 33 aircraft (registry code 2072612)
- [Cessna/Hull John 180B](https://openairdocs.org/model/cessna-hull-john-180b): 0 aircraft (registry code 2072601)

## STCs approved under this data sheet (716, 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 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 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 SA12389AK](https://openairdocs.org/stc/SA12389AK): Installation of Hartzell Propeller Inc. DHC-G2YF-1BFP/F8849 propeller. Hartzell Propeller LLC
- [STC SA00785AT](https://openairdocs.org/stc/SA00785AT): Installation of a Teledyne Continental Model IO-550-D engine and Hartzell propellers PHC-C3YF-1RF/F8468()-6R, PHC C3YF-1RF/F7691() or McCauley D3A34C401/90DFA-10. Air Plains Services Corporation
- [STC SA01345AT](https://openairdocs.org/stc/SA01345AT): Installation of Teledyne Continental IO-520-D and either Hartzell PHC-C3YF-1RF/F8468A( )-6R, Hartzell PHC-C3YF-1RF/F7691( ), or McCauley D3A34C401/90DFA-10, 3 bladed propellers.. Air Plains Services Corporation
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc.
- [STC SA01866WI](https://openairdocs.org/stc/SA01866WI): Installation of Garmin GFC 500 Autopilot with Electronic Stability and Protection. Garmin International Inc.
- [STC SA01005DE](https://openairdocs.org/stc/SA01005DE): Installation of a EarthX ETX900-TSO Lithium battery. EarthX Inc.
- [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 SA2918NM](https://openairdocs.org/stc/SA2918NM): Attach a casting to the landing gear fuselage attach angles just above main landing gear legs. McFarlane Aviation LLC
- [STC SA4170NM](https://openairdocs.org/stc/SA4170NM): Installation of part numbers PPA1301-1/-2 and PPA1201-1.. McFarlane Aviation LLC
- [STC SA01087SE](https://openairdocs.org/stc/SA01087SE): Installation of titanium main landing gear assembly. Mr. Thomas Anderson
- [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector.. Alcor LLC
- [STC SA02385AK](https://openairdocs.org/stc/SA02385AK): Installation of replacement engine exhaust system assembly (P/N P55C180ESA). Power Flow Systems Inc.
- [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 SA1603SO](https://openairdocs.org/stc/SA1603SO): Installation of Snider speed kit.. Snider Aircraft Accessories Inc.
- [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 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 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 SA00871SE](https://openairdocs.org/stc/SA00871SE): Installation of cockpit sunvisors. Rosen Sunvisor Systems LLC
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc.
- [STC SA01293LA](https://openairdocs.org/stc/SA01293LA): Installation of a modified exhaust collector assembly. Aerospace Welding Minneapolis Inc.
- [STC SA349CE](https://openairdocs.org/stc/SA349CE): Installation of Aqua Model 180-85 floats.. Outpost X Aviation Inc.
- [STC SA01708WI](https://openairdocs.org/stc/SA01708WI): Installation of third lap belt restraint in the center of the main cabin rear bench seat. MN Engineering LLC
- [STC SA04353CH](https://openairdocs.org/stc/SA04353CH): Installation of Hartzell propeller model DHC-G2YF-1BFP/F8068+2 and applicable spinner. Hartzell Propeller Inc.
- [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc.
- [STC SA02576AK](https://openairdocs.org/stc/SA02576AK): Installation of Cleveland and ABI, LLC Wheel and Brake Kits. ABI LLC
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio.. Peregrine
- [STC SA04192NY](https://openairdocs.org/stc/SA04192NY): KFD 900 Primary Flight Display System Additional Functions. Honeywell International Inc
- [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance  Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine
- [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SA02221AK](https://openairdocs.org/stc/SA02221AK): Installation of Alternate Fuel outlet screens per Installation Instructions. Burl's Aircraft LLC

All 716: https://openairdocs.org/tcds/5A6/stcs.md

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