# TCDS A-790: Textron Aviation Inc.

- Type: Type certificate data sheet
- Status: Current
- Holder: Textron Aviation Inc.
- Revision: 37
- Revised: July 29, 2015
- Product: Aircraft, Small Airplane
- Certification basis: CAR 3
- Registered aircraft: 511, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/92/b4/92b4b4225ed66dd877270a8d8d4861e490d314074dfe6255c85f03ab126cf91d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2DB763BCDEE1D2EA86257ED20070E25A.0001
- Page: https://openairdocs.org/tcds/A-790

## Models (4)

As the data sheet lists them.

- 195A ((LC-126A,B,C))
- 190
- 195B
- 195

## What the data sheet says

From the PDF's text layer, line by line; tables lose their columns. The PDF is the record.

```text
Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 
Rev. No. 37 35 35 35 33 33 33 33 33 33 33 33 36 37 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
A-790  
Revision 37 
Textron Aviation Inc. 
190 
(LC-126A,B,C)  195 
195A 
195B 
July 29, 2015 
 
TYPE CERTIFICATE DATA SHEET NO. A-790 
 
This data sheet which is part of Type Certificate No. A-790 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 195 (LC-126A,B,C), 5 PCLM (Normal Category), Approved June 12, 1947; 2 PCLM (Utility Category),  
 Approved November 21, 1947; 5 PCSM (Normal Category), Approved May 3, 1948. 
 (The LC-126C version incorporates relocated battery, aileron control system, and large baggage door to facilitate dual  
 stretchers, reference Items 302(b), 605(c) and 609.  Eligible landplane, seaplane and skiplane).  
 
 Engine Jacobs R755-A2 with magneto-battery combination ignition system 
  (See items 106 and 109 for optional engines) 
 
 Fuel 80 min. octane aviation gasoline 
 
 Engine Limits For all operations, 2200 r.p.m. (300 hp.) 
 
 Airspeed Limits  Landplane: Maneuvering  125 m.p.h. (109 knots) True Ind.(Normal Category) 
      130 m.p.h. (113 knots) True Ind.(Utility Category) 
    Max. structural cruising 178 m.p.h. (155 knots)True Ind. 
    Never exceed 200 m.p.h. (174 knots)True Ind. 
    Flaps extended 130 m.p.h. (113 knots)True Ind. 
     (See Note 3 for item 610) 
  Seaplane:  Maneuvering 125 m.p.h. (109 knots)True Ind. 
    Max. structural cruising 165 m.p.h. (144 knots)True Ind. 
    Never exceed 200 m.p.h. (174 knots)True Ind. 
    Flaps extended 130 m.p.h. (113 knots)True Ind.

A-790 2 Rev. 37 
 
I. Model 195   (cont’d) 
 
 C.G. range  Landplane: (See NOTE 3 for items 610 and 611) 
    (Normal Category) (+44.5) to (+48.3) at 3350 lb. 
     (+36.9) to (+48.3) at 2500 lb. or less 
    Straight line variation between points given 
36 38 40 42 44 46 48
2000
2500
3000
3500
INCHES
LB.
NORMAL
CATEGORY
FRONT
LIMIT
REAR
LIMIT
 
    (Utility Category) (+39.1) to (+42.2) at 2950 lb. 
     (+36.9) to (+42.2) at 2500 lb. or less 
 
   Straight line variation between points given 
   
36 38 40 42 44 46 48
2000
2500
3000
3500
INCHES
LB.
UTILITY
CATEGORY
FRONT
LIMIT
REAR
LIMIT
 
  Seaplane:   
   (Normal Category)  
   (+44.5) to (+47.4) at 3600 lb.  
   (+38.2) to (+47.4) at 2850 lb. or less 
   Straight line variation between points given 
 
36 38 40 42 44 46 48
2000
2500
3000
3500
INCHES
LB.
NORMAL
CATEGORY
FRONT
LIMIT
REAR
LIMIT
 
 Empty Wt. C.G. Range Not available 
 
 Maximum Weight Landplane: (Normal Category) 3350 lb. 
    (Utility Category) 2950 lb. 
  Seaplane: (Normal Category) 3600 lb. 
 
 No. of Seats 5   (two at +36, three at +69.5) 
 
 Maximum Baggage 220 lb. (+92) (Model 195 Standard).  No baggage for Utility Category. 
  (See item 606 for other baggage arrangements)

Rev. 37 3 A-790 
 
I. Model 195   (cont’d) 
 
 Fuel Capacity 81 gal. total (two 40.5 gal. tanks in wings at (+63). (38 gal. usable fuel in each tank).   
  (See NOTE 1 for unusable fuel and item 108 for optional fuel tanks). 
 
 Oil Capacity 5 gal. (+4.5) (See NOTE 1 for data on unusable oil) 
 
 Control Surface Movements Wing flaps   Down 45° 
  Aileron tab Fixed 
  Ailerons Up 25° Down 25° 
  Elevator tab (See NOTE 3 for item 611)  Up 12.5° Down 31° 
  Elevators Up 28° Down 17° 
  Rudder Right 21° Left 21° 
   
 Serial Nos. Eligible 7004 through 7999 
  16000 through 16183 
 
  Prior to civil certification of LC-126A,B and C aircraft, which have been operated by the 
Military Services, must be modified in accordance with Cessna Dwg. 0400115.  This 
drawing and FAA approved airplane flight manual may be obtained thru Cessna's dealer 
organization.  The dealer should also have a file of Cessna Service Letters which should 
be reviewed for applicability. 
 
 Required Equipment Landplane: Items 1(a) and (b), 102(a), 103, 104, 201, 202, 204, 301, 302(a), 303 (when 
used in night operation if flap position indicator not installed), and 403(a) 
or (b). 
  Skiplane: Items 1(a) and (b), 102(a), 103, 104, 204, 208, 301, 302(a), 303 (when used 
in night operation if flap position indicator not installed), and 403(a). 
  Seaplane: Items 1(a) and (b), 102(a), 103, 104, 209, 301, 302, 302(a), 303 (when used 
in night operation if flap position indicator not installed), 403(a) and 602. 
 
 
II. Model 190 (5 PCLM (Normal Category)), Approved July 1, 1947; 2 PCLM (Utility Category), Approved  
 November 21, 1947; 5 PCSM (Normal Category), Approved May 3, 1948. (Same as Model 195 except for engine  
 installation) 
 
 Engine Continental W670-23.  Eligible with either dual magnetos or magneto-battery  
  combination engine ignition system. 
 
 Fuel 80 min. octane aviation gasoline 
 
 Engine Limits For all operations, 2200 r.p.m. (240 hp.) 
 
 Airspeed Limits  Landplane: Maneuvering 125 m.p.h.(109 knots) True Ind. 
      (Normal Category) 
     130 m.p.h.(113 knots) True Ind. 
      (Utility Category) 
    Max.structural cruising 178 m.p.h.(155 knots) True Ind. 
    Never exceed 200 m.p.h.(174 knots) True Ind. 
    Flaps extended 130 m.p.h.(113 knots) True Ind. 
    (See NOTE 3 for item 610) 
  Seaplane: Maneuvering 125 m.p.h.(109 knots)True Ind. 
    Max.structural cruising 165 m.p.h.(144 knots)True Ind. 
    Never exceed 200 m.p.h.(174 knots)True Ind. 
    Flaps extended 130 m.p.h.(113 knots)True Ind.

A-790 4 Rev. 37 
 
II. Model 190  (cont’d) 
 
 C.G. Range  All limits same as Model 195 - see figures under Section I 
  Landplane: (See NOTE 3 for items 610 and 611) 
    (Normal Category) (+44.5) to (+48.3) at 3350 lb. 
     (+36.9) to (+48.3) at 2500 lb. or less 
    (Utility Category) (+39.1) to (+42.2) at 2950 lb. 
     (+36.9) to (+42.2) at 2500 lb. or less 
  Seaplane: (Normal Category) (+44.5) to (+47.4) at 3600 lb. 
     (+38.2) to (+47.4) at 2850 lb. or less 
  Straight line variation between points given. 
 
 Empty Wt. C.G. Range Not available 
 
 Maximum Weight Landplane: (Normal Category)  3350 lb. 
    (Utility Category) 2950 lb. 
  Seaplane (Normal Category)  3600 lb. 
 
 No. of Seats 5   (two at +36, three at +69.5) 
 
 Maximum Baggage 220 lb. (+92).  No baggage for Utility Category.  See Item 606 for auxiliary baggage  
  compartment 
 
 Fuel Capacity 81 gal. total (two 40.5 gal. tanks in wings at (+63).  
  (Usable fuel in each tank:  38 gal. with item 102(b); 37.5 gal. with gravity fuel system).  
  (See NOTE 1 for unusable fuel, NOTE 2 for placard with gravity fuel system, and Item  
  108 for optional fuel tanks). 
 
 Oil Capacity 5 gal. (+4.5)   See NOTE 1 for data on unusable oil. 
   
 Control Surface Movements Wing flaps   Down 45° 
  Aileron tab Fixed 
  Ailerons Up 25° Down 25° 
  Elevator tab (See NOTE 3 for item 611) Up 12.5° Down 31° 
  Elevators Up 28° Down 17° 
  Rudder Right 21° Left 21° 
   
 Serial Nos. Eligible 7004 through 7999 
  16000 through 16183 
 
 Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following  
  items of equipment must be installed: 
  Landplane: Items 1(a) and (c), 102(b), 103, 201, 202, 204, 301, 302(a), 303 (when 
used in night operation if flap position indicator not installed), and 403(a) 
or (b). 
   Skiplane: Items 1(a) and (c), 102(b), 103, 204, 208, 301, 302(a), 303 (when used in  
    night operation if flap position indicator not installed), 403(a). 
  Seaplane: Items 1(a) and (c), 102(b), 103, 209, 301, 302(a), 303 (when used in night 
operation if flap position indicator not installed), 403(a) and 602. 
 
 
III. Model 195A; 5 PCLM (Normal Category), Approved January 6, 1950; 2 PCLM (Utility Category),  
Approved January 6, 1950; 5 PCSM (Normal Category), Approved August 18, 1950.  (Same as Model 195 except 
for engine.) 
 
 Engine Jacobs L-4MB (R-755-9) with magneto-battery combination ignition system. 
 
 Fuel 73 min. octane aviation gasoline 
 
 Engine Limits Maximum continuous, 2000 r.p.m. (225 hp.) 
  Takeoff (one minute), 2200 r.p.m. (245 hp.)

Rev. 37 5 A-790 
 
III. Model 195A   (cont’d) 
 
 Airspeed Limits  Landplane: Maneuvering 125 m.p.h.(109 knots)True Ind. 
         (Normal Category) 
     130 m.p.h.(113 knots)True Ind. 
         (Utility Category) 
    Max. structural cruising 178 m.p.h.(155 knots)True Ind. 
    Never exceed 200 m.p.h.(174 knots)True Ind. 
    Flaps extended  130 m.p.h.(113 knots)True Ind. 
    (See Note 3 for item 610.) 
  Seaplane: Maneuvering 125 m.p.h.(109 knots)True Ind. 
    Max. structural cruising 165 m.p.h.(144 knots)True Ind. 
    Never exceed 200 m.p.h.(174 knots)True Ind. 
    Flaps extended 130 m.p.h.(113 knots)True Ind. 
 
 C.G. Range  All limits same as Model 195 - See figures under Section I. 
  Landplane: (See NOTE 3 for items 610 and 611) 
    (Normal Category) (+44.5) to (+48.3) at 3350 lb. 
     (+36.9) to (+48.3) at 2500 lb. or less 
    (Utility Category) (+39.1) to (+42.2) at 2950 lb. 
     (+36.9) to (+42.2) at 2500 lb. or less 
  Seaplane: (Normal Category) (+44.5) to (+47.4) at 3600 lb. 
     (+38.2) to (+47.4) at 2850 lb. or less 
  Straight line variation between points given 
 
 Empty Wt. C.G. Range  Not available 
   
 Maximum Weight Landplane: (Normal Category) 3350 lb. 
    (Utility Category) 2950 lb. 
  Seaplane: (Normal Category) 3600 lb. 
 
 No. of Seats 5   (two at +36, three at +69.5) 
 
 Maximum Baggage 220 lb. (+92).  No baggage for Utility Category.  See item 606 for auxiliary baggage  
  compartment. 
 
 Fuel Capacity 81 gal. total (two 40.5 gal. tanks in wings at (+63) 
  (38 gal. usable fuel in each tank) (See NOTE 1 for unusable fuel) 
 
 Oil Capacity 5 gal. (+4.5) (See NOTE 1 for data on unusable fuel) 
 
 Control Surface Movements Wing flaps    Down 45° 
  Aileron tab  Fixed 
  Ailerons  Up 25° Down 25° 
  Elevator tab (See NOTE 3 for item 611) Up 12.5° Down 31° 
  Elevators  Up 28° Down 17° 
  Rudder  Right 21° Left 21° 
 
 Serial Nos. Eligible 7004 through 7999 
  16000 through 16183 
       
 Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following  
  items of equipment must be installed: 
  Landplane: Items 1(a) and (b), 102(a), 103, 104, 201, 202, 204, 301, 302(a), 303 (when 
used in night operation if flap position indicator not installed), and 403(e). 
   Skiplane: Items 1(a) and (b), 102(a), 103, 104, 204, 208, 301, 302(a), 303 (when used 
in night operation if flap position indicator not installed), and 403(a). 
  Seaplane: Items 1(a) and (b), 102(a), 103, 104, 209, 301, 302(a), 303 (when used in  
    night operation if flap position indicator not installed), 403(f) and 602.

A-790 6 Rev. 37 
 
IV. Model 195B, 5 PCLM (Normal Category), Approved March 31, 1952; 2 PCLM (Utility Category), March 31, 1952;  
 5 PCSM (Normal Category), Approved March 31, 1952. (Same as Model 195 except for engine.) 
   
 Engine Jacobs R-755B2 with magneto-battery combination ignition system 
 
 Fuel 80 minimum octane aviation gasoline 
 
 Engine Limits For all operations, 2200 r.p.m. (275 hp.) 
   
 Airspeed Limits  Landplane: Maneuvering 125 m.p.h.(109 knots) True Ind. 
          (Normal Category) 
     130 m.p.h.(113 knots) True Ind. 
          (Utility Category) 
    Max. structural cruising 178 m.p.h.(155 knots) True Ind. 
    Never exceed 200 m.p.h.(174 knots) True Ind. 
    Flaps extended  130 m.p.h.(113 knots) True Ind. 
    (See Note 3 for item 610) 
  Seaplane:  Maneuvering 125 m.p.h.(109 knots) True Ind. 
    Max. structural cruising 165 m.p.h.(144 knots) True Ind. 
    Never exceed 200 m.p.h.(174 knots) True Ind. 
    Flaps extended 130 m.p.h.(113 knots) True Ind. 
   
 C.G. Range  All limits same as Model 195 - See figures under Section I. 
  Landplane: (See NOTE 3 for items 610 and 611) 
    (Normal Category) (+44.5) to (+48.3) at 3350 lb. 
     (+36.9) to (+48.3) at 2500 lb. or less 
    (Utility Category) (+39.1) to (+42.2) at 2950 lb. 
     (+36.9) to (+42.2) at 2500 lb. or less 
  Seaplane: (Normal Category) (+44.5) to (+47.4) at 3600 lb. 
     (+38.2) to (+47.4) at 2850 lb. or less 
  Straight line variation between points given 
   
 Empty Wt. C.G. Range  Not available 
 
 Maximum Weight Landplane: (Normal Category) 3350 lb. 
    (Utility Category) 2950 lb. 
  Seaplane: (Normal Category) 3600 lb. 
   
 No. of Seats 5 (two at +36, three at +69.5) 
   
 Maximum Baggage 220 lb. (+92).  No baggage for Utility Category.  See item 606 for auxiliary baggage  
  compartment. 
   
 Fuel Capacity 81 gal. total (two 40.5 gal. tanks in wings at +63) 
  (38 gal. usable fuel in each tank) (See NOTE 1 for unusable fuel) 
   
 Oil Capacity 5 gal. (+4.5)  (See NOTE 1 for data on unusable oil) 
   
 Control Surface Movements Wing flaps    Down 45° 
  Aileron tab  Fixed 
  Ailerons  Up 25° Down 25° 
  Elevator tab (See NOTE 3 for item 611)  Up 12.5° Down 31° 
  Elevators  Up 28° Down 17° 
  Rudder  Right 21° Left 21° 
   
 Serial Nos. Eligible 7004 through 7999 
  16000 through 16183

Rev. 37 7 A-790 
 
IV. Model 195B   (cont’d) 
 
 Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following  
  items of equipment must be installed: 
  Landplane: Items 1(a) and (b), 102(a), 103, 104, 201, 202, 204, 301,  302(a), 303  
    (when used in night operation if flap position indicator not installed), and  
    403(h). 
   Skiplane:  Items 1(a) and (b), 102(a), 103, 104, 204, 208, 301, 302(a), 303 (when used 
in night operation if flap position indicator not installed), and 403(h). 
  Seaplane: Items 1(a) and (b), 102(a), 103, 104, 209, 301, 302(a), 303 (when used in  
    night operation if flap position indicator not installed), 403(i) and 602. 
 
 
Specifications Pertinent To All Models 
 
Datum Front face of firewall 
 
Leveling Means Top of fuselage immediately aft of wing trailing edge 
 
Certification Basis:  
CAR 3 dated December 15, 1946. 
Model 195B certificated under delegation option provisions of Part 410 of the Regulations of the Administrator. 
Type Certificate No. A-790 issued June 12, 1947. 
 
Production Basis: 
Production Certificate No. 4. 
 
Export Eligibility 
Landplane, seaplane and skiplane eligible for export to all countries subject to the provisions of FS P8130-1.  
 
Equipment:  
A plus (+) or minus (-) sign preceding the weight of an item indicates net weight change when that item is installed. 
 
Approval for the installation of all items of equipment listed herein has been obtained by the aircraft manufacturer except those 
items preceded by an asterisk (*).  The asterisk denotes that approval has been obtained by  other than the aircraft manufacturer. 
An item marked with an asterisk may not have been manufactured under an FAA monitored or approved quality control system, 
and therefore attention should be paid to workmanship and conformity with pertinent data called for in this specification. 
 
An item preceded by two asterisks (**) indicates approval under Federal Aviation Regulations Part 21.

A-790 8 Rev. 37 
 
Specifications Pertinent To All Models (cont’d) 
 
Propellers and Propeller Accessories (Excepting Deicing equipment) 
     195  190  195A  195B 
 1. Hamilton Standard constant speed 
  (a) Hub 2B20, blades 6135-15 or 6135-16 104 lb. (-35) (-32) (-35) (-35) 
   Pitch settings at 42 in. sta. 
   ** Model 190, 195A & 195B: Low  9° - 12°,     high 24° - 27° 
   ** Model 195:  Low 10.3° - 12°, high 25.3° - 27° 
   (Propeller to be indexed with blades in line with  
   crankthrow - 0° or 180° position) 
   Diameter: (Not over 93 in.,not under 91-1/8 in. 
  (b) Governor, Hamilton Standard - 1A4      8 lb. (-5)           (-5)   (-5) 
  (c) Governor, Hamilton Standard - 1M12 or 4M12     8 lb.        (-25)             
  *(d) Montgomery spinner for Ham.Std.2B20 propeller     8 lb. (-35) (-32) (-35) (-35) 
   (Special Ham.Std.bolts,P/N70234 required for inst. this item) 
  **(e) Spinner (Cessna Dwg. 0352171)  +4.5 lb. (-35) (-32) (-35) (-35) 
  *(f) Spinner - Mfgr. Aircraft Access. Inc., 2630     8 lb. (-35) (-32) (-35) (-35) 
   So.Wabash Ave.,Chicago,Ill.(Dwg. Nos. 77596-1,-1A, 
   -2,-2A & -3). Special Ham. Std.bolts P/N 70234 required  
   for inst. this item 
 
Engine and Engine Accessories - Fuel and Oil System 
 101 Starter (Eclipse 397-13)    20 lb. (-2) (-6) (-2) (-2) 
 102. Fuel pumps 
  (a) Engine-driven(Romec RD-4140 or Pesco 2F-R400-    2 lb. (-5)         (-5)  (-5) 
   BYLA remarked and reworked by Cessna dwg.0350284) 
  (b) Engine-driven(Candler Hill Titan Model 200,   2 lb.        (-4)              
   H2E3-16) (not required with gravity fuel system) 
 103. Carburetor air filter       X    X   X   X 
 104. Oil radiator (UAP Model U-3140C)    9 lb. (-18)       (-18) (-18) 
 105. Vacuum pumps 
  (a) Engine-driven (Pesco 3P-194-E)    5 lb. (-5)       (- 5) (- 5) 
  (b) Engine-driven (Romec P-207)(Elig. with 
   gravity fuel system)      4 lb.        (- 4)                
 *106. Jacobs L-4MB (R-755-9)  Engines  Use actual wt.                       
  Eligible on 195 landplane with following limits: 
  Fuel  73 min.octane aviation gasoline 
  Engine limits Takeoff (one min.), 2200 r.p.m. (245 hp.) 
    For all other operations, 2000 r.p.m. (225 hp.) 
  When this engine is installed, revised engine baffles, relocated oil  
  cooler, modified engine mount bolts, relocated engine breather  
  and oil separator vent lines, remarked power plant instruments,  
  and FAA Approved Airplane Flight Manual Supplement dated  
  October 21, 1948, as approved for the Purdue Aeronautics Corp., 
  Lafayette, Ind., must be incorporated. 
       195 190 195A 195B 
 107. Winterization equipment (Cessna dwg. 0350285 &     2 lb. (-30) (-27) (-30) (-30) 
  0350286 for Model 195; Cessna dwg. 0350285 & 0350302 for  
  Model 190).  Item 403(c) required when this equipment installed. 
 108. Two 50.5 gal. fuel tanks in wings installed +2 lb. (+63) (+63)       (+63) 
  per Cessna dwg. 0320001 (replaces two 40.5 gal. tanks).  
  With this item installed, fuel capacity is 101 gal. total at (+63)(46 gal.) 
  usable in each tank). Item 403(d) required when these tanks are  
  installed.  (See NOTE 1 for weight of unusable fuel)

Rev. 37 9 A-790 
 
Specifications Pertinent To All Models (cont’d) 
 
Engine and Engine Accessories - Fuel and Oil System (cont’d) 
 *109. Jacobs L-6MB engine   Use actual weight                  
  Eligible on 195 landplane with the following limits: 
  Fuel  80 min.octane aviation gasoline 
  Engine limits Takeoff (one min.) 
    330 hp. 2200 r.p.m. 26 in.Hg.M.P. 
    Max. continuous 
    300 hp. 2100 r.p.m. 24.5 in.Hg M.P.at S.L. 
    200 hp. 2100 r.p.m. 23.5 in.Hg M.P. at 3700' 
  With propeller (item 1),Ham.Std.2B20/6135A-15 
  Pitch settings at 42" sta.: Low -13°, high 28° 
  Installation of this item to be accomplished in accordance  
  with data approved for Scott Aero Services, Inc., 
  4100 Donald Douglas Drive, Long Beach, Calif. 90808. 
  Item 403(g) required when this item installed. 
 
Landing Gear and Floats  
 201. Two main wheel-brake assemblies, Type III 
  (a) Goodyear Model L610HBM (6.50-10) 29 lb. (+25) (+25) (+25) (+25) 
   Wheel Assembly 530858-M 
   Brake Assembly 511613-M 
  (b) Goodyear Model CL8HBM (6.50-8 castering) 29 lb. (+25) (+25) (+25) (+25) 
   Wheel assembly 9530505 L.H. 
    9530506 R.H. 
   Brake assembly 9530503 L.H. 
    9530504 R.H. 
   Installed in accordance with Cessna dwg. 0341150 
 202. (a) Two main wheel 4-ply rating tires, 6.50-10, 28 lb. (+25) (+25) (+25) (+25) 
   Type III with regular tubes 
  (b) Two main wheel 6-ply rating tires, 7.50-10, 38 lb. (+25) (+25) (+25) (+25) 
   Type III with regular tubes 
  (c) Two main wheel 6-ply rating tires, 7.00-8, 31 lb. (+25) (+25) (+25) (+25) 
  Type III with regular tubes 
 204. Tail wheel assembly, General Model 204-A-702M with   8 lb. (+272) (+272) (+272) (+272) 
  Type I tire 
 208. Two skis. Skiplane elig. only in normal category.   8 lb. (+272) (+272) (+272) (+272) 
  (Either a Cessna Skiplane Flight Manual dated February 10,  
  1949 (190), November 14, 1947 (195) or the following required  
  as supplement to the Airplane Flight Manual with any of these  
  skis installed: 
   "PERFORMANCE WITH SKIS INSTALLED 
   Takeoff and Landing: Under the most favorable conditions  
   of smooth packed snow at temperatures approximately 30°F.  
   skiplane takeoff distance is approximately 10 percent greater  
   than the distance shown for the landplane. In applying the  
   performance data, caution should be exercised in that 
   lower temperatures or other snow conditions will increase  
   the ski friction and hence increase the takeoff run and either  
   increase or decrease the landing run. 
   Climb Performance: The skiplane rate of climb is 
   approximately 50 feet per minute less than the landplane." 
  (a) Federal A-3500 according to Cessna dwg. 0340001 Use actual wt. change 
   or Federal Inst. dwg. 11R178 
  (b) Federal A-3500A Federal Inst. dwg. 11R178 Use actual wt. change 
  (c) Federal AWB-3500 Main and AWT-3500 Tail Use actual wt. change 
   Wheel Skis, in accordance with Federal Aircraft Works  
   dwg. 11R692 and 11R874 
   The following placard is required with this installation:  
   "Do Not Extend or Retract Skis while in motion on the Ground."

A-790 10 Rev. 37 
 
Specifications Pertinent To All Models (cont’d) 
 
Landing Gear and Floats (cont’d) 
       195 190 195A 195B 
 209. Float installation, two Edo 38-3430 per Cessna +272 lb. (+43) (+43) (+43) (+43) 
  dwg. 0341102 
 210. Two wheel streamlines per Cessna dwg. 0341143     10 lb. (+25) (+25) (+25) (+25) 
 211. Tail ski, Federal AT-3500 per Cessna dwg. 0342102       8 lb. (+272) (+272) (+272) (+272) 
 212. Two 3/4 in. tapered spring type landing gear per    -25 lb. (+25) (+25) (+25) (+25) 
  Cessna dwg. 0341109 
 *213. Two "no drag" wheel fenders per Liquid Tool Co.,       8 lb. (+26) (+26) (+26) (+26)  
  Box 299, Morrow, Ohio, dwg. 105 
 
Electrical Equipment 
 301. Generator (Eclipse 308-1A or Eclipse 309-8A)     22 lb. (- 2) (- 2) (- 2) (- 2) 
 302. Battery - 12 v. 24 a. hr. 
  (a) Installation in accordance with Cessna dwg. 0310005     36 lb. (+108) (+108) (+108) (+108) 
  (b) Installation in accordance with Cessna dwg. 0311063     36 lb. (+  86) (+  86) (+  86) (+86) 
 303. Landing lights (Grimes G-3800)        5 lb.ea.(+56) (+  56) (+56) (+56) 
 *304. Generator (Eclipse 309A-8A, 50 a.     22 lb. ( -2) ( -2) (   -2) (   -2) 
 *305. Voltage regulator 
  (a) Delco-Remy 1118340   Neglect wt. 
  (b) Delco-Remy 1118713 with shock mounting kit 1910966 
 *306. Generator (Eclipse 30E01-1) 50 a.     24 lb.        ( -2)                
 *307. Voltage regulator, Eclipse 1337-17 Neglect wt. 
 *308. Generator (Eclipse 790-1-B modified per Duryee     22 lb. ( -2)        (  -2) (   -2) 
  Aero. Ser. dwg. DAS 47) 50 a. (Item 305 required) 
 *309. Voltage regulator, Delco Remy 1118884 Neglect wt. 
 *310. Generator (Eclipse 790-1-B modified per Garwin     22 lb. ( -2)       (  -2) ( -2) 
  dwg. G50A and installed according to Garwin instructions  
  dated July 25, 1955), 50 a. (Item 305 or 309 required). 
 
Interior Equipment   
 401. Cabin heater  (Exhaust manifold muff type)       3 lb.   (0)   (0)   (0)   (0) 
 402. Omitted 
 403. (a) FAA Approved Airplane Flight Manual and pertinent 
   revisions applicable to the particular model and serial number 
  (b) FAA Approved Airplane Flight Manual dated September 14,  
   1949 (pertinent to decrease in landing distance) 
  (c) FAA Approved Supplement No. 1 to Airplane Flight 
   Manual (pertinent to winterization equipment, Item 107) 
  (d) FAA Approved Supplement No. 2 to Airplane Flight 
   Manual (pertinent to 50.5 gal. fuel tanks, item 108) 
  (e) FAA Approved Airplane Flight Manual dated December 27,  
   1949 (Model 195A Landplane) 
  (f) FAA Approved Airplane Flight Manual dated August 18,  
   1950 (Model 195A Seaplane) 
  *(g) FAA Approved Airplane Flight Manual dated March 15, 1951  
   (Model 195 Landplane with item 109 installed) 
 **(h) DOA Approved Airplane Flight Manual dated March 31, 1952  
  (Model 195B Landplane and Skiplane) 
 **(I) DOA Approved Airplane Flight Manual dated March 31, 1952  
  (Model 195B Seaplane only) 
 **(j) DOA Approved Airplane Flight Manual dated April 22, 1953  
  (Model 190 Landplane and Skiplane with items 610 and 611 installed) 
 **(k) DOA Approved Flight Manual dated April 22, 1953 
  (Model 195 Landplane and Skiplane with items 610 and 611 installed) 
 **(l) DOA Approved Flight Manual dated April 22, 1953 
  (Model 195A Landplane and Skiplane with items 610 and 611 installed) 
 **(m) DOA Approved Flight Manual dated April 22, 1953 
  (Model 195B Landplane and Skiplane with items 610 and 611 installed)

Rev. 37 11 A-790 
 
Specifications Pertinent To All Models (cont’d) 
 
Interior Equipment (cont’d) 
 **(n) DOA Approved Flight Manual dated June 11, 1954 
  (Model 195 Seaplane with items 610 and 611 installed) 
 **(o) DOA Approved Flight Manual dated June 11, 1954 
  (Model 195B Seaplane with items 610 and 611 installed) 
       195 190 195A 195B 
 404. Cabin heater installation (gasoline combustion type) 17 lb. (+70) (+70) (+70) (+70) 
  (a) Stewart Warner Model 977-B-1 
  (b) Stewart Warner 979-B-1 
 405. Blind flying kit, Cessna dwg. 0300006   4 lb. (+25) (+25) (+25) (+25) 
 
       190 195 195A 195B 
 *406. (a) Lear Model L-2B(1102B)autopilot installation 40 lb. (+111) (+111) (+111) (+111) 
   according to Lear dwgs. 43733, 43654 and 43674. 
   Items 304 and 305 required with this installation.  The  
   following placard should be installed in a conspicuous  
   place near the auto-pilot controller: 
   "Do not use autopilot below 500 feet above terrain 
   except during approach when autopilot is not to be  
   used below 100 feet above terrain. Minimum altitudes 
   do not override any higher minimum operational altitudes." 
   Servo stall forces measured at the pilot's controls 
   on the ground: Rudder 20 to 25 lb.; aileron 12 to 15 lb.;  
   elevator 8 to 12 lb. 
   FAA Approved Lear Flight Manual Supplement dated 
   May 9, 1952 or Manual Supplement dated December 1, 
   1954, required. With Manual Supplement dated 
   December 1, 1954, the above placard is not required 
  (b) Lear Model 1404A altitude controller optional   2 lb. (+84.5) (+84.5) (+84.5) (+84.5) 
 
Miscellaneous (not listed above) 
 601. Flares (3 International 1 1/2 min. Mark I, Model I) 18 lb. (+108) (+108) (+108) (+108) 
 602. Auxiliary seaplane fin per Cessna dwg. 0331135   8 lb. (+264) (+264) (+264) (+264) 
  Fin eligible for installation on landplane in 
  Normal Category only. See NOTE 2 for required placard 
 603. Venturi installation per Cessna dwg. 0310007   2 lb. (+  22) (+  22) (+  22) (+  22) 
 604. Provision for Fairchild Camera. Maximum allowable Use actual wt. change 
  weight for the camera and attachments is 92 lb. 
  Camera operator's stool to be placarded "Do not 
  use for takeoff or landing", making airplane two 
  place when installed. 
  Installation in accordance with: 
  (a) Cessna dwg. 0310010, Station (+58) or 
  (b) Cessna dwg. 0310016, Station (+90) 
   No provision for baggage with item (b) installed 
 605. Gran portable stretcher installation 
  (a) Provision for single stretcher per Cessna dwg. 0300108   (+95) (+95) (+95) (+95) 
  (b) Single stretcher (stored location) 17 lb. (+92) (+92) (+92) (+92) 
   The following placard must be displayed on the baggage  
   door immediately above or below the baggage placard:  
   "Baggage 158 lb.  Maximum with stretcher installed." 
   When in use the C.G. of the stretcher and occupant 
   is at (+79)

A-790 12 Rev. 37 
 
Specifications Pertinent To All Models (cont’d) 
 
Miscellaneous (not listed above) (cont’d) 
       190 195 195A 195B 
  (c) Dual stretchers (stored location) 34 lb. (+92) (+92) (+92) (+92) 
   Install in accordance with Cessna dwgs. 0300004,  
   0300108 and 0310001.  Loading to be determined by  
   weight and balance check or from applicable loading  
   schedule. (Baggage 96 lb. maximum with both stretchers    
   occupied).  When in use the C.G. of stretcher and  
   occupant is at (+79). Eligible only with relocated aileron  
   control system and battery  (item 302(b). 
 
 606. Baggage Provision  
  (a) Auxiliary compartment, maximum capacity 50 lb.   3 lb. (+111) (+111) (+111) (+111) 
   When this is installed, the maximum capacity of 
   the standard baggage compartment is 148 lb., 
   or as determined by weight and balance check 
  (b) Large compartment, maximum capacity 320 lb.  (+97) (+97) (+97) (+97) 
   Reference Cessna dwgs. 0311061, 0311063, and 
   0310001). Less weight added under item 606(c). 
   Loading to be determined by weight and balance 
   check or from applicable loading schedule. 
  (c) Baggage shelf, maximum capacity 75 lb. (Used  (+92) (+92) (+92) (+92) 
   for baggage and/or radio equipment, reference 
   Cessna dwg. 0311837) 
 607. Two abrasion boots, Cessna dwg. 0432161, installed   2 lb. (+242) (+242) (+242) (+242) 
  per Cessna dwg. 0332000 
 *608. (a) Removable stretcher installation according to   37 lb. (+79) (+79) (+79) (+79) 
   installation instructions supplied by Clinton Aviation Co.,  
   Denver, Colo. The following additional placard must be  
   displayed on the baggage door:  "Baggage 116 lb. maximum  
   when stretcher is used." 
  (b) Right rear seat installation (optional when 11 lb. (+69.5) (+69.5) (+69.5) (+69.5) 
   Item 608(a) stretcher is installed. 
 609. Large baggage door in accordance with Cessna dwg. 0311062.   
  Facilitates use of items 605(c) or 606(b). 
 **610. 12 inch chord wing flaps replacing 8 inch chord +2 lb. (+87.0) (+87.0) (+87.0) (+87.0) 
  flaps, Cessna dwg. 0325001 (see NOTE 3 for limitations). 
 **611. Short chord elevators, Cessna dwg. 0334201 (see     -4 lb. (+264) (+264) (+264) (+264) 
  NOTE 3 for limitations). 
 **612. Stall warning indicator, Cessna Kit 52-3-535  +1 lb. (+11) (+11) (+11) (+11) 
 **613. Seaplane conversion kit consisting of: 
  (a) 0341102-46 spring 
  (b) 0341102-47 tab extension 
  (c) 0310202-1 tube assembly 
 *614. Woychik retractable lifting handles, Woychik Aircraft    1 lb. (+211) (+211) (+211) (+211) 
  Aircraft Equipment, Middleton, Wisconsin  (dwgs. 50 and 50A)

Rev. 37 13 A-790 
 
Specifications Pertinent To All Models (cont’d) 
 
NOTE 1. Current weight and balance report, together with list of equipment included in certificated empty weight, and 
loading instructions when necessary, must be in each aircraft at the time of original certification.   
 
 The certificated empty weight and corresponding center of gravity location must include unusable fuel of 30 
lb. at (+63) with 40.5 gal. tanks and item 102(a) or (b), 34 lb. at (+63) with 40.5 gal. tanks and gravity fuel 
system, or 54 lb. at (+63) with 50.5 gal. tanks (item 108) (included in the fuel capacity) and unusable oil of 5 
lb. at (-1) (not included in oil capacity).  
 
NOTE 2. The following placards must be displayed in the locations noted: 
    (a)  In front of and in clear view of the pilot: 
(1) "This airplane must be operated as a normal or utility category airplane in compliance with the flight 
manual." 
   
   NORMAL 
  "No acrobatic maneuvers, including spins, approved. 
  With 3 people on rear seat both front seats must be occupied." 
 
   UTILITY 
  "No acrobatic maneuvers except those listed in the Flight Manual. 
  Baggage compartments and rear seat must not be occupied." 
  or Aircraft using index type loading chart: 
 
  NORMAL 
  "No acrobatic maneuvers, including spins approved." 
 
  UTILITY 
  "No acrobatic maneuvers except those listed in Flight Manual. Baggage compartments and rear 
seat must not be occupied." 
 
    (2) When auxiliary seaplane fin is installed on landplane 
"Landplane with auxiliary seaplane fins.  This airplane must be operated as a Normal Category 
airplane in compliance with the Landplane Flight Manual.  No acrobatic maneuvers, including spins, 
approved. With 3 people on the rear seat, both front seats must be occupied." 
 
 or Aircraft using index type loading chart: 
"Landplane with auxiliary seaplane fins.  This airplane must be operated as a Normal Category 
airplane in compliance with the Landplane Flight Manual.  No acrobatic maneuvers, including spins, 
approved. 
 
    (b)  At the fuel selector valve with gravity fuel system in Model 190: 
    (1) "Takeoff and land with both tanks on."

A-790 14 Rev. 37 
 
Specifications Pertinent To All Models (cont’d) 
 
NOTE 3.   With the installation of items 610 and 611 the following additional limitations apply: 
    (1) C.G. range - Landplane:  
     (Normal Category) (+43.7) to (+48.3) at 3350 lb. 
       (+38.3) at (+48.3) at 2636 lb. 
     (Utility Category) (+39.9) to (+42.2) at 2950 lb. 
       (+38.3) to (+42.2) at 2636 lb. 
     Straight line variation between points given. 
 
36 38 40 42 44 46 48
2000
2500
3000
3500
INCHES
LB.
NORMAL
CATEGORY
 
    Seaplane: 
     (Normal Category) (+44.4) to (+47.5) at 3600 lb. 
       (+40.6) to (+47.5) at 3100 lb. or less 
     Straight line variation between points given. 
36 38 40 42 44 46 48
2000
2500
3000
3500
INCHES
LB.
 
 
   (2) Airspeed Limits:  Flaps extended 110 m.p.h. (95 knots) True Ind. 
 
    (3) Control Surface Movements  Elevator tab Up 10° Down 20° 
       Wing flaps  Down 30° (Seaplane only) 
    (4) Required equipment: Landplane: Items 403(j) or (k) or (l) or (m) and 612  
      Seaplane: Items 403(n) or (o), 612 and 613 
   (5) Serial Nos. eligible:  16084 and up. 
 
 
WARNING:  Use of alcohol-based fuels can cause serious performance degradation and fuel system component 
damage, and is therefore prohibited on Cessna airplanes. 
 
 
 --- END ---
```

## ADs (16, in force first)

- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [AD 2004-21-08 R1](https://openairdocs.org/ad/2004-21-08-R1): Aileron Control System · Cessna 190, 195, 195A and 1 more. Effective May 9, 2013
- [AD 2011-10-09](https://openairdocs.org/ad/2011-10-09): Seat Rails and Roller Housing Inspections · Cessna 150A, 150B, 150C and 221 more. Effective Jun 17, 2011
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2004-19-01](https://openairdocs.org/ad/2004-19-01): Upper shoulder harness adjusters · Cessna F150G, F150H, F150J and 129 more. Effective Nov 1, 2004
- [AD 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996
- [AD 84-10-01 R1](https://openairdocs.org/ad/84-10-01-R1): Bladder Fuel Cells · Cessna 180, 180A, 180B and 103 more. Effective Jul 5, 1988
- [AD 79-08-03](https://openairdocs.org/ad/79-08-03): Electrical System · Cessna 120, 140, 140A and 152 more. Effective Jun 6, 1979
- [AD 63-20-02](https://openairdocs.org/ad/63-20-02): Wing Spar Inspection · Cessna 190, 195, 195A and 1 more. Effective Oct 8, 1963
- [AD 50-39-01](https://openairdocs.org/ad/50-39-01): Rudder Cable Inspection · Cessna 190, 195, 195A and 1 more
- [AD 51-10-04](https://openairdocs.org/ad/51-10-04): Cowl Mounting Channels · Cessna 190
- [AD 51-11-02](https://openairdocs.org/ad/51-11-02): Elevator Spar Webs · Cessna 190, 195, 195A and 1 more
- [AD 2004-21-08](https://openairdocs.org/ad/2004-21-08) (historical): Magnesium Aileron Hinge Brackets · Cessna 190, 195, 195A and 1 more. Effective Nov 30, 2004
- [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

## Registered aircraft by registry model (OpenAirDocs)

- [Cessna 195](https://openairdocs.org/model/cessna-195): 209 aircraft (registry code 2073102)
- [Cessna 195B](https://openairdocs.org/model/cessna-195b): 122 aircraft (registry code 2073112)
- [Cessna 195A](https://openairdocs.org/model/cessna-195a): 106 aircraft (registry code 2073110)
- [Cessna 190](https://openairdocs.org/model/cessna-190): 74 aircraft (registry code 2072902)
- [Rearwin 190](https://openairdocs.org/model/rearwin-190): 0 aircraft (registry code 2370702)

## STCs approved under this data sheet (189, first 50)

- [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 SA2298NM](https://openairdocs.org/stc/SA2298NM): Installation of Cessna SC156001-0110 fuel filler caps.. The 195 Factory, LLC
- [STC SA4471NM](https://openairdocs.org/stc/SA4471NM): Installation of Silver Instruments FUELTRON digital fuel flow indicating system.. The 195 Factory, LLC
- [STC SA4546NM](https://openairdocs.org/stc/SA4546NM): Installation of Cleveland Part No. 040-19900 Tail Wheel Assembly and 10 x 3.50  4 tire and tube.  Installation.. The 195 Factory, LLC
- [STC SA8031NM](https://openairdocs.org/stc/SA8031NM): Installation of locking tail wheel strut.. The 195 Factory 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 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 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 SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC
- [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 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 SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc.
- [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc.
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio.. Peregrine
- [STC SA04400NY](https://openairdocs.org/stc/SA04400NY): Installation of the Integrated Back-up Battery System (IBBS). TCW Technologies LLC
- [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 SA54GL](https://openairdocs.org/stc/SA54GL): Install Cleveland wheel and brake conversion kit, P/N 199-61.. Kaman Corporation Aircraft Wheel and Brake LLC
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc.
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV).. Genesys Aerosystems Inc.
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc.
- [STC SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King)
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA02430SE](https://openairdocs.org/stc/SA02430SE): Fabrication and installation of a camera housing. Airborne Sensor LLC
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SE02712SE](https://openairdocs.org/stc/SE02712SE): Installation of the Oil Scavenging Pump System for Jacobs L-4 and R-755. Henry F. Rogers
- [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA02332AK](https://openairdocs.org/stc/SA02332AK): Installation of a fixed mounted Forward.Vision Enhanced Vision System (EVS) Models 100/600 to include an under-wing conformal fairing with sensor and a glareshield mounted dedicated display monitor. PECO Inc
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA01560WI-D](https://openairdocs.org/stc/SA01560WI-D): Installation of the Honeywell KFD 840 Primary Flight Display System.. Honeywell International Inc
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems.. Garmin International Inc
- [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies
- [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance  Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine
- [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance  Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine
- [STC SA04362CH](https://openairdocs.org/stc/SA04362CH): Installation of the uAvionix skyBeacon Automatic Dependent Surveillance-Broadcast (ADS-B) Out. uAvionix Corporation
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA01435SE](https://openairdocs.org/stc/SA01435SE): Installation of J.P. Instruments (JPI) Primary Engine Data Management System. J. P. Instruments

All 189: https://openairdocs.org/tcds/A-790/stcs.md

---
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