# TCDS A-799: Textron Aviation Inc.

- Type: Type certificate data sheet
- Status: Current
- Holder: Textron Aviation Inc.
- Revision: 55
- Revised: July 29, 2015
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21, CAR 3
- Registered aircraft: 2,085, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/a7/89/a789302f0f161892d151aa373dec42328f3a76a6b7b72f6a7b033f9c44f11dab
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6B274D3FCA582C0586257ED20071150E.0001
- Page: https://openairdocs.org/tcds/A-799

## Models (3)

As the data sheet lists them.

- 170
- 170A
- 170B

## What the data sheet says

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

```text
Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 
Rev. No. 55 50 49 50 54 49 45 45 45 53 53 45 45 45 55 55 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
           
A-799 
Revision 55 
Textron Aviation Inc. 
170 
170A 
170B 
July 29, 2015 
 
 
 
 
 
 
 
 
TYPE CERTIFICATE DATA SHEET NO. A-799 
 
This data sheet which is part of Type Certificate No. A-799 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 
 
WARNING:  Use of alcohol-based fuels can cause serious performance degradation and fuel system component 
damage, and is therefore prohibited on Cessna airplanes. 
 
I. Model 170, 4 PCLM (Normal Category), Approved June 1, 1948; 2 PCLM (Utility Category), Approved  
 July 12, 1948 
 
 Engine Continental C145-2 (See Item 112 for optional engine) 
 
 Fuel 80 Min. octane aviation gasoline 
 
 Engine Limits For all operations, 2700 r.p.m. (145 hp.) 
 
 Airspeed Limits Maneuvering 115 m.p.h. (100 knots) True Ind. 
  Maximum structural cruising 140 m.p.h. (122 knots) True Ind. 
  Never exceed 160 m.p.h. (139 knots) True Ind. 
  Flaps extended   90 m.p.h. (  78 knots) True Ind. 
 
 C.G. Range Normal Category: (+40.9) to (+45.2) at 2200 lb. 
   (+36.3) to (+45.2) at 1733 lb or less 
  Utility Category: (+38.0) to (+40.3) at 1900 lb. 
   (+36.3) to (+40.3) at 1733 lb. or less 
  Straight line variation between points given

A-799 2 Rev. 55 
 
I. Model 170  (cont’d) 
 
 C.G. Range (cont’d) 
1700
1800
1900
2000
2100
36 38 40 42 44 46
INCHES
C.G. RANGE CESSNA 170
AFT
FRONT
UTILITY
CATEGORY
AFT
FRONT
2200
37 39 41 43 45
NORMAL
CATEGORY
 
 Empty Wt. C.G. Range None 
 
 Maximum Weight 2200 lb. Normal Category 
  1900 lb. Utility Category 
 
 No. of Seats 4 (2 at +36), (2 at +70) 
 
 Maximum Baggage 120 lb. (+95) 
 
 Fuel Capacity 37.5 gal. total, 33.5 gal. usable (three 12.5 gal. tanks in wings at +45).  See NOTE 1 for 
weight of unusable fuel 
 Oil Capacity 2 gal. (-20) 
 
Control Surface Wing flaps Up  Down 30° 
Movements Ailerons Up 22° Down 14° 
 Elevator tab Up 10° Down 27° 
 Elevators Up 28° Down 17° 
 Rudder Right 16° Left 16° 
 
 Serial Nos. Eligible 18000 through 18729 
 
 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), 103, 104, 201(a), 202(a), 204(a), 402(a). 
   Skiplane: Items 1(a), 103, 104, 204(a), 208(a), 402(a), and (e) or (d). 
 
Note: For night flying, cabin dome light and instrument lights or equivalent, to provide illumination of all placards and 
instruments are required in addition to equipment required by CAR 43.

Rev. 55 3 A-799 
 
II. Model 170A, 4 PCLM (Normal Category), 2 PCLM (Utility Category), Approved December 15, 1948; 4 PCSM 
(Normal Category), 2 PCSM (Utility Category), Approved June 28, 1949. 
(Same as Model 170 except for single strut all metal wing, revised ailerons and flaps and aileron, flap and elevator control 
systems, revised fuselage to adapt metal wing, dorsal fin and gravity fuel system and fuel tanks).  
  
 Engine Continental C145-2 or -2H (See Item 112 for optional engine) 
 
 Fuel 80 Min. octane aviation gasoline 
 
 Engine Limits For all operations, 2700 r.p.m. (145 hp.) 
 
 Airspeed Limits Landplane: 
   Maneuvering  115 m.p.h. (100 knots) True Ind. 
   Maximum structural cruising 140 m.p.h. (122 knots) True Ind. 
   Never exceed  160 m.p.h. (139 knots) True Ind. 
   Flaps extended 100 m.ph.  (  87 knots) True Ind. 
  Seaplane: 
   Maneuvering (Normal Category) 105 m.p.h. (  91 knots) True Ind. 
    (Utility Category) 110 m.p.h. (  96 knots) True Ind. 
   Maximum structural cruising 110 m.p.h. (  96 knots) True Ind. 
   Never exceed  140 m.p.h. (122 knots) True Ind. 
   Flaps extended 100 m.p.h. (  87 knots) True Ind. 
 
 C.G. Range Landplane: 
   Normal Category (+40.8) to (+46.4) at 2200 lb. 
     (+36.4) to (+46.4) at 1733 lb. or less 
   Utility Category: (+38.0) to (+40.3) at 1900 lb. 
     (+36.4) to (+40.3) at 1733 lb. or less 
  Straight line variation between points given. 
 
1700
1800
1900
2000
2100
2200
36 37 38 39 40 41 42 43 44 45 46
NORMAL
CAT.
AFTUTILITY
CAT.
AFT
FRONT
INCHES
LBS.
47
C.G. RANGE
LANDPLANE
FRONT

A-799 4 Rev. 55 
 
II. Model 170A (cont’d) 
 
 C.G. Range (cont’d)  Seaplane: 
   Normal Category: (+38.8) to (+45.3) at 2106 lb. 
     (+37.0) to (+45.3) at 1800 lb. or less 
   Utility Category: (+38.8) to (+40.6) at 1975 lb. 
     (+37.0) to (+40.6) at 1800 lb. or less 
  Straight line variation between points given. 
 
1800
1900
2000
2100
2200
36 38 40 42 44 46
NORMAL
CATEGORY
C.G. RANGE (SEAPLANE)
AFT
FRONT
UTILITY
CATEGORY
AFT
FRONT
 
 Empty Weight C.G. range None 
 
 Maximum Weight Landplane: 2200 lb. Normal Category 
    1900 lb. Utility Category 
  Seaplane 2106 lb. Normal Category 
    1975 lb. Utility Category 
 
 No. of Seats 4 (2 at +36) (2 at +70) 
 
 Maximum Baggage 120 lb. (+95) 
 
 Fuel Capacity 42 gals. total, 37 gal. usable (Two 21 gal. tanks in wings at +48).  See NOTE 1 for 
weight of unusable fuel 
 
 Oil Capacity 2 gals. (-20) 
 
Control Surface  Wing flaps   Down 50° 
Movements Ailerons Up 20° Down 14° 
 Elevator tab Up 10° Down 27° 
 Elevators Up 28° Down 17° 
 Rudder Right 16° Left 16° 
 
 Serial Nos. Eligible 18730 through 20266 (except 19401). 
 
 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), 103, 201(a), 202(a), 204(a), 402(a). 
   Skiplane: Items 1(a), 103, 204(a), 208(a), 402(a) and (e) or (d). 
   Seaplane: Items 1(a), 103, 209(a), 402(a). 
 
Note: For night flying cabin dome light and instrument lights or equivalent, to provide 
illumination of all placards and instruments are required in addition to equipment 
required by CAR 43.

Rev. 55 5 A-799 
 
III. Model 170B, 4 PCLM (Normal Category), 2 PCLM (Utility Category), Approved September 28, 1950; 4 PCSM 
(Normal Category), 2 PCSM (Utility Category), Approved October 29, 1951. 
(Same as Model 170A except for slotted flaps, revised horizontal tail, flap and aileron control systems, flap limiter, and 
numerous other minor changes.) 
 
 Engine Continental C145-2 or -2H (See item 112 for optional engine) 
 
 Fuel 80 Min. octane aviation gasoline 
 
 Engine Limits For all operations, 2700 r.p.m. (145 hp) 
 
 Airspeed Limits Landplane: 
   Maneuvering  115 m.p.h. (100 knots) True Ind. 
   Maximum structural cruising 140 m.p.h. (122 knots) True Ind. 
   Never exceed  160 m.p.h. (139 knots) True Ind. 
   Flaps extended 100 m.ph.  (  87 knots) True Ind. 
  Seaplane: 
   Maneuvering (Normal Category) 105 m.p.h. (  91 knots) True Ind. 
    (Utility Category) 110 m.p.h. (  96 knots) True Ind. 
   Maximum structural cruising 110 m.p.h. (  96 knots) True Ind. 
   Never exceed  140 m.p.h. (122 knots) True Ind. 
   Flaps extended 100 m.p.h. (  87 knots) True Ind. 
 
 C.G. Range Landplane: 
   Same as Model 170A 
  Seaplane: 
   Normal Category: (+38.8) to (+44.4) at 2106 lb. 
     (+37.0) to (+44.4) at 1800 lb. or less 
   Utility Category: (+38.8) to (+40.6) at 1975 lb. 
     (+37.0) to (+40.6) at 1800 lb. or less 
  Straight line variation between points given 
 
1800
1900
2000
2100
2200
36 38 40 42 44 46
NORMAL
CATEGORY
INCHES
C.G. RANGE (SEAPLANE)
AFT
FRONT
UTILITY
CATEGORY
AFT
FRONT
 
 Empty Weight C.G. Range None 
 
 Maximum Weight Landplane: 2200 lb. Normal Category 
    1900 lb. Utility Category 
  Seaplane 2106 lb. Normal Category 
    1975 lb. Utility Category 
 
 No. of Seats 4 (2 at +36) (2 at +70)

A-799 6 Rev. 55 
 
III.  Model 170B (cont’d) 
 
 Maximum Baggage 120 lb. (+95) 
 
 Fuel Capacity 42 gals. total, 37 gals. usable (Two 21 gal. tanks in wings at +48)).  See NOTE 1 for 
weight of unusable fuel 
 
 Oil Capacity 2 gals. (-20) 
 
Wing Flaps  
All Serials S/N 20267 and on eligible Takeoff Retracted 0° 
  1st Notch 10° 
  2nd Notch 20° 
 Landing 3rd Notch 30° 
  4th Notch 40° 
 Note:  S/N 20267 through 26504 were delivered without the 10° Notch. 
 
Control Surface  Ailerons Up 20° Down 14° Up  20° Down 14° 
Movements Elevator tab Up  12° Down 25° Up  12° Down 25° 
 Elevators Up 26° Down 20° Up  26° Down 20° 
 Rudder Right  16° Left 16° Right 16° Left 16° 
 
 Serial Nos. Eligible 609, 19401 20267 through 20999, and 25000 through 27169 
 
 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), 110, 201(a), 202(a), 204(a), 402(f) and 607 
   Skiplane: Items 1(a), 110, 204(a), 208(a), 402(e), 402(f) and 607. 
   Seaplane: Items 1(a), 103, 209(b), 402(h). 
  Note: For night flying, cabin dome light and instrument lights or equivalent, to provide 
illumination of all placards and instruments are required in addition to equipment 
required by CAR 43. 
 
Specifications Pertinent to All Models 
 
Datum Front face of firewall 
 
Leveling Means Upper door sill 
 
Certification Basis:  
Models 170:  
Civil Air Regulations Part 03 dated December 15, 1946, as amended by 03-1 thru 03-3. 
   
Models 170A:   
Civil Air Regulations Part 03 dated December 15, 1946, as amended by 03-1 thru 03-4. 
   
Model 170B:   
Civil Air Regulations Part 3 dated November 1, 1949, as amended by 3-1 and 3-2. 
   
Type Certificate No. 799 issued June 1, 1948.

Rev. 55 7 A-799 
 
Specifications Pertinent to All Models (cont’d) 
 
Production Basis: 
Production Certificate No. 4.  Delegation Option Manufacturer No. CE-1 authorized to issue airworthiness certificates under 
delegation option provisions of Part 21 of the Federal Aviation Regulations. 
 
Equipment:  
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 someone other than the aircraft 
manufacturer.  An item marked with an asterisk may not have been manufactured under a FAA monitored or approved quality 
control system, and therefore conformity must be determined if the item is not identified by a Form ACA -186, PMA, or other 
evidence of FAA production approval. 
 
An item preceded by two asterisks (**) indicates approval under Part 21 of the Federal Aviation Regulations. 
 
Propellers and Propeller Accessories      170 170A 170B 
 
 1. Propeller 
  (a) McCauley 1A170     33lb. (-39) (-39) (-39) 
   Static r.p.m. at max. permissible throttle setting: 
    Landplane:  Not over 2330, not under 2230 
    Seaplane (Models 170A and 170B):  Not 
    over 2525, not under 2300. 
    No additional tolerance permitted. 
   Diameter:  Not over 76 in., not under 74.5 in. 
   Propeller spinner, dwg. No. 0550101-3      eligible  
   Propeller spinner, dwg. No. 0550162      2 lb. (-39) (-39) (-39) 
  (b) Sensenich 73BR-50 or any other fixed pitch wood  15 1b. (-39) (-39) (-39) 
   Static r.p.m. at max. permissible throttle setting: 
    Not over 2320, not under 2220 
    No additional tolerance permitted 
   Diameter:  Not over 74 in., not under 71.5 in. 
   (Not eligible on seaplane.  Not eligible for  
   new installations on Continental C-145-2 
   engines having undampered crankshafts after November 1, 1951) 
   Propeller spinner, dwg. No. 0550102-3      eligible 
  (c) Koppers Aeromatic F200-H/00-74E    41 lb.   (-38.5) (-38.5) 
   (Models 170A and 170B landplane and skiplane only) 
   Parts List Assembly No. 4356H-1 
   Low pitch setting 13° measured at 24° in. sta. 
   Static r.p.m. at max. permissible throttle setting: 
    Not over 2700, not under 2620 
    No additional tolerance permitted 
   Diameter:  Not over 74 in., not under 72.5 in.

A-799 8 Rev. 55 
 
Specifications Pertinent to All Models (cont’d) 
 
Propellers and Propeller Accessories  (cont’d)    170 170A 170B 
 1. (c) Installation of this item must be in accordance 
with Cessna dwg. No. 0550103 and adjustment 
and operation must be in accordance with 
Koppers "Adjustment Instructions and Operation 
Limitations No. 45."  Item 108 with seaplane lip, 
Item 402(c), and C145-2H engine with dampered 
crankshaft are required when this propeller is 
installed.  With this propeller installation the 
airplane performance has been demonstrated to 
equal or exceed that presented in the Airplane 
Flight Manual with a fixed pitch wood propeller 
over the altitude and temperature range shown.  
This item can only be used on C145-2H engine. 
  *(d) McCauley two-position controllable, hub 2B36C7, blades 60 lb. ____ (-39) (-39) 
   78K-2 (Models 170A and 170B landplane and skiplane 
with C-145-2H engine)  
   Pitch settings at 30 in. sta.: 
    low 13°, high 17.5° 
   Diameter:  Not over 76 in., not under 74.5 in. 
   Item 108 with seaplane lip and Item 402(j) required. 
  *(e) Sensenich M74DR, fixed pitch metal (landplane and   30 lb. (-39) (-39) (-39) 
   skiplane only) 
   Static r.p.m. at max. permissible throttle setting:  Not over 
2320, not under 2220.  No additional tolerance permitted. 
   Diameter:  Not over 74 in., not under 72 in.  
   Item 402(m) required. 
  (f) McCauley 1C172/MDM     30 lb. (-39) (-39) (-39) 
   Static r.p.m. at maximum permissible throttle setting: 
     Landplane: Not over 2350, not under 2250 
     Seaplane:  (Models 170A and 170B):  Not over 
       2525, not under 2300 
   Diameter:  Not over 76 in., not under 74.5 in. 
   No additional tolerance permitted.

Rev. 55 9 A-799 
 
Specifications Pertinent to All Models (cont’d) 
 
Engine and Engine Accessories - Fuel and Oil Systems    170 170A 170B 
 101. Starter (Delco-Remy 1109656)    16 lb. (- 6) (- 6) (- 6) 
 102. Carburetor air filter         1 lb. (-27) (-27) (-27) 
 103. Carburetor air heater and mufflers   10 lb. (-23) (-23) ____ 
 104. Fuel pump (Continental No. 40585)     2 lb. (-32) ____   
 105. Winterization equipment (Cessna dwgs. Nos.    Neglect weight change 
    0552104 and 0552101 or 0552106. 
    0552106 designed for use with 0552002 engine 
    cowl).  Item 402(b) or 402(i) required with this equipment. 
 106. Oil filter - Fram PB-5 
   (1) Installed per Cessna dwg. 0550150     4 lb. (-12) (-12) (-12) 
        *(2) Installed per Fram dwg. 62191 or 62574     4 lb. (-  3) (-  3) (-  3) 
 107. Engine cowl per Cessna dwg. 0552000    Use actual weight 
    Includes 3"-40° lip on bottom cowl 
 108. Engine cowl per Cessna dwg. 0552001 or 0552002   Use actual weight 
    Includes 3/4"-45° lip on bottom cowl 
    required for seaplane 
 109. Oil dilution system (Cessna dwg. 0550151)   No wt. ch. ____ Elig. Elig. 
 110. Hanlon-Wilson exhaust manifolds and carburetor   15 lb. (-22) (-22) (-22) 
    air heater (Cessna dwg. 0550157) 
 *111. Franklin 6A4-165-B3 engine      ____ use ____ 
   Eligible on Model 170A and 170B landplane      actual wt. 
   and seaplane with the following limits: 
    Fuel  80 min. octane aviation gasoline 
    Engine Limits For all operations, 2800 r.p.m. (165 hp.) 
    Propeller McCauley 1A170 with the following limits: 
         Static r.p.m. at max. permissible throttle 
         setting: 
         (landplane): Not over 2350, not under 2200 
         (seaplane): Not over 2500, not under 2400 
         No additional tolerance permitted 
         Diameter:  Not over 76 in., not under 74.5 in. 
    Placard  "Avoid continuous engine operation between 
    required  2150 and 2250 r.p.m." 
    Oil capacity  9 qt. (-20) 
   When this item is installed the engine mount, cowling, baffles, exhaust 
system including carburetor air heater and cabin heater, oil system, power 
plant instruments and markings, battery location, and other items must be 
changed in accordance with the installation instructions, drawings, 
photographs, and parts list approved for Green Flying Service, Eugene 
Airpark, 1953 Chamgers Street, Eugene, Oregon.  Airplane Flight Manual 
Supplement, Item 402(g), is required when this item is installed in 
landplanes.  Airplane Flight Manual Supplement, Item 402(1), obtainable 
from Carl Millard, Ltd., 307 Riverside Drive, Ontario, Canada, required 
when this item installed in seaplanes.

A-799 10 Rev. 55 
 
Specifications Pertinent to All Models (cont’d) 
 
Engine and Engine Accessories - Fuel and Oil Systems (cont’d)     170 170A 170B 
 112. Continental 0-300-A engine (Same limits as for C-145-2 or-2H engine)   Use actual weight 
 *113. 18 gal. auxiliary tank installed in accordance with  Javelin Aircraft Co.,   24 lb. (+99)  (+99) (+99) 
   1405 S. Oliver, Wichita, Kansas.  Installation Instructions dated September  
   15, 1955, and dwgs. Nos. 782-1 and 787 for landplanes and dwgs. Nos.  
   782-1, 782-2, and 787 for seaplanes. 
   (See NOTE 1 for data on unusable fuel) 
   Item 402(k) required when this tank is installed 
   Not eligible on aircraft equipped with Item 404(b) 
 
Landing Gear 
 201. 2 Main wheel-brake assemblies, 6.00-6, Type III 
   (a) Goodyear Model LF6HBD      13 lb. (+22)  (+22) (+22) 
     Wheel Assembly No. 511960-M 
     Brake Assembly No. 9521239 
   (b) Goodyear Model CL6HBM     30 lb. (+22)  (+22) (+22) 
     Wheel Assembly 9530243 L.H. 
        9530242 R.H. 
     Brake Assembly 9530369 L.H. 
        9530368 R.H. 
     Installed in accordance with Cessna dwg. No. 0541150 
     Note:  Item 210 is not eligible with this item 
 202. (a) 2 Main wheel 4 ply-rating tires, 6.00-6,    18 lb. (+22)  (+22) (+22) 
     Type III (with reg. tubes) 
   (b) 2 Main wheel 4 ply-rating tires, 7.00-6,    +1 lb. (+22)  (+22) (+22) 
     Type III (with reg. tubes) 
   (c) 2 Main wheel 4 ply-rating tires, 8.00-6,    10 lb. (+22)  (+22) (+22) 
     Type III (with reg. tubes) 
     (Items 202(a), (b) and (c) eligible for use 
     with Items 201(a) or (b)) 
 204. Tail wheel assembly 
   (a) Scott Model 3-24B, steerable       5 lb. (+246)  (+246) (+246) 
   *(b) Scott Model 3200, steerable, swiveling      8 lb. (+249)  (+249) (+249) 
      installed in accordance with Scott Bulletin I-168) 
   *(c) Maule SFS-1-2-P8         6 lb. (+246)  (+246) (+246) 
    (d) Deleted June 22, 1951 
 208.  Two skis 
    (a) Federal A-2500 according to Cessna dwg.    53 lb. (+16)  (+16) (+16) 
      No. 0541102 or Federal Instln. dwg. No. 11R170 
   *(b) Call S-5 per Call Aircraft dwg. No. 262    71 lb. (+18)  (+18) (+18) 
      (not eligible with Items 201(b) and 202(a) or (c) 
      installed) 
   *(c) Federal A-2500A Federal Instln. dwg. 11R170    Use actual weight change 
   *(d) Federal A-3500 Federal Instln. dwg. 11R170    Use actual weight change 
   *(e) Federal A-3500A Federal Instln. dwg. 11R170    Use actual weight change

Rev. 55 11 A-799 
 
Specifications Pertinent to All Models (cont’d) 
 
Landing Gear (cont’d)         170 170A 170B 
   *(f)  Federal AWA 2500 wheel-ski, Federal Instln.    78 lb.   (All Models) 
      dwg. 11R395 (Eligible with mechanical conversion  
      on ground only) 
      Note: Weight and balance of aircraft shall    Retracted  Extended 
        be checked with ski in retracted and      (+20) (+24) 
        extended position. 
      Not eligible with Item 202(c) installed 
   *(g) Federal AWB 2500 wheel-ski, Federal Instln.    102 lb.  (All Models) 
      dwg. 11R549 (Eligible with hydraulic conversion    Retracted  Extended 
      on ground and in flight)        (+14.5)  (+18) 
      Note: Weight and balance of aircraft shall be 
        checked with ski in retracted and  
        extended position. 
      Placard required: "Do not extend or retract skis while 
          in motion on the ground." 
   *(h) Federal AWB 2500A wheel-ski, Federal Instln. dwg.   108 lb.  (All Models) 
      11R549G (Effective on ski-gear shipped prior to    Retracted Extended 
      January 31, 1952) and 11R889 (Effective on ski-gear    (+14.5)  (+18.5) 
      shipped after January 31, 1952).  (Eligible with hydraulic 
      conversion on ground and in flight) 
      Note:  Weight and balance of aircraft shall be checked 
        with ski in retracted and extended position. 
      Placard required: "Do not extend or retract skis while 
          in motion on the ground." 
   *(i)  Woychik R-1A, Woychik Aircraft Equipment (Middleton,   58 lb. (+17) (+17) (+17) 
      Wisc.) dwgs. Nos. 1 thru 5 (32 psi tire pressure required). 
      Airplane Flight Manual Supplement dated November 19, 1951, 
      required 
   *(j)  Wesco, Western Aircraft Equipment Co. dwgs.Nos. 11 and 148 
      (1) A-25          69 lb. (+15) (+15) (+15) 
      (2) AS-2A          62 lb. (+15) (+15) (+15) 
      (3) AS-2B          64 lb. (+15) (+15) (+15) 
 209.  Two floats 
    (a) Edo 89-2000 per Cessna dwg. No. 0541125   251 lb.   (+41) ____ 
    (b) Edo 89-2000 per Cessna dwg. No. 0541125B  245 lb.     (+40) 
 210.  Two wheel streamlines per Cessna dwg. No. 0441143      6 lb. (+21) (+21) (+21) 
    (not eligible when Items 201(b), 202(b) or (c) are installed) 
 211.  Tail ski, Federal AT-2500 in accordance with Cessna dwg.    6 lb.   (+245) (+245) (+245) 
    No. 0542103 
 *212.  Geisse Safety Gear installed according to St. Louis Machine  12 lb. (+20) (+20) (+20) 
    Co. dwgs. Nos. 1 and 2 and instructions dated May 5, 1953 
    (revised October 8, 1953).  May be used with Item 210 provided 
    St. Louis Machine Co. conversion kit installed per instructions  
    dated February 4, 1954.  Not eligible with Items 201(b), 208, 209, 
    211, or 213 installed.

A-799 12 Rev. 55 
 
Specifications Pertinent to All Models (cont’d) 
 
Landing Gear (cont’d)         170 170A 170B 
 *213.  Whitaker Model L-19 Tandum Gear 
    (a) With Item 202(a)        +64 lb. (+22)  (+22) (+22) 
    (b) With Item 202(b)        +67 lb. (+22)  (+22) (+22) 
    Installed in accordance with A.W. Whitaker, P.O. Box 1811, 
    Portland, Ore., Installation Instructions and dwg. CTG-5 dated 
    October 11, 1952.  When this item is installed, performance  
    information in the Airplane Flight Manual does not apply. 
 *214.  Two "No drag" wheel fenders per Liquid Tool Co., Box 299,     8 lb. (+23)  (+23) (+23) 
    Morrow, Ohio, dwg. No. 105 
 
Electrical Equipment     
 301. Generator (Delco-Remy 1101876)      10 lb. (-6)  (-6) (-6) 
 302. Battery - 12 volt 24 amp. hr.        23 lb. (-3)  (-3) (-3) 
 303. Landing light - Grimes D-3040-8 (Cessna dwg. No. 0422007)     6 lb. (+44)  ------ ----- 
 304. Landing light - G.E. 4509 (Cessna dwg. No. 0523000-2)      2 lb. ------  (+32) (+32) 
 305. Generator - 25 amp. (Delco-Remy No. 1101879, Continental   14 lb. (-6)  (-6) (-6) 
   No. 40734) Must be installed with Continental No. 531325 
   Drive Gear 
 *306. Generator - 35 amp. (Delco-Remy No. 1101880 or No. 1101898)   19 lb. (-6)  (-6) (-6) 
   Eligible only on engines with dampened crankshafts. 
 *307. Voltage regulator, Delco-Remy No. 1118385     Neglect Weight 
 
Interior Equipment 
 401. Cabin heater valve assembly          1 lb. (-2)  (-2) (-2) 
 402. (a) CAA Approved Airplane Flight Manual and pertinent revisions   
applicable to the particular model, serial number, and landing gear 
installation 
  (b) CAA Approved Supplement No. 1 to Airplane Flight Manual (pertinent  
to winterization equipment, Item 105, designed for 0552000 and 0552001 
engine cowls) 
  (c) CAA Approved Supplement No. 2 to Airplane Flight Manual (pertinent   
to Koppers propeller installation, Item 4) 
  (d) CAA Approved Airplane Flight Manuals (Skiplane) dated April 24, 1948  
(Model 170) and December 3, 1948 (Model 170A) 
  (e) The following supplement to Airplane Flight Manual is required for all 
skis listed except for ski Item 208(a) which is covered by Item 402(d) 
above.  "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.  Skiplane landing distance is approximately 20 percent 
greater than that 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."

Rev. 55 13 A-799 
 
Specifications Pertinent to All Models (cont’d) 
 
Interior Equipment (cont’d)        170 170A 170B 
  (f) CAA Approved Airplane Flight Manual for Model 170B, dated    
September 28, 1950. 
  *(g) CAA Approved Supplement to Airplane Flight Manual dated March 15,  
1950 (Model 170A) (landplane) or December 30, 1955 (Model 170B) 
(landplane).  (Pertinent to Franklin 6A4-165-B3 engine installation, Item 
111.) 
   (h) CAA Approved Airplane Flight Manual for Model 170B seaplane dated    
October 29, 1951. 
   (i) CAA Approved Supplement No. 3 to Airplane Flight Manual.  (Pertinent 
to Winterization Equipment, Item 105, designed for 0552002 engine 
cowl). 
  *(j) CAA Approved Airplane Flight manual Supplement for Models 170A and 
170B dated July 5, 1955.  (Pertinent to McCauley controllable propeller 
installation, Item 5). 
  *(k) CAA Approved Airplane Flight Manual Supplement dated November 18, 
1955 (Pertinent to auxiliary fuel tank installation, Item 113). 
  *(l) CAA Approved Supplement to Airplane Flight Manual dated October 6, 
1955 (Pertinent to Franklin 6A5-164-B3 engine installation in Model 
170A and 170B seaplanes). 
  *(m) CAA Approved Airplane Flight Manual Supplement dated January 17, 
1957, prepared by Sensenich Corporation, Lancaster, Pennsylvania, 
pertinent to Sensenich Propeller Installation, Item *6. 
 403.  Blind flying kit. Cessna dwg. No. 0500006       5lb. (+26) (+26) (+26) 
 404.  Cabin heater installation 
   (a) Stewart-Warner Model 977B-1 per Cessna dwg. 0511200  10 lb. ------ (-7) ------ 
   (b) Stewart-Warner Model 979B-1 per Cessna dwg. 0511231  20 lb. ------ (+75) (+75) 
 *405.  Lear Model L-2B (1102B) automatic pilot Model 1404A altitude and  50 lb. (+75) (+75) (+75) 
   controller (optional equipment) installed in accordance with Lear   1.5 lb. (+138) (+138) (+138) 
 Installation dwg. No. 91467 Model 1350A-1 approach coupler and 
 (optional equipment) installed in accordance with Lear dwg. No.       9 lb. (+82) (+82) (+82) 
  700130 Items 306 and 307 required with this auto-pilot installation.   
  Following placard required near automatic pilot controller: 
 "(1) Do not use auto pilot below 150 feet above terrain in the cruise 
configuration. 
  (2) Do not use auto pilot below 75 feet above terrain in the approach 
configuration." 
 Servo stall torque measured at the servo on the ground: 
  Aileron 25±5 in. lb., elevator 25±5 in. lb.,  
  Rudder 50±5 in. lb., Servo drum pitch diameters for all three axes are  
  1.375 inches. 
 FAA Approved Airplane Flight Manual Supplement 
  dated October 19, 1951, is required.  Revision dated September 2, 1952 
(Lear No. 96219) or revision dated November 29, 1954, required when 
altitude controller installed.  Revision dated January 11, 1955, required  
when approach coupler installed. 
 *406.  Fairbanks Aircraft Service Model FAS-1 seat.  Installation to be in   15 lb. (+70) (+70) (+70) 
   accordance with Fairbanks Aircraft Service installation instruction  
   dated September 2, 1952.

A-799 14 Rev. 55 
 
Specifications Pertinent to All Models (cont’d) 
  
Interior Equipment (cont’d)        170 170A 170B 
 *407.  Chinook cabin heater, Model AC (eligible only on airplanes equipped with +3 lb. (+20) (+20) (+20) 
   Item 110).  Installation must be in accordance with instructions in Bulletin  
   AC-2 dated December 1, 1952, as approved for Dakota Aviation Co.,  
   Huron, S. D. 
 *408.  Javelin A-2 single axis automatic pilot installed according to Javelin dwg. 18 lb. (+110) (+110) (+110) 
   No. 725. 
 *409.  Javelin rudder trim according to Javelin dwg. No. 719 (sheets 1 and 2       5 lb. (+123) (+123) (+123) 
   revised April 14, 1955) and Instructions dated March 1955.  Airplane Flight 
Manual Supplement for Javelin Rudder Trim dated May 20, 1955, required. 
 *410.  Deleted November 26, 1957.  Now covered by STC SA1-107 
 *411.  Lear ARCON Model A according to Lear dwg. No. 703437 or dwg. No.  12 lb. (+96) (+96) (+96) 
   702090.  Lear Flight Manual Supplement for Lear "Arcon" dated  
   February 16, 1955, required. 
 *412.  Type 69A112 Gyro-Stabilizer installed according to Globe Industries, Inc.  15 lb. ------- (+99) -------- 
   Installation Manual No. 503 dated July 1955. 
   Servo cable slip clutch forces 7 to 12 lb. measured at pilot's control.  Placard 
required near automatic control controller:  "Do not use Auto pilot during 
Takeoff and Landing Within 75 feet of ground." 
 
Miscellaneous (not listed above)       
 601.  Flares, three 1 1/2 PF-11 International    18 lb. (+98)  (+98) (+98) 
 602.  Gran portable stretcher installation 
   (a) Provision for stretcher, Cessna dwg. 0511003    elig.  elig. elig. 
   (b) Gran portable stretcher (stored location)    17 lb. (+95)  (+95) (+95) 
  Note: The stretcher is adjustable for use at two lengths of approximately 72 
and 64 inches.  The co-pilot's seat may not be occupied with the 
stretcher extended to 72 inches, the co-pilot's seat back serving as the 
stretcher's forward support.  However, with the stretcher shortened to 
64 inches the co-pilot's seat may be occupied, if so desired.  The last 
sentence of the normal category placard specified in NOTE 2 is not 
applicable with this item installed.  Instead, the maximum ** allowable 
baggage is limited for each aircraft as determined by weight and 
balance check for the most rearward C.G. limit with the stretcher 
occupied at (+73) and with the co-pilot's seat unoccupied.  The 
following placard must be installed in the baggage compartment: 
    "Maximum baggage  **  lb. with stretcher installed." 
 603. Provision for camera per drawing No. 0510010 Maximum allowable weight  Use actual weight change 
  for the camera and attachments is 92 lb. at (+72).  Camera operator's stool to be 
placarded:  "No Seat during Takeoff or Landing." making the airplane two-
place when installed. 
 604. Venturi installation in accordance with Cessna dwg. 0511010A   10 lb. (+17)  (+17) (+17) 
 605. Heated pitot installation in accordance with Cessna dwg. 0511051     1 lb. (+12)  (+12) (+12) 
 *606. Spray system installation in accordance with Yingling Aircraft, Inc.   +84 lb. -------  (+33) ------- 
  dwg. Y-200 and installation instructions.   
  Spray fluid           -------  (+57) ------- 
 607. Stall warning kit in accordance with Cessna dwg. 0511062    elig.  elig. elig. 
 608. Deleted November 30, 1951 
 609. Model 170A dorsal fin (eligible on Model 170)

Rev. 55 15 A-799 
 
Specifications Pertinent to All Models (cont’d) 
 
Miscellaneous (not listed above) (cont’d)        170 170A 170B 
 *610. Whitaker Model CWS-53 "Wingspray" installation instructions CWS-15   90 lb. -------  (+35) ------- 
  (less fans and brushes) 
 *611. Woychik retractable lifting handles, Woychik Aircraft Equipment  14 oz. (+172)  (+172) (+172) 
  (Middleton, Wisc.), dwg. Nos. 50 and 50A 
 *612. Metal Plating of Wings.  Model 170 eligible when wings are Use actual  -------- -------- 
  covered with metal skin per Technical Instruction Report No. wt. change 
  101440 by Birtcraft Engineering Co., 11826 Cherry Ave., Inglewood, 
California 
 613. Omitted 
 *614. Metal skin installed in accordance with Met-Co-Aire, Fullerton,  Use actual weight change 
  California, dwg. No. 7108 
 
NOTE 1. Current weight and balance report including list of equipment included in certificated empty weight, and 
loading instructions when necessary, must be in each aircraft at the time of original certification and at all 
times thereafter (except in the case of air carrier operators having an approved weight control system).  
 
 The certificated empty weight and corresponding center of gravity location must include unusable fuel at 19 
lb. at (+53) for Model 170 and 30 lb. at (+46) for Model 170A and Model 170B (above values are included 
in total fuel capacity).  When Item 113, 18 gallon auxiliary fuel tank, is installed an additional 3 lb. unusable 
fuel at (+99) must be included. 
 
NOTE 2.  (a) The following placards must be displayed in front of and in clear view of the pilot: 
 
    Model 170: 
   “This airplane must be operated as a normal or utility category airplane in compliance with the Airplane 
Flight Manual.” 
 
    NORMAL       UTILITY 
    “No acrobatic maneuvers including spins approved. “No acrobatic maneuvers 
    With two people in the rear seat both front seats  approved except those listed 
    must be occupied.”      In the Airplane Flight Manual.  
            Baggage compartment and rear 
            seat must not be occupied.” 
 
    Models 170A and 170B: 
   “This airplane must be operated as a normal or utility category airplane in compliance with the Airplane 
Flight Manual.” 
 
    NORMAL       UTILITY 
   “No acrobatic maneuvers including spins approved.” “No acrobatic maneuvers approved 
except those listed in the Airplane 
Flight Manual.  Baggage compartment  
 
   “Both tanks on for takeoff and landing.” and rear seat must not be occupied."

A-799 16 Rev. 55 
 
Specifications Pertinent to All Models (cont’d) 
 
NOTE 2 (cont’d) Models 170A and 170B (Seaplanes): 
   "Retract Water Rudder During Takeoff and Landing." 
 
    Model 170B Seaplane: 
   "Intentional Spins Prohibited" (Normal and Utility Categories) 
 
   (b) The following placard must be displayed in the baggage compartment: 
 
   "Maximum Baggage 120 lb.  For additional loading instructions see Weight and Balance Data." 
 
  (c) The following placard must be displayed in front of and in clear view of the pilot for those aircraft with Items 
Nos. 208(g) and 208(h) installed: 
 
   "Do not extend or retract skis while in motion on the ground." 
 
 
 
--- END ---
```

## ADs (22, 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 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 2006-12-07](https://openairdocs.org/ad/2006-12-07): ECi cylinder assemblies · Aerostar AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 386 more. Effective Jul 11, 2006
- [AD 2006-03-08](https://openairdocs.org/ad/2006-03-08): Vacuum pumps · Aero Advantage 14-19, 14-19-2, 14-19-3 and 299 more. Effective Mar 10, 2006
- [AD 2005-01-19](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 98-21-21 R1](https://openairdocs.org/ad/98-21-21-R1): Electric Inflatable Door Seals · Cessna 17-30, 17-30A, 17-31 and 267 more. Effective May 1, 2000
- [AD 99-27-02](https://openairdocs.org/ad/99-27-02): Fuel Selector Valves · Cessna 170B, 172, 172A and 36 more. Effective Jan 21, 2000
- [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 96-09-06](https://openairdocs.org/ad/96-09-06): Air Filter Assemblies · Maule Aerospace Technology 7ACA, 7ECA, 7FC and 180 more. Effective Jun 7, 1996
- [AD 79-10-14 R1](https://openairdocs.org/ad/79-10-14-R1): Fuel Tank Venting · Cessna 140A, 150, 150A and 172 more. Effective May 30, 1988
- [AD 82-07-02](https://openairdocs.org/ad/82-07-02): Engine Crankcase Breather · Lycoming O-360-A1A engine and Hartzell HC-C2YK-1B/7666A-2… (Avcon Industries STC SA1324CE or 14 others). Effective Apr 8, 1982
- [AD 81-15-03](https://openairdocs.org/ad/81-15-03): Engine Inlet Air Filters · Replace existing engine induction air filter (Brackett Aero Filters STC SA693CE or SA71GL). Effective Jul 20, 1981
- [AD 79-08-03](https://openairdocs.org/ad/79-08-03): Electrical System · Cessna 120, 140, 140A and 152 more. Effective Jun 6, 1979
- [AD 74-06-02](https://openairdocs.org/ad/74-06-02): AVCON Mufflers · Lycoming 150 and160 hp Model O-320-( ) engine (Williams Robert or Barbara STC SA750CE or 3 others). Effective Mar 18, 1974
- [AD 73-17-01](https://openairdocs.org/ad/73-17-01): Fuel Transfer Pump Placard · Cessna 170, 170A, 170B and 53 more. Effective Aug 16, 1973
- [AD 69-15-03](https://openairdocs.org/ad/69-15-03): Muffler Assembly · Lycoming O-320-A1A, A1B, A3A, A3B or Lycoming O-320-B1A, B1B… (D'Shannon Products STC SA135CE or 8 others). Effective Aug 20, 1969
- [AD 54-02-02](https://openairdocs.org/ad/54-02-02): Wheel Skis · Cessna 170, 170A, 170B and 2 more
- [AD 48-43-02](https://openairdocs.org/ad/48-43-02): Continental C-145-2 Engines · Cessna 170, 170A, 15AC and 1 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

## Registered aircraft by registry model (OpenAirDocs)

- [Cessna 170B](https://openairdocs.org/model/cessna-170b): 1,300 aircraft (registry codes 2072306, 2072307)
- [Cessna 170A](https://openairdocs.org/model/cessna-170a): 513 aircraft (registry code 2072304)
- [Cessna 170](https://openairdocs.org/model/cessna-170): 272 aircraft (registry code 2072302)

## STCs approved under this data sheet (472, first 50)

- [STC SA01233SE](https://openairdocs.org/stc/SA01233SE): Fabrication and installation of Alaskan Bushwheel LLC tail wheel and fork assembly. ABI, LLC
- [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 SA12446AK](https://openairdocs.org/stc/SA12446AK): Installation of Sensenich Propeller Company 2G0M8SXX/C76PGF Composite, Ground Adjustable Propeller. Sensenich Propeller Company
- [STC SA02539AK](https://openairdocs.org/stc/SA02539AK): Installation of a Continental Aerospace Technologies IO-370CLC1U8 and Hartzell Model HC-C2YR-1N/NG8301,-3, -7 Propeller. David A. Stoots
- [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 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 SA01005DE](https://openairdocs.org/stc/SA01005DE): Installation of a EarthX ETX900-TSO Lithium battery. EarthX Inc.
- [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 SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector.. Alcor LLC
- [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 SA7965SW](https://openairdocs.org/stc/SA7965SW): Application of fabric and polyurethane finishing system.. Shady Aviation LLC
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd.
- [STC SA11841BO](https://openairdocs.org/stc/SA11841BO): Installation of T3 Tailwheel Suspension System suspension. T3 Tailwheel Suspension System
- [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 SA4503NM](https://openairdocs.org/stc/SA4503NM): Remove original cloth covering and install Ceconite covering. Ceconite Division of Poly-Fiber Inc.
- [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 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 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 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 SA00897WI](https://openairdocs.org/stc/SA00897WI): Installation of Concorde Battery Corporation (VRSLA) Valve regulated sealed lead acid battery.. Aero-Mach Wilco LLC
- [STC SA3-159](https://openairdocs.org/stc/SA3-159): Installation of Wipaire Skis Inc. Model C-3000 (Aircraft Skis) (FluiDyne) (Federal) Main (hydraulically actuated) and AWT 2500A or CT-3000 Tail Wheel skis. F.Atlee Dodge Aircraft Services
- [STC SA3-329](https://openairdocs.org/stc/SA3-329): Installation of Wipaire Skis Inc. Model C-3000 (Aircraft Skis) (FluiDyne) (Federal) Main (manually actuated) and AWT-2500A or CT-3000 Tail skis. F.Atlee Dodge Aircraft Services
- [STC SA3-339](https://openairdocs.org/stc/SA3-339): Installation of Wipaire Skis Inc. Model C-3000 (Aircraft Skis) (FluiDyne) (Federal) Main Wheel (either manually or hydraulically actuated) ski having a cross-wind wheel utilizing a 6.00-6 tire. F.Atlee Dodge Aircraft Services
- [STC SA3-423](https://openairdocs.org/stc/SA3-423): Installation of CT-3000 tail ski on airplanes equipped with Scott 3200 or 3400 tail wheels.. F.Atlee Dodge Aircraft Services
- [STC SA3-468](https://openairdocs.org/stc/SA3-468): Installation of Wipaire Skis Inc. Model CF-3000 (Aircraft Skis) (FluiDyne) (Federal) Main Wheel skis, AWT-2500A or CT-3000 Tail Wheel skis. F.Atlee Dodge Aircraft Services
- [STC SA3-53](https://openairdocs.org/stc/SA3-53): Model 3000 main and Model 1000 tail skis.. F.Atlee Dodge Aircraft Services
- [STC SA00406WI](https://openairdocs.org/stc/SA00406WI): Installation of replacement flap trailing edge bulbs with AOG Drawing. Athena Aircraft, LLC
- [STC SA00709SE](https://openairdocs.org/stc/SA00709SE): Installation of replacement control surface skin panels.. Athena Aircraft, LLC
- [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation
- [STC SA2280CE](https://openairdocs.org/stc/SA2280CE): Installation of aileron and/or flap gap seals.. Curry Aviation LLC
- [STC SA2516CE](https://openairdocs.org/stc/SA2516CE): Installation of replacement wing tips.. Curry Aviation LLC
- [STC SA2851CE](https://openairdocs.org/stc/SA2851CE): Installation of wheel fairings.. Curry Aviation LLC

All 472: https://openairdocs.org/tcds/A-799/stcs.md

---
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