# TCDS A42EU: Textron Aviation Inc.

- Type: Type certificate data sheet
- Status: Current
- Holder: Textron Aviation Inc.
- Revision: 5
- Revised: April 1, 2019
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21, Part 23, Part 36, CAR 3
- Data sheet PDF: https://openairdocs.org/files/sha256/fa/a2/faa2d116ea47cf85683df0cb6ab35f77046725c30be234239d771446b57535f7
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BE70DB24E1720172862583EE0072A028.0001
- Page: https://openairdocs.org/tcds/A42EU

## Models (3)

As the data sheet lists them.

- FR182
- F182P
- F182Q

## 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 
Rev. No. 5 5 5 4 5 2 2 2 2 2 5 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
A42EU 
Revision 5 
Textron Aviation 
F182P 
F182Q 
FR182 
April 1, 2019 
 
WARNING:  Use of alcohol-based fuels can cause serious performance degradation and fuel 
 system component damage, and is therefore prohibited on Cessna airplanes. 
 
TYPE CERTIFICATE DATA SHEET NO. A42EU 
 
This data sheet, which is a part of Type Certificate No. A42EU, 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, KS 67215 
 
Type Certificate Holder Record Cessna Aircraft Company transferred to  
   Textron Aviation Inc. on July 29, 2015 
 
Type Certificate A42EU was transferred from Reims Aviation S.A., 51 Aerodrome de Reims-Prunay, Reims, France, to Cessna 
Aircraft Company on December 11, 2006.  Coincident with this transfer, the Federal Aviation Administration (FAA) has accepted 
the status of State of Design and State of Manufacture as defined by Annex 8 to the Convention of International Civil Aviation.  
Prior to December 11, 2006, products identified under Type Certificate A42EU were approved by the FAA in accordance with the 
Federal Aviation Regulation appropriate to Imported Products (FAR 21.29).  Effective December 11, 2006, and after, these 
products are to be considered domestic products for the purpose of certification, and Federal Aviation Regulations 21.21 becomes 
appropriate. 
 
I. Model F182P, 4 PCLM (Normal Category), Approved June 18, 1976 
 
 Engine Continental O-470-S 
 
 *Fuel 80/87 minimum grade aviation gasoline 
 
 *Engine Limits For all operations, 2600 rpm (230 hp) 
 
 Propeller and 1. McCauley constant speed 
    Propeller Limits  a) Hub 2A34C201/90DA-8 
     Diameter:  not over 82 in., not under 80 in. 
     Pitch settings at 30 in. sta.:  low 13°, high 24.5° 
    b) Cessna spinner 0752637 
    c) Woodward governor 210065, 210105, 210345, 210155, A210452 or  
     Garwin 34-828-01-2A or McCauley C290D2/T1 or C290D3/T1 
 
   2. McCauley constant speed 
    a) Hub 2A34C66/90AT-8 blades 
     Diameter:  not over 82 in., not under 80 in. 
     Pitch settings at 36 in. sta.:  low 10.5°, high 22° 
    b) Cessna spinner 0752637 
    c) Woodward governor 210065, 210105, 210155, 210345, 210452 or  
     Garwin 34-828-01 or McCauley C290D2/T1 or C290D3/T1

Rev. 5  2 A42EU 
 
I. Model F182P (cont’d) 
 
 Propeller and 3. McCauley constant speed 
   Propeller Limits (cont’d)  a) Hub 2A34C203/90DCA-8 blades 
     Diameter:  not over 82 in., not under 80.5 in. 
     Pitch settings at 30 in. sta.:  low 12.5°, high 25° 
    b) Cessna spinner 0752637 
    c) Woodward governor 210065, 210155, 210345, 210105, 210452 or  
     Garwin 34-828-01 or McCauley C290D2/T1 or C290D3/T1 
 
 *Airspeed Limits (IAS) Maneuvering 127 mph (110 knots) 
   (See NOTE 4  Maximum structural cruising 162 mph (141 knots) 
   on use of IAS) Never exceed  203 mph (176 knots) 
   Flaps extended 110 mph ( 95 knots) 
 
  
 C.G. Range (+39.5) to (+48.5) at 2950 lb. 
   (+33.0) to (+48.5) at 2250 lb. or less 
   Straight line variation between points given. 
 
 Empty Weight C.G. Range None 
 
 *Maximum Weight 2950 lb. 
 
 No. of Seats 4 (2 front at +32.0 to +50.0)   
      (2 rear at +74.0) 
 Maximum Baggage 200 lb. (120 lb. at +  82.0 to +108.0) 
     (  80 lb. at +108.0 to +136.0) 
 
 Fuel Capacity Standard Range Tanks: 
   61 gal. (56 gal. usable); two 30.5 gal. tanks in wings at +48 
 
   Long Range Tanks: 
   80 gal. (75 gal. usable); two 40.0 gal. tanks in wings at +48 
 
   See NOTE 1 for data on unusable fuel 
 
 Oil Capacity 12 qt (-15)(7.5 qt usable) 
   See NOTE 1 for data on unusable oil 
 
 Control Surface Movements Wing Flaps   Down 40° + 1°, -2° 
   Elevator tab   Up 25° + 2° Down 15° + 1° 
   Ailerons  Up 20° + 2° Down 15° + 2° 
   Elevator  
     (relative to stabilizer) Up 26° + 1° Down 17° + 1° 
   Rudder  
     (parallel to 0.00 W.L.) Right 24° + 1° Left 24° + 1° 
     (perpendicular to hinge line) Right 27°13' + 1° Left 27°13' + 1° 
 
 Serial Numbers Eligible F18200001 through F18200025 
 
 
II. Model F182Q, 4 PCLM (Normal Category), Approved November 26, 1976 
 
 Engine Continental O-470-U 
 
 *Fuel 100/130 minimum grade aviation gasoline (1977 Model)  
   100LL/100 aviation grade gasoline (1978 Model and on) 
 
 *Engine Limits For all operations, 2400 rpm (230 hp)

Rev. 5  3 A42EU 
III. Model F182Q (cont’d) 
  
 Propeller and  
  Propeller Limits 1. McCauley constant speed 
       a) Hub C2A34C204/90DCB-8 
     Diameter:  not over 82 in., not under 80.5 in. 
     Pitch settings at 30 in. sta.:  low 15°, high 29.4° 
    b) Cessna spinner 0752637 
    c) McCauley governor C290D3/T14 
 
 *Airspeed Limits (IAS) Maneuvering   111 knots 
   (See NOTE 4  Maximum structural cruising  143 knots 
    on use of IAS) Never exceed  179 knots 
   Flaps extended    95 knots 
 
 C.G. Range (+39.5) to (+48.5) at 2950 lb. 
   (+33.0) to (+48.5) at 2250 lb. or less Straight line variation between points given. 
 
 Empty Weight C.G. Range None 
 
 *Maximum Weight 2950 lb. 
 
 No. of Seats 4 (2 front at +32.0 to +50.0)   
      (2 rear at +74.0) 
 
 Maximum Baggage 200 lb.   (120 lb. at +82.0 to +108.0) 
    (  80 lb. at +108.0 to +136.0) 
 
 Fuel Capacity Standard Range Tanks: 
   61 gal. (56 gal. usable); two 30.5 gal. tanks in wings at +48 
    (1977 and 1978 Models) 
   Long Range Tanks: 
   80 gal. (75 gal. usable); two 40.0 gal. tanks in wings at +48 
   (1977 and 1978 Models) 
   92 gal. (88 gal. usable); two 46.0 gal. integral tanks in wing at +46.5 
   (1979 Model and on) 
   See NOTE 1 for data on unusable fuel 
 
 Oil capacity 12 qt (-15)  (7.5 qt usable) 
   See NOTE 1 for data on undrainable oil. 
 
 Control surface movements Wing Flaps    Down   40° + 1°, -2° 
   Elevator tab Up 25° + 2° Down 15° + 1° 
   Ailerons  Up 20° + 2° Down 15° + 2° 
   Elevator  
   (relative to stabilizer) Up 26° + 1° Down 17° + 1° 
   Rudder  
   (parallel to 0.00 W.L.) Right 24° + 1° Left 24° + 1° 
   (perpendicular to hinge line) Right 27°13' + 1° Left 27°13' + 1° 
 
 Serial Numbers Eligible F18200026 through F18200169 
 
 
III.   Model FR182, 4 PCLM (Normal Category), Approved February 23, 1978 
 
 Engine Lycoming O-540-J3C5D 
 
 *Fuel 100LL/100 aviation grade gasoline 
 
 *Engine Limits For all operations, 2400 rpm (235 hp)

Rev. 5  4 A42EU 
 
III.   Model FR182 (cont’d) 
 
 Propeller and 
  Propeller Limits 1. McCauley constant speed 
       a) Hub B2D34C214/90DHB-8 
     Diameter:  not over 82 in., not under 80.5 in. 
     Pitch settings at 30 in. sta.:  low 15.8°, high 29.4° 
    b) Cessna spinner 2250003 
    c) McCauley Governor C29D3/T16 
 
 
 *Airspeed Limits (IAS) Maneuvering 112 knots 
   (See NOTE 4  Maximum structural cruising 144 knots (1978 Model) 
    on use of IAS)   160 knots(1979 Model and on) 
   Never exceed 182 knots 
   Flaps extended    95 knots 
 
  C.G. Range (+40.9) to (+47.0) at 3100 lb. 
   (+35.5) to (+47.0) at 2700 lb. 
   (+33.0) to (+47.0) at 2250 lb. or less 
   Straight line variation between points given. 
 
 Empty Weight C.G.Range None 
 
 *Maximum Weight 3100 lb. 
 
 No. of Seats 4 (2 front at +32.0 to +50.0)   
      (2 rear at +74.0) 
 
 Maximum Baggage 200 lb. (120 lb. at +82.0 to +110.0) 
    (  80 lb. at +110.0 to +134.0) 
 
 Fuel Capacity A) 1978 Model: 
    Standard Range Tanks: 
    61 gal. (75 gal. usable); two 40.0 gal. tanks in wings at +48 
 
    Long Range Tanks: 
    80 gal. (75 gal. usable); two 40.0 gal. tanks in wings at +48 
 
   B) 1979 Model and on: 
    92 gal. (88 gal. usable); two 46.0 gal. integral tanks in wings at +46.5 
 
   See NOTE 1 for data on unusable fuel 
 
 Oil Capacity 9 qt (-15.7) 
 
 Control Surface Movements Wing Flaps   Down 40° + 1°, -2° 
   Elevator tab Up 25° + 2° Down 15° + 1° 
   Ailerons Up 20° + 2° Down 15° + 2° 
   Elevator  
     (relative to stabilizer) Up 28° + 1° Down 17° + 1° 
   Rudder  
     (parallel to 0.00 W.L.)  Right 24° + 1° Left 24° + 1° 
     (perpendicular to hinge line) Right 27°13' + 1° Left 27°13' + 1° 
 
 Serial Numbers Eligible FR18200001 through FR18200070

Rev. 5  5 A42EU 
Data Pertinent To All Models 
 
Datum  Front face of firewall 
 
Leveling means Upper door sill.  Top surface centerline of tailcone (1977 Model) 
   Jig located nutplates and screws on left of tailcone (1978 Model and on) 
 
Certification basis F182 Series 
   Part 3 of the Civil Air Regulations dated November 1, 1949, as amended by 3-1  
   through 3-12 and paragraph 3.112 as amended October 1, 1959. 
 
   In addition effective 1979 Model and on, FAR 23.1559 effective March 1, 1978. 
 
   FAR 36 dated December 1, 1969, plus amendments 36-1 through 36-6 
   (Model F182Q and on). 
 
   FR182 Series 
   Part 3 of the Civil Air Regulations dated November 1, 1949, as amended by 3-1 through  
   3-12 and paragraph 3.112 as amended October 1, 1959; and Sections 23.729, 23.777(e),  
   23.781, 23.1555(e)(1) and (2), and 23.1563 of the Federal Aviation Regulations dated  
   February 1, 1965, as amended February 14, 1975. 
 
   In addition effective 1979 Model and on, FAR 23.1559 effective March 1, 1978  
   FAR 36 dated December 1, 1969, plus amendments 36-1 through 36-6. 
 
   Application for Type Certificate dated June 30, 1976. 
 
   Type Certificate No. A42EU issued June 18, 1976. 
   Equivalent Safety Items: 
 
   F182 Series 
   Airspeed indicator CAR 3.757 (See NOTE 4 for use of IAS) 
   Operating Limitations  CAR 3.778 (a) 
 
   FR182 Series 
   Airspeed Indicator CAR 3.757 (See NOTE 4 for use of IAS) 
   Operating Limitations CAR 3.778 (a) 
   Fuel System CAR 3.430 
 
Equipment The basic required equipment as prescribed in the applicable airworthiness requirements  
   (see Certification Basis) must be installed in the aircraft for certification.   
 
   This equipment must include a current Airplane Flight Manual effective 1979 Model and  
   on.  In addition, the following item of equipment is required: 
 
   Stall warning indicator, Cessna Dwg 0511062 
 
NOTE 1. Current weight and balance report including list of equipment included in certificated empty weight, and  
 locating instructions when necessary, must be provided for each aircraft at the time of original certification.   
 
(a) Models F182P 
 The certificated empty weight and the corresponding center of gravity location must include unusable  
 fuel of 30 lb. at (+46) and undrainable oil of 0 lb.  
 
(b) Models F182Q (1977 and 1978 Models) 
 The certificated empty weight and the corresponding center of gravity location must include unusable  
 fuel of 30 lb. at (+46) and include oil of 22 lb. (-15.0). 
 
(c) Models F182Q (1979 Model and on) 
 The certificated empty weight and the corresponding center of gravity location must include unusable  
 fuel of 24 lb. at (+48) and full oil of 22.5 lb. at (-15.0).

Rev. 5  6 A42EU 
 
Data Pertinent To All Models  (cont’d) 
 
NOTE 1. (cont’d) 
(d) Models FR182 (1978 Model) 
 The certificated empty weight and the corresponding center of gravity location must include unusable  
 fuel of 30 lb. at (+46) and include oil of 16.5 lb.  (-15.7) 
 
(e) Models FR182 (1979 Model and on) 
 The certificated empty weight and the corresponding center of gravity location must include unusable  
 fuel of 24 lb. at (+48) and include oil of 16.9 lb.  (-15.7). 
 
NOTE 2. The following placards must be displayed as indicated: 
 
 A. Applicable to Model F182P 
 
  (1) In full view of the pilot: 
   “This airplane must be operated as a normal category airplane in compliance with the operating 
   limitations as stated in the form of placards, markings and manuals. 
 
        Maximums 
     Maneuvering speed (IAS)   110 knots 
     Gross weight                  2950 lb. 
     Flight load factor            Flaps up    +3.8, -1.52 
           Flaps down +2.0 
 
 No acrobatic maneuvers, including spins, approved.   
 Altitude loss in a stall recovery: 160 ft.   
 Flight into known icing conditions prohibited.   
 This airplane is certified for the following flight operations as of date of original airworthiness certificate:   
 
   (DAY NIGHT VFR IFR) (As applicable)” 
 
 (2) On the fuel selector valve plate: 
  Standard range tanks: "Off.  Left tank level flight only 29 gal.  Both on 
     for landing and takeoff all flight attitudes, 56 gal. 
     Right tank level flight only 29 gal." 
 
  Long range tanks: "Off.  Left tank level flight only 37 gal.  Both on 
    for landing and takeoff all flight attitudes, 75 gal. 
    Right tank level flight only 37 gal." 
 
 (3) On the control lock: 
  "Control lock - remove before starting engine". 
 
 (4) On the baggage door: 
 "Forward of baggage door latch, 120 lb. maximum baggage and/or auxiliary passenger.  Aft of 
baggage door latch, 80 lb. maximum baggage including 25 lb. maximum in baggage wall hat shelf.  
Maximum 200 lb. combined.  For additional loading instructions see weight and balance data". 
 
 (5) On flap control indicator: 
 (a) “0° to 10° - (Blue color code and 140 kts callout; also, mechanical detent at 10°) 
 (b) “10° to 20° - Full (Indices at these positions with white color code and 95 kts callout; also,  
  mechanical detent at 10° and 20°)." 
 
 (6) Forward of the filler cap on the wing surface: 
 Standard range tanks: "Service this airplane with 80/87 minimum aviation grade  
  gasoline.  Capacity 30.5 gal." 
 Long range tanks: "Service this airplane with 80/87 minimum aviation grade 
  gasoline.  Capacity 40.0 gal." 
 
 (7) On aft panel of baggage compartment: 
  "Oxygen refill" (All models with oxygen)

Rev. 5  7 A42EU 
Data Pertinent To All Models  (cont’d) 
 
Note 2: (cont’d) 
 (8) Adjacent to overvoltage light: 
  "High voltage" 
 
 (9) Above the left fuel gauge: 
  "Do not turn off alternator in flight except in emergency" 
 
 B. Applicable to Model F182Q 
 
 (1) In full view of the pilot: 
 
 (a) 1977 and 1978 Models: 
 "This airplane must be operated as a normal category airplane in compliance with the operating 
limitations as stated in the form of placards, markings and manuals. 
 
    Maximums 
   Maneuvering speed (IAS) 111 knots 
   Gross weight   2950 lb. 
    Flight load factor   Flaps up +3.8 -1.52 
      Flaps down +2.0 
 
 No acrobatic maneuvers, including spins, approved.   
 Altitude loss in a stall recovery: 160 ft.   
 Flight into known icing conditions prohibited.   
 This airplane is certified for the following flight operations as of date of original airworthiness 
certificate:   
 
  (DAY NIGHT VFR IFR) (As applicable)” 
 
 (b) 1979 Model and on: 
 "The markings and placards installed in this airplane contain operating limitations which must 
be complied with when operating this airplane in the Normal Category.  Other operating 
limitations which must be complied with when operating this airplane in this category are 
contained in the Pilot's Operating Handbook and FAA approved Airplane Flight Manual. 
 
 No acrobatic maneuvers, including spins, approved.   
 Flight into known icing conditions prohibited.   
 This airplane is certified for the following flight operations as of date of original airworthiness 
certificate:   
 
  (DAY NIGHT VFR IFR) (As applicable)” 
 
 (c) Near airspeed indicator (1979 Model and on): 
 "Maneuver Speed 
        111 KIAS" 
 
 (2) On the fuel selector valve plate: 
 
 (a) 1977 and 1978 Models: 
 Standard range tanks: "Off.   
  Left - 29 gal. Level flight only.  
  Both - 56 gal. All flight attitudes. 
  Both on for takeoff and landing  
  Right - 29 gal.  Level flight only" 
 
 Long range tanks: "Off.   
   Left -  37 gal. Level flight only. 
   Both -  75 gal.  All flight attitudes. 
   Both on for takeoff and landing. 
   Right - 37 gal.  Level flight only"

Rev. 5  8 A42EU 
 
Data Pertinent To All Models (cont’d) 
 
NOTE 2: (cont'd) 
 (b) 1979 Model and on: "Off 
   Left - 44 gal.  Level flight only. 
   Both - 88 gal. All flight attitudes. 
   Both on for takeoff and landing. 
   Right - 44 gal.  Level flight only" 
 
 (3) On the control lock:   
  "Control lock - remove before starting engine" 
 
   (4) On the baggage door: 
  "Forward of baggage door latch, 120 lb. maximum baggage and/or auxiliary passenger.  Aft of 
baggage door latch, 80 lb. maximum baggage including 25 lb. maximum in baggage wall hat shelf.  
Maximum 200 lb. combined.  For additional loading instructions see weight and balance data". 
 
  (5) On flap control indicator: 
 
  (a) “0° to 10° (Blue color code and 140 kts callout; also, mechanical detent at 10°) 
 
   (b) 0° to 20° Full (Indices at these positions with white color code and 95 kts callout; also,  
    mechanical detent at 10° and 20°)." 
 
  (6) Forward of the filler cap on the wing surface: 
 
  (a) 1977 Model 
 Standard range tanks: "Service this airplane with 100/130 minimum aviation grade gasoline. 
     Capacity 30.5 gal." 
 Long range tanks: "Service this airplane with 100/130 minimum aviation grade gasoline. 
    Capacity 40.0 gal." 
 
 (b) 1978 Model 
 Standard range tanks: "Service this airplane with 100LL/100 minimum aviation grade gasoline. 
    Capacity 30.5 gal." 
 Long range tanks: "Service this airplane with 100LL/100 minimum aviation grade gasoline. 
    Capacity 40.0 gal." 
 
 (c) 1979 Model and on 
 "Fuel 100LL/100 minimum grade aviation gasoline.  Capacity 46 U.S. gal., capacity 34.5 U.S. 
gal. to bottom of filler collar." 
 
 (7) On aft panel of baggage compartment:  "Oxygen refill" (All models with oxygen) 
 
 (8) Adjacent to overvoltage light: 
 
 (a) 1977 and 1978 Models 
  "High Voltage" 
 
 (b) 1979 Model and on 
  "Low Voltage" 
 
 C. Applicable to Model FR182 
 
 (1) In full view of the pilot: 
 
 (a) 1978 Model 
 "This airplane must be operated as a normal category airplane in compliance with the operating 
limitations as stated in the form of placards, markings and manuals.

Rev. 5  9 A42EU 
Data Pertinent To All Models (cont’d) 
 
NOTE 2: (cont'd) 
 
   Maximums 
   Gross weight   3100 lb. 
    Flight load factor   Flaps up +3.8 -1.52 
      Flaps down +2.0 
 
 No acrobatic maneuvers, including spins, approved.   
 Altitude loss in a stall recovery: 240 ft.   
 Flight into known icing conditions prohibited.   
 This airplane is certified for the following flight operations as of date of original airworthiness 
certificate:   
 
  (DAY NIGHT VFR IFR) (As applicable)” 
 
 (b) 1979 Model and on: 
 "The markings and placards installed in this airplane contain operating limitations which must 
be complied with when operating this airplane in the Normal Category.  Other operating 
limitations which must be complied with when operating this airplane in this category are 
contained in the Pilot's Operating Handbook and FAA approved Airplane Flight Manual. 
 
 No acrobatic maneuvers, including spins, approved.   
 Flight into known icing conditions prohibited.   
 This airplane is certified for the following flight operations as of date of original airworthiness 
certificate:   
 
  (DAY NIGHT VFR IFR) (As applicable)” 
 
 (c) Near Airspeed Indicator: 
 
 "MAX SPEED - KIAS 
   Maneuver 112 
   Gear Oper. 140 
   Gear Down  140" 
 
 (2) On the fuel selector valve plate: 
 
 (a) 1978 Model: 
 Standard range tanks: "Off.   
  Left - 29 gal. Level flight only  
  Both - 56 gal. All flight attitudes 
  Both on for takeoff and landing  
  Right - 29 gal.  Level flight only" 
 
 Long range tanks: "Off.   
   Left -  37 gal. Level flight only 
   Both -  75 gal.  All flight attitudes 
   Both on for takeoff and landing 
   Right - 37 gal.  Level flight only" 
 
 (b) 1979 Model: "Off 
   Left - 44 gal.  Level flight only 
   Both - 88 gal. All flight attitudes 
   Both on for takeoff and landing 
   Right - 44 gal.  Level flight only" 
  
 (3) On the control lock:   
  "Control lock - remove before starting engine"

Rev. 5  10 A42EU 
 
Data Pertinent To All Models (cont’d) 
 
NOTE 2: (cont'd) 
 
   (4) On the baggage door: 
  "120 Pounds Maximum  
  Baggage and/or auxiliary passenger  
  Forward of baggage door latch and 80 Pounds Maximum  
 
  Baggage aft of baggage door latch 
  Maximum 200 Pounds combined 
 
  For additional loading instructions see Weight and Balance Data" 
 
  (5) On flap control indicator: 
 
  (a) “0° to 10° (Blue color code and 140 kts callout; also, mechanical detent at 10°) 
 
   (b) 0° to 20° Full (Indices at these positions with white color code and 95 kts callout; also,  
    mechanical detent at 10° and 20°)." 
 
  (6) Forward of the filler cap on the wing surface: 
 
  (a) 1978 Model 
 Standard range tanks: "Service this airplane with 100LL/100 minimum aviation grade gasoline. 
     Capacity 30.5 gal." 
 Long range tanks: "Service this airplane with 100L/100 minimum aviation grade gasoline. 
    Capacity 40.0 gal." 
 
 (b) 1979 Model 
 "Fuel 100LL/100 minimum grade aviation gasoline.  Capacity 46 U.S. gal., capacity 34.5 U.S. 
gal. to bottom of filler collar." 
 
 (7) Adjacent to overvoltage light: 
 
 (a) 1978 Model 
  "High Voltage" 
 
 (b) 1979 Model  
  "Low Voltage" 
 
 (8) Near gear hand pump: 
 "Manual Gear Extension 
 1. Select gear down. 
 2. Pull handle fwd. 
 3. Pump vertically 
 CAUTION 
      Do not pump with gear UP selected" 
 
NOTE 3. The cylinder head thermistors must be installed as follows: 
 
    Model Engine and Cylinder Head Number 
     O-470-S O-470-U O-540-J 
    F182P   3  N/A 
    F182Q N/A   3 
    FR182 N/A N/A  5

Rev. 5  11 A42EU 
NOTE 4. The marking of the airspeed indicator with IAS provides an equivalent level of safety to CAR 3.757 when the  
 approved airspeed calibration data presented in Section V of the Pilots' Operating Handbooks, listed below is 
available to the pilot: 
 
 MODEL CESSNA  P/N   MODEL YEAR 
 F182P   D1062-13 1976 Model 
 F182Q   D1087-13 1977 Model 
 F182Q   D1114-13 1978 Model 
 F182Q   D1141-13 1979 Model 
 FR182   D1115-13 1978 Model 
 FR182   D1142-13 1979 Model 
 
NOTE 5. Fourteen Volt Electrical System 
 (F182 Series thru 1977 Model) 
 
 Twenty Eight Volt Electrical System 
 (F182 Series 1978 Model and on) 
 (FR182 Series Model and on) 
 
In addition to the above specified placards, the prescribed operating limitations indicated by an asterisk (*) under Sections I  
through III of this data sheet must be also displayed by permanent markings. 
 
 
---- END ----
```

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- [AD 85-23-07](https://openairdocs.org/ad/85-23-07): Autopilot Systems · Aerostar PA-60-700P (Aerostar 700P), 172L, 172P and 37 more. Effective Jan 27, 1986
- [AD 83-22-06](https://openairdocs.org/ad/83-22-06): Aileron Hinge Pin · Cessna 152, 172N, 172P and 18 more. Effective Nov 8, 1983
- [AD 80-25-07 R1](https://openairdocs.org/ad/80-25-07-R1): Oil Coolers · American Champion 7ECA, 7GCAA, 7GCBC and 39 more. Effective Sep 24, 1981
- [AD 79-25-07](https://openairdocs.org/ad/79-25-07): Alternator Ground · Cessna 180, 180A, 180B and 95 more. Effective Dec 13, 1979
- [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

## STCs approved under this data sheet (138, 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 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 SA04439NY](https://openairdocs.org/stc/SA04439NY): Installation of an X cam Pod. J & C Engineering Services LTD
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc.
- [STC 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 SA12276IB](https://openairdocs.org/stc/SA12276IB): Payload System Installation. Icarus Aero Inc.
- [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 SA01330LA](https://openairdocs.org/stc/SA01330LA): Installation of alternate avionics support assembly.. Radiorax Aviation Systems LLC
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd.
- [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics
- [STC SA00622DE](https://openairdocs.org/stc/SA00622DE): Installation of John Deere AGRI Services, Inc. JD3 Aerial Imaging System,. Aeroptic LLC
- [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation
- [STC 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 SA04353CH](https://openairdocs.org/stc/SA04353CH): Installation of Hartzell propeller model DHC-G2YF-1BFP/F8068+2 and applicable spinner. Hartzell Propeller Inc.
- [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc.
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio.. Peregrine
- [STC SA01435LA](https://openairdocs.org/stc/SA01435LA): Installation of engines modified with Firewall Forward Technologies LLC modified camshaft. Centri-Lube Technologies LLC
- [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 SA2422CE](https://openairdocs.org/stc/SA2422CE): Installation of wing leading edge cuffs, drooped tips, stall panels, and aileron gap seals.. Curry Aviation LLC
- [STC SA02734LA](https://openairdocs.org/stc/SA02734LA): Installation of Airfilm Wing Strut Utility Mount. Airfilm Camera Systems
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc.
- [STC SA04231CH](https://openairdocs.org/stc/SA04231CH): Installation and activation of a TruTrak Vizion autopilot system. Honeywell International Inc.
- [STC SA00026IB](https://openairdocs.org/stc/SA00026IB): Validation for the Installation of Beringer Wheels, axles, brake and master-cylinders. Beringer Aero
- [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 SA220SO](https://openairdocs.org/stc/SA220SO): Tow bar, release mechanism, and safety tow link.. Fliegen Works Inc. 
      d/b/a Pacific Aerial Tow Hooks
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA04182NY](https://openairdocs.org/stc/SA04182NY): Installation of BendixKing KA 310 Autopilot Adapter. Honeywell International Inc
- [STC SA01999CH](https://openairdocs.org/stc/SA01999CH): Install BRS-182 parachute recovery system.. Ballistic Recovery Systems Inc.
- [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA1783CE-D](https://openairdocs.org/stc/SA1783CE-D): Install KAP 100 single axis, KAP 150 two axis, or KFC150 two axis flight control system and optional KAS 297B vertical speed and altitude selector.. Honeywell International Inc
- [STC SA1794CE-D](https://openairdocs.org/stc/SA1794CE-D): Install KAP 100 single axis, KAP 150 two axis, or KFC 150 two axis flight control system and optional KAS 297B vertical speed and altitude selector.. 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 SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [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 SA04287NY](https://openairdocs.org/stc/SA04287NY): Provisions for the installation of a wing strut mounted camera pod. Wooding Geospatial Solutions
- [STC SA01435SE](https://openairdocs.org/stc/SA01435SE): Installation of J.P. Instruments (JPI) Primary Engine Data Management System. J. P. Instruments
- [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc.
- [STC SA02503AK](https://openairdocs.org/stc/SA02503AK): Installation of AMSAFE State of the Art Restraint System (SOARS) inflatable restraints. AMSAFE Inc.

All 138: https://openairdocs.org/tcds/A42EU/stcs.md

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