Weight & Balance for Cessna 185
CESSNA 185 · Weight And Balance
Overview
This document provides essential weight and balance information specifically for the Cessna 185. It is intended for pilots and aviation enthusiasts who need to understand the loading limits and balance requirements for safe operation of the aircraft. The document outlines the basic empty weight, maximum takeoff weight, and other critical parameters necessary for calculating weight and balance before flight. It serves as a reference to ensure compliance with safety regulations and to optimize aircraft performance during operations.
- Basic empty weight of the Cessna 185 is essential for weight calculations.
- Maximum takeoff weight must not be exceeded for safe operations.
- Center of gravity limits are critical for stability during flight.
- Follow detailed procedures for accurate weight and balance calculations.
- Adhere to loading guidelines to maintain proper weight distribution.
Document
Source
Originally published by www.mennen.org. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Weight And Balance
- Pages
- 27
- File size
- 1.0 MB
- Publisher
- www.mennen.org
Specifications & performance
Extracted from this document.
Specifications
- Engine (hp)
- 450
- Propeller
- McCauley D2A34C58/90AT-8
- Engine model
- Continental IO-520-D
- Empty weight (lb)
- 1,677
- Fuel capacity (gal)
- 62
- Max takeoff weight (lb)
- 3,350
Weight & balance
- Useful load (lb)
- 1,673
- Basic empty weight (lb)
- 1,677
- Max takeoff weight (lb)
- 3,350
Common. Rarer than 1% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the CESSNA 185.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Basic Empty Weight
The basic empty weight of the Cessna 185 is crucial for calculating the weight and balance. This weight includes the airframe, engine, and all standard equipment, but excludes any cargo, passengers, or fuel.
Maximum Takeoff Weight
The maximum takeoff weight for the Cessna 185 is defined to ensure safe flight operations. Exceeding this weight can compromise aircraft performance and safety.
Center of Gravity Limits
The document specifies the center of gravity (CG) limits for the Cessna 185, which are critical for maintaining stability and control during flight. Proper loading within these limits is essential.
Weight Calculation Procedures
Detailed procedures for calculating the total weight and determining the center of gravity are provided. This section includes formulas and examples to assist pilots in ensuring their aircraft is within safe operating limits.
Loading Guidelines
Guidelines for loading passengers, cargo, and fuel are outlined to help pilots distribute weight appropriately and maintain balance.
Safety notes
- Exceeding maximum takeoff weight can lead to performance issues.
- Improper weight distribution can affect aircraft stability.
Full document text
Weighing Procedure Datum (Firewall, front face) Sta. 0.0 25.9". MAC 58.8" A= ✗ Level at Upper Door Sill B= Scale Position Scale Reading Left Wheel Right Wheel Tail Wheel Aircraft Empty Weight (As Weighed) B (C to C) MODEL A185F 1973 Tare Symbol Net Weight L R T W X = ARM = (A) + (T) × (B) ; x = ( ) + ( ) x ( ) = ( ) IN. W 1. Preparation: a. b. Inflate tires to recommended operating pressures. Remove all wing tank and accumulator tank drain plugs to remove all fuel. b. c. Remove oil sump drain plug to drain all oil. d. Move all sliding seats to most forward position. All seat backs should be in the most nearly vertical position. = Obtain licensed empty weight by adding weight and moment of unusable fuel to the airplane empty weight and moment. There are 3 gallons of unusable fuel (weight 18#; moment = 828 lb in.) in airplanes having an "ON-OFF" fuel system and 6 gallons of unusable fuel (weight = 36%%; moment = 1656 lb in.) in airplanes having a "SELECTOR VALVE" fuel system. e. Put flaps in the fully retracted position. 2. f. Leveling: a. Place all control surfaces in neutral position. Place scales under each main wheel (1000% minimum capacity for scales.) Place screw jack on 500# minimum capacity scale and place under tailwheel. 3300 3200 Adjust screw jack on scale to center bubble on level. (See diagram.) 3100 b. Weighing: 3. a. With the airplane level and brakes released, record the weight shown on each scale. Deduct the tare, if any, from each reading. Measuring: 4. a. 5. b. C. Obtain measurement "A" by measuring horizontally (along airplane center line) from a line stretched between the main wheel centers (determined from the axle attaching bolt pattern on the inner face of the landing gear spring) to a plumb bob dropped from the firewall. Obtain measurement "B" by measuring horizontally (parallel to airplane center line) from the line stretched between main wheel centers (determined from the axle attaching bolt pattern on the inner face of the landing gear spring) to a plumb bob dropped from the center of the tailwheel, left side. Repeat on right side and average measurements. When Cessna Castering Gear is installed add 0.7" to mea- surement "A" and subtract 0.7" from measurement "B". Completing the Form: a. Using weights from (3) and measurements from (4), the airplane weight and C. G. can be determined. AIRCRAFT WEIGHT - POUNDS 3000 2900 2800 2700 2600 2500 2400 2300 2200 2100 2000 1900 1800 33 34 FLOATPLANE WITH EDO MODEL 628-2960 FLOATS AMPHIBIAN WITH EDO MODEL 597-2790 FLOATS CENTER OF GRAVITY LIMITS NORMAL CATEGORY LANDPLANE FLOATPLANE AMPHIBIAN AMPHIBIAN* 35 36 37 38 39 40 41 42 43 44 45 46 47 C. G. LOCATION-INCHES AFT OF DATUM (STA. 0. 0 FIREWALL) *NOTE: Amphibian wheels-down take-off only Form Issue Date: 2 October 1972 Revised: 20 October 1972 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS MODEL A185F 1973 Loading and Center of Gravity Charts IT IS THE RESPONSIBILITY OF THE PILOT AND AIRCRAFT OWNER TO ENSURE THAT THE AIRCRAFT IS LOADED PROPERLY When computing aircraft loading requirements, refer to the Weight and Balance and Installed Equipment Data sheet in the aircraft file for the licensed empty weight, arm and moment of the aircraft as delivered from the factory. (If alterations have been made to the aircraft, refer to FAA form 337 for the latest empty weight, arm and moment.) The aircraft weight and balance may then be determined using the Loading Graph and Center of Gravity Moment Envelope as indicated in the Sample Loading Problem below. SAMPLE AIRPLANE YOUR AIRPLANE 600 SAMPLE LOADING PROBLEM Weight (lbs.) Moment (lb.-ins. 1000) Weight Moment (lbs.) lb.-ins. 550 LOADING GRAPH -10001 500 1. Licensed Empty Weight (Sample Airplanel 1677 60.3 2 Oil (The weight of full oil may be used for all calculations): No Oil Filter: 12 Qts. 22 Lbs -0.4 Moment/1000 22 -0.4 With Opt. Oil Filter: 13 Qts. 24 Lbs @-0.4 Moment./ 1000 3. Fuel (Standard Max. 62 Gal. 6 Lbs/Gal.) 372 17.9 Fuel (Long Range Max. 78 Gal. 6 Lbs/Gal.) 4. Pilot and Copilot (Sta. 36 to 50) 170 6.5 5. 2nd Row Passengers On Individual Seats 2nd Row Passengers On Bench Seat 3rd Row Passengers (120 Lbs Max. If Child's Seat) 6. *Cargo "A" (Sta. 10 to 50) *Cargo "B" (Sta. 50 to 90) *Cargo "C" (Sta. 90 to 108) Baggage Area (Sta. 82 to 108, 120 Lbs. Max.) བྷg 300 9.0 750 54.8 59 5.8 Baggage Area 2 (Sta. 108 to 140, 50 Lbs. Max.) Cargo Pack (Sta. 5 to 115, 300 Lbs Max.) 7. TOTAL WEIGHT AND MOMENT 3350 153.9 8. Locate this point (3350 at 153. 9) on the Center of Gravity Moment Envelope, and since this point falls within the envelope, the loading is acceptable. *Maximum allowable cargo loads will be determined by the type and number of tie-downs used, as well as by the airplane weight and C.G. limitations. Floor loading must not exceed 200 lbs per square foot. LOADING ARRANGEMENTS *Arms measured to the center of the areas shown. **Pilot or passenger center of gravity on adjustable seats positioned for average occupant. Numbers in parentheses indicate forward and alt limits of occupant center of gravity range. NOTE: Station 108 or 140 can be used as a convenient interior reference point for determining the location of baggage area fuselage stations. C.G. ARM * 30. **38- (36 to 50) CARGO OPT CARGO PACK CARGO CARGO BAGGAGE 8° AREA 2-1 STA. 0 10 50 90 108 140 **38. CO **38 PILOT PILOT PILOT PILOT CO- PILOT (36 to 50) (36 to 50) **38- 136 to 501 PILOT CO- PHOT LOAD WEIGHT (POUNDS) 450 450 400 350 300 250 200 ཱ ༔ ༔ ༔ ༔ ? 150 100 SPIL LOT & COP FUEL (6 LB. GAL. BAGGAGE AREA CA I 50 0 BAGGAGE AREA 2 0 10 15 62 GAL 78 GAL 2ND ROW PASSENGERS ON INDIVIDUAL CARCO 2ND ROW PASSENGERS ON BENCH SEAT 20 RGO 25 3RD ROW PASSENGERS 30 35 40 LOAD MOMENT/1000 (POUND INCHES) NOTES: (1) Line representing adjustable seats shows the pilot or passengers center of gravity on adjustable seats positioned for an average occupant. Refer to the Loading Arrangements diagram for forward and aft limits of occupant c.g. range.
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(2) Engine Oil: No Oil Filter; 12 Qts. 22 Lbs. at -0.4 Moment/1000. With Opt. Oil Filter: 13 Qts. 24 Lbs. at -0.4 Moment/1000. LOADED AIRCRAFT WEIGHT - (POUNDS) 3300 CENTER OF GRAVITY 3200 MOMENT ENVELOPE 3100 FLOATPLANE WITH EDO 3000 2900 2800 2700 2600 2500 2400 2300 2200 2100 65 *70 B *70. 2ND ROW PASS 2000 2ND ROW B 73 82 PASS 1900 GRD ROW BAGGAGE *99. 108 C *99. 108 97 108 *95 PASS AREA 108 1800 BAGGAGE BAGGAGE 123 *123 *123 AREA 2 AREA 2 BAGGAGE AREA 2 BAGGAGE *123 AREA 2 1700 50 140 140 140 140 1. 11. III. IV. AMPHIBIAN WITH EDO MODEL 597-2790 FLOATS LANDPLANE FLOATPLANE AMPHIBIAN AMPHIBIAN" 80 90 140 130 150 60 70 100 110 120 LOADED AIRCRAFT MOMENT/1000-(POUND-INCHES) *NOTE: Amphibian wheels-down take-off only Form Issue Date: 2 October 1972 Revised: 20 October 1972 Cessna EQUIPMENT LIST CESSNA AIRCRAFT CO MODEL A185F (1973) NOTES WICHITA, KANSAS 2. 3. 4. * Suffix letter to item numbers: -R = Required items of equipment for FAA certification -S = standard equipment items -0 = optional equipment items replacing required or standard items -A = optional equipment items which are in addition to required or standard items Refer to the sheet titled "Weight and Balance and Installed Equipment Data" for a listing of equipment installed on your aircraft at the factory. Unless otherwise indicated, true values (not net change values) for weight and arm are shown. Positive arms are distances aft of datum; negative arms are distances forward of datum (see "Weighing Procedures" sheet for datum location). A separate FAA approval must be obtained if the following items are not installed per applicable Cessna drawings or accessory kit instructions. Complete assembly installations are indicated by asterisks after the item weight and arm. Some major components of the assembly are listed on the lines immediately following. The summation of these major components does not necessarily equal the complete assembly installation. ITEM NO 001-R 002-R 002-0 003-R 004-R DESCRIPTION Engine, Continental IO-520-D Spec 23 Two Magnetos With Impulse Coupling Oil Cooler Mounting Provisions Oil Cooler Twelve 18 mm x 3/4 20-3A Spark Plugs Starter, 12 Volt Prestolite MCL 6501 Propeller, McCauley D2A34C58/90AT-8) Propeller, Floatplane (McCauley D2A34C58/90AT-4) Spinner, Propeller REF DRAWING WT LBS ARM INS 0750227 Slick 662 450.0* -17.0* 12.9 -12.5 EQ 5968 2.3 -31.5 TCM 5.3 -31.5 SL 350 3.0 19.0 TCM 634592 17.8 -4.0 C161004-0106 55.3 -40.2 C161004-0107 55.5 -40.2 0752040 4.0 -39.5 Governor, Propeller (McCauley C290-D2/T9) C161030-0107 3.0 -32.0 (Woodward A210462) (Edo-Aire 34-828-01-1)| C161040-0107 3.0 -32.0 3.0 -32.0 005-R 006-R Filter, Engine Induction Air Muffler Assembly, Including Heat Jacket for Cabin & Induction Air 0750038 1.0 -33.0 0750161 18.0 -15.5 007-0 Oil Cooler, Non-Congealing Modine TCM 639171 2.3 -31.5 Replaces Item 001-R Oil Cooler and changes engine designation to 10-520-D Spec. 24 (Net Change) ISSUED: 20 Sept. 172 REVISED 25 not. '72 APPROVED: C = 24 Oct FORM NO. 60-2123=3 Nov. 172. APPROVED Cessna Aircraft Co Fawnee Div. Delegation Option Manufacturer, CE-1 Cmates Executive Engineer 104-77 08 Date DICTE 73 (Page 2, 3, 4 Retyped) -3.38 SHT1 OF 11 Cessna. CESSNA AIRCRAFT CO EQUIPMENT LIST (CONT'D) MODEL A185F (1973) WICHITA, KANSAS ITEM NO DESCRIPTION REF DRAWING WT LBS ARM INS 010-R Tachometer, Recording C668020-0107 1.5 14.0 011-R Gage, Manifold Pressure & Fuel Flow C662037-0103 1.1 15.5 012-R Gage, Engine Cluster C669502-0202 1.3 13.5 013-R 014-R 015-R Alternator, 60 Amp, 14-Volt (C611501-0102) 1250212 Regulator, Alternator, 60 Amp, 14-Volt Battery, 12-Volt, 33 Amp Hour 11.5 -3.5 0611001-0101 1.0 -1.0 0712605 28.0 114.0 016-R 017-R 017-0 017-0-1 018-R 020-R Indicator, Stall Warning Audible Instl. Altimeter Altimeter, Sensitive Altimeter, Sensitive (Feet & Millibars) Compass, Magnetic Wheel, Tire, Tube and Brake Assy. 6.00x6 6-Ply (Main) (Two) 0700185 0.5 27.0 C661012-0101 0.8 15.5 C661071-0101 1.0 15.0 C661071-0102 1.0 15.0 0413517-14 0.5 16.0 0741025-9,-10 39.0% 21.2* 1241156-105 Wheel Assy (Cleveland 40-75B) C163001-0301 6.2 21.6 Tire C262003-0204 8.7 21.6 Tube C262023-0102 1.8 21.6 - 020-0-1 Brake Assy L.H. (Cleveland 30-52) Brake Assy R.H. (Cleveland 30-52) Wheel, Tire, Tube & Brake Assy. C163030-0303 2.8 18.9 C163030-0304 2.8 18.9 0741025-9,-10 40.2* 26.2* 6.00x6 6-Ply (Main) (Two) Wheel Assy (McCauley) (D30063-1) Tire C163016B0111 C163002-0102 6.5 21.6 C262003-0204 8.7 21.6 Tube C262023-0102 1.9 21.6 Brake Assy - 020-0-2 - L.H. (McCauley) (D30118-1) Brake Assy R.H. (McCauley) (D30118-2) Wheel, Tire, Tube and Brake Assy. 8.00x6 6-Ply (Main) (Two) Wheel Assy (Cleveland 40-75D) Tire Tube C163032-0201 3.0 18.9 C163032-0202 3.0 18.9 0741025-11,-12 43.2* 21.3* C163001-0302 6.2 21.6 C262003-0207 10.7 21.6 C262023-0104 1.9 21.6 Brake Assy - 020-0-3 Brake Assy - Wheel, Tire, Tube and Brake Assy. 8.00x6 6-Ply (Main) (Two) Wheel Assy (McCauley) Tire Tube L.H. (Cleveland 30-52N) R.H. (Cleveland 30-52N) C163030-0313 2.8 18.9 C163030-0314 2.8 18.9 0741025-11,-12 44.2* 21.2* C163016B0113 C163002-0104 6.5 21.6 C262003-0207 10.7 21.6 C262023-0104 1.9 21.6 Brake Assy - L.H. (McCauley) (D30118-1) C163032-0201 3.0 18.9 Brake Assy - R.H. (McCauley) (D30118-2) C163032-0202 3.0 18.9 021-R Wheel and Tire Assy (One) 0742147-8 4.5 260.0 8.00 Pneumatic Type Tail 021-0 Wheel and Tire Assy (One) (Net Change) 10.00 Pneumatic Type Tail 0742147-9 2.0 263.3 030-R Seat, Pilot 030-0-1 031-R Seat, Pilot Vertical Adjusting Belt, Safety Pilot 032-S Shoulder Harness Assy - Pilot 1200605-40 13.0 44.0 0515001 21.0 41.5 S-2070-103 1.0 37.0 S-2070-201 1.0 37.0 ISSUED: 20 Sept '73 REVISED: 24 Oct. 1'73 = C; Retyped 24 Oct. 173 SHT 2 OF 11 FORM NO. 80-223 ດ Cessna. CESSNA AIRCRAFT CO EQUIPMENT LIST (CONTD MODEL A185F (1973) WICHITA, KANSAS ITEM NO DESCRIPTION 033-R Light, Omni-Flashing Beacon REF DRAWING WT LBS ARM INS 0731001 1.7* 192.2* Light Assy (on Fin Tip) Flasher Assy C621001-0103 0.4 216.5 C594502-0101 0.7 217.2 034-S Landing Light, Cowl Mounted 0752031 1.6* -25.3* Light Bulbs (Each) GE 4509 0.5 -32.5 035-R Indicator, Airspeed C661060-0204 0.7 16.0 036-0 Indicator, True Airspeed 0713842 0.8 16.4 037-R Pump, Fuel, Electric 0716117 2.0 -3.5 038-S 038-0 Paint Scheme, Std Stripe (15785 sq.in.) Paint Scheme, Overall Cover 0704020 2.4 114.8 0704020 11.1* 95.2* Overall Base Cover (102282 sq.in.) Accent Stripe (15785 sq.in.) 8.9 90.3 2.2 114.8 038-0-1 Paint Scheme, AgCarryall 0704021 12.1* 95.9* 039-S 040-S AgCarryall Stripe (22834 sq.in.) Baggage Net, Retaining (Set of 2) 3.2 111.3 2015009-3 1.2 124.0 A Electrical Bus Bar and Relay |0700294 0.3* 16.0* 041-S Relay, Electronic Disconnect Overvolt Warning System Overvolt Sensor Warning Light S-1917-1 0.3 16.0 0700294 0.2* 15.0* C5921001-0101 0.2 15.0 S-2135-1 0.0 17.0 050-R Placard, Operation Limitation Landplane, 050-0 Floatplane, and Amphibian VFR Day-Night Placard, Operation Limitation - Landplane, Floatplane, and Amphibian IFR 1205001-160 0.0 1205001-161 0.0 200-A V-Brace, Floatplane Cowl Deck 0713878 2.7 25.0 B 201-A Cables, Corrosion Resistant (Net Change) 0700082 0.0 202-A Cargo Pack, External Belly Mounted 0700067 37.0 60.5 203-A Clock, Installation, Electric 0700117-1 0.7* 48.5* Clock C664508-0101 0.3 17.0 204-A Controls, Dual (Stowable Pedals) 0760000 5.5 14.0 205-A Corrosion Proofing, Internal 0700082 7.0 72.0 206-A Detector Instl. Navigation Light (Set of 2)0701013 0.0 207-A Door Installation, Stretcher 0712013 4.8 119.1 208-A Control Wheel All Purpose (Net Change) 0.0 210-A Filler Cap, Inboard Fuel Instl. (Set of 2) 0721303 2.0 41.5 (Used With 261-A Long Range Tanks) 211-A Filter, Full Flow Engine Oil 0756025 4.5 -4.0 Engine Adaptor 1250922-2 2.0 Filter Element C294505-0102 0.3 212-A Fire Extinguisher 0701014 3.0 35.0 213-A Fuel Selector Valve - - 3 Position 0716116 1.4 42.0 214-A 215-A Gage, Outside Air Temperature Ground Service Plug, Landplane 0701010 0.1 28.5 0700170 2.6 -1.9 216-A 216-A-1 215-A-1 Ground Service Plug, Floatplane Gyros, Horizon and Directional, New ros, Horizon and Cessna Directio (Use with Nav-0-Matic 300) 0712011 2.5 111.0 0706001 6.1 13.5 New 0701005-4 6.8 12,7 ISSUED: 20 Sept. 172 REVISED: A=25 Oct 172; B=3 173: Retsped 24 Oct 17. OF FORM NO. 60-223 Cessna. CESSNA AIRCRAFT CO ITEM NO EQUIPMENT LIST MODEL A185F (1973) (CONT'D) WICHITA, KANSAS DESCRIPTION REF DRAWING WT LBS ARM INS D 220-A 221-A 222-A 223-A Headrests, 1st Row Seats (Two Installed) Headrests, 2nd Row Seats (Two Installed) Hourmeter, Engine Time, Hydraulic Actuated Indicator Heating System, Pitot and Stall Warning (Net Change) 0514048-1 1.8 46.0 0514048-1 1.8 86.0 0700331 0.8* 11.6* C664501-0103 0.5 16.5 0713970 0.5 26.5 224-A Indicator, Economy Mixture 0700141 1.0 6.0 225-A 226-A Indicator, Vertical Speed Indicator, Turn Coordinator C661080-0101 0.9 15.0 0770111 1.3 15.7 226-0 Indicator, Turn and Bank S-1413N2 2.0 15.0 226-0-1 Indicator, Turn Coordinator (for use with Item 500-A) (ARC) 1.9 14.5 227-A 228-A 229-A 230-A Light Instl. Under Wing Courtesy (Set of 2) 0700615 Light, Map (Control Wheel Mounted) Light, Map & Inst. Flood (L.H. Doorpost) Strobe Light Installation 0.5 61.9 1570149 0.1 22.5 0700149 0.5 30.5 Wing Mounted 0701037 2.6* 44.4* Power Supply (Each Tip Rib Light and Lens Assys (2) - Wing) (2) C622007-0101 2.3 46.7 C622006-0101 0.3 42.0 240-A 241-A 242-A 243-A 244-A 245-A Priming System - 2 Point 246-A 247-A 250-A Oil Quick Drain Valve (Net Change) Oil Drain System, Remote (Net Change) Oil Dilution System Oxygen System, 48 ft³ Capacity, Oxygen Bottle (Empty) 48 ft3 (1800 psi) Oxygen @ 0.0832 lb/ft³ Oxygen Masks Stowed (Set of 6) Photographic Provisions 1256011 0.0 1656002 1.0 -3.0 0756017 2.0 -1.0 6-Port 0710640 34.5* 105.0* C166001-0601 22.4 112.0 4.0 112.0 1.5 14.0 0710001 10.5 82.0 0716134 1.0 10.0 Rings, Airplane Hoisting Rings, Cargo Tie-Down (Set of 6) Spray Tank & Pump Instl., Belly Mounted Sorensen 151 Gallon Capacity Tank Tank Attach Straps & Release Mechanism Sorensen Spray Pump, Valve & Mount Assy Sorensen 6 Blade 15 Inch Pump Fan Fairings, Tank Nose (Set of 2) Spray Controls & Cables, Window Mounted Misc. Attachments, Clamps & Hoses 0700612 1.0 49.1 1201039 1.5 94.0 0700222-1 143.6* 50.8* 24-95A 82.5 68.3 24-11, 24-96 7.2 66.7 4000, 6-30 32.5 17.8 7-10 3.5 6.4 24-62 2.3 19.0 24-61 12.1 32.5 3.6 38.6 251-A Spray Boom Instl., Wing Mounted 0709101-1 36.3* 41.8* Streamlined Spray Booms (Set of 4) Spray Nozzles (Set of 30) 24-24-1, -2 19.8 43.0 TeeJet 8355 7.2 40.0 Boom to Wing & Strut Braces (Set of 6) Wing Clamp Bands (Set of 4) 24-12, 24-15 3.4 43.0 24-18, 24-19 2.5 48.0 Misc. Strut Clamps, Plugs & Connectors 3.5 32.6 NOTE: Normal Category operations are prohibited when Item 251-A Wing Mounted Spray Booms are installed. 252-A -253-A Stabilizer Abrasion Boots (Set of 2) Static Discharger (Set of 7) 0500041 1.5 206.0 0700160-2 0.0 254-A Static Source, Alternate 0701032-1 0.3 13.7 255-A 256-A Step & Handle, Refueling Assist (Set of 2) Stretcher (Boxed) (Portable) 0700131-1 1.6 16.6 0700164 (Use actual weigh 257-A Sun Visors (Two) 0500040 0.8 ISSUED: 20 Sept. '72 REVISED: Page Revised 24 Oct. 173 and arm change) SHT 4 OF 11 32.8 FORM NO. 80-223 Cessna ITEM NO D CESSNA AIRCRAFT CO EQUIPMENT LIST (CONT'D) MODEL A185F (1973) WICHITA, KANSAS DESCRIPTION REF DRAWING WT LBS ARM INS 260-A Vacuum System (Engine-Driven) 0706001 6.2 -1.4 261-A Wings, Extended Range 84 Gallon Capacity, 0720015 7.0 46.5 262-A Requires Item 213-A Fuel Selector (Set of 2 Net Change) Winterization Kit (FK-85-98) 0700329-2 1.2* -30.2* Front Covers, Installed Arm Shown 0.7 -35.0 263-A Wing Leveler Partial Instl. (for complete 0701009 system see Item 402-A) 3.7* 36.4* Wing Servo (2) 1.3 51.8 264-A 265-A 266-A Misc. Hardware & Bellcrank Changes Windshield, Tinted, Net Change Wire Cutter, Main Gear (Set of 2) Wire Cutter, Windshield 2.4 28.1 0700183 0.0 - 0713963 4.0 20.0 0713963 0.8 18.9 267-A 268-A Cable Deflector, Cabin Top to Fin Shelf, Utility (With 2nd Row Bench Seat) 0713963 1.1 177.1 0513013 2.0 98.0 271-A Float Installation, Edo Model 628-2960 (This item is in addition to Items 002-0, 200-A, 255-A, 273-A, and replaces 020-R and 021-R) 272-A Float Installation, Amphibian, Edo 273-A Model 597-2790 (This item is in addi- tion to Items 002-0, 200-A, 255-A, 273-A. and replaces Items 020-R and 021-R.) Floatplane Fittings, Cessna Partial (Structural Reinforcement) 274-A Ski Installation - Wheel Replacement (Replaces Item 020-R) (Flui-Dyne) Main Ski Model A3500A, Tail Ski, Model CT3200 275-A Wheel Ski Installation, Hydraulically Actuated (Flui-Dyne) Main Ski Model C3200, Tail Ski Model CT3200 (Item 020-R required) 276-A 277-A 55770 (Edo) (Use actual weight and arm change) 42090 (Edo) (Use actual weight and arm change) 0710010 18.5 57.0 11G1561 (Flui-Dyne) 11G1560 (Flui-Dyne) (Flui-Dyne) Wheel Ski Installation, Manually Actuated |11G1562 (Flui-Dyne) Main Ski Model C-3200, Tail Ski Model CT3200 (Item 020-R required) Wheel Ski Installation, Hydraulically Actuated (Flui-Dyne) Main Ski Model C3600, Tail Ski Model CT3200 (Item 020-0 required) 11G1550 (Flui-Dyne) ISSUED: 20 Sept. 172 REVISED: FORM NO. 80-223 (Use actual weight and arm change) (Use actual weight and arm change) (Use actual weight and arm change) (Use actual weight and arm change) SHT 5 OF 11 CessnaⓇ CESSNA AIRCRAFT CO ITEM NO EQUIPMENT LIST (CONT'D) MODEL A185F (1973) WICHITA, KANSAS DESCRIPTION REF DRAWING WT LBS ARM INS D 280-A 280-A-1 281-A 281-A-1 282-A 282-A-1 284-A 285-A 285-A-1 Seat, Adjustable Fore and Aft Co-Pilot Seat, Articulating Vertical Adj. Co-Pilot Seat Assy, 2nd Row 2-Place Bench Seat Assys, 2nd Row Individual Stowable (Set of 2) Seat Assy, 3rd Row 2-Place Bench Seat Assy, 3rd Row Foldaway Child Belt & Shoulder Harness Assy, Co-Pilot Belt, 2nd Row Lap (Set of 2) 1200605 13.0 4420 0515001 21.0 41.5 0715018 21.0 72.0 0711703 19.0 72.0 0711097 5.0 100.0 0501009-4 7.6 101.5 S-2070-3 2.0 37.0 S-1746-27 2.0 73.0 Belt & Shoulder Harness Assy, 2nd Row (Set of 2) S-2070-2 4.0 73.0 286-A 286-A-1 Belt, 3rd Row Lap (Set of 2) S-1746-6 2.0 97.0 Belt & Shoulder Harness Assy, 3rd Row (Set of 2) S-2070-15 4.0 97.0 286-A-2 Belt, 3rd Row Lap (for Foldaway Child Seat Item 282-A-1) S-1746-5 0.9 97.0 NOTE: The installation weight per individual seat or belt assembly is shown above. See also Items 030-R through 032-S for pilot seats and belts. For complete seating installation, include one seat belt (or seat belt and shoulder harness assembly) for each occupant for whom seating is installed. See examples below. (Item 400-A through Item 400-A-3 Typical Seating Arrangements) Several com- binations of seating utilizing 1st Row Non-Vertical Adjusting seats and Lap Belts only in 2nd and 3rd rows are listed. 290-A 291-A Aileron-Rudder Interconnect (stowed) (Floatplane) (Installed arm shown) Rudder Centering Spring Instl. (stowed) (Floatplane) (Installed arm shown) 0742001 1.1 77.1 A 0742004-1 0.5 181.9 A 292-A Ventral Fin (Stowed) (Floatplane) 0712674-1 1.8 206.0 A (Installed Arm Shown) 400-A 400-A-1 Seating Arrangements, Typical (Net Change) 2-Place Pilot & Co-Pilot 15.0 43.1 4-Place 2nd Row 2 Place Bench Seat 38.0 60.6 400-A-2 6-Place 2nd Row Individual Stowable & 44.5 67.8 3rd Row Foldaway Child Seat 400-A-3 6-Place 2nd Row Individual Stowable & 3rd Row 2-Place Bench Seat 43.0 66.4 401-A Primary Group (FK-85-37E) 4.5* 24.7% 017-0 Sensitive Altimeter 1.0 15.0 017-R 203-A Standard Altimeter (delete) Clock -0.8 15.5 0.7 48.5 214-A OAT Gage 0.1 28.5 225-A Vertical Speed Indicator 0.9 15.0 229-A Map Light - Door Post Mounted 0.5 22.5 257-A Sun Visors 226-A Turn Coordinator 0.8 33.0 1.3 15.7 ISSUED: 20 Sept. '72 REVISED: 25 Oct. '72 =A SHT 6 OF 11 FORM NO. 80-223 CessnaⓇ CESSNA AIRCRAFT CO ITEM NO EQUIPMENT LIST (CONT'D) MODEL A185E (1973) WICHITA, KANSAS DESCRIPTION REF DRAWING WT LBS ARM INS 401-A-1 Primary Group - 402-A for use with 300 Nav-0- Matic of Wing Leveler (FK-85-37F) 400-A Standard Primary Group 226-A Turn Coordinator (delete) Wing Leveler Installation (FK-85-129B) 263-A Partial Installation 3.2* 28.4* A 4.5 24.7 -1.3 15.7 0701009 13.0* 13.3* A 3.7 36.4 403-A 002-0 Propeller - Net Change 200-A Cowl Deck V-Brace 201-A Corrosion Resistant Cables 205-A Corrosion Proofing - Internal 213-A Fuel Tank Selector Valve 246-A Hoisting Rings, Airplane 255-A Refueling Step and Handle 273-A 290-A Aileron-Rudder Interconnect 291-A Rudder Centering Springs Turn Coordinator 260-A Vacuum System Floatplane Kit, Std. Tanks (FK-85-18N) 2.8 14.9 6.2 -1.4 0742000 36.3* 63.5* A 0.2 -40.2 2.7 25.0 B 0.0 7.0 72.0 1.4 42.0 1.0 49.1 1.6 16.6 Floatplane Fuselage Reinforcements 18.5 57.0 1.1 77.1 A 0.5 181.9 A 403-A-1 404-A - 292-A Ventral Fin Floatplane Kit, Long Range Tanks (FK-85-18PD 24 Volt Electrical System (Major Components Listed) Add: Alternator 28V, 60 Amp Prestolite MHJ4002 Starter Battery 24V Alternator Output Regulator 1.8 206.0 A 38.3 62.4 B - Net Change 0770077 0.6* 304.3* C611503-0101 10.7 -3.5 16.5 -4.0 0870060 27.9 114.0 C611002-0102 0.7 -0.5 Overvolt Sensor System 0.6 0.9 Battery Box - Net Change 0.4 114.0 Delete: 405-A of the following:) - Alternator 14V, 60 Amp Battery 12V, 33 A.H. Alternator Output Regulator Overvolt Sensor System AgCarryall Kit Normal Category (Consists 020-0 Wheels & Tires Oversize (Net Change) 030-0-1 Exterior Styling (Net Change) 204-A Dual Controls 205-A Corrosion Proofing 250-A Spray Tank & Pump Installation 265-A Wire Cutters C611501-0102 -10.8 -3.5 Starter Prestolite MCL6501 -17.8 -4.0 0712605-1 -26.6 114.0 C611001-0101 -0.8 -1.0 C593001-0101 -0.2 -15.0 0700259-6 192.8* 51.0* 6.1 21.2 9.7 91.2 5.5 14.0 7.0 72.0 143.6 50.8 Main Gear 4.0 20.0 266-A Wire Cutters - Windshield 0.8 18.9 267-A Cable Deflector 1.1 177.1 280-A Co-Pilot Seat 13.0 44.0 284-A Co-Pilot Belt & Shoulder Harness 2.0 37.0 406-A - AgCarryall Kit Restricted Category 229.1* 49.5* (Consists of the following:) 405-A AgCarryall Kit Normal Category 251-A Spray Boom Instl. 192.8 51.0 36.3 41.8 ISSUED:20 Sept. '72 REVISEDA 25 Oct. 172, B=3 Nov. '72 FORM NO. 80-223 SHT 7 OF 11 CessnaⓇ CESSNA AIRCRAFT CO ITEM NO D 500-A Nav-O-Matic 300 (With Item 216-A) Controller Amplifier and Mount Gyro Installation (Item 216-A) Omni Coupler Turn Coordinator (Item 226-0-1) Vacuum System (Item 260-A) Wing Installation Items EQUIPMENT LIST (CONT'D) MODEL A185E (1972) WICHITA, KANSAS DESCRIPTION REF DRAWING WT LBS ARM INS 0770096-2 25.3* 23.7* 1.5 15.0 0701005-2 6.8 12.7 28900 0.8 12.7 1.9 14.5 6.2 -1.4 1200166-1 Servo Actuator - Roll 3.3 68.9 Misc. Parts and Wiring 3.5 60.5 510-A Electronic Option A Nav-Com Provisions 0770400-14 4.7* 78.5* Antenna & Cable VHF Communication Antenna & Cable VOR Nav 0770400-629 0.4 62.9 0770400-623 1.6 165.0 Audio Junction Box 0770400-734 0.3 11.8 Headset Installation 0770400-703 0.1 18.8 Microphone Installation - Hand Held 0770400-701 0.6 16.9 Speaker Installation, Cabin 0770400-713 1.5 37.6 Circuit Breaker S-1360-10 16.7 511-A Electronic Option B Left VHF Com Antenna Antenna 0770400-628 0.4* 62.9* C598501-0104 0.4 63.0 512-A Electronic Option C ADF Antenna Provisions 0770400-36 300 ADF Loop Antenna Cable (ARC) 300 ADF Sense Antenna Cable Assy 1.2* 20.5* 33827-0000 0.6 20.0 2070000-256 0.2 20.0 513-A Electronic Option D Nav-O-Matic Wing Prov. 1200166 0.7 69.7 514-A Electronic Option E Anti-Precip ADF Ant. 0770400-634 0.9 95.1 520-A Antenna and Cable Instl. VHF Com 0770400 1.2 42.8 521-A Antenna Instl., VOR Nav 0770400-623 1.6 165.0 522-A 523-A Antenna Instl., ADF Anti Precip Net Change 0770400 Antenna Coupler and Cables 0.7 95.3 0770400-635 0.5 5.0 524-A Audio Isolation Amplifier (KA-25C) 0770400-714 1.5 1.0 525-A Audio Junction Box 0770400-734 0.3 11.8 526-A Audio Muting Relay 0770400-752 0.1 13.5 527-A Headset Installation (0770039-1) 0770400-703 0.1 18.8 528-A Microphone Installation, Hand Held 0770400-701 0.6 16.9 529-A Microphone Instl., Doorpost Mounted Boom 0770400-750 0.8 27.0 530-A Radio Cooling System - Each Unit Instl. 0770400 0.2 8.0 531-A 532-A Radio Selector Switches & Wiring Remote Radio Rack 0770400 0.5 16.5 0.7 124.0 533-A Speaker Installation, Cabin 0770400-713 1.5 37.6 ISSUED: 20 Sept. '72 REVISED: FORM NO. 80-223 SHT 8 OF 11 CessnaⓇ CESSNA AIRCRAFT CO ITEM NO EQUIPMENT LIST (CONT'D) MODEL A185F (1973). WICHITA, KANSAS DESCRIPTION REF DRAWING WT LBS ARM INS D 550-A Cessna 300 ADF (546A or 546E) 0770400-193,194 7.9* 20.3* R-546A Receiver or 41240-1001 3.3 12.5 R-546E Receiver with BFO 41240-0101 3.3 12.5 M-346A Mounting Box 40900-0000 0.5 12.5 IN-546 Indicator 41250-1001 0.9 16.0 L-346A Antenna, Fixed Loop 41000-1000 1.4 39.3 Sense Antenna Installation 0770400-639 0.2 94.8 551-A Cessna 300 DME (KN-60C) 0770400-82 8.5* 22.0* KN-60C Transceiver 066-1020-20 C582602-0301 6.1 11.5 Mounting Box 0.6 11.5 KA-32 Antenna 0770400-616 0.3 93.3 552-A Cessna 300 Marker Beacon (502B) R-502B Receiver 0770400-192 2.7* 41.6* 31240-0014 1.0 12.2 Antenna, "L" Shaped Rod 0770681-1 0.4 142.5 553-A Cessna 300 Nav-Com 100 Channel (508A) 0770400-196 9.2* 12.3* RT-508A Receiver Transmitter Mounting Box 39360-1014 6.7 12.0 40550 0.8 12.0 IN-514R VOR Indicator 31640-0000 0.9 16.8 554-A Cessna 300 Nav-Com 360 Ch. (328A & IN514R) 9.7* 12.3* RT-328A Receiver Transmitter 41740-1114 7.1 12.0 Mounting Box 40550-0000 0.8 12.0 IN-514R VOR/LOC Indicator 31640-0000 0.9 16.8 555-A Cessna 300 Nav-Com 360 Ch. (328A & IN525A) RT-328A Receiver Transmitter 9.8* 12.3* 41740-1114 7.1 12.0 Mounting Box 40550-0000 0.8 12.0 IN-525A Indicator 32350-0000 1.0 16.8 556-A Cessna 300 Nav-Com 360 Ch. (528E & IN-514R) 0770400-197 RT-528 Receiver Transmitter 9.9* 12.3* 7.3 12.0 Mounting Box 40550 0.8 12.0 IN-514R VOR/LOC Indicator 31640-0000 0.9 16.8 557-A Cessna 300 Nav-Com 360 Ch. (528E & IN525A) 0770400-197 RT-528E Receiver Transmitter 10.0* 12.3* 7.3 12.0 Mounting Box 40550 0.8 12.0 IN-525A VOR/ILS Indicator 32350-0000 1.0 16.8 558-A Cessna 300 HF Transceiver (PT-10A) 0770400-162 21.0* 84.6* PT-10A Transceiver C582103-0101 4.2 11.2 Mounting Box PT-10PS-14 Remote Power Supply DX-10RL-14 Antenna Load Box 351 Inch Long Antenna Wire Instl. C582103-0201 8.6 117.1 C589502-0101 4.2 110.1 0770400-614 0.3 127.7 ISSUED: 20 Sept. '72 REVISED: FORM NO. 80-223 SHT 9 OF 11 CessnaⓇ CESSNA AIRCRAFT CO ITEM NO D EQUIPMENT LIST (CONT'D) MODEL A185F (1973) DESCRIPTION WICHITA, KANSAS REF DRAWING WT LBS ARM INS 559-A Cessna 300 VHF Transceiver (524A) 0770400-49 8.0* 11.1* RT-524A Transceiver M-514R Mounting Box 31390-1114 6.7 11.5 30420-0000 0.7 11.5 560-A Cessna 300 Transponder (KT-76 or KT-78) KT-76 Transceiver (High Altitude) 3901000 4.8* 40.4* C589520-0101 2.8 12.5 KT-78 Transceiver (Low Altitude) KA-48 Antenna 071-1048-00 C589520-0104 2.8 12.5 C589508-0101 0.1 126.0 570-A 571-A 572-A 573-A Cessna 400 Glideslope (443A) 3910119-5 5.4 100.2 574-A 575-A Cessna 400 ADF (Includes Antennas) Cessna 400 Nav-Com W/IN442A (VOR/LOC) Cessna 400 Nav-Com W/IN443A (VOR/ILS) Cessna 400 Transponder (Includes Ant.) (506A) 3910101 Cessna 400 VHF Transceiver 0770400-195 7.9 20.3 В 3910121-29 16.2 47.2 3910121-31 16.2 47.2 8.5 88.0 В 3910124-3 10.2 65.2 В BBBBBB 580-A Emergency Locator Transmitter 0770134 2.4* 119.0* Transmitter (C589510-0102) 2.1 118.0 Antenna (C589519-0103) 0.1 137.0 581-A Sunair SSB, HF Transceiver (ASB-125) RE-1200 Single Side Band Transceiver 0770400-162 24.6* 83.4* 99680 4.5 11.5 Mounting Box 0.8 11.5 PA-1010A Remote Power Amplifier CU-110 Antenna Coupler 351 Inch Active Length Antenna Wire 99682 8.5 117.2 99816 5.2 110.1 0770400-611 0.3 127.7 ISSUED: 20 Sept. '72 REVISED: B= 3 Nov. '72 FORM NO. 80-223 SHT 10 OF 11 *Cessna. CESSNA AIRCRAFT CO ITEM NO D EQUIPMENT LIST (CONT'D) MODEL A185F (1973) DESCRIPTION WICHITA, KANSAS REF DRAWING WT LBS ARM INS INSTRUCTIONS FOR USING RADIO EQUIPMENT LISTINGS: Complete radio installations require certain supporting equipment in addition to the individual radio items listed. The following installation examples and notes should be used as a guide in the determination of complete installations. 1 1. First Unit Cessna 300 Nav-Com 360 Channel with VOR ILS Indicator Complete Installation Consists of Items: 15.3* 33.3* 555-A Cessna 300 Nav-Com 360 Ch. (328A & IN-525A) 520-A Antenna & Cable, Left VHF Communications 9.8 12.3 1.2 42.8 521-A 525-A 527-A Antenna & Cable, VOR Navigation Audio Junction Box Headset Installation 1.6 165.0 0.3 11.8 0.1 18.8 528-A Microphone Installation, Hand-Held 0.6 16.9 530-A Radio Cooling Installation 0.2 8.0 533-A Speaker Installation, Cabin 1.5 37.6 2. Second Unit Cessna 300 Nav-Com 100 Channel with VOR Indicator Complete Installation. Consists of Items: 11.7* 15.2* Cessna 300 Nav-Com 100 Ch. (508A) 9.2 12.3 520-A Antenna & Cable, Right VHF Communication 1.2 42.8 523-A Antenna Coupler & Cables, VOR 0.5 5.0 526-A Audio Muting Relay 0.1 13.5 530-A Radio Cooling Installation 0.2 8.0 531-A Radio Selector Switches and Wiring 0.5 16.5 3. Second Unit Cessna 300 ADF with BFO Complete Installation Consists of Items: 8.5* 20.0* 550-A Cessna 300 ADF (546-A or 546-E) 7.9 20.3 526-A Audio Muting Relay 0.1 13.5 531-A Radio Selector Switches and Wiring 0.5 16.5 4. Third Unit Cessna 300 Marker Beacon Receiver Complete Installation. Consists of Item 552-A only. 2.7 41.6 5. Fourth Unit Cessna 400 Glideslope Receiver Complete Installation. Consists of Item 570-A only. 5.4 100.2 B NOTES: 1. Item 524-A (KA-25C Audio Isolation Amplifier) is required for all multiple radio installations not incorporating a "Cessna Crafted" VHF or HF. 2. All panel mounted transmitters require Item 530-A Radio Cooling System). 3. Item 532-A (Remote Radio Rack) is required for all remote installation than 2 remote units are used (Antenna Load Box not included) a second rack must be included with the 3rd remote unit installation weight. - if more ISSUED: 20 Sept. '72 REVISED: B = 3 Nov. 172 FORM NO. 80-223 SHT 11 OF 11 CESSNA AIRCRAFT COMPANY MODEL A185F WICHITA, KANSAS REVISED WEIGHT & BALANCE DATA Aircraft Serial No. 18502213 F.A.A. Registration No. N3946Q, Date: 5/19/73 Weight C.G. Arm Moment ITEM (lbs.) (inches) (lb.ins.) ORIGINAL LICENSED EMPTY WEIGHT 1845.3 38.0 70202 ADD KESS OPTIONAL EQUIPMENT WEIGHT 12.2 15.1 184 REVISED LICENSED EMPTY WEIGHT 1857.5 37.9 70386 GROSS WT. LICENSED EMPTY WT. = USEFUL LOAD 1 3350.0 LBS) ( 1857.5 LBS) 1492.5 LBS INSTALLED Weight REMOXED 300 Navcom 360CH W/VOR/LOC 2nd (lbs.) 12.2 Moment (lb.ins.) 184 SUPERSEDED Date 4-23 Signature 11 24 221497-7ED CAD CESSNA AIRCRAFT COMPANY WICHITA, KANSAS Weight & Balance and Installed Equipment Data CONTROL NUMBER DATE 305271 04/17/73 185 ITEM MODEL CESSNA SERIAL REGISTRATION NUMBER NUMBER N3946Q STANDARD AIRPLANE (EMPTY, DRY, UNPAINTED) COMPUTED INCLUDES EQUIPMENT ITEMS REQUIRED FOR FAA CERTIFICATION UNUSABLE FUEL 6.0 GALLONS ALLOVER EXT 355A TIGER YELLOW/VES WHITE INT AP CLOVE BROWN PERFORATED VINYL/BROWN 300 NAVCOM 360CH W/VOR/LOC 1ST 300 ADF WO/BFO - · DIGITAL TUNING 2ND 300 TRANSPONDER-LOW ALTITUDE GYROS NEW INCLUDES VACUUM SYSTEM INDICATOR ECONOMY MIXTURE INDICATOR TURN AND BANK EXCH RECORDER FLIGHT HOUR - CARGO PACK CONTROLS DUAL INCL DISENGAGING RH RUDDER PEDALS CONTROL WHEEL ALL PURPOSE EXCH DETECTORS NAVIGATION LIGHTS FILTER OIL FULL FLOW FLOATPLANE KIT INCL CP&CR CABLES FUEL SYSTEM EXTENDED RANGE EXCH GROUND SERVICE PLUG RECEPTACLE GROUP PRIMARY HEATED PITOT EXCH LIGHTS COURTESY SET OF TWO LOCATOR BEACON MICROPHONE BOOM OIL COOLER LARGE NON-CONGEALING EXCH PRIMING SYSTEM ENGINE SEATING ARRANGEMENT D SEAT FRONT LH STD SEAT FRONT RH ARTICULATING VERT ADJ EXCH 18502213 WEIGHT ARM MOMENT 1594.0 36.0 57384 36.0 46.0 1656 11.1 95.2 1057 NEGL. RT328A 15.2 33.4 508 R546 8.5 20.0 170 KT78 4.8 40.4 194 12.3 6.0 74 1.0 6.0 6 .7 13.7 10 .8 11.6 37.0 60.5 2239 5.5 14.0 77 NEGL. NEGL. 4.5 4.0- 18- 38.3 62.4 2390 7.0 46.5 326 2.6 111.0 289 4.5 24.7 111 .5 26.5 13 .5 61.9 31 2.4 119.0 286 .8 2.3 27.0 31.5- 22 72- 1.0 10.0 10 6.0 69.0 414 NEGL. 21.0 41.5 872 24.0 77.8 1867 1.5 206.0 309 NEGL. .3 13.7 NEGL. NEGL. NEGL. 1.2 30.2- 36- 1845.3 38.0 70202 SEATS 2 INDV CNTR & ONE 2-PLACE REAR FOLD-AWAY DSN STABILIZER ABRASION BOOTS STATIC DISCHARGERS SET OF SEVEN STATIC SOURCE ALTERNATE TIRES MAIN GEAR 600X6 WINDOWS ALL TINTED EXCH VALVE CIL QUICK DRAIN WINTERIZATION KIT ENGINE LICENSED EMPTY WEIGHT GROSS WEIGHT 3350.0 LICENSED WEIGHT 1845.3 USEFUL LOAD 1504.7
What's in the CESSNA 185 TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.
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