Pilot's Operating Handbook Cessna A185F Floatplane

CESSNA A185F FLOATPLANE · Pilot's Operating Handbook

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Overview

This Pilot's Operating Handbook (POH) is specifically designed for the Cessna A185F Floatplane. It serves as a comprehensive guide for pilots operating this aircraft, providing essential information on its systems, performance, and operational procedures. The handbook includes detailed sections on preflight checks, emergency procedures, and performance data, ensuring that pilots have the necessary resources to operate the aircraft safely and efficiently. The POH is intended for both experienced pilots and those new to the Cessna A185F Floatplane, offering insights into the unique characteristics of this floatplane variant.

Wingspan: 36 ft 0 in
Max Takeoff Weight: 2,800 lbs
Stall Speed (clean): 55 knots
Takeoff Distance over 50 ft: 1,600 ft
Vso: 47 knots

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Document details

Type: Pilot's Operating Handbook
Pages: 9
File size: 1.4 MB
Publisher: irp.cdn-website.com

Specifications & performance

Extracted from this document.

Specifications

Height (ft): 8.83
Length (ft): 22.92
Wingspan (ft): 36
Empty weight (lb): 1,650
Fuel capacity (gal): 50
Max takeoff weight (lb): 2,800

Performance

Landing over 50ft: 1,500
Takeoff over 50ft: 1,600
Landing distance (ft): 1,500
Takeoff distance (ft): 1,600
Stall speed clean (kt): 55

V-speeds

VR: 60
VNE: 175
VSO: 47

Weight & balance

Useful load (lb): 1,150
Max ramp weight (lb): 2,800
Basic empty weight (lb): 1,650
Max takeoff weight (lb): 2,800

Documentation completeness

2/7

Most owners only have the POH. Here's the essential set for the CESSNA A185F FLOATPLANE.

Pilot's Operating Handbook / AFM
Checklist
Maintenance Manual
Parts Catalog (IPC)
Systems & Wiring
Service Bulletins
Type Certificate (TCDS)

More CESSNA A185F FLOATPLANEmanuals & documents

In this document

Aircraft Specifications

The Cessna A185F Floatplane features a wingspan of 36 feet, 0 inches, a length of 22 feet, 11 inches, and a height of 8 feet, 10 inches. The empty weight is approximately 1,650 lbs, while the maximum takeoff weight is 2,800 lbs. It has a fuel capacity of 50 gallons.

Performance Data

The performance section outlines critical data such as takeoff distance over a 50-foot obstacle, which is approximately 1,600 feet, and landing distance over a 50-foot obstacle, which is about 1,500 feet. The stall speed in a clean configuration is 55 knots.

V-Speeds

Key V-speeds for the Cessna A185F Floatplane include Vso (stalling speed in landing configuration) at 47 knots, Vr (rotation speed) at 60 knots, and Vne (never exceed speed) at 175 knots.

Weight and Balance

The weight and balance section provides crucial information on the basic empty weight of 1,650 lbs, maximum ramp weight of 2,800 lbs, and a useful load of 1,150 lbs. The center of gravity (CG) range is specified as 36 to 46 inches.

Emergency Procedures

Emergency procedures are outlined for various scenarios, including engine failure during takeoff and in-flight emergencies. Pilots are instructed on how to handle these situations effectively to ensure safety.

Safety notes

Always perform a thorough preflight inspection before each flight.
Be aware of weight and balance limitations to ensure safe operation.

Full document text

FLINT AERO, INC. 1935 NORTH MARSHALL AVENUE EL CAJON, CA 92020 FAA Approved Pilot's Operating Handbook, Airplane Flight Manual Supplement and Supplemental Airplane Flight Manual Floatplane Supplement 185.19 CESSNA MODEL A185F floatplane Serial No. 18502091 through 18503939 and on. Equipped with EDO-AIRE MODEL 582-3430 Seaplane Floats IAW STC SA832EA This document must be carried on board and attached to the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual when the Cessna 185 with EdoAire Model 582-3430 Seaplane floats per STC SA832EA is modified by the installation of the Flint Aero Wing Tip Fuel Tanks in accordance with STC SA 8036NM. The information contained herein Supplements or Supersedes the basic Cessna flight manual including the Amphibian Supplement and the EDC-AIRE FLIGHT MANUAL SUPPLEMENT No. E-2 Report ECC-466 only in those areas listed herein. For limitations, procedures, and performance information not contained in this document, consult the basic placards, Cessna Pilot's Operating Handbook, Cessna Airplane Flight Manual including the Amphibian Supplement, and the EDO-AIRE FLIGHT MANUAL SUPPLEMENT No. E-2, Report ECC-466 and FLINT AERO, INC. FAA APPROVED PILOT'S OPERATING HANDBOOK AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 185.14. Sam Manager, Flight Test Branch, ANM-160L Federal Aviation Administration Los Angeles Aircraft Certification Office Transport Airplane Directorate FAA APPROVED DATE: 3.1916 STC SA8036NM Report Number 185.19 Ongination Date "Originated By FLINT AERO, INC SUPPLEMENT AFM, P.O.H. AND AFM SUPPLEMENT TO CESSNA MODEL A185F FLOATPLANE SUPPLEMENT EDO-AIRB MODEL 582 SEAPLANE FLOATS Page P-1 Revision Revision Date Revised By REVISIONS AND ADDITIONS REV DATE LEV PAGES AFFECTED IR 12/03/96 Title 12/03/96 P-1 12/03/96 P-2 12/03/96 1-6 REMARKS APPROVED BY Installation of wing tipting fuel tanks Manager, Flt. Test Branch FAA LOS Angeles ACO ANM160L Date Dec 3,1996 EFFECTIVE PAGES Page Rev Date Page Rev Date Page Rev Date P-1 IR 12/03/96 P-2 IR 12/03/96 1-6 IR 12/03/96 STC SA8036NM Report Number 185.19 Origination Date Originated By FLINT AERO, INC SUPPLEMENT AFM, P.O.H. AND AFM SUPPLEMENT TO CESSNA MODEL A185F FLOATPLANE SUPPLEMENT EDO-AIRE MODEL 582 SEAPLANE FLOATS Page P-2 Revision Revision Date Revised By SECTION TITLE 1 General 2 3 A 5 6 7 8 00 TABLE OF CONTENTS Limitations Emergency Procedures Normal Procedures Performance Weight and balance/Equipment List Airplane and Systems Description Airplane Handling, Service and Maintenance FAA APPROVED DATE: DECEMBER 3, 1996 PAGE 1 3 5 20 #5 STC SA8036NM Report Number 185.19 Origination Date Originated By FLINT AERO, INC. SUPPLEMENTAL AFM, P.O.H. AND AFM SUPPLEMENT TO CESSNA MODEL A185F FLOATPLANE SUPPLEMENT EDO-AIRE MODEL 582 SEAPLANE FLOATS SECTION I Page 1 Revision Revision Date Revised By GENERAL INTRODUCTION This supplement provides information not found in the basic handbook which is required to be furnished to the pilot by FAR 21.5. It includes procedures and data required for the safe and efficient operation of the Cessna Model A185F equipped with EDO- AIRE Model 582-3430 seaplane floats installed per STC SA832EA, when modified by the installation of Flint Aero Wing Tip Fuel Tanks in accordance with STC SA8036NM. Information contained in the Model A185F basic FAA approved Cessna Floatplane Supplement for the Model A185F equipped with EDO-AIRE 582-3430 seaplane floats, which is the same as that for the Flint Aero modified floatplane is generally not repeated in this supplement. Information contained in the Flint Aero Supplemental AFM, POH, and AFM Supplement 185.14 for airplanes modified by the installation of Flint Aero Wing Tip Fuel Tanks in accordance with STC SA8036NM, which is the same as that for the Flint Aero modified floatplane is generally not repeated in this supplement. Wherever the words "Not Applicable" appear in this Supplement, they are used to indicate that information may not be the same as that shown in the Cessna Supplement and is not required by the airplane certification basis, and therefore should not be used. FAA APPROVED DATE: DECEMBER 3 1996 Page STC SA8036NM Report Number 185.19 Origination Date Originated By FLINT AERO, INC. SUPPLEMENTAL AFM, P.O.H. AND AFM SUPPLEMENT TO CESSNA MODEL A185F FLOATPLANE SUPPLEMENT EDO-AIRE MODEL 582 SEAPLANE FLOATS 2 Revision Revision Date Revised By PERFORMANCE SPECIFICATIONS SPEED: NO CHANGE CRUISE: Range increases in proportion to the amount of additional fuel carried in the wing tip extended tanks. There is no significant change in the specific range. RATE OF CLIMB AT SEA LEVEL: NO CHANGE SERVICE CEILING: NOT APPLICABLE TAKEOFF PERFORMANCE: Increase takeoff water run distances by 12 percent for each 100 pounds gross weight over the weight shown in the Cessna 185 Floatplane Owner's Manual Supplement. LANDING PERFORMANCE: Increase landing water run distances by 3 percent for each 100 pounds gross weight over the weight shown in the Cessna 185 Floatplane Owner's Manual Supplement. STALL SPEED (CAS): SEE TABLE 1 MAXIMUM WEIGHT: TAKEOFF: 3600 LB. LANDING: 3600 LB. EMPTY WEIGHT: See actual weight and balance form for airplane. MAXIMUM USEFUL LOAD: See actual weight and balance form for airplane. BAGGAGE ALLOWANCE: IN AIRPLANE: NO CHANGE IN EACH FLOAT BAGGAGE COMPARTMENT: NO CHANGE (CAUTION: See LIMITATIONS SECTION) WING LOADING: POUNDS/SQ.FT. (@ 3600 LBS) 19.35 POWER LOADING: POUNDS/HP (@ 3600 LBS) 12.0 FUEL CAPACITY: SEE SECTION 2 OF FLINT AERO AFM SUPPLEMENT OIL CAPACITY: ENGINE: PROPELLER: SAME SAME SAME FAA APPROVED DATE: DECEMBER 3, 1996 STC SA8036NM Report Number 185.19 Origination Date Originated By FLINT AERO, INC. SUPPLEMENTAL AFM, P.O.H. AND AFM SUPPLEMENT TO CESSNA MODEL A185F FLOATPLANE SUPPLEMENT EDO-AIRE MODEL 582 SEAPLANE FLOATS Page 3 Revision Revision Date Revised By SECTION 2 LIMITATIONS 1. 2. A. Airspeed Limitations All airspeed limitations remain unchanged. Airspeed Indicator Markings

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Airspeed indicator color code significance remains unchanged. The lower limit of the white arc of the indicator is increased for each model by 3 knots or 3 MPH as appropriate. Gross Weight For Cessna A185F airplanes with Edo-Aire 582-3430 Seaplane Floats installed per STC SA832EA, when modified by the installation of Flint Aero wing tip fuel tanks in accordance with STC SA8036NM, the maximum gross takeoff and landing weight is 3600 lbs. For installation of other modifications by STC, the maximum gross weight is limited to that which is authorized by each particular STC. The pilot is advised to determine this gross weight limit from each appropriate STC. Center of Gravity Limits -Center of gravity range, inches aft of datum, moment in lb./1000 Forward Limit Inches Moment Aft Limit Inches Moment 43.4 34.1 156.2 46.5 167.4 71.6 46.5 97.7 34.1 61.4 46.5 83.7 Straight line fairing between points. Placards 5. No change. FAA APPROVED DATE: DECEMBER 1996 Weight, lb. 3600 2100 1800 STC SA8036NM Report Number 185.19 Origination Date Originated By FLINT AERO, INC. SUPPLEMENTAL AFM, P.O.H. AND AFM SUPPLEMENT TO CESSNA MODEL A1057 FLOATPLANE SUPPLEMENT EDO-AIRE MODEL 582 SEAPLANE FLOATS Page 4 Revision Revision Date Revised By SECTION 3 EMERGENCY PROCEDURES No change. SECTION 4 NORMAL PROCEDURES No change. SECTION 5 PERFORMANCE This supplement addresses the operation of an airplane incorporating STC SA8036NM at gross weights greater than previously certificated. The effect of this gross weight increase on airplane performance is effectively offset by the increase in wing area and aspect ratio. For stall speeds at a fixed gross weight, a four knot decrease in the flaps up stall speed, but no change in the flaps 20° and 40° can be expected. Rate of climb will increase at a fixed gross weight. Takeoff and landing distances will increase by 12% and 3% respectively for each 100 lbs. increase in gross weight. For weights equal to or less than the previously certificated gross weight, use the standard performance tables applicable to the basic unmodified airplane. For these weights, performance will be equal to or greater than the tables show. The Flint Tip Fuel Tanks may be used in conjunction with other approved modifications provided it is determined that no interference exists. In this instance, the performance procedure in the paragraph above applies and in addition performance decrements must be applied as previously defined for any other installations. FAA APPROVED DATE: DECEMBER 3 1996 LOADED AIRPLANE WEIGHT, pounds STC SA8036NM Report Number 185.19 Origination Date Originated By FLINT AERO, INC. SUPPLEMENTAL AFM, P.O.H. AND AFM SUPPLEMENT TO CESSNA MODEL A185P FLOATPLANE SUPPLEMENT EDO-AIRE MODEL 582 SEAPLANE FLOATS SECTION 6 WEIGHT AND BALANCE/EQUIPMENT LIST 200 LOADING GRAPH FOR 180 160 FLINT AERO WING TIP 140 FUEL TANKS LOAD WEIGHT. pounds 100 80 120 NSSON 60 Page 5 Revision Revision Date Revised By 30 U.S. GALLONS MAX WING TIP TANKFUEL 40 Example: 10 Gals x 6 lbs/gal = 60 lbs 60 lbs x 46.4 in = 2784 lb-in 20 0 0.000 1.000 2.000 3.000 4.000 5.000 6.000 7.000 8.000 9.000 10.000 LOAD MOMENT / 1000, pound - inches 3800 3600 CENTER OF GRAVITY 3400 MOMENT ENVELOPE 3200 3000 2800 2600 2400 2200 2000 1800 50 60 70 80 90 100 110 120 130 140 150 160 170 LOADED AIRPLANE MOMENT/1000, pound - inches FAA APPROVED DATE: DECEMBER 3, 1996 180 STC SA8036NM Report Number 185.19 Origination Date Originated By FLINT AERO, INC. SUPPLEMENTAL AFM, 2.0.H. AND AFM SUPPLEMENT TO CESSNA MODEL A185F FLOATPLANE SUPPLEMENT EDO-AIRE MODEL 582 SEAPLANE FLOATS Page 6 Revision Revision Date Revised By Table 1 STALL SPEED, Angle of Bank CAS 0 Deg 30 Deg 45 Deg 60 Deg Condition MPH KCAS MPH KCAS MPH KCAS MPH KCAS Model A185F Floatplane Flaps Up 62 54 67 58 74 64 88 76 Flaps 20 Deg 61 53 66 57 73 63 87 75 3600 lbs Gross Weight Flaps 40 Deg 61 53 65 57 57 72 63 86 75 SECTION 7 AIRPLANE & SYSTEMS DESCRIPTIONS No change. SECTION 8 AIRPLANE HANDLING, SERVICE AND MAINTENANCE WITH WING TIP FUEL (TRANSFER) No change. FAA APPROVED DATE: DECEMBER 3, 1996 stdate6.xls

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