CESSNA A185F AMPHIBIAN Model Guide
CESSNA A185F AMPHIBIAN · Model Guide
Overview
The CESSNA A185F AMPHIBIAN is a single-engine piston Skywagon on amphibious floats. The library data lists a 310 hp Continental IO-550 with a Hartzell 3-blade propeller, 74 gal of fuel, a 115 kt cruise at 12 gph and about 600 nm of range. Many examples are modified, so verify the installed STCs and the weight paperwork.
- Library figures: 115 kt cruise, 12 gph, 74 gal fuel, 600 nm range, 1650 lb empty weight, 1550 lb useful load.
- Library max takeoff weight is 3525 lb. The Flint Aero wing tip tank STC allows 3600 lb takeoff on land and water.
- The floats add weight and drag. A flight report calls the airplane heavy in pitch, with a floor-mounted trim wheel.
- Inspect the float nose track and nose bulkhead for looseness or cracks (Wipline Service Letter 136).
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at sprinkle.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Model Guide
- Year ·
- 2026
- File size ·
- 50 KB
- Copy found at ·
- sprinkle.com
Specifications & performance
Extracted from this document.
Specifications
- Range (nm) ·
- 600
- Engine (hp) ·
- 310
- Height (ft) ·
- 12.5
- Length (ft) ·
- 27.5
- Wingspan (ft) ·
- 38.83
- Empty weight (lb) ·
- 1,650
- Fuel capacity (gal) ·
- 74
- Max takeoff weight (lb) ·
- 3,525
Performance
- Range (nm) ·
- 600
- Fuel burn (gph) ·
- 12
- Max speed (kt) ·
- 130
- Cruise speed (kt) ·
- 115
- Landing over 50ft ·
- 2,000
- Takeoff over 50ft ·
- 2,500
- Landing distance (ft) ·
- 1,200
- Takeoff distance (ft) ·
- 1,500
V-speeds
- VA_KTS ·
- 118
- VX_KTS ·
- 63
- VY_KTS ·
- 74
- VFE_KTS ·
- 93
- VNE_KTS ·
- 182
- VNO_KTS ·
- 146
- VS1_KTS ·
- 60
- VSO_KTS ·
- 51
Weight & balance
- Useful load (lb) ·
- 1,550
- Empty weight (lb) ·
- 1,650
- Cg aft limit (in) ·
- 46
- Max ramp weight (lb) ·
- 3,200
- Baggage allowance (lb) ·
- 270
- Max landing weight (lb) ·
- 3,200
- Max takeoff weight (lb) ·
- 3,525
- Cg forward limit (in) ·
- 36
What engine does the CESSNA A185F AMPHIBIAN have?
The CESSNA A185F AMPHIBIAN library data lists a 310 hp Continental IO-550 with a Hartzell 3-blade propeller. A reviewed owner example was upgraded to an IO-550 with a 3-blade Scimitar prop, so confirm what is installed.
What is the maximum weight of the CESSNA A185F AMPHIBIAN?
The library data gives 3525 lb max takeoff and 3200 lb max ramp and landing. The Flint Aero wing tip tank STC supplement allows 3600 lb takeoff on land and water, and 3525 lb landing on land. Check the aircraft's own paperwork.
What should I inspect on a CESSNA A185F AMPHIBIAN with Wipline floats?
On the CESSNA A185F AMPHIBIAN, check the float nose track for play and the nose bulkhead for flexing or cracks. Wipline Service Letter 136 covers this, and jacking under the keel near the bow is the check it describes.
What is the CESSNA A185F AMPHIBIAN Model Guide?
The CESSNA A185F AMPHIBIAN Model Guide is a model guide for the CESSNA A185F AMPHIBIAN, dated 2026.
What year was the CESSNA A185F AMPHIBIAN Model Guide published?
The CESSNA A185F AMPHIBIAN Model Guide — the CESSNA A185F AMPHIBIAN model guide on file — is dated 2026.
Most owners only have the POH. Here's the essential set for the CESSNA A185F AMPHIBIAN.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More CESSNA A185F AMPHIBIANmanuals & documents
- Airplane Flight Manual Supplement Revision ListFlight Manual
- ® 3000 FLOATS - WipaireSystems Description
- SERVICE LETTER NUMBER 136: 3000/3450 NOSE BOX - FINGER TAB INSTALLATIONService Bulletins
- My Other Plane is a Cessna 185 AmphibianPerformance Data
- Airworthiness Directive - AD/RAD/81 Amdt 1 - CASAAirworthiness Directives
- Supplemental Type Certificate for CESSNA A185F AMPHIBIANSupplemental Type Certificate
- Pilot's Operating Handbook Cessna A185F AmphibianPilot's Operating Handbook
- Wiring Diagram for CESSNA A185F AMPHIBIANParts Catalog
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- Pilot's Operating Handbook Cessna A185F AmphibianCESSNA A185F AMPHIBIAN · Pilot's Operating Handbook
- CESSNA CARAVAN 208 FLOATPLANE Model GuideCESSNA CARAVAN 208 FLOATPLANE · Model Guide
- CESSNA 180 Model GuideCESSNA 180 · Model Guide
In this document
Weights and loading
Library data: 1650 lb empty, 1550 lb useful load, 3525 lb max takeoff, 3200 lb max ramp and landing, 270 lb baggage. The Flint Aero STC supplement allows 3600 lb takeoff (land and water) and 3600 lb water landing. Land landing stays at 3525 lb. Use the aircraft's own weight and balance form.
Performance
Library figures: 1500 ft takeoff ground run, 2500 ft over 50 ft, 1200 ft landing, 2000 ft landing over 50 ft, 115 kt cruise, 130 kt max. With the Flint Aero STC, add 12 percent to takeoff runs and 3 percent to landing runs for each 100 lb over the base supplement weight.
Floats and modifications
The 180/185 is among the most-modified aircraft flying. A reviewed example had Aerocet composite amphibious floats, a Robertson STOL kit, an IO-550 and wingtip extensions. Wipline 3000 floats have two hatches, each rated for 50 pounds. Check which STCs are installed and that the paperwork matches.
Safety notes
- Do not exceed the gross weight authorised by each installed STC. The Flint Aero supplement sets 3600 lb takeoff and 3525 lb landing on land.
- Wipline Service Letter 136 describes oblong nose track holes that loosen the joint and can crack the nose bulkhead. Compliance is optional, and the work takes about 8-10 hours.
- With the Flint Aero wing tip tank STC the supplement lists service ceiling as Not Applicable. Do not rely on the library 15000 ft figure for that setup.
Full document text
CESSNA A185F AMPHIBIAN Model Guide The CESSNA A185F AMPHIBIAN is a single-engine piston Skywagon on amphibious floats. The library data lists a 310 hp Continental IO-550 with a Hartzell 3-blade propeller, 74 gal of fuel, a 115 kt cruise at 12 gph and about 600 nm of range. Many examples are modified, so verify the installed STCs and the weight paperwork. • Library figures: 115 kt cruise, 12 gph, 74 gal fuel, 600 nm range, 1650 lb empty weight, 1550 lb useful load. • Library max takeoff weight is 3525 lb. The Flint Aero wing tip tank STC allows 3600 lb takeoff on land and water. • The floats add weight and drag. A flight report calls the airplane heavy in pitch, with a floor-mounted trim wheel. • Inspect the float nose track and nose bulkhead for looseness or cracks (Wipline Service Letter 136). Weights and loading Library data: 1650 lb empty, 1550 lb useful load, 3525 lb max takeoff, 3200 lb max ramp and landing, 270 lb baggage. The Flint Aero STC supplement allows 3600 lb takeoff (land and water) and 3600 lb water landing. Land landing stays at 3525 lb. Use the aircraft's own weight and balance form. Performance Library figures: 1500 ft takeoff ground run, 2500 ft over 50 ft, 1200 ft landing, 2000 ft landing over 50 ft, 115 kt cruise, 130 kt max. With the Flint Aero STC, add 12 percent to takeoff runs and 3 percent to landing runs for each 100 lb over the base supplement weight. Floats and modifications The 180/185 is among the most-modified aircraft flying. A reviewed example had Aerocet composite amphibious floats, a Robertson STOL kit, an IO-550 and wingtip extensions. Wipline 3000 floats have two hatches, each rated for 50 pounds. Check which STCs are installed and that the paperwork matches. Safety notes: • Do not exceed the gross weight authorised by each installed STC. The Flint Aero supplement sets 3600 lb takeoff and 3525 lb landing on land. • Wipline Service Letter 136 describes oblong nose track holes that loosen the joint and can crack the nose bulkhead. Compliance is optional, and the work takes about 8-10 hours. • With the Flint Aero wing tip tank STC the supplement lists service ceiling as Not Applicable. Do not rely on the library 15000 ft figure for that setup.