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185ECessna Aircraft Company 185E

Cessna Aircraft Company 185E
C185
Photo: Photo via Wikipedia: Cessna 185 Skywagon ·
Year
0
Owner
Cessna Aircraft Company
Last seen
— ·
MTOW
1,500 kg
Range
700 nm
Seats
5
185Ehover
Cessna Aircraft Company · 185E
,
Model overview

Fleet & certification

Built
20
Active
16
Origin
US
Certifying authorities
FAA
Variants

Per-variant specifications

VariantEngineMTOWRangeCruisePax
C185
C185
1,500 kg700 nm145 kt5
Same family

Other models in this family

Type certification

The FAA paperwork

TCDS 3A24 · 38 · issued 2006-05-03

The FAA-issued Type Certificate for this model is on file (TCDS 3A24), but we haven't yet extracted the structured spec values.

Read the TCDS (PDF) →
Safety & ops history

Where to look next

Detailed safety & ops history coming soon — view this model's FAA Airworthiness Directives at FAA.gov.
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Other airframes worth a look

Cessna Aircraft Company 185E manuals & documents

1 document on Sprinkle — POH, checklist, flight manual and related references. PDFs served from cdn.sprinkle.com.

Overview · AVIATION INVESTIGATION REPORT A11Q0136 ENGINE STOPPAGE AND FORCED LANDING ON WATER · 2011

This document is an aviation investigation report by the Transportation Safety Board of Canada, detailing an incident involving a Cessna A185E floatplane operated by Air Tamarac Inc. on July 18, 2011. The report outlines the circumstances surrounding an engine failure that led to a forced landing on water, resulting in one fatality among the five occupants. The report aims to enhance transportation safety rather than assign fault. It includes a comprehensive analysis of the flight history, aircraft information, crew qualifications, and the investigation's findings regarding the causes and contributing factors of the incident.

  • The aircraft model involved was a Cessna A185E, not A185F.
  • The engine failure occurred approximately 12 minutes after takeoff at an altitude of 1600 feet.
  • The aircraft was carrying five occupants, resulting in one fatality and three survivors.
  • The fuel system included a selector valve with three positions: LEFT, BOTH, RIGHT.
  • The aircraft's stall speed was 65 mph at maximum weight.

Documents are sourced from publicly available references. Sprinkle does not host OEM-restricted materials; if you are a rights-holder and want a document removed, email .