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310E — Cessna Aircraft Company 310E

Cessna Aircraft Company 310E
C310
Photo: Aeroprints.com · CC BY-SA 3.0
Year
Owner
Cessna Aircraft Company
Last seen
MTOW
2,400 kg
Range
640 nm
Seats
5
310Ehover
Cessna Aircraft Company · 310E
Model overview

Fleet & certification

Built
6
Active
6
Origin
US
Certifying authorities
FAA
Variants

Per-variant specifications

VariantEngineMTOWRangeCruisePax
C310
C310
2,400 kg640 nm193 kt5
Same family

Other models in this family

Type certification

The FAA paperwork

TCDS 3A10 · 62 · issued 2005-02-22

The FAA-issued Type Certificate for this model is on file (TCDS 3A10), 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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Cessna Aircraft Company 310E manuals & documents

8 documents for the Cessna Aircraft Company 310 family Airworthiness Directives · Wiring Diagram · Emergency Procedures · Systems Description · Service Bulletins · Other Documents. PDFs served from cdn.sprinkle.com.

No documents are catalogued for the 310E specifically; these are the Cessna Aircraft Company 310 family documents.

Overview
Multi-Engine Course Study Guide · 2019

The Multi-Engine Course Study Guide is designed for pilots training on multi-engine aircraft, specifically the Cessna 310. It serves as a comprehensive resource for understanding the aerodynamics, systems, and operational procedures relevant to multi-engine flying. The guide emphasizes critical thinking and retention of information through flashcard-style questions and answers. It covers essential topics such as engine failure procedures, VMC (minimum controllable airspeed), and the specifics of the Cessna 310's fuel system. The content is structured to facilitate discussion with instructors and enhance the learning experience for students preparing for multi-engine operations.

  • The Cessna 310 has 5 or 6 fuel tanks depending on configuration: 2 mains, 2 auxiliary, and 1 or 2 locker tanks.
  • There are 7 or 8 total fuel pumps depending on the number of locker tanks.
  • Critical speed is the minimum speed at which the aircraft can fly with one engine inoperative.
  • VMC is the minimum controllable airspeed and is dynamic based on configuration and power output.
  • Engine failures require prompt and correct pilot response to maintain control.

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 .

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Registered 310E aircraft

Individual 310E airframes by tail number — registration history, operator and lineage.