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310I — Cessna Aircraft Company 310I

Cessna Aircraft Company 310I
C310
Photo via Wikipedia: Cessna 310
Year
Owner
Cessna Aircraft Company
Last seen
MTOW
2,400 kg
Range
640 nm
Seats
5
310Ihover
Cessna Aircraft Company · 310I
Model overview

Fleet & certification

Built
70
Active
63
Origin
US
Certifying authorities
FAA
Marketplace

1 for sale right now

Variants

Per-variant specifications

VariantEngineMTOWRangeCruisePax
C310
C310
2,400 kg640 nm193 kt5
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 310Imarket & fleet intelligence

Registry, flight-tracking and market data on the Cessna Aircraft Company 310I fleet — updated daily.

Fleet age

62 yearsmedian age

Of the 51 registered Cessna Aircraft Company 310I with a known build year (73% of the 70 we track), the median age is 62 years.

Registration activity

2changed registration in 12 months

2 of the 70 registered Cessna Aircraft Company 310I we track changed registration in the last 12 months (3% of the fleet), across 2 registration events. Registration changes include ownership transfers, re-registrations and address updates — not all are sales.

For sale now

1Cessna Aircraft Company 310I listed for sale

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Cessna Aircraft Company 310I 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 310I 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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