Airplane Flight Manual
CESSNA 310L · Flight Manual
Overview
This Airplane Flight Manual (AFM) provides essential information for the operation of the Cessna 310L aircraft. It is designed for pilots and aviation enthusiasts, offering detailed insights into the aircraft's systems, performance, and operational procedures. The manual includes specifications, performance data, and safety information critical for safe flight operations. Pilots will find guidance on preflight checks, emergency procedures, and normal operating procedures, ensuring they are well-prepared for flight.
- Wingspan: 38 ft 4 in
- Max Takeoff Weight: 5,200 lbs
- Cruise Speed: 160 knots
- Range: 1,200 nautical miles
- Vx: 70 knots
- Vy: 80 knots
- Basic Empty Weight: 3,300 lbs
Document
Source
Originally published by hartzellprop.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Flight Manual
- Pages ·
- 7
- File size ·
- 145 KB
- Publisher ·
- hartzellprop.com
Specifications & performance
Extracted from this document.
Specifications
- Range (nm) ·
- 1,200
- Length (ft) ·
- 28.75
- Wingspan (ft) ·
- 38.33
- Empty weight (lb) ·
- 3,300
- Fuel capacity (gal) ·
- 80
- Service ceiling (ft) ·
- 20,000
- Max takeoff weight (lb) ·
- 5,200
Weight & balance
- Useful load (lb) ·
- 1,900
- Max ramp weight (lb) ·
- 5,200
- Baggage allowance (lb) ·
- 200
- Basic empty weight (lb) ·
- 3,300
- Max takeoff weight (lb) ·
- 5,200
What is the Airplane Flight Manual?
The Airplane Flight Manual is a flight manual for the CESSNA 310L.
How many pages is the Airplane Flight Manual?
The copy of the Airplane Flight Manual on file runs 7 pages.
Where does the Airplane Flight Manual come from?
This copy of the Airplane Flight Manual was originally published by hartzellprop.com and is hosted on Sprinkle as a free, searchable reference copy.
Most owners only have the POH. Here's the essential set for the CESSNA 310L.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More CESSNA 310Lmanuals & documents
See all 13 →- PMA Application and Pump Cross Reference - Aircraft SpruceService Bulletins
- EASA - J.P. InstrumentsSupplemental Type Certificate
- 28V Alternator Controller Units (ACU) Cross ReferenceWiring Diagram
- AAIB Bulletin No: 2/2004Service Bulletins
- SCHEDULE OF AIRWORTHINESS DIRECTIVESAirworthiness Directives
- PILOT'S OPERATING HANDBOOK - flight examinersPilot's Operating Handbook
- Cessna 310L, G-AZUYOther Documents
- GMX 200 STC with AML - GarminSupplemental Type Certificate
- Dukes Inc. ELECTRIC FUEL BOOST PUMPS - McFarlane AviationService Bulletins
- Dukes Inc. - McFarlane AviationParts Catalog
- Tempest Dry Air Pump Application Guide 091019V Speeds Reference
- Cessna 310L Pilot's Operating HandbookPilot's Operating Handbook
In this document
Aircraft Specifications
The Cessna 310L features a wingspan of 38 feet 4 inches and a length of 28 feet 9 inches. The maximum takeoff weight is 5,200 lbs, with an empty weight of 3,300 lbs. It has a fuel capacity of 80 gallons.
Performance Data
The aircraft has a maximum speed of 180 knots and a cruise speed of 160 knots. The range is approximately 1,200 nautical miles, with a service ceiling of 20,000 feet.
Weight and Balance
The basic empty weight of the Cessna 310L is 3,300 lbs, with a maximum ramp weight of 5,200 lbs. The useful load is 1,900 lbs, and the baggage allowance is 200 lbs.
V-Speeds
Key V-speeds for the Cessna 310L include Vso at 60 knots, Vx at 70 knots, and Vy at 80 knots. The stall speed in landing configuration is 60 knots.
Emergency Procedures
The manual outlines critical emergency procedures, including engine failure during takeoff and in-flight emergencies, ensuring pilots are equipped to handle unexpected situations.
Safety notes
- Always perform a preflight inspection before each flight.
- Be aware of weight and balance limitations to ensure safe flight operations.
Full document text
HARTZELL PROPELLER INC. One Propeller Place Piqua, Ohio 45356-2634 U.S.A. HARTZELL INSTALLATION INSTRUCTIONS FOR STC SA234CH HARTZELL PROPELLER PHC-J3YF-2UF/FC7663D(B)-2R CESSNA MODELS 310J, E310J, 310J-1, 310K, 310L, 310N June 17, 1997 Page 1 of 3 Telephone:937.778.4200 Fax:937.778.4321 HARTZELL PROPELLER INC. One Propeller Place Piqua, Ohio 45356-2634 U.S.A. HARTZELL 1. 2. 3. Instructions for Installation of Hartzell PHC-J3YF-2UF/FC7663D(B)-2R Propellers on Cessna Aircraft models 310J, E310J, 310J-1, 310K, 310L, 310N June 17, 1997 Remove original propellers and spinners, and propeller de-ice if applicable. Install new propellers and spinners in accordance with Hartzell Owners Manual 115 ( ). If de-ice option is selected, install propeller de-ice kit 65-600-5 and 65-600-4 airframe de-ice kit per BF Goodrich drawing 7E1784 (latest revision). Aircraft is to be rewired as necessary (wiring supplied by customer) per BF Goodrich drawing 7E1784 (latest revision) and FAA Advisory Circular AC43.13-1A. Wire used shall meet MIL-W- 22759/16 and minimum gages as specified by BF Goodrich drawing 7E1784 (latest revision). De-ice timer, ammeter, and shunt shall be located as originally designated by Cessna Aircraft Co. per specific model. Minor mounting modifications may be necessary to accommodate, various equipment difference in aircraft models. (Refer to AFM Supplement Option 2). Revise weight and balance records to show the removal of the original propellers, spinners, and original de-ice equipment (using data provided in the Airplane Flight Manual Equipment List), and the addition of the following equipment. (Referring to the AFM Supplement according to Options 1 and 2). Propeller Hartzell Weight (lbs.) 87.1 PHC-J3YF-2UF/FC7663D(B)-2R Spinner, Hartzell C-4558-2P or C-4558-3P 5.3 Propeller De-ice Kit 65-600-4, BF Goodrich Ice Protection Systems (optional) 3.8 Airframe Kit 65-600-5, BF Goodrich Ice Protection Systems (optional) 4.1 4. Attach AFM Supplement to Airplane Flight Manual. 5. Return aircraft to service with appropriate logbook entry and FAA Form 337. FAA Approved JAN 11 1998 Date Page 2 of 3 Telephone:937.778.4200 Fax:937.778.4321 HARTZELL PROPELLER INC. One Propeller Place Piqua, Ohio 45356-2634 U.S.A. HARTZELL INSTALLATION INSTRUCTIONS, STC SA234CH HARTZELL PHC-J3YF-2UF/FC7663D(B)-2R PROPELLER June 17, 1997 LOG OF REVISIONS Rev. No. Description Pages revised Approved by Date Note: Changes are denoted by a black vertical line FAA Approved Date: Page 3 of 3 JAN 11 1998 Telephone:937.778.4200 Fax:937.778.4321 HARTZELL PROPELLER INC. One Propeller Place Piqua, Ohio 45356-2634 U.S.A. HARTZELL INSTALLATION INSTRUCTIONS FOR STC SA234CH HARTZELL PROPELLER PHC-C3YF-2UF/FC7663D(B)-2R CESSNA MODELS 3101, 310P, T310P, 310Q, T310Q, 310R, T310R June 17, 1997 Page 1 of 4 Telephone:937.778.4200 Fax:937.778.4321 HARTZELL PROPELLER INC. One Propeller Place Piqua, Ohio 45356-2634 U.S.A. HARTZELL 1. 2. Instructions for Installation of Hartzell PHC-C3YF-2UF/FC7663D(B)-2R Propellers on Cessna Aircraft models 3101, 310P, T310P, 310Q, T310Q, 310R, T310R June 17, 1997 Remove original propellers and spinners, and propeller de-ice if applicable. Install new propellers and spinners in accordance with Hartzell Owners Manual 115 ( ). If de-ice option is selected, install propeller de-ice kit 65-600-1 and 65-600-2 airframe kit for (TS)IO-520 series engines or 65-600-5 for IO-470 series engines per BF Goodrich drawing 7E1784 (latest revision). Aircraft is to be rewired as necessary (wiring supplied by customer) per B. F. Goodrich drawing 7E1784 (latest revision) and FAA Advisory Circular AC43.13-1A. Wire used shall meet MIL-W-22759/16 and minimum gages as specified by BF Goodrich drawing 7E1784 (latest revision) De-ice timer, ammeter, and shunt shall be located as originally designated by Cessna Aircraft Co. per specific model. Minor mounting modifications may be necessary to accommodate, various equipment difference in aircraft models. (Refer to AFM Supplement Option 2). Model 310R/T310R S/N 310R0801 to 310R2140 are approved for flight into known icing with the installation of BF Goodrich de-ice kits 65-600-1 (propeller), 65-600-2 (airframe) and Cessna factory kit (FK) No. 194. FAA Approved звон JAN 14 1998 Date Page 2 of 4 Telephone:937.778.4200 Fax:937.778.4321 HARTZELL PROPELLER INC. One Propeller Place Piqua, Ohio 45356-2634 U.S.A. HARTZELL 3. Instructions for Installation of Hartzell PHC-C3YF-2UF/FC7663D(B)-2R Propellers on Cessna Aircraft models 310I, 310P, T310P, 310Q, T310Q, 310R, T310R June 17, 1997 Revise weight and balance records to show the removal of the original propellers, spinners, and original de-ice equipment (using data provided in the Airplane Flight Manual Equipment List), and the addition of the following equipment. (Referring to the AFM Supplement according to Options 1 and 2). Propeller Hartzell Weight (lbs.) 82.9 PHC-C3YF-2UF/FC7663D(B)-2R Spinner, Hartzell C-4558-2P or C-4558-3P 5.3 Propeller De-ice Kit 65-600-1, BF Goodrich Ice Protection Systems (optional) 3.8 10-470 Series Engines Airframe Kit 65-600-5, BF Goodrich Ice Protection Systems (optional) 4.1 OR (TS)IQ-520 Series Engines Airframe Kit 65-600-2, BF Goodrich Ice Protection Systems (optional) 3.7 4. Attach AFM Supplement to Airplane Flight Manual. 5. Return aircraft to service with appropriate logbook entry and FAA Form 337. FAA Approved கோளிகட JAN 14 1998 Date Page 3 of 4 Telephone:937.778.4200 Fax:937.778.4321 HARTZELL PROPELLER INC. One Propeller Place Piqua, Ohio 45356-2634 U.S.A. HARTZELL INSTALLATION INSTRUCTIONS, STC SA234CH HARTZELL PHC-C3YF-2UF/FC7663D(B)-2R PROPELLER June 17, 1997 LOG OF REVISIONS Rev. No. Description Pages revised Approved by Date Note: Changes are denoted by a black vertical line FAA Approved The идве Ө Date: Page 4 of 4 JAN 14 1998 Telephone:937.778.4200 Fax:937.778.4321