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Exceptional 1980 Cessna 335

Cessna 335 · Avionics Manual

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Overview

This document serves as an avionics manual for the 1980 Cessna 335, detailing the aircraft's avionics systems and specifications. It provides essential information for pilots and aviation enthusiasts regarding the aircraft's equipment, performance, and maintenance history. The manual outlines the features of various avionics components installed in the aircraft, including navigation systems, autopilot, and engine data monitoring systems. It also includes details about the aircraft's engines, propellers, and additional equipment, making it a comprehensive resource for understanding the capabilities and operational requirements of the Cessna 335.

  • Total Time Airframe (TTAF): 4,834 hours
  • Left Engine: Continental TSIO-520-EB, 300 HP, 741 hours since overhaul
  • Right Engine: Continental TSIO-520-EB, 300 HP, 659 hours since overhaul
  • Gross Takeoff Weight: 6,305 pounds
  • Useful Load: 1,909 pounds
  • Fuel Capacity: 163 gallons
  • Avionics include Aspen EFD Evolution 1000 Pro and Garmin GNS-430W

Document

Source

Originally published by www.silverhawkaviation.biz. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Avionics Manual
Year
1980
Pages
32
File size
3.8 MB
Publisher
www.silverhawkaviation.biz
How rare is it?
35Cessna 335 registered worldwide · 29 active

Common. Rarer than 3% of the aircraft models we track.

Documentation completeness
4/7

Most owners only have the POH. Here's the essential set for the Cessna 335.

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In this document

Avionics Overview

The Cessna 335 is equipped with advanced avionics systems including the Aspen EFD Evolution 1000 Pro EFIS PFD, Garmin GNS-430W GPS-WAAS Nav/Comm, and a Nav-o-matic 400-B Autopilot. These systems enhance situational awareness and provide critical flight data, ensuring safe and efficient operation.

Engine Specifications

The aircraft features two Continental 300 HP TSIO-520-EB engines, each with a total time of 4,834 hours. The left engine has 741 hours since major overhaul, while the right engine has 659 hours since overhaul. Both engines are maintained to high standards, ensuring reliability and performance.

Propeller Details

The Cessna 335 is fitted with McCauley propellers, with the left propeller having 741 hours since overhaul and the right propeller having 643 hours since overhaul. Regular maintenance has been performed to ensure optimal performance.

Weight and Balance

The aircraft has a gross takeoff weight of 6,305 pounds, with a useful load of 1,909 pounds. The document also notes an increase in maximum ramp weight and zero fuel weight due to STC modifications.

Fuel Management System

The Shadin Avionics DIGIFLO-L Digital Fuel Management System provides real-time fuel management data, including fuel flow, remaining fuel, and endurance calculations. This system interfaces with the Garmin GNS-430W for enhanced functionality.

Safety notes

  • Always ensure that all avionics systems are functioning properly before flight.
  • Regular maintenance and checks are crucial for engine and propeller performance.

Full document text

Exceptional 1980 Cessna 335 Serial Number: 3350056 Tail: N6594C TTAF: 4,834 Asking $159,000.00/Make Offer  Exceptionally Well Maintained  Current Owner Since August 2016  Always Hangared  Current On All SB's and AD's  Last Annual: 31 October 2019  ADS-B  Gross TOW Increase STC: + 315 Pounds to 6,305 Pounds  Useful Load: 1,909 Pounds  No Damage History  All Logs Complete & Consecutive ENGINES: Continental 300 HP TSIO-520-EB - 1,400 TBO Serial Number Left Engine: 510605 TT Left Engine: 4,834 Hours TT SMOH Left Engine: 741 Hours OH by Pennyan Aero: 6 February 2009 Serial Number Right Engine: 510594 TT Right Engine: 4,834 Hours TT SMOH Right Engine: 659 Hours OH by Newnan Aircraft Services: 20 January 2004 PROPELLERS: Serial Number Left Prop: 798863 McCauley Model: 3AF32C87 TSOH: 741 Hours Date of OH: 1 April 2008 Serial Number Right Prop: 813649 McCauley Model: 3AF32C504 TSOH: 643 Hours Date of OH: 27 May 2009 AVIONICS:  Aspen Avionics EFD Evolution 1000 Pro EFIS PFD with Optional: Terrain, Traffic, and Weather  Garmin GNS-430W GPS-WAAS Nav/Comm #1  Garmin GNS-430W GPS-WAAS Nav/Comm #2  Garmin GTX-330 Mode 'S' Transponder w/Traffic & Encoder  ADS-B  Cessna 400 Transponder  Nav-o-matic 400-B Autopilot w/Yaw Damper  Co-Pilot Instruments w/Electric Gyro Horizon  Garmin GMA 340 Audio Panel - 6-Place Intercom w/Music Input  Bendix RDR-160 Color Radar  Northstar GPS 60 Navigator  JPI EDM760-6C Engine Data Monitor - w/Recent OH and Firmware Update  Shadin Avionics DIGIFLO-L Digital Fuel Management System - w/Recent OH and Firmware Update  Shadin Avionics DIGIFLO-L Digital Fuel Management System - Interfaced to GNS-430W  Prop Synchrophaser  Avionics Cooling Fan ADDITIONAL:  Full De-Ice - Good Boots & Hot Props & Plumbed for Hot Plate (not currently FIKI)  Keith Freon Air Conditioning - OH'd and R134 Converted in 2017  BLR Boundary Layer Vortex Generators - STC#SA5198NM: Max Ramp Weight Increase: + 315 Pounds to 6,340 Pounds Gross Takeoff Weight Increase: + 315 Pounds to 6,305 Pounds Zero Fuel Weight Increase: + 230 Pounds to 5,860 Pounds  Fuel Capacity: 163 Gallons  Excellent Windshields & Pax Glass All Around  Nose and Nacelle Baggage Lights  Ground Service GPU Power Receptacle  3-Point Strobes  Aft Relief Tube  76.6 Cubic Feet Oxygen System INTERIOR:  Gray Leather Seats  Gray Carpet - New 2018  Gray Leather Side Panels  Burl Wood Stowable Executive Table  4-Place Club Seating  Flight Deck Curtain Divider PAINT: 8/10 INTERIOR: 7/10 This plane has been exceptionally well maintained, continuously and meticulously inspected, and no expenses have ever been spared. It has been expertly owner/USAF combat pilot veteran flown. Aspen EFD Evolution 1000 Pro EFIS PFD The N6594C Aspen EFD1000 Pro Features: The optional terrain, traffic, and weather features Expandable and upgradable Airspeed and altitude tapes Integral altitude alerter Slaved directional gyro with heading bug Base map with flight plan legs and waypoints, curved flight paths, and nearby navaids GPS flight plan map views: 360º & ARC Display of real-time winds aloft, OAT, TAS, and ground speed Integral Air Data Computer and Attitude Heading Reference System (AHRS) Built-in backup battery and emergency GPS Brilliant, direct sunlight-readable, 6-inch 760x400 TFT active matrix LCD display Garmin GNS-430W Integrate Your Avionics GNS 430W is an all-in-one GPS/Nav/Comm solution that features a WAAS-certified GPS, 2280-channel capacity comm and 200-channel ILS/VOR with localizer and glideslope. Fly WAAS Approaches GNS 430W comes with built-in WAAS navigation capabilities. It is approved to fly LPV “glideslope” approaches without reference to ground-based navaids of any kind. Featuring an advanced 15-channel receiver capable of 5 position updates per second, GNS 430W meets stringent TSO C146a FAA standards for WAAS "sole means" navigation — providing vertical and lateral approach guidance into thousands of U.S. airports previously inaccessible in IFR conditions. High Resolution Mapping Its 4" high-contrast display with brilliant colors makes it easy to read and interpret pilot-critical information. Effective use of color makes it easy to see your position relative to ground features, chart data, navaids, flight plan routings and approach procedures. Scan information from wide viewing angles, even in direct sunlight. Enhance Situational Awareness GNS 430W seamlessly integrates built-in terrain and navigation databases, providing a clear, concise picture of where you are and where you’re heading. Its huge Jeppesen® database — updated with front- loading data cards — contains location reference for all airports, VORs, NDBs, Intersections, Flight Service Stations, published approaches, SIDs/STARs, Special Use Airspace and geopolitical boundaries. A detailed basemap clearly shows airports, cities, highways, railroads, rivers, lakes and coastlines. With information from the built-in terrain and U.S. obstacles databases, it uses color coding to graphically alert you when proximity conflicts loom. Put It on Autopilot Working in tandem with standard autopilots that accept roll-steering commands, GNS 430W behaves like a high-end flight management system (FMS) and can automatically fly your aircraft through holding patterns, procedure turns and other position-critical IFR flight procedures. JPI EDM760-6C Engine Data Monitor  LeanFind Performs ROP and LOP, automatically finds the first and last cylinder to peak  Shock cooling checked on all cylinders w/an alarm on the cylinder w/the highest cooling rate  Voltage, For alternator failure, monitored for over and under voltage with alarms  Pilot Programmable Hi & Lo alarm limits.  ALL programming from front panel  Quick response probes, fastest accurate readings  Data Memory, reading once every 2 to 255 seconds  EZPlot-1 program for plotting and downloading data  EGT - 6 Probes  CHT - 6 Probes  Span (Highest To Lowest EGT)  EGT Normalize mode

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 EZTrends Charting and Download Software  Serial Data recording - 25 hours Additional Purchased Optional Functions of the EDM-760  Fuel Flow (USED per engine, Remaining, GPH, Total fuel USED both engines, Endurance, GPS destination)  Oil Temperature  Download box with Memory stick Shadin Avionics DIGIFLO-L Digital Fuel Management System Digiflo-L is a Digital Fuel Management System designed to provide complete fuel management information under real flight conditions without any manual entry of data (after entry of the initial fuel on board information). Digiflo-L is connected to the engine fuel flow transducer for fuel flow information and to the GPS receiver serial port for navigation data (ground speed, distance and estimated time en route). This system transmits the fuel information to the Garmin GNS-430W navigation receiver for additional calculations and display of fuel management data including:  Specific Range, Efficiency  Fuel to Destination  Fuel Reserve  Endurance  Fuel Flow  Fuel Used  Fuel Remaining Cessna Nav-o-matic 400B Auto Pilot A position-based, two-axis autopilot with full altitude functions including altitude hold and glideslope coupling. The 400B gets heading info from a DG or HSI and can interface to the Flight Director. Auto-trim is standard. LEFT ENGINE ANALYSIS RIGHT ENGINE ANALYSIS For more information on this outstanding plane, please contact: David Williams Silver Hawk Aviation, LLC Mobile: (1) 941.376.1586 Fax: (1) 941.349.5982 david@silverhawkaviation.biz www.silverhawkaviation.biz The offer for sale of this aircraft is subject to contract and the aircraft may at any time be withdrawn from the market without prior notice. Specifications subject to verification by the purchaser and are not guaranteed for accuracy and purchaser should rely on their own inspection as aircraft is sold “As is - Where is” All materials herein Copyright Silver Hawk Aviation, LLC, and may not be copied or reproduced

Type certificate, explained

What's in the Cessna 335 TCDS

A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.

TCDS 3A25Rev 25· Issued 1994
Read the full TCDS

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