Legacy 210 (1960-1971 models) SYSTEMS & PROCEDURES COURSE

CESSNA TURBO 210L · Maintenance Manual

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Overview

This document serves as a maintenance manual for the Cessna 210 series, specifically covering models produced between 1960 and 1971. It is designed for aircraft maintenance personnel and pilots who need to understand the systems and procedures associated with these aircraft. The manual includes detailed information on various aircraft systems, maintenance procedures, and troubleshooting guidelines. It aims to ensure that maintenance personnel can effectively service and maintain the aircraft, enhancing safety and operational efficiency.

The Cessna 210 series includes models from 1960 to 1971, each with specific maintenance requirements.
Flight control systems include hydraulic flaps and aileron control systems, with detailed schematics provided.
The landing gear retraction system is critical for safe operation and includes specific troubleshooting steps.
The electrical system features dual alternators and requires regular load analysis for optimal performance.

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Source

Originally published by cessna.org. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type: Maintenance Manual
Year: 2012
Pages: 312
File size: 41 MB
Publisher: cessna.org

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539CESSNA TURBO 210L registered worldwide · 483 active

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In this document

Flight Controls & Rigging

This section covers the flight control systems of the Legacy 210, detailing the hydraulic flaps, aileron control systems, and elevator control systems. It includes schematics and installation instructions for various model years, ensuring that maintenance personnel can accurately assess and repair these systems.

Landing Gear Retraction System

The manual outlines the landing gear retraction system for the Legacy 210, including the sequence of events for aircraft with engine-driven hydraulic pumps. It provides detailed diagrams and troubleshooting steps for the landing gear system, ensuring proper functionality and safety during operation.

Electrical System

This section details the electrical components and systems used in the Legacy 210. It includes information on the dual alternator setup, electrical load analysis, and troubleshooting procedures for common electrical issues.

Utilities

The utilities section covers the static system, vacuum systems, cabin heat, and defrost systems. It provides maintenance guidelines and installation procedures for these essential systems, ensuring comfort and safety for the aircraft occupants.

Safety notes

Always refer to the latest maintenance procedures to ensure compliance with safety standards.
Improper maintenance of the landing gear system can lead to catastrophic failure during operation.

Full document text

WELCOME TO THE CESSNA PILOTS ASSOCIATION Legacy 210 (1960-1971 models) SYSTEMS & PROCEDURES COURSE S1 2 CESSNA FACTORY TECH SUPPORT 316-517-5800 Cessna Support on the web! OLD - www.cessnasupport.com NEW - www.txtavsupport.com Article In The January 2012 CPA Magazine Gives All The Details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egacy 210 FLIGHT CONTROLS & RIGGING Section Three S3 2 1960-1963 Hydraulic Flaps S3 3 1960-1963 Synchronizing System S3 4 1964 thru 1966 Flap Schematics S3 5 1967 thru Early 1968 Flap Schematics S3 6 Mid 1968 and On Flap Schematics S3 7 1964-1966 Flap System S3 8 1967 Flap System S3 9 1968 and On Flap System S3 10 Flap Pre-Select S3 11 Flap Installation 1960 thru 1963 S3 12 Flap Installation 1964 thru 1966 S3 13 Flap Installation 1967 and Later S3 14 1960-1961 Control Yoke Assembly S3 15 1960-1961 Aileron Control System S3 16 1962 and On Control Yoke Assembly S3 17 Box Bearings Diagram S3 18 1960-1963 Aileron Installation S3 19 1964 and On Aileron Control System S3 20 1960-1963 Aileron Installation S3 21 1960-1963 Aileron Installation S3 22 Frise Style Aileron S3 23 1969-1984 Aileron/Rudder Interconnect S3 24 1960-1961 Elevator Control System S3 25 1962 and on Elevator Control System S3 26 Elevator Bellcrank Installation S3 27 Elevator Control Surface 1967 thru 1984 S3 28 Elevator Trim Tab Installation S3 29 Elevator Trim Tab Actuator S3 30 Electric Elevator Trim System S3 31 Rudder Pedal Assembly Rudder S3 32 Rudder Control System Ru Ru Ru Ru Ru Ru Ruu Ru R R R Ru Ru Ru Ru R Ru R R Ru Ru R Ru Ru Ruu Ru R Ruuu R Ruu Ruu Ruuddd dd dd dddddd dd dddddddddd ddd ddddddd ddddddd er Rudder S3 33 Rudder Installation S3 34 1960-1966 Rudder Trim System S3 35 1967 and On Rudder Trim System CPA Tech Note# 014 RIGGING – The Key To Speed Section Four Legacy 210 LANDING GEAR RETRACTION SYSTEM SEQUENCE OF EVENTS FOR AIRCRAFT WITH ENGINE DRIVEN HYDRAULIC PUMPS 1960 THRU 1971 S4 3 1960-1971 Landing Gear Sequence S4 4 1960-1971 Simplified Electric Schematic S4 5 Nose Gear Downlock S4 6 Main Gear Downlocks – Spring Steel Gear 17 1. Bolt 2. Retainer 3. Washer 4. Cap 5. Bearing 6. Washer 7. Sector Gear 8. Shaft 9. Seal 10. Bearing 11. Inner Race 12. Bearing 13. Actuator Clamp 14. Pivot Assembly 15. Packing 16. Collar 17. Shaft 18. Bushing 19. Setscrew 20. Nut 21. Washer 22. Inboard Forging 23. Outboard Forging 24. Strut 25. Actuator S4 7 1970 and On Main Landing Gear Installation S4 8 Main Gear Down locks – Tubular Gear S4 9 Retraction Flow Chart 1960 Model 210-210A Retraction System Diagrams S4 10 S4 11 Gear Up, Handle Neutral S4 12 Gear Up, Handle Out S4 13 Handle Down, Doors & Gear Unlocking S4 14 Handle Down, Doors Opening & Gear Extending S4 15 Gear Down, Doors Closed, Handle Releasing S4 16 Gear Locked, Doors Closed, Handle Down Neutral S4 17 Handle Up, Doors Opening S4 18 Handle Up, Gear Retracting S4 19 Handle Releasing, Gear Up, Doors Closed S4 20 Emergency Hand Pump Pressure 1962 Model 210B Retraction System Diagrams S4 21 S4 22 Gear Up, Flaps Up S4 23 Handle Down, Doors Opening S4 24 Doors Open, Gear Extending S4 25 Gear Down, Doors Closing S4 26 Gear Down, Doors Closed, Flaps Extending S4 27 Handle Up, Flaps Up S4 28 Doors Open, Gear Retracting S4 29 Gear Up, Doors Closing S4 30 Gear Up, Doors Closed S4 31 Emergency Hand Pump Pressure 1971 Model 210K Retraction System Diagrams S4 32 S4 33 Gear Up, Doors Closed S4 34 Handle Down, Doors Opening S4 35 Doors Open, Gear Extending S4 36 Gear Down, Doors Closing S4 37 Gear Down, Doors Closed, Handle Pressure Building S4 38 Handle Up, Doors Opening S4 39 Doors Open, Gear Retracting S4 40 Gear Up, Doors Closing S4 41 Gear Up, Doors Closed, Handle Pressure Building S4 42 Emergency Hand Pump Pressure /HJDF\ :+((/6 %5$.(6 6HFWLRQ)LYH Nose Gear Installation S5 2 1RVH:KHHOV 6 1RVH*HDU7LUHDQG :KHHO$VVHPEO\ 6 1RVH6WUXW$VVHPEO\ 6 1RVH6WUXW$VVHPEO\ 6 1RVH6WUXW$VVHPEO\ 6 1RVH*HDU 7RUTXH/LQNV 6 1RVH*HDU 7RUTXH/LQNV 6 6KLPP\'DPSHU 6 What about the shimmy damper? /RUG" 6 1RVH:KHHO6WHHULQJ ,QVWDOODWLRQ 6 5XGGHU3HGDO$VVHPEO\ 6 3DUNLQJ%UDNH6\VWHP 6 %UDNH0DVWHU&\OLQGHU 8VHGWKUX 6 0DLQ/DQGLQJ*HDU ,QVWDOODWLRQ 6 DQG2Q 0DLQ/DQGLQJ*HDU ,QVWDOODWLRQ 6 DQG2Q 0DLQ/DQGLQJ*HDU ,QVWDOODWLRQ 6 &OHYHODQG0DLQ :KHHODQG%UDNH 6 0DLQ*HDU7LUH %UDNH$VVHPEO\ 6 &OHYHODQG0DLQ :KHHODQG%UDNH 6 %UDNH/LQLQJ &RQGLWLRQLQJ3UR 6 :KHHO $OLJQPHQW 6 4XHVWLRQV" 6HFWLRQ6L[ /HJDF\ )8(/6<67(0 )XHO6\VWHP 6 )XHO6\VWHP 6 WR61 6 61WKUX 0RGLILHG%&' )XHO6\VWHP 6 )XHO6\VWHP 6 7 6 73 6

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___________ Max MAP? ___________ Max FF TIT max and normals CHT Max Oil Temp Red line 6 Know Your Baselines EGT at take off TIT normals in flight CHT in climb & cruise Oil pressure at 180 degrees Buss voltages 6 6 6 Tires – just to make a point 6 Cylinder Arrangement - right side (*7 (*7 (*7 7,7ULJKW &</ &</ &</ ([KDXVW 7UDQVLWLRQ 6 Cylinder Arrangement - left side &</ &</ &</ (*7 7,7OHIW (*7 (*7 &+7SUREH 6 Ignition Configuration /HIW0DJQHWR 7RS 7RS 7RS %RWWRP %RWWRP %RWWRP 6 Ignition Configuration 5LJKW 0DJQHWR %RWWRP %RWWRP %RWWRP 7RS 7RS 7RS 6 Magneto Impulse Coupling 6 NEVER turn the propeller in its operating direction. 6 Ignition System System Ops Check RPM drop EGT rise on one spark plug 6 Ignition System 6 6 Pre-ignition - broken ceramic and more. 6 Destructive Detonation sample Destructive Detonation sample 3RZHUXS )XHOIORZ &+7 H[FXUVLRQ VWDUW (*7 &+7 (*7 ([FXUVLRQ EHIRUH&+7 6 Oil Pressure vs Oil Temp 6 Oil Pressure vs Oil Temp 7\SLFDORLOSUHVVXUHDWGHJUHHV)VKRXOGEHSVL 6 Oil Pressure 6 Fuel Flow )XHO)ORZ7UDQVGXFHU/RFDWLRQ 6 Fuel Nozzles – dirt simple Naturally Aspirated Turbocharged 5HIHUHQFHWR 8SSHU'HFN SUHVVXUH 5HIHUHQFHWR $PELHQW SUHVVXUH 6 High CHT Take off #3 CHT is high but goes low in cruise. Note the EGT during the two extra leaning events. CHT is a good indicator of power. 6 Lean Test www.gami.com for full procedure Exposes fuel injector imbalance and condition (should be used to determine maintenance action) Can help identify induction leaks Establishes base line for certain maintenance events (injector cleaning) 6 Lean Test - Detail 6 Lean Test Up close view of Fuel Flow on each cylinder when it peaked. Your results may vary. :) 6 Don’t clean the fuel injector nozzles unless the data supports it. Minimize MIF 6 Induction Leak Test 6 Amps vs Volts %DWWHU\ $OWHUQDWRU ([SRVHGWRWKH (OHPHQWV 6 Troubleshooting Exercise #1 6 Troubleshooting Exercise #2 6 Putting It Together Know your Baselines Watch for Baselines in all flight situations React to Changes based on actual data. 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Type certificate, explained

What's in the CESSNA TURBO 210L 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 3A21Rev 47· Issued 2009

Read the full TCDS