Columbia 400 Pilot Operating Handbook
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Columbia 400 Pilot Operating Handbook

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Columbia Aircraft Manufacturing Corporation
THIS HANDBOOK INCLUDES THE MATERIAL REQUIRED TO BE FURNISHED TO THE PILOT
BY THE FEDERAL AVIATION REGULATIONS AND ADDITIONAL INFORMATION PROVIDED
BY THE MANUFACTURER, AND CONSTITUTES THE FAA APPROVED AIRPLANE FLIGHT
This Handbook meets GAMA Specification No. 1,
Operating Handbook,
By: E. P. Kolano
(Name)
Date: 31 Mar 06
PILOT'S OPERATING HANDBOOK
FAA APPROVED AIRPLANE

FLIGHT MANUAL

(Document No. RC050005 Revision C)
Columbia 400 (LC41-550FG)
22550 Nelson Road
Bend Municipal Airport
Bend, Oregon 97701
Phone: (541) 318-1144
Fax: (541) 318-1177
Serial Number
Registration Number
Type Certificate No. A00003SE
issued February 15, 1975 and revised September
Approved by the Federal Aviation Administration
Title: Manager. Seattle Area Certification Office
Initial Issue: _09 Dec 05__
AND
41XXX
MANUAL.
1, 1984.
Specification for Pilot's
Revised: 10 Oct 06

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  • Page 1: Flight Manual

    PILOT'S OPERATING HANDBOOK FAA APPROVED AIRPLANE FLIGHT MANUAL (Document No. RC050005 Revision C) Columbia 400 (LC41-550FG) Columbia Aircraft Manufacturing Corporation 22550 Nelson Road Bend Municipal Airport Bend, Oregon 97701 Phone: (541) 318-1144 Fax: (541) 318-1177 Serial Number 41XXX Registration Number Type Certificate No.
  • Page 3 Log of Normal Revisions Columbia 400 (LC41-550FG) PILOT OPERATING HANDBOOK LOG OF NORMAL REVISIONS Normal Description of Revision or Approved By Revision Revised Pages Referenced Narrative Date Discussion Pages Initial Revision Title Page, iii, vii to xvi, 2-6, 2-11 to 2-14, 2-18, 2-...
  • Page 4 Log of Normal Revisions Columbia 400 (LC41-550FG) This Page Intentionally Left Blank RC050005 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: C/10-10-2006...
  • Page 5 Log of Temporary Revisions Columbia 400 (LC41-550FG) PILOT OPERATING HANDBOOK LOG OF TEMPORARY REVISIONS Temporary Revision Revised Description of Revision or Referenced Approved By No. and Pages Narrative Discussion Pages Date Date Initial Issue of Manual: December 9, 2005 RC050005...
  • Page 6 Log of Temporary Revisions Columbia 400 (LC41-550FG) This Page Intentionally Left Blank RC050005 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: C/10-10-2006...
  • Page 7 List of Effective Pages Columbia 400 (LC41-550FG) LIST OF EFFECTIVE PAGES LIST OF EFFECTIVE PAGES Reissue Added Pages Reissue Added Pages Page Page Page Page 1-12 INTRODUCTION PAGES 1-13 Title 1-14 1-15 1-16 1-17 1-18 1-19 1-20 viii SECTION 2 (Limitations)
  • Page 8 List of Effective Pages Columbia 400 (LC41-550FG) LIST OF EFFECTIVE PAGES LIST OF EFFECTIVE PAGES Reissue Added Pages Reissue Added Pages Page Page Page Page SECTION 3 (Emergency Procedures) 4-10 4-11 4-12 4-13 4-14 3-10 4-15 3-11 4-16 3-12 4-17...
  • Page 9 List of Effective Pages Columbia 400 (LC41-550FG) LIST OF EFFECTIVE PAGES LIST OF EFFECTIVE PAGES Reissue Added Pages Reissue Added Pages Page Page Page Page 5-44 5-37 5-38 5-39 5-40 5-41 5-42 5-10 5-43 5-11 5-44 5-12 SECTION 6 (Weight & Balance)
  • Page 10 List of Effective Pages Columbia 400 (LC41-550FG) LIST OF EFFECTIVE PAGES LIST OF EFFECTIVE PAGES Reissue Added Pages Reissue Added Pages Page Page Page Page 6-A5 6-A15 7-18 6-A6 6-A16 7-19 6-A7 6-A17 7-20 6-A8 6-A18 7-21 6-A9 7-22 6-A10...
  • Page 11 List of Effective Pages Columbia 400 (LC41-550FG) LIST OF EFFECTIVE PAGES LIST OF EFFECTIVE PAGES Reissue Added Pages Reissue Added Pages Page Page Page Page 7-51 7-52 7-53 7-54 7-55 7-56 7-57 7-58 8-10 7-59 8-11 7-60 8-12 7-61 8-13...
  • Page 12 List of Effective Pages Columbia 400 (LC41-550FG) This Page Intentionally Left Blank RC050005 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: C/10-10-2006...
  • Page 13 Narrative Discussion of Revisions Columbia 400 (LC41-550FG) NARRATIVE DISCUSSION OF REVISIONS Revision Page Comment Level Initial revision. Title Page, Revised to indicate Revision A. iii, vii Revised LOEP. through xvi Revised Narrative Discussion of Revisions. Revised Figure 2-3. Added approach operation limitation at propeller RPM of approx.
  • Page 14 Narrative Discussion of Revisions Columbia 400 (LC41-550FG) NARRATIVE DISCUSSION OF REVISIONS Revision Page Comment Level Added paragraph directing fuel pump switch be off for descent and landing in the Descent section. Changed “boost” to “fuel” in the Balked Landings section.
  • Page 15 Narrative Discussion of Revisions Columbia 400 (LC41-550FG) NARRATIVE DISCUSSION OF REVISIONS Revision Page Comment Level Alerts, TAWS Alerts, and TAWS System Status Annunciations and Other Annunciations sections. Revised the Backup Attitude Indicator section. Revised description of the Kollsman Window in the Backup Altimeter section.
  • Page 16 Narrative Discussion of Revisions Columbia 400 (LC41-550FG) NARRATIVE DISCUSSION OF REVISIONS Revision Page Comment Level Title Page, Revised to indicate Revision B. iii, vii Revised LOEP. through xvi Revised Narrative Discussion of Revisions. Revised “Limit Load” to “Limit Load Factor”, “Ultimate Load” to 1-9 to “Ultimate Load Factor”...
  • Page 17 Changed first Warning to Note in the Garmin G1000 Integrated Cockpit System section. Revised the Alerts Window paragraph under the Annunciation and 7-23 to 7-29 Alerts section. Changed all occurrences of “Columbia 350/400” to “Columbia 400”. 7-35 Replaced Figure 7-14. 7-42 Deleted rudder hold from the Left Bus paragraph.
  • Page 18 Narrative Discussion of Revisions Columbia 400 (LC41-550FG) NARRATIVE DISCUSSION OF REVISIONS Revision Page Comment Level source switch under the Static Air Source Blockage section. Revised the bullet list in the first paragraph of the Oxygen System section. Repaginated pages. Deleted pages 3-35 and 3-36.
  • Page 19 Narrative Discussion of Revisions Columbia 400 (LC41-550FG) NARRATIVE DISCUSSION OF REVISIONS Revision Page Comment Level Changed “dimmer thumb-wheel” to “dimmer” in the Wing Flaps 7-13 section. Added Warning to the Door section. DO NOT open door during flight. Changed “Door Open” to “DOOR OPEN” in the Latching 7-15 and 7- Mechanism and Door Seal System sections.
  • Page 20 Narrative Discussion of Revisions Columbia 400 (LC41-550FG) This Page Intentionally Left Blank RC050005 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: C/10-10-2006...

  • Page 21: Table Of Contents

    Section 1 Columbia 400 (LC41-550FG) General Section 1 General TABLE OF CONTENTS THREE-VIEW DRAWING OF THE AIRPLANE ............... 1-2 INTRODUCTION ......................... 1-3 DESCRIPTIVE DATA ........................1-4 Engine ........................... 1-4 Propeller ..........................1-4 Fuel ............................1-4 Oil ............................1-4 Maximum Certificated Weights ................... 1-5 Typical Airplane Weights .....................

  • Page 22: General

    Section 1 General Columbia 400 (LC41-550FG) THREE-VIEW DRAWING OF THE AIRPLANE SPECIFICATIONS Wing Area 141.2 ft. (13.1 m Wing Span 35.8 ft. (10.9 m) Length 25.2 ft. (7.68 m) Empty Weight (±) 2500 lbs. (1134 kg) Gross Weight 3600 lbs. (1633 kg)

  • Page 23: Introduction

    Section 1 Columbia 400 (LC41-550FG) General Section 1 General INTRODUCTION This handbook is written in nine sections and includes the material required to be furnished to the pilot by Federal Aviation Regulations and additional information provided by the manufacturer and constitutes the FAA Approved Airplane Flight Manual.

  • Page 24: Descriptive Data

    Section 1 General Columbia 400 (LC41-550FG) DESCRIPTIVE DATA ENGINE Number of Engines: 1 Engine Manufacturer: Teledyne Continental Engine Model Number: TSIO-550-C Engine Type: Twin-turbocharged, direct drive, air-cooled, horizontally opposed, fuel-injected, six- cylinder engine with 552 in. (9.0 L) displacement Takeoff Power: 310 BHP at 2600 RPM , 35.5 in of Hg Maximum Continuous Power: 310 BHP at 2600 RPM Maximum Normal Operating Power: 262 BHP (85%) at 2500 RPM, and 33.5 in of Hg...

  • Page 25: Maximum Certificated Weights

    Section 1 Columbia 400 (LC41-550FG) General Total Oil Capacity Sump: 8 Quarts (7.6 L) Total: 10 Quarts (9.5 L) Drain and Refill Quantity: 8 Quarts (7.6 L) Oil Quantity Operating Range: 6 to 8 Quarts (5.7 to 7.6 L) NOTE The first time the airplane is filled with oil, additional oil is required for the filter, oil cooler, and propeller dome.

  • Page 26: Abbreviations, Terminology, And Symbols

    Section 1 General Columbia 400 (LC41-550FG) ABBREVIATIONS, TERMINOLOGY, AND SYMBOLS AIRSPEED TERMINOLOGY Calibrated Airspeed means the indicated speed of an aircraft, corrected for position and instrument error. Calibrated airspeed is equal to true airspeed in standard atmosphere at sea level.

  • Page 27: Meteorological Terminology

    Section 1 Columbia 400 (LC41-550FG) General METEOROLOGICAL TERMINOLOGY International Standard Atmosphere in which: The air is a dry perfect gas; The temperature at sea level (SL) is 15° C (59° F); The pressure at SL is 29.92 inches of Hg (1013.2 mb);...

  • Page 28: Airplane Performance & Flight Planning Terminology

    Section 1 General Columbia 400 (LC41-550FG) Revolutions Per Minute is a measure of engine and/or propeller speed. Stall Strip Small triangular strips installed along the leading edge of an airplane wing to disrupt the airflow at high angles of attack in a controlled way. The strips improve stall characteristics and spin recovery.
  • Page 29 Section 1 Columbia 400 (LC41-550FG) General gravity (C.G.) of an item. Basic Empty The Basic Empty Weight is the Standard Empty Weight plus optional Weight equipment. The Center of Gravity is the point at which the airplane will balance if suspended.

  • Page 30: Miscellaneous

    Section 1 General Columbia 400 (LC41-550FG) Standard Empty This is the weight of a standard airplane including unusable fuel, full Weight operating fluids, and full oil. Station The Station is a location along the airplane's fuselage usually given in terms of distance from the reference datum, i.e., Station 40 would be 40 inches from...

  • Page 31: Supplements

    Section 1 Columbia 400 (LC41-550FG) General SUPPLEMENTS Equipment, which is not covered in Sections 1 through 8 of the Information Manual, is included in Section 9, as applicable. USE OF THE TERMS WARNING, CAUTION, AND NOTE The following conventions will be used for the terms, Warning, Caution, and Note.

  • Page 32: Kilograms And Pounds

    Section 1 General Columbia 400 (LC41-550FG) KILOGRAMS AND POUNDS CONVERTING KILOGRAMS TO POUNDS Kilograms 2.205 4.409 6.614 8.818 11.023 13.228 15.432 17.637 19.842 22.046 24.251 26.455 28.660 30.865 33.069 35.274 37.479 39.683 41.888 44.092 46.297 48.502 50.706 52.911 55.116 57.320 59.525...

  • Page 33: Feet And Meters

    Section 1 Columbia 400 (LC41-550FG) General FEET AND METERS CONVERTING METERS TO FEET Meters 3.281 6.562 9.843 13.123 16.404 19.685 22.966 26.247 29.528 32.808 36.089 39.370 42.651 45.932 49.213 52.493 55.774 59.055 62.336 65.617 68.898 72.178 75.459 78.740 82.021 85.302 88.583...

  • Page 34: Inches And Centimeters

    Section 1 General Columbia 400 (LC41-550FG) INCHES AND CENTIMETERS CONVERTING CENTIMETERS TO INCHES Centimeters 0.394 0.787 1.181 1.575 1.969 2.362 2.756 3.150 3.543 3.937 4.331 4.724 5.118 5.512 5.906 6.299 6.693 7.087 7.480 7.874 8.268 8.661 9.055 9.449 9.843 10.236 10.630...

  • Page 35: Nautical Miles, Statute Miles, And Kilometers

    Section 1 Columbia 400 (LC41-550FG) General NAUTICAL MILES, STATUTE MILES, AND KILOMETERS Nautical Statute Kilo- Nautical Statute Kilo- Nautical Statute Kilo- Miles Miles meters Miles Miles meters Miles Miles meters Figure 1 - 8 Initial Issue of Manual: December 9, 2005...

  • Page 36: Liters, Imperial Gallons, And U.s. Gallons

    Section 1 General Columbia 400 (LC41-550FG) LITERS, IMPERIAL GALLONS, AND U.S. GALLONS CONVERTING LITERS TO IMPERIAL GALLONS Liters 0.22 0.44 0.66 0.88 1.10 1.32 1.54 1.76 1.98 2.20 2.42 2.64 2.86 3.08 3.30 3.52 3.74 3.96 4.18 4.40 4.62 4.84 5.06...
  • Page 37 Section 1 Columbia 400 (LC41-550FG) General LITERS, IMPERIAL GALLONS, AND U.S. GALLONS (Continued) CONVERTING LITERS TO U.S. GALLONS Liters 0.00 0.26 0.53 0.79 1.06 1.32 1.59 1.85 2.11 2.38 2.64 2.91 3.17 3.43 3.70 3.96 4.23 4.49 4.76 5.02 5.28 5.55...
  • Page 38 Section 1 General Columbia 400 (LC41-550FG) LITERS, IMPERIAL GALLONS, AND U.S. GALLONS (Continued) CONVERTING IMPERIAL GALLONS TO U.S. GALLONS Imperial Gallons 0.00 1.20 2.40 3.60 4.80 6.01 7.21 8.41 9.61 10.81 12.01 13.21 14.41 15.61 16.81 18.02 19.22 20.42 21.62 22.82...

  • Page 39: Temperature Relationship (Fahrenheit And Celsius)

    Section 1 Columbia 400 (LC41-550FG) General TEMPERATURE RELATIONSHIPS (FAHRENHEIT AND CELSIUS) Fahrenheit Celsius Fahrenheit Celsius Fahrenheit Celsius -40F -40C 145F 330F 166C -35F -37C 150F 335F 168C -30F -34C 155F 340F 171C -25F -32C 160F 345F 174C -20F -29C 165F...

  • Page 40: Fuel Weights And Conversion Relationships

    Section 1 General Columbia 400 (LC41-550FG) FUEL WEIGHTS AND CONVERSION RELATIONSHIPS The table below summarizes the weights and conversion relationships for liters, U.S. Gallons, and Imperial Gallons. The chart values are only to two decimal places. The table is intended to provide approximate values for converting from one particular quantity of measurement to another.
  • Page 41 Section 2 Columbia 400 (LC41-550FG) Limitations Section 2 Limitations TABLE OF CONTENTS INTRODUCTION .......................... 2-2 LIMITATIONS..........................2-3 Airspeed Limitations ......................2-3 Airspeed Indicator Markings ....................2-3 Powerplant Limitations......................2-4 Powerplant Fuel and Oil Data ....................2-4 Oil Grades Recommended for Various Average Temperature Ranges .....................

  • Page 42: Limitations

    Section 2 Limitations Columbia 400 (LC41-550FG) Section 2 Limitations INTRODUCTION Section 2 contains the operating limitations of this airplane. The Federal Aviation Administration approves the limitations included in this Section. These include operating limitations, instrument markings, and basic placards necessary for the safe operation of the airplane, the airplane’s engine, the airplane’s standard systems, and the airplane’s standard equipment.

  • Page 43: Limitations

    Section 2 Columbia 400 (LC41-550FG) Limitations LIMITATIONS AIRSPEED LIMITATIONS The airspeed limitations below are based on the maximum gross takeoff weight of 3600 lbs (1633 kg). The maximum operating maneuvering speeds (V ) and applicable gross weight limitations are shown in Figure 2 - 1.

  • Page 44: Powerplant Limitations

    Section 2 Limitations Columbia 400 (LC41-550FG) POWERPLANT LIMITATIONS Number of Engines: One (1) Engine Manufacturer: Teledyne Continental Engine Model Number: TSIO-550-C Recommended Time Between Overhaul: 2000 Hours (Time in Service) Maximum Power: 310 BHP at 2600 RPM Maximum Manifold Pressure: 35.5 inches of Hg Minimum Power Setting Above 18,000 ft.: 15 inches of Hg and 2200 RPM...

  • Page 45: Powerplant Instrument Markings

    Section 2 Columbia 400 (LC41-550FG) Limitations POWERPLANT INSTRUMENT MARKINGS The following table, Figure 2 - 3, shows applicable color-coded ranges for the various powerplant gauges displayed on the MFD. WHITE GREEN RED LINE RANGE YELLOW RANGE RED LINE Minimum RANGE...

  • Page 46: Weight Limits

    Section 2 Limitations Columbia 400 (LC41-550FG) WEIGHT LIMITS Utility Category Maximum Ramp Weight: 3600 lbs. (1633 kg) Maximum Empty Weight: 2708 lbs. (1228 kg) Maximum Takeoff Weight: 3600 lbs. (1633 kg) Maximum Landing Weight: 3420 lbs. (1551 kg) Maximum Baggage Weight:* 120 lbs.

  • Page 47: Approved Acrobatic Maneuvers

    Section 2 Columbia 400 (LC41-550FG) Limitations APPROVED ACROBATIC MANEUVERS MANEUVER ENTRY SPEED Chandelles 150 KIAS Lazy Eights 150 KIAS Steep Turns 150 KIAS Stalls Slow Deceleration* Ensure that maximum fuel imbalance does not exceed 10 gallons (38 L). Figure 2 - 6 While there are no limitations to the performance of the acrobatic maneuvers listed in Figure 2 - 6, it is recommended that the pilot not exceed 60º...

  • Page 48: Flight Load Factor Limits

    Section 2 Limitations Columbia 400 (LC41-550FG) FLIGHT LOAD FACTOR LIMITS Utility Category - Maximum flight load factors for all weights are: Flaps Position Max. Load Factor Up (Cruise Position) +4.4g and -1.76g Down (Landing Position) +2.0g and -0.0g KINDS OF OPERATION LIMITS AND PILOT REQUIREMENTS The airplane has the necessary equipment available and is certified for daytime and nighttime VFR and IFR operations with only one pilot.
  • Page 49 The autopilot must be off during takeoff and landing. The autopilot must be disengaged below 200’ AGL during approach operations and minimum engagement height on takeoff is 400’ AGL. Cruise engagement minimum height is 1000’ AGL. Autopilot operation with the G1000 in the reversionary (Display Backup) mode is limited to training operations and display failure operations.

  • Page 50: Approach Operation Limitations

    2.8 KIAS for each 1000 feet above 12,000 feet MSL. The autopilot maximum operating speed at 25,000 ft is 174 KIAS 2. Operation of the autopilot less than 400 feet above ground level is prohibited for takeoff. 3. Operation of the autopilot during takeoff and landing is prohibited.

  • Page 51: Oxygen Limitations

    Section 2 Columbia 400 (LC41-550FG) Limitations OXYGEN LIMITATIONS A4 Flowmeter and standard cannulas may be used for altitudes up to 18,000 ft (Pressure Altitude). Cannulas may only be used by persons not experiencing nasal congestion. A4 Flowmeter with oxygen mask may be used for altitudes up to 25,000 ft (Pressure Altitude) ONLY.

  • Page 52: Other Limitations

    Section 2 Limitations Columbia 400 (LC41-550FG) When two aircraft are interrogated at the same instant, the replies received by TCAD can be mixed, degrading the ability to decode the replies. This is more likely to occur in higher density areas, when both aircraft are illuminated at the same moment by the same radar. By using degarbling techniques, the processor can often provide data on the closest threat.

  • Page 53: Placards

    Section 2 Columbia 400 (LC41-550FG) Limitations PLACARDS GENERAL Federal Aviation Regulations require that a number of different placards be prominently displayed on the interior and exterior of the airplane. The placards contain information about the airplane and its operation that is of significant importance. The placard is placed in a location proximate to the item it describes.
  • Page 54 Section 2 Limitations Columbia 400 (LC41-550FG) On Crash Ax On Parking Brake Handle On the Upper Left Side of the Tower Assembly RC050005 Initial Issue of Manual: December 9, 2005 2-14 Latest Revision Level/Date: C/10-10-2006...
  • Page 55 Section 2 Columbia 400 (LC41-550FG) Limitations On Left Panel Behind Pilot’s Control Stick On Instrument Panel to Left of Backup Attitude Indicator Engraved On Fuel Selector Knob and Upper Plate LEFT RIGHT On Top Front of Center Console Initial Issue of Manual: December 9, 2005...
  • Page 56 Section 2 Limitations Columbia 400 (LC41-550FG) On Right Panel Behind Copilot's Control Stick On Flaps Panel On the Compass Without Electric A/C With Electric A/C The magnetic direction indicator is calibrated for level flight with the engine, radios, and strobes operating.
  • Page 57 Section 2 Columbia 400 (LC41-550FG) Limitations Under All Seats Under Left Rear Seat Next to Leveling Washer On Baggage Compartment Door Joggle On Oxygen Fill Port Set into Hat Shelf In Aft Cabin on Aft Baggage Bulkhead On Air Conditioning System Bay Access Cover...

  • Page 58: Exterior Placards

    Section 2 Limitations Columbia 400 (LC41-550FG) EXTERIOR PLACARDS Near Pilot and Passenger Door Handles On Flaps Near Wing Root (Both Sides) Near Fill Cap of Fuel Tank Under Each Wing Near Fuel Drains FOR DRAINING OF WING FUEL SUMP: TO OPEN: PRESS CUP GENTLY INTO BOTTOM OF VALVE TO DRAIN REQUIRED AMOUNT OF FUEL.
  • Page 59 Section 2 Columbia 400 (LC41-550FG) Limitations On Exterior of Fuselage – Forward of Wing on Copilot’s Side On Forward Portion of Nose Gear Fairing TURN LIMIT On Nose Gear Wheel Pant (if installed) On Nose Gear Wheel Pant or Nose Gear Fairing (if nose gear wheel pant not installed)
  • Page 60 Section 2 Limitations Columbia 400 (LC41-550FG) On Exterior of Fuselage – Forward of Wing on Pilot’s Side On Exterior of Gascolator Door (Underside of Fuselage) RC050005 Initial Issue of Manual: December 9, 2005 2-20 Latest Revision Level/Date: C/10-10-2006...
  • Page 61 Section 2 Columbia 400 (LC41-550FG) Limitations On Interior of Gascolator Door On Ground Power Supply Plug Cover Initial Issue of Manual: December 9, 2005 RC050005 Latest Revision Level/Date: C/10-10-2006 2-21...
  • Page 62 Section 2 Limitations Columbia 400 (LC41-550FG) This Page Intentionally Left Blank RC050005 Initial Issue of Manual: December 9, 2005 2-22 Latest Revision Level/Date: C/10-10-2006...
  • Page 63 Airspeeds for Emergency Operations..................3-3 EMERGENCY PROCEDURES CHECKLISTS ................3-4 Engine Failure During Takeoff....................3-4 Engine Failure Immediately After Takeoff (Below 400 feet AGL) ........3-4 Engine Failure During Flight....................3-4 Loss of Oil Pressure....................... 3-4 Procedures After an Engine Restart ..................3-4 Forced Landing (Engine Out or Partial Power..............
  • Page 64 Section 3 Emergency Procedures Columbia 400 (LC41-550FG) General ........................3-18 Aileron or Rudder Failure...................3-18 Elevator Failure......................3-18 Trim Tab Malfunctions 3-19 Fires............................3-19 General ........................3-19 Engine Fires ........................3-19 Cabin Fires ........................3-20 Lightning Strike ........................3-20 Engine and Propeller Problems ...................3-20 Engine Roughness.......................3-20 High Altitude Negative G Loading ................3-20 High Cylinder Head Temperatures................3-20...

  • Page 65: Emergency Procedures

    Section 3 Columbia 400 (LC41-550FG) Emergency Procedures Section 3 Emergency Procedures INTRODUCTION The emergency procedures are included before the normal procedures, as these items have a higher level of importance. The owner of this handbook is encouraged to copy or otherwise tabulate the following emergency procedures in a format that is usable under flight conditions.

  • Page 66: Emergency Procedures Checklists

    7. Ignition Switch ⎯ OFF 8. Left and Right Master Switches ⎯ OFF ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF (Below 400 Feet AGL) 1. Airspeed ⎯ 108 KIAS (with flaps in the up position)* 95 KIAS (with flaps in the takeoff position)* 2.

  • Page 67: Forced Landing

    Section 3 Columbia 400 (LC41-550FG) Emergency Procedures 1. Airspeed ⎯ APPROPRIATE TO THE SITUATION 2. Throttle ⎯ MINIMUM FOR LEVEL FLIGHT AT SAFE SPEED (Until the engine warms up.) 3. Failure Analysis ⎯ DETERMINE CAUSE (Proceed to 3.1, 3.2, or 3.3 as applicable.) Improper Fuel Management ⎯...

  • Page 68: Precautionary Landing With Engine Power

    Columbia 400 (LC41-550FG) WARNING Two special conditions associated with forced landings are specifically applicable to the Columbia 400 (and are different from many other General Aviation airplanes). These differences must be clearly understood. Because the trim tabs and flaps are electrically operated, setting the...

  • Page 69: Engine Fire On The Ground During Startup

    Section 3 Columbia 400 (LC41-550FG) Emergency Procedures 7. Approach ⎯ In high winds and heavy swell conditions, approach into the wind. In light winds and heavy swell conditions, approach parallel to the swell. If no swells exist, approach into the wind.

  • Page 70: Electrical Fire In Flight

    Section 3 Emergency Procedures Columbia 400 (LC41-550FG) 3. Fuel Selector ⎯ OFF 4. Throttle ⎯ CLOSED 5. Ignition Switch ⎯ OFF 6. Heating System ⎯ OFF 7. Propeller Control ⎯ FULL AFT 8. Right Master Switch ⎯ OFF (Left master ON for Comm/Nav and PFD.) 9.

  • Page 71: Spin Recovery

    Section 3 Columbia 400 (LC41-550FG) Emergency Procedures SPIN RECOVERY 1. Throttle ⎯ IDLE 2. Rudder ⎯ FULL AGAINST THE SPIN 3. Elevator ⎯ FULL FORWARD 4. Ailerons ⎯ FULL AGAINST THE SPIN 5. Wing Flaps ⎯ RETRACT 6. Flight Action ⎯ When rotation stops, neutralize controls, then pull out of steep dive to achieve normal attitude.

  • Page 72: Landing With A Flat Nose Tire

    Section 3 Emergency Procedures Columbia 400 (LC41-550FG) 3. Touchdown ⎯ Land on the side of the runway corresponding to the good tire. Touch down on the inflated tire first and maintain full aileron deflection towards the good tire, keeping the flat tire off the ground for as long as possible.

  • Page 73: Left Or Right Bus Failure/Crosstie Discharges Working Bus

    Section 3 Columbia 400 (LC41-550FG) Emergency Procedures 6. Good Alternator ⎯ ENSURE PROPER OPERATION (If the “Alt Off” message is displayed, reduce loads or increase RPM until the annunciation clears and the batteries are in a charging state.) 7. Electrical System ⎯ If the electrical system is not restored, land as soon as practicable.

  • Page 74: Malfunction Of Autopilot

    Section 3 Emergency Procedures Columbia 400 (LC41-550FG) PARTIAL RESTORATION OF A DISABLED TRIM SYSTEM 1. A/P Trim System Switch in Overhead ⎯ ON 2. Malfunction Analysis ⎯ DETERMINE AXIS OF MALFUNCTION 3. Circuit Breaker(s) ⎯ SET PROPERLY FUNCTIONING AXIS BREAKER TO ON MALFUNCTION OF AUTOPILOT 1.

  • Page 75: Something Stuck In Or Interfering With A Doorjamb

    Section 3 Columbia 400 (LC41-550FG) Emergency Procedures NOTE The red annunciation will stay displayed until the CO level drops below 75 ppm. Do not recycle the unit through the circuit breaker, as there is a three minute delay for the CO sensor to stabilize.

  • Page 76: Circuit Breaker Panel

    Section 3 Emergency Procedures Columbia 400 (LC41-550FG) CIRCUIT BREAKER PANEL Many of the above emergency procedures involve resetting or pulling circuit breakers, which requires a good understanding of the panel’s location and layout. The circuit breaker panel is located forward of the pilot’s front seat on the lower side-panel. A picture of the circuit breaker panel and a table listing each circuit breaker is provided in Figure 3 - 2.

  • Page 77: Amplified Emergency Procedures

    10+ knot reduction in landing speed. Engine Failure After Takeoff (Above 400 feet AGL) – With an engine failure after takeoff, there may be time to employ modified restarting procedures. Still, the most important consideration in this situation is to maintain the proper airspeed.

  • Page 78: Best Glide Speed Versus Minimum Rate Of Descent Speed

    Section 3 Emergency Procedures Columbia 400 (LC41-550FG) Best Glide Speed Versus Minimum Rate of Descent Speed – The best distance glide speed will provide the most distance covered over the ground for a given altitude loss, while the minimum rate of descent speed, as its name suggests, will provide the least altitude lost in a given time period.

  • Page 79: Engine Restarts

    Section 3 Columbia 400 (LC41-550FG) Emergency Procedures However, the FUEL PUMP message is independent of this system and will operate anytime the fuel pressure is less than 5.5 psi. In a situation involving a double failure, i.e., a malfunction of the engine driven pump and the latching relay, the FUEL PUMP message will be displayed.

  • Page 80: Forced Landing With The Throttle Stuck In The Idle Position

    Section 3 Emergency Procedures Columbia 400 (LC41-550FG) Forced Landing with the Throttle Stuck in the Idle Position – If the throttle is stuck at idle or near idle power, then a forced landing must be performed. The procedures are somewhat similar to those associated with a complete power loss.

  • Page 81: General

    Section 3 Columbia 400 (LC41-550FG) Emergency Procedures TRIM TAB MALFUNCTIONS The airplane has two axis electrically powered trim tabs. There is an autopilot/trim system on/off switch located on the right side of the overhead rocker switch panel, which turns off power to the actuators in both axes and the autopilot.

  • Page 82: Cabin Fires

    This surge protection comes from large MOVs (metal oxide varistor) soldered in behind the circuit breaker panel. The Columbia 400 system has one MOV on the avionics bus and one on the essential bus. The MOVs are located behind the circuit breaker panel and are not accessible by the pilot in-flight.

  • Page 83: High Cylinder Head Temperatures

    Section 3 Columbia 400 (LC41-550FG) Emergency Procedures resulting in partial or total loss of engine power. If the engine stops running follow the procedures described on page 3-4, Engine Failure During Flight. High Cylinder Head Temperatures – High cylinder head temperatures are often caused by improper leaning at high power setting or vapor formation in the fuel lines (indicated by rising TIT).

  • Page 84: Failure Of Engine Driven Fuel Pump

    Section 3 Emergency Procedures Columbia 400 (LC41-550FG) WARNING If turbocharger failure is a result of a loose, disconnected or burned through exhaust, then a serious fire hazard exists. Failure of Engine Driven Fuel Pump – In the event the engine driven fuel pump fails in flight or during takeoff, there is an electrically operated backup fuel pump located in the wing area.

  • Page 85: Under Voltage

    Section 3 Columbia 400 (LC41-550FG) Emergency Procedures The MFD System page shows bus voltage, as well as battery and alternator current on bar graphs with a boundary around the group marked “electrical”. Under Voltage – If there is an electrical demand above what can be produced by the alternator on either the right or left bus, the battery temporarily satisfies the increased requirement and a battery discharging condition exists.

  • Page 86: Crosstie Switch

    Section 3 Emergency Procedures Columbia 400 (LC41-550FG) the bus to normal operation. If turning on the crosstie switch negatively affects the good bus, the crosstie switch should be turned off and only the remaining bus should be used. The checklist should be reviewed for items that are on the failed bus and rendered inoperative.

  • Page 87: Static Air Source Blockage

    Section 3 Columbia 400 (LC41-550FG) Emergency Procedures STATIC AIR SOURCE BLOCKAGE The static source for the airspeed indicator, the altimeter, the rate of climb indicator, and encoder is located on the right side of the airplane’s fuselage, between the cabin door and the horizontal stabilizer.

  • Page 88: Primary Flight Display

    Section 3 Emergency Procedures Columbia 400 (LC41-550FG) PRIMARY FLIGHT DISPLAY If the malfunction results in improper information from the air data computer and/or an abnormal display of attitude information, use the standby instruments on the left side of the cockpit. The loss of air data (altitude, airspeed) is indicated by the affected indicator being removed from the display and replaced with a red X.

  • Page 89: Cabin Fire

    Section 3 Columbia 400 (LC41-550FG) Emergency Procedures NOTE If oxygen is flowing into the cabin and the oxygen system master softkey on the MFD will not turn the oxygen system off, the guarded overhead switch can be used to terminate the flow of oxygen to the cabin in the event of an emergency as required by the pilot.

  • Page 90: Crash Ax

    Section 3 Emergency Procedures Columbia 400 (LC41-550FG) It is important for the pilot to understand the procedures for using the exterior release. In some instances, the pilot may be incapacitated but conscious and able to offer verbal instructions to ground personnel.
  • Page 91 Section 4 Columbia 400 (LC41-550FG) Normal Procedures Section 4 Normal Procedures TABLE OF CONTENTS INTRODUCTION .......................... 4-3 Indicated Airspeeds for Normal Operations................4-3 NORMAL PROCEDURES CHECKLISTS................... 4-4 Preflight Inspection........................ 4-4 Before Starting Engine ......................4-6 Starting Cold Engine......................4-7 Starting Hot Engine ....................... 4-7 Starting Engine with Ground Power Cart................
  • Page 92 Section 4 Normal Procedures Columbia 400 (LC41-550FG) Engine Starting........................4-18 Normal Starting......................4-18 Under Priming......................4-19 Over Priming.......................4-19 Battery Recharging ......................4-19 Ground Power Operations ..................4-19 Left Battery Inoperative....................4-19 Right Battery Inoperative ...................4-20 Crosstie Operations Checklist....................4-20 Passenger Briefing Card ......................4-20 Control Position Versus Wind Component (Table) ............4-21 Taxiing ..........................4-21...

  • Page 93: Normal Procedures

    Section 4 Columbia 400 (LC41-550FG) Normal Procedures Section 4 Normal Procedures INTRODUCTION Section 4 contains checklists for normal procedures. As mentioned in Section 3, the owner of this handbook is encouraged to copy or otherwise tabulate the following normal procedures checklists in a format that is usable under flight conditions.

  • Page 94: Normal Procedures Checklists

    Section 4 Normal Procedures Columbia 400 (LC41-550FG) NORMAL PROCEDURES CHECKLISTS PREFLIGHT INSPECTION Figure 4-2 depicts the major inspection points, and the arrow shows the sequence for inspecting each point. The inspection sequence in Figure 4 - 2 runs in a clockwise direction; however, it does not matter in which direction the pilot performs the preflight inspection so long as it is systematic.
  • Page 95 Section 4 Columbia 400 (LC41-550FG) Normal Procedures Avionics Switch ⎯ OFF 14.4. 15. Pitot Heat, Propeller Heat, and Exterior Lights ⎯ ON AS REQUIRED, CHECK OPERATION (See Note and Warning that follows.) 16. Stall Warning Vane ⎯ CHECK WARNING HORN 17.

  • Page 96: Before Starting Engine

    Section 4 Normal Procedures Columbia 400 (LC41-550FG) 7. Nose Tire ⎯ CHECK (Remove wheel chocks, check tire for proper inflation.) 8. Right Windscreen, Cowl, Cabin Air Inlet, and Exhaust ⎯ CHECK (Condition, air inlet duct connected, no obstructions, and security of hardware.) Area 5 (Right Wing Leading Edge, Fuel Tank, and Right Tire) 1.

  • Page 97: Starting Cold Engine

    Section 4 Columbia 400 (LC41-550FG) Normal Procedures 8. Circuit Breakers ⎯ CHECK IN 9. Oxygen Masks and Cannulas ⎯ CHECK (Kinks in hose, rips or tears.) 10. Passenger Briefing Card ⎯ ADVISE PASSENGERS TO REVIEW CAUTION There is a significant amount of electric current required to start the engine.

  • Page 98: Starting Engine With Ground Power Cart

    Section 4 Normal Procedures Columbia 400 (LC41-550FG) 13. Throttle ⎯ IDLE (900 to 1000 RPM) 14. Oil Pressure ⎯ CHECK (Ensure the oil pressure gauge reads between 30 to 60 psi.) 15. Left and Right Alternator Switches ⎯ ON STARTING ENGINE WITH GROUND POWER CART...

  • Page 99: Crosstie Operation

    Section 4 Columbia 400 (LC41-550FG) Normal Procedures NAV Radios ⎯ SET 5.2. PFD and Backup Altimeters ⎯ SET 5.3. FMS Flight Plan ⎯ LOADED 5.4. Altitude and Heading Bugs ⎯ SET 5.5. Transponder ⎯ SET CODE 5.6. 6. Oxygen Quantity ⎯ ΝΟΤΕ...

  • Page 100: Ground Operation Of Air Conditioning

    Section 4 Normal Procedures Columbia 400 (LC41-550FG) WARNING If the Autotrim fails any portion of the above check procedures, do not attempt to use the autopilot until the fault is corrected. GROUND OPERATION OF AIR CONDITIONING 1. Control Head ⎯ SELECT MODE AND TEMPERATURE DESIRED 2.

  • Page 101: Minor Spark Plug Fouling

    Section 4 Columbia 400 (LC41-550FG) Normal Procedures 22. Throttle ⎯ VERIFY IDLE, THEN 900 TO 1000 RPM 23. Illuminated Switch Bulb Test ⎯ ALL LAMPS ILLUMINATED 24. Radios ⎯ SET, CROSSCHECK NAV INDICATORS 25. Flight Director ⎯ AS REQUIRED 26. Transponder ⎯ VERIFY CODE 27.

  • Page 102: Normal Takeoff

    7. Elevator Control ⎯ LIFT NOSE AT 75 KIAS 8. Climb Speed ⎯ ACCELERATE TO BEST RATE OF CLIMB SPEED OF 110 KIAS 9. Wing Flaps ⎯ RETRACT (At 400 feet AGL and at or above 95 KIAS.) SHORT FIELD TAKEOFF (Complete “Before Takeoff” checklist first) 1.

  • Page 103: Cruise

    Section 4 Columbia 400 (LC41-550FG) Normal Procedures 3. Fuel Selector ⎯ SET TO RIGHT OR LEFT TANK (As appropriate.) 4. Mixture ⎯ FULL RICH 5. Backup Fuel Pump ⎯ ARMED 6. Vapor Suppression ⎯ ON (Above 18,000 ft.) CRUISE 1. Throttle ⎯ SET AS APPROPRIATE TO ACHIEVE 85% POWER OR LESS (Refer to the cruise performance charts.)

  • Page 104: Expedited Descent

    Section 4 Normal Procedures Columbia 400 (LC41-550FG) 4. Backup Fuel Pump ⎯ OFF 5. Vapor Suppression ⎯ OFF (Below 18,000 ft.) 6. PFD and Backup Altimeters ⎯ SET 7. Altitude Bug ⎯ SET 8. Landing/Taxi Lights ⎯ AS REQUIRED EXPEDITED DESCENT 1.

  • Page 105: Balked Landing

    4. Airspeed ⎯ 82 KIAS 5. Climb ⎯ POSITIVE (Establish Positive Rate of Climb.) 6. Backup Fuel Pump ⎯ ARM 7. Wing Flaps ⎯ RETRACT (At 400 feet AGL and at or above 95 KIAS.) AFTER LANDING 1. Wing Flaps ⎯ UP (Cruise Position) 2.

  • Page 106: Amplified Procedures

    Section 4 Normal Procedures Columbia 400 (LC41-550FG) AMPLIFIED PROCEDURES PREFLIGHT INSPECTION The purpose of the preflight inspection is to ascertain that the airplane is physically capable of completing the intended operation with a high degree of safety. The weather conditions, length of flight, equipment installed, and daylight conditions, to mention a few, will dictate any special considerations that should be employed.

  • Page 107: Fuel Selector

    OFF position, a red FUEL VALVE indication is displayed on the PFD annunciation window. FUEL QUANTITY The Columbia 400 fuel quantity measuring system described on page 7-34 provides a fairly accurate indication of the onboard fuel. The system has two sensors in each tank, and flat spots in the indicating system are minimized.

  • Page 108: Before Starting Engine

    Section 4 Normal Procedures Columbia 400 (LC41-550FG) In some instances, the owners and/or operators prefer to remove the wicks after each flight to prevent breakage during storage. If the wicks are removed, they must be reinstalled before each flight. Flight without the wicks can cause the loss of, or problems with communications and navigation.

  • Page 109: Under Priming

    Section 4 Columbia 400 (LC41-550FG) Normal Procedures important to advance the throttle slowly to maintain the proper fuel-air mixture. Abnormal atmospheric conditions require special procedures and techniques for starting the airplane. Please refer to Warm and Cold Weather Operations later in this section, which begins on page 4-29.

  • Page 110: Right Battery Inoperative

    Section 4 Normal Procedures Columbia 400 (LC41-550FG) Ground Power Not Available – If a ground power unit is not available, the airplane can be started using the right battery. Turn off the flip light for 15 to 20 minutes. This time is needed for the battery to bounce back and develop enough charge to energize the left battery relay.

  • Page 111: Taxiing

    Section 4 Columbia 400 (LC41-550FG) Normal Procedures fastener, and remove the ax from its sheath. It generally works best to strike the corner edge of the window near the doorframe. Several smart blows to the window area around the perimeter of the doorframe will remove enough pieces so that the middle portion of the window can be removed with a few heavy blows.

  • Page 112: Engine Runup

    Section 4 Normal Procedures Columbia 400 (LC41-550FG) cowling around the engine maximizes cooling in flight. However, care must be used to preclude overheating during ground operations. Before starting the engine runup check, be sure the airplane is aligned for the maximum headwind component. Conversely, when the ambient temperature is low, time may be needed for temperatures to reach normal operating ranges.

  • Page 113: Crosswind Takeoff

    Maintain the best angle of climb speed (82 to 86 KIAS) until the airplane is clear of all obstacles. Once past all obstacles, accelerate to the best rate of climb speed (110 KIAS); at or above 400 feet AGL, raise the flaps. The maximum demonstrated crosswind component for takeoff is 23 knots.

  • Page 114: Vapor Suppression

    Section 4 Normal Procedures Columbia 400 (LC41-550FG) NOTE During normal climb operations above 18,000 feet, a minimum engine condition of 2,200 RPM and 15 in.Hg of manifold air pressure are required to insure proper turbocharger operation is maintained. If engine operation below 15 in.Hg of manifold air pressure is necessary, the fuel...

  • Page 115: Control By Turbine Inlet Temperature (Tit)

    Section 4 Columbia 400 (LC41-550FG) Normal Procedures Control by Turbine Inlet Temperature (TIT) – When leaning the mixture using TIT, the pilot should use the TIT gauge on the MFD. At power settings below 85% power, starting at full rich mixture, lean slowly while observing the TIT.

  • Page 116: Approach

    (See Limitations Section). If a missed approach is required, the autopilot may be re-engaged after the aircraft has been reconfigured for and established in a stabilized climb above 400 feet AGL. When making ILS approaches in the Columbia aircraft the pilot should plan to intercept the approach between 100 to 115 KTS.

  • Page 117: Short Field Landings

    Section 4 Columbia 400 (LC41-550FG) Normal Procedures CAUTION Avoid rapid throttle movement in order to reduce manifold pressure overboost. Smooth throttle movements allow the turbochargers to keep pace with the engine operating conditions. The landing attitude is slightly nose up so that the main gear touches the ground first. After touchdown, the back-pressure on the elevator should be released slowly so the nose gear gently touches the ground.

  • Page 118: Stalls

    A drop in attitude that cannot be controlled or maintained with the elevator control normally indicates this break. The maximum altitude loss during power off stalls is approximately 300 ft. to 400 ft. There are fairly benign stall characteristics when the airplane is loaded with a forward CG. In most cases, there is not a discernable break even though the control stick is in the full back position.

  • Page 119: Loading And Stall Characteristics

    CG. However, as the center of gravity moves aft, the stall handling characteristics, in terms of lateral stability, will deteriorate. On the Columbia 400, it is particularly noticeable at higher power settings with flaps in the landing position. Lateral loading is also an issue, particularly with an aft CG.
  • Page 120 Section 4 Normal Procedures Columbia 400 (LC41-550FG) oil sufficiently for proper lubrication of the engine parts. The amount of damage will vary and may not be evident for several hours of operation. In other situations, a problem may occur during or just after takeoff when full power is applied.

  • Page 121: Hot Weather Operations

    Section 4 Columbia 400 (LC41-550FG) Normal Procedures NOTE In cold weather below freezing, ensure engine oil viscosity is SAE 30, 10W30, 15W50, or 20W50. In case of temporary cold weather, consideration should be given to hangaring the airplane between flights.
  • Page 122 This is a courteous thing to do even though the noise abatement procedure might be applicable only to turbine-powered aircraft. The certificated level for the Columbia 400 (LC41-550FG) at 3600 lbs. (1633 kg) gross weight is 81.5 dB(A). The FAA has made no determination that these noise levels are acceptable or unacceptable for operations at any airport.
  • Page 123 Section 5 Columbia 400 (LC41-550FG) Performance Section 5 Performance TABLE OF CONTENTS INTRODUCTION .......................... 5-3 Airspeed Calibration (Flaps Up Position) ..................5-4 Airspeed Calibration (Flaps Takeoff Position) ................5-4 Airspeed Calibration (Flaps Landing Position)................5-5 Equivalent Airspeed Calibration 12,000 ft..................5-5 Equivalent Airspeed Calibration 18,000 ft..................
  • Page 124 Section 5 Performance Columbia 400 (LC41-550FG) This Page Intentionally Left Blank RC050005 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: C/10-10-2006...

  • Page 125: Performance

    Section 5 Columbia 400 (LC41-550FG) Performance INTRODUCTION The performance charts and graphs on the following pages are designed to assist the pilot in determining specific performance characteristics in all phases of flight operations. These phases include takeoff, climb, cruise, descent, and landing. The data in these charts were determined through actual flight tests of the airplane.
  • Page 126 Section 5 Performance Columbia 400 (LC41-550FG) Airspeed Calibration – Normal and Alternate Static Source Flaps – Up Position (0°) Example: 157 KIAS is equal to 152 KCAS when using the alternate static source. Alternate Static Source Normal Static Source Knots Calibrated Airspeed (KCAS) Figure 5 - 2 Airspeed Calibration –...

  • Page 127: Equivalent Airspeed Calibration 12,000 Ft

    Section 5 Columbia 400 (LC41-550FG) Performance Airspeed Calibration – Normal and Alternate Static Source Flaps – Landing Position (40°) Example: 70 KIAS is equal to 71 KCAS when using the normal static source. Normal Static Source Alternate Static Source Knots Calibrated Airspeed (KCAS)

  • Page 128: Equivalent Airspeed Calibration 18,000 Ft

    Section 5 Performance Columbia 400 (LC41-550FG) Equivalent Airspeed Calibration 18,000 ft Knots Equivalent Airspeed (KEAS) Figure 5 - 6 RC050005 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: C/10-10-2006...

  • Page 129: Temperature Conversion

    Section 5 Columbia 400 (LC41-550FG) Performance TEMPERATURE CONVERSION TEMPERATURE CONVERSION --40 FAHRENHEIT Figure 5 - 7 STALL SPEEDS Figure 5 - 8 shows the stalling speed of the airplane for various flap settings and angles of bank. To provide a factor of safety, the tabulated speeds are established using maximum gross weight and the most forward center of gravity (CG), i.e., 3600 pounds with the CG located 108.8 inches from the...

  • Page 130: Stalling Speeds

    Section 5 Performance Columbia 400 (LC41-550FG) generally less than 5 ° but may be up to 15 ° . Example : Using the table below, stall speeds of 64 KIAS and 65 KCAS are indicated for 30° of bank with landing flaps.

  • Page 131: Crosswind, Headwind, And Tailwind Component

    Section 5 Columbia 400 (LC41-550FG) Performance CROSSWIND, HEADWIND, AND TAILWIND COMPONENT 10º 20º 30º 40º 50º 60º 70º 80º Component Component Component Component Component Component Component Component in knots of in knots of in knots of in knots of in knots of...
  • Page 132 Section 5 Performance Columbia 400 (LC41-550FG) This Page Intentionally Left Blank R050005 Initial Issue of Manual: December 9, 2005 5-10 Latest Revision Level/Date: C/10-10-2006...

  • Page 133: Short Field Takeoff Distance (12º - Takeoff Flaps)

    Section 5 Columbia 400 (LC41-550FG) Performance SHORT FIELD TAKEOFF DISTANCE (12º - TAKEOFF FLAPS) ASSOCIATED CONDITIONS EXAMPLE Power Takeoff Power Set Before Brake Release 25°C Flaps 12° (Takeoff position) Pressure Altitude (PA) 4000 ft Runway Paved, Level, Dry Surface Takeoff Weight...

  • Page 135: Short Field Takeoff Speed Schedule

    Section 5 Columbia 400 (LC41-550FG) Performance SHORT FIELD TAKEOFF SPEED SCHEDULE The following chart should be used in conjunction with the takeoff distance chart in Figure 5 - 10 to determine the proper takeoff speed based on aircraft weight. Short Field Takeoff Speed Schedule Speed at 50 ft.

  • Page 136: Maximum Rate Of Climb (Without Flat Triangular Leading Edge Tape On The Wings)

    Section 5 Performance Columbia 400 (LC41-550FG) MAXIMUM RATE OF CLIMB (Without Flat Triangular Leading Edge Tape On The Wings RATE OF CLIMB RATE OF CLIMB RATE OF CLIMB (FT/MIN) (FT/MIN) (FT/MIN) Pressure 3000 lb (1361 kg) 3300 lb (1497 kg)

  • Page 137: Maximum Rate Of Climb (With Flat Triangular Leading Edge Tape On The Wings)

    Section 5 Columbia 400 (LC41-550FG) Performance MAXIMUM RATE OF CLIMB (With Flat Triangular Leading Edge Tape On The Wings ) RATE OF CLIMB RATE OF CLIMB RATE OF CLIMB (FT/MIN) (FT/MIN) (FT/MIN) Pressure 3000 lb (1361 kg) 3300 lb (1497 kg)

  • Page 138: Time, Fuel, And Distance To Climb (No Flat Triangular Leading Edge Tape)

    Section 5 Performance Columbia 400 (LC41-550FG) TIME, FUEL, AND DISTANCE TO CLIMB (No Flat Triangular Leading Edge Tape) Pressure Climb Speed Rate of Climb Time Fuel Used Distance Altitude KIAS Gal. (L) 1400 0.0 (0.0) 1000 1400 0.5 (1.8) 2000 1400 0.9 (3.5)

  • Page 139: Time, Fuel, And Distance To Climb (With Flat Triangular Leading Edge Tape)

    Section 5 Columbia 400 (LC41-550FG) Performance TIME, FUEL, AND DISTANCE TO CLIMB (With Flat Triangular Leading Edge Tape) Pressure Climb Speed Rate of Climb Time Fuel Used Distance Altitude KIAS Gal. (L) 1285 0.0 (0.0) 1000 1285 0.5 (1.9) 2000 1285 1.0 (3.8)

  • Page 140: Cruise Performance Overview

    Section 5 Performance Columbia 400 (LC41-550FG) CRUISE PERFORMANCE OVERVIEW The tables on pages 5-19 through 5-32 contain cruise data to assist in the flight planning process. This information is tabulated for even thousand altitude increments and ranges from Sea Level feet to 25,000 feet.

  • Page 141: Cruise Performance Sea Level Pressure Altitude

    Section 5 Columbia 400 (LC41-550FG) Performance CRUISE PERFORMANCE SEA LEVEL PRESSURE ALTITUDE -5°C 15°C 45°C (Standard (20°C Below Standard) (30°C Above Standard) Temperature) % BHP GPH LPH KTAS % BHP GPH LPH KTAS % BHP GPH LPH KTAS 2500 31.5...
  • Page 142 Section 5 Performance Columbia 400 (LC41-550FG) CRUISE PERFORMANCE 2000 FEET PRESSURE ALTITUDE -9°C 11°C 41°C (Standard Temperature) (20°C Below Standard) (30°C Above Standard) % BHP GPH LPH KTAS % BHP GPH LPH KTAS % BHP GPH LPH KTAS 2500 31.5...

  • Page 143: Cruise Performance 4000 Ft Pressure Altitude

    Section 5 Columbia 400 (LC41-550FG) Performance CRUISE PERFORMANCE 4000 FT PRESSURE ALTITUDE -13°C 7°C 37°C (Standard Temperature) (20°C Below Standard) (30°C Above Standard) % BHP GPH LPH KTAS % BHP GPH LPH KTAS % BHP GPH LPH KTAS 2500 31.5...

  • Page 144: Cruise Performance 6000 Ft Pressure Altitude

    Section 5 Performance Columbia 400 (LC41-550FG) CRUISE PERFORMANCE 6000 FT PRESSURE ALTITUDE -17°C 3°C 33°C (Standard Temperature) (20°C Below Standard) (30°C Above Standard) % BHP GPH LPH KTAS % BHP KTAS % BHP GPH LPH KTAS 2500 31.5 2400 2300 3600 lbs.

  • Page 145: Cruise Performance 8000 Ft Pressure Altitude

    Section 5 Columbia 400 (LC41-550FG) Performance CRUISE PERFORMANCE 8000 FT PRESSURE ALTITUDE -21°C -1°C 29°C (Standard Temperature) (20°C Below Standard) (30°C Above Standard) RPM MP % BHP KTAS % BHP GPH KTAS % BHP GPH LPH KTAS 2500 31.5 2400 2300 3600 lbs.

  • Page 146: Cruise Performance 10000 Ft Pressure Altitude

    Section 5 Performance Columbia 400 (LC41-550FG) CRUISE PERFORMANCE 10000 FT PRESSURE ALTITUDE -25°C -5°C 25°C (Standard Temperature) (20°C Below Standard) (30°C Above Standard) % BHP GPH LPH KTAS % BHP GPH KTAS % BHP GPH KTAS 2500 31.5 2400 2300 3600 lbs.

  • Page 147: Cruise Performance 12000 Ft Pressure Altitude

    Section 5 Columbia 400 (LC41-550FG) Performance CRUISE PERFORMANCE 12000 FT PRESSURE ALTITUDE -29°C -9°C 21°C (Standard Temperature) (20°C Below Standard) (30°C Above Standard) % BHP GPH LPH KTAS % BHP GPH LPH KTAS % BHP GPH LPH KTAS 2500 31.5...

  • Page 148: Cruise Performance 14000 Ft Pressure Altitude

    Section 5 Performance Columbia 400 (LC41-550FG) CRUISE PERFORMANCE 14000 FT PRESSURE ALTITUDE -33°C -13°C 17°C (Standard Temperature) (20°C Below Standard) (30°C Above Standard) % BHP GPH LPH KTAS % BHP GPH LPH KTAS % BHP LPH KTAS 2500 31.5 2400 2300 3600 lbs.

  • Page 149: Cruise Performance 16000 Ft Pressure Altitude

    Section 5 Columbia 400 (LC41-550FG) Performance CRUISE PERFORMANCE 16000 FT PRESSURE ALTITUDE -37°C -17°C 13°C (Standard Temperature) (20°C Below Standard) (30°C Above Standard) % BHP GPH LPH KTAS % BHP GPH KTAS % BHP GPH KTAS 2500 31.5 2400 2300 3600 lbs.

  • Page 150: Cruise Performance 18000 Ft Pressure Altitude

    Section 5 Performance Columbia 400 (LC41-550FG) CRUISE PERFORMANCE 18000 FT PRESSURE ALTITUDE -41°C -21°C 9°C (Standard Temperature) (20°C Below Standard) (30°C Above Standard) RPM MP % BHP GPH KTAS % BHP KTAS % BHP GPH LPH KTAS 2500 31.5 2400 2300 3600 lbs.

  • Page 151: Cruise Performance 20000 Ft Pressure Altitude

    Section 5 Columbia 400 (LC41-550FG) Performance CRUISE PERFORMANCE 20000 FT PRESSURE ALTITUDE -45°C -25°C 5°C (Standard Temperature) (20°C Below Standard) (30°C Above Standard) % BHP KTAS % BHP GPH KTAS % BHP GPH LPH KTAS 2500 31.5 2400 2300 3600 lbs. (1633 kg) Gross Weight Recommended Mixture Setting.

  • Page 152: Cruise Performance 22000 Ft Pressure Altitude

    Section 5 Performance Columbia 400 (LC41-550FG) CRUISE PERFORMANCE 22000 FT PRESSURE ALTITUDE -49°C -29°C 1°C (Standard Temperature) (20°C Below Standard) (30°C Above Standard) % BHP GPH KTAS % BHP KTAS % BHP KTAS 2500 31.5 2400 2300 3600 lbs. (1633 kg) Gross Weight Recommended Mixture Setting.

  • Page 153: Cruise Performance 24000 Ft Pressure Altitude

    Section 5 Columbia 400 (LC41-550FG) Performance CRUISE PERFORMANCE 24000 FT PRESSURE ALTITUDE -53°C -33°C -3°C (Standard Temperature) (20°C Below Standard) (30°C Above Standard) % BHP LPH KTAS % BHP LPH KTAS % BHP GPH LPH KTAS 2500 31.5 2400 2300 3600 lbs.

  • Page 154: Cruise Performance 25000 Ft Pressure Altitude

    Section 5 Performance Columbia 400 (LC41-550FG) CRUISE PERFORMANCE 25000 FT PRESSURE ALTITUDE -55°C -35°C -5°C (Standard Temperature) (20°C Below Standard) (30°C Above Standard) % BHP GPH LPH KTAS % BHP KTAS % BHP GPH LPH KTAS 2500 31.5 2400 2300 3600 lbs.

  • Page 155: Lean Of Peak Engine Operation

    RPM (about 2400 RPM). At higher RPM the fuel flow is slightly higher or slightly lower at lower RPM respectively. The power setting in Figure 5 - 31 is actual power. Columbia 400 Fuel Flow over Power Setting Best Power TSIO-550C Lean of Peak TSIO-550C...

  • Page 156: Range Profile

    Section 5 Performance Columbia 400 (LC41-550FG) RANGE PROFILE Figure 5 - 31 RC050005 Initial Issue of Manual: December 9, 2005 5-34 Latest Revision Level/Date: C/10-10-2006...

  • Page 157: Endurance Profile

    Section 5 Columbia 400 (LC41-550FG) Performance ENDURANCE PROFILE Figure 5 - 32 Initial Issue of Manual: December 9, 2005 RC050005 Latest Revision Level/Date: C/10-10-2006 5-35...

  • Page 158: Holding Considerations

    Section 5 Performance Columbia 400 (LC41-550FG) HOLDING CONSIDERATIONS When holding is required, it is recommended that takeoff flaps be used with an indicated airspeed of 120± knots. Depending on temperature, gross weight, and RPM, the manifold pressure will range from about 13 to 17 inches. The fuel consumption has wide variability as well and can range from about 8 to 10 GPH (30.3 to 37.9 LPH).
  • Page 159 Section 5 Columbia 400 (LC41-550FG) Performance TIME, FUEL, AND DISTANCE FOR CRUISE DESCENT The table below, Figure 5 - 34, has information to assist the pilot in estimating cruise descent times, fuel used, and distance traveled from cruise altitude to sea level or to the elevation of the destination airport.
  • Page 160 Section 5 Performance Columbia 400 (LC41-550FG) This Page Intentionally left Blank RC050005 Initial Issue of Manual: December 9, 2005 5-38 Latest Revision Level/Date: C/10-10-2006...

  • Page 161: Short Field Landing Distance (40º - Landing Flaps)

    Section 5 Columbia 400 (LC41-550FG) Performance SHORT FIELD LANDING DISTANCE (40º - LANDING FLAPS) ASSOCIATED CONDITIONS EXAMPLE Power As required to maintain 3° 25°C approach Flaps 40° Pressure Altitude (PA) 4000 ft Runway Paved, Level, Dry Surface Takeoff Weight 3200 lb.

  • Page 163: Landing Speed Schedule

    Section 5 Columbia 400 (LC41-550FG) Performance LANDING SPEED SCHEDULE The following chart should be used in conjunction with the landing distance chart in Figure 5 - 35 to determine the proper landing speed based on aircraft weight. Landing Speed Schedule Speed at 50 ft.
  • Page 164 Section 5 Performance Columbia 400 (LC41-550FG) SOLVE FOR THE FOLLOWING ITEMS Item Solution Comments What is the takeoff ground run Problem is different than example distance at the departure 1150± Feet arrows, i.e., takeoff weight - 3600 airport? lbs. and headwind - 30 knots.

  • Page 165: Oxygen System Duration Charts

    Section 5 Columbia 400 (LC41-550FG) Performance OXYGEN SYSTEM DURATION CHARTS The chart shown in Figure 5 - 37 should be used to determine the amount of oxygen available when using the A4 Flowmeter with cannulas or masks. A4 FLOWMETER WITH CANNULA OR MASKS Oxygen System Usage Duration - A4 FlowMeter - STD Cannula 99% Confidence Tolerance (42 Cu.
  • Page 166 Section 5 Performance Columbia 400 (LC41-550FG) This Page Intentionally Left Blank RC050005 Initial Issue of Manual: December 9, 2005 5-44 Latest Revision Level/Date: C/10-10-2006...
  • Page 167 Section 6 Columbia 400 (LC41-550FG) Weight & Balance - Equipment List Section 6 Weight & Balance Equipment List TABLE OF CONTENTS INTRODUCTION .......................... 6-3 Weight and Balance Procedures .................... 6-3 Equipment List........................6-3 PROCEDURES FOR WEIGHING & DETERMINING EMPTY CG General ...........................
  • Page 168 Section 5 Performance Columbia 400 (LC41-550FG) Chapters 21-24 ........................6-A3 Chapter 25 ........................... 6-A7 Chapters 26-31 ........................6-A9 Chapter 32 .........................6-A11 Chapter 33 .........................6-A12 Chapter 34 .........................6-A13 Chapter 35 .........................6-A17 Chapters 52-77 ........................6-A18 INSTALLED EQUIPMENT LIST (IEL) - APPENDIX B............6-B1...

  • Page 169: Introduction

    For pilot purposes, in the Columbia 400 (LC41-550FG), the zero datum point is one inch aft of the tip of the propeller spinner. All measurements from this point are positive or aft of the datum point and are expressed in inches.

  • Page 170: Procedures For Weighing & Determining Empty Cg

    Section 6 Weight & Balance Columbia 400 (LC41-550FG) PROCEDURES FOR WEIGHING & DETERMINING EMPTY CG GENERAL To determine the empty weight and center of gravity of the airplane, the airplane must be in a level area and in a particular configuration.

  • Page 171: Airplane Leveling

    Section 6 Columbia 400 (LC41-550FG) Weight & Balance Example: Unconservative Calculation Conventionally used fuel specific weight (6 lbs./U. S. gal.) Total Aircraft weight with fuel = 3038 lbs. Weight of fuel (98 gal. x 6 lbs./U. S. gal.) = 588 lbs.

  • Page 172: Using The Permanent Reference Point

    Section 6 Weight & Balance Columbia 400 (LC41-550FG) USING THE PERMANENT REFERENCE POINT To determine the empty weight center of gravity of the airplane, it is more convenient to work with the permanent reference. The permanent reference point on the airplane is located at the forward part of the wing bottom, in the center of the wing saddle and is 97.05 inches aft of the...
  • Page 173 Section 6 Columbia 400 (LC41-550FG) Weight & Balance NOSE GEAR TIRE (MEASUREMENT B) LATERAL REFERENCE LINE BETWEEN MARKS ON THE MAIN GEAR TIRES FUSELAGE STATION 97.05 LOCATION OF PLUMB BOB (MEASUREMENT A) MAIN GEAR TIRES CHALK MARKS Figure 6 - 3 Create a lateral reference line between the two main gear tires.

  • Page 174: Measurements

    Section 6 Weight & Balance Columbia 400 (LC41-550FG) MEASUREMENTS Measure the distance along the longitudinal axis from the permanent reference point (tip of the plumb bob) to the lateral reference line between the main gear tires. This is Measurement A in Figure 6 - 3 and Figure 6 - 4.

  • Page 175: Example Of Empty Center Of Gravity (Cg) Determination

    Section 6 Columbia 400 (LC41-550FG) Weight & Balance 4. Operation No. 4 - Using the formulas shown in Figure 6 - 5 and Figure 6 - 6, determine the arm for the main gear and nose gear. Enter this information into the fifth column.

  • Page 176: Changes In The Airplane's Configuration

    Section 6 Weight & Balance Columbia 400 (LC41-550FG) is summarized in Figure 6 - 8. All required data for determining the empty center of gravity are now available. Scale Weight Tare or Scale Corrected Moments Weight (lbs.) X Reading (lbs.)

  • Page 177: Useful Load And Stations

    Section 6 Columbia 400 (LC41-550FG) Weight & Balance PROCEDURES FOR DETERMINING GROSS WEIGHT LOADED CENTER OF GRAVITY (CG) USEFUL LOAD AND STATIONS The useful load is determined by subtracting the empty weight of the airplane from the maximum allowable gross weight of 3600 pounds. The current information obtained from the Weight &...

  • Page 178: Baggage Configuration Table

    Section 6 Weight & Balance Columbia 400 (LC41-550FG) The floor attachment points define the physical limits of each zone. That is, the area between the forward and middle cross strap defines Zone A, and the middle cross strap and aft attachment points define Zone B.

  • Page 179: Summary Of Loading Stations

    Section 6 Columbia 400 (LC41-550FG) Weight & Balance SUMMARY OF LOADING STATIONS Description Maximum Weight (Inches From Datum) Front Seat Pilot and Passenger 110.0 inches Rear Seat Passenger(s) 141.4 inches Fuel 118.0 inches 588 Lbs. (98 Gallons)* Forward Baggage Area (Zone A) 155.7 inches...

  • Page 180: Sample Problem Calculator Method

    Section 6 Weight & Balance Columbia 400 (LC41-550FG) CALCULATOR METHOD Sample Problem Actual Calculation Calculator Method For This Airplane MOMENTS MOMENTS ITEM ITEM (Lbs.) (Inches) (lbs.-in.) (Lbs.) (Inches) (lbs.-in.) Basic Empty Wt.** 2,485 260,433 Basic Empty Wt. Front Seat Wts.

  • Page 181: Sample Problem Graphical Method

    “envelope.” The center of gravity envelope graph on page 6-19 shows the envelope for the Columbia 400 (LC41-550FG). Using data from the sample problem in Figure 6 - 14, a CG of 109.5 inches at 3450 lbs. gross weight indicates the airplane, as loaded, is within the envelope.

  • Page 182: Other Weight Limitations

    Figure 6 - 15 MAXIMUM EMPTY WEIGHT The maximum empty weight of the Columbia 400 (LC41-550FG) is 2708 pounds. The FAA requires the determination of this weight for FAA certification. For airplanes certified in the IFR utility category, a passenger weight of 190 pounds for each seat plus the fuel weight for 45 minutes of flight are used for this computation.
  • Page 183 Section 6 Columbia 400 (LC41-550FG) Weight & Balance Front Seat Moment Computations 50000 40000 30000 20000 10000 Weight (lbs.) Figure 6 - 16 Rear Seat Moment Computations 60000 50000 40000 30000 20000 10000 Weight (lbs.) Figure 6 - 17 Initial Issue of Manual: December 9, 2005...
  • Page 184 Section 6 Weight & Balance Columbia 400 (LC41-550FG) Fuel Moment Computations 80000 80 Gals. 70000 60000 60 Gals. 50000 40000 30000 20000 40 Gals. 10000 Weight (lbs.) Figure 6 - 18 Baggage Moment Computations 25000 Zone B Baggage 20000 15000...
  • Page 185 Section 6 Columbia 400 (LC41-550FG) Weight & Balance COLUMBIA 400 (LC41-550FG) WEIGHT AND BALANCE ENVELOPE WEIGHT AND CG ENVELOPE LC41-550FG 3900 3800 3700 3600 3500 Max. Landing Weight 3400 Max Zero Fuel Weight 3300 3200 3100 3000 2900 M.E.W. 2800 2700 M.F.W.
  • Page 186 Section 6 Weight & Balance Columbia 400 (LC41-550FG) This Page Intentionally Left Blank RC050005 Initial Issue of Manual: December 9, 2005 6-20 Latest Revision Level/Date: C/10-10-2006...
  • Page 187 Section 6 (Appendix A) (APPENDIX A) Columbia 400 (LC41-550FG) Equipment – Types of Operation EQUIPMENT FOR TYPES OF OPERATION Install Code – The following pages contain a listing of equipment that can be installed in the airplane; this is indicated in the Install Code column by the letters B and O. The meaning of each letter code follows.
  • Page 188 Section 6 (Appendix A) (APPENDIX A) Equipment – Types of Operation Columbia 400 (LC41-550FG) This Page Intentionally Left Blank RC050005 Initial Issue of Manual: December 9, 2005 6A-2 Latest Revision Level/Date: C/10-10-2006...
  • Page 219 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems Section 7 Description of Airplane and Systems TABLE OF CONTENTS INTRODUCTION .......................... 7-5 AIRFRAME AND RELATED ITEMS..................7-6 Basic Construction Techniques ..................... 7-6 Fuselage ........................7-6 Wings and Fuel Tanks ....................7-6 Horizontal Stabilizer.....................
  • Page 220 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) ENGINE............................7-16 Engine Specifications ......................7-16 Turbochargers ........................7-16 Engine Controls ........................7-16 Throttle........................7-16 Propeller........................7-16 Mixture ........................7-16 Engine Sub-systems 7-16 Starter and Ignition ..................... 7-16 Propeller and Governor ....................7-17 Induction ........................
  • Page 221 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems Fuel Quantity Indication..................... 7-34 Fuel Selector ....................... 7-34 Fuel System Diagram ....................7-35 Fuel Low Annunciation Messages ................7-35 Fuel Vents........................7-36 Fuel Drains and Strainer..................... 7-36 Backup Fuel Pump and Vapor Suppression............... 7-36 Primer .........................
  • Page 222 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) MISCELLANEOUS ITEMS......................7-49 Emergency Locator Transmitter (ELT)................7-49 General........................7-49 Artex 200 ELT......................7-49 Switches ......................... 7-49 Testing and Reset Functions .................. 7-49 Artex ME406 ELT...................... 7-50 Accuracy ........................ 7-50 Switch Operation....................
  • Page 223 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems Section 7 Description of Airplane and Systems INTRODUCTION Section 7 provides a basic understanding of the airplane’s airframe, powerplant, systems, avionics, and components. The systems include: electrical and lighting system; flight control system; wing flap system;...
  • Page 224 Columbia 400 (LC41-550FG) AIRFRAME AND RELATED ITEMS The Columbia 400 (LC41-550FG) is a pre-molded, composite built, semi-monocoque, four seat, single engine, low wing, tricycle design airplane. The airplane is certified in the utility category and is used primarily for transportation and related general aviation uses.
  • Page 225 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems Elevator – The elevator is a two part control surface with each half connected by a torque tube. Like the ailerons, most of the stresses are carried by the control surface. The end caps and drive rib used to mount the control’s actuating hardware provide additional structural support.
  • Page 226 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) pages of the MFD. The trim servos are protected by two-amp circuit breakers. See Figure 7 – 2 for an illustration of the trim system. Trim System Diagram Control Stick...
  • Page 227 The owner or operator of the airplane may wish to adjust this tab to accommodate the most frequently used cruise configuration. The procedures for adjusting the manual tab are contained in Chapter 27 of the Columbia 400 Airplane Maintenance Manual . NOTE Do not adjust the manual rudder tab by hand since this can produce an uneven deflection or warping of the tab.
  • Page 228 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) INSTRUMENT PANEL AND COCKPIT LAYOUT DIAGRAM Instrument Panel and Cockpit Flap Panel – Flap Switch and Annunciator Engine Controls Environmental Control System (ECS) Panel or Automatic Climate Control System (ACCS) Panel...
  • Page 229 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems WING FLAPS The airplane is equipped with electric Fowler-type flaps. During flap extension, the flaps move out from the trailing edge of the wing, which increases both the camber and surface area of the wing. A motor located under the front passenger’s seat and protected by a 10-amp circuit breaker powers the...
  • Page 230 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) When the airplane is on the ground, with pressure on the nose strut, the nose wheel is free castoring and has rotational travel through about 120º, 60 ° to the left and 60 ° to the right. When the airplane is in flight with pressure off the nose strut, the nose wheel will self-center, which is accomplished by a key in the cylinder rod and a fixed cam.
  • Page 231 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems DOORS WARNING Do not open any of the airplane doors in flight. The doors are not designed to be opened in flight; subsequent airloads on an opened door will forcefully pull it completely open and detach it from the airplane.
  • Page 232 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) To lock the airplane, first engage the door latching mechanism on the passenger side, and then activate the door lock by moving the interior latch. Next, close and latch the pilot’s door, and use the key to activate the door lock.
  • Page 233 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems passengers in entering and exiting the airplane. The pilot must, in this instance, enter and exit the airplane without the use of a portable device. If a portable step is not used, it is recommended that entering and exiting the airplane be made from the front of the wing.
  • Page 234 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) ENGINE ENGINE SPECIFICATIONS The airplane engine is a Teledyne Continental Motors Aircraft Engine Model TSIO-550-C. It is a twin-turbocharged, horizontally opposed, six-cylinder, fuel injected, air-cooled engine that uses a high-pressure, wet-sump type of oil system for lubrication.
  • Page 235 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems The airplane engine is equipped with Slick 6320, pressurized magnetos with impulse couplings on each magneto. The left magneto fires the three upper left and lower right set of spark plugs, and the right magneto fires the three upper right and lower left set of spark plugs.
  • Page 236 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) induction system when the knob is pulled out. The heated induction air valves are located next to the right and left side turbochargers. When the induction heat control is pulled out, it moves a butterfly inside the valves that opens the airflow for heated air from the lower engine area.
  • Page 237 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems The dipstick and oil filler cap access door are located on the top left engine cowl about two feet from the propeller hub. The engine should not be operated with less than six quarts of oil and must not be filled above eight quarts.
  • Page 238 The following is a general description of the Garmin G1000 Integrated Cockpit System. For operating instructions on the features of the G1000 system, refer to the Garmin G1000 Cockpit Reference Guide for the Columbia 400, document number 190-00567-00. NOTE The G1000 may provide erroneous messages indicating to the pilot that airspace has been penetrated when the airplane is only close to that airspace.
  • Page 239 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems Reversionary Mode – Should a system detected failure occur in either display, the G1000 automatically enters reversionary mode. In reversionary mode, critical fight instrumentation is combined with engine instrumentation on the remaining display. Minimal navigation capability is available on the reversionary mode display.
  • Page 240 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) GCU 476 Remote Keypad – The GCU 476 interfaces with the GDU 104x PFD/MFD. The GCU 476 Remote Keypad provides alphanumeric, softkey, and flight planning function keys used to interface with the G1000.
  • Page 241 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems GDL 69A Data Link Receiver – The GDL 69A is an XM Satellite Radio data link receiver with the addition of XM Satellite Radio audio entertainment. For display of weather information and control of audio channel and volume, the GDL 69A is interfaced to the GDU 1042 via an Ethernet link.
  • Page 242 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) GMU 44 – The GMU 44 Magnetometer measures local magnetic field information. Data is sent to the GRS 77 AHRS for processing to determine aircraft magnetic heading. This unit receives power directly from the GRS 77 and communicates with the GRS 77 using a RS-485 digital interface.
  • Page 243 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems GEA 71 – The GEA 71 receives and processes signals from engine and airframe sensors. Sensor types include engine temperature and pressure sensors as well as fuel measurement and pressure sensors.
  • Page 244 Annunciations and Alerts For a more detailed description of annunciations and alerts displayed on the PFD and/or MFD, refer to the Garmin G1000 Cockpit Reference Guide for the Columbia 400, document number 190- 00567-00. Annunciation Window: The annunciation window displays abbreviated annunciation text.
  • Page 245 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems Aircraft Alerts 1. WARNING Alerts If the DOOR OPEN message is displayed, one or more of the airplane’s doors is not properly secured. If the FUEL VALVE message is displayed, the fuel selector is not set to either the left or right tank, or is not properly seated in the detent of the selected tank.
  • Page 246 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) 3. Annunciation Advisory If the OXYGEN ON message is displayed, this is a reminder to turn off oxygen. If the SPEED BRAKES message is displayed, the speedbrakes are deployed. When deploying the speedbrakes, the message stays off until they are full deployed.
  • Page 247 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems The over voltage relay has been activated. The bus voltage is below 24.0 volts. The left or right alternator has failed. Fuel Pump On – this warning is activated when the fuel pressure is less than 5.5 psi.
  • Page 248 Other Annunciations – For Garmin G1000 system annunciations and message advisories related to the PFD, MFD, LRUs, and databases refer to the Garmin G1000 Cockpit Reference Guide for the Columbia 400, document number 190-00567-00. RC050005 Initial Issue of Manual: December 9, 2005...
  • Page 249 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems FLIGHT INSTRUMENTS The backup attitude, airspeed, and altitude indicators are located in a column next to the PFD. The discussion that follows will identify each instrument. A drawing of the airplane cockpit is shown on page 7-10.
  • Page 250 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) The roll is indicated by displacement from a fixed white index at the top of the instrument. The displacement indications range left and right between 0 ° and 90 ° with major indexes of 30 ° and minor indexes of 10 °...
  • Page 251 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems annual inspections, a routine inspection is performed. Asking your mechanic how much fluid there was in the reservoir after an inspection can give you an idea of how well the airplane has been protected from excessive water accumulation.
  • Page 252 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) ENGINE RELATED SYSTEMS FUEL SYSTEM The fuel system has two tanks that gravity feed to a three-position (Left, Right, and Off) fuel selector valve located in the forward part of the armrest between the pilot and copilot seats. The fuel flows from the selected tank to the auxiliary fuel pump and then to the strainer.

  • Page 253: Fuel Selector

    Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems Fuel System Diagram FUEL FUEL FLOWS FROM CALCULATION EITHER LEFT OR GROUP ON RIGHT TANK THE MFD DEPENDING ON THE SYSTEM PAGE TANK SELECTED LOW FUEL ANNUNCIATION SWITCHES FILLER CAP...

  • Page 254: Environmental Control System (Ecs)

    Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) FUEL or R LOW FUEL message in the PFD annunciation window when there is less than 8 gallons (30 L) of usable fuel remaining in that tank. The fuel warning annunciation message has a 30 second delay switch, which limits false indications during flight in turbulent air conditions.
  • Page 255 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems Airflow – Ram air enters through a duct on the right side of the engine cowling and flows to the fresh air manifold. Cabin heat is produced using heated air off the bleed air valves (sonic nozzles) located on the back of each intercooler.

  • Page 256: Environmental Control System Diagram And Panel

    Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) Environmental Control System Diagram and Panel COLD AIR OUTSIDE HEATED AIR MIXED AIR AIR BLEED NOZZLE INTERCOOLER MANIFOLD VALVE FRONT SEAT FRONT SEAT EYEBALL VENT EYEBALL VENT DEFROSTER CONTROL...

  • Page 257: Electrical And Related Systems

    Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems ELECTRICAL AND RELATED SYSTEMS ELECTRICAL SYSTEM General Description – The electrical system in this aircraft consists of two independent buses, which are referred to as the left bus and right bus. The left and right (continuous output) alternators are 65 amp and 52 amp, respectively, and provide charging power for the two 28 volt lead-acid batteries, as well as system power.
  • Page 258 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) both switches, and pressing the bottom of the battery portion of the split-switch turns off both switches. The battery side of the switch is used on the ground for checking electrical devices and will limit battery drain since power is not required for alternator excitation.

  • Page 259: Summary Of Buses

    Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems Summary of Buses SUMMARY OF BUSES Bus Component Circuit Breaker Audio/MKR 5 amp • Integrated Avionics #2 5 amp • Com #2 5 amp • Transponder 5 amp •...

  • Page 260: Electrical System Diagram

    Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) Electrical System Diagram RIGHT RIGHT ALTERNATOR BATTERY Hobbs Meter Strobe Lights Taxi Light Right Voltage Regulator Door Seal/Power Point GROUND CO Detector POWER Oxygen Attitude Horizon PLUG Display Keypad...

  • Page 261: Airplane Interior Lighting System

    Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems AIRPLANE INTERIOR LIGHTING SYSTEM The interior lighting system is one of the more sophisticated systems available for single-engine, general aviation airplanes. A good understanding of the following discussion is important to properly use all the features of the interior lighting system.

  • Page 262: Summary Of Interior Lights And Switches

    Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) NOTE The slide dimmer switches are “alive” at all times. During daylight operation they should be slid to “off” to increase bulb life. Summary of Interior Lights and Switches...

  • Page 263: Airplane Exterior Lighting System

    Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems AIRPLANE EXTERIOR LIGHTING SYSTEM Aircraft position and anti-collision or strobe lights are required to be lighted whenever the aircraft is in operation. Anti-collision lights, however, need not be lighted when the pilot-in-command determines that, because of operating conditions, it would be in the interest of safety to turn off the lights.

  • Page 264: 12 Vdc Auxiliary Power Outlets

    Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) The procedure for starting the engine using the ground power plug and a power cart is contained on page 4-8 of this manual. 12 VDC AUXILIARY POWER OUTLETS There are two 12 VDC auxiliary power outlets. One located in the front of the center console and the other located in the back of the center console.

  • Page 265: Standard Avionics Installation

    Description of the Airplane and Systems STANDARD AVIONICS INSTALLATION NOTE The Garmin G1000 Cockpit Reference Guide for the Columbia 400, document number 190-00567-00 is the primary source document for operation of the airplane’s avionics and autopilot. This manual describes operation as well as G1000 system integration with other standard and optional systems.
  • Page 266 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) provide a significant reduction in cabin noise. The Bose headset jacks for the pilot and copilot are located under the entertainment center panel in the back of the center console.

  • Page 267: Miscellaneous Items

    Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems MISCELLANEOUS ITEMS EMERGENCY LOCATOR TRANSMITTER (ELT) General – The Emergency Locator Transmitter (ELT) is installed in the airplane as required by Federal Aviation Regulations to aid in search and rescue operations. It is located aft of the baggage compartment hat rack or storage shelf.
  • Page 268 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) move the remote switch to the ARM position. Verify that a signal is no longer audible on 121.5 MHz and that the red light on the remote switch is not flashing.
  • Page 269 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems Self Test Mode – Upon turn-off, the ELT automatically enters a self-test mode that transmits a 406 MHz test coded pulse that monitors certain system functions before returning to the ‘ARM’ed mode.

  • Page 270: Fire Extinguisher

    Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) 3 Flashes – Bad load detect. Detects open or short condition on the antenna output or cable. These problems can probably be fixed by the installer. • Check that the RF cable is connected and in good condition. Perform continuity check of center conductor and shield.

  • Page 271: Lightning Protection/Static Discharge

    The owner or operator of the airplane must only repaint the airplane according to the specifications for Columbia 400 LC41-550FG as shown in the airplane maintenance manual. Static wicks are used to bleed an accumulated static electrical charge off the airplane’s surface and discharge it into the air.
  • Page 272 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) fittings and the high-pressure stainless steel lines to the high-pressure manifold of the regulator valve assembly mounted to the inboard side of the root rib. Also attached to this high-pressure manifold are the stainless steel lines connected to the filler port located in the baggage compartment and to the remote overpressure burst assembly located in the belly of the wing.

  • Page 273: Flowmeter

    Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems OXYGEN ON – Reminder that the oxygen system is still turned on and the aircraft is on the ground. When the OXYGEN annunciation displays, the pilot should confirm the altitude and use oxygen as required.
  • Page 274 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) Filler Port – The filler port for refilling the oxygen bottles is located on the pilot’s side of the hat rack in the aft portion of the baggage compartment. The port is placarded “Oxygen Fill Port Do Not Exceed 2000 p.s.i.”...

  • Page 275: Optional Equipment

    CO concentrations and becomes approximately instant should the CO level reach 400 parts per million by volume (PPM) or above. In case of a CO alert, the red annunciation message will display, the CO level will display on the MFD, and the aural warning will state “Carbon Monoxide”...

  • Page 276: Xm Weather (Wx) Data System

    USA. Broadcast weather information received is displayed on the MFD. For additional information on the Garmin GDL 69A see page 7-23. For operating instructions on the system, refer to the Garmin G1000 Cockpit Reference Guide for the Columbia 400, document number 190- 00567-00.
  • Page 277 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems aircraft configuration). The altitude data from the intruder is referenced to pressure altitude (29.92 inches or 1013mb). The range is determined using radar time of arrival technique. Bearing to the traffic is determined using the dual directional antennas, on the top and bottom of the aircraft.
  • Page 278 If the intruder’s relative altitude is within 200 feet, “Same Altitude” is announced. The TCAD announces “Altitude Unavailable” for non-Mode C TAs. TCAD Display on the G1000 – Refer to the Garmin G1000 Cockpit Reference Guide for the Columbia 400, document number 190-00567-00. RC050005 Initial Issue of Manual: December 9, 2005...

  • Page 279: General

    Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems AUTOMATIC CLIMATE CONTROL SYSTEM (ACCS) General – The Automatic Climate Control System (ACCS), incorporating an R-134a Air Conditioning System in coordination with the aircraft’s Environmental Control System (ECS), is fully automatic and designed to cool and heat the aircraft cabin to desired temperature settings during all phases of flight operations.
  • Page 280 An air conditioning performance evaluation should be performed by an authorized Columbia Aircraft Manufacturing Corporation Service Center to determine and correct the problem prior to resuming the use of the air conditioning portion of the ACCS.
  • Page 281 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems NOTE Ground power operation of the air conditioning will require a 24 V ground power source that can deliver 100 amps during use. NOTE If the air conditioning system is turned off, wait at least 3 minutes before turning it on again.
  • Page 282 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) depressed. The selected fan speed is maintained until it is changed or the “ AUTO ” button is depressed. OAT (Outside Air Temperature) – When depressed, the outside air temperature is displayed as measured by the outside air temperature sensor.
  • Page 283 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems Figure 7 – 28 Turns the compressor On or Off in any Mode. Pressing this button Temperature Display “toggles” the compressor selection On and Off. Displays outside air temperature Raises cabin temperature in 1°...

  • Page 284: General Hints For Accs Operation

    The GFC 700 is a digital Automatic Flight Control System (AFCS) which is fully integrated within the G1000 system avionics architecture. For operating instructions on the features of the GFC 700 system, refer to the Garmin G1000 Cockpit Reference Guide for the Columbia 400, document number 190-00567-00.
  • Page 285 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems WARNING When using GPS autopilot mode in the terminal area, care should be exercised when selecting Vectors to Final on the G1000. When VTF mode is selected without selecting HDG or another autopilot roll mode first, the...
  • Page 286 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) Figure 7 – 30 GTA 82 Trim Adapter – The GTA 82 Trim Adapter is a remote mounted device that is used to allow the GFC 700 to drive a trim actuator. The GTA 82 interfaces with two GIA 63 Integrated Avionics units through serial communication on separate RS-485 ports.
  • Page 287 Section 7 Columbia 400 (LC41-550FG) Description of the Airplane and Systems • APR Key – Selects/deselects the Approach mode • NOSE UP/NOSE DN Keys – Controls the active pitch reference for the Pitch Hold, Vertical Speed, and Flight Level Change modes Figure 7 - 32 Additional AFCS Controls –...
  • Page 288 Section 7 Description of the Airplane and Systems Columbia 400 (LC41-550FG) procedure, autopilot HDG mode may be required for initial maneuvering if the missed approach sequence requires a heading to be flown to a particular altitude. When the aircraft is in position to fly direct to the missed approach hold point, the pilot should select GPS data on the HSI, then unsuspend the GPS waypoint sequencing enabling GPS navigation to the missed approach hold waypoint.
  • Page 289 Fuselage Identification Plate ..................8-3 Publications ........................8-3 Address Information..................... 8-3 SERVICES AND SERVICING ..................... 8-4 Columbia Aircraft Manufacturing Corporation Advisory Service ........8-4 Customer Delivery Package ....................8-4 Fuel Servicing........................8-4 Recommended Fuel Grades..................8-4 Fuel Capacities ......................8-4 Approved Fuel Additives .....................
  • Page 290 Section 8 Handling, Servicing, and Maintenance Columbia 400 (LC41-550FG) Jacking and Leveling ......................8-14 Jacking ........................8-14 Leveling ........................8-15 Storage ..........................8-15 Flyable Storage (7 to 30 days)..................8-15 Temporary Storage (up to 90 days)................8-15 Return to Service from Temporary Storage ............... 8-15 Indefinite Storage (over 90 days) ................

  • Page 291: Introduction

    Maintenance INTRODUCTION This section contains procedures for ground handling of the Columbia 400 (LC41-550FG), as well as recommendations and techniques for routine care of the airplane’s interior and exterior. In addition, maintenance intervals and procedures are addressed. Finally, publications, the Columbia Aircraft Manufacturing Corporation Advisory Service, and servicing information are discussed.

  • Page 292: Services And Servicing

    SERVICES AND SERVICING COLUMBIA AIRCRAFT MANUFACTURING CORPORATION ADVISORY SERVICE Changes that affect the Columbia 400 (LC41-550FG), including the maintenance and operation of the airplane, are provided to all registered owners free of charge. The Columbia Aircraft Manufacturing Corporation Advisory will contain two basic types of data, compulsory and informational.

  • Page 293: Fuel Additive Mixture Table

    Section 8 Columbia 400 (LC41-550FG) Handling, Servicing, and Maintenance Isopropyl Alcohol to the fuel supply in quantities not to exceed 3% of the total. In addition, ethylene glycol monomethyl ether (EGME) and diethylene glycol monomethyl ether (DiEGME) compounds to military specification MIL-I-27686E may be added for this purpose. The ethylene glycol monomethyl ether and diethylene glycol monomethyl ether compounds must be carefully mixed with fuel concentrations not to exceed 0.15 percent by volume.
  • Page 294 Aviation fuel is dyed according to its grade, and on new aircraft like the Columbia 400 (LC41- 550FG), the filler neck is sized to only accept fuel of the proper grade. Still, the color of the fuel shall be verified according to the specifications on page 8-4, since the fuel truck might have been refilled improperly.

  • Page 295: Oil Servicing

    Section 8 Columbia 400 (LC41-550FG) Handling, Servicing, and Maintenance final thoughts about refueling and contamination: First, remember that fuel service personnel are people of unknown training and background. It is always a good idea to personally observe refueling operations. Second, if it is necessary to operate in areas where there is questionable fuel delivery, the use of a portable fuel filter is recommended.

  • Page 296: Battery Replacement Cycles

    Normally, a trained mechanic adds brake fluid. However, this is an approved item of preventive maintenance, and servicing by a private pilot who is the owner or operator is permitted. The brake fluid levels shall be serviced according to instructions contained in the Columbia 400 (LC41-550FG) Maintenance Manual with MIL-H-5606 hydraulic fluid.
  • Page 297 11. Ensure safety cap is installed over the filler port. See the Columbia 400 Maintenance Manual for additional maintenance instructions if oxygen quantity drops faster than the duration charts in Chapter 5 indicate or there is either very high or very low outlet pressure.

  • Page 298: Maintenance And Documentation

    Section 8 Handling, Servicing, and Maintenance Columbia 400 (LC41-550FG) MAINTENANCE AND DOCUMENTATION MAINTENANCE Airplane Inspection Periods – Part 91, Subpart E of the Federal Aviation Regulations requires that each U.S. civil registered airplane not used for hire be inspected every 12 calendar months in accordance with Part 43.

  • Page 299: Airplane Documentation

    Columbia 400 (LC41-550FG) Handling, Servicing, and Maintenance Warranty Work – The Columbia 400 warranty covers basic airframe items manufactured by The Columbia Aircraft Manufacturing Corporation, but does not include tires, batteries, filters, and other consumables. In addition, the engine and its components, avionics, and other replaceable units carry their own separate warranties from their respective manufacturers.
  • Page 300 Section 8 Handling, Servicing, and Maintenance Columbia 400 (LC41-550FG) This system is the best available and ensures that the maintenance history of the airplane and all applicable ADs are precisely documented in a logical format. The system has been in use for more than 20 years and is revered by both mechanics and Part 135 operators.

  • Page 301: Handling And Storage

    Section 8 Columbia 400 (LC41-550FG) Handling, Servicing, and Maintenance HANDLING AND STORAGE GROUND HANDLING Towing – A locking, hand-held tow bar is provided with the airplane and stored in the baggage compartment. The tow bar is inserted into two small holes in the nose wheel fairing, forward of the nose wheel axle.

  • Page 302: Jacking And Leveling

    Section 8 Handling, Servicing, and Maintenance Columbia 400 (LC41-550FG) 2. It is also not a good idea to set the brakes in cold weather. Accumulations of freezing rain, ice, and snow can freeze-weld the brake pad to the disc. Landing or taxiing in standing water at near freezing temperatures can cause similar problems if the brakes are set when the airplane is parked.

  • Page 303: Storage

    Section 8 Columbia 400 (LC41-550FG) Handling, Servicing, and Maintenance Leveling – Please see page 6-5 for information about leveling the airplane. STORAGE The storage of an airplane mostly deals with engine related items. Very little needs to or can be done to preserve the airframe, particularly for flyable and temporary storage.

  • Page 304: Temporary Storage (Up To 90 Days)

    Section 8 Handling, Servicing, and Maintenance Columbia 400 (LC41-550FG) 1. Remove seal plugs, tape, and all methods of tagging the airplane, including items tagged on the airframe. 2. Remove the bottom spark plug from each of the six cylinders, and rotate the propeller several times to remove the preservation oil.
  • Page 305 Section 8 Columbia 400 (LC41-550FG) Handling, Servicing, and Maintenance 3. Remove the bottom spark plugs from each of the six cylinders, and rotate the propeller several times to remove the preservation oil. 4. Apply Champion® thread lubricant to spark plugs in accordance with the manufacturer’s instructions.
  • Page 306 Section 8 Handling, Servicing, and Maintenance Columbia 400 (LC41-550FG) Inspections During Indefinite Storage – The following inspections should be performed while the airplane is in indefinite storage: 1. Check the condition of the dehydrator plugs every 15 days to verify that the color has not changed.

  • Page 307: Airframe And Engine Care

    This good index is required to ensure the continued bonding and integrity of the composite material. Only approved Columbia Aircraft Manufacturing Corporation paint colors are permitted in these areas. Care must be taken to not lay dark, heat absorbing material on the top area of the wings and fuselage.
  • Page 308 Section 8 Handling, Servicing, and Maintenance Columbia 400 (LC41-550FG) 5. Small scratches, the type that can be seen but cannot be felt with a fingernail, should be filled with a polishing compound that has scratch filling properties. The cleaner/polisher mentioned in paragraph 3 frequently has scratch filling properties and is satisfactory for regular use.

  • Page 309: Engine And Propeller

    Refer to the Columbia 400 (LC41-550FG) Approved Maintenance Manual for additional instructions. Propeller Cleaning and Care – It is important to keep the propeller clean since it facilitates detection of cracks and other problems.
  • Page 310 Section 8 Handling, Servicing, and Maintenance Columbia 400 (LC41-550FG) This Page Intentionally Left Blank RC050005 Initial Issue of Manual: December 9, 2005 8-22 Latest Revision Level/Date: C/10-10-2006...
  • Page 311 In the Columbia Aircraft Manufacturing Corporation Information Manual for the Columbia 400, the actual supplements provided by the holder of the STC are not included. However, to assist the reader in understanding the special equipment that is installed through an STC, a discussion of these components is included on the following pages.
  • Page 312 Columbia Aircraft Manufacturing Corporation neither endorses nor opposes after-market installations; however, such an installation can limit or invalidate the warranty on the airplane. Columbia Aircraft Manufacturing Corporation does not provide technical support or documentation for after-market installations. The holder of the STC normally provides these services.

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