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Raytheon Beech Bonanza A36 Pilot's Operating Handbook And Flight Manual

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Beech Bonanza

(Serials E-1946, E-2104, E-2111 thru E-3629

Pilot's Operating Handbook

FAA Approved Airplane Flight Manual

FAA Approved in the Normal Category based on CAR Part 3. This

document must be carried in the airplane at all times, and be kept within

reach of the pilot during all flight operations. This handbook includes the

material required to be furnished to the pilot by CAR Part 3.

Airplane Serial Number:_________________________

Airplane Registration Number:____________________

FAA Approved

by:_________________________________________

Copyright © 2006 Raytheon Aircraft Company. All rights reserved.

P/N 36-590002-37B

Reissued: November, 2002

and E-3631 thru E-3635)

and

John Tigue

Raytheon Aircraft Company

DOA-230339-CE

®

A36

P/N 36-590002-37B2

Revised: January, 2006

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Summary of Contents for Raytheon Beech Bonanza A36

Page 1 CAR Part 3. Airplane Serial Number:_________________________ Airplane Registration Number:____________________ FAA Approved by:_________________________________________ John Tigue Raytheon Aircraft Company DOA-230339-CE Copyright © 2006 Raytheon Aircraft Company. All rights reserved. P/N 36-590002-37B P/N 36-590002-37B2 Reissued: November, 2002 Revised: January, 2006...
Page 3 LIST OF EFFECTIVE PAGES This listing contains all current pages with effective revision number or date. It should be used after posting changes to ensure the manual is complete and up-to-date. Always destroy superseded pages when you insert revised pages. Beech Bonanza®...
Page 4 List Of Effective Pages (Cont’d) P/N 36-590002-37B Revision B2 - January, 2006 5-11 thru 5-40..... . November, 2002 6-1 thru 6-3......November, 2002 6-4 .
Page 5 LOG OF REVISIONS Beech Bonanza ® (Serials E-1946, E-2104, E-2111 thru E-3629 and E-3631 thru E-3635) Pilot’s Operating Handbook FAA Approved Airplane Flight Manual P/N 36-590002-37B Revision B2 - January, 2006 PAGE DESCRIPTION Title Page List of Effective Pages 1 of 2 2 of 2 Log of Revisions 1 of 1...
Page 10 Attention is called to Section X, SAFETY INFORMATION. Raytheon Aircraft Company feels that it is highly important to have Safety Information in a condensed form in the hands of the pilots. The Safety Information should be read and studied.
Page 11: Important Notice
This may render the part, component, or structural assembly, even though originally manufactured by Raytheon Aircraft, unsuitable or unsafe for airplane use. Raytheon Aircraft expressly disclaims any responsibility for malfunctions, failures, damage or injury caused by use of non- Raytheon Aircraft approved parts.
Page 12: Use Of The Handbook
Raytheon Aircraft Authorized Outlets can provide recom- mended modification, service, and operating procedures issued by both the FAA and Raytheon Aircraft Company, which are designed to get maximum utility and safety from the airplane. USE OF THE HANDBOOK...
Page 13: Revising The Handbook
Section 1 General Model A36 Operating procedures, techniques, etc., which could result in damage to equipment if not carefully followed. NOTE An operating procedure, technique, etc., which is considered essential to empha- size. REVISING THE HANDBOOK The Pilot’s Operating Handbook is designed to facilitate main- taining the documents necessary for the safe and efficient operation of the airplane.
Page 14: Revision Service
1. Reissues and revisions of the Pilot’s Operating Hand- book and FAA Approved Airplane Flight Manual. 2. Original issues and revisions of FAA Approved Airplane Flight Manual Supplements. 3. Original issues and revisions of Raytheon Aircraft Ser- vice Bulletins. January, 2006...
Page 15 “Revision Service” applicable to this handbook or other Raytheon Aircraft Service Publications, consult any Raytheon Aircraft Authorized Outlet or refer to the latest revision of Raytheon Aircraft Service Bulletin No. 2001. Raytheon Aircraft Company expressly reserves the right to...
Page 16: Supplements
When a new airplane is delivered from the factory, the handbook delivered with it contains either an STC (Supplemental Type Cer- tificate) Supplement or a Raytheon Aircraft Flight Manual Sup- plement for every installed item requiring a supplement. If a new...
Page 17 Beech Bonanza A36 Section I 1-10 November, 2002...
Page 18: Ground Turning Clearance
Beech Bonanza A36 Section I GROUND TURNING CLEARANCE Radius for Wing Tip ....27 feet 7 inches Radius for Nose Wheel ....13 feet 8 inches Radius for Inside Gear.
Page 19: Descriptive Data
Beech Bonanza A36 Section I DESCRIPTIVE DATA ENGINE NUMBER OF ENGINES ENGINE MANUFACTURER Teledyne Continental Motors Corporation (Muskegon, Michigan) ENGINE MODEL NUMBER IO-550-B ENGINE TYPE Normally aspirated, Fuel-injected, direct-drive, air-cooled, hori- zontally opposed, 6-cylinder, 550-cubic-inch displacement. HORSEPOWER RATING 300 H.P.
Page 20: Propeller Type
Beech Bonanza A36 Section I PROPELLER TYPE Constant-speed, Hydraulically Actuated consisting of (X)- 82NDB-2 blades and a D3A32C409-(X) hub. NOTE The letters appearing in the place of the (X) repre- sent minor variations in the propeller hub or blades. They do not affect eligibility or interchangeability.
Page 21: Engine Oil
Beech Bonanza A36 Section I ENGINE OIL OIL CAPACITY Total ........12 Quarts...
Page 22: Cabin Baggage Volumes
Beech Bonanza A36 Section I CABIN BAGGAGE VOLUMES Rear Cabin Compartment (Rear Spar to Sta. 170.0) ..... . 37 cu ft Extended Aft Compartment (Sta.
Page 23: Symbols, Abbreviations And Terminology
Beech Bonanza A36 Section I SYMBOLS, ABBREVIATIONS AND TERMINOLOGY The following glossary is applicable within this handbook. GENERAL AIRSPEED TERMINOLOGY Calibrated Airspeed is the indicated air- speed of an airplane corrected for position and instrument error. Calibrated airspeed is equal to true airspeed in standard atmo- sphere at sea level.
Page 24 Beech Bonanza A36 Section I Maximum Flap Extended Speed is the highest speed permissible with wing flaps in a prescribed extended position. Maximum Landing Gear Extended Speed is the maximum airspeed at which an air- plane can be safely flown with the landing gear extended.
Page 25: November, 2002
Beech Bonanza A36 Section I METEOROLOGICAL TERMINOLOGY Indicated The number actually read from an altimeter Pressure when the barometric subscale has been Altitude set to 29.92 inches of mercury (1013.2 mil- libars). International Standard Atmosphere in which: (1) The air is a dry, perfect gas;...
Page 26: Power Terminology
Beech Bonanza A36 Section I Station Actual atmospheric pressure at field eleva- Pressure tion. Wind The wind velocities recorded as variables on the charts of this handbook are to be understood as the headwind or tailwind components of the reported winds.
Page 27: Engine Controls And Instrument Terminology
Beech Bonanza A36 Section I ENGINE CONTROLS AND INSTRUMENTS TERMINOLOGY The Exhaust Gas Temperature Indicator is used to identify the lean and best-power fuel flow mixtures for various power settings during cruise. Manifold The regulated absolute air pressure in the...
Page 28: Airplane Performance And Flight Planning Terminology
Beech Bonanza A36 Section I AIRPLANE PERFORMANCE AND FLIGHT PLANNING TERMINOLOGY Climb Gradient The ratio of the change in height during a portion of a climb to the horizontal distance traversed in the same time interval. Demonstrated The velocity of the crosswind component...
Page 29 Beech Bonanza A36 Section I Basic Empty The weight of an empty airplane including Weight full engine oil and unusable fuel. This equals empty weight plus the weight of unusable fuel, and the weight of all the engine oil required to fill the lines and tanks.
Page 30 Beech Bonanza A36 Section I Maximum Maximum weight approved for the start of Take-off Weight the take-off run. Maximum Zero Maximum weight exclusive of usable fuel. Fuel Weight Moment The product of the weight of an item multi- plied by its arm (moment divided by a con-...
Page 31 Beech Bonanza A36 Section I THIS PAGE INTENTIONALLY LEFT BLANK 1-24 November, 2002...
Page 42: Maneuver Limits
Section 2 Model A36 Limtations MANEUVER LIMITS This is a utility category airplane. Spins are prohibited. No acrobatic maneuvers are approved except those listed under Approved Maneuvers. APPROVED MANEUVERS MANEUVER ENTRY SPEED KCAS KIAS Chandelle Steep Turn Lazy Eight Stall (Except Whip) Use Slow Deceleration Minimum fuel for above maneuvers - 10 gallons each main tank Maximum Slip Duration .
Page 43: Seating
Section 2 Limtations Model A36 SEATING Do not take off or land with the seat back of an occupied pilot’s or copilot’s seat in the full back position. The seat back of an occupied optional copilot’s full reclining seat and all other occupied seats must be in the most upright position for take- offs and landings.
Page 214: Alternator
Section 7 Model A36 Systems Description ALTERNATOR The airplane is equipped with a 28.5-volt 60-ampere or an optional 100-ampere, gear-driven alternator. The alternator is designed to maintain up to 60- or 100-ampere output respectively at 2300 rpm to provide airplane electrical power. VOLTAGE REGULATOR A transistorized electronic voltage regulator adjusts the alternator output to maintain a constant voltage at the battery bus.
Page 215: Lighting System
Section 7 Systems Description Model A36 ulators and associated electrical equipment from voltage tran- sients (power fluctuations). If polarity is reversed, a diode in the coil circuit will prevent contactor operation. If the external power unit does not have a standard AN-type plug, check the polarity and connect the positive lead from the external power source to the positive battery terminal and the negative lead to the negative battery terminal.
Page 216: Exterior Lighting
Section 7 Model A36 Systems Description courtesy light was removed and replaced by the illumination of the three reading lights on the right side of the cabin ceiling as standard equipment). To limit battery drain, the step light and courtesy light (or reading lights) are connected to a timer which will extinguish the lights approximately 15 minutes after the door is opened.
Page 217: Heater And Defroster Operation
Section 7 Systems Description Model A36 In flight, ram air enters an intake air scoop on the left side of the engine cowl, passes through the heater muff, then into a mixer valve on the forward side of the firewall. In the mixer valve, the heated air is combined with a controlled quantity of unheated ram air picked up at an intake on the right side of the nose.
Page 226 Model A36 SECTION 8 HANDLING, SERV AND MAINT TABLE OF CONTENTS SUBJECT PAGE Introduction To Servicing ..........8-3 Publications ..............8-3 Airplane Inspection Periods ........... 8-4 Preventative Maintenance That May Be Accomplished By A Certificated Pilot ..........8-5 Alterations Or Repairs To the Airplane ......8-5 Ground Handling ..............
Page 227 Model A36 SECTION 8 HANDLING, SERV AND MAINT TABLE OF CONTENTS (CONT’D) SUBJECT PAGE Tires ................8-17 Shock Struts ..............8-18 Shimmy Damper ............8-19 Brakes ................. 8-20 Induction Air Filter ............8-20 Instrument Air Pressure System ......... 8-21 Propeller ..............8-21 Oxygen System ............
Page 228: Introduction To Servicing
Beech Bonanza in a condition equal to that of its original manufacture. This information sets the time inter- vals at which the airplane should be taken to a Raytheon Air- craft Authorized Outlet for periodic servicing or preventive maintenance.
Page 229: Airplane Inspection Periods
For detailed informa- tion on how to obtain “Revision Service” applicable to this handbook or other Raytheon Aircraft Service Publications, consult any Raytheon Aircraft Authorized Outlet, or refer to the latest revision of Raytheon Aircraft Service Bulletin No. 2001. AIRPLANE INSPECTION PERIODS 1.
Page 230: Preventative Maintenance That May Be Accomplished By A Certificated Pilot
Section 8 Model A36 Handling, Serv & Maint NOTE In event of any gear or flap extension at speeds above the respective normal exten- sion speeds, inspect gear retract rods, gear doors, and flaps, for damage or distortion before the next flight. PREVENTATIVE MAINTENANCE THAT MAY BE ACCOMPLISHED BY A CERTIFICATED PILOT 1.
Page 231 Model A36 NOTE Alterations and repairs to the airplane must be made by properly licensed personnel. Use only genuine Raytheon Aircraft or Raytheon Aircraft approved parts obtained from Raytheon Aircraft approved sources, in connection with the maintenance and repair of Beech airplanes.
Page 232: Ground Handling
Section 8 Model A36 Handling, Serv & Maint Raytheon Aircraft expressly disclaims any responsibility for malfunctions, failures, damage or injury caused by use of non- Raytheon Aircraft approved parts. GROUND HANDLING The three-view drawing in Section 1, GENERAL, shows the minimum hangar clearances for a standard airplane.
Page 233: Parking
Section 8 Handling, Serv & Maint Model A36 Do not exert force on the propeller or con- trol surfaces. Do not place weight on the empennage to raise the nose wheel. When towing with a tug, limit turns to prevent damage to the nose gear.
Page 234: Main Wheel Jacking
Section 8 Model A36 Handling, Serv & Maint 1. Install the control locks. 2. Chock the main wheels, fore and aft. 3. Using nylon line or chain of sufficient strength, secure the airplane at the three points provided. DO NOT OVERTIGHTEN;...
Page 235: Prolonged Out Of Service Care
Section 8 Handling, Serv & Maint Model A36 PROLONGED OUT OF SERVICE CARE The storage procedures listed are intended to protect the air- plane from deterioration while it is not in use. The primary objectives of these measures are to prevent corrosion and damage from exposure to the elements.
Page 236: Grounding
Section 8 Model A36 Handling, Serv & Maint GROUNDING Static ground airplane securely and effectively. PITOT TUBE Install cover. WINDSHIELD AND WINDOWS Close all windows and window vents. It is recommended that covers be installed over windshield and windows. DURING FLYABLE STORAGE Each seven days during flyable storage, the propeller should be rotated by hand.
Page 237: External Power
Section 8 Handling, Serv & Maint Model A36 EXTERNAL POWER When using external power, it is very important that the follow- ing precautions be observed: 1. A Battery must be installed in the airplane. 2. The airplane has a negative ground system. Exercise care to avoid reversed polarity.
Page 238: Servicing
Section 8 Model A36 Handling, Serv & Maint SERVICING FUEL SYSTEM Refer to Section 2, Limitations, for a list of approved engine fuels. FUEL CELLS Never leave the fuel cells completely empty for more than a few days, as the cell inner lining may dry out and crack, permitting fuel to diffuse through the walls of the cell after refueling.
Page 239: Fuel Strainers
Section 8 Handling, Serv & Maint Model A36 FUEL STRAINERS At each 100-hour inspection, the strainer plug should be removed from the fuel injection control valve, and the fuel injection control valve screen washed in fresh cleaning solvent. After the strainer plug has been reinstalled and safetied, the installation should be pressure checked for leakage.
Page 240 Section 8 Model A36 Handling, Serv & Maint 1. Remove the access plate from the engine cowl on the lower right side. 2. Locate the oil sump drain valve at the low point of the engine sump. 3. Locate drain adapter fitting packaged with loose tools and accessories (P/N 107B Probe Auto-Valve Inc.), and attach a piece of 1/2-inch inside-diameter plastic or rub- ber tubing (not supplied) of suitable length.
Page 241: Battery
Section 8 Handling, Serv & Maint Model A36 Do not exceed 25 hours of operation with factory break-in oil (MIL-C-6529, Type II, Multi viscosity, 20W50 Corrosion-preven- tive). When changing to MIL-L-22851 Ash- less Dispersant oil, change the oil and oil filter as previously described.
Page 242: Tires
When inflating tires, visually inspect them for cracks and breaks. Raytheon Aircraft cannot recommend the use of recapped tires. Recapped tires have a tendency to swell as a result of the increased temperature generated during takeoff.
Page 243: Shock Struts
Section 8 Handling, Serv & Maint Model A36 SHOCK STRUTS The following procedures may be used for servicing both the main and the nose gear shock struts. To Inflate Struts: 1. Check to see that the airplane is empty except for full fuel and oil.
Page 244: Shimmy Damper
Section 8 Model A36 Handling, Serv & Maint To Replenish Strut Hydraulic Fluid: 1. Support the airplane on jacks at the wing jack points. 2. Remove the air valve cap, depress the valve core, and allow the strut to fully deflate. 3.
Page 245: Brakes
Section 8 Handling, Serv & Maint Model A36 the depth of the insertion. When the shimmy damper is full, insertion depth is 2-3/16 inches; when empty, 3-1/16 inches. NOTE The measuring wire should be inserted in the hole in the floating piston rather than against the piston face, to give a more accurate reading.
Page 246: Instrument Air Pressure System
Section 8 Model A36 Handling, Serv & Maint To Remove Filter: 1. Remove the fuselage nose section grill. 2. Remove the threaded fasteners securing the filter and remove the filter. INSTRUMENT AIR PRESSURE SYSTEM The pressure system incorporates two filters; a pump intake fil- ter and an in-line filter.
Page 247: Oxygen System
Section 8 Handling, Serv & Maint Model A36 OXYGEN SYSTEM To service the oxygen system, use the following procedures: When filling the oxygen system, only use Aviator’s Breathing Oxygen, MIL-O-27210. Keep hands, tools, clothing, and oxygen equipment clean and free from grease and oil.
Page 248: Oxygen Cylinder Retesting
Section 8 Model A36 Handling, Serv & Maint 5. Close the cylinder shutoff valve using the push/pull con- trol knob on the pilot’s subpanel. The oxygen control knob must be pushed flush against pilot’s subpanel to ensure system is off. 6.
Page 249: Alternator
6. Do not attempt to polarize an alternator. MAGNETOS Ordinarily, the magnetos will require only occasional adjust- ment, lubrication, and breaker point replacement. This work should be done by a Raytheon Aircraft Authorized Outlet. 8-24 January, 2006...
Page 250: Cleaning
Section 8 Model A36 Handling, Serv & Maint To be safe, treat the magnetos as hot whenever a switch lead is disconnected at any point; they do not have an internal automatic grounding device. The magnetos can be grounded by replacing the switch lead at the noise filter capacitor with a wire which is grounded to the engine case.
Page 251 Section 8 Handling, Serv & Maint Model A36 Prior to cleaning, cover the wheels, making certain the brake discs are covered. Attach the pitot cover securely and plug or mask off all other openings. Be particularly careful to mask off all static air buttons before washing or waxing.
Page 252 Section 8 Model A36 Handling, Serv & Maint ered or masked off. Avoid directing high-pressure sprays toward the fuselage, wings, and empennage from the rear, where moisture and chemicals might more easily enter the structure, causing corrosion damage to structural members and moving parts.
Page 253: Windows And Windshields
Section 8 Handling, Serv & Maint Model A36 should be removed periodically. Generally, aliphatic naphtha (see the Bonanza Series Maintenance Manual) is adequate and safe for this purpose. NOTE Before returning the airplane to service, remove all maskings and coverings and relubricate as necessary.
Page 254: Engine
Section 8 Model A36 Handling, Serv & Maint After a thorough cleaning, wax the surface with a good grade of commercial wax that does not have an acrylic base. The wax will fill in minor scratches and help prevent further scratch- ing.
Page 255: Consumable Materials
Section 8 Handling, Serv & Maint Model A36 Oily spots may be cleaned with household spot removers, used sparingly. Before using any solvent, read the instructions on the container and test it on an obscure place on the fabric to be cleaned.
Page 256: Approved Engine Oils
Section 8 Model A36 Handling, Serv & Maint APPROVED ENGINE OILS COMPANY BRAND NAME BP Oil Corporation BP Aero Oil D65/80 Castrol Ltd (Australia) Grade 40, Castrolaero AD Oil Continental Oil Co. Conoco Aero S (SAE 10W30) Delta Petroleum Co. Delta Avoil Exxon Company, USA Exxon Aviation Oil EE...
Page 257: Lamp Replacement Guide
Section 8 Handling, Serv & Maint Model A36 LAMP REPLACEMENT GUIDE LOCATION ....... . NUMBER Close Focus Reading Lights, Cabin .
Page 258 Beechcraft, Inc. nor Hawker Beechcraft Corporation are affiliated any longer with Raytheon Company. Any Raytheon marks contained in this document are owned by Raytheon Company and are employed pursuant to a limited license granted by Raytheon Company. 36-590002-37 Supplement Pack...
Page 260 LOG OF SUPPLEMENTS Model A36 Bonanza® Pilot’s Operating Handbook FAA Approved Airplane Flight Manual P/N 36-590002-37 December, 2006 FAA Supplement must be in the airplane for all flight operations when subject equipment is installed. PART NUMBER SUBJECT DATE *33-590009-19 Collins ANS-351 Area Navigation 12/78 System *35-590118-13...
Page 261 Log Of Supplements (Cont’d) 36-590002-37 December, 2006 PART NUMBER SUBJECT DATE *36-590002-55 A36 Bonanza Modified for 11/91 Reduced External Noise *36-590002-57 Four Position Flap Indicator 4/91 36-590002-59 Dual Garmin GNS 430 or Garmin 08/00 GNS 530 & Garmin GNS 430 VHF Communications Transceivers/ VOR/ILS Receivers/GPS Receivers with Garmin Course...
Page 262 Log Of Supplements (Cont’d) 36-590002-37 December, 2006 PART NUMBER SUBJECT DATE 36-590002-0065 Dual Garmin GNS 430 or Garmin 09/03 GNS 530 & Garmin GNS 430 VHF Communications Transceivers/ VOR/ILS Receivers/GPS Receivers with Garmin Course Deviation Indicator with Mid- Continent Instruments GPS Annunciator Control Unit with PS Engineering PMA7000B-Series Audio Panel with BF Goodrich WX-...
Page 263 ** Supplements marked with a double asterisk will not be sup- plied with manuals sold through Authorized Raytheon Aircraft Outlets. If a document is required for your airplane, order through the applicable STC system manufacturer.

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