Beech Baron 58 Flight Manual
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. Any Raytheon marks contained in this document are owned by Raytheon Company and are employed pursuant to a limited license granted by Raytheon Company. Prior to March 26, 2007, Beechcraft Corporation was owned by Raytheon Company but is no longer affiliated wtih Raytheon Company. 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 Always destroy superseded pages when you insert revised pages. Model G58 Baron ®. List Of Effective Pages (Cont’d) P/N 58-590000-67 Revision A12 - May, 2015 3A-1 thru 3A-9.
April, 2008 3A-10. LOG OF TEMPORARY CHANGES Model G58 Baron Pilot’s Operating Handbook FAA Approved Airplane Flight Manual P/N 58-590000-67 June, 2011 Temporary Changes to this manual must be in the airplane for all flight operations.
PART NUMBER SUBJECT DATE 58-590000-67TC1 Uncommanded pulsing of the June, Rev 1 control column during overly. Log Of Temporary Changes (Cont’d) P/N 58-590000-67 Revised June, 2011 PART NUMBER SUBJECT DATE 58-590000-67TC5 Incorporated into the 58-590000- Incorpo- 67A8 revision. Please discard all rated 58-590000-67TC5 pages: 1 of 4 thru 4 of 4. NOTE: This page should be filed in the front of the manual immediately in front of the Log Of Revisions page(s). Section 3A Abnormal Procedures Model G58 Baron Temporary Change to the Pilot’s Operating Handbook FAA Approved Airplane Flight Manual P/N 58-590000-67TC1 Rev 1 Publication Model G58 Pilot’s Operating Handbook and Affected FAA Approved Airplane Flight Manual (58- 590000-67, Issued November, 2005) Airplane Serials TH-2125 thru TH-2158 not in compliance Numbers. Model G58 Baron Temporary Change to the Pilot’s Operating Handbook FAA Approved Airplane Flight Manual P/N 58-590000-67TC2 Publication Model G58 Pilot’s Operating Handbook Affected and FAA Approved Airplane Flight Manual 58-590000-67, Issued November, 2005.
Airplane Serial TH-2138, TH-2141 and after and prior Numbers Affected airplanes in compliance with Service Bulletin. Revised AIRPLANE THREE-VIEW. 1-12 and 1-13 Revised PROPELLER MANUFACTURER and PROPELLER TYPE. Added PITCH SETTINGS and PROPELLER DIAMETER. Shifted data.
Beech B55 Baron Owner's Manual (part# 96-590011-9). Aircraft Information Manual More Info » $33.88 Beech 58, 58A Baron Pilot's Operating Handbook (part# 58-590000-35.
Section 2 Reformatted to change Hawker Beechcraft Cor- poration to Beechcraft Corporation. 2-1 thru 2-4 Revised Table of Contents. Revised PROPELLER MANUFACTURER, PRO- PELLER TYPE and PROPELLER DIAMETER. Shifted data. 2-18 Revised website reference.
Section 7 Reformatted to change Hawker Beechcraft Corporation to Beechcraft Corporation. 7-1 thru 7-6 Revised Table of Contents. 7-31 Revised PROPELLERS. Shifted data. Revision A11 - July, 2014 PAGE DESCRIPTION Title Page LOEP Section 5 Reformatted to change Hawker Beechcraft Cor- poration to Beechcraft Corporation. 5-24 Added note to Manifold Pressure vs RPM graph - CONTINUOUS OPERATION AT PEAK EGT IS PERMITTED. LOG OF REVISIONS Model G58 Baron ® (Serials TH-2125 and After) Pilot’s Operating Handbook FAA Approved Airplane Flight Manual P/N 58-590000-67 Revision A10 - August, 2013 PAGE DESCRIPTION Title Page LOEP Section 4 4-22 Revised Step 4.
Of CRUISE procedure to refer- ence Leaning Using EGT Indication in Other Nor- mal Procedures. LOG OF REVISIONS Model G58 Baron ® (Serials TH-2125 and After) Pilot’s Operating Handbook FAA Approved Airplane Flight Manual P/N 58-590000-67 Revision A9 - April, 2012 PAGE DESCRIPTION Title Page LOEP Section 1 1-18 Revised definition of OAT. Section 4 4-30 Revised Step 3. Log Of Revisions (Cont’d) P/N 58-590000-67 Revision A9 - April, 2012 PAGE DESCRIPTION 5-36 thru 5-39 Revised 2300 and 2500 rpm Cruise Power Set- tings tables to replace IOAT values with OAT val- ues. Removed 2100 rpm Cruise Power Settings tables.
LOG OF REVISIONS Model G58 Baron ® (Serials TH-2125 and After) Pilot’s Operating Handbook FAA Approved Airplane Flight Manual P/N 58-590000-67 Revision A8 - June, 2011 PAGE DESCRIPTION Title Page LOEP LOTC Section 1 1-13 Incorporated 58-590000-67TC4 (Chinese Avia- tion Gasoline). 1-23 Changed Generic to Generic. Log Of Revisions (Cont’d) P/N 58-590000-67 Revision A8 - June, 2011 PAGE DESCRIPTION 2-23 Changed Versions to Version. Changed ‘and’ to ‘or’. 2-25 and 2-26 Added Item 9. Renumbered remaining items.
Shifted data. 2-27 Shifted data. Section 3A 3A-19 Changed FAILURE OF REMOTE AUTONO- MOUS INTEGRITY MONITORING (RAIM) to LOSS OF RECEIVER AUTONOMOUS INTEG- RITY MONITORING (RAIM). Log Of Revisions (Cont’d) P/N 58-590000-67 Revision A8 - June, 2011 PAGE DESCRIPTION 7-50 thru 7-53 Shifted data. 7-69 Changed Versions to Version. Changed ‘and’ to ‘or’. 7-74 Changed ‘and’ to ‘or’.
7-80 Changed ‘and’ to ‘or’. Removed ‘precision’. Added ‘approach with’. 7-83 Changed Versions to Version. Revised Propeller Manufacturer.
Added supple- ment AFMS 20002-1. Removed Pitch Settings and Propeller Diameter. 2-22 Changed FM to FPM and 45°30’30’ to 45°30’30”. Section 5 - Changed Raytheon Aircraft Company to Hawker Beechcraft Corporation. Revised Table of Contents. DESCRIPTION 5-23 Corrected spelling of angle.
5-45 Changed 196 to 190. Section 6 - Changed Raytheon Aircraft Company to Hawker Beechcraft Corporation.
Corrected Table of Contents. 7-31 Revised Propellers. Added supplement AFMS 20002-1.
7-49 Changed V to VDC (2 places). LOG OF REVISIONS Model G58 Baron ® (Serials TH-2125 and After) Pilot’s Operating Handbook FAA Approved Airplane Flight Manual P/N 58-590000-67 Revision A6 - February, 2009 PAGE DESCRIPTION Title Page LOEP Revised Table of Contents.
2-16 Added Software Version 0857.06. 2-17 Added Software Version 0857.06.
Log Of Revisions (Cont’d) P/N 58-590000-67 Revision A6 - February, 2009 PAGE DESCRIPTION 2-27 Changed “hanger” to “hangar” and shifted data. 2-28 Changed “data base” to “database” in three places and shifted data.
2-29 thru 2-41 Shifted data. 2-42 Added Magnetic Compass to the Kinds of Operations Equipment List and shifted data. 3A-13 thru 3A-17 Inserted “Cabin Heater” and “Wing Ice Light” procedures. Shifted data. 4-3 and 4-4 Inserted “Cabin Heater” procedure and updated RAC to Hawker Beechcraft. 4-10 Inserted “Cabin Heater Over-Tempera- ture Switch,” “Heater Exhaust Outlet” & “Heater Fuel Drain Line” Procedures.
LOG OF REVISIONS Model G58 Baron (Serials TH-2125 and After) Pilot’s Operating Handbook FAA Approved Airplane Flight Manual P/N 58-590000-67 Revision A4 - April, 2008 PAGE DESCRIPTION Title Page LOEP 1-1 and 1-2 Revised Table of Contents and Reformatted 1-3 thru 1-22 Revised “Introduction”, “Important Notice”, “Revi- sion Service”, “Supplements”, “Engine Controls and Instrument Terminology”. Log Of Revisions (Cont’d) P/N 58-590000-67 Revision A4 - April, 2008 PAGE DESCRIPTION 3-3 thru 3-14 Reformatted 3-15 and 3-16 Revised “Autopilot Automatic Disengagement”, “Autopilot Overspeed Recovery MAXSPD” and Reformatted 3-17 thru 3-19 Revised “Electric Pitch Trim Failure PTRM”, “Unscheduled Electric Pitch Trim” and Reformat- 3-20 thru 3-23 Revised “Garmin Terrain Awareness and Warning System (TAWS)”. Log Of Revisions (Cont’d) P/N 58-590000-67 Revision A4 - April, 2008 PAGE DESCRIPTION 4-18 thru 4-21 Revised “Before Takeoff (Runup)”, Shifted Data and Reformatted 4-22 thru 4-28 Revised “Cruise”, Shifted Data and Reformatted 4-29 thru 4-32 Revised “Leaning Using The Lean Assist Page”, “Monitoring Engine Systems (Oil, Fuel, Electri- cal)”, “Monitoring The CHTs and EGTs”, Shifted Data and Reformatted. Log Of Revisions (Cont’d) P/N 58-590000-67 Revision A4 - April, 2008 PAGE DESCRIPTION 8-5 thru 8-18 Revised “Introduction to Servicing”, “Pub- lications”, “Airplane Inspection Periods”, “Alterations or Repairs to the Airplane”, “Fuel Cells” and Reformatted 8-19 thru 8-34 Revised “Batteries”, “Tires”, “Brakes”, “Heating and Ventilating System”, “Alternators”, “Exterior Painted Surfaces”, “Magnetos”, “Consumable Materials”, “Lamp Replacement Guide”. LOG OF REVISIONS Model G58 Baron (Serials TH-2125 and After) Pilot’s Operating Handbook FAA Approved Airplane Flight Manual P/N 58-590000-67 Revision A3 - March, 2007 PAGE DESCRIPTION Title Page Revised for Company Name Change Logo Page Revised for Company Name Change LOEP Revised for Company Name Change Revised for Company Name Change. LOG OF REVISIONS Model G58 Baron (Serials TH-2125 and After) Pilot’s Operating Handbook FAA Approved Airplane Flight Manual P/N 58-590000-67 Revision A2 - January, 2007 PAGE DESCRIPTION Title Page LOEP Revised “Important Notice” 1-12 Revised “Propeller Manufacturer” 1-19 Revised “Engine Controls and Instruments Termi- nology”. (Cont’d) PAGE DESCRIPTION 3-19 Revised “Attitude and Heading Reference System (AHRS) Failure” 3A-1 and 3A-2 Revised Table of Contents 3A-5 Revised “Starter Engage L START ENGD or R START ENGD” 3A-14 Revised “Autopilot Failures” 3A-23 Revised Heading and “Altimeter Disagreement” 4-8 and 4-9 Revised “Preflight Inspection”.
(Cont’d) PAGE DESCRIPTION 7-33 thru 7-38 Added “Fuel Drain” and Shifted Data 7-39 thru 7-42 Revised “Fuel Off-Loading”, “Protective Devices”, “Distribution” and Shifted Data 7-43 Revised Illustration and Shifted Data 7-44 thru 7-48 Revised Tables and Shifted Data 7-49 and 7-50 Revised Table, “External Power”. LOG OF REVISIONS Model G58 Baron (Serials TH-2125 and After) Pilot’s Operating Handbook FAA Approved Airplane Flight Manual P/N 58-590000-67 Revision A1 - February, 2006 PAGE DESCRIPTION Title Page LOEP 1-23 Revised “Acronyms” 2-1 thru 2-4 Revised Table of Contents 2-12 Revised “Weight Limit”. (Cont’d) PAGE DESCRIPTION 3A-19 thru 3A-24 Added “Garmin Terrain Awareness and Warning System (TAWS)” and Shifted Data 4-1 thru 4-4 Revised Table of Contents 4-5 and 4-6 Reprint - No Change Revised “Preflight Inspection” 4-8 thru 4-10 Reprint - No Change 4-11 Revised “Preflight Inspection”. (Cont’d) PAGE DESCRIPTION Revised “Subpanel” and “Pedestal” 7-10 thru 7-14 Reprint - No Change 7-15 Revised “Ground Control” and “Wing Flaps” 7-16 Reprint - No Change 7-17 and 7-18 Revised “Position Lights”, “Safety Switch”, “Warn- ing Horn and GEAR UP Annunciation” and “Man- ual Extension”. (Cont’d) PAGE DESCRIPTION 7-40 and 7-41 Revised “Distribution” Shifted Data 7-42 Revised Illustration and Shifted Data 7-43 thru 7-46 Revised Tables and Shifted Data 7-47 Revised “Monitoring the Electrical System” and Shifted Data 7-48 Revised Table and Shifted Data 7-49 Revised “Starters”, “External Power”. LOG OF REVISIONS Model G58 Baron (Serials TH-2125 and After) Pilot’s Operating Handbook FAA Approved Airplane Flight Manual P/N 58-590000-67 Original Issue - November, 2005 PAGE DESCRIPTION Title Page LOEP L OR 1-1 thru 1-24 2-1 thru 2-38 3-1 thru 3-24 3A-1 thru 3A-20 4-1 thru 4-52 5-1 thru 5-58.
Model G58 SECTION 1 GENERAL TABLE OF CONTENTS SUBJECT PAGE Introduction.1-3 Important Notice. Model G58 SECTION 1 GENERAL TABLE OF CONTENTS (CONT’D) SUBJECT PAGE Fuel.1-14 Approved Engine Fuels. Attention is called to Section 10, SAFETY INFORMATION. Beechcraft Corporation feels that it is highly important to have Safety Information in condensed form in the hands of the pilots.
The Safety Information should be read and studied. Section 1 General Model G58 Salvaged airplane parts, reworked parts obtained from non-Beechcraft Corporation approved sources, or parts, components, or structural assemblies, the service history of which is unknown or cannot be authenti- cated, may have been subjected to unac. Beechcraft Corporation Authorized Outlets can provide recom- mended modification, service, and operating procedures issued by both the FAA and Beechcraft Corporation, which are designed to get maximum utility and safety from the airplane. USE OF THE HANDBOOK WARNINGS, CAUTIONS, AND NOTES. Section 1 General Model G58 Operating procedures, techniques, etc., which could result in damage to equipment if not carefully followed.
Randall L Brukardt
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.
FAA Approved Airplane Flight Manual. Original issues and revisions of FAA Approved Airplane Flight Manual Supplements. Original issues and revisions of Beechcraft Corporation Service Bulletins. The above publications will be provided only to the registered owner/operator at the address listed on the FAA Aircraft Regis- tration Branch List or the Beechcraft Corporation Domestic/ International Owner’s Notification Service List. Model G58 handbook or other Beechcraft Corporation Service Publica- tions, consult any Beechcraft Corporation Authorized Outlet or refer to the latest revision of Beechcraft Corporation Service Bulletin No.
Beechcraft Corporation expressly reserves the right to super- sede, cancel, and/or declare obsolete, without prior notice, any part, part number, kit, or publication referenced in this hand- book. Section 1 Model G58 General AIRPLANE FLIGHT MANUAL SUPPLEMENTS REVISION RECORD Section 9, SUPPLEMENTS, contains the FAA-approved Air- plane Flight Manual Supplements, headed by a Log of Supple- ments page. When new supplements are received or existing supplements are revised, a new Log page will replace the pre- vious one, since it contains a listing of all previous approvals, plus the new approval. Section 1 General Model G58 WING AREA: 199.2 SQ FT McCauley: 77 INCH DIAMETER Hartzell: 75 INCH DIAMETER 15 FT 11 IN 9 FT 7 IN 37 FT 10 IN 9 FT 9 IN 10.4 IN 8 FT 11 IN 29 FT 10 IN TH01C 054511AB.AI. Section 1 Model G58 General GROUND TURNING CLEARANCE RADIUS FOR WING TIP.31 FT. RADIUS FOR NOSE WHEEL.15 FT. RADIUS FOR INSIDE GEAR.7 FT.
RADIUS FOR OUTSIDE GEAR.17 FT. TURNING RADII ARE PREDICATED ON THE USE OF PARTIAL BRAKING ACTION AND DIFFERENTIAL POWER. Section 1 General Model G58 DESCRIPTIVE DATA ENGINES NUMBER OF ENGINES ENGINE MANUFACTURER Teledyne Continental Motors, Inc., (Mobile, Alabama) ENGINE MODEL NUMBER IO-550-C ENGINE TYPE Normally aspirated, Fuel-injected, direct-drive, air-cooled, six- cylinder, horizontally opposed, 550-cubic-inch displacement HORSEPOWER RATING 300 H.P. NUMBER OF PROPELLERS PROPELLER MANUFACTURER McCauley Propeller (Vandalia, Ohio). Section 1 Model G58 General NOTE The letters appearing in the place of the (X) represent minor variations in the propeller hub or blades. They do not affect eligibility or interchangeability.
Hartzell Propellers (Optional): Constant speed, variable-pitch, three-blade propeller using a PHC-J3YF-2UF hub with FC7391D(K) blades. Section 1 General Model G58 FUEL APPROVED ENGINE FUELS Aviation Gasoline Grade 100LL (blue) Aviation Gasoline Grade 100 (green) Aviation Gasoline Grade 115/145 (purple) Chinese Aviation Gasoline RH-95/130 Chinese Aviation Gasoline RH-100/130 FUEL CAPACITY STANDARD SYSTEM Total Capacity.200 Gallons Total Usable.
Section 1 Model G58 General ENGINE OIL OIL CAPACITY Total.12 Quarts (each engine) SPECIFICATION Use MIL-L-22851 Ashless Dispersant Oils meeting the require- ments of the latest revision of Teledyne Continental Motors. Section 1 General Model G58 CABIN BAGGAGE VOLUMES Aft Cabin Compartment.37 cu ft Between Spars. 12 cu ft Extended Rear Compartment. Section 1 Model G58 General True Airspeed is the airspeed of an airplane relative to undisturbed air, which is the CAS corrected for altitude, temperature, and compressibility. Air Minimum Control Speed is the minimum flight speed at which the airplane is directionally controllable as determined in accordance with Title 14 Code of Federal Regulations.
Section 1 General Model G58 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 speed at which an airplane can be safely flown with the landing gear extended. Section 1 Model G58 General METEOROLOGICAL TERMINOLOGY Flight in Icing Flight when the OAT is 5°C (41°F) or colder, Conditions and in the presence of visible moisture. Indicated The number actually read from an altimeter Pressure when the barometric subscale has been set Altitude 29.92 inches. Section 1 General Model G58 Station Actual atmospheric pressure field Pressure elevation.
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. POWER TERMINOLOGY Cruise Climb Power recommended for cruise climb. Section 1 Model G58 General Mixture This lever, in the idle cut-off position, stops Control the flow of fuel at the injectors and in the intermediate through the full rich positions, regulates the fuel air mixture. Propeller Used to control the RPM setting of the Control propeller governor. Section 1 General Model G58 Demonstrated The velocity of the crosswind component for Crosswind which adequate control of the airplane Velocity during takeoff and landing was actually demonstrated during certification tests. The value shown is not limiting. Gallons per hour.
Route A part of a route. Section 1 Model G58 General Jack Points Points on the airplane identified by the manufacturer as suitable for supporting the airplane for weighing or other purposes. Leveling Those points which are used during the Points weighing process to level the airplane.
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Maximum Maximum weight approved for ground Ramp. Section 1 General Model G58 Tare The weight of chocks, blocks, stands, etc., used on the scales when weighing an airplane. Unusable Fuel Fuel that is not available for flight planning. Useful Load Difference between Ramp Weight, and Basic Empty Weight. Usable Fuel Fuel available for flight planning. Section 1 Model G58 General Garmin: GDC.Garmin Air Data Computer GDU.Garmin Display Unit GEA.
S Tucker Taft
Section 1 General Model G58 THIS PAGE INTENTIONALLY LEFT BLANK 1-26 May, 2015. Model G58 SECTION 2 LIMITATIONS TABLE OF CONTENTS SUBJECT PAGE Airspeed Limitations.2-5 Airspeed Indicator Display. Model G58 SECTION 2 LIMITATIONS TABLE OF CONTENTS (CONT’D) SUBJECT PAGE Power Plant Instrument Markings (Cont’d) Oil Temperature.2-11 Oil Pressure.
Model G58 SECTION 2 LIMITATIONS TABLE OF CONTENTS (CONT’D) SUBJECT PAGE Avionics.2-16 General. Section 2 Limitations Model G58 THIS PAGE INTENTIONALLY LEFT BLANK May, 2015. Section 2 Model G58 Limitations The limitations included in this section have been approved by the Federal Aviation Administration and must be observed in the operation of this airplane. AIRSPEED LIMITATIONS SPEED KCAS KIAS REMARKS Never Exceed Do not exceed this speed in any operation. Section 2 Limitations Model G58 AIRSPEED INDICATOR DISPLAY COLOR CODED SPEED KIAS SIGNIFICANCE RANGE STRIP OR MARKING RANGE White Strip 74 - 122 Full Flap Operating Range Lower Limit = Stall speed with flaps down at maximum weight. Upper Limit = Maximum speed permissible with flaps fully extended.
Section 2 Model G58 Limitations Reference speeds for Glide, V, and V are pilot programma- ble and selectable using the TMR/REF soft key on the PFD. If one or more of these speeds is selected for display, a pointer will be positioned on the right side of the airspeed display opposite the speed that was programmed. Section 2 Limitations Model G58 FUEL LIMITS APPROVED ENGINE FUELS 100LL (blue) 100 (green) 115/145 (purple) RH-95/130 (Chinese) RH-100/130 (Chinese) FUEL CAPACITY STANDARD FUEL SYSTEM Total Capacity.200 Gallons Total Usable.
Section 2 Model G58 Limitations NUMBER OF PROPELLERS PROPELLER MANUFACTURER McCauley Propeller (Vandalia, Ohio) Hartzell Propeller, Inc (Piqua, Ohio) NUMBER OF BLADES Three PROPELLER TYPE McCauley propellers (Standard): Constant-speed, variable-pitch, three-blade propeller using a 3AF32C512-(X) hub with (X)-82NEA-5 blades. NOTE The letters appearing in the place of the (X) represent minor variations in the propeller hub or blades. Section 2 Limitations Model G58 POWER PLANT INSTRUMENT MARKINGS Power Plant displays are found on the MFD on the Engine Default page, the Systems page, and the Lean page in both digital and analog formats. When the MFD is not operable, the displays are found on the PFD. Section 2 Model G58 Limitations FUEL FLOW Operating Range (Green Bar).
3 to 27.4 GPH Prohibited Range (Red Bar). 27.4 to 30.0 GPH Leaning Indicator (Cyan Pointer) - This pointer will automati- cally be displayed during MCP Climb and Cruise Climb power settings. Section 2 Limitations Model G58 Prohibited Range (Red Bar).0 to 10 psi Caution Range (Yellow Bar).10 to 30 psi Operating Range (Green Bar). Section 2 Model G58 Limitations PROPELLER DEICE AMMETER Normal Operating Range (Green Arc).14 to 18 amps WEIGHT LIMITS Maximum Take-off.5500 lbs Maximum Landing. Section 2 Limitations Model G58 MANEUVER LIMITS This is a normal category airplane. Acrobatic maneuvers, including spins, are prohibited.
FLIGHT LOAD FACTORS (5500 Pounds) Positive Maneuvering Load Factors: Flaps Up (0°).3.8 G Flaps Down (30°). Section 2 Model G58 Limitations Ground use of windshield heat is limited to 10 minutes at a time. Sustained flight in icing conditions with flaps extended is pro- hibited except for approach and landings. LIMITATIONS WHEN ENCOUNTERING SEVERE ICING CONDITIONS (Required By FAA AD 98- 04-24) Severe icing may result from environmental conditions outside of those for which the.
NOTE: This supersedes any relief provided by the Mas- ter Minimum Equipment List (MMEL). AVIONICS GENERAL 1.
The appropriate Garmin G1000 Cockpit Reference Guide for the Beechcraft Baron 58/G58, must be imme- diately available to the flight crew. COCKPIT REFERENCE AIRFRAME SYSTEM GUIDE P/N SOFTWARE VERSION 0500.01, 0500.02. Refer to the MFD upon initial power up. The “Splash Screen” will display the current system software ver- sion at the top of the page, (e.g. “Beechcraft 58/G58 System 0857.05”). Select the SYSTEM STATUS page of the AUX Group on the MFD. Model G58 The following methods may be used to determine if the soft- ware loaded in the airplane is the most current software avail- able.
Call the Beechcraft Corporation Customer Support at 1-800-429-5372. Visit the customersupport/technicalpublications/ web site. Section 2 Model G58 Limitations AIRFRAME SYSTEM SOFTWARE VERSION 0500.02 SYSTEM ABBREVIATION SOFTWARE VERSION Primary Flight Display PFD1 6.00 Multifunction Display MFD1 6.00 Audio Control Panel & GMA1 2.07 Marker Beacon System Attitude and Heading GRS1 2.03 Reference System (AHRS) Air Data Computer (ADC) GDC1 2.05.
Section 2 Limitations Model G58 AIRFRAME SYSTEM SOFTWARE VERSION 0857.05 SYSTEM ABBREVIATION SOFTWARE VERSION Primary Flight Display PFD1 8.10 Multifunction Display MFD1 8.10 Audio Control Panel & GMA1 3.03 Marker Beacon System Attitude and Heading GRS1 2.11 Reference System (AHRS) Air Data Computer (ADC) GDC1 3.01. Section 2 Model G58 Limitations AIRFRAME SYSTEM SOFTWARE VERSION 0857.06 SYSTEM ABBREVIATION SOFTWARE VERSION Primary Flight Display PFD1 8.10 Multifunction Display MFD1 8.10 Audio Control Panel & GMA1 4.02 Marker Beacon System Attitude and Heading GRS1 2.11 Reference System (AHRS) Air Data Computer (ADC) GDC1 3.01. Section 2 Limitations Model G58 DISPLAY UNITS DEFAULT SETTING RESULTS DIS. SPD Nautical (NM, KT) Distance will be shown in nautical miles and speed in knots.
VS Feet (FT, FPM) Altitude will be shown in feet and vertical speed in feet per minute. Section 2 Model G58 Limitations 3.
Use of the VOR/ILS receiver to fly approaches not approved for GPS require VOR/ILS navigation data to be valid on the PFD display. Fuel Planning information found on the MFD by selecting the TRIP PLANNING page of the AUX Group are advi- sory only and do not replace the primary fuel quantity and fuel flow displays on the PFD. Section 2 Limitations Model G58 3.
Navigation using the GPS system is prohibited unless the pilot verifies the currency of the Aviation Database or verifies each selected waypoint for accuracy by refer- ence to current approved data. The Aviation Database version is displayed on the MFD power-up page immedi- ately after system power-up and must be acknowledged. Model G58 Baron LIMITATIONS AVIONICS GENERAL GARMIN TERRAIN AWARENESS AND WARNING SYSTEM (TAWS) (TH-2138, TH-2141 and after and prior airplanes in compliance with Service Bulletin 34-3774) 1. The terrain data base provides world coverage. The obstacle data base provides coverage for only the conti- nental U.S. Model G58 Baron information for primary terrain avoidance.
TAWS is intended only to enhance situational awareness. P/N 58-590000-67TC2 4 of 4 May, 2008. Section 2 Model G58 Limitations 2) Operations South of 55° Latitude are prohibited between 120° East and 165° East Longitude.
Instrument approaches must be accomplished in accor- dance with approved instrument approach procedures that are retrieved from the GPS database. The GPS database must incorporate the current update cycle or be verified for accuracy using current approved naviga- tion data. Section 2 Limitations Model G58 11.
Airplanes equipped with Baro VNAV: Baro VNAV is approved for enroute and terminal vertical navigation only. Baro VNAV is not approved for instru- ment approaches. GARMIN GFC 700 AUTOPILOT SYSTEM (AUTOPI- LOT, FLIGHT DIRECTOR, ELECTRIC TRIM) 1.
Section 2 Model G58 Limitations 10. The autopilot system is only approved for Category I ILS approaches and non-precision approaches. Airplanes with Airframe Software Version 0500.01 or 0500.02: When conducting GPS assisted intercepts of ILS final approach courses with the autopilot engaged, the ILS CDI Capture mode on the Systems Setup page of the Auxiliary Page Group must be set to Manual.
Section 2 Limitations Model G58 GARMIN TERRAIN AWARENESS AND WARNING SYSTEM (TAWS) (TH-2138, TH-2141 and after and prior airplanes in compliance with Service Bulletin 34-3774.) 1. The terrain database provides world coverage. The obstacle database provides coverage for only the conti- nental U.S.
Section 2 Model G58 Limitations PLACARDS/MARKINGS Placards/markings are required to remind the flight crew and occupants of operating limitations and safety device limita- tions. The following illustrations depict placards/markings perti- nent to operations and safety of flight. On Left Side Panel TURN STROBE LIGHTS OFF WHEN TAXING IN VICINITY OF OTHER AIRCRAFT, OR WHEN FLYING IN FOG OR CLOUDS. Section 2 Limitations Model G58 On Instrument Panel Above MFD: E#02C 051578AA.AI On Upper Left Side Panel, Airplanes Approved for Flight In Icing Conditions: On Upper Left Side Panel, Airplanes Not Approved for Flight In Icing Conditions: On Upper Right Side of Instrument Panel (TH-2173 and After): TH02C 063324AA.AI 2-30. Section 2 Model G58 Limitations FOR STANDARD 194 GALLON CAPACITY FUEL SYSTEM Between Fuel Selector Handles: FUEL SELECTOR LEFT WING RIGHT WING USE CROSS FEED 97 GAL 97 GAL IN LEVEL FLIGHT ONLY CROSS FEED DO NOT TAKE OFF IF FUEL QUANTITY GAGES INDICATE IN YELLOW ARC OR WITH LESS THAN 13 GALLONS IN EACH WING SYSTEM TH00C.
Section 2 Limitations Model G58 On Inboard Side of Seat Backs for 3rd and 4th Seats: On Top of Front Spar Carry-Thru Structure Between Front Seats: EMERGENCY LANDING GEAR INSTRUCTIONS TO EXTEND ENGAGE HANDLE IN REAR OF FRONT SEAT AND TURN COUNTERCLOCKWISE AS FAR AS POSSIBLE (50 TURNS) TH02C. Section 2 Model G58 Limitations On Emergency Crank Access Cover: Adjacent To Cabin Door Handle: On Inside of Cabin Door Adjacent to Door Handle: May, 2015 2-33. Section 2 Limitations Model G58 On Lower Sidewall Adjacent to Pilot: WARNING EMERGENCY AIRSPEED STATIC SOURCE EMERGENCY SEE PILOTS CHECK LIST OR FLIGHT MANUAL EMERGENCY PROCEDURES FOR AIRSPEED & ALTIMETER CALIBRATION ERROR NORMAL TH02C 060621AA.AI Adjacent to Openable Cabin Window Handles: 2-34 May, 2015.
Section 2 Model G58 Limitations On Face of Emergency Exit Latch Cover: On Emergency Exit Handle: On Openable Cabin Windows: On Window Adjacent to Pilot’s Seat: May, 2015 2-35. Section 2 Limitations Model G58 On Window Adjacent to Copilot’s Seat: On Windows Adjacent to 5th and 6th Seats and 3rd & 4th For- ward Facing Seats: On Windows Adjacent to 3rd & 4th Aft Facing Club Seats: On Inside of Utility Door on Left Sidewall of Utility Compart- ment, or on Aft Bulkhead: C95TH02C0160 2-36. Section 2 Model G58 Limitations On Left Sidewall of Utility Compartment or Aft Bulkhead (with utility door removal kit): C95TH02C0161 On Panel When Utility Doors are Removed: In Plain View When Nose Baggage Compartment Door is Open: On Left Side of Instrument Panel (if Air Conditioner installed): AIR COND.
Section 2 Limitations Model G58 Adjacent to Oil Filler Caps: TH02D 082106AA.AI Adjacent to Fuel Filler Caps: AVGAS ONLY GRADE GRADE 100LL FOR ALTERNATE FUELS SEE PILOTS OPERATING HANDBOOK CAUTION DO NOT INSERT FUEL NOZZLE MORE THAN 3' INTO TANK TH02D 082107AA.AI 2-38. Section 2 Model G58 Limitations For Standard 194 Gallon Capacity Fuel System Adjacent to Fuel Filler Caps: TH02D 082105AA.AI For Optional 166 Gallon Capacity Fuel System Adjacent to Fuel Filler Caps: TH02D 082103AA.AI May, 2015 2-39. Section 2 Limitations Model G58 On External Power Compartment Door: TH02D 082104AA.AI 2-40 May, 2015.
Section 2 Model G58 Limitations KINDS OF OPERATIONS The Model G58 is approved for the following types of opera- tions when the required equipment as shown in the KINDS OF OPERATIONS EQUIPMENT LIST, is installed and operable. VFR day and night 2.
Screenshot of Default Baron 58 panel. How to use it: The Manual/Checklist is intended to start with a 'dark and cold' panel/engine. If you want to get the maximum from this booklet, you should create an adequate starting situation. If you are used to start flight simulator with running engines and avionics ready for takeoff, place the aircraft at a gate, or a parking position, use the Manual/Checklist items at its end from 'Taxi to ramp' until 'Shutdown' and 'Securing'; then you should have the desired situation.
As a guideline, I gave the Manifold pressure values for different sections of the flight. The manifold pressure values my be incorrect, if you takeoff and/or land on airports much above 2500ft MSL.