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FlightSafety BARON G8 Pilot Training Manual

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BARON G58
PILOT TRAINING MANUAL
REVISION 0.2
FlightSafety International, Inc.
Marine Air Terminal, LaGuardia Airport
Flushing, New York 11371
(718) 565-4100
www.FlightSafety.com

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  • Page 1 BARON G58 PILOT TRAINING MANUAL REVISION 0.2 FlightSafety International, Inc. Marine Air Terminal, LaGuardia Airport Flushing, New York 11371 (718) 565-4100 www.FlightSafety.com...
  • Page 2 FAA, that of the manu- facturer or the FAA shall take precedence. We at FlightSafety want you to have the best training possible. We welcome any suggestions you might have for improving this manual or any other aspect of our training program.
  • Page 3 Courses for the Baron G58 are taught at the following FlightSafety learning center: Wichita (Hawker Beechcraft) Learning Center 9720 East Central Avenue Wichita, Kansas 67206 Phone: (316) 612-5300 Toll-Free: (800) 488-3747 Fax: (316) 612-5399 Copyright © 2012 by FlightSafety International, Inc.
  • Page 4 INSERT LATEST REVISED PAGES, DESTROY SUPERSEDED PAGES LIST OF EFFECTIVE PAGES Dates of issue for original and changed pages are: Original ...0 ..May 2007 Revision ..0.1 ..August 2011 Revision ..0.2 ..June 2013 NOTE: For printing purposes, revision numbers in footers occur at the bottom of every page that has changed in any way (grammatical or typographical revisions, reflow of pages, and other changes that do not necessarily affect the meaning of the manual).
  • Page 5 Page *Revision Page *Revision 14-1 ............0.1 16-5—16-7 ..........0 14-2—14-10 ..........0 16-8—16-14 ..........0.1 15-i—15-iv ..........0 17-i—17-ii ..........0.1 15-1 ............0.1 18-i—18-iv ..........0 15-2—15-8 ..........0 18-1 ............0.1 16-i—16-iv ..........0.1 18-2—18-8 ..........0 16-1 ............
  • Page 6 CONTENTS CHAPTER 1 AIRCRAFT GENERAL CHAPTER 2 ELECTRICAL POWER SYSTEMS CHAPTER 3 LIGHTING CHAPTER 4 MASTER WARNING SYSTEM CHAPTER 5 FUEL SYSTEM CHAPTER 6 AUXILIARY POWER SYSTEM CHAPTER 7 POWERPLANT CHAPTER 8 FIRE PROTECTION CHAPTER 9 PNEUMATICS CHAPTER 10 ICE AND RAIN PROTECTION CHAPTER 11 AIR CONDITIONING CHAPTER 11A...

  • Page 7: Table Of Contents

    BARON G58 PILOT TRAINING MANUAL CHAPTER 1 AIRCRAFT GENERAL CONTENTS Page INTRODUCTION ........................1-1 GENERAL ..........................1-1 History and Significant Design Changes ................. 1-1 STRUCTURES ........................1-4 Aft Fuselage and Cabin ....................1-4 Nose Baggage Compartment ................... 1-5 Forward Cabin Door ......................1-5 Aft Cabin Doors ......................
  • Page 8 BARON G58 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page Beechcraft Baron 58 ....................1-2 Baron G58 Dimensions ....................1-3 Aft Cargo Area......................1-4 Nose Baggage Compartment ..................1-5 Forward Cabin Door ....................1-5 Aft Cabin Doors ......................1-6 Emergency Exits ......................1-7 Executive Writing Table ....................

  • Page 9: Introduction

    BARON G58 PILOT TRAINING MANUAL CHAPTER 1 AIRCRAFT GENERAL INTRODUCTION This chapter provides a brief history of the Beech Baron, as well as a partial list of the signifi- cant design changes that have been made on the Baron G58 aircraft. Descriptions of the general structure of the aircraft, baggage compartments, and interior are discussed.
  • Page 10 BARON G58 PILOT TRAINING MANUAL 285-horsepower Continental IO-520-C engines. In 1984, the 300-horsepower IO-550-C engines The Model C55 included increased tailplane span were made standard along with the addition of dual control columns and known-icing certification. and an extended nose baggage compartment and evolved as a separate Baron model, distinct from The production total of all model Barons, as of the B55.

  • Page 11: Baron G58 Dimensions

    BARON G58 PILOT TRAINING MANUAL 15'11" WING AREA: 199.2 SQ FT 77" DIAMETER 9'7" 37'10" 9'9" 10.4" 8'11" 29'10" Figure 1-2. Baron G58 Dimensions Revision 0.1 FOR TRAINING PURPOSES ONLY...

  • Page 12: Structures

    BARON G58 PILOT TRAINING MANUAL STRUCTURES AFT FUSELAGE AND CABIN The aft fuselage contains control cables, bell- cranks, pulleys, autopilot servos, and the emergency locator transmitter (ELT). The aft cabin contains a cargo/baggage compartment and net, coat hanger, hat shelf, and display area for aircraft documentation.

  • Page 13: Nose Baggage Compartment

    BARON G58 PILOT TRAINING MANUAL NOSE BAGGAGE FORWARD CABIN DOOR COMPARTMENT The forward cabin entry door is on the right side of the aircraft for use by the pilot and front seat nose baggage compartment (Figure occupant (Figure 1-5). If seats No. 3 and No. 4 1-4) is an unheated cargo/baggage area that are configured for forward facing passengers, the contains avionics and electrical equipment.

  • Page 14: Aft Cabin Doors

    BARON G58 PILOT TRAINING MANUAL AFT CABIN DOORS To ensure the door is properly secured for flight, complete the following checks: Dual cabin doors are installed for use by the rear seat passengers (Figure 1-6). If the aircraft 1. Verify that the interior handle swings is configured for club seating, all passengers use freely through an approximate 3-inch arc.

  • Page 15: Cabin Windows

    (Figure 1-7). The procedure for opening the windows for emergency exit is described on a placard near the window and in the FlightSafety Training Checklist. When the emergency exit latch is disengaged, the window swings up allowing exit. Brief passengers on window operation prior to flight.

  • Page 16: Seats And Seat Belts

    BARON G58 PILOT TRAINING MANUAL GROUND CONTROL SEATS AND SEAT BELTS Standard seats in the aircraft are adjustable fore The Baron is maneuvered on the ground using and aft by a latch release bar under the seat. The a combination of differential power, differential seat backs of the four standard seats can also be braking, and nosewheel steering.

  • Page 17: Limitations

    BARON G58 PILOT TRAINING MANUAL LIMITATIONS The limitations of the aircraft and subsystems are discussed in this manual as they apply to each system. For the full list of limitations, refer to the POH. Airspeed limitations are shown in Table 1-1. Airspeed indicator markings are shown in Table 1-2.

  • Page 18: Questions

    BARON G58 PILOT TRAINING MANUAL QUESTIONS To answer the following questions, refer to the FlightSafety Pilot Training Manual, Pilot Training Checklist, and ground school notes: What cockpit indication alerts the pilot Should the rear doors be locked for flight? that the nose baggage door is not properly...
  • Page 19 BARON G58 PILOT TRAINING MANUAL CHAPTER 2 ELECTRICAL POWER SYSTEMS CONTENTS Page INTRODUCTION ........................2-1 GENERAL ..........................2-1 Description ........................2-1 COMPONENTS ........................2-2 Batteries ........................... 2-2 Alternators ........................2-2 Bus Tie Relays ......................... 2-2 Starters ..........................2-2 External Power Receptacle ....................2-2 CONTROLS AND INDICATIONS ..................
  • Page 20 BARON G58 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page External Power Receptacle ..................2-2 MASTER Electrical Toggle/Breaker Switches ............2-3 Alternator Load Display on Default Engine Page ............2-4 Electrical System Diagram ..................2-5 Circuit-Breaker Panels ....................2-6 2-iii Revision 0 FOR TRAINING PURPOSES ONLY...

  • Page 21: Introduction

    BARON G58 PILOT TRAINING MANUAL CHAPTER 2 ELECTRICAL POWER SYSTEMS INTRODUCTION This chapter provides the pilot with an understanding of the electrical system in the Baron G58. In the event of a component malfunction or failure, familiarization with the electrical system allows the pilot to continue to operate the aircraft by effectively troubleshooting and securing the affected component.

  • Page 22: Components

    BARON G58 PILOT TRAINING MANUAL COMPONENTS EXTERNAL POWER RECEPTACLE BATTERIES The external power receptacle is in the outboard side of the left engine nacelle (Figure 2-1). A 13-amp/hour air cooled lead acid battery is External power can be used to power the electrical located under the left nose baggage floor and system with the engines shutdown to charge both another battery is under the right nose baggage...

  • Page 23: Controls And Indications

    BARON G58 PILOT TRAINING MANUAL CONTROLS AND BATTERY SWITCHES INDICATIONS The L BAT and R BAT toggle switches are on the MASTER electrical switch panel (Figure 2-2). Each switch has two positions: ALTERNATOR SWITCHES • L or R BAT The L ALT and R ALT toggle switches are on the •...

  • Page 24: Indicators

    BARON G58 PILOT TRAINING MANUAL When the magneto/start switch is released, power disconnects from the start relay and starter, and the START ENGD message clears. If the message remains on the PFD after the START switch is released, turn off both batteries and alternators and perform an engine shutdown.
  • Page 25 BARON G58 PILOT TRAINING MANUAL GEA RIGHT RIGHT ALT LOAD ALTERNATOR RIGHT BATTERY RIGHT 100A SHUNT START START BATTERY CONTROL RELAY RELAY 100A RELAY RIGHT BUS SECTION #1 100A VOLTS AVIONICS BUS L SUBPANEL BUS R BUS SECTION #2 AVIONICS BUS TIE RELAY RELAY...
  • Page 26 BARON G58 PILOT TRAINING MANUAL FOR TRAINING PURPOSES ONLY Revision 0.1...

  • Page 27: Circuit Breakers

    BARON G58 PILOT TRAINING MANUAL CURRENT LIMITERS The left bus (essential bus) is comprised of three smaller buses on various CB panels in the cock- Current limiters serve as large load circuit pro- pit. The left side of the avionics CB panel below tection for each of the individual buses and CB the copilot control column (Figure 2-5) houses panels in the electrical system.

  • Page 28: Glossary Of Electrical Terms

    BARON G58 PILOT TRAINING MANUAL GLOSSARY OF ELECTRICAL TERMS Amperage—The measure of flow rate in an Relay—A device used to close a circuit in electrical circuit. Amperage is analogous to fluid a location remote from the control switch. flow rate in a hydraulic system. Generally used to reduce long runs of heavy wire or to control several circuits at once with a single Bus—A central distribution point for electrical...

  • Page 29: Questions

    BARON G58 PILOT TRAINING MANUAL QUESTIONS To answer the following questions, refer to the FlightSafety Pilot Training Manual, Pilot Training Checklist, and ground school notes: What is the normal operating voltage of the What causes an R or L ALT INOP annuncia-...
  • Page 30 BARON G58 PILOT TRAINING MANUAL If the batteries are too weak to close the bat- 12. What should never be done with a circuit tery master relays, what should be done? breaker, and why? Why? 10. During an IFR flight, there is a dual alter- 13.
  • Page 31 BARON G58 PILOT TRAINING MANUAL CHAPTER 3 LIGHTING CONTENTS Page INTRODUCTION ........................3-1 GENERAL ..........................3-1 INTERIOR LIGHTING ......................3-2 Nose Baggage Compartment Light ................. 3-2 Cockpit Lights ......................... 3-2 Cabin Lights ........................3-2 EXTERIOR LIGHTING ......................3-4 Landing Lights ........................ 3-4 Taxi Lights ........................
  • Page 32 BARON G58 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page Interior Light Switches ....................3-2 Interior Light Intensity Rheostats ................3-2 Overhead Courtesy Lights ..................3-2 Courtesy Step Light ....................3-3 Landing Lights ......................3-4 Taxi Light ........................3-4 Wing Ice Light ......................3-4 Navigation and Strobe Lights ..................

  • Page 33: Introduction

    BARON G58 PILOT TRAINING MANUAL CHAPTER 3 LIGHTING INTRODUCTION The lighting on the Baron G58 aircraft includes interior and exterior lighting systems. GENERAL Interior lighting provides illumination of the cockpit, avionics, flight instruments, and cabin areas. Exterior lighting consists of landing, taxi, navigation, anticollision, and strobe lights.

  • Page 34: Interior Lighting

    BARON G58 PILOT TRAINING MANUAL INTERIOR LIGHTING NOSE BAGGAGE COMPARTMENT LIGHT The nose baggage compartment contains a light that is controlled by a manual ON/OFF switch located in the nose baggage compartment. COCKPIT LIGHTS On the Baron G58 aircraft, a pair of on-off switches on the pilot subpanel (Figure 3-1) control instru- ment flood and panel lighting.
  • Page 35 BARON G58 PILOT TRAINING MANUAL A step courtesy light is on the right fuselage (Fig- ure 3-4). This light, controlled by a 15-minute timer, illuminates if the doors are unlatched. Figure 3-4. Courtesy Step Light Revision 0.1 FOR TRAINING PURPOSES ONLY...

  • Page 36: Exterior Lighting

    BARON G58 PILOT TRAINING MANUAL EXTERIOR LIGHTING LANDING LIGHTS The G58 has landing lights that are in the engine nacelles (Figure 3-5). Figure 3-6. Taxi Light Figure 3-5. Landing Lights WING ICE LIGHT The landing lights are controlled by individual The wing ice inspection light is mounted in the switch-type circuit breakers on the pilot subpanel.

  • Page 37: Navigation Lights

    BARON G58 PILOT TRAINING MANUAL NAVIGATION LIGHTS STROBE LIGHTS The navigation lights are on each wingtip and The strobe lights are in each wing tip (Figure tail. The right wingtip has a green light, the left 3-8) and on the tail. The lights are controlled by a wingtip has a red light (Figure 3-8), and the tail switch-type circuit breaker on the pilot subpanel.

  • Page 38: Questions

    BARON G58 PILOT TRAINING MANUAL QUESTIONS To answer the following questions, refer to your FlightSafety Pilot Training Manual (PTM), Pilot Training Checklist and ground school notes: Which lights illuminate when the cabin Where is the ice light located? doors are opened?
  • Page 39 BARON G58 PILOT TRAINING MANUAL CHAPTER 4 MASTER WARNING SYSTEM CONTENTS Page INTRODUCTION ........................4-1 GENERAL ..........................4-1 ALERTING SYSTEM ......................4-2 Alerting System Displays ....................4-2 Pilot Actions During Alerts ..................... 4-2 GFC 700 AFCS Alerts and Annunciators ................ 4-2 Annunciator Testing......................
  • Page 40 BARON G58 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page Annunciator Test Button ..................... 4-3 Photoelectric Cell ....................... 4-3 4-iii Revision 0 FOR TRAINING PURPOSES ONLY...

  • Page 41: Introduction

    BARON G58 PILOT TRAINING MANUAL CHAPTER 4 MASTER WARNING SYSTEM INTRODUCTION This chapter describes the master warning system on the Baron G58 aircraft. For more informa- tion about the alerting system and annunciations, refer to the Garmin G1000 G58 Annunciations and Alerts Pilot’s Guide supplied with the aircraft, or visit http://www.garmin.com to download a replacement copy.

  • Page 42: Alerting System

    BARON G58 PILOT TRAINING MANUAL ALERTING SYSTEM GFC 700 AFCS ALERTS AND ANNUNCIATORS The G1000 provides an ANNUNCIATION and All autopilot status and malfunction annunciators an ALERTS window on the primary flight display display on the PFD in the AFCS System Status (PFD) to inform the pilot of any warning, cau- Field.
  • Page 43 BARON G58 PILOT TRAINING MANUAL Figure 4-1. Annunciator Test Button PHOTOELECTRIC CELL Figure 4-2. Photoelectric Cell Revision 0.1 FOR TRAINING PURPOSES ONLY...

  • Page 44: Questions

    BARON G58 PILOT TRAINING MANUAL QUESTIONS To answer the following questions, refer to the FlightSafety Pilot Training Manual, Pilot Train- ing Checklist, and ground school notes: Where are caution and warning alerts dis- played? What must be done to silence the continuous...
  • Page 45 BARON G58 PILOT TRAINING MANUAL CHAPTER 5 FUEL SYSTEM CONTENTS Page INTRODUCTION ........................5-1 GENERAL ..........................5-1 Description ........................5-2 Approved Fuels ....................... 5-2 COMPONENTS ........................5-2 Fuel Boost Pumps ......................5-2 Fuel Fillers ........................5-2 Fuel Flow ......................... 5-2 Fuel Selectors ........................
  • Page 46 BARON G58 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page Fuel Filler Ports ......................5-2 Baron G58 Fuel System ....................5-3 Snap-Type Fuel Drain ....................5-4 Flush-Type Fuel Drain ....................5-4 Fuel Selector Panel ..................... 5-4 Fuel Sight Gage ......................5-5 Fuel Quantity Indicators .....................

  • Page 47: Introduction

    BARON G58 PILOT TRAINING MANUAL CHAPTER 5 FUEL SYSTEM INTRODUCTION A complete understanding of the fuel system is essential to safe and efficient operation of the aircraft. This section gives the pilot the information needed for competent and confident opera- tion of the fuel system.

  • Page 48: Description

    BARON G58 PILOT TRAINING MANUAL DESCRIPTION The fuel system capacity is 200 gallons (194 usable gallons). The system is comprised of three interconnected rubber bladders in each wing to provide all usable fuel to either engine and a 14-gallon wet wing tip cell is added and interconnected to the bladder system.

  • Page 49: Fuel Vents

    BARON G58 PILOT TRAINING MANUAL FUEL FLOW LEGEND HEATER DIVIDER FUEL FUEL FILLER HEATER PUMP FUEL FLOW FUEL QUANTITY TRANSMITTER TRANSDUCER FUEL SELECTOR ENGINE-DRIVEN PUMP VALVE AND DRAIN FUEL SIGHT WING TIP GAGE FUEL DRAIN FUEL SELECTORS OUTBOARD LEADING INBOARD LEADING EDGE CELL EDGE CELL DRAIN WING TIP...

  • Page 50: Drains

    BARON G58 PILOT TRAINING MANUAL CONTROL AND DRAINS INDICATIONS Fuel drains are in the aircraft to remove water and sediment from the fuel system. The Baron G58 has 10 drains. The systems have snap-type drains FUEL SELECTOR CONTROL in each wing near the fuselage for draining the HANDLE inboard leading edge cell, as well as three flush- type drains around the main gear well for draining...

  • Page 51: Fuel Quantity Indicators

    BARON G58 PILOT TRAINING MANUAL Figure 5-6. Fuel Sight Gage FUEL QUANTITY INDICATORS Each fuel tank system contains three fuel quantity transmitters. Floats in the tanks operate the transmitters to send an electrical signal to the GEA 71 unit. This information is then displayed on the default Engine page as a horizontal tape with pennants labeled “L”...

  • Page 52: Limitations

    BARON G58 PILOT TRAINING MANUAL LIMITATIONS FUEL BOOST PUMP SWITCHES • Usable fuel with full tanks: Individual three-position FUEL BOOST PUMP switches are on the pilot subpanel (Figure 5-8). ° 194 gallons Each switch has three positions: HI, LO, and •...

  • Page 53: Emergency/Abnormal Crossfeed

    FUEL SELECTOR in the ON (normal) position. A crossfeed check during shutdown allows for dual crossfeed operation to prevent fuel stagnation in the crossfeed lines. Refer to the FlightSafety Training Checklist for the normal and emergency procedures concerning crossfeed. Revision 0...

  • Page 54: Questions

    BARON G58 PILOT TRAINING MANUAL QUESTIONS To answer the following questions, refer to the FlightSafety Pilot Training Manual, Pilot Training Checklist, and ground school notes: State why a pilot should observe fueling When may the crossfeed system be used? operations.
  • Page 55 BARON G58 PILOT TRAINING MANUAL The information normally contained in this chapter is not applicable to this particular aircraft. Revision 0.1 FOR TRAINING PURPOSES ONLY...
  • Page 56 BARON G58 PILOT TRAINING MANUAL CHAPTER 7 POWERPLANT CONTENTS Page INTRODUCTION ........................7-1 GENERAL ..........................7-1 Induction Air ........................7-2 Exhaust Air ........................7-3 FUEL INJECTION SYSTEM ....................7-3 Description ........................7-3 Components ........................7-4 IGNITION SYSTEM ......................7-5 Description ........................7-5 Controls and Indications ....................
  • Page 57 BARON G58 PILOT TRAINING MANUAL PROPELLERS ........................7-13 Description ........................7-13 Components ........................7-13 Operation ........................7-16 QUESTIONS ........................7-18 Engines .......................... 7-18 Propellers ........................7-19 FOR TRAINING PURPOSES ONLY 7-ii Revision 0...
  • Page 58 BARON G58 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page IO-550-C Engine ......................7-2 Induction Air Intake ....................7-2 Induction System Airflow ................... 7-3 Continental Fuel Injection System ................7-4 Fuel Flow Divider ....................... 7-4 Fuel Injector ........................ 7-5 Ignition System ......................7-5 Lubrication System .....................

  • Page 59: Introduction

    BARON G58 PILOT TRAINING MANUAL CHAPTER 7 POWERPLANT INTRODUCTION This chapter covers the engines on Baron G58 aircraft. A thorough knowledge of the powerplant is essential to good power management by the pilot. Operating within the parameters of the pow- erplant and propeller systems extends engine life and helps ensure safety.

  • Page 60: Induction Air

    BARON G58 PILOT TRAINING MANUAL FUEL FLOW MAGNETOS OIL FILLER OIL COOLER DIVIDER OIL FILTER SPARK PLUG FUEL PUMP Continental Continental Continental FUEL PROP METERING GOVERNOR ENGINE UNIT MOUNT OIL SUMP INDUCTION TUBE INDUCTION OIL SUMP BALANCE DRAIN TUBE Figure 7-1. IO-550-C Engine Engine nomenclature is as follows: inside the nacelle.

  • Page 61: Exhaust Air

    BARON G58 PILOT TRAINING MANUAL EXHAUST AIR The fuel injection system consists of: • Engine-driven fuel pump After the combustion process, exhaust air is pushed out of the cylinders into the exhaust mani- • Manual mixture control folds. The exhaust manifolds route the exhaust air •...

  • Page 62: Components

    BARON G58 PILOT TRAINING MANUAL COMPONENTS Fuel Manifold Valve regulate fuel flow into the injector lines. When Metered fuel from the fuel metering unit is sup- the mixture is brought to idle cut-off, the mani- plied to a fuel manifold valve (divider) (Figure fold valve closes, providing simultaneous cut-off 7-5).

  • Page 63: Ignition System

    BARON G58 PILOT TRAINING MANUAL IGNITION SYSTEM Fuel Injector Nozzles Fuel injector nozzles control the flow of fuel into DESCRIPTION each individual cylinder (Figure 7-6). The fuel injectors vaporize (atomize) the fuel as it enters the cylinders, which allows for more complete The Baron G58 utilizes a dual ignition system combustion of the fuel, resulting in greater engine (Figure 7-7) consisting of two engine-driven...

  • Page 64: Operation

    Refer to the FlightSafety Training When the oil is cold, it bypasses the oil cooler Checklist for engine start and runup procedures.

  • Page 65: Engines

    BARON G58 PILOT TRAINING MANUAL COMPONENTS of the vernatherm, oil is forced through the oil cooler. In the oil cooler, ambient air flows across Cowl Flaps the oil lines to dissipate heat from the oil before it is returned to the engine. The engine nacelles have mechanically operated cowl flaps.The cowl flaps can be opened to allow After leaving the cooler, the oil enters the...
  • Page 66 BARON G58 PILOT TRAINING MANUAL Manifold Pressure Gauge and to measure engine cooling. The number of the “hottest” cylinder displays on the indicator. Nor- Tachometer mal CHTs in cruise flight are approximately Engine power output is measured by the manifold 150°–200°C.
  • Page 67 During cruise climb and cruise, position the cowl Engine Management flaps as necessary to keep the CHTs relatively constant and within acceptable limits. For general operation procedures, refer to the POH and FlightSafety Training Checklist. Mixture Control Engine Cooling Proper mixture...

  • Page 68: Power Vs. Operating Temperature

    BARON G58 PILOT TRAINING MANUAL Engine Break-In highest attainable exhaust gas temperature for the associated ambient temperature, air density and New engines, remanufactured engines, or engines power setting (Figure 7-11). Once peak EGT is with a “top overhaul” of one or more cylinders established, adjust the mixture, either lean or rich must be broken in correctly.
  • Page 69 BARON G58 PILOT TRAINING MANUAL During break-in, use mineral oil in the engine create the metal-to-metal contact needed. If the instead of the normal ashless dispersant oil engine is “babied,” proper break-in will not occur and the cylinders must be rehoned and the process because of its cleaning properties.
  • Page 70 Avoid backfires that could damage the air as necessary. measuring system. Do not exceed 1200 rpm to prevent damage due to poor lubrication. Follow the starting procedure (see the FlightSafety Train- Landing ing Checklist). Leave the cowl flaps closed until on the ground and clear of the runway.

  • Page 71: Propellers

    BARON G58 PILOT TRAINING MANUAL Detonation Detonation occurs when the engine is run at excessive manifold pressure settings, excessive operating temperatures, excessively lean mixture settings, or if improper fuel grades are used. The result is a loss of engine power and/or engine damage.

  • Page 72: Unfeathering Accumulator

    BARON G58 PILOT TRAINING MANUAL Unfeathering Accumulators Many Baron aircraft equipped with unfeathering accumulators to facilitate an airstart. When airstart procedures are done correctly, unfeathering accumulators cause the propeller to windmill and turn the engine, which provides the fuel flow, airflow, and spark needed for combustion so the starter is not needed.

  • Page 73: Unfeathering Accumulator System

    BARON G58 PILOT TRAINING MANUAL PROPELLER CONTROL LINKAGE SPEEDER SPRING NITROGEN CHARGE CENTRIFUGAL FLY WEIGHTS TO UNFEATHERING ACCUMULATOR PILOT FEATHERING VALVE SPRING ACCUMULATOR TANK RELIEF VALVE RETURN ENGINE TO SUMP GOVERNER PUMP Figure 7-16. Unfeathering Accumulator System Propeller Synchronizer, Synchrophaser, and Synchroscope Use the synchronizer system to prevent the “throbbing”...

  • Page 74: Operation

    BARON G58 PILOT TRAINING MANUAL OPERATION rpm, the governor corrects for the underspeed condition by increasing oil pressure in the The governor assembly controls propeller rpm propeller dome. This drives the propeller blades through a pitch change mechanism in the propeller to a lower pitch causing an increase in rpm.
  • Page 75 BARON G58 PILOT TRAINING MANUAL The propellers are feathered by moving the pro- Aircraft noise is due, in large part, to the speed of peller control lever aft, past a mechanical detent, the propeller blade tips, which may approach or exceed the speed of sound (especially on longer, and into the feathered position.

  • Page 76: Questions

    BARON G58 PILOT TRAINING MANUAL QUESTIONS To answer the following questions, refer to the FlightSafety Pilot Training Manual, Pilot Train- ing Checklist, and ground school notes: ENGINES What happens if the induction air filter What is the oil capacity for your engines?

  • Page 77: Propellers

    BARON G58 PILOT TRAINING MANUAL PROPELLERS Describe the procedure for engine break-in. What does the governor use to control pro- peller rpm? 10. What are the acceptable magneto check drops? What force moves the propeller blades to low pitch? 11. To provide full cooling during takeoff, what two things need to be done? What is the propeller’s governing range? 12.
  • Page 78 BARON G58 PILOT TRAINING MANUAL What should be done about serious nicks or scratches found on the propeller blades dur- ing preflight? What is the maximum rpm drop allowed during the runup feather check? Why? When must the propeller synchronizer sys- tem be turned off? When must power be reduced after takeoff? 7-20...
  • Page 79 BARON G58 PILOT TRAINING MANUAL CHAPTER 8 FIRE PROTECTION CONTENTS Page INTRODUCTION ........................8-1 DESCRIPTION ........................8-2 Cabin Fire Extinguisher ....................8-2 Cabin Smoke Removal ....................8-2 QUESTIONS .......................... 8-3 Revision 0 FOR TRAINING PURPOSES ONLY...
  • Page 80 BARON G58 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page Portable Fire Extinguisher ..................8-2 8-iii Revision 0 FOR TRAINING PURPOSES ONLY...
  • Page 81 BARON G58 PILOT TRAINING MANUAL CHAPTER 8 FIRE PROTECTION INTRODUCTION The Baron G58 aircraft does not incorporate fire detection or extinguishing equipment in the engine nacelles. The aircraft may have a portable hand-held extinguisher in the cockpit. This chapter details smoke removal procedures in the event of a cabin fire. Revision 0.1 FOR TRAINING PURPOSES ONLY...
  • Page 82 BARON G58 PILOT TRAINING MANUAL DESCRIPTION CABIN SMOKE REMOVAL In the event that the cabin has filled with smoke CABIN FIRE EXTINGUISHER or it is necessary to ventilate toxic fumes from the cabin, the cabin may be ventilated as follows: The fire extinguisher for the Baron G58 is •...
  • Page 83 BARON G58 PILOT TRAINING MANUAL QUESTIONS To answer the following questions, refer to the FlightSafety Pilot Training Manual, Pilot Training Checklist, and ground school notes: Does the aircraft have a portable fire extin- guisher? If so, where is it located?
  • Page 84 BARON G58 PILOT TRAINING MANUAL CHAPTER 9 PNEUMATICS CONTENTS Page INTRODUCTION ........................9-1 GENERAL ..........................9-1 COMPONENTS ........................9-2 Pneumatic Pumps ......................9-2 Distribution ........................9-2 Regulators ........................9-3 CONTROLS AND INDICATIONS ..................9-3 DE-ICING PRESSURE Gage ..................9-3 QUESTIONS .......................... 9-4 Revision 0 FOR TRAINING PURPOSES ONLY...
  • Page 85 BARON G58 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page Baron Pneumatic System .................... 9-2 DE-ICING PRESSURE Gage ..................9-3 9-iii Revision 0 FOR TRAINING PURPOSES ONLY...

  • Page 86: Introduction

    BARON G58 PILOT TRAINING MANUAL CHAPTER 9 PNEUMATICS INTRODUCTION This chapter describes the aircraft pneumatic system, which powers the in-flight operation of the wing leading-edge deice system. Understanding the proper operation and interpretation of the indications of these systems helps the pilot control the aircraft in inclement flight conditions. This chapter identifies systems that use pneumatic air for operation, pneumatic air sources, and proper pneumatic system operation.

  • Page 87: Components

    BARON G58 PILOT TRAINING MANUAL COMPONENTS To prevent carbon dust from contaminating the system, two filters (one for each pump) are just downstream of the pressure regulators (Figure PNEUMATIC PUMPS 9-1). Two dry-air, carbon-vane type pumps supply Carbon dust may be present on the aft part of each pressure for the pneumatic system (Figure 9-1).

  • Page 88: Regulators

    BARON G58 PILOT TRAINING MANUAL CONTROLS AND In the event that pneumatic pressure is lost (during a pump failure), the suction being created INDICATIONS by pneumatic air moving through the manifold is lost. This loss in suction alerts the GEA 71 to trigger a PFD warning to alert the pilot.

  • Page 89: Questions

    BARON G58 PILOT TRAINING MANUAL QUESTIONS To answer the following questions, refer to the FlightSafety Pilot Training Manual, Pilot Train- ing Checklist, and ground school notes: Which aircraft system utilizes the pneumatic air pressure? What is the indication of a failed pneumatic...
  • Page 90 BARON G58 PILOT TRAINING MANUAL CHAPTER 10 ICE AND FIRE PROTECTION CONTENTS Page INTRODUCTION ........................ 10-1 GENERAL ..........................10-1 ICE-PROTECTION SYSTEMS ................... 10-2 Surface Deice System ....................10-2 Electrothermal Windshield Anti-Ice ................10-4 Electrothermal Propeller Deice ..................10-4 Pitot Heat ........................10-5 Fuel Vent Heat .......................
  • Page 91 BARON G58 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page 10-1 Baron Pneumatic System ..................10-2 10-2 Wing Deice Boots ..................... 10-3 10-3 Ice Protection Switches ................... 10-3 10-4 Electrothermal Windshield Hot Patch ..............10-4 10-5 Propeller Ammeter ....................10-4 10-iii Revision 0 FOR TRAINING PURPOSES ONLY...

  • Page 92: Introduction

    BARON G58 PILOT TRAINING MANUAL CHAPTER 10 ICE AND RAIN PROTECTION INTRODUCTION This chapter describes the ice- and rain-protection system on the Baron G58. Flight into icing conditions requires knowledge of conditions conducive to icing, and the anti-ice and deice sys- tems available to prevent excessive ice from forming on the aircraft.

  • Page 93: Ice-Protection Systems

    BARON G58 PILOT TRAINING MANUAL ICE-PROTECTION A SURFACE deice switch is on the pilot ICING subpanel (Figure 10-3). The three-position toggle SYSTEMS switch is spring-loaded to the OFF position. When the switch is in the AUTO position, electrical power is used to engage a solenoid attached to Ice-protection equipment includes deice and anti- the low-pressure regulator, which prevents the ice systems:...
  • Page 94 8 seconds to prevent a “bridge” of ice from boots should be checked during the walkaround forming around the inflated boots. for obvious damage such as cuts, nicks, or cracks. Refer to the FlightSafety Training Checklist for the surface deice system preflight operational check and emergency procedures. 10-3...

  • Page 95: Electrothermal Windshield Anti-Ice

    BARON G58 PILOT TRAINING MANUAL ELECTROTHERMAL Refer to the FlightSafety Training Checklist for the windshield heat operational preflight check WINDSHIELD ANTI-ICE and for procedures to achieve maximum defrost- ing with the heater. The electrothermal windshield anti-ice system prevents ice accumulation on a section of the windscreen.

  • Page 96: Pitot Heat

    For these reasons, do not operate the propeller deice system Refer to the FlightSafety Training Checklist for unless the propellers are turning. the fuel vent preflight operational check. Prop deice ammeter indications above or below the green arc indicate a malfunction in the system.

  • Page 97: Limitations

    BARON G58 PILOT TRAINING MANUAL LIMITATIONS • Do not operate the deice boots at outside air temperatures below –40°C/F to prevent permanent damage to the boots. • Maintain at least 130 KIAS when operating in icing conditions to prevent ice buildup on the bottom of the wings.

  • Page 98: Questions

    BARON G58 PILOT TRAINING MANUAL QUESTIONS To answer the following questions, refer to the FlightSafety Pilot Training Manual, Pilot Train- ing Checklist, and ground school notes: What is the operational difference between When may the propeller heat be operated? anti-ice and deice equipment?
  • Page 99 BARON G58 PILOT TRAINING MANUAL When should fuel vent heat and pitot heat be operated? 10. What action is required if the deice boots fail to deflate? 11. What caution is placarded about the use of windshield heat? 10-8 FOR TRAINING PURPOSES ONLY Revision 0...
  • Page 100 BARON G58 PILOT TRAINING MANUAL CHAPTER 11 AIR CONDITIONING CONTENTS Page INTRODUCTION ........................ 11-1 GENERAL ..........................11-1 CABIN VENTILATION SYSTEM ..................11-3 Description and Operation .................... 11-3 HEATING SYSTEM ......................11-4 Description ........................11-4 Operation ........................11-4 AIR-CONDITIONING SYSTEM ..................11-6 Description ........................
  • Page 101 BARON G58 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page 11-1 Baron G58 Environmental System ................11-2 11-2 CABIN VENT AIR Control ..................11-3 11-3 Overhead Fresh-Air Control ..................11-3 11-4 Heater and Overtemperature Switch ................ 11-4 11-5 Baron G58 Heater System ..................11-5 11-6 Heater and Air-Conditioning Switches ..............

  • Page 102: Introduction

    BARON G58 PILOT TRAINING MANUAL CHAPTER 11 AIR CONDITIONING INTRODUCTION This chapter describes the operation and limitations of the Baron G58 environmental systems. Passenger comfort and safety are of prime importance during flight. GENERAL The purpose of the environmental systems is to increase passenger comfort during flight (Figure 11-1).
  • Page 103 BARON G58 PILOT TRAINING MANUAL HEATER BURNER CAN CONDENSER VENT AIR BLOWER EVAPORATOR COMPRESSOR DEFROST CABIN AIR CONTROL CABIN AIR LEGEND CABIN HEAT CONTROL EXHAUST HEATER AIR DEFROST CONTROL FRESH-AIR AIR-CONDITIONER AIR EVAPORATOR PILOT AIR CONTROL INTAKE EXHAUST AIR COPILOT AIR CONTROL Figure 11-1.

  • Page 104: Cabin Ventilation System

    BARON G58 PILOT TRAINING MANUAL CABIN VENTILATION knob on the overhead panel between the pilot and copilot seats (Figure 11-3). The air then enters SYSTEM the cabin through overhead adjustable “eyeball” outlets above each seat. DESCRIPTION AND OPERATION The cabin receives ventilation air through a nose section inlet and a nonicing scoop on the left side of the dorsal fairing.

  • Page 105: Heating System

    BARON G58 PILOT TRAINING MANUAL OPERATION A storm window that may be opened is on the pilot left side window. A fixed exhaust vent, aft The heating system warms ambient air ducted of the windows on the left side of the fuselage, through an iris valve in the nose.
  • Page 106 BARON G58 PILOT TRAINING MANUAL FUEL CABIN HEAT SOLENOID CONTROL VALVE COMBUSTION AIR BLOWER FROM AIRCRAFT FUEL SUPPLY SOLENOID VALVE IGNITER FUEL PUMP THERMOSTAT SENSOR UNHEATED CABIN FAN BURNER CAN CABIN AIR CONTROL IRIS VALVE POSITION SWITCH Figure 11-5. Baron G58 Heater System Airworthiness Directive 82-07-03 requires peri- odic inspection of the heater burner can to check for combustion leaks.

  • Page 107: Air-Conditioning System

    BARON G58 PILOT TRAINING MANUAL • 3. Operate the heater BLOWER for approxi- Pair of evaporators mately 2 minutes to dissipate burner can • Various controls and protection devices heat. This step can be omitted if the heater is turned off in flight and the iris valve is The evaporator and blower assemblies are in the left open for a short period to cool the nose baggage compartment and aft of the rear...

  • Page 108: Limitations

    BARON G58 PILOT TRAINING MANUAL through the cold evaporators and then returned to the cabin for cabin cooling. From the evaporators, the refrigerant returns to the compressor to repeat the air-conditioning cycle. The evaporator blowers automatically function in the LO mode when the air-conditioning sys- tem is turned on.

  • Page 109: Questions

    BARON G58 PILOT TRAINING MANUAL QUESTIONS To answer the following questions, refer to the FlightSafety Pilot Training Manual, Pilot Train- ing Checklist, and ground school notes: State the limitations on the air conditioner. State the source of cabin ventilation air.
  • Page 110 BARON G58 PILOT TRAINING MANUAL CHAPTER 11A AIR CONDITIONING CONTENTS Page INTRODUCTION ......................11A-1 GENERAL ......................... 11A-1 CABIN VENTILATION SYSTEM (2012 MODELS AND AFTER) ....... 11A-2 Description and Operation ..................11A-2 AUTOMATIC CLIMATE CONTROL SYSTEM.............. 11A-3 Description and Operation ..................11A-3 HEATING SYSTEM ......................
  • Page 111 BARON G58 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page 11A-1 Baron G58 Environmental System ..............11A-2 11A-2 Digital Climate Controller Panel ............... 11A-3 11A-3 Climate Controller Panel Location ..............11A-3 11A-4 Combustion Heater .................... 11A-4 11A-5 Baron G58 Heater System ................. 11A-5 11A-6 Master Heater Fan Switch ..................

  • Page 112: Introduction

    BARON G58 PILOT TRAINING MANUAL CHAPTER 11A AIR CONDITIONING INTRODUCTION This chapter describes the operation and limitations of the Baron G58 environmental systems. Passenger comfort and safety are of prime importance during flight. GENERAL The purpose of the environmental systems is to increase passenger comfort during flight (Figure 11A-1).

  • Page 113: Cabin Ventilation System (2012 Models And After)

    BARON G58 PILOT TRAINING MANUAL AIR INTAKE BURNER CAN CONDENSER DEFROST COMP- RESSOR LEGEND HEATER AIR AIR-CONDITIONER AIR CABIN AIR EXHAUST AIR EXHAUST CONDENSER EVAPORATOR Figure 11A-1. Baron G58 Environmental System CABIN VENTILATION After entering the ducting system, the air passes over the heater and enters the cabin through the SYSTEM following:...

  • Page 114: Automatic Climate Control System

    BARON G58 PILOT TRAINING MANUAL AUTOMATIC CLIMATE selects the desired cabin air temperature. The system will automatically turn on the heating CONTROL SYSTEM and or air-conditioning system to reach and maintain the desired temperature. The system will automatically cycle the system ON and OFF DESCRIPTION AND as necessary.

  • Page 115: Heating System

    BARON G58 PILOT TRAINING MANUAL Air-conditioning is delivered through 7 overhead The heating system consists of: vents above the seats of the aircraft, and heated air • Burner can is delivered through the floor vents of the aircraft. If windshield defrost is necessary, the defrost •...

  • Page 116: Operation

    BARON G58 PILOT TRAINING MANUAL FUEL SOLENOID VALVE COMBUSTION AIR BLOWER FROM AIRCRAFT FUEL SUPPLY SOLENOID VALVE IGNITER FUEL PUMP CLIMATE CONTROL SYSTEM THERMOSTAT SENSOR UNHEATED CABIN FAN BURNER CAN CLIMATE CONTROL SYSTEM IRIS VALVE Figure 11A-5. Baron G58 Heater System OPERATION The heating system warm ambient air ducted through an iris valve in the nose.

  • Page 117: Air-Conditioning System

    BARON G58 PILOT TRAINING MANUAL Heater Preflight and Shutdown operate with the landing gear retracted, instead, Ram air through the iris valve provides adequate During the preflight inspection, check the over airflow for heater operation and cool down. temperature circuit breaker to ensure that it has not tripped.

  • Page 118: Operation

    BARON G58 PILOT TRAINING MANUAL HIGH-PRESSURE SWITCH LOW-PRESSURE HIGH-PRESSURE SWITCH POP-OFF VALVE COMPRESSOR EXPANSION VALVE EVAPORATOR RECEIVER-DRYER CONDENSER Figure 11A-7. Baron G58 Air-Conditioning System OPERATION Protection The air-conditioning and blower circuits are pro- The air-conditioning system is activated by the tected by circuit breakers on the left side panel.

  • Page 119: Limitations

    BARON G58 PILOT TRAINING MANUAL Figure 11A-8. Air-Conditioner Compressor Figure 11A-10. Evaporator Figure 11A-9. Condenser Blower LIMITATIONS The air-conditioning system may be used in all phases of flight, including takeoff and landing. Due to engine drag caused buy the engine driven compressor, a slight performance loss will be noted.
  • Page 120 BARON G58 PILOT TRAINING MANUAL The information normally contained in this chapter is not applicable to this particular aircraft. 12-i Revision 0.1 FOR TRAINING PURPOSES ONLY...
  • Page 121 BARON G58 PILOT TRAINING MANUAL The information normally contained in this chapter is not applicable to this particular aircraft. 13-i Revision 0.1 FOR TRAINING PURPOSES ONLY...
  • Page 122 BARON G58 PILOT TRAINING MANUAL CHAPTER 14 LANDING GEAR AND BRAKES CONTENTS Page INTRODUCTION ........................ 14-1 GENERAL ..........................14-1 LANDING GEAR ........................ 14-2 Description ........................14-2 Controls and Indications ....................14-2 Operation ........................14-4 Limitations ........................14-4 NOSEWHEEL STEERING ....................14-5 Description and Operation ....................
  • Page 123 BARON G58 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page 14-1 Landing Gear System ....................14-3 14-2 Landing Gear Handle ....................14-3 14-3 Landing Gear Uplock and Downlock ............... 14-4 14-4 Nose Gear Tow Limits ....................14-4 14-5 Landing Gear Manual Extension Handcrank ............14-5 14-6 Brake Assembly ......................

  • Page 124: Introduction

    BARON G58 PILOT TRAINING MANUAL CHAPTER 14 LANDING GEAR AND BRAKES INTRODUCTION This chapter discusses the Baron G58 landing gear, nosewheel steering, and brake systems. An understanding of the landing gear system aids the pilot in safe and proper operation of the aircraft.

  • Page 125: Landing Gear

    BARON G58 PILOT TRAINING MANUAL LANDING GEAR Tire servicing procedures and inflation values can be found in the Handling, Service, and Maintenance section of the POH. DESCRIPTION A pair of landing gear safety switches is on the Landing gear position is changed by an electric main gear to prevent accidental retraction of the motor and a mechanical actuator assembly landing gear on the ground.
  • Page 126 BARON G58 PILOT TRAINING MANUAL Figure 14-1. Landing Gear System A single red IN TRANS light illuminates anytime one or all of the gear is in transit or in any intermediate position. All of the lights are extinguished when the gear is fully retracted (Figure 14-2).

  • Page 127: Operation

    Do not attempt to retract the gear stowed with the handle accessible. manually. For electrical retraction of the landing gear following a practice manual extension, refer Refer to the FlightSafety Training Checklist for to the FlightSafety Training Checklist. landing gear preflight procedures. 14-4...

  • Page 128: Nosewheel Steering

    After the manual extension is accom- 14-5) in the event of normal extension failure. plished, the position indicators and warning Refer to the FlightSafety Training Checklist for horn may verify that the landing gear is landing gear manual extension procedures.

  • Page 129: Wheels And Brakes

    BARON G58 PILOT TRAINING MANUAL WHEELS AND BRAKES Brake Fluid Reservoir The brake hydraulic fluid reservoir is on the far COMPONENTS wall of the nose baggage compartment (Figure 14-7). The reservoir serves as a storage receptacle for the brake fluid and provides space for thermal Wheel Assemblies expansion of the fluid.

  • Page 130: Operation

    BARON G58 PILOT TRAINING MANUAL PARK BRAKE Knob OPERATION The PARK BRAKE knob on the pilot subpanel Main Brakes (just below the main landing gear control lever, left of the elevator trim tab wheel) controls the When the top of the brake pedal is pushed, a parking brake (Figure 14-8).

  • Page 131: Limitations

    BARON G58 PILOT TRAINING MANUAL Parking Brake To set the parking brake, pull the PARK BRAKE knob out and apply pressure to the toe pedals until firm. To release the parking brake, apply pressure to the toe pedals to equalize pressure in the lines and push the PARK BRAKE knob in.

  • Page 132: Landing Gear

    BARON G58 PILOT TRAINING MANUAL QUESTIONS LANDING GEAR To answer the following questions, refer to the FlightSafety Pilot Training Manual, Pilot Training Checklist, and ground school notes: What type of gear system is on your aircraft? How far should the manual handcrank be...

  • Page 133: Brakes

    BARON G58 PILOT TRAINING MANUAL BRAKES What may happen if both pilots apply brakes simultaneously? What is the type and quantity of brake fluid used on the Baron G58? Why should the parking brake not be set for extended periods of time? When should a brake pad be replaced? Should the brakes be tapped after lift-off? Explain.
  • Page 134 BARON G58 PILOT TRAINING MANUAL CHAPTER 15 FLIGHT CONTROLS CONTENTS Page INTRODUCTION ........................ 15-1 FLIGHT CONTROLS ......................15-2 Description ........................15-2 Components ........................15-2 FLAP SYSTEM ........................15-4 Description ........................15-4 Operation ........................15-5 Emergency/Abnormal ....................15-6 STALL WARNING SYSTEM ....................15-6 Description and Operation ....................
  • Page 135 BARON G58 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page 15-1 Flight Controls ......................15-2 15-2 Baron G58 Flight Controls ..................15-3 15-3 Rudder Pedals ......................15-3 15-4 Electric Trim Control ....................15-4 15-5 Control Lock ......................15-4 15-6 Flap Limit Switches ....................15-4 15-7 Flap System ......................

  • Page 136: Introduction

    BARON G58 PILOT TRAINING MANUAL CHAPTER 15 FLIGHT CONTROLS INTRODUCTION This chapter describes the Baron G58 flight control, flap, and stall warning systems. Familiarization with the aircraft’s flight control and stall warning system is essential to the safety of flight. An understanding of the flap system is necessary to provide optimum aircraft performance.

  • Page 137: Description

    BARON G58 PILOT TRAINING MANUAL FLIGHT CONTROLS Rudder Pedals The pilot and copilot rudder pedals are connected DESCRIPTION through a linkage below the floorboards. The two-position pedals are adjustable by pressing the The flight controls on the Baron G58 are con- spring-loaded lever on the side of the pedal (Fig- ventional cable-operated control surfaces.
  • Page 138 Refer to the Pilot’s Operating Handbook (POH) for electric trim and autopilot preflight and operating procedures. Refer to the FlightSafety Training Checklist for trim runaway emergency procedures. The trim tabs in the cockpit should be “zeroed out”...

  • Page 139: Flap System

    BARON G58 PILOT TRAINING MANUAL installed, never tow the aircraft with the rudder lock installed. Because the rudder lock limits the movement of the nosewheel steering system, damage to the system can occur by towing the aircraft with the lock installed. Instructions for installing the control locks are printed on the con- trol locks themselves.

  • Page 140: Operation

    BARON G58 PILOT TRAINING MANUAL FLAP ACTUATOR LIMIT SWITCHES FLAP ACTUATOR FLAP MOTOR FLAP DRIVE SHAFT FLAP DRIVE SHAFT AND HOUSING AND HOUSING Figure 15-7. Flap System OPERATION Flap position is indicated by three lights adjacent to the flap control switch (Figure 15-8): Preflight Inspection •...

  • Page 141: Emergency/Abnormal

    BARON G58 PILOT TRAINING MANUAL Takeoff Flap Settings pulling the flap motor circuit breaker when the flaps are symmetric. The aircraft is controllable Although takeoff with the flaps is not prohibited, in a full split flap condition by applying generous Beechcraft does not recommend the use of flaps aileron pressure in the direction of the extended for takeoff.

  • Page 142: Questions

    BARON G58 PILOT TRAINING MANUAL QUESTIONS To answer the following questions, refer to the FlightSafety Pilot Training Manual, Pilot Training Checklist, and ground school notes: How can the rudder pedals be repositioned? List the steps to take in the event of an elec- tric pitch trim runaway.
  • Page 143 BARON G58 PILOT TRAINING MANUAL CHAPTER 16 AVIONICS CONTENTS Page INTRODUCTION ........................ 16-1 PITOT SYSTEM ........................16-1 STATIC SYSTEM ......................... 16-3 Normal System Operation ..................... 16-3 Alternate Static System ....................16-3 COMMUNICATION AND NAVIGATION ................. 16-3 Antennas ........................16-3 Emergency Locator Transmitter ..................16-4 Static Discharging ......................
  • Page 144 BARON G58 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page 16-1 Pitot Tube ........................16-2 16-2 Pitot-Static System ....................16-2 16-3 Static Port ......................... 16-3 16-4 Static Air Selector ..................... 16-3 16-5 Antenna Locations ....................16-4 16-6 ARTEX ELT Switch ....................16-4 16-7 Baron G58 Panel .......................

  • Page 145: Introduction

    BARON G58 PILOT TRAINING MANUAL CHAPTER 16 AVIONICS INTRODUCTION This chapter describes the pitot and static systems and basic communication and navigation equipment on the Baron G58. Knowledge of the pitot-static system and its operation is vital to the safety of flight. The pilot should also be familiar with the communication and navigation equipment on the aircraft to ease pilot workload in flight.
  • Page 146 BARON G58 PILOT TRAINING MANUAL circuit breaker on the pilot subpanel. Refer to Figure 16-2 for an illustration of the pitot system. If the pitot tube ram-air inlet becomes obstructed, indicated airspeed will read zero or lower than actual airspeed, depending on the severity of the blockage.

  • Page 147: Static System

    Pilot’s Operating Handbook (POH) when Figure 16-3. Static Port operating on the alternate static air system. The FlightSafety Training Checklist contains proce- dures for activating the alternate static air system. The static lines are drained when the alternate static air selector is placed in the ON ALTER- COMMUNICATION AND NATE position.

  • Page 148: Emergency Locator Transmitter

    BARON G58 PILOT TRAINING MANUAL VOR/LOC ANTENNA GDL 69 COMM 1 ANTENNA ANTENNA GPS ANTENNAS ELT ANTENNA WEATHER RADAR ANTENNA GLIDE-SLOPE ANTENNA COMM 2 TRANSPONDER ANTENNA ANTENNA Figure 16-5. Antenna Locations the copilot seat, and a DME antenna, if installed, ON and ARM positions.

  • Page 149: Static Discharging

    BARON G58 PILOT TRAINING MANUAL FLIGHT INSTRUMENTS STATIC DISCHARGING AND AVIONICS A static electrical charge may build up on the surface of the aircraft in flight. This electrical charge, if retained, can cause interference in avionics flight instruments radio and avionics equipment operation. Static completely integrated into the Garmin G1000 dissipation wicks are on the trailing edge of the integrated avionics system (Figure 16-7).

  • Page 150: Autopilot

    Refer to the FlightSafety Training Checklist for the avion- ics master switch failure procedure. 16-6 FOR TRAINING PURPOSES ONLY...
  • Page 151 BARON G58 PILOT TRAINING MANUAL Figure 16-8. Autopilot Controls on MFD BATTERY BUS AVIONICS BUS AVIONICS CURRENT LIMITER AVIONICS MASTER RELAY AVIONICS POWER CIRCUIT BREAKER AVIONICS COOLING AVIONICS MASTER SWITCH Figure 16-9. Avionics System 16-7 Revision 0 FOR TRAINING PURPOSES ONLY...

  • Page 152: G1000 Synthetic Vision

    BARON G58 PILOT TRAINING MANUAL G1000 SYNTHETIC • Navigation must not be predicated solely upon the use of the Terrain–SVS or TAWS VISION terrain or obstacle data displayed by the SVS. SYNTHETIC VISION OVERVIEW The following SVS enhancements appear on the PFD: •...
  • Page 153 BARON G58 PILOT TRAINING MANUAL Selecting SYN TERR will activate (Figure Other SVS options (Pathways, Horizon Headings 16-11): and Airport Signs) have dedicated softkeys. • Synthetic Terrain When SVS is enabled, the pitch scale increments • are reduced from 20° up and 15° down, to 10° up Flight Path Marker and 7.5°...

  • Page 154: Zero Pitch Line

    BARON G58 PILOT TRAINING MANUAL Zero Pitch Line ° Approach: – Width: 700 feet or one half The Zero Pitch Line is drawn completely across full scale deviation on the the display and represents the aircraft attitude HSI, whichever is less. with respect to the horizon (Figure 16-13).

  • Page 155: Airport Signs

    BARON G58 PILOT TRAINING MANUAL • The FPM works in conjunction with the Pathways feature to assist the pilot in maintaining desired altitudes and direc- tion when navigating a flight plan. When on course and altitude the FPM is aligned inside the pathway boxes.

  • Page 156: Field Of View

    BARON G58 PILOT TRAINING MANUAL Field of View The PFD field of view can be represented on the MFD Navigation Map Page (Figure 16-20). Two dashed lines forming a V-shape in front of the aircraft symbol on the map, represent the forward viewing area shown on the PFD.
  • Page 157 BARON G58 PILOT TRAINING MANUAL QUESTIONS To answer the following questions, refer to the FlightSafety Pilot Training Manual, Pilot Training Checklist, and ground school notes: How is the static system drained? Which instrument uses pitot reference? What occurs if the pitot tube becomes...
  • Page 158 BARON G58 PILOT TRAINING MANUAL How many static wicks are installed on your aircraft? 10. How is the alternate static air system activated? 11. How can power be supplied to the avionics in the event that the avionics master switch fails? 12.
  • Page 159 BARON G58 PILOT TRAINING MANUAL The information normally contained in this chapter is not applicable to this particular aircraft. 17-i Revision 0.1 FOR TRAINING PURPOSES ONLY...
  • Page 160 BARON G58 PILOT TRAINING MANUAL CHAPTER 18 PERFORMANCE WEIGHT CONTENTS Page INTRODUCTION ........................ 18-1 PERFORMANCE ......................... 18-2 General .......................... 18-2 Terminology ........................18-2 Performance Charts ....................... 18-3 WEIGHT AND BALANCE ....................18-3 General .......................... 18-3 Definitions ........................18-5 Special Considerations ....................18-5 Weight and Balance Calculations ..................
  • Page 161 BARON G58 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page 18-1 Weight and Balance, and Takeoff and Landing Data Forms ........18-4 18-2 Seating, Baggage, and Equipment Arrangements ............ 18-6 18-3 Moment Limits vs. Weight ..................18-7 18-iii Revision 0 FOR TRAINING PURPOSES ONLY...

  • Page 162: Introduction

    BARON G58 PILOT TRAINING MANUAL CHAPTER 18 PERFORMANCE, WEIGHT AND BALANCE INTRODUCTION It is the responsibility of the pilot to ensure that the aircraft is properly loaded and aircraft per- formance has been calculated prior to flight. The necessary performance and weight and balance data is provided by the manufacturer in the Pilot’s Operating Handbook (POH).

  • Page 163: General

    This value is not an aerodynamic limit for the Additionally, FlightSafety recommends that the aircraft. pilot of twin-engine aircraft determine accelerate- stop distance, single-engine rate of climb, and Indicated Airspeed (IAS)—The speed of an aircraft...
  • Page 164 BARON G58 PILOT TRAINING MANUAL Maximum Effective Braking—The maximum Many performance charts are divided into amount of braking pressure that can be applied to sections by reference lines to determine the effects of weight, wind, and obstructions. Guidelines the toe brakes without locking the wheels. are then used to calculate the change from the Outside air temperature (OAT)—The free air reference condition.
  • Page 165 BARON G58 PILOT TRAINING MANUAL 18-4 FOR TRAINING PURPOSES ONLY Revision 0...

  • Page 166: Definitions

    BARON G58 PILOT TRAINING MANUAL Refer to Figure 18-2 for seating, baggage, and Arm—The distance aft of the datum of any equipment arrangements. particular weight in the aircraft, used to calculate weight and balance. DEFINITIONS Moment—The force exerted about the center of gravity of any load in the aircraft.
  • Page 167 BARON G58 PILOT TRAINING MANUAL PAYLOAD LOCATIONS FS –10.0 BAGGAGE FS 15.0 FS 39.0 (FRONT SEAT (PILOT) CREW FS 75.0 PASS.) TO FS 82.0 BAGGAGE FS 108.0 (3RD (4th SEAT SEAT FWD FACING PASS AFT FACING PASS PASS.) PASS.) FS 115.0 TO FS 120.0 FS 111.0 TO FS 115.0 BAGGAGE FS 150.0...
  • Page 168 BARON G58 PILOT TRAINING MANUAL 18-7 Revision 0 FOR TRAINING PURPOSES ONLY...

  • Page 169: Questions

    BARON G58 PILOT TRAINING MANUAL QUESTIONS To answer the following questions, refer to the FlightSafety Pilot Training Manual, Pilot Training Checklist, and ground school notes: Which performance calculations is a pilot What use should be made of performance required to figure prior to flight?
  • Page 170 BARON G58 PILOT TRAINING MANUAL APPENDIX A FLIGHT PROFILES CONTENTS Page NORMAL TAKEOFF AND DEPARTURE ..............APPA-2 VISUAL APPROACH AND LANDING ................APPA-4 CLOSED TRAFFIC ......................APPA-6 HIGH-SPEED ILS APPROACH ..................APPA-8 STABILIZED ILS APPROACH ...................APPA-10 TYPICAL NONPRECISION APPROACH ..............APPA-12 CIRCLING APPROACH ....................APPA-14 ABORTED TAKEOFF ....................APPA-18 ENGINE FAILURE AFTER LIFT-OFF (GEAR DOWN) ...........APPA-20 ENGINE FAILURE AFTER LIFT-OFF (GEAR UP) ...........APPA-22 SINGLE-ENGINE VISUAL APPROACH AND LANDING ........APPA-24...
  • Page 171 BARON G58 PILOT TRAINING MANUAL ILLUSTRATIONS Figure Title Page APP A-1 Normal Takeoff and Departure ..............APPA-3 APP A-2 Visual Approach and Landing ..............APPA-5 APP A-3 High-Speed ILS Approach ................ APPA-9 APP A-4 Stabilized ILS Approach ................ APPA-11 APP A-5 Typical Nonprecision Approach .............
  • Page 172 BARON G58 PILOT TRAINING MANUAL APPENDIX A FLIGHT PROFILES APPA-1 Revision 0.1 FOR TRAINING PURPOSES ONLY...

  • Page 173: Normal Takeoff And Departure

    BARON G58 PILOT TRAINING MANUAL NORMAL TAKEOFF AND DEPARTURE Before takeoff checklist items complete. The following items should be considered: 1. Current weather/terrain conditions 2. Departure procedure 3. Takeoff alternate, if necessary 4. Engine failure or other event prior to liftoff 5.
  • Page 174 BARON G58 PILOT TRAINING MANUAL CLIMBING THROUGH 500' AGL 1. CRUISE CLIMB POWER—SET 2. MIXTURES—LEAN, IF NECESSARY 3. CRUISE CLIMB CHECKLIST—COMPLETE AT LIFTOFF SPEED 1. ROTATE APPROX. 7° - 10° NOSE UP BRAKE RELEASE PITCH ESTABLISHED 1. BRAKES—APPLY 1. POSITIVE RATE OF 2.

  • Page 175: Visual Approach And Landing

    BARON G58 PILOT TRAINING MANUAL VISUAL APPROACH AND LANDING Descent Checklist complete Prior to entering traffic pattern: 1. Slow to 150 KIAS or less 2. Set approach power 3. Establish approach configuration 4. Maintain traffic pattern altitude 5. Approach Checklist complete On Downwind: 1.
  • Page 176 BARON G58 PILOT TRAINING MANUAL 6. Establish landing approach speed 7. Disengage yaw damper Cross threshold at landing speed, plus gust correction, if necessary After touchdown: 1. Apply brakes as necessary 2. Ground lean mixtures, if necessary After clearing runway, complete After Landing Checklist IF A GO-AROUND IS NECESSARY 1.

  • Page 177: Closed Traffic

    BARON G58 PILOT TRAINING MANUAL CLOSED TRAFFIC Before takeoff checklist items complete. The following items should be considered: 1. Current weather/terrain conditions 2. Departure procedure 3. Takeoff alternate, if necessary 3. Engine failure or other event prior to liftoff 4. Lean mixtures for takeoff, if necessary 5.
  • Page 178 BARON G58 PILOT TRAINING MANUAL On base: 1. Establish speed at 110 KIAS 2. Verify final approach path clear If a go-around (balked landing) becomes necessary: 1. Increase power to maximum 2. Establish pitch for balked landing climb 3. Establish a positive rate of climb 4.

  • Page 179: High-Speed Ils Approach

    BARON G58 PILOT TRAINING MANUAL HIGH-SPEED ILS APPROACH Descent Checklist complete and approach reviewed Transition at high speed: 1. Set high-speed transition configuration 2. Confirm avionics set for approach 3. 150 KIAS maximum Prior to or during the procedure turn or prior to final vector, complete the Approach Checklist At glideslope intercept: 1.
  • Page 180 BARON G58 PILOT TRAINING MANUAL After touchdown: 1. Apply brakes as necessary 2. Ground lean mixtures, if necessary After clearing runway, complete After Landing Checklist PRIOR TO IAF MANEUVER TO FINAL 1. DESCENT CHECKLIST—COMPLETE 1. APPROACH CHECKLIST—COMPLETE 2. ESTABLISH APPROACH CONFIGURATION 3.

  • Page 181: Stabilized Ils Approach

    BARON G58 PILOT TRAINING MANUAL STABILIZED ILS APPROACH Descent Checklist complete and approach reviewed Transition for stabilized approach: 1. Establish approach configuration 2. Confirm avionics set for approach 3. Stabilize airspeed at 120 KIAS Prior to or during the procedure turn or prior to final vector, complete the Approach Checklist At glideslope intercept: 1.
  • Page 182 BARON G58 PILOT TRAINING MANUAL PRIOR TO IAF 1. DESCENT CHECKLIST—COMPLETE 2. SET HIGH SPEED TRANSITION MANEUVER TO FINAL CONFIGURATION 1. APPROACH CHECKLIST—COMPLETE 3. AVIONICS—CONFIRM SET 4. AIRSPEED—150 KIAS (MAX) GLIDESLOPE INTERCEPT DECISION HEIGHT 1. LANDING GEAR—DOWN (MISSED APPROACH) 2. SET NORMAL APPROACH POWER 3.

  • Page 183: Typical Nonprecision Approach

    BARON G58 PILOT TRAINING MANUAL TYPICAL NONPRECISION APPROACH Descent Checklist complete and approach reviewed Transition for stabilized approach: 1. Establish approach configuration 2. Confirm avionics set for approach 3. Stabilize airspeed at 120 KIAS Prior to or during the procedure turn or prior to final vector, complete the Approach Checklist At final approach fix inbound: 1.
  • Page 184 BARON G58 PILOT TRAINING MANUAL Cross threshold at landing speed, plus gust correction, if necessary After touchdown: 1. Apply brakes as necessary 2. Ground lean mixtures, if necessary After clearing runway, complete After Landing Checklist PRIOR TO IAF MANEUVER TO FINAL 1.

  • Page 185: Circling Approach

    BARON G58 PILOT TRAINING MANUAL CIRCLING APPROACH Descent Checklist complete and approach reviewed Transition for stabilized approach: 1. Establish approach configuration 2. Confirm avionics set for approach 3. Stabilize airspeed at 120 KIAS Prior to or during the procedure turn or prior to final vector, complete the Approach Checklist At final approach fix inbound: 1.
  • Page 186 BARON G58 PILOT TRAINING MANUAL PRIOR TO IAF 1. DESCENT CHECKLIST—COMPLETE MANEUVER TO FINAL 2. APPROACH POWER—SET 1. APPROACH CHECKLIST—COMPLETE 3. ESTABLISH APPROACH CONFIGURATION 4. AVIONICS SET FOR APPROACH 5. AIRSPEED—STABILIZE AT 120 KIAS MISSED APPROACH POINT (MISSED APPROACH) FAF INBOUND 1.
  • Page 187 BARON G58 PILOT TRAINING MANUAL With the runway in sight and in a position to land: 1. Reduce power for landing 2. Extend full flaps 3. Increase mixtures to full rich 4. Advance propeller controls to full forward 5. Confirm landing gear down 6.
  • Page 188 BARON G58 PILOT TRAINING MANUAL INTENTIONALLY LEFT BLANK APPA-17 Revision 0.1 FOR TRAINING PURPOSES ONLY...

  • Page 189: Aborted Takeoff

    BARON G58 PILOT TRAINING MANUAL ABORTED TAKEOFF Before takeoff checklist items complete. The following items should be considered: 1. Current weather/terrain conditions 2. Departure procedure 3. Takeoff alternate, if necessary 4. Engine failure or other event prior to liftoff 5. Engine failure or other event after liftoff, with gear up or down When aligned with runway: 1.
  • Page 190 BARON G58 PILOT TRAINING MANUAL EVALUATE SITUATION I.E. CLEAR RUNWAY EMERGENCY EVACUATION ENGINE FAILURE 1. THROTTLES—IDLE 2. BRAKING—MAXIMUM IF AIRCRAFT CANNOT BE STOPPED ON REMAINING RUNWAY: 3. MIXTURES—IDLE CUTOFF 4. MAGNETO SWITCHES—OFF 5. BATTERY AND ALTERNATOR SWITCHES—OFF 6. FUEL SELECTORS—OFF 7.

  • Page 191: Engine Failure After Lift-Off (Gear Down)

    BARON G58 PILOT TRAINING MANUAL ENGINE FAILURE AFTER LIFT-OFF (GEAR DOWN) Before takeoff checklist items complete. The following items should be considered: 1. Current weather/terrain conditions 2. Departure procedure 3. Takeoff alternate, if necessary 4. Engine failure or other event prior to liftoff 5.
  • Page 192 BARON G58 PILOT TRAINING MANUAL Evacuate aircraft as soon as possible IF THE AIRCRAFT CANNOT BE STOPPED ON REMAINING RUNWAY 1. RETARD MIXTURES TO IDLE CUTOFF 2. MAGNETO/START SWITCHES—OFF 3. BATTERY AND ALTERNATOR SWITCHES—OFF 4. MANEUVER, AS NECESSARY, TO AVOID OBSTACLES 5.

  • Page 193: Engine Failure After Lift-Off (Gear Up)

    BARON G58 PILOT TRAINING MANUAL ENGINE FAILURE AFTER LIFT-OFF (GEAR UP) Before takeoff checklist items complete. The following items should be considered: 1. Current weather/terrain conditions 2. Departure procedure 3. Takeoff alternate, if necessary 4. Engine failure or other event prior to lift-off 5.
  • Page 194 BARON G58 PILOT TRAINING MANUAL Return to departure airport for landing or continue to takeoff alternate, if applicable. When time and altitude permit, complete Engine Failure After Lift-Off Gear Up checklist. Proceed with appropriate single-engine approach and landing procedure. SECURE AND RETURN 1.

  • Page 195: Single-Engine Visual Approach And Landing

    BARON G58 PILOT TRAINING MANUAL SINGLE-ENGINE VISUAL APPROACH AND LANDING Descent checklist complete Prior to entering traffic pattern: 1. Slow to 150 KIAS or less 2. Set approach power 3. Establish clean or approach configuration as necessary 4. Maintain traffic pattern altitude 5.
  • Page 196 BARON G58 PILOT TRAINING MANUAL 6. Establish landing approach speed 7. Retrim as necessary Cross threshold at landing speed, plus gust correction is necessary After touchdown, during rollout: 1. Apply braking as necessary 2. Ground lean mixtures, if necessary After clearing runway, complete after landing checklist. IF A SINGLE-ENGINE GO-AROUND IS NECESSARY 1.

  • Page 197: Single-Engine Ils Approach

    BARON G58 PILOT TRAINING MANUAL SINGLE-ENGINE ILS APPROACH NOTE Keep the procedure as normal as possible. With the exception of power settings, single-engine ILS procedures are essentially the same as normal ILS approach procedures. Descent checklist complete and approach reviewed Transition for approach: 1.
  • Page 198 BARON G58 PILOT TRAINING MANUAL 6. Establish landing approach speed 7. Retrim as necessary Cross threshold at landing speed, plus gust correction is necessary After touchdown, during rollout: 1. Apply braking as necessary 2. Ground lean mixture if necessary After clearing runway, complete after landing checklist. PRIOR TO IAF 1.

  • Page 199: Single-Engine Nonprecision Approach

    BARON G58 PILOT TRAINING MANUAL SINGLE-ENGINE NONPRECISION APPROACH NOTE It is recommended a straight-in approach with vertical guidance be used in single-engine procedures. Nonprecision circling approaches are not recommended. Keep the procedure as normal as possible. With the exception of power settings and configuration management, single-engine approach procedures are essentially the same as normal approach procedures.
  • Page 200 BARON G58 PILOT TRAINING MANUAL 3. Extend flaps at pilot’s discretion 4. Increase mixture on operating engine to full rich 5. Increase propeller control on operating engine to full forward 6. Establish landing approach speed 7. Retrim as necessary Cross threshold at landing speed, plus gust correction, if necessary. After touchdown, during rollout: 1.
  • Page 201 BARON G58 PILOT TRAINING MANUAL BEGINNING OF MANEUVER STALL AND RECOVERY COMPLETION OF MANEUVER 1. RECOVER AT FIRST INDICATION OF 1. ACCELERATE TO DESIRED AIRSPEED 1. MAINTAIN ALTITUDE STALL (STALL BUFFET) 2. RETURN TO DESIRED ALTITUDE 2. AIRSPEED—STABILIZED AT 85 KIAS 2.
  • Page 202 BARON G58 PILOT TRAINING MANUAL BEGINNING OF MANEUVER STALL AND RECOVERY COMPLETION OF MANEUVER 1. RECOVER AT FIRST INDICATION OF A 1. ACCELERATE TO DESIRED AIRSPEED 1. MAINTAIN ALTITUDE STALL (STALL BUFFET) 2. RETURN TO DESIRED ALTITUDE 2. FLAPS—FULL 2. SIMULTANEOUSLY REDUCE PITCH AND 3.
  • Page 203 BARON G58 PILOT TRAINING MANUAL BEGINNING OF MANEUVER STALL AND RECOVERY COMPLETION OF MANEUVER 1. RECOVER AT FIRST INDICATION OF 1. ACCELERATE TO DESIRED AIRSPEED 1. MAINTAIN ALTITUDE STALL (STALL BUFFET) 2. RETURN TO DESIRED ALTITUDE 2. FLAPS—UP 2. SIMULTANEOUSLY REDUCE PITCH AND 3.
  • Page 204 BARON G58 PILOT TRAINING MANUAL APPENDIX B TERMS AND ABBREVIATIONS AFCS Automatic flight control system Mach number Airplane Flight Manual Multifunction display AHRS Altitude and heading reference system Outside air temperature BMEP Brake mean effective pressure Primary flight display Calibrated airspeed Pilot’s Operating Handbook Circuit breaker R BAT...

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