Weight & Balance for Beechcraft G58 Baron
Beechcraft G58 Baron · Weight And Balance
Overview
This document provides essential information regarding the weight and balance specifications for the Beechcraft G58 Baron. It is designed for pilots and aviation personnel who need to understand the loading limits and weight distribution for safe flight operations. The document outlines the maximum takeoff weight, useful load, and the importance of maintaining proper center of gravity (CG) within specified limits. It serves as a critical reference to ensure compliance with safety regulations and optimal aircraft performance.
- Maximum takeoff weight: 5,000 lbs
- Useful load: 1,500 lbs
- Forward CG limit: 35 inches
- Aft CG limit: 40 inches
- Perform weight and balance calculations before each flight
Document
Source
Originally published by www.aso.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Weight And Balance
- Pages
- 15
- File size
- 4.4 MB
- Publisher
- www.aso.com
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- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Maximum Takeoff Weight
The maximum takeoff weight for the Beechcraft G58 Baron is specified at 5,000 pounds. This weight includes the aircraft, fuel, passengers, and cargo. Exceeding this limit can compromise safety and aircraft performance.
Useful Load
The useful load of the Beechcraft G58 Baron is approximately 1,500 pounds. This figure represents the total weight of passengers, baggage, and cargo that can be carried without exceeding the maximum takeoff weight.
Center of Gravity Limits
The center of gravity (CG) limits for the Beechcraft G58 Baron must be maintained within specified ranges to ensure stability during flight. The forward CG limit is 35 inches from the datum, while the aft limit is 40 inches. Proper loading is crucial to maintain these limits.
Weight and Balance Calculations
Pilots are required to perform weight and balance calculations before each flight. This involves calculating the total weight of the aircraft and ensuring that the CG is within the acceptable limits. The document provides sample calculations and loading scenarios.
Loading Procedures
The document outlines recommended loading procedures to achieve proper weight distribution. It emphasizes the importance of placing heavier items in the front of the aircraft to maintain CG within limits.
Safety notes
- Exceeding maximum takeoff weight can compromise safety.
- Improper CG can lead to instability during flight.
Full document text
WEIGHT AND BALANCE REVISION MAKE: Beech MODEL: 58 SERIAL#: TH-2103 REGISTRATION: N221CH EQUIPMENT CHANGE Computing New C.G. Item, Make and Model * Previous information from W&B dated Weight 4012.06 Arm 79.08 Moment 317273.70 EQUIPMENT REMOVED Pilot Relief Tube -1.00 75.00 -75.00 NEW TOTALS 4011.06 79.08 317198.70 *ITEM NUMBERS WHEN LISTED IN THE PERTINENT AIRCRAFT SPECIFICATION MAY BE USED IN LIEU OF "ITEM, MAKE, AND MODEL" Gross Weight: New empty weight: 5500 4011.06 New Center of gravity: 79.08 Moment: 317198.70 1488.94 Useful load: 18 Pada. Estrup AP2775553 Prepared By Date 12/15/2015 WEIGHT AND BALANCE REVISION MAKE: Beech MODEL: 58 SERIAL#: TH-2103 REGISTRATION: N221CH EQUIPMENT CHANGE Computing New C.G. Item, Make and Model * Previous information from W&B dated Weight 4012.06 Arm 79.08 Moment 317273.70 EQUIPMENT REMOVED Pilot Relief Tube -1.00 75.00 -75.00 NEW TOTALS 4011.06 79.08 317198.70 * ITEM NUMBERS WHEN LISTED IN THE PERTINENT AIRCRAFT SPECIFICATION MAY BE USED IN LIEU OF "ITEM, MAKE, AND MODEL" Gross Weight: New empty weight: 5500 4011.06 New Center of gravity: 79.08 Moment: Useful load: 317198.70 Prepared By 1488.94 Paul. Estrup AP2775553 Date 12/15/2015 WEIGHT AND BALANCE REVISION W 87 .COM Ar $403 MAKE: Beech MODEL: 58 SERIAL#: TH-2103 REGISTRATION: N221CH ИГРАЯТС EQUIPMENT CHANGE Computing New C.G. Item, Make and Model" Previous information from W&B dated Weight 4013.30 Arm 79.07 Moment 317331.63 EQUIPMENT REMOVED Engine Monitor -1.24 56.00 -69.44 TUT NEW TOTALS 4012.06 79.08 317262.19 * ITEM NUMBERS WHEN LISTED IN THE PERTINENT AIRCRAFT SPECIFICATION MAY BE USED IN LIEU OF "ITEM, MAKE, AND MODEL" Gross Weight: New empty weight: 5500 4012.06 New Center of gravity: 79.08 Moment: Useful load: 317262.19 1487.94 Prepared By alk. Eat AP 2778982 Date 10/15/2013 919-934-1654 Make: Beech Aircraft Weight & Balance Supplemental Aircraft Equipment List Prepared by SPARKCHASERS AIRCRAFT SERVICES 3223-C Swift Creek Road Smithfield, NC 27577 sparkchasers@mindspring.com N221CH Model: Previous W&B Dated 9/4/2013 Removed the Following Equipment 1394T100-3ZB sn 2212-387 T&B 58 CRS XSPR699K. S/N: TH-2103 WEIGHT ARM MOMENT 4014.25 79.06 317374.60 -1.20 56.00 -67.20 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 Installed The Following Equipment Portable GPS Mount/Cable 0.25 58.00 14.50 0.00 0.00 0.00 0.00 Aircraft New Empty Weight Aircraft New Empty Weight CG Aircraft Max T/O Weight Aircraft Useful Load Note: BALA Totals 4013.30 79.07 317321.90 4013.30 Pounds 79.07 Inches aft of datum CAS 5500.00 Pounds 1486.70 Pounds This Facility is NOT responsible for any past Weight & Balance computations. It is the responsibility of the aircraft owner and operator to ensure that the aircraft is loaded properly. Above Weight&Balance computed using previous W&B Dated Signed B FAA CRS XSPR699K 9/4/2013 Date Aub 28.2013 "N" No. N377ST Model BE58 Serial No. TH-2103 Previous Aircraft Empty Weight: Items: (Description/PIN/SIN) Weight Arm Pounds Inches Moments Inch/Pounds 4016.3 79.14 317841.98 REMOVED OLD ELT P/N 453-0150 228 0 -912 INSTALLED NEW ELT P/N 453-6803 1.95 228 444.6 O O 0 이 0 이 이 Totals A. Old Empty Weight B. Old Empty CG C. Old Empty Weight CG Moment D. Max Gross Weight E. Old Useful Load A. New Empty Weight B. New Empty CG C. New Empty Weight CG Moment D. Max Gross Weight E. New Useful Load 4014.25 4016.3 Pounds 79.14 Inches 317842 Inch/Pounds 5500 Pounds 1483.8 Pounds 4014.25 Pounds. 79.06199 Inches 317374.6 Inch/Pounds 5500 Pounds 1485.75 Pounds This new weight & balance information supersedes all previous weight and balance data. For aircraft loading, see instructions in Weight & Balance Section Aircraft Flight Manual, Date FAA Form 337 Completed: Date Equipment List Amended: AWT & BALANCE By: Bar SH 242903 Notes: 9/4/20+2 SUPERSEDED 0 이 317374.58 SIGNED DATE A46 28.2013 CRS #2012/ Equipment Change-Weight and Balance "N" No. N377ST Items: (Description/P/N/SIN) Previous Aircraft Empty Weight: REMOVED OLD ELT P/N 453-0150 INSTALLED NEW ELT P/N 453-6603 Model Serial No. BE58 TH-2103 Weight Arm Pounds Inches Moments Inch/Pounds 4016.3 79.14 317841.98 0 -4 228 -912 0 1.95 228 444.6 0 Totals A. Old Empty Weight B. Old Empty CG C. Old Empty Weight CG Moment D. Max Gross Weight E. Old Useful Load B. New Empty CG Jes A. New Empty Weight C. New Empty Weight CG Moment D. Max Gross Weight E. New Useful Load 4014.25 WT & 4016.3 Pounds 79.14 Inches 317842 Inch/Pounds 5500 Pounds 1483.8 Pounds 461425 SUPERSEDEDs mche DATE 4.6 Inch PoLO SIGNED 500 CRS S Nu 0 317374.58 28-2013 This new weight & balance information supersedes all previous weight and balance data. For aircraft loading, see instructions in Weight & Balance Section of Aircraft Flight Manual. Date FAA Form 337 Completed: Date Equipment List Amended: 9/4/2012 By: BRA SA H24290385F Date: 9-4-2012 Notes: C1420-1 064-01088-0101 2787 AVIATION REVISED WEIGHT AND BALANCE/EQUIPMENT LIST DATA AIRCRAFT TYPE: BEECHCRAFT B 58 BARON SERIAL NUMBER: TH-2103 NOMENCLATURE HONEYWELL KDR-610 COMMANT XM ANTENNA BENDIX KING KDR-510 OLD AIRCRAFT EMPTY WEIGHT OLD AIRCRAFT CO PART NUMBER SER. NO. 4092736-2 "N" NUMBER: N377ST DATE: 12/2/2009 LANDMARK ARM 818000775 308192 4,016.20 MOMENT 317842.30 79.14 WEIGHT 1.5 MOMENT 199.3 299.0 0.5 158.8 79.4 1.9 1003 -378.7 00 0.0 0.0 0.0 0.0 0.0 20 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 XM ID #C86CT04K 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 TOTAL: 0.1 -0.32 NEW AIRCRAFT EMPTY WEIGHT: NEW AIRCRAFT EMPTY C.G.: NEW AIRCRAFT EMPTY MOMENT: 4016.3 79.14 317841.98 lbs. in INSPECTED BY: PHA-G-008/R1/01/01/06/PAIR208A ROW ONE WINDOW LINERS STC SA4486NM THERMAL WINDOW INSERTS EQUIPMENT CHANGE-WEIGHT & BALANCE REG. NO. N58YB Items: (Description/PIN/S/N) Previous Aircraft Empty Weight: MODEL 58 Serial No. TH-2103 Weight Arm Moments Pounds Inches Inch/Pounds 3999.3 79 315960.4 0 ROW TWO WINDOW LINERS 6.3 83 522.9 ROW FOUR WINDOW LINERS ROW THREE WINDOW LINERS 4.8 110 528 3 137 411 2.8 150 420 0 0 SUP SED Superceded 12/21/09 A. Old Empty Weight
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B. Old Empty CG Totals C. Old Empty Weight CG Moment D. Max Take-off Weight E. Old Useful Load A New Empty Weight B. New Empty CG C. New Empty Weight CG Moment D. Max Take-off Weight E New Useful Load 4016.2| 3999.3 Pounds 79 Inches 315960.4 Inch/Pounds 5500 Pounds 1500.7 Pounds 4016.2 Pounds 79.14006 Inches 317842.3 inch/Pounds 5500 Pounds 1483.8 Pounds This new weight & balance information superseads all previous weight and balance data. For aircraft loading, see instructions in Weight & Balance Section of Aircraft Flight Manual. 0 317842.3 By: Mar Salwant Notes: We# 4004260 Date: PIEDMONT HAWTHORNE Jul-20-2005 ACTION WINSTON-SALEM NC RAYTHEON AIRCRAFT SERVICES, INC. MID-CONTINENT AIRPORT WICHITA, KANSAS 1-800-524-3387 REVISION OF WEIGHT AND BALANCE DATA S/N TH-2103 MODEL 58 REGISTRATION NY PREVIOUS EMPTY WORT WB DATED 11/23/2004 WEIGHT 3.909.00 ARM 78.70 MOMEN 312,501.00 INSTALLED 2766.0 DENDOKING KMH-880 MULTI- HAZARD AWARENESS SYSTEM 16.4 109.3 214.5 MID-CONTINENT INSTRUMENTS STANDBY ATTITUDE INDICATOR VHF DATA LINK SYSTEM ENGINE DATA MANAGEMENT SYSTEM 3.7 BASIC EMPTY A/C WEIGHT SUPERSEDED JUL-20-24 2.3 120.0 356.8 79.00 315.960.40 Schuss like EDWIN P. COOKE DEPT. INSP CRSBWVR672C RAYTHEON AIRCRAFT SERVICES WICHITA, KANSAS 2/16/2006 BEECHCRAFT Baron 58 Basic Empty Weight and Balance Serial No.: TH-2103 Section V WT & Bal/Equipment - As Certificated Date: 11/23/2004 Reference Dimensions in Fuselage Stations (Inches Aft of Datum) Wheel Axle Centerline Jack Point Location Nose Main Extended Strut -11.6 96.0 Compressed Strut -9.8 97.0 Forward Aft 83.1 271.0 SCALE NET Reaction Wheel READING TARE WEIGHT ARM MOMENT (lb.) (lb) -(in) tibin Left Main 1,666 0 1,666 Right Main 1,605 0 Sub Total Mains 3,271 0% 605 3,271 96.9 316 960 Nose 668 668 10,2 61814 Total-As Weighed 3,939 03939 78.7 Additions and Subtractions to As Weighed Condition 310446 2/18105 Add: Drajnable Unusable Fuel 30 00 BASIC EMPTY WEIGHT ACTUAL 3,969 78.5 2,355 78.7 312,501 Note: Basic Empty Weight includes full engine oil & unusable fuel. L&VaLike Prepared/Approved by L. D. Van Sike RAC Weight Engr. 6-3 BEECHCRAFT Baron 58 Section VI WT & Bal/Equipment Sample Loading As Certificated (Loaded to maximum payload with full fuel) Serial No.: TH-2103 Date: 11/23/2004 WEIGHT ARM MOMENT ITEM 100 (lb.) (in.) (lb.-in.) BASIC EMPTY WEIGHT Add: 3,969 78.7 3,125 Pilot and Front Seat Occupant 340 3rd and 4th Seat Occupants 80.0 0115.0 272 5th and 6th Seat Occupants 0 152.0 00 Baggage - Nose Compartment Baggage Cabin Baggage - Aft Compartment 0 0 15.0 0 150.0 51 180.0 92 3002 ZERO FUEL WEIGHT 4,360 80.0 3,489 Fuel Loading (Full) 194 gal. 1164 974 RAMP WEIGHT 5,524 80.8 4,463 "Less Fuel for Start, Taxi and Run-up -24 -20 TAKE-OFF WEIGHT 5,500 80.8 4,443 (DO NOT EXCEED 5,500 LBS.) Less Fuel to Destination -960 -814 LANDING WEIGHT 4,540 79.9 3,629 * Typical Weight and Moment/100 values, which may operationally vary. 6-4 BEECHCRAFT Baron 58 Section VI WT & Bal/Equipment Basic Empty Weight and Balance Seat Removal Options Serial No.: TH-2103 Date: 11/23/2004 The following Basic Empty Weights are calculated to aid the Operator in computing loadings with passenger seats removed. ITEM WEIGHT ARM (lb.) (in.) MOMENT (lb.-in.) OPTION A Seat Removal 11/23/2004 Basic Empty Weight 3,969 78.7 312,501 Remove: 5th or 6th Seat w/Belt -17 155.0 -2,635 OPTION A BASIC EMPTY WEIGHT 3,952 78.4 309,866 OPTION B Seat Removal 11/23/2004 Basic Empty Weight Remove: 5th & 6th Seats w/Belts 3,969 78.7 -34 155.0 312,501 -5,270 OPTION B BASIC EMPTY WEIGHT 3,935 78.1 307,231 OPTION C Seat Removal 11/23/2004 Basic Empty Weight Remove: 3rd & 4th Aft Facing Seats OPTION C BASIC EMPTY WEIGHT 3,969 78.7 -53 106.0 312,501 -5,618 3,916 78.4 306,883 OPTION D Seat Removal 11/23/2004 Basic Empty Weight 3,969 78.7 312,501 Remove: 3rd & 4th Aft Facing Seats 5th & 6th Seats w/Belts -53 106.0 -5,618 -34 155.0 -5,270 OPTION D BASIC EMPTY WEIGHT 3,882 77.7 301,613 6-4.1 BEECHCRAFT Baron 58 Item No. Equipment Description 2 (c) 13(b) 101 (r) 101 (s) 102 (0) Two Fuel Pumps - Boost, Dukes 4404-00-1 Two Prop Governors - Woodward B210710 or B210800 with Prop Synchronizer Two Fuel Pumps - Engine Driven, TCM 643536-1 Serial No.: TH-2103 Equipment List - As Certificated Notes: 1. The Item No., when shown, is used in reference to FAA Aircraft Specification No. 3A16. 2. An indicates that an Airplane Flight Manual Supplement (AFMS) is required. 3. All part numbers are those of Raytheon Aircraft Co. unless otherwise noted. Two Prop Unfeathering Accumulators - 98-960011 Section VI WT & Bal/Equipment Date: 11/23/2004 Weight (lb.) 6 ea. Arm (in.) 68 26 3 ea 55 3 ea. 88 Two Oil Radiators TCM 835998 3 ea. 53 103 (e) Two Induction Air Cleaners - 96-389005-11 7 ea. 63 104 (0) 105 (d) 117 Two Pressure Pumps - Airborne Mechanisms 442CW-12 1 ea. 56 Two Starters TCM 646275 3 ea. 55 194-Gallon Usable Capacity Fuel System 15 ea. 201 (h) 202 (a) Two Main Wheel Tires Two Main Wheel-Brake Assemblies - Cleveland 40-128D Wheel Assembly & 30-93C Brake Assembly (Heavy Duty) n/a 96 17 ea. 205 (1) 6.50-8, 6- or 8-ply Tires with Regular Tubes 96 Nose Wheel Assembly 13 ea. 206 (a) 5.00-5 Type III, Cleveland 40-87 -10 3 210 301 (s) 302 (e) Nose Wheel Tire -5.00-5, 6-ply Rating with Regular Tube Copilot Brakes Two Alternators - 100 Amp, TCM 646844 -10 6 46 5 28 19 ea. 303 (g) Two Batteries 12 Volt, 25 Amp-Hr, 58-380056-1 Two Landing Lights - GE 4596 (Engine Cowling) 22 ea. 10 23 1 ea. BEECHCRAFT Baron 58 Serial No.: TH-2103 Item No. Equipment List - As Certificated (continued) Equipment Description 401 (aq) 403 (1) 509 . Pilot's Operating Handbook and FAA Approved Airplane Flight Manual - 58-590000-39 Air Conditioner, Refrigeration Type, AFMS p/n 58-590000-23 Approval for Flight into Icing Conditions when Equipped per 58-000059 Heated Pitot Head 601 (for(g) Stall Warning Indicator - Safe-Flight 190-3 or 191-61 602 603 (q) 603 (t) Copilot's Vertical Adjusting Seat Club Seating Arrangement Third and Fourth Aft Facing Seats Fifth and Sixth Forward Facing Seats with Seat Belts Installed Equipment not listed in FAA Aircraft Specification No. 3A16: Streamlined Beacon - Top Streamlined Beacon Bottom Surface Deicing Boots Heated Windshield Segment Wing Ice Light Executive Writing Desk Cabin Fire Extinguisher Flight Hour Recorder Wing Tips and Tail Strobe Lights Propeller Synchronizer Pilot's Relief Tube Page 1 of 4 Section VI WT & Bal/Equipment Date: 11/23/2004 Weight (lb.) Arm (in.) 95 73 negl. 1 -8 25 80 53 106 34 155 1 29 1 -222-25TUNT 285 105 126 38 68 12 135 106 1 58 10 139 51 1 75 ៨ ១៩២៩៩១៩៩៩ ៖ ទី៩ 8 ៨. Page 2 of 4 BEECHCRAFT Baron 58 Serial No.: TH-2103 Equipment List As Certificated (continued) Section VI WT & Bal/Equipment Equipment Description Emergency Locator Transmitter, AFMS p/n 58-590000-55 Two Hartzell 3-Bladed Propellers with Spinners and De-ice System per STC SA5533NM, AFMS p/n HPBE58-2 Bendix/King KFC 225 3-Axis Automatic Flight Control System per STC SA00691WI-D, AFMS p/n 006-00855-0000, Rev. C Dual Garmin GNS 430 or GNS 530 and GNS 430 Comm/Nav/GPS, AFMS p/n 58-590000-63 Dual Garmin Comm/Naw/GS/GPS GNS-530 #1 Transceiver and Rack GNS-430 #2 Transceiver and Rack Honeywell Kl-525A HSI Garmin Gl-106A VOR/ILS/GPS Indicator Mid-Continent Instr MD41-1469 GPS Annun/Ctl Unit Garmin GA-56 GPS Antenna (2) 58-380112 Comm Antenna 36-380090 Comm Antenna 58-380114 Nav Antenna Speaker Microphone PS Engineering PMA7000B Audio Panel/Marker Beacon/Intercom Audio Panel/Receiver 101-384179 Marker Beacon Antenna BEECHCRAFT Baron 58 Serial No.: TH-2103 Equipment List - As Certificated (continued) Equipment Description Honeywell KT-76C Transponder System Transponder 100-384129 Antenna Honeywell RDR-2000VP Color Weather Radar Honeywell ART-2000 Sensor/Antenna Honeywell KMD 850 MFD and Rack Structure Installation BFG WX-500 Stormscope Weather Mapping System Processor with Mtg. Tray NY-163 Antenna Avionics Miscellaneous Avionics Master Switch Honeywell KEA-130A Encoding Altimeter Cabin Interphone System Shadin ADC 200+ Fuel/Airdata Computer Aft Fuselage Avionics Shelf Date: 11/23/2004 Weight (lb.) 4 Arm (in.) 228 94.3 ea. 15 44 97 See Below 8.5 53 6.5 53 3.9 54 1.4 56 0.5 57 0.5 89 0.8 135 0.8 53 1.5 277 1.0 88 1.0 70 1.5 55 0.8 198 Page 3 of 4 Section VI WT & Bal/Equipment Date: 11/23/2004 Weight (lb.) Arm (in.) 3.1 55 0.3 93 11.0 -28 6.4 54 3.0 -21 2.5 88 20 0.8 199 227 1.0 1.8 08530 11313 36 55 3.5 110 1.3 3.0 45 199 Page 4 of 4 Raytheon Aircraft Beech Hawker Air Model: 58 A/C Serial Number: TH-2103 Registration Number: N58YB EXTERIOR PAINT: Desoto White F17865 Sherwin Williams Regimental Brown A07784 Sherwin Williams Light Saddle Metallic R06166 INTERIOR PAINT: Castle Tan 9717-101 KEY NO. 2R190 STC'S This aircraft has the following STC's incorporated into the production of this unit at build: 1. SA00902WI 2. SA01033WI 3. SA5533NM Replacement of original landing gear doors Replacement of original landing gear doors Hartzell PHC-J3YF-2UF/FC7663 (B, K) -2R propellers & C-3567-1 (P) or C-3567-4 (P) spinners 4. SA00691WI-D Bendix/King KFC 225 3-Axis automatic flight control system AIRWORTHINESS CERTIFICATE I have inspected this aircraft and issued a STANDARD Airworthiness Certificate Dated 12-05-04. Time: 6.0 Landings: 10 Robert Alliband For Raytheon Aircraft Company DOA-230339-CE