CODE 208 REVISION 8 – AUGUST 16, 2010 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 WEIGHT AND BALANCE MANUAL LIST OF EFFECTIVE PAGES LIST OF EFFECTIVE PAGES WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 ORIGINAL ................. 0.................. AUG 30, 2005 REVISION ................. 1................... JAN 16, 2006 REVISION ................. 2...................JUN 30, 2006 REVISION ................. 3...................SEP 14, 2006 REVISION ................. 4.................. OCT 25, 2007 REVISION ................. 5.................. APR 10, 2008 REVISION ................. 6.................. DEC 17, 2008 REVISION ................. 7.................. AUG 14, 2009 REVISION ................. 8.................. AUG 16, 2010 0-LEP REVISION 8 code 208 Page 1 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 LIST OF EFFECTIVE PAGES WEIGHT AND BALANCE MANUAL WB-1914 INTENTIONALLY BLANK 0-LEP Page 2 code 208 REVISION 8 WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 WEIGHT AND BALANCE MANUAL LIST OF EFFECTIVE PAGES Change REVISION 7 Applicability (model, engine, authority, other) 195 STD/LR/AR 1 REVISION 2 CC 01 01 2 REVISION 4 0-LOR 01 3 REVISION 5 0-LOR 01 4 0-LOR 01 5 0-LOR 01 6 0-LEP 208 1 0-LEP 208 2 0-LEP 208 3 0-LEP 208 4 1-00 01 1 REVISION 4 1-00 01 2 ORIGINAL Block 0-TITLE Code 208 Page cover 0-LOR 01 0-LOR * * * * * * * * REVISION 8 REVISION 8 REVISION 8 REVISION 8 REVISION 8 REVISION 8 1-00 02 1 REVISION 2 1-00 02 2 REVISION 2 1-05 01 1 1-05 01 2 1-05 02 1 1-05 02 2 1-10 01 1 REVISION 4 1-10 01 2 REVISION 4 1-10 02 1 REVISION 2 1-10 02 2 REVISION 2 1-20 01 1 REVISION 4 1-20 01 2 REVISION 4 1-20 01 3 REVISION 4 1-20 01 4 REVISION 4 1-20 02 1 REVISION 2 1-20 02 2 REVISION 2 1-20 02 3 REVISION 2 1-20 02 4 REVISION 2 1-30 01 1 REVISION 4 1-30 01 2 REVISION 4 ORIGINAL * EMBRAER 190 EMBRAER 195 EMBRAER 190/kg REVISION 8 REVISION 2 * CC 208 REVISION 8 EMBRAER 195/kg REVISION 8 EMBRAER 190/kg EMBRAER 195/kg EMBRAER 190/kg EMBRAER 195/kg EMBRAER 190/kg * Asterisk indicates pages revised, added or deleted by the current revision. 0-LEP REVISION 8 code 208 Page 3 WEIGHT AND BALANCE MANUAL Block 1-30 Code 01 Page 3 Change ORIGINAL 1-30 01 4 ORIGINAL 1-30 01 5 ORIGINAL 1-30 01 6 REVISION 4 1-30 02 1 REVISION 2 1-30 02 2 REVISION 2 1-30 02 3 REVISION 2 1-30 02 4 REVISION 2 1-30 02 5 REVISION 2 1-30 02 6 REVISION 2 1-35 01 1 REVISION 4 1-35 01 2 ORIGINAL 1-35 02 1 REVISION 4 1-35 02 2 REVISION 2 1-40 01 1 REVISION 4 1-40 01 2 1-40 02 1 1-40 02 2 * EMBRAER 195/kg EMBRAER 190/kg EMBRAER 195/kg EMBRAER 190/kg REVISION 8 REVISION 2 * Applicability (model, engine, authority, other) EMBRAER 195/kg REVISION 8 WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 LIST OF EFFECTIVE PAGES 0-LEP Page 4 code 208 REVISION 8 WEIGHT AND BALANCE MANUAL WEIGHT AND BALANCE DATA WEIGHT AND BALANCE TABLE OF CONTENTS Block Page Introduction..................................................................... 01-00 ........02 Weight and Center Of Gravity Limits .............................. 01-05 ........01 Moment/CG Changes (All EMBRAER 190 Models except EMBRAER 190 ECJ) ................................. 01-05 ........02 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 Balance Reference System (All EMBRAER 190 Models) 01-10 ........01 Balance Arms/Body Station ....................................... 01-10 ........01 Airplane Jacking (All EMBRAER 190 Models)................. 01-10 ........02 Jack Points Location .................................................. 01-10 ........02 Configuration Checklist/Equipment List (All EMBRAER 190 Models except EMBRAER 190 ECJ).......................... 01-20 ........01 Passenger Location ................................................... 01-20 ........01 Standard Configuration .............................................. 01-20 ........01 Flight Crew Items....................................................... 01-20 ........03 Fuel Data (All EMBRAER 190 Models except EMBRAER 190 ECJ) ................................................. 01-30 ........01 Fuel Quantities .......................................................... 01-30 ........01 Fuel Distribution Table............................................... 01-30 ........02 Miscellaneous Fluids (All EMBRAER 190 Models except EMBRAER 190 ECJ) ...................................... 01-30 ........06 Weighing Computation (All EMBRAER 190 Models except EMBRAER 190 ECJ) ...................................... 01-35 ........01 Baggage Loading (All EMBRAER 190 Models except EMBRAER 190 ECJ) ................................................. 01-40 ........01 Baggage Weight and Location ................................... 01-40 ........01 Carry-on Baggage...................................................... 01-40 ........01 Baggage Compartment .............................................. 01-40 ........01 WB-1914 Baggage Loading Procedures .................................... 01-40 ........02 ANAC APPROVED REVISION 4 1-00 code 01 Page 1 WEIGHT AND BALANCE DATA WEIGHT AND BALANCE MANUAL INTRODUCTION The Weight and Balance Manual provides instructions referring to the weighting and loading of the EMBRAER 190 airplane models. The instructions and data herein presented are approved by the airworthiness authority to comply with the applicable regulations. Based on the presented information, the operator can determine airplane weight and CG at any time of flight. 1-00 Page 2 code 01 CTA APPROVED ORIGINAL WBM-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 The basic empty weight value obtained during the airplane weighing procedures should be used as point of departure for each loading operation. WEIGHT AND BALANCE MANUAL WEIGHT AND BALANCE DATA WEIGHT AND BALANCE TABLE OF CONTENTS Block Page Introduction ........................................................................ 01-00........ 02 Weight and Center Of Gravity Limits ................................. 01-05........ 01 Moment/CG Changes (EMBRAER 195 Models).......... 01-05........ 02 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 Balance Reference System (EMBRAER 195 Models)...... 01-10........ 01 Balance Arms/Body Station.......................................... 01-10........ 01 Airplane Jacking (EMBRAER 195 Models) ....................... 01-10........ 02 Jack Points Location .................................................... 01-10........ 02 Configuration Checklist/Equipment List (EMBRAER 195 Models).............................................. 01-20........ 01 Passenger Location...................................................... 01-20........ 01 Standard Configuration (EMBRAER 195 Models) ....... 01-20........ 01 Flight Crew Items (EMBRAER 195 Models) ................ 01-20........ 03 Fuel Data (EMBRAER 195 Models) .................................. 01-30........ 01 Fuel Quantities ............................................................. 01-30........ 01 Fuel Distribution Table (EMBRAER 195 Models) ........ 01-30........ 02 Miscellaneous Fluids (EMBRAER 195 Models) ................ 01-30........ 05 Weighing Computation (EMBRAER 195 Models) ............. 01-35........ 01 Baggage Loading (EMBRAER 195 Models) ..................... 01-40........ 01 Baggage Weight and Location ..................................... 01-40........ 01 Carry-on Baggage ........................................................ 01-40........ 01 Baggage Compartment ................................................ 01-40........ 01 WB-1914 Baggage Loading Procedures...................................... 01-40........ 02 ANAC APPROVED REVISION 2 1-00 code 02 Page 1 WEIGHT AND BALANCE DATA WEIGHT AND BALANCE MANUAL INTRODUCTION The Weight and Balance Manual provides instructions referring to the weighting and loading of the EMBRAER 195 airplane models. The instructions and data herein presented are approved by the airworthiness authority to comply with the applicable regulations. Based on the presented information, the operator can determine airplane weight and CG at any time of flight. 1-00 Page 2 code 02 ANAC APPROVED REVISION 2 WBM-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 The basic empty weight value obtained during the airplane weighing procedures should be used as point of departure for each loading operation. WEIGHT AND BALANCE MANUAL WEIGHT AND BALANCE DATA WEIGHT AND CENTER OF GRAVITY LIMITS To comply with the performance and operating limitations of the regulations, the maximum allowable takeoff and landing operational weights may be equal to, but not greater than design limits. WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 Refer to AFM Section 2, Limitations, for further information. CTA APPROVED ORIGINAL 1-05 code 01 Page 1 WEIGHT AND BALANCE DATA WEIGHT AND BALANCE MANUAL MOMENT/CG CHANGES (ALL EMBRAER 190 MODELS EXCEPT EMBRAER 190 ECJ) When the landing gear is retracted, there is a moment reduction in respect to the airplane datum. − For 30000 kg: CG moves forward 0.4% of MAC (most critical case). DUE TO FUEL CONSUMPTION AND DENSITY VARIATION TEMPERATURE The fuel CG variation in relation to consumption is shown in the Fuel Distribution Table. The variation of fuel density with temperature has negligible effects in the airplane CG. 1-05 Page 2 code 01 ANAC APPROVED REVISION 8 WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 DUE TO LANDING GEAR CONFIGURATION WEIGHT AND BALANCE MANUAL WEIGHT AND BALANCE DATA WEIGHT AND CENTER OF GRAVITY LIMITS To comply with the performance and operating limitations of the regulations, the maximum allowable takeoff and landing operational weights may be equal to, but not greater than design limits. WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 Refer to AFM Section 2, Limitations, for further information. ANAC APPROVED REVISION 2 1-05 code 02 Page 1 WEIGHT AND BALANCE DATA WEIGHT AND BALANCE MANUAL MOMENT/CG CHANGES (EMBRAER 195 MODELS) DUE TO LANDING GEAR CONFIGURATION − For 34000 kg: CG moves forward 0.4% of MAC (most critical case). DUE TO FUEL CONSUMPTION AND DENSITY VARIATION TEMPERATURE The fuel CG variation in relation to consumption is shown in the Fuel Distribution Table. The variation of fuel density with temperature has negligible effects in the airplane CG. 1-05 Page 2 code 02 ANAC APPROVED REVISION 8 WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 When the landing gear is retracted, there is a moment reduction in respect to the airplane datum. WEIGHT AND BALANCE MANUAL WEIGHT AND BALANCE DATA BALANCE REFERENCE SYSTEM (ALL EMBRAER 190 MODELS) BALANCE ARMS/BODY STATION User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 Longitudinal location of the Centers of Gravity (CG) identified throughout this manual regarding airplane and components will be referred to as Balance Arms. Balance Arms are the distance in meters from Airplane Datum, which is located at the zero station of the fuselage. Balance Arms (BA) are equivalent to Body Station (BS) on the EMBRAER 190. AIRPLANE DATUM The Airplane Datum is a plane, perpendicular to the fuselage centerline, located at 14.443 m ahead of the wing stub’s front spar. For external reference, the Datum is located at 14.487 m ahead of the wing jack points. WING MEAN AERODYNAMIC CHORD (MAC) For the EMBRAER 190 models: MAC length = 3.682 m. Leading Edge MAC balance arm (LEMAC) = 15.896 m. Percentage of MAC is obtained using the following formula: % MAC = ( B. A. − 15.896) × 100 3.682 WB-1914 Where B.A. = Balance arm of airplane CG measured in meters. ANAC APPROVED REVISION 4 1-10 code 01 Page 1 WEIGHT AND BALANCE MANUAL WEIGHT AND BALANCE DATA AIRPLANE JACKING (ALL EMBRAER 190 MODELS) Refer to Chapter 7 of the Aircraft Maintenance Manual for airplane jacking procedures. BALANCE ARM CENTERLINE DISTANCE (meters) (meters) A 14.857 2.326 B 30.480 0 POINT NOTE: The jack points balance arms refer to the Airplane Datum. A CENTER LINE A B DATUM EM170AOM990003A.DGN JACK POINTS 1-10 Page 2 code 01 ANAC APPROVED REVISION 4 WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 JACK POINTS LOCATION WEIGHT AND BALANCE MANUAL WEIGHT AND BALANCE DATA BALANCE REFERENCE SYSTEM (EMBRAER 195 MODELS) BALANCE ARMS/BODY STATION User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 Longitudinal location of the Centers of Gravity (CG) identified throughout this manual regarding airplane and components will be referred to as Balance Arms. Balance Arms are the distance in meters from Airplane Datum, which is located at the zero station of the fuselage. Balance Arms (BA) are equivalent to Body Station (BS) on the EMBRAER 195. AIRPLANE DATUM The Airplane Datum is a plane, perpendicular to the fuselage centerline, located at 15.256 m ahead of the wing stub’s front spar. For external reference, the Datum is located at 15.670 m ahead of the wing jack points. WING MEAN AERODYNAMIC CHORD (MAC) For the EMBRAER 195 models: MAC length = 3.682 m. Leading Edge MAC balance arm (LEMAC) = 16.708 m. Percentage of MAC is obtained using the following formula: % MAC = ( B. A. − 16.708) × 100 3.682 WB-1914 Where B.A. = Balance arm of airplane CG measured in meters. ANAC APPROVED REVISION 2 1-10 code 02 Page 1 WEIGHT AND BALANCE DATA WEIGHT AND BALANCE MANUAL AIRPLANE JACKING (EMBRAER 195 MODELS) Refer to Chapter 7 of the Aircraft Maintenance Manual for airplane jacking procedures. JACK POINTS LOCATION BALANCE ARM CENTERLINE DISTANCE (meters) (meters) A 15.670 2.326 B 32.893 0 NOTE: The jack points balance arms refer to the Airplane Datum. A CENTER LINE A B DATUM EM170AOM990011A.DGN JACK POINTS 1-10 Page 2 code 02 ANAC APPROVED REVISION 2 WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 POINT WEIGHT AND BALANCE MANUAL WEIGHT AND BALANCE DATA CONFIGURATION CHECKLIST/EQUIPMENT LIST (ALL EMBRAER 190 MODELS EXCEPT EMBRAER 190 ECJ) PASSENGER LOCATION User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 The passenger location and respective balance arm are shown in the applicable Interior arrangement. Herein, the Standard Configuration is presented as an illustrative example, including the plan view and the Balance Arms. For other interior configuration options, the passenger locations and the respective Balance Arms are supplied together with the “Airplane Weighing Form”, inserted in the “FINAL INSPECTION REPORT”, by the time of the airplane’s delivery. WB-1914 STANDARD CONFIGURATION SEATS ROW PASSENGER SEATS BALANCE ARM (m) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 1, 2 3, 4, 5, 6 7, 8, 9, 10 11, 12, 13, 14 15, 16, 17, 18 19, 20, 21, 22 23, 24, 25, 26 27, 28, 29, 30 31, 32, 33, 34 35, 36, 37, 38 39, 40, 41, 42 43, 44, 45, 46 47, 48, 49, 50 51, 52, 53, 54 55, 56, 57, 58 59, 60, 61, 62 63, 64, 65, 66 6.690 7.503 8.316 9.128 9.941 10.754 11.567 12.380 13.192 14.005 14.818 16.304 17.116 17.929 18.742 19.555 20.368 ANAC APPROVED REVISION 4 1-20 code 01 Page 1 WEIGHT AND BALANCE MANUAL SEATS ROW PASSENGER SEATS BALANCE ARM (m) 18 19 20 21 22 23 24 25 67, 68, 69, 70 71, 72, 73, 74 75, 76, 77, 78 79, 80, 81, 82 83, 84, 85, 86 87, 88, 89, 90 91, 92, 93, 94 95, 96, 97, 98 21.180 21.993 22.806 23.619 24.432 25.244 26.057 26.870 NOTE: Pax Balance Arm = Seat Balance Arm – 0.155 m. Balance Arm (m) FWD Galley (G1) 3.970 FWD Lavatory 4.220 FWD Flight Attendant 4.940 FWD Galley (G2) 5.437 Wardrobe 6.147 st 28.187 2 Aft Flight Attendant (*) nd 27.679 AFT Galley (G3) 28.947 AFT Lavatory 28.947 1 Aft Flight Attendant (*) Optional FWD BAGGAGE COMPARTMENT CAPACITY: 1850 kg. AFT BAGGAGE COMPARTMENT CAPACITY: 1650 kg. 1-20 Page 2 code 01 ANAC APPROVED REVISION 4 WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 WEIGHT AND BALANCE DATA WEIGHT AND BALANCE MANUAL WEIGHT AND BALANCE DATA FLIGHT CREW ITEMS WEIGHT BALANCE ARM (kg) (m) 87 2.810 87 2.810 87 3.500 ** 4.940 ** 28.187 ** 82 27.679 CREW BAGGAGE (Wardrobe) 15 6.147 NAVIGATION KIT 10 3.200 ITEM CAPTAIN * FIRST OFFICER User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 OBSERVER * * FWD ATTENDANT * 82 st * nd * 1 AFT ATTENDANT 2 AFT ATTENDANT 82 (*) Occupant Balance Arm. (**) 82 kg stands for standard average male weights. For female standard average weights refer to 73 kg. NOTE: - The adopted flight crew items are in accordance with the approved average weight, not including the respective carryon baggage. nd WB-1914 - 2 Aft Attendant seat is optional. Check the airplane actual internal configuration. ANAC APPROVED REVISION 4 1-20 code 01 Page 3 WEIGHT AND BALANCE MANUAL User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 WEIGHT AND BALANCE DATA A: Wardrobe B: Fwd Galley G2 C: Fwd Galley G1 (Stowage) D: Fwd Lavatory E: Fwd Attendant Seat st F: 1 Fwd Attendant Seat G: Aft Lavatory H: Aft Galley G3 nd I: 2 Fwd Attendant Seat (Optional) 1-20 Page 4 code 01 ANAC APPROVED REVISION 4 WB-1914 STANDARD CONFIGURATION (ALL EMBRAER 190 MODELS EXCEPT EMBRAER 190 ECJ) WEIGHT AND BALANCE MANUAL WEIGHT AND BALANCE DATA CONFIGURATION CHECKLIST/EQUIPMENT LIST (EMBRAER 195 MODELS) PASSENGER LOCATION User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 The passenger location and respective balance arm are shown in the applicable Interior arrangement. Herein, the Standard Configuration is presented as an illustrative example, including the plan view and the Balance Arms. For other interior configuration options, the passenger locations and the respective Balance Arms are supplied together with the “Airplane Weighing Form”, inserted in the “FINAL INSPECTION REPORT”, by the time of the airplane’s delivery. WB-1914 STANDARD CONFIGURATION (EMBRAER 195 MODELS) SEATS ROW PASSENGER SEATS BALANCE ARM (m) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 1, 2 ,3, 4 5, 6, 7, 8 9, 10, 11, 12 13, 14, 15, 16 17, 18, 19, 20 21, 22, 23, 24 25, 26, 27, 28 29, 30, 31, 32 33, 34, 35, 36 37, 38, 39, 40 41, 42, 43, 44 45, 46, 47, 48 49, 50, 51, 52 53, 54, 55, 56 57, 58, 59, 60 61, 62, 63, 64 65, 66, 67, 68 69, 70, 71, 72 73, 74, 75, 76 7.501 8.314 9.127 9.939 10.752 11.565 12.378 13.191 14.003 14.816 15.629 17.042 17.855 18.668 19.480 20.293 21.106 21.919 22.732 ANAC APPROVED REVISION 2 1-20 code 02 Page 1 WEIGHT AND BALANCE MANUAL SEATS ROW PASSENGER SEATS BALANCE ARM (m) 20 21 22 23 24 25 26 27 77, 78, 79, 80 81, 82, 83, 84 85, 86, 87, 88 89, 90, 91, 92 93, 94, 95, 96 97, 98, 99, 100 101, 102, 103, 104 105, 106, 107, 108 23.544 24.357 25.170 25.983 26.796 27.608 28.421 29.234 NOTE: Pax Balance Arm = Seat Balance Arm – 0.155 m. Balance Arm (m) FWD Galley (G1) 3.970 FWD Lavatory 4.220 FWD Flight Attendant 4.940 FWD Galley (G2) 5.437 Wardrobe 6.147 st 30.600 2 Aft Flight Attendant (*) nd 30.092 AFT Galley (G3) 31.360 AFT Lavatory 31.670 1 Aft Flight Attendant (*) Optional FWD BAGGAGE COMPARTMENT CAPACITY: 1900 kg. AFT BAGGAGE COMPARTMENT CAPACITY: 1800 kg. 1-20 Page 2 code 02 ANAC APPROVED REVISION 2 WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 WEIGHT AND BALANCE DATA WEIGHT AND BALANCE MANUAL WEIGHT AND BALANCE DATA FLIGHT CREW ITEMS (EMBRAER 195 MODELS) WEIGHT BALANCE ARM (kg) (m) 87 2.810 87 2.810 87 3.500 82 ** 4.940 82 ** 30.600 82 ** 30.092 CREW BAGGAGE (Wardrobe) 15 6.147 NAVIGATION KIT 10 3.520 ITEM CAPTAIN * FIRST OFFICER * OBSERVER * User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 FWD ATTENDANT * st * nd * 1 AFT ATTENDANT 2 AFT ATTENDANT (*) Occupant Balance Arm. (**) 82 kg stands for standard average male weights. For female standard average weights refer to 73 kg. NOTE: - The adopted flight crew items are in accordance with the approved average weight, not including the respective carry-on baggage. WB-1914 - 2nd Aft Attendant seat is optional. Check the airplane actual internal configuration. ANAC APPROVED REVISION 2 1-20 code 02 Page 3 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 WEIGHT AND BALANCE DATA WEIGHT AND BALANCE MANUAL I H J G A: Wardrobe B: Fwd Galley G2 C: Fwd Galley G1 D: Fwd Lavatory E: Fwd Attendant Seat F: Wardrobe G: 1st Aft Attendant Seat H: Aft Lavatory I: Aft Galley G3 J: 2nd Aft Flight Attendant Seat (Optional) F A E D C EM170AOM990012A.DGN B 1-20 Page 4 code 02 ANAC APPROVED REVISION 2 WB-1914 STANDARD CONFIGURATION (EMBRAER 195 MODELS) WEIGHT AND BALANCE MANUAL WEIGHT AND BALANCE DATA FUEL DATA (ALL EMBRAER 190 MODELS EXCEPT EMBRAER 190 ECJ) FUEL QUANTITIES VOLUME (liters) WEIGHT (kg) CG BALANCE ARM (m) UNUSABLE UNDRAINABLE 15.4 12.5 16.314 UNUSABLE DRAINABLE 98.0 79.5 16.554 TOTAL UNUSABLE 113.4 92.0 16.521 USABLE 16153 13100 16.378 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 FUEL CATEGORY WB-1914 NOTE: The values specified above have been determined for an adopted fuel density of 0.811 kg/l. ANAC APPROVED REVISION 4 1-30 code 01 Page 1 WEIGHT AND BALANCE MANUAL WEIGHT AND BALANCE DATA FUEL DISTRIBUTION TABLE VOLUME (liters) CG BALANCE ARM (meters) 200 16.119 400 16.023 600 15.962 800 15.917 1000 15.883 1200 15.855 1400 15.834 1600 15.820 1800 15.808 2000 15.800 2200 15.795 2400 15.790 2600 15.787 2800 15.785 3000 15.784 3200 15.784 3400 15.783 3600 15.784 3800 15.785 4000 15.786 1-30 Page 2 code 01 ANAC APPROVED REVISION 4 WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 FUEL DISTRIBUTION ON THE LEFT AND RIGHT WING TANKS WEIGHT AND BALANCE DATA WEIGHT AND BALANCE MANUAL WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 FUEL DISTRIBUTION ON THE LEFT AND RIGHT WING TANKS VOLUME (liters) CG BALANCE ARM (meters) 4200 15.788 4400 15.789 4600 15.791 4800 15.793 5000 15.796 5200 15.798 5400 15.801 5600 15.804 5800 15.807 6000 15.810 6200 15.813 6400 15.816 6600 15.820 6800 15.823 7000 15.826 7200 15.829 7400 15.833 7600 15.836 7800 15.840 8000 15.844 8200 15.847 8400 15.851 CTA APPROVED ORIGINAL 1-30 code 01 Page 3 WEIGHT AND BALANCE DATA WEIGHT AND BALANCE MANUAL VOLUME (liters) CG BALANCE ARM (meters) 8600 15.855 8800 15.858 9000 15.862 9200 15.866 9400 15.870 9600 15.874 9800 15.878 10000 15.882 10200 15.886 10400 15.890 10600 15.895 10800 15.900 11000 15.905 11200 15.910 11400 15.916 11600 15.924 11800 15.935 12000 15.947 12200 15.960 12400 15.974 12600 15.988 12800 16.004 13000 16.021 1-30 Page 4 code 01 CTA APPROVED ORIGINAL WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 FUEL DISTRIBUTION ON THE LEFT AND RIGHT WING TANKS WEIGHT AND BALANCE MANUAL WEIGHT AND BALANCE DATA WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 FUEL DISTRIBUTION ON THE LEFT AND RIGHT WING TANKS VOLUME (liters) CG BALANCE ARM (meters) 13200 16.038 13400 16.056 13600 16.075 13800 16.095 14000 16.115 14200 16.137 14400 16.160 14600 16.183 14800 16.207 15000 16.232 15200 16.258 15400 16.285 15600 16.314 15800 16.343 16000 16.373 16153 16.378 CTA APPROVED ORIGINAL 1-30 code 01 Page 5 WEIGHT AND BALANCE MANUAL WEIGHT AND BALANCE DATA MISCELLANEOUS FLUIDS (ALL EMBRAER 190 MODELS EXCEPT EMBRAER 190 ECJ) WEIGHT (kg) BALANCE ARM (m) ENGINE OIL (1) 32 14.002 APU OIL (1) 3.7 34.304 HYDRAULIC (2) 54 16.709 8 29.632 110 28.437 WASTE TANK FLUID POTABLE WATER (3) NOTE: (1) Adopted engine oil Density (ref. MIL-L-7808): 0.98 kg/l. Engine oil considers oil from engine, integrated driven generator (IDG), oil lines and starter. (2) Adopted hydraulic fluid density (ref. SAE AS 1241A TYPE IV): 0.99 kg/l. (3) Potable water is stored in a potable water tank. Tank capacity may vary between 35, 70, 90 and 110 liters. 1-30 Page 6 code 01 ANAC APPROVED REVISION 4 WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 FLUID WEIGHT AND BALANCE DATA WEIGHT AND BALANCE MANUAL FUEL DATA (EMBRAER 195 MODELS) FUEL QUANTITIES EMBRAER 195 STD/LR/AR MODELS VOLUME (liters) WEIGHT (kg) CG BALANCE ARM (m) UNUSABLE UNDRAINABLE 15.4 12.5 17.127 UNUSABLE DRAINABLE 98.0 79.5 17.367 TOTAL UNUSABLE 113.4 92.0 17.334 USABLE 16153.0 13100.0 17.191 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 FUEL CATEGORY WB-1914 NOTE: The values specified above have been determined for an adopted fuel density of 0.811 kg/l. ANAC APPROVED REVISION 2 1-30 code 02 Page 1 WEIGHT AND BALANCE DATA WEIGHT AND BALANCE MANUAL FUEL DISTRIBUTION TABLE (EMBRAER 195 MODELS) EMBRAER 195 STD/LR/AR MODELS VOLUME (liters) CG BALANCE ARM (meters) 200 16.933 400 16.837 600 16.775 800 16.731 1000 16.696 1200 16.669 1400 16.648 1600 16.633 1800 16.622 2000 16.614 2200 16.608 2400 16.603 2600 16.601 2800 16.598 3000 16.597 3200 16.596 3400 16.596 3600 16.597 3800 16.597 4000 16.598 1-30 Page 2 code 02 ANAC APPROVED REVISION 2 WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 FUEL DISTRIBUTION ON THE LEFT AND RIGHT WING TANKS WEIGHT AND BALANCE DATA WEIGHT AND BALANCE MANUAL WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 FUEL DISTRIBUTION ON THE LEFT AND RIGHT WING TANKS VOLUME (liters) CG BALANCE ARM (meters) 4200 16.600 4400 16.602 4600 16.603 4800 16.606 5000 16.608 5200 16.611 5400 16.613 5600 16.616 5800 16.619 6000 16.622 6200 16.625 6400 16.628 6600 16.631 6800 16.635 7000 16.638 7200 16.642 7400 16.645 7600 16.649 7800 16.652 8000 16.656 8200 16.659 8400 16.663 ANAC APPROVED REVISION 2 1-30 code 02 Page 3 WEIGHT AND BALANCE DATA WEIGHT AND BALANCE MANUAL VOLUME (liters) CG BALANCE ARM (meters) 8600 16.666 8800 16.670 9000 16.674 9200 16.678 9400 16.681 9600 16.685 9800 16.689 10000 16.693 10200 16.697 10400 16.701 10600 16.706 10800 16.710 11000 16.715 11200 16.721 11400 16.726 11600 16.733 11800 16.743 12000 16.754 12200 16.767 12400 16.780 12600 16.794 12800 16.809 13000 16.825 1-30 Page 4 code 02 ANAC APPROVED REVISION 2 WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 FUEL DISTRIBUTION ON THE LEFT AND RIGHT WING TANKS WEIGHT AND BALANCE DATA WEIGHT AND BALANCE MANUAL WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 FUEL DISTRIBUTION ON THE LEFT AND RIGHT WING TANKS VOLUME (liters) CG BALANCE ARM (meters) 13200 16.842 13400 16.859 13600 16.878 13800 16.897 14000 16.917 14200 16.938 14400 16.960 14600 16.982 14800 17.006 15000 17.030 15200 17.055 15400 17.082 15600 17.109 15800 17.138 16000 17.168 16153 17.191 ANAC APPROVED REVISION 2 1-30 code 02 Page 5 WEIGHT AND BALANCE DATA WEIGHT AND BALANCE MANUAL MISCELLANEOUS MODELS) FLUIDS (EMBRAER 195 EMBRAER 195 STD/LR/AR MODELS WEIGHT (kg) BALANCE ARM (m) ENGINE OIL (1) 32 14.815 APU OIL (1) 3.7 34.717 HYDRAULIC (2) 56 17.522 8 32.045 110 5.168 WASTE TANK FLUID POTABLE WATER (3) NOTE: (1) Adopted engine oil Density (ref. MIL-L-7808): 0.98 kg/l. Engine oil considers oil from engine, integrated driven generator (IDG), oil lines and starter. (2) Adopted hydraulic fluid density (ref. SAE AS 1241A TYPE IV): 0.99 kg/l. (3) Potable water is stored in a potable water tank. Tank capacity may vary between 35, 70, 90 and 110 liters. 1-30 Page 6 code 02 ANAC APPROVED REVISION 2 WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 FLUID WEIGHT AND BALANCE MANUAL WEIGHT AND BALANCE DATA WEIGHING COMPUTATION (ALL EMBRAER 190 MODELS EXCEPT EMBRAER 190 ECJ) User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 The OEW (Operational Empty Weight) is the BEW (Basic Empty Weight) plus the weight of operational items (crew, catering, lavatory fluid, etc.). The OEI (Operational Empty Index) is the index for the OEW. In order to determine the OEW and OEI, it is necessary to add to the BEW all the weight and moment variations referent to the operational items. The BEW is obtained from the aircraft weighting record. Example: Computation of OEW/OEI for the EMBRAER 190. For a BEW equal to 26118.10 kg and BEW moment equal to 437791.592 kg.m: Weight (kg) Arm (m) Moment (kg.m) 26118.10 16.762 437791.592 Captain and First Officer 174.00 2.810 488.940 Fwd flight attendant 82.00 4.940 405.080 82.00 28.187 2311.334 2 Aft flight attendant 82.00 27.679 2269.678 Waste Tank Fluid 8.00 29.632 237.056 Potable Water 110.00 28.437 3128.070 Navigation kit 10.00 3.520 35.200 Crew baggage 15.00 6.147 92.205 Catering galley G1 30.00 3.970 119.100 Catering galley G2 162.00 5.437 880.794 Catering galley G3 280.00 28.947 8105.160 27153.10 16.789 455864.21 Item BEW st 1 Aft flight attendant nd OEW WB-1914 NOTE: - BEW computation considers APU oil, engine oil, hydraulic fluid and unusable fuel. - Potable water is stored in a potable water tank. Tank capacity may vary between 35, 70, 90 and 110 liters. The OEW calculated in this example takes into account potable water tank’s maximum capacity. ANAC APPROVED REVISION 4 1-35 code 01 Page 1 WEIGHT AND BALANCE DATA WEIGHT AND BALANCE MANUAL 1-35 Page 2 code 01 ANAC APPROVED ORIGINAL WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 - Catering weight was considered above, but its weight is not constant. Use the airplane actual internal configuration for galleys location. - 2nd Aft Attendant seat is optional. Check the airplane actual internal configuration. - The values above are an example. Use the airplane actual BEW for determining the OEW. WEIGHT AND BALANCE MANUAL WEIGHT AND BALANCE DATA WEIGHING COMPUTATION (EMBRAER 195 MODELS) User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 The OEW (Operational Empty Weight) is the BEW (Basic Empty Weight) plus the weight of operational items (crew, catering, lavatory fluid, etc.). The OEI (Operational Empty Index) is the index for the OEW. In order to determine the OEW and OEI, it is necessary to add to the BEW all the weight and moment variations referent to the operational items. The BEW is obtained from the aircraft weighting record. Example: Computation of OEW/OEI for the EMBRAER 195. For a BEW equal to 27800.40 kg and BEW moment equal to 494541.316 kg.m: Weight (kg) Arm (m) Moment (kg.m) 27800.40 17.789 494541.316 Captain and First Officer 174.00 2.810 488.940 Fwd flight attendant Item BEW 82.00 4.940 405.080 st 82.00 30.600 2509.200 nd 2 Aft flight attendant 82.00 30.092 2467.544 Waste Tank Fluid 8.00 32.045 256.360 Potable Water 110.00 5.168 568.48 Navigation kit 10.00 3.520 35.200 Crew baggage 15.00 6.147 92.205 Catering galley G1 30.00 3.970 119.100 Catering galley G2 162.00 5.437 880.794 Catering galley G3 280.00 31.160 8724.800 28835.40 17.724 511089.019 1 Aft flight attendant OEW WB-1914 NOTE: - BEW computation considers APU oil, engine oil, hydraulic fluid and unusable fuel. - Potable water is stored in a potable water tank. Tank capacity may vary between 35, 70, 90 and 110 liters. The OEW calculated in this example takes into account potable water tank’s maximum capacity. ANAC APPROVED REVISION 4 1-35 code 02 Page 1 WEIGHT AND BALANCE DATA WEIGHT AND BALANCE MANUAL 1-35 Page 2 code 02 ANAC APPROVED REVISION 2 WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 - Catering weight was considered above, but its weight is not constant. Use the airplane actual internal configuration for galleys location. - 2nd Aft Attendant seat is optional. Check the airplane actual internal configuration. - The values above are an example. Use the airplane actual BEW for determining the OEW. WEIGHT AND BALANCE MANUAL WEIGHT AND BALANCE DATA BAGGAGE LOADING (ALL EMBRAER 190 MODELS EXCEPT EMBRAER 190 ECJ) BAGGAGE WEIGHT AND LOCATION User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 The baggage weight limits, location and the respective balance arm may be obtained from the applicable interior arrangement. The data shown enclosed are applicable to the airplane’s Standard Configuration. For other interior configuration options, the weight limits, location and the respective balance arm are supplied together with the “Airplane Weighing Form”, inserted in the “FINAL INSPECTION REPORT”. CARRY-ON BAGGAGE Carry-on volumes may be stowed in the overhead bins and in the wardrobe closet. There is no specific requirement for underseat carryon volumes; however a maximum of 9.0 kg is allowable, provided the volume is properly restrained to avoid sliding. BAGGAGE COMPARTMENT Whenever possible, baggage should be distributed between both compartments, taking into account CG position. The baggage should be evenly distributed in each compartment to avoid load concentration. Baggage/Cargo must not become a hazard to the airplane structure or systems as a result of shifting under operational loads. Therefore, sharp edge volumes (like wooden or metal containers) and/or dense cargo (objects significantly more dense than typical passenger baggage) must be arranged with adjacent soft volumes or protections thus preventing aircraft damage in case of baggage/cargo shifting due to operational loads. WB-1914 The use of vertical cargo nets is not required. In case of total or partial use of vertical nets in the forward or aft cargo compartments, maximum cargo compartment section weights must be observed. These weights must be observed even when the vertical cargo nets are not installed. ANAC APPROVED REVISION 4 1-40 code 01 Page 1 WEIGHT AND BALANCE DATA WEIGHT AND BALANCE MANUAL BAGGAGE LOADING PROCEDURES The aft tipping limit is at 56.0% CG, which corresponds to the CG of the main landing gear wheel axle position measured from airplane datum. From CG positions greater than this, tipping is expected. Baggage loading and unloading procedures must be established for each Customer Configuration in order to maintain the airplane CG within the recommended static margin. 1-40 Page 2 code 01 ANAC APPROVED REVISION 8 WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 The minimum recommended static margin (difference between the aft tipping limit and the airplane CG) is 5%. WEIGHT AND BALANCE MANUAL BAGGAGE MODELS) LOADING WEIGHT AND BALANCE DATA (EMBRAER 195 BAGGAGE WEIGHT AND LOCATION User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 The baggage weight limits, location and the respective balance arm may be obtained from the applicable interior arrangement. The data shown enclosed are applicable to the airplane’s Standard Configuration. For other interior configuration options, the weight limits, location and the respective balance arm are supplied together with the “Airplane Weighing Form”, inserted in the “FINAL INSPECTION REPORT”. CARRY-ON BAGGAGE Carry-on volumes may be stowed in the overhead bins and in the wardrobe closet. There is no specific requirement for underseat carryon volumes; however a maximum of 9.0 kg is allowable, provided the volume is properly restrained to avoid sliding. BAGGAGE COMPARTMENT Whenever possible, baggage should be distributed between both compartments, taking into account CG position. The baggage should be evenly distributed in each compartment to avoid load concentration. WB-1914 Baggage/Cargo must not become a hazard to the airplane structure or systems as a result of shifting under operational loads. Therefore, sharp edge volumes (like wooden or metal containers) and/or dense cargo (objects significantly more dense than typical passenger baggage) must be arranged with adjacent soft volumes or protections thus preventing aircraft damage in case of baggage/cargo shifting due to operational loads. ANAC APPROVED REVISION 2 1-40 code 02 Page 1 WEIGHT AND BALANCE DATA WEIGHT AND BALANCE MANUAL BAGGAGE LOADING PROCEDURES The aft tipping limit is at 56.0% CG, which corresponds to the CG of the main landing gear wheel axle position measured from airplane datum. From CG positions greater than this, tipping is expected. Baggage loading and unloading procedures must be established for each Customer Configuration in order to maintain the airplane CG within the recommended static margin. If no procedures are adopted to ensure loading of the airplane within these limits, to avoid airplane tail down it is recommended that the forward baggage compartment be always loaded before the aft baggage compartment. If no procedures are adopted to ensure unloading of the airplane within these limits, to avoid airplane tail down it is recommended that the aft baggage compartment be always unloaded before the forward baggage compartment. 1-40 Page 2 code 02 ANAC APPROVED REVISION 8 WB-1914 User: okhaled0f - Printed By myTechCare - Dec 04/22 - 07:43:30 The minimum recommended static margin (difference between the aft tipping limit and the airplane CG) is 5%.
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