Flight Manual. Thrust setti ng: The appropriate EPR thrust setting curve (EPR or PT 7), in the FAA Approved Airplane Flight Manual or AFM Appendices must be used for control of engine thrust. Airspeed limits: VMO/MMO - 390/0.9 (KEAS), Dual Mode 390/350/0.88 (KEAS) For other airspeed limits see the appropriate FAA approved Airplane Flight Manual. Every airplane flight manual, including Boeing 737 provides tables and/or graphs for V1 calculations on any given day. We will go through the example below. 1. Weight. Increasing weight increases V1. 2. Configuration. Increasing the flap angle decreases V1. 3. Field slope and wind. Downslopes reduce V1, upslopes increase V1. Boeing 737-800 Operating Manual 5 Boeing B737-800 Technical Specifications Dimensions Length 129 Ft 6 In Height 41 Ft 2 In Wingspan 117 Ft 7 In Without Winglets Wing Area 1,344 Sq. Ft Power plants Engine Type 2 ea. CFM 56—7B27 Maximum Thrust 27,300 Lbs./Engine Weights Empty Weight 91,300 Lbs. Max Zero Fuel Weight 130,180 Lbs. TCDS No.: EASA.IM.A.S.02479 Boeing 737 Page 6 of 7 Issue: 02 Date: 16 May 2012 IV Operating and Service Instructions 1. Flight Manual Supplement: IAI Flight Manual Supplement 365-00-00-B4014-EASA IAI Weight and Balance Supplement 365-08-00-B4052-XXXX 2. Mandatory Maintenance Instructions: April 29, 2013. National Airlines Flight 102, a Boeing 747-400 BCF (Boeing Converted Freighter), was a scheduled cargo flight from Bagram Air Base, Bagram, Afghanistan to Dubai, United Arab Emirates on April 29, 2013. During takeoff, the airplane immediately climbed steeply then descended in a manner consistent with an aerodynamic stall and Weight and balance records can be emailed or saved to the eFlite server for up to 30 days. eFlite Online™ helps synchronize operations that utilize multiple personnel during the flight planning process (i.e. data entry by passenger agents, baggage handlers and cabin and cockpit crew members). This manual is written in a different style from the “Quick Start Manual”, in order to simulate the actual operations manual. It is not intended to be “entertaining”; instead the writing is more technical and “formal” in nature. This is realistic to the actual Operations Manual for the 737, or for any aircraft. Boeing 737-800 (738) Boeing 737-800 (738) In-page Links. Seat Specifications, Go to Maximum weight for an assistive device carried in the cargo hold: 150 lb/sq ft The center of gravity (CG) of an aircraft is the point over which the aircraft would balance. [1] Its position is calculated after supporting the aircraft on at least two sets of weighing scales or load cells and noting the weight shown on each set of scales or load cells. The center of gravity affects the stability of the aircraft. For Training Purposes Only FRA US/T JG 01.03.01 Page 26 Lufthansa Technical Training DOCUMENTATION A319/A320/A321 FLIGHT OPERATIONS DOCUMENTATION 00-00 For Training Purposes Only Figure 14 Weight and Balance Manual FRA US/T JG 01.03.01 Page 27 Lufthansa Technical Training DOCUMENTATION A319/A320/A321 COMMONLY USED MAINTENANCE DOCUMENTATION 00 9mDqQL.