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Author: r | 2025-04-24

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When changing lanes. Leaving the turn signal on may cause others to misunderstand your intended Right turn “” Set the switch to the “” side to make the direction of travel, and cause crashes. Page 128 ENGINE STOP SWITCH / ELECTRIC STARTER SWITCH  Changing the engine stop switch from Engine Stop Switch     Stop the engine immediately in emergency or from while rid- situations such as a fall. Placing the engine ing may damage to the engine or the cat- stop switch in the “”... Page 129 Electric Starter Switch “” HAZARD WARNING SWITCH “” Pressing the electric starter switch causes The hazard warning switch is used in emer- the starter motor to turn over and starts the gency situations, such as when a malfunc- engine. tion has occurred. Moving the switch to the For details, see “STARTING THE ENGINE”... Page 130 2. Check that the engine stop switch is set to “”. 3. Set the ignition switch to ON. NOTE: This motorcycle features the Suzuki 4. Check that the malfunction indicator light Easy Start System, allowing you to start the has gone out. Page 131 Do not push and hold the electric starter switch for 5 seconds or more or use the Suzuki Easy Start System to turn the starter motor over continuously. 2-91... Page 132 If they are not providing the indications described below, have your motorcycle inspected If you hold the electric starter switch promptly by a Suzuki dealer. down while the malfunction indicator is • When the gear position indicator lit, the battery may run down. Page 133 You can start the engine with a single push battery, the engine might not start easily by of the electric starter switch. The starter Suzuki Easy Start System. If the engine is motor continues to turn over after you take difficult to start, squeeze the clutch lever... Page 134 Proper Warm up In the following circumstances, allow suffi- cient idling time to warm it up before riding. • When you have not used the motorcycle Leaving the engine running for an for an extended period extended period without riding, in order •... Page 135 SIDE STAND / IGNITION INTERLOCK  WARNING SYSTEM The motorcycle has a system to prevent rid- ers from forgetting to retract the side stand If you move the side stand down while and then traveling with it down. riding the

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ELECTRIC SYSTEM RS125 7.1.2. IGNITION SYSTEM TROUBLESHOOTING • Check the condition of the 7.5 A and 20 A fuses. NOTE For instructions on how to test electric components, see (ELECTRIC PARTS TROUBLESHOOTING CHART). • Check the spark plug and replace as required. •... Page 186: Charging System And Main Power Supply ELECTRIC SYSTEM RS125 7.1.3. CHARGING SYSTEM AND MAIN POWER SUPPLY Charging system test • Start the engine and rev it up to 6000 rpm. • Connect a tester placed into voltmeter mode across battery terminals. • Turn on the low beam. •... Page 187 ELECTRIC SYSTEM RS125 Test data Flywheel test • Disconnect the alternator wiring connector. • Start the engine and rev it up to 5000 rpm. • Use the hand-held tester to measure voltage (VAC) across the three yellow wires. A reading lower than 53 V indicates a faulty alternator. Page 188: Starter Circuit ELECTRIC SYSTEM RS125 7.1.4. STARTER CIRCUIT TROUBLESHOOTING NOTE For instructions on how to test electric components, see (ELECTRIC PARTS TROUBLESHOOTING CHART). • Check the condition of the fuses. • Check the starter button. • Check the starter relay. • Check the starter motor. •... Page 189: Stoplight Circuit ELECTRIC SYSTEM RS125 7.1.5. STOPLIGHT CIRCUIT Key: Front brake switch Rear brake switch Fuse (15 A) Fuse (20 A) Battery Tail light Stoplights NOTE For instructions on how to test electric components, see (ELECTRIC PARTS TROUBLESHOOTING CHART). TROUBLESHOOTING • Check the condition of the 15-A and 20-A fuses. •... Page 190 ELECTRIC SYSTEM RS125 Switches

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192: Failures In Hydraulic System Abnormal Operating DA 42 AFM Procedures 4B.6 FAILURES IN HYDRAULIC SYSTEM 4B.6.1 CONTINUOUS HYDRAULIC PUMP OPERATION 1. Landing gear indication lights ... . check 2. Prepare for manual landing gear extension. Refer to Section 3.6.2 - MANUAL EXTENSION OF THE LANDING GEAR. Page 193: Starting Engine With External Power Abnormal Operating DA 42 AFM Procedures 4B.7 STARTING ENGINE WITH EXTERNAL POWER 4B.7.1 BEFORE STARTING ENGINE 1. Pre-flight inspection ....complete 2. Passengers ......instructed... Page 194 Abnormal Operating DA 42 AFM Procedures CAUTION When switching the External Power Unit ON, the electrically driven hydraulic gear pump may activate itself for 5 to 20 seconds in order to restore the system pressure. Should the pump continue to operate continuously or periodically, terminate flight. Page 195: 7.2 Starting Engine Abnormal Operating DA 42 AFM Procedures 4B.7.2 STARTING ENGINE 1. Strobe lights (ACL) ....ON 2. ELECT. MASTER ..... ON 3. Page 196 Abnormal Operating DA 42 AFM Procedures CAUTION Do not overheat the starter motor. Do not operate the starter motor for more than 10 seconds. After operating the starter motor, let it cool off for 20 seconds. After 6 attempts to start the engine, let the starter cool off for half an hour. Page 197: Landing With High Landing Mass Abnormal Operating DA 42 AFM Procedures 4B.8 LANDING WITH HIGH LANDING MASS CAUTION Damage of the landing gear can result from a hard landing with a flight mass above the maximum landing mass. NOTE If MÄM 42-088 is carried out, a landing with a mass between 1700 kg (3748 lb) and 1785 kg (3935 lb) is admissible. Page 198 Abnormal Operating DA 42 AFM Procedures Intentionally left blank. Page 4B - 34 Rev. 4 30-Nov-2005 Doc. No. 7.01.05-E... Page 199 DA 42 AFM Performance CHAPTER 5 PERFORMANCE Page INTRODUCTION ........5-2 USE OF THE PERFORMANCE TABLES AND DIAGRAMS . Page 200: Introduction Performance DA 42 AFM 5.1 INTRODUCTION The performance tables and diagrams on the following pages are presented so that, on the one hand, you can see what performance you can expect from your airplane, while on the other they allow comprehensive and sufficiently accurate flight planning. The values... Page 201: Performance Tables And Diagrams DA 42 AFM Performance 5.3 PERFORMANCE TABLES AND DIAGRAMS 5.3.1 AIRSPEED CALIBRATION NOTE The position of the landing gear (extended/retracted) has no influence on the airspeed indicator system. Doc. No. 7.01.05-E Rev. 4 30-Nov-2005 Page 5 - 3... Page 202 Performance DA 42 AFM Page 5 - 4 Rev. 4 30-Nov-2005 Doc. No. 7.01.05-E... Page 203 DA 42 AFM Performance Doc. No. 7.01.05-E Rev. 4 30-Nov-2005 Page 5 - 5... Page 204: Fuel Flow Diagram Performance DA 42 AFM 5.3.2 FUEL FLOW DIAGRAM CAUTION. Brother HL-L3270CDW,Starter Black Toner Cartridge (1,000 pages)^Starter Cyan Toner Cartridge (1,000 pages)^Starter Yellow Toner Cartridge (1,000 pages)^Starter Magenta Hide sub-pages of Application Starters Application Starters. Show sub-pages of Bakery App Starter Bakery App Starter. Overview. Running, building and packaging. Using an

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This article is in the Product Showcase section for our sponsors at CodeProject. These articles are intended to provide you with information on products and services that we consider useful and of value to developers. This is a showcase review for our sponsors at CodeProject. These reviews are intended to provide you with information on products and services that we consider useful and of value to developers. Download the Corporate Site Starter Kit for ASP.NET 2.0 ASP.NET 2.0 and Visual Studio 2005 make web site development dramatically easier. If you combine their power with a flexible content management system, you get an incredible set of tools for creating professional web sites. The Corporate Site Starter Kit uses Kentico CMS for ASP.NET, an open content management solution for .NET developers. This article will show you how you can customize the Starter Kit, create new content and develop a custom page template. You will need Visual Studio 2005 or Visual Web Developer 2005 Express Edition and Microsoft SQL Server 2000 or 2005. Installing the Starter KitDownload the Starter Kit from unpack the ZIP file to your disk and open the solution in Visual Studio 2005 (or Visual Web Developer) using the CorporateSite.sln file. Run the project and you will be asked for creating a Microsoft SQL Server database. After you create the database, you will see the default web site like this: Modifying the Default ContentNow we will sign in to the administration interface and create a new page. Follow the "Click here to sign in" link at the top of the page and sign in as administrator (the password is blank by default). Click Content in the main menu, click the Services page in the left tree view and click New in the main toolbar. Choose to create a new Page (Menu Item) and enter the following values: Caption: Web Design Order: leave empty Type: Page Template Page Template: click Select... and choose Simple Text with Left Menu Page Title, Page Description, Page Keywords: leave empty Show in Site Map: checked Hide in Navigation: unchecked Click OK to create the page. Click Site in the main toolbar. Enter some text in the editable regions and save changes using the Save page link. After you sign out, you will see the changes published on your live web site. You have used a built-in page template to create a new page. The page

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Based assays, micro dosing, cell perfusion, immunolabeling, periodicinjections or calcium imaging. 355APPLICATIONPACKAGES& PLATFORMSAPPLICATION PACKAGES & PLATFORMS | OOACOOACOrgan-on-a-chip Fluigent has partnered with Micronit to offer a versatile fully integrated organ-on-a-chip kit which reproduces numerous characteristics of the in vivo environment cells. Independant Physiological Save time: Compact monitoring conditions Protocol System for each flow mimiking automation chamberCharacteristicsThe Fluigent/Micronit organ-on-a-chip kit focuses on modeling the main biochemical andbiophysical features of the native environment of cells in order to induce their growthand differentiation as functional tissues. Air-liquid interface, flow induced shear stress,mechanical stimulation, biochemical gradient, cell-cell coculture have been reported tosignificantly improve the functionality of in vitro models. All these parameters are con-trolled by the system. Top chamber solution Flow-Rate Platform FLOW UNIT S The Organ-on-a-chip kit is composedFLOWTM-EZ FLOW of multiple microfluidic components: UNITS porous • Flow EZ™ (page 8) membrane Flow-Rate Platform FLOW UNIT lined by cell • Fluiwell (page 15) S • Flow Units (page 12) A Micronit chip is included. Bottom chamber solution 37APPLICATION PACKAGES & PLATFORMS | DROPLET STARTER PACK DROPLET STARTER PACK Get started within minutes Droppack The Droplet Starter Pack is designed for microfluidic droplets experiments. It includes the EZ Drop chips, and liquid handling solution accessories. Characteristics The Droplet Starter Pack includes: • 2 Flow EZ™ for pressure-driven injection (page 8) • 2 Flow Units for flow rate control (page 12) • 2 P-Cap 2 mL (page 14) • 1 Droplet Kit (page 26) • All tubing fitting and accessories (page 26) Highly monodispersed Most

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To be followed in the event of an emergency. Engine failure or other airplane-related emergencies are most unlikely to occur if the prescribed procedures for pre-flight checks and airplane maintenance are followed. Page 73: Certain Airspeeds In Emergencies Emergency DA 42 AFM Procedures 3.1.2 CERTAIN AIRSPEEDS IN EMERGENCIES Event One engine inoperative minimum 68 KIAS control speed (Air) v One engine inoperative speed for 82 KIAS best rate of climb v 3.1.3 SELECTING EMERGENCY FREQUENCY In an in-flight emergency, depressing and holding the Com transfer button »º on the G1000 for 2 seconds will tune the emergency frequency of 121.500 MHz. Page 74: Airplane-Related G1000 Warnings Emergency DA 42 AFM Procedures 3.2 AIRPLANE-RELATED G1000 WARNINGS 3.2.1 WARNINGS / GENERAL "Warning" means that the non-observation of the corresponding procedure leads to an immediate or important degradation in flight safety. The warning text is displayed in red color. A warning chime tone of 1.5 seconds duration will sound and repeat without delay until the alarm is acknowledged by the crew. Page 75: L/R Oil Temp Emergency DA 42 AFM Procedures 3.2.3 L/R OIL TEMP Left / Right engine oil temperature is in the upper red L/R OIL TEMP range (too high / above 140 °C). Oil temperatures above the limit value of 140 °C can lead to a total loss of power due to engine failure. Page 76: L/R Gbox Temp Emergency DA 42 AFM Procedures 3.2.5 L/R GBOX TEMP Left / Right engine gearbox temperature is in the L/R GBOX TEMP upper red range (too high / above 120 °C). Gearbox temperatures above the limit value of 120 °C can lead to a total loss of power due to engine failure. Page 77: L/R Altn Amps Emergency DA 42 AFM Procedures 3.2.7 L/R ALTN AMPS Left / Right engine alternator output is in the upper red L/R ALTN AMPS range (too high / above 60 amps). Proceed according to: 3.7.2 HIGH CURRENT 3.2.8 L/R ENG FIRE... Page 78: L/R Starter Emergency DA 42 AFM Procedures 3.2.9 L/R STARTER Left / Right engine starter is engaged L/R STARTER Proceed according to: 3.7.3 STARTER MALFUNCTION 3.2.10 DOOR OPEN Front and/or rear canopy and/or baggage door are/is DOOR OPEN not closed and locked. Page 79: G1000 System Warnings Emergency DA 42 AFM Procedures 3.3 G1000 SYSTEM WARNINGS 3.3.1 RED X A red X through any display field, such as COM frequencies, NAV frequencies, or engine data, indicates that display field is not receiving valid data. 3.3.2 POSN ERROR... Page 80: Altitude Fail Emergency DA 42 AFM Procedures 3.3.5 ALTITUDE FAIL ALTITUDE FAIL The display system is not receiving altitude input from the air data computer; accompanied by a red X through the altimeter display.. Brother HL-L3270CDW,Starter Black Toner Cartridge (1,000 pages)^Starter Cyan Toner Cartridge (1,000 pages)^Starter Yellow Toner Cartridge (1,000 pages)^Starter Magenta