Usable fuel capacity 48USG/182 L. Tabs.34 USG / 130 litres Fuel consumption/hour 10 USG/38L Per hour without leaning OIL 5-7 QTS American quart=approx.1 litre Max. take off weight 2325lbs/1054kg Check weight and balance if 3 pob. G limits 4.4 - 0 Aerobatics and spinning prohibited Vso 44 kts IAS Stall speed, landing configuration Vs1 50 kts IAS Stall speed without flap Vr 55 kts IAS Not applicable to grass runway Vy 79 kts IAS Best rate of climb airspeed Vx 63 kts IAS Best angle of climb airspeed WARRIOR PA28-161 Vat Full 65 kts IAS Final approach speed with flap Vat Flapless 70 kts IAS Final approach speed without flap CHECK LIST Vat perf 60 kts IAS Final approach short runway V best glide 73 kts IAS Glide speed for best range GoFly Hangar 1, Vfe 103 kts Max. flap extension speed Old Sarum Airfield, Max. cross wind 17 kts As demonstrated by expert pilot! SALISBURY SP4 6DZ O1722 444890 www.goflyuk.com STARBOARD WING Piper PA-28 Checklist ………..…………PA-28-161-Warrior II Flap…………………………..…………………….. Linkages, hinges, condition (free of mud) Aileron………….……………………..…………… . Linkages, hinges, full & free movement Copyright GoFly March 2013 Wing tip………………………………..…………………. Condition, security, navigation light Wing surface………………………..…………… …… ...Condition, upper & lower surfaces Leading edge…………………………………………………………………………….Check for dents PREFLIGHT CHECK Fuel tank………………………………………..Contents visually checked, fuel cap secure, Tie down and chocks……………………………………………………………………….…..REMOVE Fuel drain………………………………………………...Examine sample, check fully closed. Control locks and covers……………………………………………..……REMOVE AND STOW Fuel vent.…………………………………..………………………………………………………………Open Avionics………………………………………………………………………………………………………..OFF Park Brake………………………………………………………………………………………………… ON Ignition…………………………………………………………………………………………OFF/ KEY OUT STARBOARD UNDERCARRIAGE Master switch……………………………………………………………………………………………….ON Tyre………………………….……………..……...Condition, inflation, creep marks aligned Annunciator panel (if equipped)………………………………………………………………CHECK Hydraulic lines…………………………………………………………………….…..Conditions, leaks Fuel quantity gauges…………….……………….…..check, on tank with lowest content Disc brake block…………………………………………………………………….…………..Condition External electrical switches…………………………………………………………………….ALL ON Oleo/Strut…………………………………………….Normal extension (approx.4.5 inches) Navigation lights………………………………………………………………………………………CHECK Torque link………………………………………..…………………….Nuts and split pins secure Strobes…………………………………………………………………………………………………….CHECK Landing light…………………………………………………………………………………………… CHECK Stall Warner…………………………………………………………………………………….…….. CHECK FRONT FUSELAGE & ENGINE Pitot heat………………………………………………………………………………….. CHECK Starboard cowling……………………………………………………….…Check oil level (6 qts.) Anti-collision beacon………………………………………….………………………………….. CHECK Engine compartment…………Check for leaks, contamination, loose connections. External electrical switches.(except anti-collision beacon)…………………….ALL OFF Secure cowling Master switch………………………………………………………………………………………………OFF Windscreen………………………………………..……………………..CLEAN, OAT probe secure First aid kit…………………………………………………………………………….In position, secure Nose leg……..………Oleo/strut extension (3.25inch), torque link, nuts & split Fire extinguisher………………………………..………………………………… In position, secure pins Cockpit…………………………………...……..Check for & remove/stow any loose items Nosewheel…………………………………...…..Condition, inflation, creep marks aligned Flaps………………………………………………………………………………………………………SET 25° Front cowling…………………………..…..……...Condition & security, air intakes clear Propeller……………………………………………Check Condition, especially leading edge Port Cowling………………………………………………………………..…Check brake fluid level Engine compartment…………………….Check for leaks, contamination, loose leads EXTERNAL Secure cowling Check all of exterior and all surfaces for damage, interference, ice, snow, frost Fuel drain……………………………………………………Examine sample, check fully closed PORT UNDERCARRIAGE INTERNAL Tyre………………………….…………..………...Condition, inflation, creep marks aligned Mobile phones…………………………………………………………………OFF / FLIGHT MODE Hydraulic lines…………………………………………………………………….…..Conditions, leaks Passenger brief…………………………………………………………………………………If required Disc brake block…………………………………………………………………….…………..Condition Seats…………………………………………………………………………….………..Adjusted &locked Oleo/Strut…………………………………………….Normal extension (approx.4.5 inches) Hatches & harnesses………………………………Closed and latched: tight and locked Torque link………………………………………..…………………….Nuts and split pins secure Parking Brake………………………………………………….…………………………….……………..ON Radios………………………………………………………………….........................................OFF PORT WING Instruments……………………………….…..Legible, serviceable, readings within limits Flying Controls……………………………….……….Full & free movement, correct sense Flap…………………………..…………………….. Linkages, hinges, condition (free of mud) Trimmers…………………………………….……….Full & free movement, set for take-off Aileron………….……………………..…………… . Linkages, hinges, full & free movement Flaps……………………………………………………………………..……Check in stages, select up Wing tip………………………………..…………………. Condition, security, navigation light Cabin air controls………………………………………………….………………………...Closed (Off) Wing surface………………………..…………………....Condition, upper & lower surfaces Fuel………………………………..………….…….…….On, select tank with lowest contents Leading edge…………………………………………………………………………….Check for dents Fuel tank………………………………..……..Contents visually checked, fuel cap secure, START Fuel drain………………………………………………...Examine sample, check fully closed. COLD START Fuel vent.…………………………………..………………………………………………………………Open Throttle………………………………Operate full & free movement, set 1/2 inch open Mixture………………………………………….…………….….Full & free movement, set rich PORT FUSELAGE Throttle friction………………………………………..………………..Operate and check loose Carburettor heat………………………………………..…...Full & free movement, set cold Windows…………………………………………………………..……..…………….………………..Clean Master switch……………………………………………..………………………………………………ON Skin…………………………………………………………………………………… Examine condition Circuit breakers/fuses………………………………………………………………….........In/secure Aerials……………………………………………………………………………….……………………Secure Beacon……………………………………………………………….………………….………..Confirm ON Tail Fin………………………………………. condition & security, fairings, aerials, beacon Fuel pump……………………………………….…..………ON, check fuel pressure, then OFF Rudder……………………………………. condition, linkages, nuts & split pins, nav. light Primer…………………………………………………..………….…Prime (2-6 strokes*) &LOCK Stabilator………………………………….…. condition, linkages, full and free movement Lookout…………………………………................Good look around, call “CLEAR PROP” Anti-balance tab ……………………………………………………...condition, hinges, linkage. Starter……………………………………………...........................................................Engage RPM on start-up……………………………………….…………Avoid high revs. Set 1200 rpm STARBOARD FUSELAGE * Depending on ambient temperature Skin…………………………………………………………………………………… Examine condition STARTING ENGINE WHEN HOT Aerials……………………………………………………………………………………….…………….Secure As detailed above except:- Windows…………………………………………………………….…………………………………..…Clean Initially avoid priming. If unsuccessful try 2 strokes of primer. Baggage door………………………………..………………………………………Closed and secure DO NOT pump with the throttle. Doors………………………………………………….………………..…………Latch & Hinges secure DO NOT engage starter motor for more than 10 secs. continuous. STARTING ENGINE WHEN FLOODED TAXYING Brakes………..…..…………………………………….Park brake ON. Brake pedals covered Throttle…………………………………………………………………………………….………Fully open Brakes……………………………………………………...………….Checked as soon as possible Master switch………………………………………………………….………………………………….ON Rudder………………….…………….…Full Movement & nose wheel steering checked Electric fuel pump……………………………………………………………………………………….OFF Differential braking…………………………………………………….…………………………Checked Mixture…………………………………………………………………………………………….Idle cut-off Flight instruments*…………………………………………………………………Checked in turns Lookout………………………………….............…Good look around, call “CLEAR PROP” * HI, Compass, Turn Co-ordinator, Attitude Indicator Starter………………………………………………………………………………………………...ENGAGE When engine fires:- Mixture………………………………………………………………………………………………..Advance POWER CHECKS Throttle…………………………………………………………………………………………………..Retard Position………………………………..…….Into wind, check clear all round, esp. behind STARTING WITH EXTERNAL POWER SOURCE Parking brake………………………………………………………………..………………………………ON Master switch……………………………………………………………………………………………..OFF Throttle…………………………………………………………………………………………1200 rpm set All electrical equipment……………………………………………………………………………….OFF Fuel…………………………………………………………………..…Note time and change tanks External power plug………………………………………………………………..Insert in fuselage Engine temp. & press……………………….…………………………..……………..Within limits Proceed with normal start: after engine is running:- Throttle……………………………………………...……SET 2000rpm – check brakes holding Throttle…………………………………………………………………………….Lowest possible RPM Carb. Heat…ON for 15 secs.…………….., drop approx. 75 rpm, steady, SET COLD External power plug…………………………………………………..Disconnect from fuselage Magnetos…………………………………………………Check left & right & back to BOTH Master switch………………………..……………………………………………………………..……..ON Max. Drop 175rpm, max. Difference between mags. 50 rpm Ammeter……………………………………………if no reading do not proceed with flight Engine temp. & pressures (oil and fuel).……………………………….……….Within limits Ammeter……………………………………………………………………….……………..………Charging AFTER START Suction……………………………………………………………………………………………………….3”-5” Throttle fully closed………………….……………..……………………………….
Relative Navigation Light Detection and Ranging (LIDAR) Sensor Development Test Objective (DTO) Performance Verification
NASA/TM2013-217992 NESC-RP-11-00753 Relative Navigation Light Detection and Ranging (LIDAR) Sensor Development Test Objective (DTO) Performance Verification Cornelius J. Dennehy/NESC Langley Research Center, Hampton, Virginia May 2013 NASA STI Program . in Profile Since its founding, NASA has been dedicated to the CONFERENCE PUBLICATION. advancement of aeronautics and space science. The Collected papers from scientific and NASA scientific and technical information (STI) technical conferences, symposia, seminars, program plays a key part in helping NASA maintain or other meetings sponsored or co- this important role. sponsored by NASA. The NASA STI program operates under the SPECIAL PUBLICATION. Scientific, auspices of the Agency Chief Information Officer. technical, or historical information from It collects, organizes, provides for archiving, and NASA programs, projects, and missions, disseminates NASA’s STI. The NASA STI often concerned with subjects having program provides access to the NASA Aeronautics substantial public interest. and Space Database and its public interface, the NASA Technical Report Server, thus providing one TECHNICAL TRANSLATION. of the largest collections of aeronautical and space English-language translations of foreign science STI in the world. Results are published in scientific and technical material pertinent to both non-NASA channels and by NASA in the NASA’s mission. NASA STI Report Series, which includes the following report types: Specialized services also include organizing and publishing research results, distributing specialized research announcements and feeds, TECHNICAL PUBLICATION. Reports of providing information desk and personal search completed research or a major significant phase support, and enabling data exchange services. of research that present the results of NASA Programs and include extensive data or For more information about the NASA STI theoretical analysis.
Lighting up to 7 Times Brighter Than Other LED Landing Lights!
Lighting FAA-PMA Approved AeroLEDs Lighting Increase safety and reduce operating cost! See the Difference... Lighting Know the Difference... • Increased safety • Direct replacement • Up to 80% reduced power consumption • Long life - over 50,000 hours! • Lighter weight - no heavy power supply - save up to 3 lbs • Reduced drag • Zero maintenance • 10x more efficient than incandescent! Increased Safety AeroLED lights allow you to comply with the latest FAA recommendations (Operation Lights On) regarding extended use of taxi, landing, and anti-collision lights without fear of reduced light performance or life. They all feature optimized light color (6500k sunlight equivalent) for proven superior air-to-air recognition. The landing and taxi lights also feature an optional pulsed recognition light mode. Reduced Power Consumption High efficiency LED lights use less than 1/3 the power of halogen bulbs. They significantly reduce the load on the electrical system and they won't dim due to low voltage, typical of low RPM final approaches when you need them most! Postition lights aerodynamic design results in less drag than original equipment! Longer Life - Zero Maintenance All AeroLED products are designed to be a "lifetime buy". They last over 50,000 hours when properly installed and do not degrade with on/off cycles. They are extremely rugged and hardened against all kinds of electrical damage, shock, and vibration. Up to 7 times brighter than other LED landing lights! PAR36 Landing Light Comparison Measured Brightness at 50 Ft. Manufacturer Intensity
NAVSTROBE LIGHTING – KUNTZLEMAN AIRCRAFT SEXTANT NAV NAVSTROBE PAR 36 LED SYSTEM WITH CONSTANT + LANDING LIGHT CM FAST STROBE 40W Aircraft PAR36 Landing Light, 220w, 109, 400 LM These bulbs are standard parts and have been LEDs. designed to meet the requirements of TSO-C30c. These are non-TSO’d Complete combination navigation and strobe lights P/N 11-14745 .........$209.95 for your aircraft. Emitter Types: Cree LED’s. Turn on first: Constant lighting / Turn on second time <3s: WP Fast Strobe. Switch between modes in fog/cloud etc. P/N 11-14934 .........$429.00 NAVSTROBE PAR 36 LED TAXI LIGHT NAVSTROBE AIRCRAFT Aircraft PAR36 Taxi Light, 220w, 109, 400 LM LEDs. NAVIGATION SYSTEM These are non-TSO’d ME 2 Modes: Constant & Fast Strobe. P/N 11-14744 .........$221.95 Kit Includes: • 2ea. Wingtip combination navigation and strobe light (BAY15scs-10w-A-1512) • 1ea. White tailfin combination navigation and strobe light BEACON LIGHT CONSTANT (BA15sWcs-10w-1156) • 2ea. Lens cover gaskets (Sextant A450) • 1ea. Dielectric grease pouch & FAST WHITE STROBES HA (Sextant 31880) ...........P/N 11-16470 .........$166.80 Note: For Experimental aircraft use only. Not FAA/ PMA Approved. NavStrobe Aircraft Beacon Light AIRCRAFT ANTI- with Constant & Fast White Strobe 503 LM LED’s. Dimensions: 1.9 in x 0.7 in (49.0 mm x 1.8 cm) COLLISION STROBE LIGHT Weight: 0.32 oz (9 g). 10-28VDC. Aircraft Anti-Collision Strobe Light, 45w, Turn on first: Constant lighting / Turn on second time <3s: Fast Strobe. 1350 LM CREE LEDs. Total Emitters: 9 x AP Switch between modes in fog/cloud etc.
GENERAL the Lighting System Provides Interior and Exterior
Bombardier Challenger 605 - Lighting GENERAL The lighting system provides interior and exterior illumination of the aircraft. In addition, lights provide information and guidance to passengers in normal and emergency situations. The lighting system includes: • Exterior lighting; • Flight compartment lighting; • Passenger compartment (cabin) lighting; • Service lighting; and • Emergency lighting. EXTERIOR LIGHTING Description The exterior lighting system is controlled from the EXTERNAL LTS panel or the LANDING LTS panel, and consists of the following: • Navigation lights; • Beacon light; • Anti-collision lights; • Logo lights; • Wing inspection lights; • Landing lights; and • Recognition/taxi lights. Components and Operation Navigation Lights The navigation lights are located in each wing tip, fuselage tail cone tip, and at the tip of the stabilizer fairing. A wing tip assembly contains two navigation lights that work simultaneously. Wing Tip Navigation Light Figure 16−10−1 The NAV switch controls the navigation lights (see Figure 16−10−2). Page 1 Bombardier Challenger 605 - Lighting EXTERIOR LIGHTING (CONT'D) Beacon Light There are two red beacon lights located on the top and bottom of the fuselage, near the middle of the aircraft. The BEACON switch controls the beacon lights (see Figure 16−10−3). Anticollision Lights The anticollision lights consist of two wing tip strobe lights, located in the wing tip assembly, and one strobe light at the tip of the fuselage tail cone, co-located with the navigation light. The A/COLL switch controls the anticollision strobe lights (see Figure 16−10−3). Logo Lights The logo lights are located on top of the aircraft’s engine pylons. When selected, these lights illuminate the aircraft’s vertical stabilizer.
FOR TRAINING USE ONLY C-5 HANDBOOK FOR TRAINING USE ONLY INTRODUCTION This book is designed to be used as a T.O. title. Example: page 3-1 comes from quick-reference pocket handbook T.O. 1C-5A-2-3/Pneudraulics. describing the systems and subsystems of the C-5 Galaxy aircraft. Basically, the handbook consists of descriptive text relating to pictures or As a training aid, this book gives you the drawings of the airplanes structural and distinct advantage of having the general system components. information of twelve aircraft T.O.s condensed into one handbook. For the most part, pictures and text within the book reflect that of the C-5B model The book is formatted in accordance with aircraft. However, in some cases, the aircraft T.O.s, 1C-5A-2-1 through references to "A-model not modified" and 2-13, with the exception of the 2-11 wiring AF68-213 and AF68-216 "Space diagrams, which, due to the size and Container Module (SCM) airplanes " have content could not be included. Each been included. chapter in the handbook represents an aircraft T.O. starting with the 2-1. ALTHOUGH THIS HANDBOOK IS Additionally, for quick reference DERIVED FROM TECH DATA, IT IS purposes, the first digit of the page NOT INTENDED TO REPLACE THE numbers represents the last number of T.O.s. NOR, WILL IT BE USED AS the T.O. from which the information was SUCH. obtained and the page header reflects the i PRESSURES, READINGS, AND LIMITATIONS ARE SUBJECT TO CHANGE AND ARE ONLY USED IN THIS BOOK TO PROVIDE GENERAL PARAMETERS ii TABLE OF CONTENTS INTRODUCTION .
® NAVIGATION LIGHTS Navigation Lights Disclaimer: This information is correct as “A set of lights shown by a ship or aircraft between sunset and at 1st November 2016, and is sunrise, and in rain and fog, to indicate its position and orientation.” designed as a basic guide and RAILBLAZA illuminate Series Battery Powered Navigation introduction to navigation Lights are designed primarily to meet the US Coast Guard requirements lighting for water craft. It is (USCG 2NM) for navigation lights on power boats under 12 metres (39.4’) not to be used as a technical in length. They are made in New Zealand, from high quality materials, and reference. RAILBLAZA assume no deliver fantastic performance at an affordable price. responsibility for any errors or omissions. Please check with the Requirements for vessels under 12 metres appropriate governing body regarding full regulations for navigation All vessels under 12 metres shall exhibit one of the following: lights in your area. • Separate or combined sidelights; a masthead light and a stern light • Separate or combined sidelights and an all round white light. Some internet references for your local region; The masthead or white all round light shall be carried at least one metre New Zealand above the sidelights. http://www.maritimenz.govt.nz/recreational/documents/Safer-Boating- an-essential-guide-2014.pdf Power-driven vessels less than 7 meters in length whose maximum Australia: speed does not exceed 7 knots may in lieu of the above exhibit an all- • QLD http://www.msq.qld.gov.au/Safety/Navigation-lights round white light and shall, if practicable, also exhibit sidelights • NSW http://www.rms.nsw.gov.au/maritime/safety-rules/rules- Form and Function of RAILBLAZA Lights regulations/night-safety.html There are two models in the illuminate Series, the i360 All-round white, • TAS http://www.mast.tas.gov.au/recreational/navigation/ and the iPS Port/Starboard.
SPECIFICATIONS OFFICIAL NO 1147419 LENGTH 50FT BREADTH 15.0 FT GROSS TONNAGE 33 SPEED 28 MPH PASSENGERS 25 FUEL 500 DECK SPACE 16X10 DESCRIPTION: Vessel was built of all welded aluminum construction by owner in Chauvin, La during 2004. Vessel has a flush deck, model bow, square stern and aluminum superstructure with aluminum watertight doors and rubber gasket mounted weather tight windows This vessel is a typical coastal crew boat with a hard chine and a vee'd bottom. The construction is a typical all aluminum crew boat utilized in the oil industry. This vessel has been updated and repowered in July of 2011 HULL CONSTRUCTION Bottom plating is 1/4" original thickness except for last 20ft which is 3/8" aluminum plate. Side plating is 1/4" original thickness. Vessel is framed both longitudinally and transversely with aluminum bulbous tees. FENDER SYSTEM Hull is fitted with the following fender system. Upper strake is located at the weather deck elevation and extends from bow to stern. Second strake is located approximately 18' below and extends from stern forward approximately 20". Fender system is constructed of approximately 2-1/2" split aluminum pipe. Fender system is installed on each side. In addition, vessel is fitted with heavy tires installed on each side from the pilothouse aft to the stern on each side. BULWARKS Bulwarks are non-existent; however vessel is fitted with an approximate 12" high toe rail, installed from the bow stem aft approximately 10" on each port and starboard side DECK FITTINGS Deck fittings are located as follows; located on the bow on centerline, is one (1) approximate 3" diameter single aluminum bit.
SECTION X SERVICING TABLE OF CONTENTS Introduction 10-3 GROUND HANDLING Towing by Hand 10-3 Towing with a Tug 10-3 Tie-Down 10-3 SERVICING Battery 10-4 External Power 10-4 Recharging Battery Using Auxiliary Power 10-4 Checking Electrical Equipment 10-4 Magnetos 10-4 Propellers 10-4 Propeller Dome Air Pressure Setting 10-4 Propeller Blade Bearing Lubrication 10-5 Induction Air Filters 10-5 Landing Gear 10-5 Main Wheel Jacking 10-5 Shock Struts 10-5 Brakes 10-6 Parking Brake 10-6 Tires 10-6 Fuel System 10-6 Oil System 10-7 Oxygen System 10-7 Oxygen Cylinder Retesting 10-7 MINOR MAINTENANCE Cleaning 10-7 Cleaning Deice Boots 10-7 Interior 10-8 Engines 10-8 Cleaning and Care of Aircraft Finish 10-8 Cleaning Plastic Windows 10-8 Lubrication Diagram 10-9 Lubrication Points 10-10 Recommended Servicing Schedule 10-16 Consumable Materials 10-19 Approved Engine Oils 10-22 Lamp Replacement Guide 10-23 i . '. Duke 60 & A60 Supplemental Operational Data 10·1 INTENTIONALLY LEFT BLANK 10-2 Duke 60 & A60 Supplemental Operational Data INTRODUCTION TO SERVICING The purpose of this section is to help you keep your BEECHCRAFT Duke in top condition between visits to your BEECHCRAFT Parts and Service Outlet. This information will aid you in determining when the airplane should be taken to a shop for periodic servicing or preventive maintenance. It will also guide you should you choose, or be obliged by circumstances, to do some minor servicing yourself. These procedures are in no sense a substitute for the services performed at your BEECHCRAFT Parts and Service Outlet.