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fli 450s manualIt will provide you with a lifetime of trouble free use providing you follow a few simple guidelines. Mounting Guidelines Your FLI amplifier is designed with a swift installation routine in mind. Please mount the amplifier in a dry location on a solid surface. At least an 8 gauge cable should be used. The amplifier ground should be connected directly to the chassis of the vehicle, to bare metal. The cable length should be kept to an absolute minimum. To optimise your setup seek the advise of a professional installation engineer or visit your local FLI audio dealer. Always test the speakers and confirm that they are wired correctly first. If in any doubt get help from a qualified auto electrician. Amplifier Will Not Power Up Check for good ground connections. Other cookies, which increase the comfort when using this website, are used for direct advertising or to facilitate interaction with other websites and social networks, are only set with your consent.Other cookies, which increase the usability of this website, serve for direct advertising or simplify interaction with other websites and social networks, will only be used with your consent. Combining and synchronizing the arm with the temperature controller, it guarantees a perfect quality and high repeatability of your process. To browse Academia.edu and the wider internet faster and more securely, please take a few seconds to upgrade your browser. This compilation was prepared on 13 March 2017 taking into account amendments up to Manual of Standards Part 173 Amendment Instrument 2017 (No. 1). It is a compilation of the Manual of Standards Part 173 — Standards Applicable to Instrument Flight Procedure Design as amended and in force on 9 March 2017. Prepared by the Flight Standards Branch, Aviation Group, Civil Aviation Safety Authority, Canberra.http://www.goldfingers.fr/userfiles/federal-personnel-manual-296-33.xml
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You may download, display, print and reproduce this material in unaltered form only (retaining this notice) for your personal, non-commercial use or use within your organisation. Apart from any use permitted under the Copyright Act 1968, all other rights are reserved.In those parts of the MOS where it is necessary to establish the context of standards to assist in their comprehension, the sense of parent regulations has been reiterated. 1.1.3.5 Readers should understand that in the circumstance of any perceived disparity of meaning between MOS and CASRs, primacy of intent rests with the regulations. 1.1.3.6 Service providers must document internal practices ( Rules) in their own operational manuals, to ensure the maintenance of and compliance with standards. 1.1.3.7 ACs are intended to provide recommendations and guidance to illustrate a means, but are not necessarily the only means of complying with the Regulations. ACs may explain certain regulatory requirements by providing interpretive and explanatory material. Note This procedure is to complement the obligation on CASA under paragraph 2.1.9A of the Manual of Standards (MOS) — Part 139 Aerodromes that where an aerodrome with a TIFP ceases (for whatever reason) to be certified and does not become registered, or ceases to be registered and does not become certified, CASA will take every reasonable step necessary to give written notification to the certified or authorised designer of the TIFP. 6.1.4.2 At intervals not exceeding three years, CASA shall conduct a flight re-validation of a procedure. This focus is facilitated through the use of various obstacle and terrain databases. Such a case would indicate that the unforeseen obstacle is higher than the controlling obstacle and that it may affect the procedure. If such an unforeseen obstacle is observed, its location and observed height AMSL must be recorded for subsequent detailed analysis by the procedure designer. 7.1.10 25 and 10 NM Minimum Sector Altitude 7.http://milkexim.ru/imgeditor/federal_personnel_manual_chapter_610.xml1.10.1 Each 25 NM sector, or the 25 NM circle, and the 10 NM circle must be checked at their specified altitudes. 25 NM and 10 NM MSAs include obstacles out to 30 NM and 15 NM respectively from the navigation aid or ARP upon which the MSA is based. Checks must include the controlling obstacle in addition to other obviously high terrain or obstacles. TAAs include obstacles out to 30 NM from the initial approach fix upon which the TAA is based. Where adjacent TAAs do not have greatly differing terrain elevations, judgement may be exercised regarding the tracks flown to provide a full coverage of the area. These obstacles must be checked at the specified altitude. Additionally, each step in the final and intermediate segments must be flown at the OIS altitude. Each step must be flown around the radius of the step plus 1 NM, between the lateral limits of the sector splay. Figure 7?2: Final and missed approach segments 7.1.17 Holding and Initial Segments 7.1.17.1 The controlling obstacles for the holding and initial segments must be checked at their specified altitude and any unforeseen obstacles identified. This check should be flown at the maximum segment speeds for the fastest category of aircraft served by the procedure. In particular, the following points should be noted: (a) pay particular attention to airspeed during manoeuvres with high angles of bank; (b) be vigilant for inconspicuous towers and power transmission lines. Those segments that do not apply should be so annotated. Procedures should normally be designed for category groups. The primary areas for instrument approach procedures other than DME Arrivals must not be closer than one nautical mile to the primary area of a procedure to a second aerodrome, unless all procedures involved are wholly contained in controlled airspace. Note: If airspace considerations require a nominal gradient greater than 5, the IAL chart must show a climb gradient identified by an asterisk. 8.1.1.http://ninethreefox.com/?q=node/170855 Prohibited and Restricted (P and R) Areas. Note: If a gradient of greater than 5 is required, the IAL chart must show the climb gradient identified by an asterisk. 8.1.1.6 Danger Area Associated with High-Velocity Gas Efflux. Minimum runway width of 30 m and a minimum strip width of 90 m for procedures limited to code 1, 2 and 3C aeroplanes. For aerodromes with a runway strip width less than 300 m, the MDA must be adjusted in accordance with paragraph 8. 1.4.1. Runways accommodating aeroplanes above code 3C require a minimum graded runway strip width in accordance with MOS Part 139. (b) Approach OLS Area and Gradient. The approach OLS area and gradient parameters are as per MOS Part 139, except that the length of inner edge may be reduced to a minimum length equal to the runway strip width provided in accordance with paragraph 8.1.3.2 (a). Where an OLS area survey to the Non-Precision Approach Runway criteria is not available, a straight-in approach minima may be published, provided the MDA is 500ft or more above the aerodrome elevation and an operational assessment confirms the visual approach path is clear of obstacles. The obstacle free plane extends from this “Nominal Intercept Point” at an altitude equal to the MDA minus MOC, to a point 50 ft above the runway threshold. (See Fig u re 8?1 ). Laterally, the visual approach path will commence with a width equal to the runway strip width provided and splay at 10 to the visual approach point described above. Figure 8?1: Visual descent segment (c) Surface Wind Information. Surface wind information must be provided in accordance with C A O 92.2. (d) Runway Edge Lighting. Runway edge lighting shall have 60 m spacing, except that existing 90 m spacing is acceptable subject to assessment for Non-Precision Approach Runways intended to be used in visibility conditions of 1.5 km or more. The suitability of existing 90 m spaced lighting for night approaches must be assessed during the instrument approach validation process. 8.1.4 Visual Segment Limitations 8.1.4.1 Runway Strip Width less than 300 Metres. The vertical and horizontal accuracy of the maps and charts used during instrument approach procedure design must be accounted for. In addition, an allowance must be made for vegetation growth and the erection of new obstacles in the period between obstacle surveys. The allowance for these factors must be 100 ft over open country or water suitable only for leisure boating and 200 ft over tropical rain forest, open water, or built-up areas. For an approach type mentioned in column 1 of Table 8-1A, the minimum visibility values approved for precision approach Category II or III procedures are those in column 2 of the Table which, subject to the runway capability conditions mentioned in column 3 of the Table, correspond to the approach type. Table 8-1A: Category II and III minimum visibility based on runway capability Approach type Minimum runway visual range (RVR) (metres) Runway capability Precision approach Category II 350 Precision approach runway Category II. Precision approach Category II and III lighting system. RVR sensors at all zones. Precision approach Category IIIB 75 Precision approach Category IIIC Not applicable in the Australian environment. 8.1.6.3 Circling. Circling visibility must be determined from the following table. (The basis upon which the values for circling visibility have been determined are contained in Sect i on 9.1.) Table 8?2: Circling visibility Aircraft Category A B C D E Circling Visibility (km) 2.0 2.4 4.00 5.00 7.00 8.1.6.4 Where a procedure terminates outside the circling area, a visual segment may be provided. Note: A DH or RA height is not required for Category III procedures. For precision approaches, the State DA must be adjusted for pressure error to determine the AOM. Aircraft pressure error correction must be applied or, alternatively, at least 50 ft added to the DA. 8.1.9 General Alternate Minima 8.1.9.1 The general alternate minima must be calculated by adding the tolerance for the forecast ceiling and visibility to the circling minima (500 ft and 2 km). 8.1.10 Special Alternate Minima 8.1.10.1 Airborne Equipment. Although not specified and not required, it is assumed that such aircraft will also have duplicated ADF systems. 8.1.10.2 Ground Equipment. For a location to be considered it must be served by ILS, LLZ or straight in VOR instrument approach procedures to at least two runway directions which are suitable for use by all aircraft likely to use the special low alternate minima. 8.1.10.3 The instrument approach procedures should preferably utilise different VHF ground equipment. However, the use of the same ground equipment for both approaches is acceptable provided the equipment meets the requirements of ICAO Annex 10, Volume 1, Attachment C, Table C2 or Attachment F, as applicable, and an alternative straight in instrument approach procedure which utilises a different aid is available. 8.1.10.4 Other Requirements. Only controlled aerodromes qualify. The Special Alternate Minima shall not be available during any period when ATC and Bureau of Meteorology (BoM) observations and forecasting services are not provided at the aerodrome concerned. 8.1.10.5 Calculation of Special Alternate Minima. Ceiling values should be rounded out to the nearest 50 ft.However, this does not absolve the captain of the pre-flight planning responsibility referred to in paragraph 8.1.1 1.5. Further, the operator must demonstrate that the value selected will satisfy paragraph 8.1. 11 for all operations, both scheduled and unscheduled which may occur during the calendar period of application of the values selected. The demonstration must account for the three standard deviation wind values for both landing and crosswind components and may account for a downwind landing to the value allowed in the relevant aircraft certification. 8.1.12 Australian Differences to ICAO PANS-OPS Vol II 8.1.12.1 Circling Area. Where the circling area has been segmented to facilitate a lower minima and the missed approach point is located within the NO CIRCLING area, the area should be extended by an arc of no less than 2 NM to include the missed approach point within the applicable circling area. (See Figure 8?3.) Figure 8?3: Circling area modified to exclude MAPT 8.1.12.2 Height Above Aerodrome (HAA) and Height Above Threshold (HAT). The minima for non-precision approach procedures shall include a HAA, and for precision approach procedures shall include a HAT. 8.1.12.3 GPS Non-Precision Approach Missed Approach Procedures—Use of Secondary Areas. This instruction clarifies the application of secondary areas in the design of GPS NPA missed approach procedures within the Australian FIR. (a) ICAO PANS-OPS Vol II Part III paragraph 33.7.2 and Appendix paragraph 6.5 support the use of secondary areas for GPS NPA missed approach design. However, the text following the asterisks in Figures III-33-6 and III-33-7 state that, until further operational experience is obtained with basic GNSS receivers, the full width of the missed approach area should be treated as the primary area. (b) Until the ICAO position is reviewed, the following standards are to be applied to GPS NPA missed approach design within the Australian FIR. The provisions of PANS-OPS Vol II Part III paragraph 7.2.2 may be used for straight missed approach segments. Secondary areas will not apply to turning missed approach procedures after the earliest turn point on the inner edge of the turn and the intersection of the extended secondary splay and the wind spiral on the outer edge of the turn. The aerodrome at which the runway is located must be a controlled aerodrome. Note: Aircraft operators will not be permitted to conduct SA Category I instrument approach operations unless aerodrome control is in operation. 8.1.14.3 Runway Eligibility. The relevant aeronautical telecommunications service and radio navigation service provider must have given the designer information that the runway has precision approach facilities suitable for SA Category I operations, including information about whether the precision approach aid is suitable for only HUD-equipped aircraft. 8.1.14.5 Instrument Approach Procedure. IALS means an intermediate ALS with: (a) a simple approach lighting system; or (b) a Category I lighting system; or (c) a Category II and III lighting system; (d) that is at least 420 m and less than 720 m long. BALS means a basic ALS that is at least 210 m and less than 420 m long. NALS means no approach lights, or an ALS that is less than 210 m long. 8.1.14.9 Instrument Approach Chart. Note: As detailed below, for an SA Category II approach procedure, the landing system and some ground facilities must meet all Category II requirements. However, Category II and III approach lighting, TDZ lighting and runway centreline lighting is not necessarily required. 8.1.15.2 Air Traffic Control. Note: Aircraft operators will not be permitted to conduct SA Category II instrument approach operations unless aerodrome control is in operation. 8.1.15.3 Runway Eligibility. The relevant aeronautical telecommunications service and radio navigation service provider must have given the designer information that the runway has precision approach facilities suitable for SA Category II operations. 8.1.15.5 Instrument Approach Procedure. The SA Category II DH minimum must be the higher of the following: (a) 100 ft; (b) the calculated OCH. 8.1.15.6 The RA and DA minima must be calculated directly from the calculated DH value without rounding. 8.1.15.7 The SA Category II RVR minima must be the longest of the following: (a) for a runway with TDZ lights and no runway centreline lights — 400 m; (b) for a runway with no TDZ lights and no runway centreline lights — 450 m; (c) the distance derived in accordance with Table 8?5, taking into account the type and length of the ALS, the aircraft category and the DH. In particular, it states that the LSALT determined shall be at least 1,000 ft above the highest obstacle located within the area concerned. 8.2.1.2 The purpose of this standard is to outline the rules and parameters to be used for the calculation of LSALT for IFR en-route operations. The particular issues addressed are: (a) effective areas; (b) charts; (c) altitude tolerances; (d) failure of radio navigation aids; (e) applicability. 8.2.2 Effective Areas 8.2.2.1 Route defined by Radio Navigation Aids or by Dead Reckoning. The area to be considered for the LSALT calculation for a particular route or route segment must be a 5 NM area surrounding and including the route navigation tolerance area. The maximum width of the route navigation tolerance area is 50 NM. For route or route segments served by VORs, the navigation aid coverage to be applied for the determination of the route navigation tolerance area must be the lesser of 60 NM or the maximum coverage published in ERSA. The effective areas for various circumstances are shown at paragraph 8. 2.5. 8.2.2.2 Operations with Area Navigation Systems (including GPS). However, whenever doubt exists concerning the accuracy of the information on the WAC, larger scale maps must be used. The RAAF Joint Operations Graphic (Air) Chart, at a scale of 1:250,000, is ideal for this purpose. 8.2.3.2 The terrain to be considered in the determination of the LSALT for any route segment must be: (a) when heights are shown on charts by spot heights and hachuring only—the highest spot height within the navigation tolerance area. (b) where heights are shown on charts as spot heights, contours and hypsometric tints—the highest spot height within the navigation tolerance area or, where there is no spot height, the highest terrain within the intruding contours. 8.2.3.3 As spot height information shown on charts may not necessarily indicate the highest terrain in that area, it is necessary to examine the contour information to ensure that no higher terrain exists that would control the LSALT. Further, whenever contour intervals are used to determine the highest terrain, then the highest terrain must be assumed to be at the level of the next higher contour. 8.2.3.4 Obstacles shown on Australian produced WACs are generally limited to those having a height of 360 ft (110 m) or more. Therefore, whenever these charts are used for the determination of LSALTs an obstacle allowance of 360 ft must be made. The procedure is prescribed for particular tracks or sectors and takes the form of a series of descending steps at appropriate distances. 8.3.1.2 The procedure normally uses a DME that is located close to the azimuth facility but in some cases use is made of a remote beacon. Procedures must be contained within the demonstrated coverage of the navigation aids used. Where more than one tracking aid exists at an aerodrome, tracking is normally permitted to either aid. However, only one GPS reference waypoint is nominated as the GPS distance source. In addition, steps are to be designed to maintain an aircraft in controlled airspace where this is applicable to the particular route. To account for control area steps, the step information is frequently extended beyond the initial approach fix (IAF) into the en-route segment. For instance, the steps should be so arranged that a steady descent will result, rather than a series of steps, which if followed by an aircraft, would require large variations in the rate of descent. Figure 8?20 shows an example of good design. In such cases a higher MDA may be necessary. In the calculation of obstacle heights, additional clearance should be made for chart error, mountainous terrain, vegetation and built-up areas. (f) Add to the identified obstacles the applicable MOC required by paragraph 8.3.3. (g) Plot the obstacles on a sheet of graph paper, after the determination of a suitable DME distance v Altitude scale. For this purpose 160 ft per NM is a satisfactory figure. ATP means approach termination point that is for a specialised helicopter operation that is to or from: (a) an off-shore installation; or (b) a point in space above the surface of the ocean used for operations connected with the off-shore installation. Note Specialised helicopter operation and off-shore installation are defined in the CASR Dictionary. CAR 1988 means the Civil Aviation Regulations 1988. CASR 1998 means Civil Aviation Safety Regulations 1998. GNSS means Global Navigation Satellite System. ISA means International Standard Atmosphere.Note Coastal land features include, for example, islets, shoals and cays. MAPt means missed approach point. MDA means minimum descent altitude. MDH means minimum descent height. MSA means minimum sector altitude. NM means nautical miles. OIP means offset initial point. TAS means true air speed. TIFP means a terminal instrument flight procedure as defined in the CASR Dictionary. VF means validation fix. Note Variations to approach designs occasioned by technological change may be presented to CASA and, in the light of aviation safety evaluation, may result in amendment of the MOS or the issue of appropriate instrument. 8.6.3 Airborne radar equipment and ground radar equipment 8.6.3.1 Airborne radar equipment. Distance, bearing and coordinate data must comply with the quality control requirements specified in Chapter 2 of Annex 11, and in Chapter 2 of Annex 14 — Aerodromes, Volume II, of the Convention on International Civil Aviation, published by ICAO. 8.6.6.6 Reduction of closest distance to nearest land to 15 NM. The following applies: (a) minimum obstacle clearance over obstacles and low terrain must be 1 000 ft; and (b) if the elevation of an obstacle or low terrain, including small structures on the obstacle or terrain, exceeds 500 ft AMSL, then the elevation must be added to the initial approach altitude. Note Vertical errors associated with mapping or a database must be included in the 500 ft obstacle clearance. 8.6.9.2 Obstacle clearance after the VF. Operators must adjust the calculations for actual conditions in accordance with paragraph (a), (b) or (c), whichever is the greater. 8.6.13 Determination of obstacle avoidance For paragraph 8.6.12.1 (c), the formula is in Appendix 3, Determination of obstacle avoidance, in this section. Note To determine obstacle avoidance, calculations in accordance with the formula in Appendix 3 must be undertaken by the TIFP designer, as part of the process of determining the visibility required for the TIFP. Results from the formula are compared with the visibility requirements in paragraphs 8.6.12.1 (a) and (b) to arrive at the correct applicable visibility. (Figure 8-27 is illustrative only.) 8.6.14 Missed approach point (MAPt) For a TIFP, the minimum distance from a radar defined MAPt to the reference target is the airborne radar’s near echo suppression range. 8.6.15 Administration CASA Head Office is responsible for issuing design authorisations in accordance with Part 173 of CASR 1998 and this MOS. Note The relevant CASA Area Office will normally be the first point of contact and will advise, review and otherwise assist applicants’ requests for approvals. Appendix 3 Determination of obstacle avoidance Note 1 See paragraph 8.6.12.1 (c) and paragraph 8.6.13. Note 2 Calculation of the minimum visual segment visibility is based on paragraph 157 (3) (b) of CAR 1988 to avoid obstacles by 300 m horizontally. The use of the specialised helicopter procedures is limited to CASA?approved operators only. The Manager provides operators with an approval for each TIFP, in accordance with Part 173 of CASR 1998 and this MOS. Helicopter procedures are dependent upon visual segment procedures developed by the operator in consultation with the procedure designer. Operational procedures must include key visual features, hazards, routes to be flown and action to be taken in the event that meteorological conditions deteriorate below specified requirements and any other conditions relating to the procedure. 8.8.3.2 The operating procedures are to be included in the Operations Manual of an operator approved to use the procedure. 8.8.4 Visual Approach Area—Helicopter 8.8.4.1 Helicopter procedures will normally be designed with a Visual Approach Area - Helicopter (VAA-H). 8.8.4.2 Procedures that do not provide a VAA-H are to be noted accordingly on the approach chart. 8.8.4.3 The VAA-H criteria are based on the establishment of key visual lead-in features to the HLS. In this respect, each procedure will be unique and requires an operational specification to be included in an operator’s operations manual. 8.8.4.4 The procedure designer must liaise with operators to define key lead-in features. 8.8.4.5 During validation, particular attention has to be considered for local operating procedures and key lead-in features. 8.8.4.6 This area is located between the MAPT and the HLS within which obstacle clearance at MDA is assured. 8.8.4.7 Operations within a VAA-H are visual flight manoeuvres. Its boundaries join at a tangent to a circle of 926 m radius centred on the HLS (see Figure 8-28). Figure 8-28: Visual approach area — helicopter 8.8.5.2 Length. The nominal length of the VAA-H is 3 km. The actual length is determined by the distance from the MAWP to the centre of the HLS. In any event, it should be such as to allow visual reference to be maintained with the HLS or key lead-in points. 8.8.6 Obstacle Clearance 8.8.6.1 A minimum obstacle clearance (MOC) of 90 m (295 ft) shall apply throughout the VAA-H. The principle of secondary areas does not apply. 8.8.7 Missed Approach 8.8.7.1 In addition to the standard missed approach analysis, a missed approach analysis for the VAA-H is also required. When considering these missed approaches, the obstacle distance (d oH ) is measured via the shortest distance from the boundary of the VAA-H or missed approach turn initiation area boundary (see Figure 8-29). Figure 8-29: Turning missed approach 8.8.7.2 Straight Missed Approach. The VAA-H sits within the protected area of the straight missed approach segment. Accordingly, no adjustments are required for the straight missed approach splay (see Figure 8-30). Figure 8-30: Straight missed approach 8.8.7.3 Turning Missed Approach. Depending on the turn angle, the VAA-H can extend beyond the protected area of the turning missed approach segment (see Figure 8-29) In this event, the turning missed approach area is extended on the outside of the turn by drawing a straight line from the outside edge of the splay at the nominal MAHWP or MATWP at a tangent to the 926 m radius arc around the HLS. Text in () should be inserted as shown eg. Prefix with S or E, as appropriate (eg. S38 21.5) ARP Latitude and Longitude in degrees and minutes to one decimal place. Prefix with S or E, as appropriate (eg. S38 06.9 E147 09.9) Derived or declared positions are suffixed with an asterisk. (ii) Elevations Threshold ELEV nn All other elevations Nn (c) Instrument Approach Charts (i) Plan Grid Degrees and minutes to one decimal place. Note the final and visual track should be a continuous line to 50 ft above threshold. Text Where a gradient is greater than 3.3 it must be repeated at the start of the text description of the procedure. REVISION HISTORY Note: The Revision History shows the most recent amendment first. Scroll down the table to view details of previous amendment information. Cover page Cover page and verso changed to introduce J.S. McMillan as the source of supply for the manual and to reflect version change. All Introduced new CASA logo. 1.0 February 2003 All First issue of MOS Part 173 NOTES TO MANUAL OF STANDARDS PART 17 3 Note 1 The Manual of Standards Part 173 (in force under the Civil Aviation Safety Regulations 1998 ) as shown in this compilation comprises Manual of Standards Part 173 amended as indicated in the Tables below. After subsection 8.1.6.2, (including Table 8-1) Inserted text and table. Subsection 8.1.7.2 Substituted text. After paragraph 8.1.7.2 (d) Inserted paragraph. 1.1 May 2003 All Reissued. To get the best experience using our site we recommend that you upgrade or switch browsers.Read our policy. The Legacy 450 is the 500’s little brother; sharing the same wing, engines, empennage and cockpit. Their only major differences are the 450’s reduced cabin size and fuel capacity. The 450 is 1.06m (3ft 6in) shorter than the 500, reducing passenger cabin length. Unlike shrinks of many aircraft, the 500 was not shortened by removing a few frames. In an effort to keep cabin windows aligned with interior seating areas, the 450’s mid fuselage is an entirely new design. Size is important, and the 450 has on ovoid cross section and flat floor that offers stand-up height (1.83m). At its widest point, the cabin is 2.08m wide, wider than any Cessna, but slightly narrower than the Challenger 350. The 450 offers a club seating area at mid-cabin, with one seat forward and two aft, while the 500 typically seats eight. The 450 shares many cabin elements with the 500, each having an aft lavatory with externally serviced vacuum commode. Just aft of the lavatory is an in-flight accessible 0.99m 3 (35.0ft 3 ) baggage area. In both the 450 and 500, club seating areas are fully breathable, offering lie-flat beds. The cabins come with a Honeywell Ovation Select cabin management system as standard.