P2012 TRAVELLER - Tecnam España
P2012 TRAVELLERInnovation in aviation
P2012 TRAVELLERIntroductionThe piston powered twin engine aircraftmarket is today characterized by very fewmodels and the majority of aircraft in operation belonging to this category are olderthan 35 years and are no longer in production. Tecnam Aircraft Industries is committed to the design, development and production of a new, innovative, efficient andaffordable next-generation 11 seater twinaircraft, complying with both FAR part 23and EASA CS-23 requirements.The airplane design, named Tecnam P2012Traveller, was developed by Tecnam Research and Design team is under development at Tecnam Aircraft Industries followinga preliminary design by Professor Luigi Pascale, Tecnam’s well renowned and award1070 nmMax Range190 ktasMax Cruise Speedwinning expert in the design of many generalaviation aircraft.The Tecnam P2012 Traveller will first seeservice as a passenger aeroplane with USbased Cape Air but has been designedfrom the start to be a very versatile andflexible aerial platform, offering many multirole opportunities including Hydro, VIP,cargo shipping, parachuting and medevacservices.The key features of the aircraft have beendeveloped in close co-operation with potential customers.11 seats9 Passengers 1-2 crew1350 kg (lbs 2976)Useful LoadDesigned primarily with the passenger inmind, the P2012’s large cabin can accommodate up to 11 seats (with a maximumof nine passengers).Easy cabin access, cabin comfort and spacious luggage compartments have all beenspecifically designed to ensure a pleasurable flight experience.The aircraft will be equipped with twopowered Lycoming TEO-540-C1A enginesrated 375hp each. This modern engine isfully electronically controlled, fuel injectedand provided with several features to pre-Low in servicecostsEasymaintenanceserve component life in addition to savingfuel. The mixture lever is no longer presenton the cockpit pedestal since the entirecontrol of mixture is made automatically.The P2012 has been designed to complywith both FAR Part 23 and EASA CS-23,for which certification will be achieved atthe same time, in order to expedite asmany country validations as possible.Single or dualpilotState of artdesign
Market analysisThe Part 135 dedicated aircraft market istoday based on old ‘heritage’ models, manyof which are coming to the end of their usefulcommercial life.The arrival into service of the next-generation11 seat P2012 Traveller has been much anticipated by many airlines, who have beendemanding a replacement for the many hundreds of ‘heritage’ aeroplanes in theFAR23/CS23 category currently in servicearound the world.Airlines have been demanding a replacementfor many hundreds of airplanes in the Part23/CS23 category currently in service aroundthe world - as many are now coming to theend of their useful commercial life.The main rationale behind the design, development and introduction of the P2012Traveller is to ensure that not only passenger’s demand for comfort and safety aremet, but also that potential operators of theP2012 Traveller are now able to afford anairplane with significantly improved direct operating costs, more efficient and modernmaintenance procedures and appreciationfor ensuring that the industry takes into account global environmental considerationssuch as the need for lower fuel burn andless noise emissions. As shown in the table,all the aircraft within the 8-11 seats segmentwere introduced more than 45 years agoand many are still in commercial service usetoday, flying with an average age of 50 years!With a forecast of an annual reduction ofonly 0.1% flight hours for the next 20 years1,the need of a modern and far more efficientaircraft is self-evident. It is noticeable thatalmost all aircraft listed in the table are characterized by a twin-engine arrangement, withthe Caravan as the only single-engine aircraft in this category that has had commercial success. However in most countriescommercial passenger transportation witha single engine aircraft is forbidden.One of the essential features potential operators have also requested for this nextgeneration aircraft is to have short take-offcapability, enabling them to operate on veryshort or even non-prepared runways. TheP2012 has been designed to have a verylow minimum control speed and this resultsin a take-off distance of about 1970 ft overthe obstacle. The following table shows thetechnical comparison between the TecnamP2012 Traveller and its direct competitors(including aircraft no longer in production).GAMA data: Actually in US more than 1.100 piston airplanes operate as Passengers Carrying Platforms. Theyhave now an average age of 45 years and within 20years they will be 65 years old.1
Comparisonand handlingModel Spec. chart - volumes[unit]C402Service EntryWing 910,42Cabin heightm1.27Cabin lengthm4.98HeightCabin widthLanding gearmmEngine manufacturerEngine Model3.491.421967B2NP2012 etr.FixedTricycle Retr.Tricycle FixedTricycle eyHartzellMcCauleyHartzellMT-PropContin.mMax gross weightkg31073286294829943600Useful loadkg1262160095811281350Fuel capacitylt7801211708492800Std. empty weightSeating capacity (pax)kgWing loadinglb/sqftSpeed, VNEPower loading18459170892.031990728.352x300LycomingProp. diameter2.442x310Lycominghp2.251x750LycomingEngine PowerPropeller 183240Cruise speed 75%kt190 (FL 100)151 (FL 120)180 (FL 100)139 (SL)190 (FL 100)Stall sp. landingkt7160634060Min control speedBest RoCRange - Max (FL100, 75%)Takeoff distanceLanding 7579981430Na748601500371600850503 (FL?)554299907500
Single Pilot vs Dual PilotOne of the main advantages of the P2012Traveller is the option to operate in singlepilot mode in most countries around the worldwhen carrying passengers.While under FAA requirements it is possibleto carry commercial passengers on a singleengine aircraft, such as the Caravan. In mostof countries this is not allowed.This means that, in order to carry passengersfor hire or commercial gain the aircraft mustbe at least multi engined. Nevertheless, anaircraft powered by two turboprop engines isclassified as "complex" and thus it requiresthe presence of a co-pilot. This dual pilot requirement significantly increases the overalloperating cost. Not only is it a question offunding an additional pilot but primarily as aresult for the need for a "dual pilot" cockpitconfiguration results in the need for perfectsymmetry of all the functions and displays,most of them simply doubled!The most economical solution to performingpassengers transport especially over smalldistances is via a twin engine, single pilot operation with a capable, modern and efficientpiston aircraft such as the Tecnam P2012Traveller.The P2012 cockpit design, in addition to theprovision of workload reducing equipmentsuch as the state-of-art autopilot, will significantly improve the pilot's work station andlower stress during long IFR flights.
Sizing and configurationThe sizing and overall dimensions of theP2012 has been achieved through the useof classical fine methodologies and approach.The design of the aircraft has been accomplished starting from the following designspecifications:a) Ease of cabin access and cabin comfort;Cabin seatspitch and measurein metresb) Spacious luggage compartments (noseand tail located);c) Reduced take nt for thewhole length of the fuselage extension asopposed to ‘legacy’ aircraft in this classwhich traditionally feature a tapered fuselage in the back portion, there providing lessspace and especially disadvantaging passengers seated in the rear rows TecnamP2012 has the advantage of having a cabinwhose measures are constant for its wholeextension, so that the ergonomy remainsthe same for all passengers and seats.The conclusion is that advantages of theP2012 configuration include: P2012 offers additional 0.26ft (80mm)for overhead space compared with itscompetitors; P2012 offers additional 0.15ft (46mm) ofcabin width; P2012 offers a seats pitch of 32in(0.813m).The access to the cabin is enabled via threedoors, two for flight crew and one in the rearside divided in 3 separate hatches for pas-Following pictures show the ventilation layoutand a preliminary interior configuration.Doors dimensionHigh densityCabin ventilation schematicsenger’s access only or for cargo/baggageloading purposes. An integrated handrail allowsa comfortable entrance and exit.
Interior configurationsExecutiveCargoAir AmbulanceTypical arrangement of interiorParachuteInterior configurationsRear fuselage opening and step
Volumes and handlingBaggage area (w/o cabin)Cabinvolume (w/o baggage area) from pilot seat shoulderto baggage area wallCargo ground handling Pax boardingPropellerTecnam P20121.68 m³ (rear) - 0.52 m³ (nose)TOTAL 2.2 m³6.8 m³High wing, no wing strut presence,low cabin floor height from groundFar from groundRemarksP2012 has the bestvolume for baggageP2012 has the largest cabin volumefor passengersP2012 has the best configurationfor ground operations and handlingWith prop discs far from ground,P2012 lowers the risks of propellers damage
Large cargo load - Fast technical support
Weights and Performance tableWeightsBASIC EMPTY WEIGHT STANDARD2250 kg4960 lbsOPERATIONAL EMPTY WEIGHT (single pilot luggage)2350 kg5181 lbsMAX LANDING WEIGHT3600 kg7937 lbsMTOWRAMP WEIGHTZERO FUEL WEIGHT (9 passengers single pilot luggage)3600 kg3620 kg7672 lbs4.8 kg/hp10.6 lbs/hp142 kg/mFUEL CAPACITY800 ltPerformanceMAX CRUISE SPEED (KTAS)7981 lbs3480 kgWING LOADINGPOWER LOADING7937 lbs29 lbs/ft212 US Gal190 kts@ 10.000 ftSTALL SPEED (T.O. configuration)65 kts120 km/hVMC74 kts137 km/hSTALL SPEED (full flap)RATE OF CLIMBRATE OF CLIMB (single engine)60 ktsTAKE OFF DISTANCE (50ft obs)1970 ftTAKE OFF RUN1150 ftLANDING DISTANCE (50ft obs)LANDING RUN1640 ft820 ft111 km/h1500 ft/min300 ft/min600 m500 m350 m250 m
PowerplantThe Lycoming TEO-540-C1A Engine is a direct-drive six-cylinder, horizontally opposed,turbocharged, air-cooled engine. It has electronic fuel injection, electronic ignition, downexhaust. As equipment, the engine has an automotive type starter, one 28V alternator(140A) and a propeller governor pad.The EECS (Electronic Engine Control) is anelectronic, microprocessor controlled systemthat which continuously monitors and adjustsignition timing, fuel injection timing, and fuelmixture based on operating conditions. TheLycoming TEO-540-C1AEECS eliminates the need for magnetos andmanual fuel/air mixture control lever.The main advantages and features of the Lycoming TEO-540-C1A engine are listed in thetable below: as shown, include the P2012’sadvantage on fuel consumption, as well asthe active engine protection it affords againstknock, overboost and temperatures willthereby guarantee a trouble free engine life,compared with any other old generation, turbocharged engines.Comparison chart - volumes and handlingTEO-540 -C1ATIO-540-J2BFuel (Min Octane)100/130, 100LL and UL100100/130, or 100LLTime limited takeoffratingAnticipated in SoftwareN.A.Alternator1 x Alternator – 28 Volt, 140 AmpMax 28 Volt, 70 AmpDiagnosticsNotification of Shorted/OpenSensor orActuatorsN.A.Only 2 Control Levers per engine(PWR, PROP)Single Button Start3 Control Leversper engineManual StartFuelScheduling/MappingEngine ProtectionfeaturesPilot InterfaceChangeable in SoftwareKnock Control(independent for each cylinder)CHT, TIT over temp protection- Overspeed protection- Overboost protectionOut-of Range FailuresIn-Range Errors from sensor(Cross Checks)All faults are logged in the ECU memoryService Fault HistoryRecord since last clearing byan authorized service toolRecord of ’’Fault clearing History’’Lycoming TEO-540 Vs TIO-540 main features comparisonN.A.N.A.
Weights and Performances tableThe illustration here show two typical conditions and related flight profiles: the first oneis related to the endurance at 5.000’ over a200nm flight including IFR reserve and with150 kTAS 30.0USG/h2136 Ib170 kTAS 41.0USG/h2114 Ib160 kTAS 35.5180 kTAS 47.6USG/hUSG/hfull FIKI capability. The second one represents the 99min flight (90min enroute) atseveral airspeed (kTAS) each one with thecorrespondent payload and range.5,000 ft 99 min flight90 min enrouteincl. IFR reserve & Full TKS5,000 ft 200 min flightincl. IFR reserve & Full TKS2137 Ib2068 IbTested PerformanceP2012 - 3600 kg standard conditions sea level80 min75 min71 min67 min150 kTAS 30.0160 kTAS 35.5170 kTAS 41.0180 kTAS 47.6270 nm / 90 min255 nm / 90 min240 nm / 90 min225 nm / 90 min2106 IbUSG/h 2052 IbUSG/h 1997 IbUSG/hUSG/h1930 IbTake-Off up to 50 ftRate of Climb Clean:1500 ft/minTake-Off Ground RollRate of Climb OEI* Clean:300 ft/minOEI* One Engine Inoperative350 m - 1148.29 ft600 m - 1968,5 ft
Landing from 50 ft to touch downLanding Distance (total)250 m - 820 ft500 m - 1640,42 ft
Standard avionic packageThe P2012 Traveller is designed around aflexible, intuitive and low pilot workloadwith roomy and comfortable access for asecond pilot when required.NOTE: some optional equipment (such as theADF) may be mandatory in some countriesto enable the P2012 to fly under IFR conditions as an airline passenger transport.The avionics suite is based on the latestgeneration Garmin G1000 Nxi, composedof two 10 inch PFDs and a single central12 inchMFD. Remote redundant AHRS andADC (inertial and air data units) providethe main flight and attitude informationwhilst a backup is provided by a small,vertical layout MD-302 (Mid-Continent).Communications and navigation are basedon dual remote units which provide selectable data on the cockpit screens. An optionally provided Flight Management System keyboard allows immediate andcomfortable insertion of frequencies andwaypoints, while another optionally provided Garmin Flight Stream device allowsan immediate and wireless link betweenflight suite and portable devices such astablets or smartphones for immediate introduction of flight plans, waypoints, routes,frequencies etc.A remote unit transponder, mode-S, is provided as standard with ADS-B OUT, ADS-BIN, FIS-B to match the incoming future Gen-eral Aviation requirements for navigationand traffic awareness.Dual heated pitot probes, one providedwith AoA indication output, is also providedas standard to enhance the flight safety inall phases, supporting flight especially during single pilot operations.A single, latest generation Garmin GMA350C audio panel, manages the ATC andinternal communications with several facilities such as 3D audio and separationCockpit layoutof pilot/co-pilot communication channels(split function). The standard avionics suiteis then completed by the latest generationGarmin Automatic Flight Control System,with three axis of operations and providedby yaw damper (selectable also when A/Pis OFF). A/P mode controller, installed onthe top of flight deck, allows immediateinteraction via dedicated pushbuttons androtary wheels. Engines monitoring is fullyintegrated inside the avionics suite screensand allows a perfect management of power,with significant and revolutionary features:fully automatic mixture control, absence ofrelated lever and always guarantees thebest fuel/air ratio for every single cylinder.NOTE:refer to the following chapters for thelist of standard and optional equipmentavailable.
Standard P2012 Traveller EquipmentStandard avionic and flight instruments packageThe following table describes the standard avionics package in terms of units, theirquantity and main features descriptionUnitPFD LHQ.ty Description1PFD RH1MFD D30221Primary Flight Display, Pilot In Command side (LH), shows the main flight andnavigation data - dimension of screen is 10 inches. Annunciator lights andalarms are also displayed on PFD displayPrimary Flight Display, co-pilot side (RH), shows the main flight and navigationdata - dimension of screen is 10 inches. Annunciator lights and alarms are alsodisplayed on PFD displayMulti Function Display - installed between LH and RH PFDs, provides via multiplepages menu information concerning: aircraft position and map (GPS), navigationand communication set frequencies, engines monitoring, fuel quantity, fuel flowand range management, electric busses power management and power sourcesmonitoring, flaps position, flight time and total time and many other useful dataRemote units, allow the management of dual channels communication and navigation frequencies, each one with standby frequency selection and frequencymonitoring via PFD1, PFD2 and MFDDME – KN631Audio Panel1Pitot Probes2Transponder1AFCS1EIU2ELT1OAT probes2Remote units, provide attitude information with redundancy to PFDRemote units, provide air data information with redundancy to PFD. Calibrationcurve to display IAS-CAS-TAS is loaded in the PFD in order to provide “correctionfree” speedsRemote units, provide compass indication to PFDs. Their remote location allowsinterference free reading of magnetic headingCentral mounted, provides an additional reading of magnetic headingBack up instrument, provides the redundancy on primary flight and airspeeddata. It is normally powered by aircraft busses, emergency bus and it has an in-ternal battery to be used in extremely remote event of complete power loss(loss of both alternators and batteriesGarmin integrated DMEProvide the OAT value, also used by PFDs to reduce altitude and speed dataproviding correct reading of TASCentrally mounted, it is a last technology audio management system made byGarmin (GMA 350c), featuring the “3D” audio function, COM1/2 SPLIT to enablepilot talking with COM1 and co-pilot communicating on COM2 frequency contemporarily. It is also provided by marker beacons overfly indication lampsBoth heated, allow safe information of airspeed even during IFR operation. Oneof them outputs Angle of Attack data, factory calibrated, for safe attitude andspeed management in all phases of flightSingle unit, remotely mounted, features Mode-S xtr, ADS-B OUT/IN, FIS-B providingstate-of-art capabilities and being ready for incoming requirements on air trafficmanagementGarmin made, state-of-art automatic flight control system with separate modecontroller panel (GMC 710) provides the best solution for automatically controllingthe aircraft during almost all flight phases, dramatically reducing the pilot’sworkload and allowing single pilot operation where its presence is mandatory tocarry passengers for hire. All three axis are managed by A/P, with rudder servothat can be used also with A/P OFF as yaw damper. HDG, APR, NAV, ALT, VS andmany other functions, such as a complete following a flight plan (includingvertical navigation) are its main featuresThe engines interface units allow the engine data to be monitored in Garminsuite. 2x GEA71B fully redundant units are installed as standardRemotely mounted, with emergency antenna outside the aircraft skin, the ELT isprovided by a remote control switch on the pilot’s cockpit side
Standard P2012 Traveller EquipmentFlight ControlsThe following table shows and describes the main features of flight controls.ControlBrakesControl wheelRudder pedalsControl locksTrim controlsPower controlsFlapsDescriptionToe operated, braking system features 4 independent master cylinders andremote reservoir for easy access and refilling practices. Braking system isfully hydraulic while wheels and brakes are manufactured by Cleveland.Parking brake valve control is located on cockpit bottom pedestalTwo control yokes are installed on pilot and co-pilot sides, featuring chartsholders and several switches to control: MIC, A/P disconnect, A/P CWS,pitch trimProvided on both LH and RH sides with independent rudder and brakingcontrolsProvided for all surfaces, allows protection of control systems against windgusts while aircraft is parkedStandard provided on pitch, rudder and aileron, they are all electrically operated with dedicated switch, emergency disconnect and indicatorsCentral pedestal provided with: LH and RH engine PWR lever; LH and RH prop levers. Props are full feathering delete; Alternate air source control (LH and RH)Electrically controlled and monitored wing flaps with 3-position switch andflap overspeed annunciation inside PFDs for T/O position, tooElectrical Power and lightsThe P2012 electrical system is based on 24Vdc busses. The primary electrical powersource is provided by LH and RH engine driven alternators rated of 140A each. Thesecondary power source is provided by three batteries listed below:a. One Main battery (27Ah)b. One LH ECU battery (16Ah)c. One RH ECU battery (16Ah)The batteries can operate individually or in combination in order to provide power tothe loads on the distribution busses to start the engines. They also act as a reserve ofpower in emergency conditions (dual alternator failure). When the engines are runningthe alternators supply the power required in order to keep the batteries charged.The system features four distribution buses, namely Main bus, Essential bus, LH bus,RH bus. Dedicated switches allow the selection of active/inactive busses. Essentialbus is fed from 4 points and includes main electrical loads.Electrical circuits other than engine starters are connected to the buses via circuitbreakers, all located on cockpit overhead dedicated panel, easy to check, maintainand service. Switches are installed in order to allow the pilot the control of loads,where required.An external power socket allows ground operations and is located on rear fuselage,adequately protected and far from propeller disc areas.
Exterior lightsAll P2012 exterior lights are LED type, state-of-art technology featuring extremely longlife, high illumination power and low electric consumption, including during the pre-enginestart checklist. Lights provided as standard are listed in the table below:Light/functionDescriptionLND LightFull LEDNAV LightFull LED, integrated with StrobeTAXI LightSTROBE LightPOSITION LightCourtesy LightsFull LEDFull LED, integrated with NAV LightsFull LED, tail mounted single lightFull LED, illuminates passenger entrance areasInterior lightsAll P2012 interior lights are LED type, state-of-art technology featuring extreme longlife, high illumination power and low electric consumption. They provide a comfortableand efficient illumination of cockpit area, controls and passenger seats:Light/functionINSTR LightMap LightOverhead COCKPITPAX LightOverhead CABINDescriptionIlluminates the cockpit panel and all the panel mounted instruments, providing dimming features for night flightsProvides a source of illumination to be used to consult POH,charts or DocumentsCourtesy lamp, provide illumination of cockpit lining and related controls/monitoring equipment such as fuel selectors,breakers and switchesOne for each seat (9 in total), they are independently controlled and swivelling upon passenger needsCourtesy lamps, provide illumination of cabin volume fornight boarding procedures
Standard P2012 Traveller EquipmentEnvironmentalThe P2012 environmental management features a standard heating and ventilationsystem. All aircraft will be manufactured with provisions and pre-installation of supportingracks for palletized and easy to remove air conditioning system. This will ensure an 27efficient management of payload depending on the operation area and period, leavingon ground those items not requested for a certain period of flight operations. Air Conditioning system is optionally provided.The following table shows the list of main environmental and air management systemsprovided as standard roofingDescriptionHeating air is generated by a combustion heater, which provideshot air to passengers and pilot compartment. Hot air lines routingis easy to access via the removal of lower cabin lexan fairings.ON/OFF and heating power controls are on cockpit panel, air management section, while each passenger has the possibility toopen/close/swivel his own ventDefroster flow picks up air from combustion heaterStandard P2012 equipment features a fresh air system management. Ventilation system can be easily connected to an optionallyprovided, palletised air conditioning unitLatest technology panels, together with sealing of all structuralitems and dedicated studies on cabin noise when subject to typicalnoise frequencies guarantee an adequate comfort to passengerswhile seated in P2012.Interior - standard airline packageThe following table shows the list of cabin interior features provided as standard package for airline public transport.ItemChart holderBeverage cupholdersRear BaggagepartitionSafety beltsPilot(s) seatsSunvisorsPassengerseatsCharging devicesDescriptionLocated on both control yokes, provide a clip-made retaining device for charts and checklists. In addition to the dedicated POHholder pocket, they improve the pilot(s) work placeUseful provision for all seatsThe wall is made, together with the retaining nets, to separatethe baggage volume from passengers. As described in the previous chapters, rear door features a dedicated opening to extendthe direct access to both cabin and rear baggage areaAll restraint systems are made by 3 point safety belts, easy touse and car-style to offer an user friendly connectionPilot and co-pilot seats are adjustable along their longitudinal position, vertically (through electric motor and dedicated switch)Pilots have two sunvisors adjustable and folding which, togetherwith the deep cockpit upper cover, optimise navigation and approaches with sun aheadPassengers seats are fixed and provided with foldin
Engine manufacturer Contin. PW Lycoming Lycoming Lycoming Engine Model TSIO520VB PT6A-34 TIO-540A IO-540 TEO540C1A Engine Power hp 2x325 1x750 2x310 2x300 2x375 Propeller manufacturer McCauley Hartzell McCauley Hartzell MT-Prop Prop. diameter m 2.25 2.44 2.
With the 11 seater P2012 Traveller, Tecnam welcomes a . and coast Guard/Border control sea units. . The P92 JS is a two-seater, side by side, single strut braced high wing aircraft. Its outstanding perfo
Earlier this year, Future Foundation authored a report detailing 'Who' travel providers will need to serve and market to in the next fifteen years: Future Traveller Tribes 2030: Understanding tomorrow's traveller. Future Foundation's research identified six Traveller Tribes that will shape global travel in 2030: Simplicity Searchers; Reward
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SPECIFICATION!!DESCRIPTION!!&!!PRICE!!!!Pag.! !1" www.tecnam.com*! TECNAM P92 EAGLET Specification,!Description!&!Price!!!!! INDROD UCTION This!document!applies!only .
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The state-of-the-art Tecnam P TwentyTen is the most advanced high-wing modern single-engine aircraft in the marketplace, today with Continental CD-170 . The P2010TDI is where performance and comfort meet in one sexy IFR package. 4 seats. 3 passenger doors. 1 baggage door. Continental CD-170. Metal wings, landing gear and stabilator .
Embed issues of equality and diversity throughout the school, particularly ensuring a curriculum that is relevant and accessible to Gypsy, Roma and Traveller pupils. Provide a relevant, appropriate, enjoyable and inclusive school experience for Gypsy, Roma and Traveller pupils and their parents.
possibility of a leak from a storage tank? MANAGING RISK This starts with the design and build of the storage tank. International codes are available, for example API 650, which give guidance on the matter. The following is an extract from that standard: 1.1.1 This standard covers material, design, fabrication, erection, and testing
