This chapter shall include the necessary procedures to lift and shore aircraft in any of the conditions to which it may be subjected. Includes an explanation of the system of zoning and measurement used. Those charts, diagrams, and text which show the area, dimensions, stations, access doors / zoning and physical locations, of the major structural members of the aircraft. Includes inspections and checks such as hard landing, overweight landing, bird strike, turbulent air, lightning strike, slush ingestion, radioactive contamination, maintenance checks prior to engine-out ferry, etc. Those maintenance checks and inspections on the aircraft, its systems and units which are dictated by special or unusual conditions which are not related to the time limits specified in -10 above. Airlines desire the manufacturer's recommended time limits and scheduled maintenance checks but these should be provided in a separate document.
ATA CHAPTER 36 MANUAL
NOTE: Inclusion of the data described in -10 through -40 above, in any manual or manual publication is specifically prohibited unless required by government regulation. Reserved for use in those cases where the number of breakouts provided by the fourth digit of the -20 breakout is not sufficient to cover all of the maintenance checks dictated by subsystem -10 above. This section shall list in more detail the items which are outlined on the airline job forms (usually by title only), and shall cross -reference the detailed procedures included in the individual Maintenance Practices. Those manufacturer recommended maintenance checks and inspections of the aircraft, its systems and units dictated by the time limits specified in -10 above. For engine manufacturers this will include the flight cycle lives of major rotating components and other items designated critical.
Those manufacturer recommended time limits for inspections, maintenance and overhaul of the aircraft, its systems and units, and life of parts. Manufacturers' recommended time limits for inspections, maintenance checks and inspections (both scheduled and unscheduled). Includes dimensions and areas, lifting and shoring, leveling and weighing, towing and taxiing, parking and mooring, required placards, servicing. This is achieved by placing the wing at an angle of yaw which such that the component Mach number normal to its long axis be subsonic.AIRCRAFT PARTS MANUFACTURING ASSISTANCE (PMA)ġ0 PARKING, MOORING, STORAGE AND RETURN TO SERVICEġ8 VIBRATION AND NOISE ANALYSIS (HELICOPTER ONLY)ģ9 ELECTRICAL - ELECTRONIC PANELS AND MULTIPURPOSE COMPONENTSĥ1 STANDARD PRACTICES AND STRUCTURES - GENERALĦ0 STANDARD PRACTICES - PROPELLER / ROTORħ0 STANDARD PRACTICES - ENGINE 71 POWER PLANT - GENERAL 72 ENGINE 72(T) ENGINE - TURBINE / TURBOPROP, DUCTED FAN / UNDUCTED FAN 72(R) ENGINE - RECIPROCATING 73 ENGINE - FUEL AND CONTROL 74 IGNITION 75 BLEED AIR 76 ENGINE CONTROLS 77 ENGINE INDICATING 78 EXHAUST 79 OIL 80 STARTING 81 TURBINES (RECIPROCATING ENGINES) 82 WATER INJECTION 83 ACCESSORY GEAR BOXES (ENGINE DRIVEN) 84 PROPULSION AUGMENTATION 91 CHARTSĪTA DEFINITIONS OF AIRCRAFT GROUPS, SYSTEMS AND SUB-SYSTEMS Īdvantages And Disadvantages Of Aerodynamic Reynolds number for flow through the catalytic bed. friction coefficient calculated by Ergun and Hicks formula:
The four basic components of Rankine cycle are shown in figure 1 each component in the cycle is regarded as control v.Ĭatalytic Oxidation Of Benzene Case Study RIGIDITY IN SPACE – characteristic of a gyroscope that prevents its axis of rotation tilting as th. What Is A Sensitive Component In A Barometer That Measure Absolute Pressure Of The AirĪBSOLUTE PRESSURE – measured from zero pressure or vacuum. The event weight and balance form listed the stabilizer setting as 5.26 units, while the actual setting recorded on the DFDR was 5.94 at the start of the tak. There thermal and kinetic energy are converted into mechanical energ.Īdvantages And Disadvantages Of Air Transport The hot and rapidly expanding gases are directed aft through the turbine rotor assembly. Das, Wear assessment in biodiesel fuelled compression ignition engine, Journal of Engineering for Gas Turbines & Powe. The photo was taken after manufacturing of the electric motor part. 1 features the case study of the high-speed rotor. It has curved surfaces designed to give requ.Īir is a bit different than a fluid although it acts as though it were a fluid through an orifice, meaning that by compressing it tightly, one could compress.Ĭase Study Of Rotor And Touchdown Bearing Modelsįig. 1.1 What is aerofoil? Aerofoil is a large stucture which is attached to the airplane.
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