catia page16

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SIZES OF DRAWING: DRAWING BREAKDOWN 1.Part : A Single item which has no components other than itself (bracket, angle, plate, bush) 2.Assembly (Minor) / Sub assembly : Group of parts & standard parts assembled (Bracket Assy., Locking System, Lever Assy.) 3.Assembly (Major) : Group of parts / sub assemblies to form a major assembly with standard parts (Canopy Assy., Air-intake, Floor Assy., skin & stringer) 4.Installation : A group of assemblies which forms a major component which is directly installed on the aircraft. Should contain reference parts, stations, contour details, datum (Canopy instl., air-intake, wing etc.,) Drawing Procedures and Practices 25.02.2006 5.Standard Part : Generally used item manufactured as per approved standard. (Bolt, rivet, washer, nut, spring, pin)

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CATIA Page1

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SIZES OF DRAWING:

DRAWING BREAKDOWN1.Part : A Single item which has no components other than itself (bracket, angle, plate, bush)

2.Assembly (Minor) / Sub assembly : Group of parts & standard parts assembled (Bracket Assy., Locking System, Lever Assy.)

3.Assembly (Major) : Group of parts / sub assemblies to form a major assembly with standard parts (Canopy Assy., Air-intake, Floor Assy., skin & stringer)

4.Installation : A group of assemblies which forms a major component which is directly installed on the aircraft. Should contain reference parts, stations, contour details, datum (Canopy instl., air-intake, wing etc.,)

Drawing Procedures and Practices

25.02.2006

5.Standard Part : Generally used item manufactured as per approved standard. (Bolt, rivet, washer, nut, spring, pin)

6. Bought Out Item : Proprietary item purchased from a manufacture or supplier (LRUs, Ejection Seat, Valves, Heat Exchangers)

DRAWING NUMBERING PROCEDURERefer Fig.1

IDENTIFIABLE PART (S) (MANDATORY)The part failure may endanger the safety of an aircraft. Hence a greater control over the dimensions, machining, heat treatment process, and selection of material to be taken care.

The identifiable parts to be related back to their origin, i.e Source of material supply,Batch & year of production,Supplier and other details, etc.,

INTERCHANGEABILITY (MANDATORY)Component / assembly can be readily and easily exchanged for or replace a similar component / assy. on the same aircraft or another aircraft of same type and modelClass I:items that can be fitted straight away without any rework

Class II:with minor rework

Class III:not interchangeable at allNON-DESTRUCTIVE TESTING METHODS

Method used to determine the soundness of engineering materials / components without destroying them beyond their point of usefulness