(b)
Airborne contamination (e.g. dust, precipitation, paint particles, filings) should be kept to a minimum to ensure aircraft/components surfaces are not contaminated, if this is not possible all susceptible systems should be sealed until acceptable condi-tions are re-established.
(c)
Lighting should be adequate to ensure each inspection and maintenance task can be performed effectively.
(d)
Noise levels should not be allowed to rise to the level of distraction for inspection staff or if this is not possible inspection staff should be provided with personnel equipment to reduce excessive noise.
AMC M.A.402 (e) Performance of maintenance
Facilities should be provided appropriate for all planned maintenance. This may require aircraft hangars that are both available and large enough for the planned maintenance.
Aircraft component workshops should be large enough to accommodate the compo-nents that are planned to be maintained.
Protection from inclement weather means the hangar or component workshop struc-tures should be to a standard that prevents the ingress of rain, hail, ice, snow, wind and dust etc.
AMC M.A.403 (b) Aircraft defects
An assessment of both the cause and any potentially hazardous effect of any defect or combination of defects that could affect flight safety should be made in order to initiate any necessary further investigation and analysis necessary to identify the root cause of the defect.
AMC M.A.403 (d) Aircraft defects
All deferred defects should be made known to the pilot/flight crew, whenever possible, prior to their arrival at the aircraft.
Deferred defects should be transferred on to worksheets at the next appropriate main-tenance check, and any deferred defect which is not rectified during the maintenance check, should be re-entered on to a new deferred defect record sheet. The original date of the defect should be retained.
The necessary components or parts needed for the rectification of defects should be made available or ordered on a priority basis, and fitted at the earliest opportunity.
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ED 2008/013/R
AMC M.A.501 (a) Installation
1. To ensure a component is in a satisfactory condition, the person referred to under
M.A.801 or the approved maintenance organisation should perform checks and veri-fications.
2.
Performance of above checks and verifications should take place before the compo-nent is installed on the aircraft.
3.
The following list, though not exhaustive, contains typical checks to be performed:
(a)
verify the general condition of components and their packaging in relation to damages that could affect the integrity of the components;
(b)
verify that the shelf life of the component has not expired;
(c)
verify that items are received in the appropriate package in respect of the type of component: e.g. correct ATA 300 or electrostatic sensitive devices packaging, when necessary;
(d)
verify that component has all plugs and caps appropriately installed to prevent damage or internal contamination. Tape should not be used to cover electrical connections or fluid fittings/openings because adhesive residues can insulate electrical connections and contaminate hydraulic or fuel units.
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