MAINTENANCE CONTROL MANUAL                                                                  NAC 228
PART 127                                                    Part 1.7.1
                                             DEFECT REPORTS
                                            (CAR PART 43.02.4)
1.   SCHEDULED MAINTENANCE
     Defects that are identified during any maintenance or inspection of an Aircraft or component as a result
     of a work pack/task card, shall be recorded on a TFU, and will form part of the issued work pack.
     This shall be depicted on an Index of the particular work pack.
2.   PROCEDURE FOR DEFERMENT AND RECORDING OF DEFECTS. (SA-
     CATS-GMR, PART 43.02.3 & AIC 60.14 06-07-07 REQUIREMENT ‘J’)
     2.1.Deferred Defects Policy
             All aircraft flight folios are to be actioned at all stations prior to continuation of flights.
             Transfer of items to the “Deferred Defects Check List” are only to be made when rectification action
             cannot be accomplished due to technical reasons, lack of spares or because the flight schedule is
             to be maintained, under consideration of the MEL and DDPM/CDL. Open reports are transferred
             solely by the responsible Manager of his authorized designates in the following manner: DEFER
             DEFECT SHEETS
             2.1.1.   Confirmation of the defect and the reason for deferment shall be entered together with the
                      MEL and DDPM/CDL reference and category type plus expiry date in the action block
                      of the relevant flight folio. The entry must start with the wording “DEFERRED DEFECT”.
                      Refer to check item if arising from hanger maintenance.
             2.1.2.   Remove original (white) slip with the yellow copies. Place a coloured sticker next to the
                      affected system i.e. switch, gauge, light etc. On the sticker write the MEL/DDPM/CDL
                      Authority
                      number and flight folio reference of the inoperative condition. This will alert the crew to the
                      Deferred item.
             2.1.3.   Enter the Flight sequential number the MEL reference and category and expiry date
                      plus Limitations as well as a short description of the defect onto the deferred defect check
                      list. Stamp for authorization (Only designates may stamp for authorization).
                      The following persons shall be advised of any deferred defects prior to aircraft dispatch:
                      A.     NAC Person Responsible Aircraft.
                      B.     Aircrew informed prior to A/C Acceptance
             2.1.4.   The Contracted AMO to capture and file defer defect from the flight folio.
                      All are responsible for reworking of deferred defects in a timely manner. On subsequent
                      clearance of deferred defect the following action shall be taken by the relevant Crew
                      Chief, Flight Line or Hanger Maintenance.
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                  MAINTENANCE CONTROL MANUAL                                                               NAC 228
                                                 PART 127                                                  Part 1.7.1
             2.1.5.    On the next available blank Flight Folio, cross refer to the original deferred defect
                       slip in the cross reference block, entering the original Flight Folio sequence number.
             2.1.6.    The Flight Folio sequence number along with the date repaired and authority stamp shall
                       entered onto the deferred check list under the appropriate column.
             2.1.7.    Remove and destroy the alerting sticker.
3.   CONTROL DEFERRED DEFECTS.
     All defects should, where practicable, be rectified as soon as they are entered in the Flight Folio. However,
     due to operational reasons, certain defects may be deferred until a later date, if time, spares or resources
     prevent their immediate rectification. In this case, defects shall be deferred as per Minimum Equipment List.
     Aircraft defects are classified as “A”, “B”, “C” or “D” defects – (Minimum Equipment List MEL refers.)
     If a defect cannot be actioned/rectified in the specified time frame a one time extension of the rectification
     interval CAT B or C for the same duration as specified in the MEL may be granted. This MEL extension
     application will be recorded and retained on record.
     3.1Category “A”
             “A” defects usually require immediate rectification. They are normally of an airworthiness nature
             outside the scope of the Minimum Equipment List or the Structural Repair Manual for example and
             are not capable of being carried forward. Where practicable be rectified immediately, if not, it must be
             rectified at next Base stop.
     3.2     Category “B”
             “B” defects should, where practicable, be rectified immediately. They may be of an airworthiness
             nature; however, they are less serious than “A” defects and can be identified within the Minimum
             Equipment List, Aircraft Maintenance Manual, or Structural Repair Manual, they may be deferred for
             3 consecutive calendar days (72 hours). Such deferments must be made in accordance with
             approved data, i.e. Flight Manual or Minimum Equipment List. Rectification of “B” defects should
             take place at the earliest opportunity.
     3.3     Category “C”
             “C” defects are defects with no airworthiness implications or limitations via the Minimum Equipment
             List, Maintenance Manual or Structural Repair Manual. “C” defects may be deferred until
             rectification is practicable. Items in this category shall be repaired within ten (10) consecutive
             calendar days (240 hours)excluding the day the malfunction was recorded in the Flight Folio.
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                 MAINTENANCE CONTROL MANUAL                                                                 NAC 228
                                                 PART 127                                                  Part 1.7.1
     3.4     Category “D”
             “D” Defects are defects with no Airworthiness implications or limitations via the Minimum Equipment List,
             Maintenance Manual or Structural Repair Manual. “D” Defects may be deferred until rectification is
             practicable. Items in this category shall be repaired within one hundred and twenty
             (120) consecutive calendar days (2880 hours) excluding the day the malfunction was recorded in
             the Flight Folio.
4.   ANALYSIS
     Flight Folio pages must be examined at regular intervals by the Contracted AMO to provide information
     concerning defects occurring, Pilot's reports, maintenance actions and defects of a repetitive nature.
     Maintenance input records (work-packs) will also be reviewed for significant findings by the Contracted AMO
     which may have airworthiness or operational implications.
     The Person Responsible Aircraft will assess the findings as necessary and has to agree to any action
     required before implementation. Implementation may take the form of a Maintenance Programme
     amendment or modification action.
5.   LIAISON WITH MANUFACTURERS
     The Person Responsible Aircraft shall ensure that all major defects that can adversely effect the
     airworthiness of the Aircraft, be communicated to the Manufacturer.
6.   NON DEFERRABLE DEFECTS POLICY
     Non deferrable defects must be repaired before further flight. If defects are not covered by approved data the
     Type Certificate Holder has to be involved. Alternately an exemption application is to be submitted to the SA
     CAA.
7.   REPETITIVE DEFECTS
     The Flight Folio is monitored by the Person Responsible Aircraft to identify these defects as and
     when they arise. Remedial action will be taken by the Contracted AMO in consultation with the Person
     Responsible Aircraft.
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            MAINTENANCE CONTROL MANUAL                                  NAC 228
                                   PART 127                             Part 1.7.1
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