@Berkshire
The authority asked us to develop a general (Part 23, 25, 27 & 29) procedure on how to develop the inspection limits and intervals for modification/repair (minor).
For an example: installation of an antenna on the fuselage (part 27) of the rotorcraft. We put 'on condition' for the...
I am required to develop a procedure on how to develop the inspection limits and intervals for modifications/repair (minor).
Are there any references that I can refer to? Our current practice is 'ON CONDITION' for the intervals unless there is an instruction from the equipment manual to comply...
Thank you all for the reply.
But the examples that I states earlier are not Major repair and does not involves the primary structures therefore I don't think it should complies with para .571 (the aircraft is unpressurized) and .572.
Or should I make an assumption that any repairs that does...
The repair is not done according to the SRM but thru the approval of DOA. The aircraft types are more specifically on PART 23, 27 and 29 (e.g AS350, EC120, AW139 etc).
Examples of minor repair performed:
Aft Fuselage Upper Panel delaminated - repaired by removing the delaminated area and...
