CHAPTER 51
PAGE 31
MAINTENANCE MANUAL EXTRA 300/SC
PAGE DATE: 1. August 2014
51-70-05 Structural Repair of Steel Components
Restoration of a damaged fuselage to its original design
strength, shape and alignment involves careful evaluation of
the damage, followed by exacting workmenship in perform-
ing the repairs.
I M P O R T A N T Should structural repairs practicable on the aircraft
be necessary, refer to "Aircraft Inspection and Repair
FAA AC 43.13-1A" and "Aircraft Alterations Accept-
able Methods, Techniques and Practices FAA AC 43.13-
2A".
I M P O R T A N T Alterations or repair of the airplane must be accom-
plished by licensed personnel. Consult EXTRA-
FLUGZEUGPRODUKTIONS- UND VERTRIEBS-
GmbH in case of doubt about a repair not specifically
mentioned there.
N O T E If welding work must be performed, use only the TIG
procedure (Tungsten Inert Gas). Use steal welding wire
1.7734.2 for welding additive.
REPAIRS
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