Faa 337 title major repair alteration airframe powerplant propeller or appliance edition date october 01 2006 orientation portrait unit of issue ea responsible office afs 350 comments.
Form 337 sheet metal repair example.
See title 14 cfr 43 9 part 43 appendix b and ac 43 9 1 or.
Vii thin sheet webs of beams.
2120 0020 major repair and alteration airframe powerplant propeller or appliance 05 21 1987 advisory circulars acs.
Forming at room temperature is known as cold forming.
The mailing address information resides in regulation far part 43 appendix b as.
X wing main ribs and compression members.
Referenced form 337 and proposed changes to be made.
The following instructions apply to items 1 through.
5 31 2018 electronic tracking number for faa use only instructions.
Faa form 337 10 06 major repair and alteration us department of transportation airframe powerplant propeller or appliance federal aviation administration omb no.
Types of shrinking and stretching tools used for aircraft metal structural repair.
Handout material ac 43 9 1e instructions for completing faa form 337 excerpt from faa order 6 8300 10 field approvals fsaw 98 03 fsaw 98 18 example of completed 337 copy of this presentation.
Instructions for completion of faa form 337 omb no.
Xi wing or tail surface brace struts.
Viii keel and chine members of boat hulls or floats.
Example form 337 field approval author.
Faa form 337 major repair alteration airframe powerplant prpeller appliance created date.
Print or type all entries.
Any bend formed on a.
The form is executed at least in duplicate and is used to record major repairs and major alterations made to an aircraft airframe powerplant propeller appliance or a component part thereof.
Aircraft technician relies on a wide variety of powered and hand operated tools to precisely bend and fold sheet metal to achieve the perfect shape.
Major repair and alteration of airframe powerplant propeller or appliance keywords.
Forming sheet metal requires a variety of tools and equipment both powered and manual.
Ix corrugated sheet compression members which act as flange material of wings or tail surfaces.
Faa form 337 major repair and alteration must be completed for repairs to the following parts of an airframe and repairs of the following types involving the strengthening reinforcing splicing and manufacturing of primary structural members or their replacement when replacement is by fabrication such as riveting or welding.