Federal Aviation Administration, DOT

Pt. 43, App. B

spaschal on DSK3GDR082PROD with CFR

burner is designated as interchangeable in
the balloon type certificate data and the baskets and burners are specifically designed for
quick removal and installation.
(28) The installations of anti-misfueling devices to reduce the diameter of fuel tank
filler openings provided the specific device
has been made a part of the aircraft type
certificiate data by the aircraft manufacturer, the aircraft manufacturer has provided FAA-approved instructions for installation of the specific device, and installation
does not involve the disassembly of the existing tank filler opening.
(29) Removing, checking, and replacing
magnetic chip detectors.
(30) The inspection and maintenance tasks
prescribed and specifically identified as preventive maintenance in a primary category
aircraft type certificate or supplemental
type certificate holder-s approved special inspection and preventive maintenance program when accomplished on a primary category aircraft provided:
(i) They are performed by the holder of at
least a private pilot certificate issued under
part 61 who is the registered owner (including co-owners) of the affected aircraft and
who holds a certificate of competency for the
affected aircraft (1) issued by a school approved under Section 147.21(e) of this chapter; (2)
issued by the holder of the production certificate for that primary category aircraft
that has a special training program approved
under Section 21.24 of this subchapter; or (3) issued
by another entity that has a course approved
by the Administrator; and
(ii) The inspections and maintenance tasks
are performed in accordance with instructions contained by the special inspection and
preventive maintenance program approved
as part of the aircraft-s type design or supplemental type design.
(31) Removing and replacing self-contained, front instrument panel-mounted
navigation and communication devices that
employ tray-mounted connectors that connect the unit when the unit is installed into
the instrument panel, (excluding automatic
flight control systems, transponders, and
microwave frequency distance measuring
equipment (DME)). The approved unit must
be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. Prior to the unit-s
intended use, and operational check must be

performed in accordance with the applicable
sections of part 91 of this chapter.
(Secs. 313, 601 through 610, and 1102, Federal
Aviation Act of 1958 as amended (49 U.S.C.
1354, 1421 through 1430 and 1502); (49 U.S.C.
106(g) (Revised Pub. L. 97-449, Jan. 21, 1983);
and 14 CFR 11.45)
[Doc. No. 1993, 29 FR 5451, Apr. 23, 1964, as
amended by Amdt. 43-14, 37 FR 14291, June
19, 1972; Amdt. 43-23, 47 FR 41086, Sept. 16,
1982; Amdt. 43-24, 49 FR 44602, Nov. 7, 1984;
Amdt. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt.
43-27, 52 FR 17277, May 6, 1987; Amdt. 43-34, 57
FR 41369, Sept. 9, 1992; Amdt. 43-36, 61 FR
19501, May 1, 1996; Amdt. 43-45, 77 FR 71096,
Nov. 29, 2012]

APPENDIX B TO PART 43 - RECORDING OF
MAJOR REPAIRS AND MAJOR ALTERATIONS

(a) Except as provided in paragraphs (b),
(c), and (d) of this appendix, each person performing a major repair or major alteration
shall - 
(1) Execute FAA Form 337 at least in duplicate;
(2) Give a signed copy of that form to the
aircraft owner; and
(3) Forward a copy of that form to the FAA
Aircraft Registration Branch in Oklahoma
City, Oklahoma, within 48 hours after the
aircraft, airframe, aircraft engine, propeller,
or appliance is approved for return to service.
(b) For major repairs made in accordance
with a manual or specifications acceptable
to the Administrator, a certificated repair
station may, in place of the requirements of
paragraph (a) - 
(1) Use the customer-s work order upon
which the repair is recorded;
(2) Give the aircraft owner a signed copy of
the work order and retain a duplicate copy
for at least two years from the date of approval for return to service of the aircraft,
airframe, aircraft engine, propeller, or appliance;
(3) Give the aircraft owner a maintenance
release signed by an authorized representative of the repair station and incorporating
the following information:
(i) Identity of the aircraft, airframe, aircraft engine, propeller or appliance.
(ii) If an aircraft, the make, model, serial
number, nationality and registration marks,
and location of the repaired area.
(iii) If an airframe, aircraft engine, propeller, or appliance, give the manufacturer-s
name, name of the part, model, and serial
numbers (if any); and
(4) Include the following or a similarly
worded statement - 
 - The aircraft, airframe, aircraft engine,
propeller, or appliance identified above was
repaired and inspected in accordance with

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