NorthStar 1200-02-01, Installation Manual

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Appendix D—Specimen Form 337
PAGE 48 M3 GPS INSTALLATION MANUAL Revision D
G. An Airplane
(or Rotorcraft)
Flight Manual Supplement, Document No.
(or Report or
Part No.) (or Supplemental Flight Manual)
is approved by the FAA Form 337, dated
_______, and has been installed within the Airplane
(or Rotorcraft)
Flight Man-
ual.
(Refer to AC 20-138, Appendix 2.)
H. All inspection records and other documents pertaining to this major alteration
are on file at
(Your Avionics Company)
under Work Order _______ .
I. The alteration was performed in accordance with AC 43.13-1A, Chapter 11,
Paragraphs 424, 425, 427, and 429 through 452, 464 through 466, 478 through
481, 514 through 519, and Chapter 15, Paragraphs 748 through 753, 820
through 822, 826, 827, and 842, and Chapter 16, Paragraphs 880 through 882
and 913; and AC 43.13-2A, Chapter 1, Paragraphs 1 through 12, Chapter 2,
Paragraphs 21 through 23, and Chapter 3, Figure 3.6 and Paragraph 39.
(Note: List appropriate subject Chapters and Paragraphs which apply to your alteration.)
J. The aircraft weight and balance, and the equipment list were amended in accor-
dance with AC 43.13-1A, Chapter 13, Paragraphs 659 through 663.
K. An electrical load analysis was performed in accordance with AC 43.13-1A,
Chapter 11, Paragraph 428, and determined that the total load does not exceed
80% of the total rated alternator capacity.
END