What it approves
Configuration 1: Installation of three-tank auxiliary fuel transfer system (1340 US gallon) in the forward lower cargo compartment; or Configuration 2: Installation of seven-tank auxiliary fuel transfer system (2850 US gallon) in the lower fuselage. (73 7-2H6 S/N 22620)
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
Number SA83NE
This certificate issued to
Part 25 of the Federal Aviation Regulations.
Configuration 1: Installation of seven-tank auxiliary fuel transfer system (2850 U.S. gallons) in the lower fuselage in accordance with the data listed in PATS, Inc. Master Drawing List No. 937-201RL (red-lined), Revision B dated March 1, 1983.
OR Configuration 2: Installation of seven-tank auxiliary fuel transfer system (2850 U.S. gallons) in the lower fuselage in accordance with the data listed in P.A.T.S., Inc. Master Drawing List No. 737-001, Revision B dated November 30, 1982.
Configuration 1:
a. Descriptive data pertaining to this design change are considered inadequate for duplication in other products. This approval is limited to only the installation made in Boeing 737-2H6, 737-200 Series, Serial Number 22620.
(See STC Continuation Sheet 2)
Number The Leading Edge Group, LLC 5400 Carillon Point Kirkland, WA 98033 A16WE Make : Boeing Model : 737-2H6 S/N 22620, 737-200 Series
Date reissued : July 20, 2004, April 27, 2009
Date amended : November 9, 1982, December 20, 1982, March 25, 1983
( Signature) Anthony Socias Manager New York Aircraft Certification Office
( Title) Date of application : November 24, 1981
Date of issuance : May 27, 1982
FAA Form 8110-2-1(10-69) Page 2 of 2
SA83NE Date Reissued: July 20, 2004, April 27, 2009
b. Item b for Configuration 2 is also required with this installation.
c. Item c for Configuration 2 also applies to this installation.
d. The installer must determine whether this design change is compatible with previously approved modifications.
e. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.
Configuration 2:
a. This approval limited to those 737-200 series airplanes having Maximum Flight Weights of not less than 127, 000 pounds.
b. Patrick Aircraft Tank System, Inc. Supplement No. 3 to the Boeing 737-200 Series Aircraft Flight Manual, FAA approved November 9, 1982, is required with this installation.
c. PATS, Inc. Report No. TO-23.4 “Maintenance Manual for 737-001 Auxiliary Fuel System”, dated October 11, 1982, applies to this installation.
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ADs that name this STC · 2
An AD can apply because an STC is installed, or mention one in its text.