What it approves
Installation of 1000-gallon, 2-tank auxiliary fuel system in aft cargo compartment. CONFIGURATION 8: Eligible on 737-200, Aircraft Serial No. 22620 only.
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 SA725NE This certificate issued to
Part 25 of the Federal Aviation Regulations.
Installation of Auxiliary Fuel System in aft cargo compartment in accordance with PATS, Inc Master Drawing List:
Configuration 1: No. 300-1-011, Rev. A, dated January 25, 1990.
Configuration 2: No. 300-1-014, Rev. N/C, dated October 22, 1990.
Configuration 3: No. 300-1-011, Rev. D, dated October 1, 1990.
1. Configuration 1: Eligible on 737-300 Series airplanes.
2. Configuration 2: Eligible only on 737-200C Series airplanes.
3. Configuration 3: Eligible on 737-200 Series airplanes.
4. Configuration 4: Eligible on 737-400 Series airplanes.
5. Configuration 5: Eligible on 737-500 Series airplanes.
6. Configuration 6: Eligible on 737-300 Series airplanes.
The Leading Edge Group, LLC 5400 Carillon Point Kirkland, WA 98033 A16WE Make : Boeing Model : 737-500, -400, -300, -200 and 200C Series
Date of application : December 13, 1989
Date of issuance : March 12, 1990
Date reissued : July 20, 2004, April 27, 2009
Date amended : February 27, 1992; August 11, 1994;
November 10, 1994; August 02, 1995; November 28, 1995;
April 24, 1996; April 07, 2000, August 6, 2001
( Signature) Anthony Socias Manager New York Aircraft Certification Office
( Title)
FAA Form 8110-2-1(10-69) Page 2 of 2
Number SA725NE Reissue Date: July 20, 2004, April 27, 2009
Description of Type Design Change: (Continued) Configuration 4: No. 300-1-006, Rev. B, dated July 19, 1995.
Configuration 5: No. 300-1-007, Rev. B, dated Nove mber 17, 1995, ADCN No. 11, dated November 17, 1995 and ADCN No. 12, dated November 22, 1995.
Configuration 6: No. 300-1-011, Rev. E, dated April 10, 1996.
Configuration 7: No. 300-1-019, Rev. C, dated March 9, 2000.
Configuration 8: No. 300-1-020, Rev. C, dated August 1, 2001.
Limitations and Conditions : (Continued)
7. Configuration 7: Eligible on 737-300 Series airplanes.
8. Configuration 8: Eligible on 737-200, Aircraft Serial No. 22620 only.
9. PATS, Inc. Flight Manual Supplem ent No. 9, FAA approved March 12, 1990, revised November 10, 1994, are required for Configuration 1.
10. PATS, Inc. Flight Manual Supplement No. 4, FAA approved February 27, 1991 is required for Configuration 2.
11. PATS, Inc. Flight Manual Supplement No. 13, FAA approved August 11, 1994 is required for Configuration 3.
12. PATS, Inc. Flight Manual Supplement No. 2, FAA approved August 1, 1995 is required for Configuration 4.
13. PATS, Inc. Flight Manual Supplement No . 2, to the Boeing 737-500 Series aircra ft FAA approved November 28, 1995 is required for Configuration 5.
14. PATS, Inc. Flight Manual Supplement No. 9, FAA approved March 12, 1990, re vised April 24, 1996 is required for Configuration 6.
15. PATS, Inc. Flight Manual Supplement No. 13, FAA approved April 7, 2000 is required for Configuration 7.
16. PATS, Inc. Flight Manual Supplement No. 115, for an aft two tank auxiliary fuel system, FAA approved August 3, 2001 is required for Configuration 8.
17. Auxiliary fuel tanks are life limited to 13 years time in service.
18. PATS, Inc. Maintenance Manual for B-737 two-tank auxiliary fuel system, dated Septembe r 10, 1990 or later approved revision, applies to Configurations 1, 2 and 3.
19. PATS, Inc. Maintenance Manual Supplement for Boeing 737-400, aft two-tank auxiliary fuel system , Rev. A, dated July 17, 1995 applies to Configuration 4.
20. PATS, Inc. Maintenance Manual Supplement for Boeing 737-500, af t two-tank auxiliary fuel system, dated November 6, 1995 or later FAA approved revision, is required for Configuration 5.
21. PATS, Inc. Maintenance Manual Supplement for Boeing 737-300, aft two-tank auxiliary fuel system, Rev. 2, dated April 4, 1996 or later FAA approved revision, is required for Configuration 6.
22. PATS, Inc. Maintenance Manual Supplement for Boeing 737-300, af t four-tank auxiliary fuel system, Document No. TO-1005 is required for Configuration 7.
23. PATS, Inc. Maintenance Manual Supplemen t for Boeing 737-200, Document No. TO- 1223 dated January 1, 2001 or later FAA approved revision is required for Configuration 8.
24. The installer must determine whether this design change is compatible with previously approved modifications.
25. If the holder agrees to permit another pers on to use the certificate to alter a product, the holder must give the other person written evidence of that permission.
…. END….
ADs that name this STC · 2
An AD can apply because an STC is installed, or mention one in its text.