STC SA2968SO

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

FAA Form 8110-2 (5/14) Page 1 of 5

Number: SA2968SO

This certificate issued to: Pemco World Air Services 4102 N. Westshore Blvd.

Tampa, FL 33614

Part 25 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: A16WE Make: Boeing Model: 737-200 Series, 737-300 Series, 737-400 Series, 737-700 Series Description of Type Design Change:

For Boeing 737-200 Series, 737-300 Series, 737-400 Series only: Modification of floor in accordance with Pemco World Air Services, Inc. Master Data List (MDL), Report No. 2316 Revision P dated June 18, 2013, or later FAA approved revision. For Boeing737-700 Series only: Modification of floor in accordance with Pemco World Air Services, Inc. Master Data List (MDL), Report No. 2316 Revision AA dated May 08, 2020; and Airplane Flight Manual Supplement P03-0701 revision IR dated 28 April 2020; or later FAA approved revisions.

1. The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft.

Continued on Page 3

Date of Application: October 05, 1989 Date Reissued: June 29, 1998; November 5, 1999; April 2, 2003;

October 24, 2006; August 20, 2012; August 31, 2012, Date of Issuance: June 20, 1991 Date Amended: February 17, 1994; May 1, 2003; June 23, 2006;

November 18, 2011; September 30, 2013; July07, 2020 By Direction of the Administrator Signature

Title: (for) Christina M. Underwood Manager, Atlanta ACO Branch

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

FAA Form 8110-2 (5/14) Page 2 of 5

Transfer the ownership of Supplemental Type Certificate Number: SA2968SO

To (Name and address of transferee)

From (Name and address of grantor)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

FAA Form 8110-2 (5/14) Page 3 of 5

STC Number: SA2968SO Date of Issuance: June 20, 1991 Date Amended: July 07, 2020

Limitations and Conditions: (Continued from Page 1)

2. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

3. The approval of this modification applies to the above noted airplane model series only.

4. A copy of this STC must be included in the permanent record of the modified aircraft.

5. For Boeing 737-200 Series, 737-300 Series, 737-400 Series only: Instructions for Continued Airworthiness (ICA), Pemco Report 2917 Revision L dated August 14, 2013 or later FAA approved revision, is part of this STC, and must be incorporated into the operator’s maintenance program.

6. For Boeing 737-200 Series only: Weight and Balance Control and Loading Manual Supplement for Boeing 737-200 Series Airplane, Pemco Report No. P03-132WB Revision 1 dated April 5, 1994 or later FAA approved revision is a required part of this STC.

7. For Boeing 737-300 Series only: Weight and Balance Control and Loading Manual Supplement for Boeing 737-300 Series Airplane Quick Change and Freighter, Pemco Report No. P03 -004WB Revision 13 dated May 17, 2006 or later FAA approved revision is a required part of this STC.

8. For Boeing 737-400 Series only: Weight and Balance Control and Loading Manual Supplement for Boeing 737-400 Series Airplane, Pemco Report No. P03-212WB Revision 26 dated September 19, 2013 or later FAA approved revision is a required part of this STC.

9. For Boeing 737-700 Series only: Operate in accordance with FAA Approved PEMCO Aircraft Flight Manual Supplement (AFMS) P03-0701, Revision IR, dated 28 April 2020; and Weight and Balance, Control and Loading Manual Supplement, Report No. P03-0700WB, Rev. 1, dated 13 March 2020; or later FAA approved revisions.

10. For Boeing 737-700 Series only: Maintain in accordance with: FAA Accepted PEMCO Instructions for Continued Airworthiness (ICA), Report No. 6534, Rev. IR, dated June 18, 2020; FAA Accepted PEMCO Basic Scheduled Maintenance Check Supplement, Document No. P03 -0705IM, Rev. 1, dated June 23, 2020; or later FAA accepted revisions. These documents must be incorporated into the operator’s maintenance program.

Certification Basis:

1. For Boeing 737-200 Series, 737-300 Series, 737-400 Series only: Based on 14 CFR §§ 21.115 and

21.101 for significant changes to type design, the certification basis for this change is as follows:

a. The certification basis for parts not changed or not affected by this change is in accordance with Type Certificate Data Sheet A16WE.

b. The certification basis for parts changed or affected by the change since the reference date of application of the latest amendment, January 17, 2011, is based upon 14 CFR Part 25 as amended by amendment 25-132. Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

FAA Form 8110-2 (5/14) Page 4 of 5

modification was determined to be:

STC Number: SA2968SO Date of Issuance: June 20, 1991 Date Amended: July 07, 2020

Certification Basis: (Continued from Page 3) 14 CFR Part 25 Regulations at the latest amendment 25-0 through 25-117

25.1, 25.23, 25.487, 25.495, 25.503, 25.507, 25.511, 25.561, 25.601, 25.603, 25.605, 25.607, 25.609,

25.611, 25.613, 25.619, 25.623, 25.625, 25.793, 25.855, 25.857, 25.1529, 25.1583 .

14 CFR Part 25 Regulations at intermediate amendment:

None.

14 CFR Part 25 Regulations at the amendment level in TCDS A16WE

25.301, 25.303, 25.305, 25.307, 25.321, 25.331, 25.335, 25.337, 25.341, 25.349, 25.351, 25.365,

25.471, 25.473, 25.479, 25.481, 25.483, 25.485, 25.489, 25.491, 25.493, 25.499, 25.509

14 CFR Part 26 regulations:

Based on 14 CFR §21.101(g), applicable provisions of 14 CFR part 26 are included in the certification basis. For any future 14 CFR Part 26 amendments, the holder of this STC must demonstrate compliance with the applicable sections. As of the issuance date of this STC, complianc e has been found for the following regulations: §§ 26.11 (Amdt 26-0), 26.47 (Amdt 26-1).

2. For Boeing 737-700 Series only: Based on 14 CFR §§ 21.115 and 21.101 for significant changes to type design, the certification basis for this change is as follows:

a. The certification basis for parts not changed or not affected by this change is in accordance with Type Certificate Data Sheet A16WE.

b. The certification basis for parts changed or affected by this change is:

14 CFR Part 25 Regulations at the amendment level in TCDS A16WE:

§§ 25.1(a)(b), 25.23(a)(b), 25.301(a)(b)(c), 25.303, 25.335, 25.337, 25.365(a)(b)(c)(d)(e)(f),

25.471(a)(b)(c), 25.489, 25.495, 25.509(a)(b)(c), 25.601, 25.603(a)(b)(c), 25.605(a), 25.607(a)(b)(c),

25.609(a), 25.619(a)(b)(c), 25.625(a), 25.793, 25.1519, 25.1529.

14 CFR Part 25 Regulations at intermediate amendment:

§§25.571(a)(b) amendment 25-96.

14 CFR Part 25 Regulations at the latest amendment level 25-0 through 25-142:

§§ 25.305(a)(b), 25.307(a), 25.321(a)(b)(c), 25.331(a)(b)(c), 25.341(a)(b)(c), 25.349(a)(b),

25.351(a)(b)(c)(d), 25.473(a)(b), 25.479(a)(b)(c)(d)(e), 25.481(a)(b)(c), 25.483(a)(b), 25.485(a)(b),

25.491, 25.493(a)(b)(c), 25.499(a)(b)(c)(d)(e), 25.561(a)(b)(c), 25.611(a), 25.613(a)(b)(c), 25.793,

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

FAA Form 8110-2 (5/14) Page 5 of 5

25.853(a), 25.855(d), 25.857 (c)(e), 25.1301(a), 25.1583(c).

STC Number: SA2968SO Date of Issuance: June 20, 1991 Date Amended: July 07, 2020

Certification Basis: (Continued from Page 4) 14 CFR Part 26 regulations:

Based on 14 CFR §21.101(g), applicable provisions of 14 CFR part 26 are included in the certification basis. For any future 14 CFR Part 26 amendments, the holder of this STC must demonstrate compliance with the applicable sections. As of the issuance date of this STC, compliance has been found for the following regulations: 14 CFR §§ 26.47(c), (e), (Amdt No. 26-1).

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