STC ST00056IB

ST00056IB LUFTHANSA TECHNIK AG WEG BEIM JAEGER 193 22335

HAMBURG GERMANY 25 Civil Air/Federal Aviation Regulations A16WE The Boeing Company 737-800 (MSN 32777)

1) Installation of a VIP Cabin configuration in accordance with supplemental type definition documents STDD00-01/07M, Revision 00, issue 3, dated July 07, 2004 and STDD21-07/06M, Revision 0 - Issue 01, dated January 30, 2008 or later EASA approved revisions.

.............................(Description of Type Design continued on page 3 of 3)............................................

1) The installer must determine whether this design change is compatible with previously approved modifications.

……………………. (Limitation and Conditions continued on page 3 of 3)…………………………………… November 18, 2021 September 22, 2022 Anthony E. Gallo Manager, International validation Branch Compliance & Airworthiness Division Aircraft Certification Service 3

ST00056IB 3

ST00056IB Description of Type Design Change: (continued from page 1 of 3)

2) Maintenance in accordance with Lufthansa maintenance Planning Data (MPD) A-00-03/025-MPD, Revision 02, dated May 21, 2015, Aircraft Maintenance Manual Supplement (AMMS), Revision IR, dated April 18, 2003, and Wiring Diagram Manual Supplement (WDMS), Revision 02, dated June 30, 2006 or later LBA/EASA approved revision.

3) Operation must be in accordance with Operating Limitations section of the Airplane Flight Manual Supplement referenced in below or later LBA/EASA approved:-

• Cabin Configuration for Taxi, Take-off and Landing, A-25-03/031-AFM, Revision IR, dated June 11, 2003.

• Passenger Cabin Internal Doors Indication, A-52-03/032-AFM, Revision 02, dated July 22, 2022.

• Passenger Cabin Smoke Detection System, A-26-03/033-AFM, Revision 01, dated March 08, 2004.

Limitations and Conditions: (continued from page 1 of 3)

2) Installation and activation of dryer unit 2001-006 is prohibited. Unit must be modified to P/N 2001-306 in accordance with Lufthansa Technik AG Engineering Bulletin Document number B737-EB21-0195 dated December 17, 2007 or any later EASA approved revisions.

3) Maximum passenger seating capacity: 19

4) 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.

5) The aircraft must be operated in accordance with the Operating Limitations section of the Airplane Flight Manual Supplement referenced in the Description of Type Design Change section of this STC.

Certification Basis:

Based on 14 CFR § 21.115, § 21.101, and the FAA policy for changes that are not significant in FAA Order 8110.48A, the certification basis is as follows:

a. The existing type certification basis for the Boeing company 737-800 (MSN 32777) aircraft as shown on FAA Type Certification Data Sheet A16WE for parts not changed or not affected by this change.

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