MODIFICATIONS OF Lufthansa Technik AG (300)

ADS-B OUT ACTIVATION

ADS-B Out Activation
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KA-BAND IN-FLIGHT CONNECTIVITY SYSTEM AND IN-CABIN DISTRIBUTION SYSTEMACTIVATION

Ka-Band In-Flight Connectivity System and In-Cabin Distribution SystemActivation
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PROVISIONS FOR LARGE KA-BAND ANTENNA AND SYSTEM INSTALLATION

Provisions for large KA-band antenna and system installation
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A320FAM GLOBAL XPRESS: PARTIAL REMOVAL

A320Fam Global Xpress: Partial Removal
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THE INSTALLATION OF PHOTOLUMINESCENT EMERGENCY FLOOR PATH MARKING SYSTEM GUIDELINE

The installation of photoluminescent emergency floor path marking system guideline
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INSTALLATION OF WATER VAPOR SENSOR SYSTEM II

Installation of Water Vapor Sensor System II
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INSTALLATION OF VC ON A380

Installation of VC on A380
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A340 VIP CABIN MODIFICATION.

A340 VIP Cabin Modification.
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PREMIUM ECONOMY SEATS IN A350

Premium Economy Seats in A350
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WLAN MODIFICATION AND CABIN INTEGRATION

WLAN Modification and Cabin Integration
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INSTALLATION OF KA-BAND SATCOM SYSTEM.

Installation of KA-Band SATCOM System.
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MODIFICATION FOR KA-BAND SATCOM SYSTEM GX CONNECTIVITY

Installation of electrical and structural modifications forKa-bandSATCOM System GX Connectivity
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CABIN WIRELESS DATALINK SYSTEM UPGRADE

Cabin Wireless Datalink System Upgrade This modification activate an Internal Wireless Datalink system for newCabin Wireless Access Points supporting IEEE 802.11ac standard.
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WLAN UPGRADE

WLAN UpgradeReplacement of approved wireless access points with WLAN IEEE 802.11a/b/g standard by new units with WLAN IEEE 802.11 a/n/ac standard
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ACTIVATION OF ATN/MODE 2 DATA LINK FOR PROTECTED MODE-CPDLC

Activation of ATN/Mode 2 Data Link for Protected Mode-CPDLC
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INTRODUCTION OF NEW CABIN LAYOUT,,THIS CABIN MODIFICATION WILL INCREASE THE...

Introduction of new Cabin Layout,,This cabin modification will increase the cabin layout from 168 M-Classseats in the current cabin layout up to 174 M-Class seats after themodification. This will be accomplished by the removal of lavatories,the installation of new narrower lavatories and one additio...
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CENTER CEILING STOWAGE INSTALLATIONTHE CHANGE RELATED TO THIS STC DEALS...

Center Ceiling Stowage InstallationThe change related to this STC deals with the installation of a CenterCeiling Stowage (CCS). The CCS is a small compartment unit locatedbetween C63 and C65, in the Ceiling and center area of the aircraft.Itis used by the Cabin Crew, which means that the CCS is not...
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PAC GCS A380 LARGE ANTENNA INSTALLATION

PAC GCS A380 Large Antenna Installation
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INSTALLATION OF SWISS MAX CABIN RECONFIGURATION

Installation of Swiss Max cabin reconfiguration
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COMMUNICATION - ACTIVATION OF CPDLC.

Communication - Activation of CPDLC.
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INSTALLATION OF NEW PREMIUM ECONOMY CLASS IN THE MAIN CABIN...

Installation of New Premium Economy Class in the main cabin between doors 2 & 3
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NEW PREMIUM ECONOMY CLASS (A330-300)IN THE MAIN CABIN OF THE...

New Premium Economy Class (A330-300)In the main cabin of the main floor on the aircraft, the change consistof the removal of 10 per cent of the Economy Class Seats between door 2and door 3 and the installation of new developed Premium Economy Seatswith a Panasonic IFE System instead. The new seating...
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TCAS CHANGE 7.1REPLACEMENT OF THE TCAS II COMPUTER WITH SOFTWARE...

TCAS Change 7.1Replacement of the TCAS II computer with software version 7.0 currentlyinstalled on Lufthansa German Airlines (DLH) MD11 aircraft by a newgeneration TCAS II computer with software version 7.1.
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INSTALLATION OF NEW PREMIUM ECONOMY CLASS IN THE MAIN CABIN...

Installation of New Premium Economy Class in the main cabin between doors 3 & 4
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NEW PREMIUM ECONOMY CLASS (A330-300)IN THE MAIN CABIN OF THE...

New Premium Economy Class (A330-300)In the main cabin of the main floor on the aircraft, the change consistof the removal of 10 per cent of the Economy Class Seats between door 2and door 3 and the installation of new developed Premium Economy Seatsinstead. The new seating will have a greater pitch a...
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NEW PREMIUM ECONOMY CLASS (B747-400)IN THE MAIN CABIN OF THE...

New Premium Economy Class (B747-400)In the main cabin of the main floor on the aircraft, the change consistof the removal of 10 per cent of the Economy Class Seats between door 2and door 3 and the installation of new developed Premium Economy Seatsinstead. The new seating will have a greater pitch a...
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PATIENT TRANSPORT COMPARTMENT / PATIENT TRANSPORT UNIT INSTALLATION

Patient Transport Compartment / Patient Transport Unit installation
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RADOME INSTALLATION FOR LIVE TV ANTENNA INSTALLATION RADOMEINSTALLATIONFOR LIVE TV...

Radome Installation for Live TV Antenna Installation Radomeinstallationfor Live TV antenna installationRevision 1: incorporation of the B747-300 installationRevision 2: incorporation of the B747-8 installation, STC number oldformat EASA.A.S.00701 replaced by new format 10013967.
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INSTALLATION OF CABIN INTERIOR B747-4 IK RETROFIT FOR ALL BUSINESS...

Installation of Cabin Interior B747-4 IK Retrofit for all business class seats which results in an i
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INSTALLATION OF PHOTOLUMINESCENT EMERGENCY FLOOR PATH MARKING SYSTEM

Installation of Photoluminescent Emergency Floor Path Marking System
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INSTALLATION OF PHOTOLUMINESCENT EMERGENCY FLOOR PATH MARKING SYSTEM

Installation of Photoluminescent Emergency Floor Path Marking System
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INSTALLATION OF PHOTOLUMINESCENT EMERGENCY FLOOR PATH MARKING SYSTEM

Installation of Photoluminescent Emergency Floor Path Marking System
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INSTALLATION OF PHOTOLUMINESCENT EMERGENCY FLOOR PATH MARKING SYSTEM

Installation of Photoluminescent Emergency Floor Path Marking System
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NEW PREMIUM ECONOMY CLASS FOR A340-300IN THE MAIN CABIN OF...

New Premium Economy Class for A340-300In the main cabin of the main floor on the aircraft, the change consistof the removal of 10 per cent of the Economy Class Seats between door 2and door 3 and the installation of new developed Premium Economy Seatsinstead. The new seating will have a greater pitch...
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VC INSTALLATION ON A380:NEW ECONOMY CLASS SEATS (RECARO CL3510) INSTALLED...

VC installation on A380:New Economy Class seats (Recaro CL3510) installed in the aft section ofthe upper deck aft of door 3
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NEW PREMIUM ECONOMY CLASS FOR A380-800IN THE MAIN CABIN OF...

New Premium Economy Class for A380-800In the main cabin of the main floor on the aircraft, the change consistof the removal of 10 per cent of the Economy Class Seats between door 2and door 3 and the installation of new developed Premium Economy Seatsinstead (with Panasonic IFE). The new seating will...
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LUFTHANSA B747-4 IK-RETROFIT -THIS MODIFICATION REFLECTS ANEXCHANGE OF ALL BUSINESS...

Lufthansa B747-4 IK-Retrofit -This Modification reflects anexchange of all Business Class Seats,which results in an increase of 59 passengers. A new IFE System will becomplete integrated, which also involved a modification of all Economyseats, Partitions and Monuments.
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NEW PREMIUM ECONOMY CLASS FOR A340-600IN THE MAIN CABIN OF...

New Premium Economy Class for A340-600In the main cabin of the main floor on the aircraft, the change consistof the removal of 10 per cent of the Economy Class Seats between door 2and door 3 and the installation of new developed Premium Economy Seatsinstead. The new seating will have a greater pitch...
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INSTALLATION AND ACTIVATION OF AN ELECTRONIC FLIGHT BAG (EFB) ON...

Installation and activation of an Electronic Flight Bag (EFB) on aB777-FThis STC installs (using provisions from OEM options) and activates aClass 2 EFB in the cockpit, composed of touch screen displays mounted atthe OEM locations for the LH and RH Class 3 EFB, and docking stationshoming personalize...
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NEW PREMIUM ECONOMY CLASS FOR B747-8IN THE MAIN CABIN OF...

New Premium Economy Class for B747-8In the main cabin of the main floor on the aircraft, the change consistof the removal of 10 per cent of the Economy Class Seats between door 3and door 4 and the installation of new developed Premium Economy Seatsinstead. The new seating will have a greater pitch a...
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UPGRADE OF THE ACARS CMU SOFTWARE - INSTALLATION OF AOA-ONLY...

Upgrade of the ACARS CMU software - Installation of AOA-only softwareconfiguration.
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ACTIVATION OF THE WIRELESS INFLIGHT ENTERTAINMENT SYSTEM - BOARDCONNECT

Activation of the Wireless Inflight Entertainment System - BoardConnect
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INSTALLATION OF DATA BROADBAND TRANSCEIVER SYSTEM WITH FULL PROVISIONS FOR...

Installation of Data Broadband Transceiver System with full provisions for On-Board Mobile Telephony System
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COMMUNICATIONS - INSTALLATION OF AOA SOFTWAREUPDATE OF THE ACARS CMU...

Communications - Installation of AOA SoftwareUpdate of the ACARS CMU Software
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A330-200 NEW MODEL PAX SEATS AND LD- MCR1. EXCHANGE OF...

A330-200 new model pax seats and LD- MCR1. Exchange of 285 pax 2-class seating with 275 pax 2-class seating. Newseat models Thompson Vantage (22 B/C) and ZIM Eco 01 (253 Y/C).2. Integration of Lower Deck Mobile Crew Rest (LD-MCR) containerincluding staircase and secondary escape path (hatch).3. Assoc...
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A330-300 NEW MODEL PAX SEATS AND MONUMENTS INSTALLATION1. EXCHANGE OF...

A330-300 new model pax seats and monuments installation1. Exchange of 332 pax 2-class seating with 315 pax 2-class seating. Newseat models Thompson Vantage (B/C) and ZIM Eco 01 (Y/C) includingrelated IFE equipment.2. Installation of monuments and associated cabin interior modifications
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INTRODUCTION OF TAILWIND 550 ANTENNA.WITH THE REVISION 2 OFTHIS STC...

Introduction of Tailwind 550 Antenna.With the revision 2 ofthis STC the previous life limit of 500 FlightCycles is removed.
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INSTALLATION OF DATA BROADBAND TRANSCEIVER SYSTEM WITH FULLPROVISIONFOR ON-BOARD MOBILE...

Installation of Data Broadband Transceiver System with fullprovisionfor On-Board Mobile Telephony System
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LHT - INSTALLATION OF 1000 SERIES PHOTO LUMINESCENT FLOOR PATH...

LHT - Installation of 1000 Series photo luminescent floor path marking
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INSTALLATION OF CABIN INTERIOR RECONFIGURATION (INCLUDING SEATING, IFE, MONUMENT, GALLEYS,...

Installation of Cabin Interior Reconfiguration (including Seating, IFE, Monument, Galleys, Stowage Bins, Lavatories and other general structures)
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DLH A340-600 CABIN INTERIOR RECONFIGURATION. DESCRIPTION - SUMMARY : CABIN...

DLH A340-600 Cabin Interior Reconfiguration. Description - Summary : Cabin Reconfiguration by replacing of all Business- and Economy Class Seats and modification of several components, also the InflightEntertainment System. Limitations: - Certification Program CP00-12/22M iss 1 at rev 4- Supplemental Type Definition Document STDD00-12/22M issue 1 rev 4- ICA, ref A-00-13/07-ICA, Issue 1 rev 0- Compliance Record List CRL00-12/22M iss 2 at rev 0or later revisions ...
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INSTALLATION OF MAJLIS VIP CABIN INTERIOR AND ENTERTAINMENT SYSTEM FOR...

Installation of Majlis VIP Cabin Interior and Entertainment System for model 777-200, serial number 29271.
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ONE-ONLY STC: STRUCTURAL MOUNTING PROVISIONS FOR LARGE ANTENNA AND RADOME...

ONE-ONLY STC: Structural mounting provisions for large antenna and radome installed on Boeing 777-200, serial number MSN29271.
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ONE-ONLY STC: MAJLIS VIP CABIN INTERIOR AND ENTERTAINMENT SYSTEM INSTALLED...

ONE-ONLY STC: Majlis VIP Cabin Interior and Entertainment System installed on Boeing 777-200, serial number 29271.
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SEAT LAYOUT RECONFIGURATION AND INSTALLATION OF AVIO INTERIOR ECONOMY CLASS...

Seat layout reconfiguration and installation of Avio Interior Economy Class Seats and Recaro Business Class Seats with PC-Power and PC-Data outlets.
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INSTALLATION OF ZONAL DRYING SYSTEM IN ACCORDANCE WITH LUFTHANSA TECHNIK...

Installation of Zonal Drying System in accordance with Lufthansa Technik Supplemental Type Definition Document STDD 21-04/01M, Issue 01, dated January 4, 2005.
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INSTALLATION OF A TCAS II UPGRADE TO SOFTWARE VERSION 7....

Installation of a TCAS II Upgrade to Software Version 7. Approved for 747-230B serial numbers 21588, 21590, 21591, 21643, 22670, 23407, 23509, 23622, 22363, 22671, 23286, 23287, 23393, and 747-230F serial numbers 21592, 22668, 23348, 23621, and 24138.
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INSTALLATION OF A VIP EXECUTIVE INTERIOR. APPROVED FOR MODEL 737-700...

Installation of a VIP Executive Interior. Approved for model 737-700 IGW serial number 32805 ONLY.
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INSTALLATION OF HELIOJET LED CABIN LIGHT. LIMITATIONS: -,,SUPPLEMENTAL TYPE DEFINITION...

Installation of HelioJet LED cabin light. Limitations: -,,Supplemental Type Definition Document STDD33-13/19M Issue 1 Rev 0dated 16/08/2013-,,Compliance Record List CRL33- 13/19M Issue 1 Rev 0 dated 16/08/2013- ,,Instructions for Continued Airworthiness A- 00-13-41-ICA Issue 1 Rev0dated 14/08/2013- ,,Applic (...) Conditions: Prior to installation of this design change it must be determined that the interrelationship between this design change and any other previously installed design change and/ ...
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DLH A330 IK RETROFIT.DESCRIPTION - SUMMARY : INSTALLATION OF NEW...

DLH A330 IK Retrofit.Description - Summary : installation of new Y-Class, C-Class and FirstClass seats and lining. Limitations: - Certification Plan CP25-12/31M iss 1 at rev 2- Supplemental Type Definition Document STDD25-12/31M issue 1 rev 0(Master document and definition)- ICA, ref A-00-12/40 ICA, rev 01- Compliance Record List CRL25- 12/31M iss 1 at rev 0or later revisions of the above listed documents approved by EASA. Conditions: ...
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A340-600 CABIN RETROFIT ETIHAD ETD06EASA STC 10029134 REVISION DUE TO...

A340-600 Cabin Retrofit Etihad ETD06EASA STC 10029134 revision due to removal of EWIS limitation Limitations: -,,Supplemental Type Definition Document, ref. Doc. No STDD00-09/20M,Issue 1, dated 24th February 2010-,,Compliance Record List ref. doc. No. CRL 00-09/20M iss.2, dated 24thApril 2013-,,Instructions for Continued Airworthiness, ref. Doc. No.A-25-10/ (...) Conditions: Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any ...
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NG STRETCHER INSTALLATION IN AFT AREA OF THE MAIN DECK...

NG Stretcher installation in aft area of the main deck Limitations: Description document STDD25-12/32M Issue 01 Rev. 00Certification Program CP25- 12/32M Issue 01 Rev. 00Compliance Record List CRL25-12/32M Issue 01 Rev. 00Engineering Bulletin 747-EB25-1536 Rev 0or later revisions of the above listed documents approved by EASA Conditions: Conditions1. All equipment (stretcher, oxygen bottles, etc.) must be approvedagainst the appropriate qualification standard, if any.2. The stretcher shall ...
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INSTALLATION OF ANTENNA, RECEIVER TRANSMIT SYSTEM, AND NETWORK SERVICES.THIS STC...

Installation of Antenna, Receiver Transmit System, and Network services.This STC installs through the cabin a set of equipment to allow dataexchange.The Revision 1 has introduced some modifications through the initial STCdesign by upgrading the exis (...) Limitations: Supplemental Type Definition Document, ref. STDD46-11/14, Issue 1;Instruction for Continued Airworthiness, ref. R-00-04/120, Revision 5;Aircraft Fligth Manual Supplement, ref. A-00-04/133-AFM, Revision 2;or later revisions of the above listed documents ...
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INSTALLATION OF NEK CABIN MODIFICATION. LIMITATIONS: -,,DECLARATION OF COMPLIANCE ADC...

Installation of NEK cabin modification. Limitations: -,,Declaration of Compliance ADC 3499 Rev. IR, dated 18/01/2013;-,,Compliance Record List CRL25-12/30M Issue 1 Rev. 0,dated 18/01/2013;-,,Supplemental Type Definition Document STDD25-12/30M Issue 1 Rev. 0,dated 18/01/2013;-,,Instructions for Continu (...) Conditions: Prior to installation of this design change it must be determined that the interrelationship between this design change and any other previously installed design change and/ or repair will introduce ...
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REVISION OF EASA.A.S.01534 IR PER MAJOR CHANGE 0010002739-001:OPERATIONAT 8.99 PSI...

Revision of EASA.A.S.01534 IR per Major Change 0010002739-001:Operationat 8.99 psi maximum cabin differential pressure (Lower Cabin Altitude,LCA)Original STC Title: B737- 700 IGW VIP Cabin 19 Pax. Limitations: Once LCA is activated (installation of FAA STC ST01697SE as validatedper EASA STC 10042295) on an individual aircraft, the maintenancerequirements defined in Doc A-00- 06/100-ICA will apply for the life ofthis aircraft. This limitation remains valid also in. Conditions: ...
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REVISION OF EASA.A.S.02752 REV.4 PER MAJOR CHANGE 0010002741-001:OPERATION AT 8.99...

Revision of EASA.A.S.02752 Rev.4 per Major Change 0010002741-001:Operation at 8.99 psi maximum cabin differential pressure (Lower CabinAltitude, LCA)Original STC Title: Design and Implementation of VIP interior andmiscellaneous aircraft systems. Limitations: Once LCA is activated (installation of FAA STC ST01697SE as validatedper EASA STC 10042295) on an individual aircraft, the maintenancerequirements defined in Doc A-00- 07/784-ICA will apply for the life ofthis aircraft. This limitation remains valid ...
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INTEGRATION OF THE W-IFE (WIRELESS IN-FLIGHT ENTERTAINMENT) SYSTEM ONA320. LIMITATIONS:...

Integration of the W-IFE (Wireless In-Flight Entertainment) system onA320. Limitations: This approval is limited to MSN 0110.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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INSTALLATION OF NON-ELECTRICAL FLOOR PATH MARKING SYSTEM GUIDELINE® LIMITATIONS: N/A....

Installation of non-electrical Floor Path Marking System Guideline® Limitations: n/a. Conditions: n/a
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INSTALLATION OF NON-ELECTRICAL FLOOR PATH MARKING SYSTEM GUIDELINE® LIMITATIONS: N/A....

Installation of non-electrical Floor Path Marking System Guideline® Limitations: n/a. Conditions: n/a
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INSTALLATION OF NON-ELECTRICAL FLOOR PATH MARKING SYSTEM GUIDELINE® LIMITATIONS: N/A....

Installation of non-electrical Floor Path Marking System Guideline® Limitations: n/a. Conditions: n/a
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INSTALLATION OF NON-ELECTRICAL FLOOR PATH MARKING SYSTEM GUIDELINE® LIMITATIONS: LUFTHANSA...

Installation of non-electrical Floor Path Marking System Guideline® Limitations: Lufthansa Technik AG AFM Supplement A-33- 06/472-AFM. Conditions: n/a
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INSTALLATION OF NON-ELECTRICAL FLOOR PATH MARKING SYSTEM GUIDELINE® LIMITATIONS: N/A....

Installation of non-electrical Floor Path Marking System Guideline® Limitations: n/a. Conditions: n/a
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INSTALLATION OF NON-ELECTRICAL FLOOR PATH MARKING SYSTEM GUIDELINE

Installation of non-electrical Floor Path Marking System Guideline® Limitations: n/a. Conditions: n/a
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INSTALLATION OF NON-ELECTRICAL FLOOR PATH MARKING SYSTEM GUIDELINE® LIMITATIONS: N/A....

Installation of non-electrical Floor Path Marking System Guideline® Limitations: n/a. Conditions: n/a
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INSTALLATION OF NON-ELECTRICAL FLOOR PATH MARKING SYSTEM GUIDELINE® LIMITATIONS: ATR42/72...

Installation of non-electrical Floor Path Marking System Guideline® Limitations: ATR42/72 except those aircraft with convertible seats which do not have a fixed lateral position.See Airplane Flight Manual Supplement AFMS A-33-06/497-AFM Initial Revision or later approved revisions.Instructions for Continued Airworthiness ICA33-06/04M I. Conditions: n/a
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INSTALLATION OF NON-ELECTRICAL FLOOR PATH MARKING SYSTEM GUIDELINE® LIMITATIONS: N/A....

Installation of non-electrical Floor Path Marking System Guideline® Limitations: n/a. Conditions: n/a
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INSTALLATION OF NON-ELECTRICAL FLOOR PATH MARKING SYSTEM GUIDELINE® LIMITATIONS: N/A....

Installation of non-electrical Floor Path Marking System Guideline® Limitations: n/a. Conditions: n/a
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INSTALLATION OF NON-ELECTRICAL FLOOR PATH MARKING SYSTEM GUIDELINE® CERTIFICATION BASIS...

Installation of non-electrical Floor Path Marking System Guideline® Certification Basis Limitations CRJ-EB33-0320 Revision 1 dated 11 April 2007AFM A-33-07/012-AFM Revision Initial dated 5 January 2007or later revisionsof the above listed documents approved by EASA Conditions
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INSTALLATION OF NON-ELECTRICAL FLOOR PATH MARKING SYSTEM GUIDELINE

Installation of non-electrical Floor Path Marking System Guideline   Limitations: This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer.. Conditions: n/a
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INTRODUCTION OF TAILWIND 550 ANTENNA LIMITATIONS: THIS MODIFICATION IS LIMITED...

Introduction of Tailwind 550 Antenna Limitations: This modification is limited to MSN 29953.This modification has a temporary life limit of 500 Flight Cycles.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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VIP CABIN INTERIOR COMPLETION BBJ2 LIMITATIONS: 1) AS PER AFM...

VIP Cabin Interior Completion BBJ2 Limitations: 1) As per AFM limitations A-00-11/006-AFM, Issue05, Rev 00 :- The aircraft is certified for non-commercial use.- Required Crew: in case passengers are on board one (1) cabin attendantis required and has to be seated at door #1, left hand side.- Cabin WLAN:. Conditions: 1) LCA compatibility necessary: Lufthansa Technik AG has shown withinthe substantiation data package that the installations ...
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REPLACEMENT OF LITTON MK-1 GLOBAL POSITIONING SYSTEM SENSOR UNIT (GPSSU)BY...

Replacement of Litton MK-1 Global Positioning System Sensor Unit (GPSSU)by CMC Electronics GPSSU CMA-5024(STC revised for validity extension to A319 and A321 models) Limitations: None. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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INSTALLATION OF CLASS 2 EFB DOCKING STATION WITH DISPLAY, COCKPIT...

Installation of class 2 EFB docking station with display, cockpit doorsurveillance cameras an taxi aid cameras at vertical stabilizer and atfuselage belly. Limitations: Only for EFB installation. No installation of the belly and tail fincamera in the frame of this STC.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will ...
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CAMERA INSTALLATION IN THE VERTICAL STABILIZER FOR GROUND MANOEUVRINGSERVICE. LIMITATIONS:...

Camera installation in the vertical stabilizer for ground manoeuvringservice. Limitations: none. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalledmodification and/ or repair will introduce no adverse effect upon theairworthiness of the product.
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STDD 21-09/02M: B-777-200 - ZONAL DRYING SYSTEM INSTALLATION LIMITATIONS: NONE....

STDD 21-09/02M: B-777-200 - Zonal Drying System Installation Limitations: none. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalledmodification and/ or repair will introduce no adverse effect upon theairworthiness of the product.
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NAVIGATION - ADS-B OUT (AUTOMATIC DEPENDENT SURVEILLANCE BROADCAST)CAPABILITY ON A340-...

Navigation - ADS-B Out (Automatic Dependent Surveillance Broadcast)Capability on A340- 300This STC consists in installing AOS-B Out capability.This surveillance function is based on the aircraft capability tobroadcast, without any ground request, aircraft p Limitations: None.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness ...
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CABIN COMPLETION "TIGER" LIMITATIONS: REFER TO AFM LIMITATIONS ON THE...

Cabin Completion "Tiger" Limitations: Refer to AFM limitations on the use of Portable Electronic devices. Conditions: Lufthansa Technik AG has shown within the substantiation data packagethat the installations covered by this Supplemental Type Certificate iscompatible with FAA approved FAA STC ST01697SE (identified thereafter asLow Cabin Altitude - LCA) for aircraft opera
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A340-300 GPSSU REPLACEMENTTHIS STC CONSISTS IN REPLACING THE CURRENT GLOBAL...

A340-300 GPSSU ReplacementThis STC consists in replacing the current Global Positioning SystemSensor Unit (GPSSU) by a new standard able to transmit GPS qualityinformation. Limitations: None.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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THAI AIRWAYS A330-300 - SEAT EXCHANGE AND ELECTRICAL ADAPTION.THIS STC...

Thai Airways A330-300 - Seat exchange and electrical adaption.This STC installs 263 Y class seats, with associated electricaladaptations. Limitations: None.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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REPLACEMENT OF GLOBAL POSITIONING SYSTEM SENSOR UNIT AND GPS ANTENNA....

Replacement of Global Positioning System Sensor Unit and GPS Antenna. Limitations: None.. Conditions: None.
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INSTALLATION OF A VIP CABIN FOR A MAXIMUM OF 19...

Installation of a VIP cabin for a maximum of 19 passengers. The designdetails are described in General Description C-AAA057-SPA.Deletion of the Airworthiness Limitation Item reference 530000-01-S forA318-112 Elite 14 MSN 4169 Limitations: None. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the ...
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A318-112 - ELITE 16 MSN 4503INSTALLATION OF A VIP CABIN...

A318-112 - ELITE 16 MSN 4503Installation of a VIP Cabin Interior Completion. Limitations: Not applicable. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product
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UPGRADE OF FIRST CLASS CABIN REPLACING 16 FIRST CLASS SEATS...

Upgrade of first class cabin replacing 16 first class seats by 8modified first class seats and installation of 8 single beds and halfsize partitions in accordance with STDD25-10/13M Issue 01, rev 00<(>,<)>d.d. 11-05-2011 Limitations: None. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness ...
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A330-200 CABIN RETROFIT ETD01 LIMITATIONS: NONE. CONDITIONS: PRIOR TO INSTALLATION...

A330-200 Cabin retrofit ETD01 Limitations: None. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product
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DLH STRETCHER INSTALLATION LIMITATIONS: NONE. CONDITIONS: PRIOR TO INSTALLATION OF...

DLH Stretcher Installation Limitations: None. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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THAI AIRWAYS A330-300 - SEAT EXCHANGE AND ELECTRICAL ADAPTIONTHIS STC...

Thai Airways A330-300 - Seat exchange and electrical adaptionThis STC installs 263 Y class seats, with associated electricaladaptations. Limitations: None. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product
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ACTIVATION OF ADS-B OUT CAPABILITY VIA 1090MHZ EXTENDED SQUITTER INACCORDANCE...

Activation of ADS-B Out capability via 1090MHz Extended Squitter inaccordance with Lufthansa Supplemental Type Definition DocumentSTDD34-10/02M Issue 01, Rev 02, dated Feb. 10, 2011 or later approvedrevision. Limitations: none. Conditions: Doc. No. A-00-10/225 Rev IR Airplane Flight Manual Supplement shall beavailable on board of the modified airplaneDoc. No. A-00-10/225-ICA Issue 1, Rev. IR Instructions for ContinuedAirworthiness shall be incorporated in the maintenance documentation ofthe
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INSTALLATION OF PHOTOLUMINESCENT EMERGENCY FLOOR PATH MARKING SYSTEMGUIDELINE® LIMITATIONS: NOT...

Installation of Photoluminescent Emergency Floor Path Marking SystemGuideline® Limitations: Not Applicable. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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A340-300 - "GAF" VIP CABIN INTERIOR COMPLETION LIMITATIONS: NONE. CONDITIONS:...

A340-300 - "GAF" VIP Cabin Interior Completion Limitations: None. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product
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DLH NEW EUROPEAN CABIN FOR 737-500 AIRCRAFT.MODIFICATION OF THE AIRCRAFT...

DLH New European Cabin for 737-500 Aircraft.Modification of the Aircraft seat layout to increase the seat capacityfrom currently 111 seats to 120 new seats, produced by RecaroAircraftseating, Germany. Limitations: Not Applicable. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and / or repair will introduce no adverse effectupon the airworthiness of the product.
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A340-600 CABIN RETROFIT - ETD05 LIMITATIONS: NOT APPLICABLE. CONDITIONS: PRIOR...

A340-600 Cabin Retrofit - ETD05 Limitations: Not applicable. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product
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NEW EUROPEAN CABIN MODIFICATION LIMITATIONS: NOT APPLICABLE. CONDITIONS: PRIOR TO...

New European Cabin Modification Limitations: Not applicable. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product
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ZONAL DRYER SYSTEM INSTALLATION IN ACCORDANCE WITH 737-EB21-0212 LIMITATIONS: NONE....

Zonal Dryer System Installation in accordance with 737-EB21-0212 Limitations: None. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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ACTIVATION OF ADS-B OUT CAPABILITY VIA 1090MHZ EXTENDED SQUITTER INACCORDANCE...

Activation of ADS-B Out capability via 1090MHz Extended Squitter inaccordance with Lufthansa Supplement Type Definition DocumentSTDD34-10/01M Iss. 2, dated Sep. 20, 2010 or later approved revision Limitations: none. Conditions: Doc. No. A-00-10/153 Rev IR Airplane Flight Manual Supplement shall beavailable on board of the modified airplaneDoc. No. A-00-10/153-ICA IR Instructions for Continued Airworthinessshall be incorporated in the maintenance documentation of the aircraft. Pri
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TRIAL INSTALLATION OF 2 ROWS OF THE BE/AEROSPACE V-SEATS MODEL...

Trial installation of 2 rows of the BE/Aerospace V-seats model BE 15.0PN series 1012121 as replacement for 3 rows of Recaro EC seat model 3410in Section B of the Lufthansa B747- 400 reg D-ABVW, in accordance withLHT document STDD00-10/16M Issue 01 Limitations: This STC is limited to Lufthansa B747-400 aircraft sn 629493, reg D-ABVWThe approval for this trial is valid until November 30, 2010Compliance with CS ...
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A319-133 "GAF" VIP CABIN COMPLETION, REVISION 2TO INCORPORATE ADDITIONAL CMR...

A319-133 "GAF" VIP Cabin Completion, Revision 2To incorporate additional CMR in the ICA and MPD SupplementClosure of post certification action item D-08-01. Limitations: None.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/or repair will introduce no adverse effectupon the airworthiness of the product.
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A340-200 - INSTALLATION OF PROVISIONS FOR LIVE TV, SATCOM, AND...

A340-200 - Installation of provisions for Live TV, Satcom, and W-LANThis STC installs several structural provisions for Live TV, Satcom, andW-LAN systems, relocates the existing upper Anti-Collision Light (ACL)and installs a additional upper ACL. Limitations: Limited to MSN 151. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no ...
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A340-500 CABIN RETROFIT ETD03THIS STC MODIFIES THE CABIN LAYOUT BY...

A340-500 Cabin retrofit ETD03This STC modifies the cabin layout by replacing First Class seats andall associated seat monuments. Limitations: None. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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INSTALLATION OF CLASS 2 EFB LAPTOP CRADLE LIMITATIONS: THIS STC...

Installation of Class 2 EFB Laptop Cradle Limitations: This STC is only intended for the defined Class 2 EFB with Type A andType B software applications, in accordance with JAA Temporary GuidanceLeaflet TGL-36 and FAA Advisory Circular AC120-76A.Operation of type C software applications in accordance with FAAA. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other ...
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A318-112 - ELITE 11 - VIP CABIN COMPLETION LIMITATIONS: NOT...

A318-112 - Elite 11 - VIP Cabin Completion Limitations: Not applicable. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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FUSELAGE - STRUCTURAL PROVISIONS AND SATCOM ANTENNA INSTALLATION, SATCOMEQUIPMENT RACK...

Fuselage - Structural provisions and Satcom antenna installation, Satcomequipment rack installation and VHF antenna installation.This STC installs Satcom and VHF antennae, as well as the provision forthe future support of a Satcom system installation. Limitations: Limited to: MSN 484. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no ...
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A340-600 CABIN RETROFIT ETIHAD ETD06 LIMITATIONS: THE STC HOLDER SHALL...

A340-600 Cabin Retrofit Etihad ETD06 Limitations: The STC holder shall provide by 7th June 2010 Instructions for ContinuedAirworthiness on Electrical Wiring Interconnection System - EWIS ICA -in accordance with CS-25, Appendix H "Electrical Wiring InterconnectionSystem".. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness ...
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A330-200 - VIP CABIN INTERIOR COMPLETION LIMITATIONS: AS PER AFMS...

A330-200 - VIP Cabin Interior Completion Limitations: as per AFMS A-00-09/009-AFM issue 5 as listed in the associatedtechnical documentation. Conditions: as per AFMS A-00-09/009-AFM issue 5 as listed in the associatedtechnical documentation Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/
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INSTALLATION OF SELF-ILLUMINATING FLOOR PATH MARKING SYSTEM. LIMITATIONS: FOKKER F50...

Installation of self-illuminating Floor Path Marking System. Limitations: Fokker F50 (F27 Mark 050) aircraft series in standard airline cabinconfiguration described as typical cabin layout in Engineering BulletinF50-EB33-0343, Rev. 01, CH. 4.2. Cabin layout with convertible seats(non fixed lateral position may result in covering. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or ...
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A318-100 - ELITE - PROJECT COMLUX3. GREEN AIRCRAFT COMPLETION TO...

A318-100 - ELITE - Project Comlux3. Green aircraft completion to a VIPcabin configuration. Limitations: n/a. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.The ins
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RADOME INSTALLATION FOR LIVE TV ANTENNA INSTALLATION LIMITATIONS: 1. MAINTENANCE...

Radome Installation for Live TV Antenna Installation Limitations: 1. Maintenance requirements, Doc. No. C- AAL900-MR shall be incorporated in the aircraft maintenance documentation.2. This STC is approved only for the product configuration as defined in the approved design data. Compatibility with other aircraft/eng. Conditions: n/a
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A318 ELITE – RAK – STRUCTURAL FLOOR PANEL – SFP...

A318 ELITE – RAK – Structural Floor Panel – SFP - Retrofit Limitations: 1. Prior to installation of this modification the installer must determine that the interrelationship between this modification andany other previously installed modification will introduce no adverse effect upon the airworthiness of the product.2. The ins. Conditions: n/a
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A318-112 - ELITE - PROJECT TANKER 1INSTALLATION OF A VIP...

A318-112 - ELITE - Project Tanker 1Installation of a VIP cabin for a maximum of 16 passengers for non-commercial operation only. The design details are described in General Description C-AAA024-SPA. Limitations: 1. Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product.2.. Conditions: ...
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A318-112 - ELITE - PROJECT HKINSTALLATION OF A VIP CABIN...

A318-112 - ELITE - Project HKInstallation of a VIP cabin for a maximum of 19 passengers for commercial and non-commercial operation. The design details are described in General Description S-00-08/731. Limitations: Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product.. Conditions: n/a
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STRUCTURAL FLOOR PANEL RECONFIGURATIONTHE LIMITATION FOR DIVANS THAT THEY MUST...

Structural Floor Panel ReconfigurationThe limitation for divans that they must not be occupied for taxi, take off and landing has been suspended for 1315 FH or 14 monthswhatever occurs first, starting at June 26th, 2008.The modification is described in the Limitations: 1. Side facing divans may not be used for taxi, take off and landing after1315 FH or 14 months whatever occurs first, starting at June ...
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A318 ELITE - PROJECT COMLUX 2; VIP CABIN COMPLETION LIMITATIONS:...

A318 ELITE - Project Comlux 2; VIP Cabin completion Limitations: Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product.. Conditions: n/a
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A318 ELITE - PROJECT BAA; VIP CABIN COMPLETION. LIMITATIONS: 1....

A318 ELITE - Project BAA; VIP Cabin completion. Limitations: 1. Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product.2.. Conditions: n/a
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CONDOR B767 INTERIOR MODIFICATION LIMITATIONS: • PRIOR TO INSTALLATION OF...

Condor B767 Interior Modification Limitations: • Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product.• Th. Conditions: n/a
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REPLACEMENT OF ZONAL DRYER RELATED TO EASA AD 2006-0140-E.THE ABOVE...

Replacement of Zonal Dryer related to EASA AD 2006-0140-E.The above reference EASA AD required the de-activation of Zonal Drying Systems installed via LBA STC LBA.21E2.TA0270 due to the potential for combustion of contaminants in the dryerunit. A ne (...) Certification Basis Limitations STDD21-02/01M, Issue 04STDD21-07/06M, Issue 01, CL-600-EB21-0192AD 2006-0140- E Conditions See related STC LBA.21E2.TA0270
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REPLACEMENT OF ZONAL DRYER RELATED TO EASA AD 2006-0140-E.THE ABOVE...

Replacement of Zonal Dryer related to EASA AD 2006-0140-E.The above reference EASA AD required the de-activation of Zonal Drying Systems installed via LBA STC LBA.21E2.TA0270 due to the potential for combustion of contaminants in the dryer unit. A new drye Limitations: See related STC LBA.21E2.TA0270. Conditions: n/a
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REPLACEMENT OF ZONAL DRYER RELATED TO EASA AD 2006-0140-E.THE ABOVE...

Replacement of Zonal Dryer related to EASA AD 2006-0140-E.The above reference EASA AD required the de-activation of Zonal Drying Systems installed via LBA STC LBA.21E2.TA0636 due to the potential for combustion of contaminants in the dryer unit. A new drye Limitations: See related STC LBA.21E2.TA0636. Conditions: n/a
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REPLACEMENT OF ZONAL DRYER RELATED TO EASA AD 2006-0140-E.THE ABOVE...

Replacement of Zonal Dryer related to EASA AD 2006-0140-E.The above reference EASA AD required the de-activation of Zonal Drying Systems installed via LBA STC TA0733 due to the potential for combustion of contaminants in the dryer unit. A new dryer unit ha Limitations: See related STC TA0733. Conditions: n/a
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REPLACEMENT OF ZONAL DRYER RELATED TO EASA AD 2006-0140-E.THE ABOVE...

Replacement of Zonal Dryer related to EASA AD 2006-0140-E.The above reference EASA AD required the de-activation of Zonal Drying Systems installed via LBA STC LBA.21E2.TA0609 due to the potential for combustion of contaminants in the dryer unit. A new drye Limitations: See related STC LBA.21E2.TA0609. Conditions: n/a
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REPLACEMENT OF ZONAL DRYER RELATED TO EASA AD 2006-0140-ETHE ABOVE...

Replacement of Zonal Dryer related to EASA AD 2006-0140-EThe above reference EASA AD required the de-activation of Zonal Drying Systems installed via LBA STC LBA.21E2.0307 due to the potential for combustion of contaminants in the dryer unit. A new dryer u Limitations: See related STC LBA.21E2.0307. Conditions: n/a
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STRUCTURAL MODIFICATIONS FOR THE INSTALLATION OF A DUAL GPS ANTENNA...

Structural modifications for the installation of a dual GPS antenna in place of the existing Gatelink antenna
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REARRANGEMENT OF VIP CABIN INTERIOR (MAJLIS) & SYSTEMS AND MODIFICATION...

Rearrangement of VIP cabin interior (Majlis) & systems and modification of pax entertainment system (IFE) including installation oftailwind 560 Live TV system. Limitations: 1.This modification is limited to a/c serial number MSN29271.2. Occupancy of this zone is limited to Zero Passengers for Taxi, Take-off and Landing, pending substantiation of evacuation through the adjacent compartments. Conditions: n/a
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STRUCTURE MODIFICATION FOR GPS ANTENNAE INSTALLATIONTHIS STC DEFINES THE STRUCTURAL...

Structure modification for GPS antennae installationThis STC defines the structural modification for the installation of a dual GPS antennae, in place of the existing Gatelink antenna Limitations: n/a. Conditions: n/a
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CABIN COMPLETION - 15 PASSENGERS LIMITATIONS: 1. INSTALLATION OF "CL-600-2B19-INSTALLATION...

Cabin Completion - 15 Passengers Limitations: 1. Installation of "CL-600-2B19-Installation of Structural Provisions for Cabin Completion" approved with EASA STC No. EASA.A.S.03097, is required prior to installation of this STC.2. The Limitation "Installation of Ferry-Kit M/S TC 601R16990" given. Conditions: n/a
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CABIN COMPLETION - 15 PASSENGERS CERTIFICATION BASIS LIMITATIONS - LUFTHANSA...

Cabin Completion - 15 Passengers Certification Basis Limitations - Lufthansa Technik Supplement Type Definition Document No. STD00-07/08M Issue 1 dated 26 February 2008 or later approved revision- Airplane Flight Manual Supplement No. A-00-07/694-AFM Issue 01 or later approved revision Conditions 1. Installation of "CL-600-2B19-Installation of Structural Provisions for Cabin Completion" approved with EASA STC No. EASA.A.S.03097, is required prior to installation of thisSTC.2. The Limitation Installation ...
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A300B4-603 / -605R CABIN RECONFIGURATIONCABIN RECONFIGURATION FROM CURRENT VERSION (280...

A300B4-603 / -605R Cabin ReconfigurationCabin Reconfiguration from current version (280 MC) to two possible versions (58 CC / 188 MC or 40 CC / 220 MC). Limitations: The installation of this STC has a prerequisite aircraft configuration.2. This STC is only applicable on aircraft in association with the EASA STC ref: EASA.A.S.02663.3. The Certification Review Item A-01 has to be considered, in addition to the. Conditions: ...
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INSTALLATION OF A NEW STRETCHER FOR KUWAIT AIRWAYS LIMITATIONS: N/A....

Installation of a new Stretcher for Kuwait Airways Limitations: n/a. Conditions: n/a
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CABIN COMPLETION LIMITATIONS: 1. INSTALLATION OF "CL-600-2B19 - INSTALLATION OF...

Cabin Completion Limitations: 1. Installation of "CL-600-2B19 - Installation of structural provisions for cabin completion", approved with EASA STC No. EASA.A.S.03097 is required prior to the installation of this STC.2. The limitation "Installation of Ferry-Kit M/S TC 601R16990". Conditions: n/a
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CABIN COMPLETION CERTIFICATION BASIS LIMITATIONS LUFTHANSA TECHNIK SUPPLEMENTAL TYPE DEFINITION...

Cabin Completion Certification Basis Limitations Lufthansa Technik Supplemental Type Definition Document No.STDD00-07/07M Issue 01 dated 13/02/08 or later approved revision.Airplane Flight Manual Supplement No. A-00-07/693-AFM Issue 01 or later approved revision. Conditions 1. Installation of "CL-600-2B19 - Installation of structural provisions for cabin completion", approved with EASA STC No. EASA.A.S.03097 is required prior to the installation of this STC.2. The limitation Installation of Ferry-Kit M/S TC ...
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ZONAL DRYING SYSTEM INSTALLATION LIMITATIONS: N/A. CONDITIONS: N/A

Zonal Drying System Installation Limitations: n/a. Conditions: n/a
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INSTALLATION OF STRUCTURAL PROVISIONS FOR AEROH ANTENNA SYSTEM LIMITATIONS: 1....

Installation of Structural Provisions for AeroH Antenna system Limitations: 1. For all flights with "Green Aircraft" and "Structural Provisions for AeroH Antenna System" (2,5 [kg]) installed the installationof Ferry-Kit M/S TC 601R16990 (867 [kg]) is necessary.2. With the installation of Ferry-Kit M/S TC 601R16990 (867 [kg]) the a. Conditions: n/a
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INSTALLATION OF STRUCTURAL PROVISIONS FOR AEROH ANTENNA SYSTEM CERTIFICATION BASIS...

Installation of Structural Provisions for AeroH Antenna system Certification Basis Limitations LHT Declaration of Compliance No. 1613 dated 22 January 2008LHT Supplemental Type Definition Document No. STDD-07/06M dated 22 January 2008 Conditions 1. For all flights with "Green Aircraft" and Structural Provisions for AeroH Antenna System" (2,5 [kg]) installed the installationof Ferry-Kit M/S TC 601R16990 (867 [kg]) is necessary.2. With the installation of Ferry-Kit M/S TC ...
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INSTALLATION OF STRUCTURAL PROVISIONS FOR CABIN COMPLETION LIMITATIONS: 11. FOR...

Installation of Structural Provisions for Cabin Completion Limitations: 11. For all flights with "Green Aircraft" and "Structural Provisions for cabin completion" (293,7 [kg]) installed the installation of Ferry-Kit M/S TC 601R16990 (867 [kg]) is necessary.2. With the installation of Ferry-Kit M/S TC 601R16990 (867 [kg]). Conditions: n/a
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INSTALLATION OF STRUCTURAL PROVISIONS FOR CABIN COMPLETION CERTIFICATION BASIS LIMITATIONS...

Installation of Structural Provisions for Cabin Completion Certification Basis Limitations LHT Declaration of Compliance No. 1611 dated 29 January 2008LHT Supplemental Type Definition Document No. STDD00- 07/05M, Issue 1 dated 29 January 2008 Conditions 11. For all flights with "Green Aircraft" and Structural Provisions for cabin completion" (293,7 [kg]) installed the installation of Ferry- Kit M/S TC 601R16990 (867 [kg]) is necessary.2. With the installation of ...
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CL-600-2B19 - CABIN COMPLETION - 15 PAX # CONFIGURATION D....

CL-600-2B19 - Cabin Completion - 15 PAX # Configuration D. Certification Basis Limitations 1. Supplement Type Definition Document STDD00-05/12M, issue 04, dated November 13, 2007, or later approved revision2. Configuration Identification Document CID-15- 01619-LHT,issue 03, dated November 2, 2007, or later approved revisionConfigurat (...) Conditions 1. Certification Basis of Change: JAR-25 Change 13, additionally:Configuration A and B*:CRI D-01, Side facing Divan (Deviation)CRI F-01, Executive Power Systems ...
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CL-600-2B19 - CABIN COMPLETION - 15 PAX – CONFIGURATION D....

CL-600-2B19 - Cabin Completion - 15 PAX – Configuration D. Limitations: 1. Certification Basis of Change: JAR-25 Change 13, additionally:Configuration A and B*:CRI D-01, Side facing Divan (Deviation)CRI F-01, Executive Power Systems (Guidance Material)JAA TGL No. 17, Passenger service and In-Flight Entertainment (IFE) syste. Conditions: n/a
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INSTALLATION OF A NEW STRETCHER FOR KUWAIT AIRWAYS. LIMITATIONS: N/A....

Installation of a new Stretcher for Kuwait Airways. Limitations: n/a. Conditions: n/a
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INSTALLATION OF A ROCKWELL COLLINS TAILWIND 550 LIVE TV SYSTEM...

Installation of a Rockwell Collins Tailwind 550 Live TV system in Boeing MD-11 as detailed in STDD53-06/19M Supplemental Type Definition Document for Tailwind 550 Live TV installation MD-11 Limitations: n/a. Conditions: n/a
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INSTALLATION OF A NEW STRETCHER FOR KUWAIT AIRLINES B747-400 IN...

Installation of a new stretcher for Kuwait Airlines B747-400 in accordance with Supplemental Type Definition Document STDD25-06 09MIss. 01, Rev. 01 or later EASA approved revision. Limitations: n/a. Conditions: n/a
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INSTALLATION OF ZONAL DRYING SYSTEM LIMITATIONS: PRIOR TO INSTALLATION OF...

Installation of Zonal Drying System Limitations: Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install. Conditions: n/a
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INSTALLATION OF A STRETCHER IN THE PASSENGER COMPARTMENT FOR KUWAIT...

Installation of a stretcher in the passenger compartment for Kuwait Airways Limitations: Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install. Conditions: n/a
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WLAN INSTALLATIONDESIGN AND IMPLEMENTATION OF WIRELESS LOCAL AREA NETWORK SYSTEM...

WLAN InstallationDesign and implementation of Wireless Local Area Network System Limitations: n/a. Conditions: n/a
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INSTALLATION OF A NEW STRETCHER FOR KUWAIT AIRWAYS LIMITATIONS: PRIOR...

Installation of a new Stretcher for Kuwait Airways Limitations: Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install. Conditions: n/a
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PTU AND/OR STRETCHER INSTALLATION ON A319-100 /OPTIONAL REPLACEMENT OF SEATS...

PTU and/or Stretcher Installation on A319-100 /Optional replacement of seats by up to 2 Passenger Transport Units (PTU) and/or up to 4 stretchers. Limitations: • Detailed visual inspection of the Oxygen Discharge Plug at an interval of 750 FC ( C check ), as reported in the document Instruction for Continued Airworthiness, ref. Doc. A-00-07/641-ICA Issue 03, dated 19.09.07. Conditions: n/a
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CL-600-2B19 CABIN COMPLETION - 13 PAX CERTIFICATION BASIS LIMITATIONS SUPPLEMENTAL...

CL-600-2B19 Cabin Completion - 13 PAX Certification Basis Limitations Supplemental Type Definition Document STDD00-06/11M, Issue 01, dated September 18, 2007 or later approved revisionAeroplane Flight Manual Supplement A-00-07/580-AFM, Issue 01, dated June 13, 2007 or later approved revision.Instructions forContinued (...) Conditions 1. Certification Basis of Change: JAR-25 Change 13, additionally:CRI D-01, Side- Facing DivanCRI D-04, Door between passenger compartment with integrated blocking functionalityCRI D-05, Isolated compartmentCRI ...
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CL-600-2B19 CABIN COMPLETION - 13 PAX LIMITATIONS: 1. CERTIFICATION BASIS...

CL-600-2B19 Cabin Completion - 13 PAX Limitations: 1. Certification Basis of Change: JAR-25 Change 13, additionally:CRI D-01, Side-Facing DivanCRI D-04, Door between passenger compartment with integrated blocking functionalityCRI D-05, Isolated compartmentCRI F-01, Executive Power SystemJAA TGM Leaflet No.. Conditions: n/a
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ZONAL DRYING SYSTEM INSTALLATION LIMITATIONS: PRIOR TO INSTALLATION OF THIS...

Zonal Drying System Installation Limitations: Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install. Conditions: n/a
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REMOVAL OF ANTENNA AND RECEIVER TRANSMIT SYSTEM AND NETWORK SERVICES....

Removal of Antenna and Receiver Transmit System and Network Services. Limitations: The AFM Supplement Doc. No. A-00-04/133 can be removed with the installation of this STC.. Conditions: n/a
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REMOVAL OF ANTENNA AND RECEIVER TRANSMIT SYSTEM AND NETWORK SERVICES...

Removal of Antenna and Receiver Transmit System and Network Services Limitations: The AFM Supplement Doc. No. A-00-04/072 can be removed with the installation of this STC.. Conditions: n/a
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REMOVAL OF ANTENNA AND RECEIVER TRANSMIT SYSTEM AND NETWORK SERVICES...

Removal of Antenna and Receiver Transmit System and Network Services Limitations: The AFM Supplement Doc. No. A-00-04/5856 can be removed with the installation of this STC.. Conditions: n/a
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A330 - INSTALLATION OF ZONAL DRYING SYSTEM /THE SYSTEM IS...

A330 - Installation of Zonal Drying System /The system is installed to get rid of the humidity between the cabin lining and the fuselage Limitations: n/a. Conditions: n/a
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NAVIGATION # RETROFIT OF DUAL FMC CERTIFICATION BASIS LIMITATIONS COMPLIANCE...

Navigation # Retrofit of Dual FMC Certification Basis Limitations Compliance Record List CRL 34-07/01M, issue 1 (rev. 0)AFM Supplement LBAS310060301, issue IRInstruction for Continued Airworthiness LBAS310071201, issue IR (rev. 0) Conditions None
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CL-600-2B19 - CABIN COMPLETION - 16 PAX LIMITATIONS: 1. CERTIFICATION...

CL-600-2B19 - Cabin Completion - 16 PAX Limitations: 1. Certification Basis of the Change: JAR-25 Change 13, addtionally: CRI F-01, Executive Power System (Guidance Material)CRI D-01, Side Faching Divans (Deviation)CRI D-04, Door between passenger compartments with integrated blocking functionality (Deviatio. Conditions: n/a
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CL-600-2B19 - CABIN COMPLETION - 16 PAX CERTIFICATION BASIS LIMITATIONS...

CL-600-2B19 - Cabin Completion - 16 PAX Certification Basis Limitations Supplemental Type Definition Document STDD00-06/06M, Issue 01, dated March 27, 2007 or later approved revisionsAeroplane Flight Manual Supplement A-00-06/461-AFM, Issue 01, dated January 05, 2007 or later approved revisionsInstructions forContinued (...) Conditions 1. Certification Basis of the Change: JAR-25 Change 13, addtionally: CRI F-01, Executive Power System (Guidance Material)CRI D-01, Side Faching Divans (Deviation)CRI D-04, Door ...
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A300F4-605R MULTI MODE RECEIVER (MMR) AND GLOBAL POSITIONING SYSTEM (GPS)...

A300F4-605R Multi Mode Receiver (MMR) and Global Positioning System (GPS) installation Limitations: n/a. Conditions: n/a
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ATC MODE S – ENHANCED SURVEILLANCE UPGRADE LIMITATIONS: COMPATIBILITY OF...

ATC Mode S – Enhanced Surveillance Upgrade Limitations: Compatibility of this design change with other previously approved modifications must be determined by the installer.. Conditions: n/a
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INTRODUCTION OF LINK 2000+ LIMITATIONS: CERTIFICATION BASIS OF THE CHANGE:...

Introduction of Link 2000+ Limitations: Certification Basis of the Change: CS 25 Amdt 02. Conditions: n/a
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INTERIOR AND SYSTEMS INSTALLATION INCL. CONVERTIBLE CABIN CONFIGURATION LIMITATIONS: INSTRUCTION...

Interior and systems installation incl. convertible cabin configuration Limitations: Instruction for Continued Airworthiness, Airworthiness Limitations, Section 4.3, ref. C- AAA000-ICA, issue 2, dated January 12, 2007or later approved revision. Conditions: n/a
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A300B4-603 CABIN RECONFIGURATION FROM CURRENT VERSIONS TO INTERCONTINENTAL LAYOUTCABIN RECONFIGURATION...

A300B4-603 Cabin Reconfiguration from current versions to Intercontinental LayoutCabin Reconfiguration from current versions (total 280 and 232 Passengers) to Intercontinental Layout (total 217 Passengers). Limitations: This STC is approved only for the product configuration as defined in the approved design data referred to in paragraph ‘Description’. Compatibility with other aircraft/engine configurations shall be determined by the installer.. Conditions: n/a
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ATC SYSTEM, UPGRADE TO ENHANCED SURVEILLANCENOTE: THIS REVISION EXPANDS THE...

ATC System, Upgrade to Enhanced SurveillanceNote: This Revision expands the application range of the existing STC. Limitations: 1. Certification Basis of the change: CS 25 Change O, additionaly JAA Leaflet No. 18 (Mode-S EHS)2. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibili. Conditions: n/a
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STRUCTURAL MOUNTING PROVISION FOR LARGE ANTENNA AND RANDOM FOR LIVE...

Structural mounting provision for large antenna and random for Live TV Tailwind 560 Limitations: 1. EASA CS25, without Amendment, Certification Specifications for Large Aeroplanes plus FAA Generic Issue Paper A-X "Structural Certification Criteria for Large Antenna Installations".2. This STC is approved only for the product configuration as defined in. Conditions: n/a
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VVIP CABIN INSTALLATIONSTDD 25-05 / 06M ISSUE 1, STDD 25-05...

VVIP Cabin InstallationSTDD 25-05 / 06M issue 1, STDD 25-05 / 19 issue1 Limitations: --. Conditions: n/a
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INSTALLATION OF THE CONNEXION BY BOEING NEXT GENERATION ANTENNA SYSTEM...

Installation of the Connexion By Boeing Next Generation Antenna System and Wireless Airborne Local Area Network.
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INSTALLATION OF PNEUMATIC METRIC ALTIMETER LIMITATIONS: CERTIFICATION BAISIS OF THE...

Installation of Pneumatic Metric Altimeter Limitations: Certification Baisis of the Change: CS-25 Amdt. 1. Conditions: n/a
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UPGRADE PACKAGE OF EXISTING VIP CABIN CONFIGURATION FROM PRIVATE OPERATION...

Upgrade Package of existing VIP Cabin Configuration from private Operation to Commercial Operation Limitations: As indicated in the applicable AFM Supplement:- A_00_01_311_AFM Supplement Cabin TT&L for Private Operation- A_25_06_17M_ AFM Supplement Cabin TT&L for Commercial Operation.And as indicated in the LBA STC LBA.21E2.TA0307Compatibility of this design c. Conditions: n/a
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INSTALLATION OF THE CONNEXION BY BOEING NEXT GENERATION ANTENNA SYSTEM...

Installation of the Connexion By Boeing Next Generation Antenna System and Wireless Airborne Local Area Network.
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INSTALLATION OF AN ATC MODE S - ENHANCED SURVEILLANCE UPGRADE...

Installation of an ATC Mode S - Enhanced Surveillance Upgrade in Boeing 747 series aircraft Limitations: EASA approved Airplane Flight Manual Supplement, Lufthansa Technik Document A- 34-06/135-AFM, Rev IR or later EASA approved revisionis required part of this STC. Conditions: n/a
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A319 CJ VIP CABIN 34 PAX LIMITATIONS: 1. JAR-25 CHANGE...

A319 CJ VIP Cabin 34 Pax Limitations: 1. JAR-25 Change 112. FAR 25.981 (a) (b) Amdt. 102 'Fuel Tank [ignition prevention]'3. 'CRI D-03 'Type III Emergency Exit Access' dated 31. March 20064. CRI F-01 'Dimestic Power' dated 18 May 20065. TGL No. 17 'Passenger Service and In-Flight Entertainment. Conditions: n/a
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INTRODUCTION OF TAILWIND 550 ANTENNA AND LIVE TV FOR VIP...

Introduction of Tailwind 550 Antenna and Live TV for VIP B777-200. Limitations: This modification is limited to a/c serial number MSN29271.. Conditions: n/a
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A310-300 SIBERIA AIRLINES CABIN RECONFIGURATION FROM 248 TO 255 PAX...

A310-300 Siberia Airlines Cabin Reconfiguration from 248 to 255 pax Limitations: n/a. Conditions: n/a
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A300-600 CABIN RECONFIGURATION FROM CURRENT CONTINENTAL VERSION TO INTERCONTINENTAL LAYOUT...

A300-600 Cabin Reconfiguration from Current Continental Version to Intercontinental Layout Limitations: This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer.. Conditions: n/a
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A320 PAX CAPACITY INCREASE FROM 156 TO 168 PAX

A320 Pax Capacity Increase from 156 to 168 Pax
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INSTALLATION OF NEW RECARO AIRCRAFT SEATING CONVERTIBLE AND STANDARD SEATS...

Installation of new Recaro Aircraft Seating convertible and standard seats and cabin refurbishment to PG-design on Lufthansa's Boeing B737-500 aircraft. Limitations: Certification Basis of the change: FAR25 as defined in FAA TCDS A16WE.. Conditions: n/a
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ATC, SYSTEM UPGRADE FOR EHS LIMITATIONS: CERTIFICATION BASIS OF THE...

ATC, System Upgrade for EHS Limitations: Certification Basis of the Change: CS 25 Change 0, additionally JAA Leaflet No 18 (Mode-S EHS). Conditions: n/a
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COMMUNICATION - MODIFICATION/UPGRADE OF THE IN-FLIGHT ENTERTAINMENT SYSTEM, INSTALLATION OF...

Communication - Modification/Upgrade of the In-Flight Entertainment System, Installation of Tailwing 560 Live TV Equipment. Limitations: EASA CS25, without Amendment, Certifications Specifications for Large Aeroplanes plus JAA INT/POL/25/3 Issue 2, JAA INT/POL/25/4 Issue 3, JAA Leaflet No. 17.. Conditions: n/a
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ATC, SYSTEM UPGRADE FOR EHS LIMITATIONS: CERTIFICATION BASIS OF THE...

ATC, System Upgrade for EHS Limitations: Certification Basis of the Change: CS 25, additionaly JAA Leaflet No. 18 (Mod-S EHS). Conditions: n/a
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INSTALLATION OF NEW RECARO SEATING CONVERTIBLE AND STANDARD SEATS AND...

Installation of new Recaro Seating convertible and standard seats and cabin refurbishment to PG-design on Lufthansa's Boeing B737-300 aircraft Limitations: Certification Basis of the change: FAR25 as defined in FAA TCDS A16WE. The applicant showed compliance to CS 25.0785(h)(2), CS 25.811(d), (g), CS 25.812€, CS 25.0853(a), (c), (d), (f).. Conditions: n/a
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INSTALLATION OF NEW B/E AEROSPACE CONVERTIBLE AND STANDARD SEATS AND...

Installation of new B/E Aerospace convertible and standard seats and cabin refurbishment to PG-design on Lufthansa's A321 aircrafts Limitations: This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer.. Conditions: n/a
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INSTALLATION OF NEW B/E AEROSPACE CONVERTIBLE AND STANDARD SEATS AND...

Installation of new B/E Aerospace convertible and standard seats and cabin refurbishment to PG-design on Lufthansa's A320 aircrafts Limitations: n/a. Conditions: n/a
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INSTALLATION OF NEW B/E AEROSPACE CONVERTIBLE AND STANDARD SEATS AND...

Installation of new B/E Aerospace convertible and standard seats and cabin refurbishment to PG-design on Lufthansa's A319 aircrafts Limitations: n/a. Conditions: n/a
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BUSINESS CLASS INSTALLATION WITH SICMA SEATS

Business Class Installation with Sicma Seats
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BUSINESS CLASS INSTALLATION WITH SICMA SEATS LIMITATIONS: N/A. CONDITIONS: N/A

Business Class Installation with Sicma Seats Limitations: n/a. Conditions: n/a
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INSTALLATION OF ARINC-429 INTERFACE BETWEEN INERTIAL REFERENCE UNITS (IRUS), AFCS...

Installation of ARINC-429 interface between Inertial Reference Units (IRUs), AFCS Mode Control Panel (MCP) and both ATC/Mode S transponders.
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B747-400 BAHRAIN ROYAL FLIGHT, VIP CABIN INSTALLATION LIMITATIONS: N/A. CONDITIONS:...

B747-400 Bahrain Royal Flight, VIP Cabin Installation Limitations: n/a. Conditions: n/a
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INSTALLATION OF GUIDELINE-SELF ILLUMINATING FLOOR PATH MARKING SYSTEM. LIMITATIONS: N/A....

Installation of Guideline-Self Illuminating Floor Path Marking System. Limitations: n/a. Conditions: n/a
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INSTALLATION OF ANTENNA AND RECEIVER TRANSMIT SYSTEM AND NETWORK SERVICES(ACC.:...

Installation of Antenna and Receiver Transmit System and Network Services(acc.: STDD 00- 03/11M issue 02) Limitations: 1. "The IEEE 802.11 a, b, g (as customized) Wireless Local Area Network (WLAN) introduced by this modification, may be activated onboard Airbus A340-600 Aircraft for operation with commercial IEEE 802.11a, b, g & h compliant WLAN enabled portable electroni. Conditions: n/a
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"INSTALLATION OF COMMUNICATION SYSTEM IFE UPDATE"ACC.: STDD 23-05/07M LIMITATIONS: LIMITED...

"Installation of Communication System IFE Update"acc.: STDD 23-05/07M Limitations: Limited to s/n 354. Conditions: n/a
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CABIN AND IFE MODIFICATION AS DEFINED IN SUPPLEMENTAL TYPE DEFINITION...

Cabin and IFE Modification as defined in Supplemental Type Definition DocumentSTDD00 - 05/05 M, Issue 01, Rev.00 Limitations: n/a. Conditions: n/a
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B747-400 GUGGENHEIM SEAT ARRANGEMENT MODIFICATION FROM 384 PASSENGERS (MAIN DECK16...

B747-400 Guggenheim Seat Arrangement Modification from 384 passengers (main deck16 FC, 28 BC, 310 Y) to 398 passengers (main deck 12 FC, 0 BC, 46 Y + 310 Y) according to STD00-05/10M Limitations: n/a. Conditions: n/a
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INSTALLATION OF THE CONNEXION BY BOEING NEXT GENERATION ANTENNA SYSTEM...

Installation of the Connexion By Boeing Next Generation Antenna System and network services via Wireless Airborne Local Area Network (Wireless ALAN)
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"AVIONICS UPGRADE BY- INSTALLATION OF TCAS- INSTALLATION OF DUAL MODE...

"Avionics Upgrade by- Installation of TCAS- Installation of Dual Mode S Transponder- Installation of Add. Parameters for Digital FDR- Digital Flight Data Acquisition Unit, Software Upgrade- Installation of Enhanced Ground Proximity Warning System" Limitations: n/a. Conditions: n/a
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INSTALLATION OF AN OPTICAL QUICK ACCESS RECORDER (OQAR) ACCORDING TO...

Installation of an Optical Quick Access Recorder (OQAR) according to LHT Engineering Bulletin No. 767-EB31-0203, dated 09.09.04 or later approved Revision for FOQA Purpose Limitations: This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other Aircraft configurations shall be determined by the installer.. Conditions: n/a
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INSTALLATION OF AN OPTIAL QUICK ACCESS RECORDER (OQAR) ACCORDING TO...

Installation of an Optial Quick Access Recorder (OQAR) according to LHT Engineering Bulletin No.737-EB31- 0202, dated 29.09.04 or later approved Revision for FOQA Purpose. Limitations: This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other Aircraft configurations shall be determined by the installer.. Conditions: n/a
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"INSTALLATION OF ANTENNA AND RECEIVER TRANSMIT SYSTEM AND NETWORK SERVICES"....

"Installation of Antenna and Receiver Transmit System and Network Services". Acc.: STDD 00-04/10M. Ref. to former LBA STCs: TA0810 and TA0811. AFM Suppllement: A-34-05/260- AFM. ICA: R-00-04/120 Limitations: "The IEEE 802.11 a,b,g (as customized) Wireless Local Area Network (WLAN) introduced by this midification, may be activated on board Airbus A340-600 Aircraft for operation with commercial IEEE 802.11a, b, g & h compliant WLAN enabled portable electronic ...
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PROVISIONS FOR INSTALLATION OF PC POWER AND PC DATA OUTLETS...

Provisions for installation of PC Power and PC Data Outlets on the existing Business Class seats and installation of new Avio Economy Class seats.
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NAVIGATION - INTRODUCTION OF ATC MODE S ENHANCED SURVEILLANCE LIMITATIONS:...

Navigation - Introduction of ATC Mode S Enhanced Surveillance Limitations: n/a. Conditions: n/a
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ATC, SYSTEM UPGRADE FOR ENHANCED SURVEILLANCE, ACC.: STDD 34-05/06M LIMITATIONS:...

ATC, System Upgrade for Enhanced Surveillance, acc.: STDD 34-05/06M Limitations: 1. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer.. Conditions: n/a
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INSTALLATION OF NETWORK SERVICES VIA WIRELESS AIRBORNE LOCAL AREA NETWORK...

Installation of network services via Wireless Airborne Local Area Network (Wireless ALAN) in accordance with Lufthansa Technik Supplemental Type Definition Document STDD 00-04/09M, Issue 00, dated May 25, 2003. The airborne LAN system provides internet services to the passengers and interfaces with the Connexion by Boeing Next Generation Antenna System.
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INSTALLATION OF THE CONNEXION BY BOEING NEXT GENERATION ANTENNA SYSTEM,...

Installation of the Connexion By Boeing Next Generation Antenna System, in accordance with Lufthansa Technik Supplemental Type Definition Document STDD00-04/10M, Issue 00, dated May 25, 2003, to be used for Airborne Local Area Network System by passengers.
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NAVIGATION - ATC SYSTEM, INSTALLATION OF UPGRADE FOR ENHANCED SURVEILLANCE...

Navigation - ATC system, Installation of Upgrade for Enhanced Surveillance and associated Airplane Flight Manual Supplement. Limitations: n/a. Conditions: n/a
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B-767- CABIN LAYOUT CHANGE - AIR EUROPE LIMITATIONS: N/A. CONDITIONS:...

B-767- Cabin Layout Change - Air Europe Limitations: n/a. Conditions: n/a
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FLIGHT MANAGEMENT SYSTEM (FMS), ACTIVATION OF ADVISORY VNAV MODEACCORDING TO...

Flight Management System (FMS), Activation of Advisory VNAV Modeaccording to Lufthansa Technik Supplemental Type Definition Document STDD34-05/02M, Issue 01, Rev 00, dated April 20, 2005 or laterapproved revision Limitations: n/a. Conditions: n/a
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A330-200 AIR ALGERIE QUICK CHANGE VIP KIT ONEPLUS. LIMITATIONS: N/A....

A330-200 Air Algerie Quick Change VIP Kit OnePlus. Limitations: n/a. Conditions: n/a
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INSTALLATION OF PC POWER AND PC DATA OUTLETS ON THE...

Installation of PC Power and PC Data Outlets on the existing B/C Seats and installation of new ECO Class Seats with new P/N and PC- Power/PC-Data Outlets on Boeing 777-300 A/C of Cathay Pacific Airways. Limitations: n/a. Conditions: n/a
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INSTALLATION OF A VIP EXECUTIVE INTERIOR. APPROVED FOR BOEING 737-800...

Installation of a VIP Executive Interior. Approved for Boeing 737-800 model, serial number 32438 ONLY.
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STRUCTURAL PROVISIONS FOR INSTALLATION OF A VERTICAL STABILIZER TIP RADOME....

Structural provisions for installation of a vertical stabilizer tip radome. For model 737-700 IGW and 737-800
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