MODIFICATIONS OF STC Twenty One Limited (105)

ACTIVATION CONTROLLER PILOT DATA-LINK COMMUNICATIONS [CPDLC] CAPABILITY

Activation of a Controller-Pilot Data-Link Communications [CPDLC] capability on Spectralux "D-LINK" ACARS VDL Mode 2 transceiver.
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GOGO 2KU - STRUCTURAL PROVISIONSREV.1: EDITORIAL CORRECTION

Gogo 2KU - Structural ProvisionsRev.1: Editorial Correction
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CERTIFICATION OF AIRCRAFT CONFIGURATION AFTER THE REMOVAL OF LIVETVSYSTEM APPROVED...

Certification of aircraft configuration after the removal of LiveTVsystem approved under FAA STC ST00788SE.
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INTRODUCTION OF VIP CABIN RECONFIGURATION

Introduction of VIP Cabin Reconfiguration
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CONVERSION OF THE MAIN PASSENGER CABIN TO A CLASS E...

Conversion of the main passenger cabin to a class E cargo compartment for the carriage of freight and change to the location of rapid decompression vents for planned future bulk cargo loading operations
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INSTALLATION OF BULK CARGO RESTRAINT SYSTEM WITH TRANSVERSE NETS AT...

Installation of bulk cargo restraint system with transverse nets at discrete positions in the aircraft main cabin converted to class E cargo compartment
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UPGRADE TO CABIN INTERIOR.

Upgrade to Cabin Interior.
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INTRODUCTION OF CORPORATE VIP INTERIOR

INTRODUCTION OF CORPORATE VIP INTERIOR
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INSTALLATION OF GOGO 2KU-STRUCTURAL AND ELECTRICAL PROVISIONS

Installation of Gogo 2KU-Structural and Electrical Provisions
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INSTALLATION OF GOGO 2KU - SYSTEM ACTIVATION

INSTALLATION OF GOGO 2KU - System Activation
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SAAB 340 CLASS E CARGO COMPARTMENT (AS DEFINED IN DOCUMENT...

Saab 340 Class E Cargo Compartment (as defined in document S21MDL-0033). This is a major change of the EASA STC EASA.A.S. 01681. It isdesigned by STC Twenty One Limited and will document changes to thelocation of rapid decompression vents for planned future bulk cargoloading operations.This STC appro...
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INTRODUCTION OF AFIRS 228.

Introduction of AFIRS 228.
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INSTALLATION OF GOGO 2KU - STRUCTURAL AND ELECTRICAL PROVISIONS

INSTALLATION OF GOGO 2KU - STRUCTURAL AND ELECTRICAL PROVISIONS
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INSTALLATION OF AN AVIATOR 300 SWIFTBROADBAND SYSTEM

Installation of an Aviator 300 SwiftBroadband System
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INSTALLATION OF GOGO 2KU – STRUCTURAL AND ELECTRICAL PROVISIONS

Installation of Gogo 2KU – Structural and Electrical Provisions
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INTRODUCTION OF TCAS CHANGE 7.1

Introduction of TCAS Change 7.1
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INSTALLATION OF GOGO 2KU - STRUCTURAL AND ELECTRICAL PROVISIONS.

Installation of Gogo 2KU - Structural and Electrical Provisions.
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INTRODUCTION OF UPGRADED IFE, CABIN LIGHTING AND UNIVERSAL OUTLETS

Introduction of Upgraded IFE, Cabin Lighting and Universal Outlets
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ACTIVATION OF A CONTROLLER-PILOT DATA-LINK COMMUNICATIONS [CPDLC]CAPABILITY ON SPECTRALUX "D-LINK"...

Activation of a Controller-Pilot Data-Link Communications [CPDLC]capability on Spectralux "D-LINK" ACARS VDL Mode 2 transceiver.Amendment to STC 10039812 Rev 2
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ATR - INSTALLATION OF A DUAL GARMIN GTN-725 GPS NAVIGATOR...

ATR - Installation of a dual Garmin GTN-725 GPS Navigator System forEuropean P-RNAV complianceThe purpose of this modification is to install a dual Garmin GTN-725 GPSnavigator system with 2 Garmin GA-36 WAAS/GPS antennas, as a replacementto the existing Honeywell GPS systems (KLN900 or KLN90B). Thei...
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INTRODUCTION OF CORPORATE VIP INTERIOR LIMITATIONS: STC TWENTY ONE LTD...

Introduction of Corporate VIP Interior Limitations: STC Twenty One Ltd Master Document List No. S21.MDL-1081 Issue 2STC Twenty One Ltd Flight Manual Supplement No. S21.FMS- 0100 Issue 1or later revisions of the above listed documents approved by EASA Conditions: None
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INTRODUCTION OF TCAS 2000 V7.1 LIMITATIONS: MASTER DOCUMENT LIST -...

Introduction of TCAS 2000 v7.1 Limitations: Master Document List - S21.MDL-1105 Issue 1Flight Manual Supplement - S21.FMS-0096 Issue 1Flight Manual Supplement - S21.FMS- 0098 Issue 1or later revisions of the above listed documents approved by EASA. 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 ...
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INTRODUCTION OF SATLINK ANTENNA IN ACCORDANCE WITH ARCHEIONHOLDINGSLLC. IRIDIUM ANTENNA...

Introduction of SatLINK antenna in accordance with ArcheionHoldingsLLC. Iridium Antenna Installation Subkit 2604773K- 1-101 Revision H Limitations: Report 26047-ICA Rev F: Instructions for Continued Airworthiness for the installation of an Avionica Inc. SatLINK communication management system with cabin wireless capability in a Boeing 737-300/-400/-700/-800 series aircraft or later revisions of the above listed documents approved by EASA. Conditions: Prior to installation of this design change it ...
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INTRODUCTION OF REPLACEMENT ELT ANTENNA ONTO REPAIRED FUSELAGE CROWNSKIN FS...

Introduction of replacement ELT Antenna onto repaired fuselage crownskin FS 837, Str 1 to 2R. Limitations: Compliance checklist S21.CCL-1129 dated May 02nd, 2013Master Document List S21.MDL-1129 dated May 02nd, 2013Compliance record S21.COMP-1128 dated April 30th, 2013Technical Report S21.TREP-1722 dated April 30th, 2013or later revisions of the above listed documents approved by EASA Conditions: Applicability limited to aircraft Serial Number 29072Prior to installation of this design change ...
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ACTIVATION OF A CONTROLLER-PILOT DATA-LINK COMMUNICATIONS [CPDLC]CAPABILITY ON SPECTRALUX "D-LINK"...

Activation of a Controller-Pilot Data-Link Communications [CPDLC]capability on Spectralux "D-LINK" ACARS VDL Mode 2 transceiver. Limitations: -Certification Programme S21.PROG-0813, Issue 3, dated 12 February 2012-Compliance Check List, S21.CCL, Issue 2, dated 22 February 2012-Master Data List S21.MDL- 0813, Issue 1, dated 19 April 2012-AFM Supplement S21.FMS-0069, Issue 3, dated7 March 20 (...) Conditions: This CPDLC installation is only intended to be used for routine datalinkexchanges during ...
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INTRODUCTION OF VHF COMM & SATCOM ANTENNAS. LIMITATIONS: STC TWENTY...

Introduction of VHF Comm & Satcom Antennas. Limitations: STC Twenty One Limited Master Document List No. S21.MDL-0998 Initial Issue dated 07 March 2013;Instructions for Continued Airworthiness Supplement Manual No.S21.TEC-0370;or later revisions of the above listed documents approved by EASA. Conditions: Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair ...
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UPGRADE TO EXISTING VIP INTERIOR.THIS REV. 1 IS TO AMEND...

Upgrade To Existing VIP Interior.This Rev. 1 is to amend a typographical error in Description of Designchange". Certification Basis The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:- Special Condition(s): D-05 Glass Screens of Displays and MonitorsThe requirements for environmental protection and the (...) Limitations STC Twenty One Master Document List No. S21.MDL-1118 Initial Issue,dated 21 March 2013;Instructions for Continued ...
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INTRODUCTION OF CABINVU 123 CABIN SURVEILLANCE SYSTEM. LIMITATIONS: INSTALLATION MUST...

Introduction of CabinVu 123 Cabin Surveillance System. Limitations: Installation must be in accordance with STC Twenty One Master Document List S21.MDL- 0826,Issue 3;Maintenance must be in accordance with Supplement Manual S21.TEC-0278,Issue 3;Operation must be in accordance with AD Aerospace Operating Manual CabinVu (...) Conditions: Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design ...
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STC TWENTY ONE LIMITED PROJECT NO. S21.53- 115-1037INSTALLATION OF SATCOM...

STC Twenty One Limited Project No. S21.53- 115-1037Installation of Satcom AntennaThis design change introduce a satcom antenna to the crown skin of theaircraft. The design change is limited to the mechanical changes to theaircraft only.The antenna wi (...) Certification Basis The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the ...
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INTRODUCTION OF IRIDIUM ANTENNA. LIMITATIONS: NONE.. CONDITIONS: PRIOR TO INSTALLATION...

Introduction of Iridium Antenna. 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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INTRODUCTION OF ANTENNA MOUNTING PROVISION LIMITATIONS: NONE. CONDITIONS: PRIOR TO...

Introduction of Antenna Mounting Provision 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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INTRODUCTION OF SWIFT BROADBAND CERTIFICATION BASIS EASA.IM.A.023THE CERTIFICATION BASIS FOR...

Introduction of Swift Broadband Certification Basis EASA.IM.A.023The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original product areunch (...) Limitations STC Twenty One Ltd Master Document List No. S21.MDL-0879 Issue 3.Flight Manual Supplement No. S21.FMS-0078 Issue 1.or later revisions of the above listed documents approved by EASA Conditions none
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INTRODUCTION OF CUSTOM INTERIOR LIMITATIONS: THIS DESIGN CHANGE APPROVAL IS...

Introduction of Custom Interior Limitations: This design change approval is applicable on Aircraft model AirbusA319-115, aircraft serial number 4622. Any subsequent change to the modes of operation of the WLAN approvedunder this design change will require a re-examination to determine ifthe complianc. Conditions: This STC has associated a supplement to the original TC Holder’s EWISInstructions for Continued Airworthiness. This supplement KCJ1- 0000RR100"Instructions for continued airworthiness (EWIS)" ...
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INTRODUCTION OF AN AVIONICA MINI QUICK ACCESS RECORDER MK III...

Introduction of an Avionica Mini Quick Access Recorder MK III withCellular Module 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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INTRODUCTION OF CABINVU 123 CABIN SURVEILLANCE SYSTEM. LIMITATIONS: NONE.. CONDITIONS:...

Introduction of CabinVu 123 Cabin Surveillance System. 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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INTRODUCTION OF CORPORATE INTERIOR CERTIFICATION BASIS EASA.IM.A.023THE CERTIFICATION BASIS FOR...

Introduction of Corporate Interior Certification Basis EASA.IM.A.023The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original product areunch (...) Limitations STC Twenty One Master Document List No. S21.MDL-0954 Initial Issue,dated 22 September 2011Midcoast Aviation AFMS No. 34-424M005Midcoast Aviation AFMS No. 34- 261M017or later revisions of the above listed documents ...
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OMNIBUS MODIFICATION FOR THE APPROVAL OF AIR NEW ZEALAND ENGINEERINGORDERS...

Omnibus Modification for the Approval of Air New Zealand EngineeringOrders Embodied on the A/C 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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CUSTOMIZED INTERIOR COMPLETION - ASN 9308 CERTIFICATION BASIS EASA.IM.A.009THE CERTIFICATION...

Customized Interior Completion - ASN 9308 Certification Basis EASA.IM.A.009The Certification Basis for the original product remains applicable tothis certificate/ approvalThe requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original product areuncha (...) Limitations STC Twenty One Ltd Master Document List No S21.MDL-0794 Issue 1STC Twenty One Ltd Flight Manual Supplement No. S21.FMS- 0084 Issue 1Midcoast Aviation Inc. Instructions for Continued ...
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CUSTOM INTERIOR A320 JUBILEE LIMITATIONS: THIS DESIGN CHANGE APPROVAL IS...

Custom Interior A320 Jubilee Limitations: This design change approval is applicable on Aircraft model AirbusA320-214, aircraft serial number 4199.. Conditions: This STC has associated a supplement to the original TC Holder's EWISInstructions for Continued Airworthiness. This supplement is included inthe document JUBL-CCR-400-EWA "Instructions for continued airworthiness(EWIS source document)" Prior to installatio
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INTRODUCTION ON EMB-145 OF SAFTGLO PHOTOLUMINESCENT FPEEPMS LIMITATIONS: NONE. CONDITIONS:...

Introduction on EMB-145 of Saftglo photoluminescent FPEEPMS 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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INTRODUCTION OF NUMBER 2 GALLEY ASSEMBLY LIMITATIONS: NONE. CONDITIONS: PRIOR...

Introduction of Number 2 Galley Assembly 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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CARRIAGE OF HORSES & GROOMS IN FREIGHTER A/C LIMITATIONS: THIS...

Carriage of Horses & Grooms in Freighter a/c Limitations: This design change is applicable to Boeing 757- 200 aircraft convertedunder Boeing's Special Freighter Programme, approved by the UK CAA underAirworthiness Approval Note AAN 27308 (acceptable to EASA under the EASAGrandfather provisions).. 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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REMOVAL OF DIVAN SEATING RESTRICTION CERTIFICATION BASIS EASA IM.A.023THE CERTIFICATION...

Removal of Divan Seating Restriction Certification Basis EASA IM.A.023The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original product areunch (...) Limitations STC 21.MDL-0793 Issue 1 dated 30 September 2010.or later revisions of the above listed documents approved by EASA Conditions This design change will allow the removal of ...
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REMOVAL OF DIVAN SEATING RESTRICTION LIMITATIONS: THIS DESIGN CHANGE WILL...

Removal of Divan Seating Restriction Limitations: This design change will allow the removal of an existing limitation onoccupation of the forwardmost seating position on the installed divan(EASA STC No. EASA.A.S.03452 and EASA.A.S.03022 refers). If the arrester block installation assembly becomes unservic. 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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INTRODUCTION OF CABIN VU-123 CABIN SURVEILLANCE SYSTEM LIMITATIONS: NONE. CONDITIONS:...

Introduction of Cabin Vu-123 Cabin Surveillance System 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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CUSTOMIZED AIRCRAFT COMPLETION - ASN 9365 CERTIFICATION BASIS EASA.IM.A.009THE CERTIFICATION...

Customized Aircraft Completion - ASN 9365 Certification Basis EASA.IM.A.009The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approval.CRIF-01 Installation of Wireless System"CRI D-01 Installation of Interi (...) Limitations STC Twenty One Ltd Master Document List No. S21.MDL-0795.STC Twenty One Ltd Airplane Flight Manual Supplement No. S21.FMS-0068.Instructions for Continued Airworthiness Midcoast Aviation Inc.Supplemental Maintenance Manual No. 35-027E225.orlater revi ...
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INTRODUCTION OF CABINVU-123 CABIN SURVEILLANCE SYSTEM LIMITATIONS: NONE. CONDITIONS: PRIOR...

Introduction of CabinVu-123 Cabin Surveillance System 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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INTRODUCTION OF SWIFT BROADBAND CERTIFICATION BASIS EASA.IM.A.023THE CERTIFICATION BASIS FOR...

Introduction of Swift Broadband Certification Basis EASA.IM.A.023The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original product areunch (...) Limitations STC Twenty One Ltd Master Document List S21.MDL-0786 Issue 1 dated 26August 2010.STC Twenty One Ltd Flight Manual Supplement S21.FMS-0067or later revisions of the above listed documents approved by ...
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REWORK OF THE CLASS E COMPARTMENT FOR INCLUSION OF A...

Rework of the Class E Compartment for inclusion of a courier seatingarea for up to 5 occupants, S21.25-63-1355. Limitations: EASA.A.S.01681 R1 and EASA.A.S.01738 must be installed. 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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INTRODUCTION OF AIR CONDITIONING FILTER LIMITATIONS: INSTALLATION OF STC21 LIMITED...

Introduction of Air Conditioning Filter Limitations: Installation of STC21 Limited Minor Change S21.21-15-1004, must beembodied prior to<(>,<)> or concurrent with<(>,<)> 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 introduce no adverse effectupon the airworthiness of the product
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CUSTOMIZED AIRCRAFT COMPLETION - ASN 9266 CERTIFICATION BASIS EASA.IM.A.009THE CERTIFICATION...

Customized Aircraft Completion - ASN 9266 Certification Basis EASA.IM.A.009The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approvalCRI F-01 Installation of Wireless System"CRI D-01 Installationof Interio (...) Limitations STC Twenty One Ltd Master Document List No. S21.MDL-0655.STC Twenty One Ltd Airplane Flight Manual Supplement No. S21.FMS-0054.Instructions for Continued Airworthiness Midcoast Aviation Inc.Supplemental Maintenance Manual No. 35-027E134.orlater revi ...
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CUSTOMIZED AIRCRAFT COMPLETION - ASN 9251. CERTIFICATION BASIS EASA.IM.A.009.THE CERTIFICATION...

Customized Aircraft Completion - ASN 9251. Certification Basis EASA.IM.A.009.The Certification Basis for the original product and the followingadditional or alternative airworthinessrequirements are applicable tothis certificate/ approval.CRI F- 01 "Installation of Wireless System".The certificated noise and/ or (...) Limitations STC Twenty One Ltd Master Document List No. S21.MDL-0726 dated 15January 2010.STC Twenty One Ltd Airplane Flight ManualSupplement No. S21.FMS- 0057.Instructions for Continued Airworthiness Midcoast Aviation Inc.Supplemental Maintenance ...
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INTRODUCTION OF WIRELESS LOCAL AREA NETWORK. CERTIFICATION BASIS EASA.IM.023 PLUS...

Introduction of Wireless Local Area Network. Certification Basis EASA.IM.023 plus CRI F-01. Limitations - S21.25-89-1302.- MDL-0580 Issue 4. Conditions
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INTRODUCTION OF WIRELESS LOCAL AREA NETWORK. LIMITATIONS: N/A. CONDITIONS: 1....

Introduction of Wireless Local Area Network. Limitations: n/a. Conditions: 1. Prior to installation of this modification the installer mustdetermine that the interrelationship between this modification and anyother previously installed modification will introduce no adverse effectupon the airworthiness of the product.2. The insta
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CARRIAGE OF HORSES & GROOMS LIMITATIONS: 1. THIS DESIGN CHANGE...

Carriage of Horses & Grooms Limitations: 1. This design change is applicable to Boeing 737-300 aircraft converted under FAA STC SA2968SO, SA2969SO, and SA2970SO & SA2971SO as previously been validated by the UK CAA under Airworthiness Approval Note AAN 24984.2. The certification basis has b. Conditions: n/a
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INTRODUCTION OF PASSENGER CABIN INTERIOR. LIMITATIONS: EASA STC NO. EASA.IM.A.S.01752...

Introduction of Passenger Cabin interior. Limitations: EASA STC No. EASA.IM.A.S.01752 must be fitted.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. Conditions: n/a
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INTRODUCTION OF PASSENGER CABIN INTERIOR. CERTIFICATION BASIS LIMITATIONS 1. STC...

Introduction of Passenger Cabin interior. Certification Basis Limitations 1. STC 21 Master Document List No. 21.MDL-0316 Issue 1 dated 10 January 2008 or later approved revision.2. STC 21Flight Manual Supplement No. S21.FMS-0033 Issue 1 or later approved revision. Conditions EASA STC No. EASA.IM.A.S.01752 must be fitted.Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed ...
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INTRODUCTION OF PASSENGER CABIN INTERIOR. CERTIFICATION BASIS LIMITATIONS - STC...

Introduction of Passenger Cabin Interior. Certification Basis Limitations - STC Twenty One Ltd Master Document List S21.MDL-0532 dated 09 December 2008 or later approved revision.- STC Twenty One Ltd Flight Manual Supplement S21.FMS- 0048 Issue 1 or later approved revision. Conditions 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 ...
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REWORK OF CLASS E CARGO ROLE OF QC VARIANT LIMITATIONS:...

Rework of Class E cargo role of QC variant 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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INTRODUCTION OF WINGSPEED XLLINK COMMUNICATIONS AND DATA MANAGEMENT SYSTEM LIMITATIONS:...

Introduction of Wingspeed XLLink Communications and Data Management 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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INTRODUCTION OF PASSENGER CABIN INTERIOR. CERTIFICATION BASIS LIMITATIONS STC 21...

Introduction of Passenger Cabin Interior. Certification Basis Limitations STC 21 Master Document List No. S21.MDL- 0360 at Issue 1 dated 19 August 2008 or later approved revision.STC 21 Flight Manual Supplement No. S21. FMS-0041 at Issue 1 or later approved revision. Conditions Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce ...
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INTRODUCTION OF CHANGE 7.0 ACAS II AND DUAL MODE S...

Introduction of Change 7.0 ACAS II and Dual Mode S Limitations: n/a. Conditions: n/a
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INTRODUCTION OF CABINVU-123 CABIN SURVEILLANCE SYSTEM LIMITATIONS: N/A. CONDITIONS: N/A

Introduction of CabinVu-123 Cabin Surveillance System Limitations: n/a. Conditions: n/a
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INTRODUCTION OF DUAL GNS-430/530 CERTIFICATION BASIS LIMITATIONS STC TWENTY ONE...

Introduction of Dual GNS-430/530 Certification Basis Limitations STC Twenty One Ltd Major Change S21.34- 29-1085Flight ManualSupplementS21.FMS- 0032 Issue 1 Conditions
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INTRODUCTION OF PASSENGER CABIN INTERIOR. LIMITATIONS: N/A. CONDITIONS: N/A

Introduction of Passenger Cabin interior. Limitations: n/a. Conditions: n/a
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INTRODUCTION OF PASSENGER CABIN INTERIOR. CERTIFICATION BASIS LIMITATIONS STC 21...

Introduction of Passenger Cabin interior. Certification Basis Limitations STC 21 Master Document List No. S21.MDL- 0482 Issue 1 dated 3 March 2008 or later approved revisions.STC 21 Flight Manual Supplement No. S21.FMS-0034 at Issue 1 or later approved revision. Conditions
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INSTALLATION OF CABIN VU-123 CABIN SURVEILLANCE SYSTEM. LIMITATIONS: N/A. CONDITIONS:...

Installation of Cabin Vu-123 Cabin Surveillance System. Limitations: n/a. Conditions: n/a
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INSTALLATION OF HONEYWELL MK V EGPWS.THIS SUPPLEMENTAL TYPE CERTIFICATE INSTALLS...

Installation of Honeywell MK V EGPWS.This supplemental Type Certificate installs a Terrain Awareness Warning System. Limitations: n/a. Conditions: n/a
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INTRODUCTION OF SSR MODE S ENHANCED SURVEILLANCE SYSTEM. LIMITATIONS: BOEING...

Introduction of SSR Mode S Enhanced Surveillance System. Limitations: Boeing 767-200/300 series.It is a condition of this STC that transponders of different manufacturers must not be intermixed, refer to STC 21 IPC supplement S21.TEC-0033 for further details.. Conditions: n/a
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INTRODUCTION OF HOENYWELL RDR-4B WEATHER RADAR SYSTEM LIMITATIONS: N/A. CONDITIONS:...

Introduction of Hoenywell RDR-4B Weather Radar System Limitations: n/a. Conditions: n/a
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INTRODUCTION OF ROCKWELL COLLINS DUAL ADF-60 SYSTEM IN THE F27...

Introduction of Rockwell Collins Dual ADF-60 System in the F27 Mark 200. This installation replaces the existing Bendix Dual ADF System.In accordance with STC Twenty One Limited Master Drawing List document S21. MDL-0264 dated 14/12/2006 or later EASA appr Limitations: Instructions for Continued Airworthiness: STC Tewnty One Limited Change Supplement Manual document S21.TEC-0094 Revision 0, dated 21/03/2002, or later EASA approved revision.. Conditions: n/a
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SAAB 340 BULK CARGO RESTRAINT SYSTEM (AS DEFINED IN DOCUMENT...

Saab 340 Bulk Cargo Restraint System (as defined in document S21 MDL-0034). This major change will introduce transverse nets at discrete positions in the aircraft main cabin (converted to Class E under STC Twenty One Limited major change S21.25-63-1015) to Limitations: This STC must be used in conjunction with EASA STC EASA.A.S.01681 "Saab 340 Class E Cargo Compartment".. Conditions: n/a
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SAAB 340 CLASS E CARGO COMPARTMENTTHIS SIGNIFICANT MAJOR CHANGE, DESIGNED...

Saab 340 Class E Cargo CompartmentThis significant major change, designed by STC WP EASA.A.S.01681Twenty One Limited, will convert the main passenger cabin to a class E cargo compartment for the carriage of freight Limitations: --. Conditions: n/a
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INTRODUCTION OF SKYLARK 2 RADAR.

Introduction of Skylark 2 Radar.
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REDUCTION OF OVER-WING EMERGENCY EXITS FROM 4 TO 2. LIMITATIONS:...

Reduction of Over-Wing Emergency Exits from 4 to 2. 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 T2CAS COLLSION AVOIDANCE & TERRAIN AWARENESS WARNING SYSTEM...

Introduction of T2CAS Collsion Avoidance & Terrain Awareness Warning System Limitations: --. Conditions: n/a
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INTRODUCTION OF PASSENGER CABIN INTERIOR CERTIFICATION BASIS LIMITATIONS STC TWENTY...

Introduction of Passenger Cabin Interior Certification Basis Limitations STC Twenty One MDL No. S21.MDL-0131 at Issue 1 or later approved revision. Midcoast Aviation Inc. AFM supplement 34-261M021 or later approved revision Conditions
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INTRODUCTION OF FLIGHTVU CABIN SURVEILLANCE SYSTEM LIMITATIONS: N/A. CONDITIONS: N/A

Introduction of FlightVu Cabin Surveillance System Limitations: n/a. Conditions: n/a
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INTRODUCTION OF EMERGENCY LOCATOR TRANSMITTER LIMITATIONS: N/A. CONDITIONS: N/A

Introduction of Emergency Locator Transmitter Limitations: n/a. Conditions: n/a
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INTRODUCTION OF AN AIRCELL SATELLITE TELEPHONE SYSTEM ST 3100 TO...

Introduction of an AirCell Satellite Telephone System ST 3100 to the aircraft.This modification installs the handset into an arm rest on the rear starboard side of the aircraft. The Satellite Phone Transceiveris installed in the mid cabin drinks sto (...) Certification Basis Limitations Installation: Accomplishment Instruction, Serial No.: S21.ACC-0026, Iss. 1Aircraft Maintenance Manual, Wiring Diagram Manual, Illustrated Parts Catalogue, refer to STC Twenty One Ltd Supplemental ...
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INTRODUCTION OF T2 CAS COLLISION AVOIDANCE & TERRAIN AWARENESS SYSTEM...

Introduction of T2 CAS Collision Avoidance & Terrain Awareness System Limitations: -. Conditions: n/a
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USE OF TRA-45A DISPLAY INDICATOR LIMITATIONS: N/A. CONDITIONS: N/A

Use of TRA-45A Display Indicator Limitations: n/a. Conditions: n/a
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INTRODUCTION OF HONEYWELL MKV ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS)...

Introduction of Honeywell MKV Enhanced Ground Proximity Warning System (EGPWS) Limitations: n/a. Conditions: n/a
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INTRODUCTION OF SSR MODE S ENHANCED SURVEILLANCE LIMITATIONS: N/A. CONDITIONS:...

Introduction of SSR Mode S Enhanced Surveillance Limitations: n/a. Conditions: n/a
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