MODIFICATIONS OF Jet Aviation AG (197)

HONEYWELL FMS CDU UPGRADE TO CD-830

In order to provide a solution to replace obsolete Honeywell CD800, CD 810 and CD820 FMS controllers, Jet Aviation has achieved an AML STC to replace this controller with Honeywell’s latest LCD touchscreen technology CD830 giving equivalent functionality at much improved reliability. 
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PLUG AND PLAY DISHWASHER

Jet Aviation Basel has developed a plug and play in-flight dishwasher (ADW) with a 3-minute wash cycle that requires just 3 liters of water. The user-friendly ADW is compatible with an eco-friendly soap that can be used to clean silver and aluminum dishes. Available in different sizes to ensure the perfect fit for all galleys, including that of the B787, the ADW utilizes a quick connection system ...
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ADDITIONAL WATER TANKS INSTALLATION

Water Tanks Installation Installation of two additional water tanks in the AFT lower lobe area between frame FR62 and frame FR65 on the LH and RH side.
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WIRELESS LOCAL AREA NETWORK (WLAN) ACTIVATION

Wireless Local Area Network (WLAN) Activation, addressing the technical aspects of Tranmitting Portable Electronic Devices (T-PED) on board. Operational aspects are not covered by the STC.
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WIRELESS LOCAL AREA NETWORK (WLAN) ACTIVATION

Wireless Local Area Network (WLAN) Activation in the 2.4 GHz frequency band, addressing the technical aspects of Tranmitting Portable Electronic Devices (T-PED) on board. Operational aspects are not covered by the STC.
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WIRELESS LOCAL AREA NETWORK (WLAN) ACTIVATION

Wireless Local Area Network (WLAN) Activation, addressing the technical aspects of Tranmitting Portable Electronic Devices (T-PED) on board. Operational aspects are not covered by the STC.
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WIRELESS LOCAL AREA NETWORK (WLAN) ACTIVATION

Wireless Local Area Network (WLAN) Activation, addressing the technical aspects of Tranmitting Portable Electronic Devices (T-PED) on board. Operational aspects are not covered by the STC.
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WIRELESS LOCAL AREA NETWORK (WLAN) ACTIVATION

Wireless Local Area Network (WLAN) Activation, addressing the technical aspects of Tranmitting Portable Electronic Devices (T-PED) on board. Operational aspects are not covered by the STC.
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WIRELESS LOCAL AREA NETWORK (WLAN) ACTIVATION

Wireless Local Area Network (WLAN) Activation, addressing the technical aspects of Tranmitting Portable Electronic Devices (T-PED) on board. Operational aspects are not covered by the STC. Including installation of a "WLAN OFF" switch in the cockpit.
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DIRECT VIEW CAMERA SYSTEM INSTALLATION

Installation of an AD Aerosapce Direct View Camera System in the cabin.
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AMT-3800 SATCOM ANTENNA INSTALLATION B737-900ER

Honeywell/EMS AMT-3800 SATCOM Antenna installation for Boeing B737-900ER. This STC has been assessed for compatibility for installation onaircrafts, which are equipped for lower cabin altitude LOC under FAA STCST01697SE.    
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TAIL CAMERA INSTALLATION A340-200/-300

Camera Unit and Structural provision installation This STC installs one camera on the tail of the aircraft, viewing forward, the data package covers the mechanical installation of the camera unit and the pressure vessel penetration for the wiring.
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AMT-3800 SATCOM ANTENNA INSTALLATION B737-700

Honeywell/EMS AMT-3800 SATCOM Antenna installation for Boeing B 737-700. Installation option STA.727E to STA.787 orSTA.727B to STA.727E  
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EXTERNAL CAMERAS INSTALLATION A390/A320

installation of external cameras tail (looking forward) belly quad view (FWD/AFT, LH/RH) belly landdscape (looking down, zoom)  
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TAILWIND 550/560 ANTENNA INSTALLATION A340-200/-300

Tailwind 550/560 antenna installation Installation of an antenna and radome located top of fuselage.  
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TAILWIND 550/560 ANTENNA AND RACK INSTALLATION A330-200/-300

Tailwind 550/560 Antenna and Rack Installation Installation of an antenna and radome located top of fuselage. Installation of a system rack inside the cabin crown area.
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WIRELESS LAN ACTIVATION WIRELESS ACCESS SERVICE POINT

Please contact one of our Sales Person to discuss the STC in details.
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GSM SECURAPLANE ANTENNA INSTALLATION

Please get in touch with one of our sales persons to discuss the STC  in details.
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ACTIVATION OF RAAS

Please contact one of our sales perons to discuss the STC in details.
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EMS SATCOM AMT-3800 INSTALLATION:INSTALLATION OPTION BETWEEN STA. 727E TO STA.787...

EMS SATCOM AMT-3800 Installation:Installation option between STA. 727E to STA.787 and STA.727B to STA.727E (Major change to EASA STC No. EASA.A.S. 03322 Rev.1)
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ACTIVATION OF RUNWAY AWARENESS AND ADVISORY SYSTEM (RAAS).

Activation of Runway Awareness and Advisory System (RAAS).
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INSTALLATION OF AN EXECUTIVE INTERIOR ARRANGEMENT, INCLUDING CABINSEATS, JUMPSEAT, POCKET...

Installation of an Executive Interior Arrangement, including CabinSeats, Jumpseat, Pocket Doors, Divan, PassengerOxygen System,Emergency Equipment, and Emergency Lighting System.
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MODIFICATION OF AN EXECUTIVE INTERIOR ARRANGEMENT INCLUDINGCABIN SEATS,DIVANS, MID CABIN...

Modification of an Executive Interior Arrangement IncludingCabin Seats,Divans, Mid Cabin Pocket Door, Removable Mid Cabin Bulkhead, PassengerOxygen System Mods, Emergency Lighting System Mods and EmergencyEquipment.
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INSTALLATION OF A WINDOW SHADE SYSTEM

Installation of a Window Shade System
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INSTALLATION OF A WIRELESS LOCAL AREA NETWORK (WLAN)

Installation of a Wireless Local Area Network (WLAN)
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INSTALLATION OF A 3-PLACE DIVAN

Installation of a 3-Place Divan
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CERTIFICATION OF THE AIRCRAFT DATA LINK SYSTEM USED FOR COMMUNICATION...

Certification of the aircraft data link system used for communication supporting Air Traffic Service
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ACAS II UPGRADE TO SOFTWARE VERSION 7.1OUT: HONEYWELL TPA-81A P/N...

ACAS II upgrade to software version 7.1Out: Honeywell TPA-81A P/N 066-50000-2320 or TPA-100A P/N940-0300/0400-001In: Honeywell TPA-100B P/N 940-0351/0451-010
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INSTALLATION OF SECURAPLANE EXTERNAL AND GLARESHIELD CAMERA SYSTEM

Installation of Securaplane External and Glareshield Camera System
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MODIFICATION OF AN EXECUTIVE INTERIOR ARRANGEMENT INCLUDING CABIN SEATS, DIVANS,...

Modification of an Executive Interior Arrangement Including Cabin Seats, Divans, Mid Cabin pocket Do
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CERTIFICATION OF P-RNAV CAPABILITY OF AIRCRAFT EQUIPPED WITH FLIGHTMANAGEMENT SYSTEM...

Certification of P-RNAV capability of aircraft equipped with FlightManagement System Universal UNS-1D
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TCAS II (ACAS II) UPGRADE TO VERSION 7.1UPGRADE OF EXISTINGHONEYWELL...

TCAS II (ACAS II) UPGRADE TO Version 7.1Upgrade of existingHoneywell CAS67 Traffic Alert and CollisionAvoidance Systemto incorporate 7.1 logic software:Change consists of Honeywell TPU-67A TCAS 7.0 processor P/N066-01146-1211Upgrade to orreplacement by a TPU-67B TCAS 7.1 processor P/N066-01146-222...
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REPLACEMENT OF A DUAL ALLIED SIGNAL HIGH FREQUENCY (HF) RADIO...

Replacement of a dual Allied Signal High Frequency (HF) Radio by dualRockwell Collins Air Transport (RCAT) HFS-900D HF Radio equipment (ARINC753) with HF Data Link activation in accordance with Jet Aviation MasterData List Doc. No. B7428343-006 Rev D, dated 20 october 2010 or laterapproved revision....
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WIRELESS FIDELITY (WI-FI) ACTIVATION OF A PREVIOUSLY INSTALLED (IEEE 802.11...

Wireless Fidelity (Wi-Fi) Activation of a Previously Installed (IEEE 802.11 b, g only) Router and Transmitting Portable Electronic Device (T-PED) Aircraft Tolerance Testing
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WIRELESS LAN (WLAN) ACTIVATIONEXPANDING DEMONSTRATION OF THE EXISTING IMMUNITY TO...

Wireless LAN (WLAN) ActivationExpanding demonstration of the existing immunity to IEEE 802.11 a/b/g/nfrom the B737-700 to the B737-800/900/900ER and expand the immunity toIEEE 802.11 ac.
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COBHAM AVIATOR 700D SATCOM UPGRADE CERTIFICATION BASIS THE CERTIFICATION BASIS...

Cobham Aviator 700D SATCOM Upgrade Certification Basis The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Limitations FAA STC No. ST03229CH-D dated 18 June 2013.Jet Aviation St.Louis, Inc Master Data List 35-354G001 Rev A, dated 18June 2013.or later ...
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INSTALLATION OF 42-INCH GAS PLASMA DISPLAY IN ACCORDANCE WITH JET...

Installation of 42-inch gas plasma display in accordance with Jet Aviation Master Data List No. CD-2002-004, Rev. H, dated 1/15/04, or later FAA approved revision. Use of FAA approved Airplane Flight Manual Supplement (AFMS), Jet Aviation Engineering Services Document No. CD-2002-020, Rev. IR, dated February 9, 2004, or later FAA approved revision, is required.
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INSTALLATION OF NEW DECORATIVE LIMINATES ON SELECTED INTERIOR COMPARTMENT SURFACES...

Installation of new decorative liminates on selected interior compartment surfaces and replacements of Y-class seats with Weber TSO-C39c seats.
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INSTALLATION OF ELECTRIC FAN, HARDWARE AND WIRING TO PROVIDE VENTILATION...

Installation of electric fan, hardware and wiring to provide ventilation of In Flight Entertainment avionics boxes on Boeing 747-400 aircraft.
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THE UPGRADE OF EXISTING DUAL GARMIN GTX 330D TRANSPONDER SYSTEM...

The upgrade of existing Dual Garmin GTX 330D Transponder System for Enhanced Surveillance
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CABIN INSULATION IMPROVEMENT AS DEFINED IN BB73725801-500_REV_A_PROJECT DESCRIPTION AND MDL...

Cabin Insulation Improvement as defined in BB73725801-500_REV_A_Project Description and MDL BB73725801-001 Master Data List Limitations: - Engineering Order, Doc. No. BB73725801- 258000, Rev. IR, 26.06.2013- Master Data List, Doc. No. MDL BB73725801-001, Rev. A, 08.08.2013or later revisions of the above listed documents approved by EASA. Conditions: Prior to installation of this modification it must be determined that the interrelationship between this modification and any other previously ...
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SOFTWARE UPGRADE TO -218-218 OF THE HONEYWELL MK V ENHANCED...

Software Upgrade to -218-218 of the Honeywell MK V Enhanced Ground Proximity Warning System (EGPWS).
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INSTALLATION OF HONEYWELL TCAS-2000 TCAS-II SYSTEM WITH DUAL HONEYWELL RCZ-852...

Installation of Honeywell TCAS-2000 TCAS-II System with Dual Honeywell RCZ-852 Mode S Transponders.
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P-RNAV APPROVAL OF UNS-1K CERTIFICATION BASIS THE CERTIFICATION BASIS (CB)...

P-RNAV Approval of UNS-1K Certification Basis The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Limitations -Airplane Flight Manual Supplement 2013-6- 8, Rev. IRor later revisions of the above listed documents approved by EASA.-Engineering Order 2013-6, Rev. A, ...
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INSTALLATION OF 4 PLACE AMBULANCE STRETCHER SYSTEM/ VIP INTERIOR. LIMITATIONS:...

Installation of 4 Place Ambulance Stretcher System/ VIP interior. Limitations: Master Data List reference 2011-8-16, Revision A, dated 26th February2012;Engineer Order reference 2011 8, Revision A, dated 26th February 2012;AFM Supplement, reference 2011-8- 8,Revision A, dated 24th February2012;or later revisions of the above listed documents approved by EASA. Conditions: None. -
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INSTALLATION OF 40 CUBIC FOOT OXYGEN BOTTLE. CERTIFICATION BASIS THE...

Installation of 40 Cubic Foot Oxygen Bottle. Certification Basis The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Limitations FAA STC No. ST02574CH-D dated 30 January 2013.Jet Aviation St. Louis, Inc. Master Data List 41-261G001, Revision G,dated 30 ...
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INSTALLATION OF AN EXECUTIVE INTERIOR ARRANGEMENT, INCLUDING CABIN SEATS, DIVAN,...

Installation of an Executive Interior Arrangement, Including Cabin Seats, Divan, Pocket Door and Emergency Equipment
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INSTALLATION OF A COCKPIT CONSOLE STORAGE BIN, FLASHLIGHTS & VARIOUS...

Installation of a Cockpit Console Storage Bin, Flashlights & Various Existing Cockpit Trim Panels Material Coverings
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INSTALLATION OF AN IRIDIUM ANTENNA ON THE TOP OF THE...

Installation of an Iridium Antenna on the top of the fuselage.According to Master Document List 2013-1-16, rev IR, dated 18 March2013. Certification Basis The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Limitations Jet Aviation Master Document List ...
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P-RNAV COMPLIANCE IN INSTALLED GNS-XLS(S) FMS, I.A.W. INSTALLATIONINSTRUCTIONS, DOC NO....

P-RNAV Compliance in installed GNS-XLS(s) FMS, i.a.w. InstallationInstructions, Doc No. OPM-006Revision 2 has been issued to reflect the removal of the limitation toC650 (CitationIII up to S/N -199), AFMS Certification Basis The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this ...
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EXCHANGE TO UNIVERSAL AVIONICS FMS UNS- 1LWOUT: UNIVERSAL AVIONICS FMS...

Exchange to Universal Avionics FMS UNS- 1LwOut: Universal Avionics FMS UNS-1Msp systemIn: Universal Avionics FMS UNS-1Lw system Certification Basis The Certification Basis for the original product remains applicable tothis certificate/ approval.The certificated noiseand/ or emissions levels of the original productare unchanged and remain applicable to this certificate/ approval. Limitations Master Data List Doc. No. BSDYB004-004 Rev. C of 21.02.2013Instructions for Continued Airworthiness Doc. No. BSDYB004-150-04 Rev. ...
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EMS SATCOM AMT-3800 ANTENNA INSTALLATION.THIS MODIFICATION INSTALLS EMS SATCOM AMT-3800...

EMS Satcom AMT-3800 antenna installation.This modification installs EMS Satcom AMT-3800 high gain antenna,Diplexer Low Noise Amplifier, and associated structural provision.The revision has withdrawn the STC limitations following additionalsubstantiations delivery. Limitations: Master Data List, ref : BA33023261-001, Revision E Instruction for Continued Airworthiness, ref : BA33023261-150- 01,Revision C Weight & Balance Statement, ref : BA33023261-121-01.orlater revisions of the above listed documents approved by EASA. Conditions: Prior to ...
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WLAN ACTIVATIONELECTRO-MAGNETIC COMPATIBILITY DEMONSTRATIONOF AEROPLANE'S REQUIREDSYSTEMS IMMUNITY TO WORST CASE...

WLAN activationElectro-Magnetic Compatibility demonstrationof aeroplane's requiredsystems immunity to worst case WLAN IEEE 802.11 a/b/g/n passengerscarry- on TPED transmissions. Certification Basis The Certification Basis for the original product remains applicable tothis certificate/ approval.The certificated noiseand/ or emissions levels of the original productare unchanged and remain applicable to this certificate/ approval. Limitations - Master Data List, Doc. No. BFSLA001-002, Rev. IR, dated 11.01.2013- AFMS, Doc. No. BFLSA001-201-02, Rev. ...
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MDL BDBMW002-001 REV. IR CERTIFICATION BASIS JAR-25 CHANGE 15 AND...

MDL BDBMW002-001 Rev. IR Certification Basis JAR-25 Change 15 and JAR AWO Change 2 with the exceptions as per EASATCDS IM.A.070The Certification Basis for the original product remains applicable tothis certificate/ approval.The certificated noise and/ or emissions levels of the original produc (...) Limitations Rosen Aviation Remote Display STM 105478 Rev. Aor later revisions of the above listed documents approved by EASA Conditions S/N: 5336
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WX-950 STORMSCOPE INSTALLATION. CERTIFICATION BASIS CS 23 AMDT: 40THE CERTIFICATION...

WX-950 Stormscope installation. Certification Basis CS 23 Amdt: 40The Certification Basis for the original product remains applicable tothis certificate/ approval.Derogation to latest amendment (Part 21A.101):Do not materially contribute to safety.The certificated noise and/ or emissions levels of th (...) Limitations - Master Data List, Doc. No. 2016-6-16, Rev. IR, dated 12.12.2012;- AFMS, Doc. No. 2016 6-8, Rev. A, dated 25.10.2012;-ICA, Doc. No. 2016-6-10, Rev. IR, dated ...
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EASA VALIDATION OF FAA ORIGINALLY APPROVED STC SA02789CE "INSTALLATIONOF A...

EASA validation of FAA originally approved STC SA02789CE "Installationof a Bendix/King CAS-81 TCAS System". Certification Basis The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noiseand/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Limitations See original FAA approved STC SA02789CE documents:-,,Jet Aviation Certification Drawing List No. AD910011, Revision ...
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INSTALLATION OF DRAIN MAST CERTIFICATION BASIS EASA.IM.A.023THE CERTIFICATION BASIS FOR...

Installation of Drain Mast 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 FAA STC No. ST02868CH-D.Jet Aviation St. Louis, Inc. MasterData List 41-260G001, Rev C dated 09February 2012.or later revisions of the above listed documents approved by EASA inaccordance with EASA ...
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EMS SATCOM AMT-3800 ANTENNA INSTALLATION.THIS MODIFICATION INSTALLS EMS SATCOM AMT-3800...

EMS Satcom AMT-3800 antenna installation.This modification installs EMS Satcom AMT-3800 high gain antenna,Diplexer Low Noise Amplifier, and associated structural provision. Limitations: This STC approval has been granted for 100 Flight Cycle (FC) or 6months, counted from the STC approval date, whichever occurred first.. 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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INSTALLATION OF A MOVING MAP SYSTEM. CERTIFICATION BASIS THE CERTIFICATION...

Installation of a Moving Map System. Certification Basis The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noiseand/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Limitations Jet Aviation Master Data List: ref 2012-4-16, rev IR, date 30 July 2012;Jet Aviation AFM Supplement: ref 2012-4-8, rev A, date 21 ...
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INSTALLATION OF A ROCKWELL COLLINS WIRELESS LOCAL AREA NETWORK (WLAN)....

Installation of a Rockwell Collins Wireless Local Area Network (WLAN). Certification Basis The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noiseand/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Limitations FAA STC No. ST02744CH-D dated 30 November 2011;Midcoast Aviation Index List 35-409G007, Revision NC dated 05 August2009;Midcoast Airplane ...
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INSTALLATION OF A CABIN INTERIOR ARRANGEMENT, PASSENGER OXYGEN SYSTEMAND EMERGENCY...

Installation of a Cabin Interior Arrangement, Passenger Oxygen Systemand Emergency Lighting Certification Basis EASA.IM.A.009The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approval.EASA Generic CRIs D-01, D-02, D-03The requirements for environmental prot (...) Limitations FAA STC No. ST01376WI-D dated 30 November 2011.Jet AviationIndex List 35- 299G009, Revision N, dated 29 May 2011.Jet Aviation Master Drawing List 35-299G013, ...
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IRIDIUM ANTENNA STRUCTURAL PROVISIONSBETWEEN FUSELAGE STATION BS 727C & 727D...

Iridium Antenna Structural Provisionsbetween fuselage station BS 727C & 727D 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 A PASSENGER ADDRESS SYSTEM CERTIFICATION BASIS THE CERTIFICATION...

Installation of a Passenger Address System Certification Basis The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noiseand/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Limitations FAA STC No. ST02658CH-D dated 30 November 2011.Jet AviationMaster Data List 35-411G001, Revision C, dated 5 December2008Jet Aviation Airplane Flight Manual Supplement ...
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INSTALLATION OF A SUPPLEMENTAL CREW OXYGEN SYSTEM CERTIFICATION BASIS THE...

Installation of a Supplemental Crew Oxygen System Certification Basis The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noiseand/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Limitations FAA STC No. ST01065WI-D dated 30 November 2011.Midcoast Master Data List 35-261G001 Revision K, dated 20 September 2010Airplane Flight Manual Supplement(s) ...
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INSTALLATION OF 4 PLACE AMBULANCE STRETCHER SYSTEM/ VIP INTERIOR.DESCRIPTION AS...

Installation of 4 Place Ambulance Stretcher System/ VIP interior.Description as per:Master Data List reference 2011-8-16, Revision A, dated 26th February2012. Engineer Order reference 2011-8, Revision A, dated 26th February 2012.AFM Supplement, reference 2 Limitations: None.. Conditions: None.
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FA2100 CVR INSTALLATIONREMOVED EQUIPMENT:- I.A.W. INSTALLATION INSTRUCTIONS, DOC. NO. OPM-007NEW...

FA2100 CVR installationRemoved Equipment:- i.a.w. Installation Instructions, Doc. No. OPM-007New Installed Equipment:- FA2100 Cockpit Voice Recorder Systemi.a.w. Installation Instructions, Doc. No. OPM- 007Revision 1 has been issued to reflect the transfer of STC. Certification Basis The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noiseand/or emissions levels of the original product areunchanged and remain applicable to ...
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RAAS ACTIVATION ON THE HONEYWELL MK-VII EGPWSI.A.W. INSTALLATION INSTRUCTIONS, DOC....

RAAS activation on the Honeywell MK-VII EGPWSi.a.w. Installation Instructions, Doc. No. OPM-005Revision 1 has been issued to reflect the transfer of STC. Certification Basis FAA TCDS A9NMThe 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 areuncha (...) Limitations - Master Document List, Doc. No. MDL-061, Rev. A- AFMS, ...
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PRIMUS 880 WX & MFRD INSTALLATIONREMOVED EXISTING WEATHER RADAR EQUIPMENT:-...

Primus 880 WX & MFRD installationRemoved existing Weather Radar Equipment:- i.a.w Installation Instructions, Doc. No. OPM-003New Installed Weather Radar Equipment:- Primus 880 Weather Radar System- Honeywell Multi Function Display, P/N 80-5204-XX-Xi (...) Certification Basis FAA TCDS A9NMThe 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 areuncha (...) Limitations ...
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MK VII EGPWS INSTALLATION.REMOVED EXISTING EQUIPMENT:I.A.W.INSTALLATION INSTRUCTIONS, DOC. NO. OPM-004NEW...

MK VII EGPWS Installation.Removed existing Equipment:i.a.w.Installation Instructions, Doc. No. OPM-004New installed EGPWS Equipment:- Honeywell MK-VII EGPWSi.a.w. Installation Instructions, Doc. No. OPM- 004Revision 1: By revising the interface betwe (...) Certification Basis FAA TCDS A9NMThe 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 areuncha (...) Limitations - Master data ...
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MODIFICATION OF AN EXECUTIVE INTERIOR ARRANGEMENT TO INCLUDE CABIN SINGLE...

Modification of an Executive Interior Arrangement to Include Cabin Single Seats, Double Seats, Pocket Door, Oxygen System, and Emergency Equipment in accordance with Jet Aviation St. Louis, Inc. Master Data List 35-299G030, Rev B, dated December 28, 2011 or later FAA approved revision.
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INSTALLATION OF AN EXECUTIVE INTERIOR ARRANGEMENT, INCLUDING CABIN SEATS, JUMPSEAT,...

Installation of an Executive Interior Arrangement, including Cabin Seats, Jumpseat, Pocket Doors, Divan, Passenger Oxygen System, Emergency Equipment, and Emergency Lighting System in accordance with Jet Aviation Index List 35-299G009, Rev N, dated May 29, 2011 or later FAA approved revision.
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INSTALLATION OF A SUPPLEMENTAL CREW OXYGEN SYSTEM IN ACCORDANCE WITH...

Installation of a Supplemental Crew Oxygen System in accordance with Midcoast Master Data List 35-261G001 Revision K, dated September 20, 2010, or later FAA approved revision.
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REMOVED EQUIPMENT:-AEROSONIC VSI 1 & 2- SKYWATCH 497 TCASI SYSTEMNEW...

Removed Equipment:-Aerosonic VSI 1 & 2- Skywatch 497 TCASI SystemNew installed equipment:-Honeywell TA/VSI Indicator 1 & 2- PS-578A XPDR/TCAS Control HeadCAS- 67A TCAS II System Certification Basis The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approval.SCs or ESFs: Voluntary compliance to CS-23 First Issue for the changeDerogation to lat (...) Limitations - Master Document List, Doc. ...
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INSTALLATION OF AN EMERGENCY FLOOR PATH LIGHTING SYSTEM IN ACCORDANCE...

Installation of an Emergency Floor Path Lighting System in accordance with Jet Aviation St. Louis, Inc. Master Data List 41-415G001, Rev A, dated September 27, 2011 or later FAA approved revision.
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MODIFICATION OF AN EXECUTIVE INTERIOR ARRANGEMENT INCLUDING CABIN DOUBLE SEATS,...

Modification of an Executive Interior Arrangement including Cabin Double Seats, Divans, Oxygen System, Emergency Lighting, and Emergency Equipment in accordance with Jet Aviation Master Data List 05-299G001 Revision D, dated July 22, 2011 and FAA Approved Jet Aviation Airplane Flight Manual Supplement 05-169M001, Revision NC, dated July 29, 2011, or later FAA approved revisions.
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IRIDIUM ANTENNA INSTALLATION.STRUCTURAL JUSTIFICATION OF THE INSTALLATION OF AN AIRCELL...

Iridium antenna installation.Structural justification of the installation of an Aircell low profiledual patch antenna on top of the fuselage between frames 17 and 18. Certification Basis The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noiseand/or emissions levels of the original product areunchanged and remain applicable to this certificate/approval. Limitations Master Data List Doc. No. BOSIR001-002 ...
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INSTALLATION OF A BENDIX/KING CAS-81 TCAS SYSTEM. DATA REQUIRED: (1)...

Installation of a Bendix/King CAS-81 TCAS System. Data Required: (1) Jet Aviation Certification Drawing List No. AD910011, Revision F, dated March 11, 2011, (2) Jet Aviation Report No. 13-328M001, Revision F, FAA Approved Flight Manual Supplement for the Avions Marcel Dassault-Breguet Aviation Model Mystere-Falcon 50 Airplane, dated May 13, 2011, or later FAA approved revision of (1) or (2).
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INSTALLATION OF AFT VOR/LOC-LSR AND MARKER BEACON ANTENNAS IN ACCORDANCE...

Installation of Aft VOR/LOC-LSR and Marker Beacon Antennas in accordance with Jet Aviation Index List 41-395G001, Rev NC dated May 28, 2011 or later FAA approved revision.
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NZ2000 6.1 UPGRADE WITH CD820 CDU REPLACEMENT.EXISTING DUALOR TRIPLE HONEYWELL...

NZ2000 6.1 upgrade with CD820 CDU replacement.Existing dualor triple Honeywell NZ2000 Flight Management System isupgraded as follows:- NCU NZ2000 FMS 1&2 version NZ5.2 or later is replaced with versionNZ6.1- CD800/CD810 1&2 CDU replaced with CD820.No change in sensors and capabilities. Certification Basis The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noiseand/ or emissions levels of ...
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: INSTALLATION OF THE BENDIX/KING INTEGRATED HAZARD AVOIDANCE SYSTEM (IHAS)...

: Installation of the Bendix/King Integrated Hazard Avoidance System (IHAS) 8000 with Traffic Alert System and Class B Terrain Awareness Warning System functionality in accordance with Jet Aviation Engineering Services Master Data List 2334-001, Revision G, dated July 23, 2003, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement Document No. PAD550-013, Revision A, dated November 5, 2003, or later FAA approved revision is ...
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REPLACEMENT OF A DUAL ALLIED SIGNAL HIGH FREQUENCY (HF) RADIO...

Replacement of a dual Allied Signal High Frequency (HF) Radio by dualRockwell Collins Air Transport (RCAT) HFS-900D HF Radio equipment (ARINC753) with HF Data Link activation in accordance with Jet Aviation MasterData List Doc. No. B7428343-006 Rev D, date 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 ...
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AMT-3800 SATCOM ANTENNA INSTALLATION B737-800

Honeywell/EMS AMT-3800 SATCOM Antenna installation for Boeing B737-800
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RUNWAY AWARENESS AND ADVISORY SYSTEM (RAAS). SMART RUNWAY ACTIVATION.I.A.W. JET...

Runway Awareness and Advisory System (RAAS). Smart Runway Activation.i.a.w. Jet Aviation Master Data List BF5EX34461-001 Revision B or laterEASA Approved revisions. Certification Basis The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approval.In addition compliance has been shown i.a.w. EASA CRI F-01 Issue 02"Activation of the (...) Limitations See:·,,Jet Aviation Master Data List BF5EX34461-001 Revision B and·,,Jet ...
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MID CABIN DOOR CERTIFICATION BASIS CS-25THE CERTIFICATION BASIS FOR THE...

Mid Cabin Door Certification Basis CS-25The Certification Basis for the original product remains applicable tothis certificate/ approvalThe certificated noise and/ or emissions levels of the original productare unchanged and remain applicable to this certificate/ approval Limitations Master Data List BGLF525001-001 Rev. AAirplane Flight Manual Supplement BGLF525001-201-01 Rev. IRInstructions for Continued Airworthiness BGLF525001-150- 01 Rev. Aor later revisions of the above listed documents approved by EASA Conditions ...
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MINIQAR INSTALLATION; BY INSTALLING AN AVIONICA MINIQAR MK II AND...

MINIQAR installation; By installing an Avionica miniQAR MK II and the MKIII according to the Installation Instructions OPM- 009. Certification Basis FAR 23.The Certification Basis for the original product remains applicable tothis approval.Derogation to latest amendment (Part 21A.101): non significant change.The certificated noise and/ or emissions levels of the original productare unchanged and (...) Limitations - Master Document List, Doc. No. MDL-069- ICA, Doc. No. ICA-036or ...
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COCKPIT VOICE RECORDER INSTALLATIONBY INSTALLING A NEW L3 FA2100 COCKPIT...

Cockpit Voice Recorder InstallationBy installing a new L3 FA2100 Cockpit Voice Recorder (CVR) Certification Basis FAA CAR-4b, FAR 25 for the Change Limitations - Master Document List, Doc. No. MDL-068, Rev. B or latestapprovedRevision - AFMS, Doc. No. FMS-041, Rev. IR or latest approved Revision - ICA, Doc. No. ICA-034, Rev. IR or latest approved Revision Conditions None
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ACTIVATION OF THE RUNWAY AWARENESS AND ADVISORY SYSTEM (RAAS) I.A.W....

Activation of the Runway Awareness and Advisory System (RAAS) i.a.w. JetAviation Master Data List BF9EX34461-001 Certification Basis Limitations #,,Jet Aviation Master Data List BF9EX34461 001 Revision B,dated 06thJuly 2009#,,Jet Aviation Aeroplane Flight Manual Supplement BF9EX34461-201-01Revision IR#,,Jet Aviation Engineering Order (installation) BF9EX34461-344600Revision IROr later EASA Approved revisions of these documents. Conditions - 1.,,Prior to installation of this modification the installer mustdetermine that the interrelationship between this modification ...
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ACTIVATION OF THE RUNWAY AWARENESS AND ADVISORY SYSTEM (RAAS) I.A.W....

Activation of the Runway Awareness and Advisory System (RAAS) i.a.w. Jet Aviation Master Data List BF90034461-001 Certification Basis Limitations -Jet Aviation Master Data List BF90034461- 001 Revision A dated 19th May 2009-Jet Aviation Aeroplane Flight Manual Supplement BF90034461-201-01 Revision IR-Jet Aviation EngineeringOrder (installation) BF90034461- 344600 Revision IROr later EASA Approved revisions of these documents. Conditions 1) Prior to installation of this modification the installermust determine that ...
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FMS UPGRADE INSTALLATION NEW EHSI 4000. NZ2000 SW 6.0 INSTALLATION,...

FMS Upgrade Installation new EHSI 4000. NZ2000 SW 6.0 Installation, NewCDU CD- 820. Certification Basis Limitations - Master Data List, doc. no. GHIMY221-001, Rev. IR- AFMS (EHSI), doc. no. GHIMY221- 201-06, Rev. IR- AFMS (FMS), doc. no. GHIMY221-201-14, Rev. IR- ICA (EHSI), doc. no. GHIMY221-150-06, Rev. IR- ICA (FMS), doc. no. GHIMY221-150-14, Rev. IR Conditions Reg.: HB-IMY, S/N: 1084
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ACTIVATION OF THE RUNWAY AWARENESS AND ADVISORY SYSTEM (RAAS)EGPWC UPGRADE...

Activation of the Runway Awareness and Advisory System (RAAS)EGPWC upgrade to software level 228-228 and activation of the RAAS Certification Basis Limitations Installation in accordance with Jet Aviation Engineering Order BGLF334461 and Master Drawing List Doc No BGLF334461-001Rev IR or later approved revisions.Operation in accordance with Jet Aviation Airplane Flight Manual Supplement ref BGLF334461-201-01 Rev IR or later approved revisions. Conditions None
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CTT ZONAL DRYER ACTIVATIONREPLACEMENT OF ZONAL DRYER RELATED TO EASA...

CTT Zonal dryer activationReplacement 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 Swiss FOCA STC Z 25-20-77 due to the potential for combustion of contaminants i Limitations: S/N 32627. Conditions: n/a
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ACTIVATION OF THE RUNWAY AWARENESS AND ADVISORY SYSTEM (RAAS) CERTIFICATION...

Activation of the Runway Awareness and Advisory System (RAAS) Certification Basis Limitations - Jet Aviation Declaration of Compliance ref BGLEX34461 dated23/02/2009.- Jet Aviation Master Data List No. BGLEX34461-001, Revision IR, dated23/02/2009.- Jet Aviation AFMS No. BGLEX34461-201-01, Revision IR. Conditions Prior to installation of this modification the installer must determinethat the interrelationshipbetween this modification and any other previously installedmodification will introduce noadverse effect upon the airworthiness of ...
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ACTIVATION OF RAAS

Activation of RAAS
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ACTIVATION OF RAAS CERTIFICATION BASIS LIMITATIONS MASTER DATA LIST NO....

Activation of RAAS Certification Basis Limitations Master Data List No. BCL6134461-001, Rev. D of 12-01-2009 or later approved revision.AFM Supplement Bo. BCL6134462- 201-01, Rev. A of 12-01-2009 or later revision. Conditions
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IRIDIUM ANTENNA INSTALLATIONA DUAL IRIDIUM ANTENNA HAS BEENINSTALLED ON TOP...

Iridium Antenna InstallationA dual Iridium antenna has beeninstalled on top of the fuselage located between Sta. 539.5& Sta. 554.5. Certification Basis Limitations Iridium Antenna Installation In accordance with JET AVIATION Master Data List No.: BGLF553301-001 Rev l R, Dated 14th December 2008or later approved revisions.Instructions for Continued Airworthiness ref BGLF553301-150-01No AFMS has been generated for this modification. Conditions Prior to installation of this modification the installer ...
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INSTALLATION OF WIRING AND HARDWARE FOR STRUCTURAL PROVISIONS ONLY OF...

Installation of wiring and hardware for structural provisions only of Flight Guard Civil Aviation Self Protection Suite System.
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INSTALLATION OF AN AUDIO INTERNATIONAL ARTICULATED MOUNTINGARM AND DATA CONNECTIVITY...

Installation of an Audio International Articulated MountingArm and Data Connectivity for an Electronic Flight Bag Certification Basis Limitations FAA STC No. ST02544CH-D dated 07 March 2008.Midcoast Aviation, Inc. Master Data List 41-343G001 Revision C, dated March07, 2008, 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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1. FMZ-2000 SOFTWARE UPGRADE;2. APPLICATION OF HONEYWELL SERVICE BULLETIN NO....

1. FMZ-2000 Software Upgrade;2. Application of Honeywell Service Bulletin No. 7018879-34-A6060. Certification Basis Limitations 1. Master Data List No. BF90034621 Rev. K or later approved versions;2. AFM Supplement DOC No BF90034621-201-01, Rev. A. 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 no adverse effect upon the airworthiness of the ...
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AIRCELL IRIDIUM ANTENNA P/N.015-10306-001 INSTALLATION CERTIFICATION BASIS LIMITATIONS JET AVIATION...

Aircell Iridium Antenna P/N.015-10306-001 Installation Certification Basis Limitations Jet Aviation Declaration of Compliance dated 12 August 2008Jet Aviation Master Data List No. B7REPCUS1044-001, RevisionA dated 12 August 2008 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 no adverse effect upon the airworthiness of the product. The (...)
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INSTALLATION OF A HONEYWELL MK VIII ENHANCED GROUND PROXIMITY WARNING...

Installation of a Honeywell MK VIII Enhanced Ground Proximity Warning System (EGPWS). Certification Basis Limitations # Master Data List BDMET063-001, Revision B dated 19th June 2008.# Airplane Flight Manual (AFM) Supplement BDMET063 201-25, Rev. B, dated 19th June 2008# Instructions forContinued Airworthiness BDMET063-150-25, Revision IR, dated01st May 20 (...) Conditions Prior to installation of this modification the installer must determine that the - interrelationship between this ...
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INSTALLATION OF THE ALLIED SIGNAL MK-V ENHANCED GROUND PROXIMITY WARNING...

Installation of the Allied Signal MK-V Enhanced Ground Proximity Warning System (EGPWS). Certification Basis Limitations Midcoast Certification Drawing List No. 34- 327G001 RevisionD, dated August 24, 1999,Midcoast Airplane Flight Manual Supplement, Document No. 34-327M001, Revision "Original", dated August 24, 1999, or later Approved Revisions to (1) or (2).< Conditions Gama Support Services Modification No. GSSL-MIN-CL604-226 (Including Gama Support Services Flight Manual Change Sheet No. GSS-FMS-CL604-226 EASA ...
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INSTALLATION OF A CABIN INTERIOR ARRANGEMENT, PASSENGER OXYGEN SYSTEM, AND...

Installation of a Cabin Interior Arrangement, Passenger Oxygen System, and Emergency Lighting. Certification Basis Limitations Midcoast Aviation Inc. Master Data List 41- 299G001, Revision H, dated April 9, 2008.Midcoast Aviation Inc. Airplane Flight Manual Supplements 41-261M002, Revision NC, dated April 09, 2008 and 41-424M001 Revision NC,dated April 9, 2008 or later approved revision. Conditions Restricted to ASN 5701.
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IRIDIUM ANTENNA INSTALLATION AIRCELL ST2100. CERTIFICATION BASIS LIMITATIONS INSTRUCTION FOR...

Iridium Antenna Installation Aircell ST2100. Certification Basis Limitations Instruction for Continued Airworthiness.JBSL Doc. No. BCL6153301-150-01. Conditions Reg.: ZS-SGC S/N: 5070
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INSTALLATION OF PASSENGER OXYGEN SYSTEM. CERTIFICATION BASIS LIMITATIONS MIDCOAST AVIATION...

Installation of Passenger Oxygen System. Certification Basis Limitations Midcoast Aviation Certification Drawing List 34-261G001 Revision B dated March 15, 1999, or Conditions This STC must be installed with Cabin interior arrangement per EASA STC No. EASA.IM.A.S.02745 and an emergency lightingper EASA STC. No. IM.A.S.02743 or other approved interior arrangement and emergency lighting system.
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CABIN INTERIOR ARRANGEMENT. CERTIFICATION BASIS LIMITATIONS MIDCOAST AVIATION CERTIFICATION DRAWING...

Cabin Interior Arrangement. Certification Basis Limitations Midcoast Aviation Certification Drawing List 34-299G001, Revision D, dated 18 March 1999, or later approved revision. Conditions This STC must be installed concurrent with an emergency lighting system per EASA STC No. EASA.IM.A.S.02743 and an oxygen system perEASA.IM.A.S.02744 or other approved emergency lighting and oxygen system.
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INSTALLATION OF EMERGENCY LIGHTING SYSTEM. CERTIFICATION BASIS LIMITATIONS MIDCOAST AVIATION...

Installation of Emergency Lighting System. Certification Basis Limitations Midcoast Aviation Certification Drawing List 34-415-G001 Revision E dated March 20, 1999 or later approved revisions. Conditions This STC must be installed with Cabin interior arrangement per EASA STC No. EASA.IM.A.S.02745 and an oxygen system per EASA STC EASA.IM.A.S.02744 or other approved interior arrangement and oxugen system.
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WIRELESS LAN (WLAN) ACTIVATION CERTIFICATION BASIS LIMITATIONS MASTER DRAWING LIST...

Wireless LAN (WLAN) Activation Certification Basis Limitations Master Drawing List BGLF523261-001 Rev. AAFMS BGLF523261-201-01 Rev. IR Conditions
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W-LAN ACTIVATION.BY INSTALLING:A SWIVEL DIPOLE ANTENNA IN THE CABIN, A...

W-LAN Activation.By installing:A swivel dipole antenna in the cabin, a WLAN ON/OFF switch and new wiring between the router, antenna and the HD-710. Certification Basis Limitations # Declaration of Compliance, Doc. No. BGLEX23261.# Master Data List, Doc. No. BGLEX23261-001, Rev. A or latest approved revision.# AFMS, Doc. No. BGLEX23261- 201-01, Rev. IR or latest approved revision. Conditions Prior to installation of this modification the installer must ...
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INSTALLATION OF BULKHEADS AND DOOR IN THE MID CABIN. CERTIFICATION...

Installation of bulkheads and door in the mid cabin. Certification Basis Limitations Flight Manual Supplement doc no. GVCES002-201-02. Conditions 1. S/N: 669.2. Prior to installation of this modification the installer must determine that the interrelationshipbetween this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness (...)
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EHS INTEGRATION INTO AIRCRAFT.BY UPGRADING BOTH EXISTING RCZ-833E TO RCZ-833K...

EHS integration into Aircraft.By upgrading both existing RCZ-833E to RCZ-833K and integrated Mode S Transponder Module XS- 852A to XS-852F, with the Honeywell Service Bulletin No. 7510700-23-6046. Certification Basis Limitations Master Data List, Doc. MDL-055, Rev. IR or latest approved Revision.Flight Manual Supplement, Doc. No. FMS-028, Rev. IRor latest approved revision.Instruction for Continued Airworthiness, Doc. No. ICA-021, Rev. IR or latest approved revision. Conditions Ref.: \-\ ...
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SOFTWARE UPGRADE TO 218-218 OF THE HONEYWELL MK-V ENHANCED GROUND...

Software upgrade to 218-218 of the Honeywell MK-V Enhanced Ground Proximity Warning System to support Runway Awareness & Advisory System (RAAS). Certification Basis Limitations FAA STC ST01318WI-D, dated 11 April 2005.Midcoast Master Data List No. 34- 327G004 Revision N/C dated 11 April 2005 or later approved revision. Conditions Prerequisite: MK V EGPWS must be installed per Bombardier Service Bulletin 604-34-020 or 604-34-025.
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ADDITION OF RUNWAY AWARENESS & ADVISORY SYSTEM-RAAS TO HONEYWELL MK-V...

Addition of Runway Awareness & Advisory System-RAAS to Honeywell MK-V & MK-VII Enhanced Ground Proximity Warning System- EGPWS Certification Basis Limitations FAA STC ST01319WI-D dated April 22 2005.Midcoast Aviation Master Data List No. 34-327G003 Revision N/C dated April 22 2005 or later approved revision. Conditions 1. Prerequisite: MK V or MK VII EGPWS must be installed at Software Level - 218-218 or greater.2. Prior to installation ...
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ACTIVATION OF RAAS ON MK-V OR MK-VII EGPWS WITH SOFTWAREVERSION...

Activation of RAAS on MK-V or MK-VII EGPWS with Softwareversion -218-218 or higher up to -226-226 Limitations: S/N 21824 as initial installationSTC Valid for B727-200 Series with EGPWS MK-V or MK- VII with Softwareversion -218-218 or higher up to -226-226. Conditions: n/a
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MK-V EGPWS UPGRADE. CERTIFICATION BASIS LIMITATIONS # MASTER DATA LIST...

MK-V EGPWS upgrade. Certification Basis Limitations # Master Data List Doc No: BFA5034462- 001.# AFMS Doc No: BFA5034462-201-01. Conditions 1. Required Avionics Configuration:# Collins ProLine II# Collins EFIS 84/85/86# Collins WXP 8502. This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description". Co (...)
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INSTALLATION OF UNIVERSAL UNS-1K+ CERTIFICATION BASIS LIMITATIONS AFM SUPPLEMENT REPORT...

Installation of Universal UNS-1K+ Certification Basis Limitations AFM Supplement Report 2005-35-8, Rev. C or later EASA approved revision Conditions Instructions for Continued Airworthiness, Doc. No. 2005-35-10 Rev. B
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CAIR TM SYSTEM INSTALLATION LIMITATIONS: THE AIRCRAFT MAXIMUM NUMBER OF...

CAIR TM System Installation Limitations: The aircraft maximum number of passengers is reduced by 7 (seven) passengers.. Conditions: n/a
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INSTALLATION OF UNIVERSAL TAWS AND MFD 640 CERTIFICATION BASIS LIMITATIONS...

Installation of Universal TAWS and MFD 640 Certification Basis Limitations AFM Supplement Beechcraft 1900 and Series with Universal TAWSand MFD 640, Report 2005-36-8, Rev. B, or later approved revision Conditions
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INSTALLATION OF BLUESKY C-1000 SATCOM CERTIFICATION BASIS LIMITATIONS JET AVIATION...

Installation of Bluesky C-1000 SATCOM Certification Basis Limitations Jet Aviation Modification 2004-7 Revision A dated November 14, 2005 or alter approved revision Conditions --
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WEATHER RADAR INSTALLATION CERTIFICATION BASIS LIMITATIONS DECLARATION OF COMPLIANCE PROJECT...

Weather Radar Installation Certification Basis Limitations Declaration of Compliance Project BTAAI008Master Data List BTAAI008-001 Conditions --
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INSTALLATION OF UNIVERSAL UNILINK UL-601 CERTIFICATION BASIS LIMITATIONS ENGINEERING ORDER,...

Installation of Universal Unilink UL-601 Certification Basis Limitations Engineering Order, Report 2005-5 dated 16 February 2005, Rev. B or later EASA approved RevisionsAirlpane Flight Manual Supplement, Report 2005-5-8, dated 09 March 2006 Rev. B or later EASA approved RevisionsInstruction for Continued Airworthiness, Maintenance Manual Supplement Rep. 2005-5-10 Conditions Certification Basis:FAR Part 25, TGL Leaflet No. 15 and 16
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INSTALLATION OF A HONEYWELL MK VII EGPWS CERTIFICATION BASIS LIMITATIONS...

Installation of a Honeywell MK VII EGPWS Certification Basis Limitations Master Data List Doc. No.BFA5034461- 001AFM Supplement Doc.No.BFA5034461- 201-01 Conditions none
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INSTALLATION OF HONEYWELL EGPWS MARK VIII CERTIFICATION BASIS LIMITATIONS AIRPLANE...

Installation of Honeywell EGPWS Mark VIII Certification Basis Limitations Airplane Flight Manual Supplement Cessna C560 Citation V with Honeywell EGPWS Mark VIII, Revision A dated 23.02.2004 or later approved Revision, Jet Aviation Doc.No.2003-4-8Aircraft Maintenance Manual Supplement Jet Aviation Doc. No. 2003-4-10, Rev.A Conditions
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INSTALLATION OF FLIGHT DATA RECORDER F1000 CERTIFICATION BASIS LIMITATIONS -ENGINEERING...

Installation of Flight Data Recorder F1000 Certification Basis Limitations -Engineering Order 2003-8, Rev B or later EASA approved revisions Conditions
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FLIGHT MANAGEMENT SYSTEM (FMS) UPGRADE & TERRAIN AWARENESS WARNING SYSTEM...

Flight Management System (FMS) Upgrade & Terrain Awareness Warning System (TAWS) Installation Certification Basis Limitations Jet Aviation Master Data List Document Number BOHET004-001 Rev B dated July 14 2005 or later approved revisionJet Aviaiton AFM Supplement BOHET004-201-01 Rev B & BOHET004-201-04 Rev B or later approved revisions Conditions This STC is approved only for the product configuration as defined in the approved design data referred to ...
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ACTIVATION OF THE RUNWAY AWARENESS AND ADVISORY SYSTEM (RAAS). CERTIFICATION...

Activation of the Runway Awareness and Advisory System (RAAS). Certification Basis Limitations Master Data List Doc No BLJ3134461- 001FOCA approved AFM SupplementDocument No BLJ3134461-201- 01 Rev IR Conditions 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.
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INSTALLATION OF THE HONEYWELL MK VII ENHANCED GROUND PROXIMITY WARNING...

Installation of the Honeywell MK VII Enhanced Ground Proximity Warning System (EGPWS) in accordance with Jet Aviation Master Drawing List (MDL) F20-20311-010, Revision IR, Dated May 21, 2004, or later FAA approved revision.
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INSTALLATION OF A HONEYWELL MODEL MK VIII ENHANCED GROUND PROXIMITY...

Installation of a Honeywell Model MK VIII Enhanced Ground Proximity Warning System (EGPWS)
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INSTALLATION OF A COLLINS ADC-87A AIR DATA COMPUTER (ADC) AND...

Installation of a Collins ADC-87A Air Data Computer (ADC) and an Innovative Solutions & Support (IS&S) Air Data Display Unit (ADDU) and an optional Stand-by Altimeter.
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UPGRADE OF ALLIEDSIGNAL GNS-X FMS SYSTEM TO BECOME A CDU-XLS...

Upgrade of AlliedSignal GNS-X FMS system to become a CDU-XLS FMS system for the purpose of GPS navigation and reception of additional long range INS data.
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PERMANENT CHANGE IN SEATING CAPACITY FROM A MAXIMUM OF 10...

Permanent change in seating capacity from a maximum of 10 passengers to a maximum of 8 passengers.
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INSTALLATION OF A SUNDSTRAND MARK VII GROUND PROXIMITY WARNING SYSTEM(GPWS)...

Installation of a Sundstrand Mark VII ground proximity warning system(GPWS) without windshear software.
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INSTALLATION OF A COLLINS ALT-55 RADIO ALTIMETER SYSTEM AND KOLLSMAN/TDC...

Installation of a Collins ALT-55 radio altimeter system and Kollsman/TDC Type 522 servo altimeter, radio barometric system with type995 radio altimeter converter with voice terrain advisories.
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