Szkoda, że generał Andrzej Błasik nie 'jarał fajki' w wypasionym kiblu TU154M PLF101 (napewno zadziałał by czujnik dymu jak w POLSKIM BUSIE !

http://albatros.salon24.pl/503836,acarsd-tu-154m-plf-101-10-04-2010

a pił tylko dla kurażu jedynie "małpki" - taki był zestresowany lotem samolotem TU154M PLF101 - Dowódca Wojsk Lotniczych !

A tak na SERIO !

&&&

Gdzie jest zapis trajektorii lotu TU154M PLF101 w dniu 10 kwietnia 2010  przechowywany na DYSKACH KOMPUTERA PANSA w III Rzeczpospolitej:

i inne ZAPISY dla celów dowodowych i procesowych lotów do Smoleńska w dniu 7, 9 i 10 kwietnia 2010 roku a i także w EUROCONTROL pod Paryżem.

Urządzenie:

Transponder ADS-B wg podpisanej przez RP Konwencji ICAO temu służy.

Nie ma TUTAJ "zmiłuj się", że wcięło.

Bo albo jest zapis albo takowego LOTU TU154M PLF 101 w tym właśnie kierunku w dniu 10 kwietnia 2010 roku PO PROSTU NIE BYŁO.

Był lot dwóch JAK-ów 40 z 36 PLT i jeden lot Boeinga 737 LOT "czarter" o godzinie 05:52 UTC do Mińska i dalej do Moskwy bez jakiejkolwiek katastrofy lotniczej. Stąd loty wojskowo-cywilne !

Dobitnie pokazuje to premier FR PUTIN na konferencji rządowej z udziałem ambasadora RP Bahra i minister Kopacz na Kremlu w dniu 13 kwietnia 2010 roku.

"Pagibli Ci, którzy mieli zginąć". Głownie z Rodziny Katyńskiej.

Samolot ten z rejestru łotewskiego został przerejestrowany w dniu 12 kwietnia 2010 po oblocie technicznym przez Agencję Żeglugi Powietrznej PANSA na EPWA Okęciu na rejestrację polską.

Pisałem o tym !

Inna HISTORIA przypisana jest dla TU154M PLF101.

Tak naprawdę od wizyty w Pradze pod wieczór 8 kwietnia 2010 roku: LOTY SAMOLOTU TU154M PLF101 SĄ NIEZNANE. CZYŻBY "CZESKA DZIUPLA" LOTNISKO WOJSKOWE POD PRAGĄ "KBELY" - DO LISTOPADA 2010 ROKU? UDZIAŁ CZECHÓW SIĘ POWTARZA JAK W GIBRALTARZE 4 lipca 1943 roku. I WTEDY BYŁY OFIARY: GENERAŁ SIKORSKI PREMIER RZĄDU I NACZELNY WÓDZ NA UCHODŹCTWIE? ANGLICY NA KOLEJNE 50 LAT UKRYLI DOKUMENTY ! CZY TAK BĘDZIE I TYM RAZEM ?

ZA CO ? -ZA KRESY POLSKIE I OFIARY KATYNIA. TERAZ PODOBNIE NAWET PO 70 LATACH OD TAMTYCH WYDARZEŃ !

·  24th Air Transportation Base at Prague - Kbely | Ministry of ...

www.army.cz › ... › Units › Air Force

Tłumaczenie strony

The Air Transportation Base located at Prague-Kbely is used for air transport of ... Theairport is located 11 kilometres from Prague's downtown in course of 072 ...

·  Kbely Air Base Airport (LKKB) - World Airport Codes

https://www.world-airport-codes.com/.../kbely-air-ba...

Tłumaczenie strony

Radisson Blu Alcron Hotel, Prague. 5.95 miles away from airport. Longin Center, Prague - Marriott Executive Apartments Visit Site ...

To stamtąd wyszła informacja o zagrożeniu terrorystycznym !

&&&

TU154M PLF101 był wyposażony w transponder TRA-67A Mode S

·  TRA-67A Mode S Transponder Features, Specs, Price, and ...

www.sea-avionics.com/lc/cart.php?...TRA-67A

Tłumaczenie strony

Serve as an integral part of the CAS-81 Collision Avoidance System; The TRA-67AEnhanced ATC Transponder is designed to meet the above requirements ...

·  [PDF]TRA-67A ATC Transponder Configurations

www.seaerospace.com/documents/tra67a_pn.pdf

Tłumaczenie strony

TRA-67A ATC Transponder Configurations. FEATURES. Honeywell. Part Number. Basic. Unit. Foreign. Approval. JTSO. Approval. TCAS. Compat. Boeing. CMC.

·  [PDF]SP13_Honeywell ADS-B Seminar 130415 - ICAO

www.icao.int/.../SP13_Honeywell%20ADS-B%20Se...

Tłumaczenie strony

15.04.2013 - Transponder (DO-260) used ... Honeywell TRA-67A Mode S Transponders have been ... In Development: Primus Apex TRA 67 MST 67A.

·  [PDF]CAS 100 System - Honeywell

www51.honeywell.com/.../TCAS_DATASHEET.pdf

Tłumaczenie strony

TRA-67A Enhanced Mode S Transponder. Power. Requirements. Per ARINC 413A. Power Input. 115 VAC, 400 Hertz. 60 Watts Max Dissipation. Transmitter RF.

·  TRA 67 and TRA 100 Transponder - Honeywell Aerospace

https://aerospace.honeywell.com/.../smarttraffic-traffi...

Tłumaczenie strony

TRA 67 and TRA 100 Transponder. This air transport Mode S Transponder provides the data capability that identifies the aircraft to other surrounding ACAS ...

·  MyAerospace Catalog System Display-Mode S Transponders

https://commerce.honeywell.com/.../eSystemDisplay?...

Tłumaczenie strony

The TRA-67A Mode S ATC Transponder provides standard TCAS/ACAS data link functionality with growth provisions necessary to meet existing and anticipated ...

·  Service Bulletin: Navigation : TRA-67A Mode S Transponder ...

books.google.com/books/.../Service_Bulletin.html?id... - Tłumaczenie strony

books.google.comhttp://books.google.com/books/about/Service_Bulletin.html?id=ywARMwEACAAJ&utm_source=gb-gplus-shareService Bulletin Service ...

http://www.icao.int/APAC/Meetings/2013_ADS_B_SITF12/SP13_Honeywell%20ADS-B%20Seminar%20130415.pdf

Automatic Dependent Automatic Dependent Surveillance – Broadcast (ADS-B) Sunny Kancharla Customer Business Leader, Aerospace – India 1 Honeywell Confidential Honeywell Proprietary 2013 ICAO ADS-B Update Semina r April 15, 2013 Æ Honeywell.com Honeywell and ADS Honeywell and ADS - B • Honeywell has been developing ADS Honeywell has been developing ADS -B enabled avionics for B enabled avionics for several years. • A number of ADS-B In and Out products are currently in operation in virtually all segments of aviation – General Aviation General Aviation – Corporate Aviation – Regional Transport – Air Transport – Military Transport • Honeywell is proud to support new ADS-B capabilities that will offer clear benefits to our customers and help the world’s airspace l i t ffi i t d f i t f i ti 2 Honeywell Proprietary 2013 evolve in to a more effi cien t an d sa fer environmen t for aviation. Æ Honeywell.com What’s Been Done? What’s Been Done? ADS-B Based Surveillance and Data Link for Autopilot Honeywell Bendix King KT- 73 M d S P l M t and Data Link for Autopilot Coupled station keeping provided by Honeywell MILACAS-FR 73 Mode S Panel Mount Transponder (DO-260) used in Air Services Australia ADS B Trials MILACAS FR. Military is an excellent first adopter and proving ground f d di li ti ADS-B Trials Honeywell TRA-67A Mode S Transponders have been capable of DO 260 1090ES for several years Shipping on for demanding applications which can transition to civil sector when appropriate Traffic Computer infrastructure (ground and air) capable of DO-260 1090ES for several years. Shipping on virtually all Air Transport Types. infrastructure (ground and air) in place. Traffic Computer Honeywell certified Traffic Computer with SmartTraffic™ for use by Airbus for integration of Airborne Traffic AZA557 +10↓ AFR6512 +10↓ AZA557 +10↓ AFR6512 +10↓ for integration of Airborne Traffic Situational Awareness (ATSAW) applications like In Trail Procedure in non-oceanic airspace 3 Honeywell Proprietary 2013 oceanic airspace. Æ Honeywell.com What Are We Doing for ADS What Are We Doing for ADS -B Out? ADS-B OUT Avionics Equipage transitions to DO-260B Honeywell is modifying the following Mode S Transponders to transmit DO-260B, US NPRM com pliant ADS-B Out • TSO Received : Primus II &Primus EPIC • In Development: Primus Apex TRA In Development: Primus Apex TRA -67 MST 67A 67 MST 67A 4 Honeywell Proprietary 2013 Æ Honeywell.com ADS-B Out Product Planning B Out Product Planning Product Product Application Application DO-260 DO-260A DO-260B AESU (A380) Air Transport -- Available Available TRA 67A Air Transport Available Replace with TRA-67A Air Transport Available -- p TRA-100B TRA-100B Air Transport - - TSO 1Q15 Epic Regional, Helicopter -- Available Available Business Aviation Primus II Regional Business Aviation -- -- Available Ri l R l ith MST-67 Regional Business Aviation -- -- Replace with MST 100B MST 100B Regional Business Aviation _ _ TSO 1Q15 APEX Business Aviation General Aviation -- -- TSO 4Q13 5 Honeywell Proprietary 2013 Æ Honeywell.com Traffic/Aircraft Collision Avoidance System Traffic/Aircraft Collision Avoidance System Traffic Selectors ADS-B Traffic from Traffic Computer on Navigation display Additional information from Traffic Computer on MCDU SmartTraffic ™ - Foundation for Honeywell’s ADS -B enabled Hybrid 6 Honeywell Proprietary 2013 SmartTraffic - Foundation for Honeywell s ADS - B enabled Hybrid Surveillance and Airborne Traffic Situational Awareness (ATSAW) Æ Honeywell.com SmartTrafficTM for TCAS Traffic Computer for TCAS Traffic Computer Airborne Traffic Situational Awareness (ATSA-AIRB) Enhanced Visual Separation on Approach (ATSA-VSA) In-Trail Procedures in Oceanic Awareness (ATSA AIRB) on Approach (ATSA VSA) Airspace (ATSA Airspace (ATSA-ITP) -20È +10 +09 IBE7274 355 M • Better situational awareness relative to preceding aircraft. • ICAO & FAA* recognized procedure Ai it i t • Position, Orientation, Relative Altitude, Vertical Tendency Ai ft ID G d S d • Runway capacity improvement • Airspace capacity improvement • Fuel burn reduction through transoceanic flight routing Honeywell is first to certify ATSAW; Software only upgrade solution • Aircraft ID, Ground Speed, Wake Vortex (when traffic selected) 7 Honeywell Proprietary 2013 Honeywell is first to certify ATSAW; Software only upgrade solution http://www.honeywell.com/SmartTraffic Æ Honeywell.com Motivation for ADS Motivation for ADS-B In-Trail Procedures (ITP) Trail Procedures (ITP) D i d Altit d FL360 FL350 Desired Altitude St d d S ti FL340 Standard Separation NEED CHALLENGE OPPORTUNITIES = 4 The combination of locally dense traffic and large separation 4 Use airborne ADS-B applications to enable altitude changes 4 Altitude Changes required for better fuel economy winds and large separation minima limits altitude changes altitude changes otherwise blocked by conventional operations fuel economy, winds, and ride quality 8 Honeywell Proprietary 2013 Source: FAA Æ Honeywell.com Cockp py ( ) it Display of Traffic Information (CDTI)* – In Trail Procedures (ITP) ITP request formulation based on traffic selection based on traffic selection and criteria checks. 9 Honeywell Proprietary 2013 Note: * denotes under development Æ Honeywell.com S tT ffi SmartTraffic™ – CDTI* • Initial functions – (Enhanced) Traffic Situation Awareness (TSA) – (ATSA AIRB) – (Enhanced) Visual Separation on Approach (VSA) – Oceanic In-Trail Procedures (ITP) for Air Transport aircraft – Airport Surface Situation Awareness (ASSA) – (ATSA SURF)* • Platform for future CDTI – Ad d A h A li ti h Advanced Approach Applications such as: • CDTI Assisted Visual Separation (CAVS)* • CDTI-Assisted Pilot Procedures (CAPP)* – Various Interval Management (IM) applications • Flight Deck Interval Management – Spacing (FIM-S)* • Flight Deck Interval Management – Defined Interval (FIM-DI)* • Interval Management - Defined Interval, Oceanic (IMDIO)* – VFR-like Separation in All Weather Conditions or Electronic Flight Rule (EFR)* 10 Honeywell Proprietary 2013 Note: * denotes under development Æ Honeywell.com Runway Occupied Alert Runway Occupied Alert Examples* Examples* C ti Al t 11 Honeywell Proprietary 2013 Caution Aler t Warning Alert Note: * denotes under development Æ Honeywell.com ASSA versus ASSA versus FAROA* ASSA (Airport Surface Situational A ) FAROA (Final Approach and Runway Awareness) Occ panc Occupancy A areness) Awareness) 12 Honeywell Proprietary 2013 Note: * denotes under development Æ Honeywell.com H ll ADS Honeywell ADS-B C bilit Pl i B Capability Planning 2008 2010 2012 2014 2016 2018 Horizon 1 ADS-B Out • Adding ADS-B Out to p p roduction transponders • Hybrid Surveillance Horizon 2 Initial ADS-B In SmartTraffic™ Applications • Enhanced Visual Separation on Approach • AIRB • In Trail Procedure • SURF Hi 3 or zon 3 Advanced ADS-B In Applications • Flight Deck Interval Management Advanced Technology R&D 13 Honeywell Proprietary 2013 • SURF IA Æ Honeywell.com ADS-B In Trail Procedure Operational Evaluation B In Trail Procedure Operational Evaluation • The objective of the program is to d t t t ti l f l i demonstrate potential fuel savings opportunities enabled by the ADS-B In – In Trail Procedure (ITP). • Under an FAA funded program, Honeywell is developing, system integrating, and certifying a complete ITP avionics capability to be STC’d U it d Ai li 747 400 First Officer EFB on United Airlines 747-400s. • The system consists of Honeywell’s TPA 100B Traffic Computer with ADS-B In and ITP bili TRA 6 A T d i h ITP capability, TRA 67A Transponders with ADS-B Out, and a Class 3 EFB running Honeywell ITP display software. ADS-B ITP Enabled Climbs • United Airlines will operate approximately 12 Honeywell ITP avionics equipped 747-400 aircraft in the South Pacific (SOPAC) route f 1 O ti l E l ti Optimal 14 Honeywell Proprietary 2013 for a 1 year Operational Evaluation. Sub-Optimal Cruise Æ Honeywell.com System Concept System Concept Honeywell TPA 100B Traffic Computer Honeywell Type C H ll T ffi Goodrich SmartDisplay® EFB with Honeywell SmartTraffic™ ITP Application Honeywell TRA 67A Mode S ADS-B Out Transponder Honeywell Type C CDTI / ITP Software Honeywell Traffic Computer Goodrich Class 3 EFB ADS-B In In Trail Procedure B In In Trail Procedure SW Goodrich Class 3 EFB Platform (DEOS) 15 Honeywell Proprietary 2013 A429 Display Data Æ Honeywell.com ITP Operational Benefits ITP Operational Benefits • The objective of the In Trail Procedure (ITP) Operational Evaluation The objective of the In Trail Procedure (ITP) Operational Evaluation program is to demonstrate potential positive economic benefit opportunities enabled by ADS-B In. • The Economic Benefit is projected to be realized as follows: – ITP certified aircraft will be able to climb to more efficient altitudes more ITP certified aircraft will be able to climb to more efficient altitudes more often than current separation standards allow thereby saving fuel burn – An ITP certified fleet can save weight and fuel burn by loading and carrying An ITP certified fleet can save weight and fuel burn by loading and carrying less contingency fuel based on the expectation that desirable climbs will be possible more often – The weight savings generated by reductions in contingency fuel can be converted to revenue generating cargo or passengers. 16 Honeywell Proprietary 2013 Æ Honeywell.com Conclusion • Honeywell is committed to supporting ADS-B globally – H d d f ADS Hundreds of ADS-B t d d li d B transponders delivered – More research & development underway – Helping to develop the global standards for ADS-B – Aircraft equipage decisions required for older aircraft • Performance-Based Requirements – Install DO260 equipage for early applications – Align position performance and operational requirements • ADS-B is a relatively simple technology – Varying business cases for operators and ANSPs – Plans must deliver value to all stakeholders throughout the transition Plans must deliver value to all stakeholders throughout the transition – This will accelerate aircraft user adoption and airspace benefits – ADS-B In system complexity still in work with Merging and CDTI implementations 17 Honeywell Proprietary 2013 ADS-B is a Key Building Block for ATM Modernization

6.11.2013 02:00Kategoria: Polityka Odsłon: 942 1 Komentuj

Order Biały - już witał się z gąską Przypadki Koszałka Opałka

ciąg dalszy ...

 

Wyniki wyszukiwania

   

1.      Polish President and wife killed in Tu-154 crash - Page 107 ...

forums.jetphotos.net/showthread.php?t=50144...‎

o    

Tłumaczenie strony

8 gru 2012 - Liczba postów: 20 - ‎Liczba autorów: 7

He thinks that a Transponder Landing System was used. Tu-154 had a TRA 67A-(Mode S) transponder installed.Pic 2 shows what the ATC ...

2.       [PDF]

Technika lotnicza i jej eksploatacja - faktySmolensk.gov.pl

faktysmolensk.gov.pl/przebieg-badania?file=files/pliki/raport/...

s. 8. Wibracja. Skrzynka napędów mm/s. 10. Tylna podpora mm/s. 13 .... stwierdziła, że samolot Tu-154M nr 101 miał wykonane wymagane remonty i obsługi oraz ...... 25) 2 xTransponder TRA-67. ...... The quality seals were not broken, meaning that the TAWS LRU had not been ..... descent mode the vertical extents of the.

3. Wyniki podobnych wyszukiwań

4.     TRA-67A Mode S Transponder - Honeywell Aerospace

www.honeywell.com/.../TCAS3_C4BC908E6-ED12-...‎

o    

o    

Tłumaczenie strony

The TRA-67A Mode S ATC Transponder provides standard TCAS/ACAS data link ...The TRA-67A has demonstrated industry leading reliability and also ...

Więcej wyników dla tu 154 had a tra 67a mode s transponder installed

5.     TRA-67A Mode S Transponder Features, Specs, Price, and Availability

www.sea-avionics.com/.../cart.php?...model=TRA-67...‎

o    

o    

Tłumaczenie strony

TRA-67A. FEATURES.Air Traffic Control (ATC) Mode S Transponder; Remote ... TheTRA-67A ATC Transponder is designed to meet the following requirements: .... Item is not available for over-the-counter(OTC) sale and must be installed by ...

Więcej wyników dla tu 154 had a tra 67a mode s transponder installed

 

 

1.     107 - JetPhotos.Net Forums

forums.jetphotos.net/showthread.php?t=50144&page...‎

o    

Tłumaczenie strony

8 gru 2012 - Liczba postów: 20 - ‎Liczba autorów: 7

Page 107- Polish President and wife killed in Tu-154 crash Aviation Safety DiscussionForum. ... -Manipulating the airplane avionics to deactivate the GA functions ...http://www.youtube.com/watch?v=gbPhN...ture=endscreen ...

 

 

http://forums.jetphotos.net/showthread.php?t=50144&page=107

 

 

http://forums.jetphotos.net/attachment.php?attachmentid=5186&d=1357262445

 

 

 

 

 

 http://www.honeywell.com/sites/aero/TCAS3_C4BC908E6-ED12-48C9-C18D-DF3761231807_

 H90D7FCE8-398A-9300-D426-12FF07625576.htm

 

TRA - 67A Mode S Transponder

The TRA - 67A Mode S ATC Transponder provides standard TCAS/ACAS data link functionality with growth provisions necessary to meet existing and anticipated user requirements for the next ten years. The TRA - 67A has demonstrated industry leading reliability and also expansion capability to incorporate mandated operational capability. The TRA - 67A Mode S transponder is certified to or supports:    RTCA DO 181C and ARINC 718A    TSO for TCAS Change 7 requirements per ARINC 735A and RTCA DO - 185A, including RA downlink reporting and air-to-air RF link protocols    ACAS II regulatory requirements    European Surveillance       Elementary and Enhanced Downlink Aircraft Parameters per ICAO Annex 10 Amendment 77       TSO for Elementary(ELS) & Enhanced(EHS) Surveillance       Boeing and Airbus certification       Honeywell Service Bulletin available for ELS/EHS modifications

 

01-04-2013, 01:24 AM	#2131
Northwester Member   Join Date: Nov 2010 Posts: 772	One of the Russian bloggers discovered this in the FMS data. FMS logged plane's position in relation to VOR and TACAN points that is different from the official one. Attached Thumbnails

 

 

 

01-05-2013, 01:05 AM

#2132

Jonathan_Creek Junior Member   Join Date: May 2010 Posts: 31

' alt=Default class=inlineimg border=0 title=Default v:shapes="_x0000_i1032">   Quote: Originally Posted by Northwester  alt="View Post" class=inlineimg title="View Post" v:shapes="_x0000_i1034"> One of the Russian bloggers discovered this in the FMS data. FMS logged plane's position in relation to VOR and TACAN points that is different from the official one. This "discovery" is at least 12 months old. I do not understand the meaning of it, or what you imply in your post, but I would like to point to a full FMS Data Extraction report published in the Appendix #4 to the official Polish report.  Full document is available here http://mswia.datacenter-poland.pl/pr...sploatacja.pdf FMS extraction report starts on page 644, all in English.  I noticed the following paragraph right above Table 3-10 you quoted: "An RRS was configured on ARINC input port 3. The RRS contains DME, VOR, and TACAN receivers. The DME, VOR, and TACAN receivers were operational, but no stations were in range" I do not understand any of it therefore I provided the link to full FMS report.  Live and learn. Attached Thumbnails

 

 

01-05-2013, 03:07 AM	#2133
Northwester Member   Join Date: Nov 2010 Posts: 772	Quote: Originally Posted by Jonathan_Creek  This "discovery" is at least 12 months old. I do not understand the meaning of it, or what you imply in your post, but I would like to point to a full FMS Data Extraction report published in the Appendix #4 to the official Polish report.  Full document is available here http://mswia.datacenter-poland.pl/pr...sploatacja.pdf FMS extraction report starts on page 644, all in English.  I noticed the following paragraph right above Table 3-10 you quoted: "An RRS was configured on ARINC input port 3. The RRS contains DME, VOR, and TACAN receivers. The DME, VOR, and TACAN receivers were operational, but no stations were in range" I do not understand any of it therefore I provided the link to full FMS report.  Live and learn. Yes, it was published long time ago, but so far I have not noticed anyone pointing to this piece of data.  FMS calculated the distance to TACAN and VOR stations based on plane's position and known coordinates of these stations.