MODIFICATIONS OF PMV Engineering (45)

TRANSMITTING PORTABLE ELECTRONIC DEVICES (T-PED) TOLERANCE B777

After TPED tolerance STCs for the use of Wifi aboard A320, B737, and ATR -600 family aircraft, PMVE has completed its TPED STC collection with B777 models. This last EASA STC (ref. 10061590) is aligned with the latest EASA requirements and Eurocae/RTCA standards and allow gate to gate operation (including all phases of flight without restrictions) for the airlines. 
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TRANSMITTING PORTABLE ELECTRONIC DEVICES (T-PED) TOLERANCE ATR42 AND ATR72

PMV Engineering (EASA DOA 21J.487) achieved TPED tolerance demonstration for ATR42 and ATR72 aircraft, thus allowing the installation of wireless IFE and the use of wireless devices for all phases of flight (including take off and landing in all weather conditions). 
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TPED TOLERANCE DEMONSTRATION ON B737 AIRCRAFT

EASA STC for TPED (Transmitting Portable Electronic Devices) tolerance demonstration on the following B737 aircraft: 737-600 737-700 737-800 737-900 737-900ER  
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TCAS 7.1 UPGRADE FOR B737 (ALL SERIES)

PMV Engineering received FAA STC ST0376NY approval for its TCAS 7.1 upgrade STC using the EASA-FAA bilateral agreement. 
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DUAL CMA9000 FMS INSTALLATION ON AIRBUS A300-600

PMV Engineering avionics team brings a huge project to success with the EASA STC for the Installation of a dual FMS CMA-9000 on A300-600 aircraft . This STC is the result of a close cooperation with Esterline CMC Electronics and the operator over the last 10 months. PMV Engineering demonstrated its ability to drive this project, including full flight simulator sessions and flight testing with EASA ...
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INSTALLATION TECHTEST SURVIVAL ELT ON AIRBUS A320 FAMILY

PMV Engineering received an EASA STC certificate for the installation of a TECHTEST survival ELT on Airbus A320 family aircraft.  This STC deals with the latest EASA requirements for embodiment of non-rechargeable Lithium Batteries, e.g compliance with ETSO C142A associated with a risk assessment at aircraft level in order to substantiate that a thermal runaway of the Lithium battery included in the ELT would not impair ...
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VIRTUAL WINDOW

Travelling on board of an Aircraft without seating next to a window is a known frustration that many passengers are suffering. This is even reinforced for the VIP passenger having booked a “mini suite” seat position in the center cabin. PMV Groupe and LATECOERE LATvision™ have jointly worked out a solution providing a “virtual window” easy to integrate in any type of seat.
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NEW HEADSET CERTIFICATION – CVR ANALYSIS

New cockpit  headsets: to comply with CS 25.1301 and CS 25.1457, new cockpit headset installation has to be covered by CVR analysis. VR²C and PMV Engineering provide this kind of analysis in the frame of an EASA approved minor modification (through SB).
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TRANSMITTING PORTABLE ELECTRONIC DEVICES (T-PED) TOLERANCE

PMV Engineering is proud to announce its new EASA STC ref. 10058429 related to «  TPED tolerance on A320 family  ». It currently covers more than 100 aircraft equipment lists (A319/A320/A321) and will significantly ease your life if you intend to use Wifi in cockpit and cabin environments. Partnering with Adcisse, PMVE developed its own software-driven methodology to reduce the number of vacations necessary to cover aircraft ...
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ACTIVATION OF TRUENORTH GSM SYSTEM ONBOARD ,,THE MODIFICATION CONSISTS IN:-...

Activation of TrueNorth GSM system onboard ,,The modification consists in:- Installation of GSM Base Station (BTS) on fwd RH cargo rack-Activation of the systemRefer to doc Certification Investigation Report (CIR) ref.SCA-00330-CIR-R03. Prior to this modification the installation of thefull provision...
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B767 CABIN INTERIOR CHANGE AND IN-FLIGHT ENTERTAINMENT (IFE) SYSTEMINSTALLATIONTHE MODIFICATION...

B767 Cabin interior change and In-Flight Entertainment (IFE) systeminstallationThe modification consists in the reconfiguration of the cabin from a twoclass 221 PAX (30 B/C + 191 Y/C) to a three class 197 PAX (3F/C + 30 B/C+ 164 Y/C), together with the installation of an IMS/Zodiac InflightInnovatio...
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TCAS 7.1 UPGRADE ON AIRBUS A340.THE MODIFICATION CONSISTS IN SOFTWARE...

TCAS 7.1 upgrade on Airbus A340.The modification consists in software modification within the TCAScomputer to cover TCAS7.1 changes.
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MARK II AIRCRAFT COMMUNICATIONS ADDRESSING AND REPORTING SYSTEM (ACARS)INSTALLATION ON...

Mark II Aircraft Communications Addressing and Reporting System (ACARS)installation on B737-600/-700/-800/-900.
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ELECTRONIC FLIGHT BAG (EFB) CLASS 2 INSTALLATION ON BOEING 767THIS...

Electronic Flight Bag (EFB) class 2 installation on Boeing 767This modification deals with the installation of a dual (Captain andFirst Officer) class 2 Electronic Flight Bag (EFB) system from CMCEsterline, on Boeing B767 Aircraft. For each side, this system iscomposed of a mount arm located on wind...
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ELECTRONIC FLIGHT BAG (EFB) CLASS 2 INSTALLATION ON BOEING 757-200THIS...

Electronic Flight Bag (EFB) class 2 installation on Boeing 757-200This modification deals with the installation of a dual (Captain andFirst Officer) class 2 Electronic Flight Bag (EFB) system from CMCEsterline, on Boeing B757 Aircraft. Foreach side, this system iscomposed of a mount arm located onU...
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IN-FLIGHT ENTERTAINMENT SYSTEM INSTALLATION ON BOEING 757-200THIS STC CHANGES THE...

In-Flight Entertainment System Installation on Boeing 757-200This STC changes the cabin lay-out (introduction of new seats and newLOPA), and installs an IFE System, developed by the IMS Company, withindividual displays incorporated to the new seats.Notes:1-,,This STC constitutes an AMOC to AD 2007-1...
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IN-FLIGHT ENTERTAINMENT SYSTEM INSTALLATION ON A330.THIS STC INSTALLS IFE SYSTEM,...

In-Flight Entertainment System Installation on A330.This STC installs IFE System, developed by the IMS Company. Limitations: Certification Investigation Report, ref : SCA- 00210-CIR Revision 5,dated 29 August 2013;Instruction for Continued Airworthiness, ref : SCA-00210-ICA, dated 16May 2013;or later revisions of the above listed documents approved by EASA. Conditions: 1-,,The IFE system installation, defined in this STC, is only valid for a seat configuration identical to the ...
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BOEING-CMC CLASS 3 EFB SYSTEM OPERATING SYSTEM INSTALLATIONON B737NG. LIMITATIONS:...

Boeing-CMC Class 3 EFB system Operating System installationon B737NG. Limitations: Certification Investigation Report AVI-00450- CIR Rev.00;Instructions for continued airworthiness AVI-00450-ICA Rev.00;or later revisions of the above listed documents approved by EASA. Conditions: The installation of an EFB according to certificate 10044973 or10045157 is a prerequisite for the installation of the above- mentioned Operating System. Prior to installation of this design change it must be determined that ...
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INSTALLATION OF PROVISIONS FOR THE USE OF EFB LIMITATIONS: N/A....

Installation of provisions for the use of EFB Limitations: n/a. Conditions: n/a
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INSTALLATION OF PROVISIONS FOR THE USE OF EFB LIMITATIONS: N/A....

Installation of provisions for the use of EFB Limitations: n/a. Conditions: n/a
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