AIRCRAFT GENERAL (ATA 5-18) MODIFICATIONS (501)

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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AED installation

The use of automated external defibrillators (AED) is essential to increase the chances of survival in case of a cardiac arrythmias such as ventricular fibrillation (VF) and non-perfusing ventricular tachycardia (VT) when used in the first 10 minutes.

AMC1 CAT.IDE.A.220 (b) (4) stipulates that the aircraft operators should carry automated external defibrillator (AED) on board all aircraft equipped with a first-aid kit and required to carry at least one cabin crew.

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BAM 350 Eagle Eye, Maritime Surveillance Aircraft

Estonia is the first country to get the new MSS 7000 system, after operating the MSS 6000 for more than 10 years. The new MSS 7000 system for Estonia has installed on board a new Beech King Air 350ER aircraft.

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Underwater Locator Device - ULD - Fokker Services

Events related to aircraft missing over oceanic areas have led to several new requirements, amongst which is the introduction of a long-range Underwater Locator Device (ULD).

The ULD low frequency (8.8kHz) technology is used to increase the range at which aircraft submerged wreckage can be located.

It will be mounted on the aircraft structure free of sound absorbent materials and not in wing sections or empennage. The installation is in accordance with ARINC specification 667, which describes the removal, installation and maintenance aspects of an ULD installation.

Note that the ULD is not to be confused with the Underwater Locator Beacons (ULB) as installed on the CVR and FDRs. The ULD is complementary to the ULB and is mounted to the aircraft structure.

ICAO states that by January 1st 2018 aircrafts flying long range over water with a MTOW>27.000 kg must be equipped with an ULD. Long range over water is determined by the exceedance of the distance from a suitable emergency landing spot. The distance corresponds to 120 min at cruise speed or 400NM whichever is the lesser.

EASA states that by January 1st 2019 Passenger aircraft flying long range over water with a MTOW>27.000 kg and cargo aircraft with MTOW > 45.500kg must be equipped with an ULD. Long range over water is determined by a distance >180 NM from shore.

CARS 121 MOS 11.64 states that aircraft with a MTOW>27.000 kg carrying a life raft should have an ULD by December 2, 2023.

Other authorities have accepted similar rules.

Contact Fokker Services for other aircaft types.

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SBAS / GNSS Aircraft Integration by Fokker Services

Global Navigation Satellite System (GNSS) refers to a constellation of satellites providing signals from space that transmit positioning and timing data to GNSS receivers. The receivers then use this data to determine position, altitude, time, and velocity. This performance can be improved by regional satellite-based augmentation systems (SBAS).

SBAS improves the accuracy and reliability of GPS information by correcting signal measurement errors and by providing information about the integrity of its signals.  SBAS is essential for applications where accuracy and integrity are critical. SBAS is a key enabler of Performance Based Navigation (PBN) usage for Automatic Dependent Surveillance-Broadcast (ADS-B) and Localizer Performance with Vertical Guidance (LPV).

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LED Logo Light to replace Halogen based logo lights

Talon Aerospace LED logo light Assemblies to replace Halogen  replacement.

Do you recognize the following problems with your existing logo lights?

  • Halogen bulbs are replaced frequently
  • Lights are installed in difficult to reach areas and requires use of cherrypicker or lift
  • Lens sealant does not have sufficient time to dry, leading to moisture ingress within horizontal stabilizer
  • Transformer requires frequent replacement
  • Incandescent bulb color temperature changes appearance of corporate logo

Get Light-Years ahead of your competition!

Talon Aerospace LED logo light assemblies are designed to allow for plug and play replacement for the existing HLX64621 halogen bulb based logo lights. Talon uses a rack to replace the OEM logo light housing. The LED module and transformer assembly are mounted to the rack. The OEM aircraft connector is mounted on the transformer assembly, making the LED logo light assembly plug and play.

The lens, lens gasket and hardware can be retained from the OEM unit, but Talon does make replacement lenses available for most applications. The Talon logo light assemblies operate on 115VAC 400Hz aircraft power. A transformer within the assembly steps the voltage down to 14V to power the LED module. All internal connectors are circular mil-spec connectors.

 Approved Model List:

  • Airbus A320
  • Airbus A330
  • Airbus A340
  • Boeing B737NG
  • Boeing 757
  • Boeing 777

 Planned for Approval:

  • Embraer Embraer E170, Embraer E175, Embraer E190, Embraer E195

Talon and Proponent

Proponent is the exclusive global distributor of all Talon Aerospace products.
This relation provides customers with the latest generation of LED lights.

Proponent

Proponent is the new identity representing Kapco Global and Avio-Diepen as one united company, and the unique capabilities that the new organization brings to the aerospace market. With extensive experience in supporting the MRO, OEM and airline markets, our organization offers innovative inventory and supply chain management solutions to OEM and aftermarket customers.

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Transmitting Portable Electronic Devices (T-PED) Tolerance on B777

After TPED tolerance STCs for the use of Wifi aboard A320 family, B737, and ATR 42 / 72 aircrafts, PMV Engineering 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 on ATR42 - 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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Installation of Sliding Seat Mechanism for Pilatus PC-12

This is is a modification for the seat adapter system to the seat rail. During flight the seat can be unlocked and moved from its certified taxi, take-off and landing position and repositioned in increments of 1 inch as desired by the passenger.  

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